N602FE

Part: MSC — FAULTED (PITOT HEAT) · airframe 93,673 hrs · 23,817 cycles

AT FL 370 IN ICING CONDITIONS, RECEIVED A IAS FLAG. HAD AUTOPILOTS DISCONNECT CAPTAINS & FOS AIRSPEEDS SPLIT SIGNIFICANTLY. DECIDED TO DESCEND IN VFR CONDITIONS WHILE RUNNING AIRSPEED UNRELIABLE CHECKLIST. WHILE RUNNING CHECKLIST, CAPTAIN LOOKED LIKE IT WAS THE ONE THAT WAS FAULTY. BEFORE FINISHING CHECKLIST, AIRSPEEDS THEN ALIGNED & OPS NORMAL. COMPLETION OF CHECKLIST HAD AIRPLANE SWITCHED & INDICATIONS BACK TO NORMAL FLT EMERGENCY WAS DECLARED. INSPECTED PITOT TUBES IAW MM 34-11-01-6, ALL FOUND CLEAR. BLOWED PITOT LINES, ALSO CHECKED FOR HEATING. ALL OK. FOUND MSC FAULTING FOR THE 9 PREVIOUS LEGS, R &R MSC IAW MM 31-42-00-0, NO FAULTS FOR MSC. PITOT HEAT NORMAL.

Part: STRUCTURE — CRACKED (RT MLG DOOR) · airframe 93,649 hrs · 23,807 cycles

RH MLG DOOR CRACKED AT TOP HINGE AREA REOVED AND REPLACED DOOR PER AMM MD11 32-14-20-4.

Part: ENGINE — FAILED (NR 2) · airframe 93,121 hrs · 23,667 cycles

ENGINE NR 2 FLAMED OUT DUE TO FUEL STARVATION, CAUSED BY NOT COMPLETING FUEL MANUAL CHECKLIST. NO FAULT STORED IN CFDS RELATED WITH NR 2 ECU. DID NR 2 ECU R-T-S TEST AND PASSED IAW AMM 73-21-05-1. DID NR 2 FUEL BOOST PUMP PRESSURE CHECK AND NO DEFECT FOUND IAW AMM 28-22-01-5. DID NR 2 ENG POST-WINDMILL INSPECTION WITH ENGINE RUN IAW AMM 72-00-05-6-1, NO DEFECT FOUND. ACFT OK FOR SERVICE.

Part: EMER POWER — NO TEST · airframe 92,843 hrs · 23,589 cycles

EMER PWR TST FAIL AFTER TURNING SWITCH TO ARM POSITION. PERFORMED EMERGENCY POWER TEST PER MD11 AMM 24-24-00-5. OPS CHECK GOOD.

Part: CHECK VALVE — MALFUNCTIONED (FUEL SYSTEM) · airframe 92,552 hrs · 23,497 cycles

ENROUTE HNL OVER PHX LVL 2 FUEL QTY/USED CHECK, POSSIBLE FUEL ALERT. DID A FUEL USED SUMMARY AND DETERMINED 3,000 LBS SHORT OF FUEL AND STILL DECREASING . COMPLIED WITH QRH AND ISOLATED ALL TANKS. FUEL STABILIZED 8000# LOW. WE DUMPED 6000# TO LOWER LANDING WEIGHT. NO FURTHER ALERTS. FIRE DEPARTMENT SAW NO EVIDENCE OF LEAK AFTER LANDING. COMPONENT REPLACEMENT AND FINAL LEAK CHECK ACCOMPLISHED

Part: PANEL — DELAMINATED (ZONE 230) · airframe 92,464 hrs · 23,472 cycles

CABIN - FLOOR PANEL #231LF FOUND DELAMINATED AT STATION 675 - 735. DELAMINATED FLOOR PANEL #231LF AT CABIN STATION675 - 735 REMOVED AS PER AMM 53-21- 04. FLOOR PANEL #231LF FABRICATED AS PER FEDEX DRAWING SRZ-25-005 REVISION R. FLOOR PANEL #231LF INSTALLED AS PER AMM 53-21-04. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SPLICE — CRACKED (ZONE 184) · airframe 92,464 hrs · 23,472 cycles

CENTER CARGO BILGE AREA AFTER REMOVAL SPLICE FOR ACCESS AT STATION 5-123 LONGERON 48 LEFT HAND FOUND OUTBROAD SPLICE CRACKED. CENTER CARGO BILGE AREA STATION 5-123 LONGERON 48 LEFT HAND OUTBOARD CRACKED SPLICE REMOVED AND REPLACED AS PER SRM 51-33-01-OG. SPLICE FABRICATED AS PER DOUGLAS DRAWING A5A7124 REVISION D. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SPLICE — CORRODED (CENTER CARGO) · airframe 92,464 hrs · 23,472 cycles

CENTRE CARGO BILGE AT STATION 5-113 LONGERON 48 LEFT HAND SPLICE FITTING FOUND CORROSION . CENTRE CARGO BILGE AT STATION 5-113 LONGERON 48 LEFT HAND SPLICE FITTING CORROSION EVALUATED FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER SRM 53-00-00-2R FIGURE 5 REPAIR GENERAL. CORRODED LONGERON SPLICE AT STATION 5-113 LONGERON 48 LEFT HAND REMOVED AND REPLACED AS PER SRM 51-33-01-OG. SPLICE FABRICATED AS PER DOUGLAS DRAWING A5A7123 REVISION D. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: LONGERON — CRACKED (ZONE 183) · airframe 92,464 hrs · 23,472 cycles

CENTER CARGO COMPARTMENT BILGE AT STATION 5-113LONGERON 48 LEFT HAND AFTER REMOVAL OF UPPER DAMAGED SPLICE FOUND LONGERON 48 LEFT HAND CRACKED AT STATION 1538. CENTER CARGO COMPARTMENT BILGE CRACKED LEFT HAND LONGERON 48 AT STATION 1538 REPAIRED AS PER SRM 53-00-05-2R REPAIR 1 FIGURE 202. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: RIB — CRACKED (ZONE 600) · airframe 92,464 hrs · 23,472 cycles

WHILE PERFORMING INTERNAL BORESCOPE INSPECTION (SPECIAL/NONROUTINE MAINTENANCE FORM NUMBER N00974), RIGHT HAND WING NUMBER 6 SLAT INTERNAL RIB FOUND CRACK AT LOOSE RIVETS AREA. RIGHT HAND WING NUMBER 6 SLAT INTERNAL LOOSE RIVETS AND CRACKED RIB AT STATION XOS 847.073 REMOVED AND REPLACED AS PER SRM 57-40-01-2R REPAIR 13. RIB FABRICATED AS PER DOUGLAS DRAWING ARB1827 REVISION C. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2- 100.

Part: RIB — CRACKED (ZONE 600) · airframe 92,464 hrs · 23,472 cycles

WHILE PERFORMING INTERNAL BORESCOPE INSPECTION (SPECIAL/NONROUTINE MAINTENANCE FORM NUMBER N00976), RIGHT HAND WING NUMBER 8 SLAT INTERNAL RIB FOUND CRACK AT LOOSE RIVETS AREA. RIGHT HAND WING NUMBER 8 SLAT INTERNAL LOOSE RIVETS AND CRACKED RIB AT STATION XOS 1092.116 REMOVED AND REPLACED AS PER SRM 57-40-01-2R REPAIR 13. RIB FABRICATED AS PER DOUGLAS DRAWING ARB1928 REVISION G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2- 100.

Part: SPAR CAP — CORRODED (ZONE 500) · airframe 92,464 hrs · 23,472 cycles

LEFT WING - TRAILING EDGE REAR SPAR LOWER CAP FOUND CORROSION AT STATION XORS 1051 AFTER REMOVAL OF OUTBOARD ISLAND. LEFT WING TRAILING EDGE REAR SPAR LOWER CAP AT STATION XORS 1051 CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER SRM 57-00-10-1A FIGURE 101 ALLOWABLE DAMAGE 1. LEFT HAND WING REAR SPAR LOWER CAP AT STATION XORS 1051 REPAIR CARRIED OUT AS PER SRM 57-30-10-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6- 2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 92,464 hrs · 23,472 cycles

CABIN - RIGHT HAND STATION 5-73 X = - 8.5 SEAT TRACK FLANGE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT EXISTING SPLICES STATION 5-63 TO STATION 5-123 / 1531 , X = - 8.5 AS PER SRM 53-00-52-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 92,464 hrs · 23,472 cycles

CABIN - RIGHT HAND STATION1259 - 1301 , X = - 107.25 SEAT TRACK FLANGE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1229 TO STATION 1331 , X = - 107.25 AS PER SRM 53-00-52-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 92,464 hrs · 23,472 cycles

CABIN - LEFT HAND STATION 5-73 X = 8.5 SEAT TRACK FLANGE FOUND CORRODED. REMOVED AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 5-43 TO EXISTING SPLICE STATION 5-123 / 1531 X = 8.5 AS PER SRM 53-00-52-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: ACCESS DOOR — CRACKED (RT WING SLAT) · airframe 92,464 hrs · 23,472 cycles

DURING HIGH FREQUENCY EDDY CURRENT INSPECTION ON RIGHT HAND WING SLAT OF ACTUATOR ACCESS DOOR FORWARD INBOARD CORNER FOUND 01EA CRACK APPROXIMATELY 0.2 INCH. RIGHT HAND WING SLAT ACTUATOR ACCESS DOOR FORWARD INBOARD CORNER CRACKED AREA AT STATION XOS 490.850. REPAIR CARRIED OUT AS PER SRM 57-40-01-2R. REPAIR 17 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: LONGERON — CORRODED (BS 1119 L52) · airframe 92,464 hrs · 23,472 cycles

AFTER REMOVAL OF CORRODED LONGERON 52 SPLICE FITTING AT STATION 1119 - 6-10 LONGERON 52 CORRODED AT 6-10. FOUND LONGERON 52 CORRODED AT 6-10. CORROSION AT LONGERON 52 STATION 6-10 EVALUATED , FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER SRM 53-00-00-2R FIGURE 205 REPAIR GENERAL. CORRODED LONGERON 52 AT STATION 6-10 REPAIRED AS PER SRM 53-00-05-2R REPAIR 1 FIGURE 202. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CRACKED (ZONE 600) · airframe 92,464 hrs · 23,472 cycles

RIGHT HAND WING SLAT TRACK NUMBER 9 CUTOUT LOWER OUTBOARD CORNER SKIN AT APPROXIMATELY STATION XOS 607 FOUND WITH CRACK. RIGHT HAND WING SLAT TRACK NUMBER 9 CUTOUT LOWER OUTBOARD CORNER SKIN AT APPROXIMATELY STATION XOS 607 CRACKED AREA REPAIR CARRIED OUT AS PER SRM 57-40-01- 2R REPAIR 18 FIGURE 202, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (600) · airframe 92,464 hrs · 23,472 cycles

RIGHT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT STATION XOS 637 TO 643 FOUND CRACK. RIGHT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT STATION XOS 637 TO 643 CRACKED AREA REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100

Part: DOUBLER — CRACKED (600) · airframe 92,464 hrs · 23,472 cycles

RIGHT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT STATION XOS 542 TO 547 FOUND CRACK. RIGHT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT STATION XOS 542 TO 547 CRACKED AREA REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (600) · airframe 92,464 hrs · 23,472 cycles

RIGHT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT STATION XOS 789 TO 795 FOUND CRACK. RIGHT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT STATION XOS 789 TO 795 CRACKED AREA REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 92,464 hrs · 23,472 cycles

RIGHT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT STATION XOS 584 TO 588 FOUND CRACK. RIGHT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT STATION XOS 584 TO 588 CRACKED AREA REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 92,464 hrs · 23,472 cycles

RIGHT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT STATION XOS 643 TO 648 FOUND CRACK. RIGHT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT STATION XOS 643 TO 648 CRACKED AREA REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 92,464 hrs · 23,472 cycles

LEFT HAND WING OUTBOARD LEADING EDGE COMPARTMENT BEADED DOUBLER AT STATION XOS 616 TO 621 FOUND CRACK. LEFT HAND WING OUTBOARD LEADING EDGE COMPARTMENT BEADED DOUBLER AT STATION XOS 616 TO 621 CRACKED AREA REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 92,464 hrs · 23,472 cycles

RIGHT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT STATION XOS 697 TO 703 FOUND CRACK. RIGHT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT STATION XOS 697 TO 703 CRACKED AREA REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CRACKED (RT WING) · airframe 92,464 hrs · 23,472 cycles

RIGHT HAND WING SLAT TRACK NUMBER 12 CUTOUT LOWER OUTBOARD CORNER SKIN AT APPROXIMATELY STATION XOS 776 FOUND WITH CRACK. RIGHT HAND WING SLAT TRACK NUMBER 12 CUTOUT LOWER OUTBOARD CORNER SKIN AT APPROXIMATELY STATION XOS 776 CRACKED AREA REPAIR CARRIED OUT AS PER SRM 57-40-02- 2R REPAIR 7 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (500) · airframe 92,464 hrs · 23,472 cycles

LEFT HAND WING OUTBOARD LEADING EDGE COMPARTMENT BEADED DOUBLER AT STATION XOS 759 TO 763 FOUND CRACK. LEFT HAND WING OUTBOARD LEADING EDGE COMPARTMENT BEADED DOUBLER AT STATION XOS 759 TO 763 CRACKED AREA REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 92,464 hrs · 23,472 cycles

RIGHT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT STATION XOS 691 TO 697 FOUND CRACK. RIGHT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT STATION XOS 691 TO 697 CRACKED AREA REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SPLICE — CORRODED (ZONE 127) · corrosion level 2 · airframe 92,464 hrs · 23,472 cycles

FORWARD CARGO BILGE FROM STATION 1119 - 6-10 LONGERON 52 SPLICE FITTING FOUND CORROSION. FORWARD CARGO BILGE FROM STATION 1119 TO STATION 6-10 AT LONGERON 52 SPLICE , CORROSION EVALUATED FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER SRM 53-00-00-52- 2R FIGURE 205 REPAIR GENERAL. CORRODED LONGERON 52 SPLICE AT STATION 1119 TO STATION 6-10 REMOVED AND REPLACED AS PER SRM 51-31-01-0G. LONGERON 52 SPLICE FABRICATED BY MACHINING AS PER DOUGLAS DRAWING ADA8424 REVISION A. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: MFC — FAILED (N/A) · airframe 92,413 hrs · 23,459 cycles

APPROXIMATELY T/O PLUS 1 HOUR, RECEIVED A LEVEL 1 AIR SYS 2 OFF ALERT. NOTED A RED MANF LIGHT ON R&R ESC PER MM 21-08-01-4, AIR SYSTEM TEST PASS, RAN ALL 3 ENGINES DURING 10 MINUTES, NO FAULTS ALL TESTS PASS. ALSO R&R MFC PER MM 36-23-01-4, ALL TESTS PASS.

Part: INDICATION SYS — NO TEST (R1 DOOR SLIDE) · airframe 90,261 hrs · 22,851 cycles

MDIS 602 25-60 1083 21MAY21 LAX OPEN U R1 DOOR EVACUATION SLIDE REMOTE PRESSURE PRESS-TO-TEST INDICATION IS NOT TESTING MEL 21MAY21 12:59 LAX U RELEASED FOR SERVICE PER MEL : 25-61-02 CATEGORY : C EXPIRATION : 31MAY21 "MEL 25-61-02: R1 EVAC SLIDE REMOTE PRESS INDICATOR - INOP. PER MEL 25-61-02, VERIFYAND RECORD IN THE AML, EVAC SLIDE SYS PRESS ADEQAUTE ONCE EACH FLIGHT DAY." C/7271000 FACT 22MAY21 18:30 MEM RELAMPED SWITCH BULBS IN REFERENCE TO AMM 25-61-04-5. OPS CHECK GOOD AT THIS TIME. A/C OK FOR SERVICE.

Part: FLANGE — CORRODED (ENGINE LINER) · airframe 90,010 hrs · 22,782 cycles

NR 2 ENGINE HAS SIGNS OF CORROSION ON FAN CASE FWD FLANGE FROM APPROXIMATELY 4 TO 8 O'CLOCK POS. REFERENCE NONROUTINE N00018 WORK ORDER 79912 ITEM FOUND DURING B-CHECK. CORROSION IS MORE THAN 10 INCHES IN CUMULATIVE CIRCUMFERENCE. CIRCUMFERENCE. REF N18 WORK ORDER 79912 ITEM 1 JPF. REMOVED CORROSION IN REF TO AMM 72-32-00-6-1 REF N18 WORK ORDER 79912 ITEM 2 JPF. AREA TREATED WITH PRIMER IN REF TO SRM 51-23-01-0G REF N18 WORK ORDER 79912 ITEM 3 JPF. INNER LINER WAS INSPECTED NO CORROSION FOUND IN REF TO AMM 72-32-00-6-1

Part: RETAINER — DAMAGED (LT FAIRING SEAL) · airframe 89,786 hrs · 22,700 cycles

LEFT WHEEL WELL, AFT OUTBOARD DOOR JAMB STRUCTURE, INBOARD FLAP, INBOARD FAIRING SEAL RETAINER CHANNEL DAMAGED DUE TO CONTACT WITH INBOARD FLAP, INBOARD FAIRING. INSTALLED REPAIR DOUBLER PER ENGINEERING AUTHORIZATON 1-5310-T0360413, INSTALLED SEAL AND SEAL RETAINER

Part: SENSOR — MAKING METAL (ENGINE) · airframe 89,197 hrs · 22,534 cycles

AFTER TAKEOFF PASSING 1000', 5 IN SUCCESSION LOUD BANGS WITH HEAVY SHUTTERS. ENGINE INDICATIONS APPEARED NORMAL AND THERE WAS NO YAW ASSOCIATED WITH THE BANG/SHUTTERING. DURING NR 2 ENGINE INLET AND EXHAUST INSPECTION FOUND LEFT HAND FAN STATOR AFT INNER SEGEMENT PANEL AT 11:00 POSITION BLEW OFF AND DEPARTED AIRCRAFT, LEFT T/R HALF DAMAGED AS WELL. T/R DAMAGE IS A GOUGE ON INTERIOR WALL ABOUT 9:00 POSITION. GOUGE IS APPROXIMATELY 6" LONG BY 5" WIDE AND INTO THE HONEY COMB STRUCTURE. PICTURES OF DAMAGE ATTACHED. REVERSER R & R ON SEPARATE WRITE UP. WRI 78-30/0645. CHECKED ECU 2A AND ECU 2B, NO CURRENT FAULTS AND NO FAULTS STORED IN FAULT REVIEW. INSTALLED MISSING NR 2 FAN STATOR INNER AFT LINER SEGMENT REFERENCE MD-11 AMM 72-33-01-4-1. R & R NR 2 ENGINE HMU, REF MM 73-21-01-4-1. FAILED OPERATIONS CHECK. TROUBLESHOOTING CONTINUES. FOUND ROD ENDS WORN ON BOTH VSV ACTUATORS. ALSO R & R, N1 SENSOR, N2 SENSOR, CIT SENSOR, STATOR CONTROL ALTERNATOR. HMU, AND ECU, REF AMM MANUAL REFERENCES. 75-31-01-4-1,77-11-01-4, 77-11-02-4-1,73-21-11-4-1,73-21-21-4-1,73-21-01-4-1, AND 73-21-02-5-1. RAN UP ENGINE TO 83 PERCENT PER JRH POWER ASSURANCE TEST NO FAULTS FOUND AC OK FOR SERVICE.

Part: B-NUT — LEAKING (HYD SYSTEM) · airframe 88,148 hrs · 22,265 cycles

HYD 1 OFF LEVEL 1 ALERT 15 MIN INTO CRUISE AT FL380. HYD 1 QTY LO AND HYD 1 PUMP 1R/1L OFF ALERTS CYCLED DURING CONFIGURATION. EMERGENCY DECLARED. SERVICED SYSTEM 1 HYDRAULIC RESERVOIR REF AMM 12-13-02-3. OPERATED NR 1 HYDRAULIC SYSTEM. TRACED LEAK TO LOOSE HYDRAULIC LINE B-NUT ON NR 1 BRAKE SYSTEM UPPER FWD ACCUMULATOR. SECURED THE FITTING IAW AMM 32-44-01-4. SERVICED AND OPERATED THE BRAKES IAW AMM 32-43-20-6. BRAKES OPERATED NORMALLY, WITH NO LEAKS NOTED. AIRCRAFT OK FOR SERVICE.

Part: HYDRAULIC LINE — LEAKING (BRAKE ACCUMULATO) · airframe 88,148 hrs · 22,265 cycles

HYD 1 OFF LEVEL 1 ALERT, 15 MIN INTO CRUISE AT FL380. HYD 1 QTY LO AND HYD 1 PUMP 1R/1L OFF ALERTS CYCLED DURING CONFIGURATION. EMERGENCY DECLARED. FOUND A FITTING ON ONE OF THE NR 1 BRAKE SYS ACCUMULATORS IN THE LEFT WHEEL WHEEL LOOSE.

Part: RECEIVER — FAILED (RADIO ALTIMETER) · airframe 87,845 hrs · 22,177 cycles

IMMEDIATELY AFTER TAKEOFF, SPURIOUS CAWS WARNINGS BEGAN WITH CONSTANT RAD ALT CALL OUTS. AT ABOUT 4000 FEET MSL 'TAILSTRIKE GO AROUND' ALERT AND AP/AT DISCONNECTED. UNABLE TO RECONNECT AP OR AT AT THIS TIME. AFTER CLIMB TO FL200 AND NO IMPROVEMENT TO CONDITION OF AUTOPILOT AND AUTOTHROTTLE, RETURN TO WSSS, APPROX 93LBS OF FUEL DUMPED. AFTER DESCENT TO FL140, WE WERE ABLE TO USE AUTOPILOT BUT NO AUTOTHROTTLES. SPURIOUS CAWS ALERTS BEGAN AT 2500' MSL ON APPROACH AND CEASED PRIOR TO 500'. FROM 500' TO TOUCHDOWN ALL CAWS ALERTS WERE APPROPRIATE. INSPECTION PERFORMED AND FOUND RA-2 RCVR COAX CABLE C6-15 SHIELD OPEN. REPLACED COAX CABLE REF WDM 34-42-02 AND BOTH ANTENNAS A3-8 (RA-2 XMTR) AND A3-10 (RA-2 RCVR) REF 34-42-03-4. REPLACED RA-2 TRANSCEIVER AND CARRIED OUT FUNCTIONAL TEST AND AUTOLAND TEST REF 34-42-01-2. ALL SATIS. A/C OK FOR SERVICE.

Part: FITTING — CRACKED (VERTICAL STAB) · airframe 87,829 hrs · 22,174 cycles

CRACK INDICATION FOUND ON 01 EACH HOLE DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION ON SKIN PANEL LAYER AT NUMBER 4 BANJO FITTING. RIGHT HAND SIDE FORWARD EXISTING REPAIR 5TH HOLE COUNTING FROM BELOW CRACK ON 01 EACH HOLE DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION ON SKIN PANEL LAYER AT NUMBER 4 BANJO FITTING RIGHT HAND SIDE FORWARD EXISTING REPAIR AREA 5TH HOLE COUNTING FROM BELOW AT STATION 2164 REPAIRED AS PER EA 1-5530-T0354707 PART 1 TITLE: STABILIZERS - VERTICAL STABILIZER - CRACK REPAIR ON VERTICAL STABILIZER REAR SPAR RT SIDE FWD AND AFT FLANGES. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FITTING — DAMAGED (VERTICAL STAB) · airframe 87,829 hrs · 22,174 cycles

01 EACH FASTENER HOLE FOUND ELONGATED DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION AT NUMBER 4 BANJO FITTING RIGHT HAND SIDE AFT 4TH HOLE COUNTING FROM BELOW 01 EACH FASTENER. HOLE ELONGATED DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION AT NUMBER 4 BANJO FITTING RIGHT HAND SIDE AFT 4TH HOLE COUNTING FROM BELOW AT STATION 2164 REPAIRED AS PER EA 1-5530-T0354707 PART 1 TITLE: STABILIZERS - VERTICAL STABILIZER - CRACK REPAIR ON VERTICAL STABILIZER REAR SPAR RT SIDE FWD AND AFT FLANGES. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE — CORRODED (RT WING) · corrosion level 2 · airframe 87,829 hrs · 22,174 cycles

RIGHT HAND WING OUTBOARD FLAP OUTBOARD HINGE FORWARD (WING SIDE) BARREL NUT HOLE SURFACE CORROSION. CORROSION AT RIGHT HAND WING OUTBOARD FLAP OUTBOARD HINGE FORWARD (WING SIDE) BARREL NUT HOLE SURFACE REWORKED AS PER CMM 57-44-09 AND FOUND EXCEED LIMIT BASED THE DIFFERENCE BETWEEN DRAWING LIMITS AND CMM MAXIMUM REWORK LIMITS FOR BARREL NUT HOLE. MINIMUM THICKNESS 0.3765". REPAIR SHIM FABRICATED AND INSTALLED AS PER CMM 57-44-09 AND EA 1-5750-T0354598 PART 1 STEP 2, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- RT WING- OUTBD FLAP, OUTBD FWD HINGE (WING SIDE) -CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NR N00347 ATTACHED EA 1-5750-T0354598 PART 1 FOR WORK DETAILS.

Part: SUPPORT FITTING — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 87,829 hrs · 22,174 cycles

RIGHT HAND WING TRAILING EDGE - OUTBOARD FLAP VANE NR 4 FROM INBOARD FITTING FOUND CORROSION AROUND A HOLE. CORROSION AROUND HOLE AT THE RIGHT WING TRAILING EDGE, OUTBOARD FLAP VANE NR 4 FROM INBOARD FITTING REWORKED AND FOUND EXCEEDS LIMITS IAW SRM 57-50-02-2R, REPAIR 5, FIGURE 201. AN OVERSIZED BUSHING WAS FABRICATED IAW SRM 57-50-02-2R, REPAIR 5, FIGURE 201, AND EA 1-5750-T0354672, PART 1, STEP 1A. THE OVERSIZED BUSHING WAS INSTALLED IAW AMM 27-50-32-4. THE REPAIR WAS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: SUPPORT — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 87,829 hrs · 22,174 cycles

RIGHT HAND WING TRAILING EDGE - OUTBOARD FLAP VANE NR 2 FROM INBOARD FITTING FOUND WITH HOLE CORRODED. CORRODED HOLE AT RIGHT HAND WING TRAILING EDGE - OUTBOARD FLAP VANE #2 FROM INBOARD FITTING REWORKED AND FOUND EXCEEDED LIMITS IAW SRM 57-50-02-2R, REPAIR 5, FIGURE 201. OVERSIZED BUSHING FABRICATED IAW SRM 57-50-02-2R REPAIR 5 FIGURE 201 AND EA. #: 1-5750-T0354672 PART 1 STEP 1A. BUSHING INSTALLED IAW AMM 27-50-32-4. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SUPPORT FITTING — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 87,829 hrs · 22,174 cycles

RIGHT HAND WING TRAILING EDGE - OUTBOARD FLAP VANE NR 5 FROM INBOARD FITTING FOUND CORRODED AROUND HOLE. CORROSION AROUND HOLE WAS REWORKED AND FOUND EXCEEDED LIMITS IAW SRM 57-50-02-2R, REPAIR 5, FIGURE 201. AN OVERSIZED BUSHING WAS FABRICATED IAW SRM 57-50-02-2R, REPAIR 5, FIGURE 201, AND EA 1-5750-T0354672, PART 1, STEP 1A. THE OVERSIZED BUSHING WAS INSTALLED IAW AMM 27-50-32-4. THE REPAIR WAS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: SUPPORT FITTING — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 87,829 hrs · 22,174 cycles

RIGHT HAND WING TRAILING EDGE - OUTBOARD FLAP VANE NR 3 FROM INBOARD FITTING FOUND WITH HOLE CORRODED. CORROSION AROUND HOLE AT THE RIGHT WING TRAILING EDGE OUTBOARD FLAP VANE NR 3 FROM INBOARD FITTING REWORKED AND FOUND EXCEEDS IAW SRM 57-50-02-2R, REPAIR 5, FIGURE 201. OVERSIZED BUSHING FABRICATED IAW SRM 57-50-02-2R, REPAIR 5, FIGURE 201, AND EA. 1-5750-T0354672, PART 1, STEP 1A. OVERSIZED BUSHING INSTALLED IAW AMM 27-50-32-4. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: SUPPORT FITTING — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 87,829 hrs · 22,174 cycles

RIGHT HAND WING TRAILING EDGE - OUTBOARD FLAP VANE NR 1 FROM INBOARD FITTING FOUND WITH HOLE CORRODED. CORRODED HOLE AT RIGHT HAND WING TRAILING EDGE - OUTBOARD FLAP VANE #1 FROM INBOARD FITTING REWORKED BY MACHINING AND FOUN REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: FITTING — CRACKED (VERTICAL STAB) · airframe 87,829 hrs · 22,174 cycles

ULTRASONIC INSPECTION FOUND CRACK INDICATION ON LOWER VERTICAL STABILIZER NR 4 BANJO FITTING RIGHT HAND SIDE FORWARD FLANGE. REPAIR AREA AND UNABLE TO DETERMINE THE CRACK LENGTH DUE TO REPAIR BLOCKAGE AT APPROXIMATE STATION Y=2164 CRACK ON LOWER VERTICAL STABILIZER NR 4 BANJO FITTING RIGHT HAND SIDE FORWARD FLANGE REPAIR AREA AT STATION 2164 REPAIRED AS PER EA 1-5530-T0354707 PART 1 TITLE: STABILIZERS - VERTICAL STABILIZER - CRACK REPAIR ON VERTICAL STABILIZER REAR SPAR RT SIDE FWD AND AFT FLANGES. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 87,829 hrs · 22,174 cycles

CABIN, FOUND SEAT TRACK STATION 1551, X = - 8.5 CROWN DAMAGED. CABIN, AT SEAT TRACK STATION 1551 X = - 8.5, DAMAGED CROWN EVALUATED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT EXISTING SPLICES STATION 1531 TO STATION 1571 X= - 8.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 87,829 hrs · 22,174 cycles

CABIN, FOUND SEAT TRACK STATION 630, X = 27.5 CROWN DAMAGED. CABIN, DAMAGED CROWN AT SEAT TRACK STATION 630, X = 27.5 EVALUATED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A F FIGURE 101 ALLOWABLE DAMAGE 1. CROWN DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT EXISTING SPLICES STATION 625 TO STATION 645 X = 27.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: PLATE — WORN (CARGO DOOR) · airframe 87,829 hrs · 22,174 cycles

UPPER CARGO DOOR, FOUND DOOR HINGE PLATE NR 4 WITH LOBE NR 1 TO NR 5 WORN. NR 1 TO NR 5 WORN HOLE AT UPPER CARGO DOOR HINGE PLATE NR 4 REWORKED AND FOUND EXCEED LIMIT AS PER SRM 52-30-16-1A FIGURE 101 SHEET 3. OVERSIZED BUSHING 05 EACH FABRICATED BY MACHINING AND INSTALLED AS PER EA 1-5230-T0354678 PART 1 STEP 2 AND STEP 5. TITLE: DOORS- CARGO DOOR- MAIN DECK UPPER CARGO DOOR JAMB- WORN HINGE LOBE BORES. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE — CORRODED (RT WING) · airframe 87,829 hrs · 22,174 cycles

RIGHT HAND WING OUTBOARD FLAP OUTBOARD HINGE FORWARD (WING SIDE) INBOARD LOWER MOUNT SURFACE CORROSION. CORROSION AT RIGHT HAND WING OUTBOARD FLAP OUTBOARD HINGE FORWARD (WING SIDE) INBOARD LOWER MOUNT SURFACE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. REPAIR SHIM FABRICATED AND INSTALLED AS PER CMM 57-44-09 AND EA 1- 5750-T0354598 PART 1 STEP 2, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- RT WING- OUTBD FLAP, OUTBD FWD HINGE (WING SIDE) -CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NR N00347 ATTACHED EA 1-5750-T0354598 PART 1 FOR WORK DETAILS.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 87,829 hrs · 22,174 cycles

CABIN, FOUND SEAT TRACK STATION 630, X = 47.5 CROWN DAMAGED. CABIN, DAMAGED CROWN AT SEAT TRACK STATION 630, X = 47.5 EVALUATED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT EXISTING SPLICES STATION 605 TO STATION 645 X = 47.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRAP — DAMAGED (NR 1 SPOILER) · airframe 87,829 hrs · 22,174 cycles

AGING AIRCRAFT EXISTING REPAIR FOUND AT LEFT HAND WING NR 1 SPOILER UPPER SURFACE TRAILING EDGE XISP 226. EXISTING REPAIR AT LEFT HAND WING NR 1 SPOILER UPPER SURFACE TRAILING EDGE XISP 226 EVALUATED AND FOUND EXISTING REPAIR STRAP DAMAGED. NR 1 SPOILER UPPER SURFACE CARRIED OUT REPAIR IN ACCORDANCE WITH SRM 57-70-02-2R FIGURE 201 REPAIR 1. EO 1-5100-7-5001 B6 PART 1 TITLE: STRUCTURES - REPAIR CATALOG - REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 87,829 hrs · 22,174 cycles

CABIN, MAIN DECK CARGO COMPARTMENT FOUND SEAT TRACK FLANGE CORRODED AT STATION 1504 TO STATION 1465, X = 8.5 LEFT HAND SIDE. CABIN, AT SEAT TRACK FLANGE STATION 1504 TO STATION 1465 X = 8.5, CORROSION FOUND EXFOLIATED AND EXCEED LIMIT AS PER SRM 53-00-52- 1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT EXISTING SPLICES STATION 1451 TO STATION 1531 X = 8.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 87,829 hrs · 22,174 cycles

AFT CABIN, FLOOR PANEL 291EF DELAMINATED AT STATION 1914 - STATION 2007/ZONE 290. DELAMINATED FLOOR PANEL 291 EF AT AFT CABIN LEFT HAND STATION 1914 - STATION 2007 ZONE 290. REMOVED AS PER AMM 53-21-04. FLOOR PANEL 291 EF FABRICATED AS PER DRAWING SRZ-25-005 REVISION R. FABRICATED FLOOR PANEL INSTALLED AS PER AMM 53-21-04. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE — CORRODED (RT WING) · airframe 87,829 hrs · 22,174 cycles

RIGHT HAND WING OUTBOARD FLAP OUTBOARD HINGE FORWARD (WING SIDE) LOWER BARREL HOLE CORROSION. CORROSION AT RIGHT HAND WING OUTBOARD FLAP OUTBOARD HINGE FORWARD (WING SIDE) LOWER BARREL NUT HOLE (7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER CMM 57-44-09 AND EA 1-5750-T0354598 PART 1 STEP 2B AND STEP 2, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- RT WING- OUTBD FLAP, OUTBD FWD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NR N00347 ATTACHED EA 1-5750-T0354598 PART 1 FOR WORK DETAILS.

Part: HINGE — CORRODED (RT WING) · airframe 87,829 hrs · 22,174 cycles

RIGHT HAND WING OUTBOARD FLAP OUTBOARD HINGE FORWARD (WING SIDE) UPPER BARREL HOLE CORROSION. CORROSION AT RIGHT HAND WING OUTBOARD FLAP OUTBOARD HINGE FORWARD (WING SIDE) UPPER BARREL NUT HOLE (7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER CMM 57-44-09 AND EA 1-5750-T0354598 PART 1 STEP 2B AND STEP 2, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- RT WING- OUTBD FLAP, OUTBD FWD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NR N00347 ATTACHED EA 1-5750-T0354598 PART 1 FOR WORK DETAILS.

Part: HINGE — CORRODED (RT WING) · airframe 87,829 hrs · 22,174 cycles

RIGHT HAND WING OUTBOARD FLAP OUTBOARD HINGE FORWARD (WING SIDE) PIVOT HOLE BORE CORROSION.

Part: HINGE — CORRODED (RT WING) · airframe 87,829 hrs · 22,174 cycles

RIGHT HAND WING OUTBOARD FLAP INBOARD HINGE FORWARD (WING SIDE) OUTBOARD LOWER MOUNT HOLE CORROSION. CORROSION AT RIGHT HAND WING OUTBOARD FLAP INBOARD HINGE FORWARD (WING SIDE) OUTBOARD LOWER MOUNT HOLE BORE (7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08. SHOULDER BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER CMM 57-44-08 AND EA 1-5750-T0354641 PART 1 STEP 1D AND STEP 1, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- RT WING- OUTBD FLAP INBD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NR N00380 ATTACHED EA 1-5750-T0354641 PART 1 FOR WORK DETAILS.

Part: HINGE — CORRODED (RT WING) · airframe 87,829 hrs · 22,174 cycles

RIGHT HAND WING OUTBOARD FLAP INBOARD HINGE FORWARD (WING SIDE) OUTBOARD FORWARD MOUNT HOLE BORE CORROSION. CORROSION AT RIGHT HAND WING OUTBOARD FLAP INBOARD HINGE FORWARD (WING SIDE) OUTBOARD FORWARD MOUNT HOLE BORE (6 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER CMM 57-44-08 AND EA 1-5750-T0354641 PART 1 STEP 1C AND STEP 1, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- RT WING- OUTBD FLAP INBD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NR N00380 ATTACHED EA 1-5750-T0354641 PART 1 FOR WORK DETAILS.

Part: HINGE — CORRODED (RT WING) · airframe 87,829 hrs · 22,174 cycles

RIGHT HAND WING OUTBOARD FLAP INBOARD HINGE FORWARD (WING SIDE) INBOARD LOWER MOUNT HOLE CORROSION. CORROSION AT RIGHT HAND WING OUTBOARD FLAP INBOARD HINGE FORWARD (WING SIDE) INBOARD LOWER MOUNT HOLE BORE (7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08. SHOULDER BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER CMM 57-44-08 AND EA 1-5750-T0354641 PART 1 STEP 1D AND STEP 1, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- RT WING- OUTBD FLAP INBD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NR N00380 ATTACHED EA 1-5750-T0354641 PART 1 FOR WORK DETAILS.

Part: HINGE — CORRODED (RT WING) · airframe 87,829 hrs · 22,174 cycles

RIGHT HAND WING OUTBOARD FLAP OUTBOARD HINGE FORWARD (WING SIDE) INBOARD LOWER MOUNT BORE HOLE CORROSION. CORROSION AT RIGHT HAND WING OUTBOARD FLAP OUTBOARD HINGE FORWARD (WING SIDE) INBOARD LOWER MOUNT BORE HOLE (3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. SHOULDER BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER CMM 57-44-09 AND EA 1-5750-T0354598 PART 1 STEP 2A AND STEP 2, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- RT WING- OUTBD FLAP, OUTBD FWD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NR N00347 ATTACHED EA 1-5750-T0354598 PART 1 FOR WORK DETAILS.

Part: HINGE — CORRODED (RT WING) · airframe 87,829 hrs · 22,174 cycles

RIGHT HAND WING OUTBOARD FLAP OUTBOARD HINGE FORWARD (WING SIDE) INBOARD UPPER MOUNT BORE HOLE CORROSION. CORROSION AT RIGHT HAND WING OUTBOARD FLAP OUTBOARD HINGE FORWARD (WING SIDE) INBOARD UPPER MOUNT BORE HOLE (2 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER CMM 57-44-09 AND EA 1-5750-T0354598 PART 1 STEP 2B AND STEP 2, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- RT WING- OUTBD FLAP, OUTBD FWD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NR N00347 ATTACHED EA 1-5750-T0354598 PART 1 FOR WORK DETAILS.

Part: HINGE — CORRODED (RT WING) · airframe 87,829 hrs · 22,174 cycles

RIGHT HAND WING OUTBOARD FLAP OUTBOARD HINGE FORWARD (WING SIDE) OUTBOARD ACTUATOR HOLE BORE CORROSION. CORROSION AT RIGHT HAND WING OUTBOARD FLAP OUTBOARD HINGE FORWARD (WING SIDE) OUTBOARD ACTUATOR HOLE BORE (8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER CMM 57-44-09 AND EA 1-5750-T0354598 PART 1 STEP 2B AND STEP 2, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- RT WING- OUTBD FLAP, OUTBD FWD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NR N00347 ATTACHED EA 1-5750-T0354598 PART 1 FOR WORK DETAILS.

Part: HINGE — CORRODED (RT WING) · airframe 87,829 hrs · 22,174 cycles

RIGHT HAND WING OUTBOARD FLAP INBOARD HINGE FORWARD (WING SIDE) UPPER BARREL NUT HOLE CORROSION. CORROSION AT RIGHT HAND WING OUTBOARD FLAP INBOARD HINGE FORWARD (WING SIDE) UPPER BARREL NUT HOLE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER CMM 57-44-08 AND EA 1-5750-T0354641 PART 1 STEP 1F AND STEP 1, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- RT WING- OUTBD FLAP INBD HINGE (WING SIDE) -CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NR N00380 ATTACHED EA 1-5750- T0354641 PART 1 FOR WORK DETAILS.

Part: HINGE — CORRODED (RT WING) · airframe 87,829 hrs · 22,174 cycles

RIGHT HAND WING OUTBOARD FLAP INBOARD HINGE FORWARD (WING SIDE) BARREL NUT HOLE CORROSION. CORROSION AT RIGHT HAND WING OUTBOARD FLAP INBOARD HINGE FORWARD (WING SIDE) BARREL NUT HOLE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER CMM 57-44-08 AND EA 1-5750-T0354641 PART 1 STEP 1E AND STEP 1, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- RT WING- OUTBD FLAP INBD HINGE (WING SIDE) -CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NR N00380 ATTACHED EA 1-5750-T0354641 PART 1 FOR WORK DETAILS.

Part: HINGE — CORRODED (RT WING) · airframe 87,829 hrs · 22,174 cycles

RIGHT HAND WING OUTBOARD FLAP OUTBOARD HINGE FORWARD (WING SIDE) OUTBOARD LOWER MOUNT BORE HOLE CORROSION CORROSION AT RIGHT HAND WING OUTBOARD FLAP OUTBOARD HINGE FORWARD (WING SIDE) OUTBOARD LOWER MOUNT BORE HOLE (3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. SHOULDER BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER CMM 57-44-09 AND EA 1-5750-T0354598 PART 1 STEP 2A AND STEP 2, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- RT WING- OUTBD FLAP, OUTBD FWD HINGE (WING SIDE) -CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NR N00347 ATTACHED EA 1-5750-T0354598 PART 1 FOR WORK DETAILS.

Part: HINGE — CORRODED (RT WING) · corrosion level 2 · airframe 87,829 hrs · 22,174 cycles

RIGHT HAND WING OUTBOARD FLAP OUTBOARD HINGE FORWARD (WING SIDE) PIVOT HOLE BORE CORROSION. CORROSION AT RIGHT HAND WING OUTBOARD FLAP OUTBOARD HINGE FORWARD (WING SIDE) PIVOT HOLE BORE (4 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER CMM 57-44-09 AND EA 1-5750-T0354598 PART 1 STEP 2B AND STEP 2, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- RT WING- OUTBD FLAP, OUTBD FWD HINGE (WING SIDE) -CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NR N00347 ATTACHED EA 1-5750-T0354598 PART 1 FOR WORK DETAILS.

Part: HINGE — CORRODED (RT WING) · airframe 87,829 hrs · 22,174 cycles

RIGHT HAND WING OUTBOARD FLAP INBOARD HINGE FORWARD (WING SIDE) INBOARD FORWARD MOUNT HOLE BORE CORROSION. CORROSION AT RIGHT HAND WING OUTBOARD FLAP INBOARD HINGE FORWARD (WING SIDE) INBOARD FORWARD MOUNT HOLE BORE (6 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER CMM 57-44-08 AND EA 1-5750-T0354641 PART 1 STEP 1C AND STEP 1, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- RT WING- OUTBD FLAP INBD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NR N00380 ATTACHED EA 1-5750-T0354641 PART 1 FOR WORK DETAILS.

Part: HINGE — CORRODED (RT WING) · airframe 87,829 hrs · 22,174 cycles

RIGHT HAND WING OUTBOARD FLAP INBOARD HINGE FORWARD (WING SIDE) INBOARD UPPER MOUNT HOLE CORROSION. CORROSION AT RIGHT HAND WING OUTBOARD FLAP INBOARD HINGE FORWARD (WING SIDE) INBOARD UPPER MOUNT BORE HOLE (2 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER CMM 57-44-08 AND EA 1-5750-T0354641 PART 1 STEP 1A AND STEP 1, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- RT WING- OUTBD FLAP INBD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NR N00380 ATTACHED EA 1-5750-T0354641 PART 1 FOR WORK DETAILS.

Part: HINGE — CORRODED (RT WING) · airframe 87,829 hrs · 22,174 cycles

RIGHT HAND WING OUTBOARD FLAP INBOARD HINGE FORWARD (WING SIDE) OUTBOARD UPPER MOUNT HOLE CORROSION. CORROSION AT RIGHT HAND WING OUTBOARD FLAP INBOARD HINGE FORWARD (WING SIDE) OUTBOARD UPPER MOUNT BORE HOLE (2 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER CMM 57-44-08 AND EA 1-5750-T0354641 PART 1 STEP 1A AND STEP 1, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- RT WING- OUTBD FLAP INBD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NR N00380 ATTACHED EA 1-5750-T0354641 PART 1 FOR WORK DETAILS.

Part: HINGE — CORRODED (RT WING) · airframe 87,829 hrs · 22,174 cycles

RIGHT HAND WING OUTBOARD FLAP INBOARD HINGE FORWARD (WING SIDE) LOWER BARREL NUT HOLE CORROSION. CORROSION AT RIGHT HAND WING OUTBOARD FLAP INBOARD HINGE FORWARD (WING SIDE) LOWER BARREL NUT HOLE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER CMM 57-44-08 AND EA 1-5750-T0354641 PART 1 STEP 1F AND STEP 1, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- RT WING- OUTBD FLAP INBD HINGE (WING SIDE) -CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NR N00380 ATTACHED EA 1-5750-T0354641 PART 1 FOR WORK DETAILS.

Part: HINGE — CORRODED (RT WING) · airframe 87,829 hrs · 22,174 cycles

RIGHT HAND WING OUTBOARD FLAP OUTBOARD HINGE FORWARD (WING SIDE) OUTBOARD UPPER MOUNT BORE HOLE CORROSION. CORROSION AT RIGHT HAND WING OUTBOARD FLAP OUTBOARD HINGE FORWARD (WING SIDE) OUTBOARD UPPER MOUNT BORE HOLE (2 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER CMM 57-44-09 AND EA 1-5750-T0354598 PART 1 STEP 2B AND STEP 2, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- RT WING- OUTBD FLAP, OUTBD FWD HINGE (WING SIDE) -CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NR N00347 ATTACHED EA 1-5750-T0354598 PART 1 FOR WORK DETAILS.

Part: HINGE — CORRODED (RT WING) · airframe 87,829 hrs · 22,174 cycles

RIGHT HAND WING OUTBOARD FLAP OUTBOARD HINGE FORWARD (WING SIDE) INBOARD ACTUATOR HOLE BORE CORROSION. CORROSION AT RIGHT HAND WING OUTBOARD FLAP OUTBOARD HINGE FORWARD (WING SIDE) INBOARD ACTUATOR HOLE BORE (8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER CMM 57-44-09 AND EA 1-5750-T0354598 PART 1 STEP 2B AND STEP 2, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- RT WING- OUTBD FLAP, OUTBD FWD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE — CORRODED (RT WING) · airframe 87,829 hrs · 22,174 cycles

RIGHT HAND WING OUTBOARD FLAP INBOARD HINGE FORWARD (WING SIDE) PIVOT HOLE BORE CORROSION. CORROSION AT RIGHT HAND WING OUTBOARD FLAP INBOARD HINGE FORWARD (WING SIDE) PIVOT HOLE BORE (4 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER CMM 57-44-08 AND EA 1-5750-T0354641 PART 1 STEP 1B AND STEP 1, TITLE WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- RT WING- OUTBD FLAP INBD HINGE (WING SIDE) -CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 87,829 hrs · 22,174 cycles

AGING AIRCRAFT - EXISTING REPAIR AT MAIN DECK CARGO SEAT TRACK DAMAGED STATION 1541 X = 8.5.

Part: DOUBLER — CRACKED (RT WING) · airframe 87,829 hrs · 22,174 cycles

RIGHT HAND WING LEADING EDGE BEADED DOUBLER FOUND CRACKS AT STATION XOS 740. REPAIR CARRIED OUT AT RIGHT HAND WING LEADING EDGE DOUBLER AT STATION XOS 740 AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 87,829 hrs · 22,174 cycles

RIGHT HAND WING LEADING EDGE BEADED DOUBLER FOUND CRACK AT STATION XOS 499. REPAIR CARRIED OUT AT RIGHT HAND WING LEADING EDGE DOUBLER AT STATION XOS 499 AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 87,829 hrs · 22,174 cycles

RIGHT HAND WING LEADING EDGE BEADED DOUBLER FOUND CRACKS AT STATION XOS 650 - 653. REPAIR CARRIED OUT AT RIGHT HAND WING LEADING EDGE DOUBLER AT STATION XOS 650 - XOS 653 AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 87,829 hrs · 22,174 cycles

AGING AIRCRAFT EXISTING REPAIR AT MAIN DECK CARGO SEAT TRACK STATION 1531 TO STATION 5-63 X = -8.5. RIGHT HAND SIDE EXISTING REPAIR AT MAIN DECK CARGO SEAT TRACK STATION 1531 TO STATION 5-63 X=-8.5. RIGHT HAND SIDE EVALUATED AND FOUND DAMAGED AT STATION 5-10. MATERIAL DAMAGED AT CROWN = 0.300". EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. SEAT TRACK REPAIR CARRIED OUT FROM STATION 1531/5-0 TO STA 5-63 X= -8.5 RIGHT HAND SIDE IN ACCORDANCE WITH SRM 53-00-52-2R FIGURE 201 REPAIR 1. EO 1-5100-7-5001 B6 PART 1 TITLE: STRUCTURES - REPAIR CATALOG - REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 87,829 hrs · 22,174 cycles

AGING AIRCRAFT EXISTING REPAIR AT MAIN DECK CARGO SEAT TRACK STATION 625 TO STATION 645 X = - 47.5. RIGHT HAND SIDE EXISTING REPAIR AT MAIN DECK CARGO SEAT TRACK STATION 625 TO STATION 645 X = - 47.5. RIGHT HAND SIDE EVALUATED AND FOUND DAMAGED AT STATION 630 AND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. MATERIAL DAMAGED 0.300". SEAT TRACK REPAIR CARRIED OUT FROM STATION 625 TO STATION 645 X = - 47.5 RIGHT HAND SIDE IAW SRM 53-00-52-2R FIGURE 201 REPAIR 1. EO 1-5100-7-5001B6 PT1 TITLE : STRUCTURES - REPAIR CATALOG - REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 87,829 hrs · 22,174 cycles

AGING AIRCRAFT EXISTING REPAIR AT MAIN DECK CARGO SEAT TRACK STATION1811 TO STATION 1887 X = - 8.5. RIGHT HAND SIDE EXISTING REPAIR AT MAIN DECK CARGO SEAT TRACK STATION 1811 TO STATION 1887 X = - 8.5. RIGHT HAND SIDE EVALUATED AND FOUND DAMAGED AT SEAT TRACK CROWN AT STATION 1832 AND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. MATERIAL DAMAGED 0.350" MAIN DECK CARGO SEAT TRACK FROM STATION 1811 TO STATION 1887 X = - 8.5 CARRIED OUT REPAIR IAW SRM 53-00-52-2R FIGURE 201 REPAIR 1. EO 1-5100-7-5001B6 PART 1 TITLE : "STRUCTURES - REPAIR CATALOG - REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707" ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 87,829 hrs · 22,174 cycles

AGING AIRCRAFT EXISTING REPAIR AT MAIN DECK CARGO SEAT TRACK STATION 1771 TO STATION 1831 X = 47.5. LEFT HAND SIDE EXISTING REPAIR AT MAIN DECK CARGO SEAT TRACK STATION 1771 TO STATION 1831 X = 47.5. LEFT HAND SIDE EVALUATED AND FOUND SEAT TRACK CROWN DAMAGE AT STATION 1801 AND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. MATERIAL DAMAGED : 0.390". SEAT TRACK REPAIR CARRIED OUT FROM STATION 1771 TO STATION 1831 X = 47.5 IAW SRM 53-00-52-2R FIGURE 201 REPAIR 1. EO 1-5100-7-5001B6 PART 1 TITLE : "STRUCTURES - REPAIR CATALOG - REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707" ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 87,829 hrs · 22,174 cycles

AGING AIRCRAFT EXISTING REPAIR AT MAIN DECK CARGO SEAT TRACK STATION 725 TO STATION 765 X = 47.5. LEFT HAND SIDE EXISTING REPAIR AT MAIN DECK CARGO SEAT TRACK STATION 725 TO STATION 765 X = 47.5. LEFT HAND SIDE EVALUATED AND FOUND DAMAGED AT STATION 758 AND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. MATERIAL DAMAGED : 0.350". SEAT TRACK REPAIR CARRIED OUT FROM STATION 725 TO STATION 765 X = 47.5 LEFT HAND SIDE IAW SRM 53-00-52-2R FIGURE 201 REPAIR 1. EO 1-5100-7-5001B6 PT1 TITLE : STRUCTURES - REPAIR CATALOG - REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 87,829 hrs · 22,174 cycles

AGING AIRCRAFT EXISTING REPAIR AT MAIN DECK CARGO SEAT TRACK STATION1401 TO STATION 1531 X = - 47.5. EXISTING REPAIR AT MAIN DECK CARGO SEAT TRACK STATION 1401 TO STATION 1531 X= -47.5. EVALUATED AND FOUND DAMAGED AT STATION 1418. MATERIAL DAMAGED AT CROWN = 0.300" EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. SEAT TRACK REPAIR CARRIED OUT FROM STATION 1401 TO STATION 1531 X= -47.5 IN ACCORDANCE WITH SRM 53-00-52-2R FIGURE 201 REPAIR 1. EO 1-5100-7-5001 B6 PART 1 TITLE: STRUCTURES - REPAIR CATALOG - REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CRACKED (RT WING) · airframe 87,829 hrs · 22,174 cycles

RIGHT HAND WING LEADING EDGE LOWER SKIN AND SUPPORT DOUBLER FOUND CRACK AT STATION XOS 995.5. REPAIR CARRIED OUT AT RIGHT HAND WING LEADING EDGE LOWER SKIN AND SUPPORT DOUBLER AT STATION XOS 995.5 AS PER SRM 57-40-01-2R FIGURE 201 REPAIR 9. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. INITIAL INSPECTION TO BE CARRIED OUT AT 24 MONTHS (AFTER REPAIR EMBODIMENT) AND REPETITIVE INSPECTION TO BE CARRIED OUT AT EVERY 24 MONTHS BY VISUAL INSPECTION AS PER SRM 57-40-01-2R REPAIR 9 TABLE 201.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 87,829 hrs · 22,174 cycles

AGING AIRCRAFT EXISTING REPAIR AT MAIN DECK CARGO SEAT TRACK STATION 745 TO STATION 765 X = - 8.5 RIGHT HAND SIDE. EXISTING REPAIR AT MAIN DECK CARGO SEAT TRACK STATION 745 TO STATION 765 X = - 8.5 RIGHT HAND SIDE EVALUATED AND FOUND DAMAGED AT STATION 761 AND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. MATERIAL DAMAGED 0.350". SEAT TRACK REPAIR CARRIED OUT FROM STATION 745 TO STATION 765 X = - 8.5 RIGHT HAND SIDE IAW SRM 53-00-52-2R FIGURE 201 REPAIR 1. EO 1-5100-7-5001B6 PT1 TITLE : STRUCTURES - REPAIR CATALOG - REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707. ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 87,829 hrs · 22,174 cycles

AGING AIRCRAFT EXISTING REPAIR AT MAIN DECK CARGO SEAT TRACK STATION 745 TO STATION 785 X = 27.5. LEFT HAND SIDE EXISTING REPAIR AT MAIN DECK CARGO SEAT TRACK STATION 745 TO STATION 785 X = 27.5. LEFT HAND SIDE EVALUATED AND FOUND DAMAGED AT STATION 755 AND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. MATERIAL DAMAGED : 0.380" SEAT TRACK REPAIR CARRIED OUT FROM STATION 745 TO STATION 785 X = 27.5 LEFT HAND SIDE IAW SRM 53-00-52-2R FIGURE 201 REPAIR 1. EO 1-5100-7-5001B6 PT1 TITLE : STRUCTURES - REPAIR CATALOG - REPAIR IDENTIFICATION AND TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 87,829 hrs · 22,174 cycles

AGING AIRCRAFT EXISTING REPAIR AT MAIN DECK CARGO SEAT TRACK STATION 625 TO STATION 645 X = - 8.5. RIGHT HAND SIDE EXISTING REPAIR AT MAIN DECK CARGO SEAT TRACK STATION 625 TO STATION 645 X = - 8.5. RIGHT HAND SIDE EVALUATED AND FOUND DAMAGED AT STATION 630 AND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. MATERIAL DAMAGED : 0.380". SEAT TRACK REPAIR CARRIED OUT FROM STATION 625 TO STATION 645 X = - 8.5 RIGHT HAND SIDE IAW SRM 53-00-52-2R FIGURE 201 REPAIR 1. EO 1-5100-7-5001B6 PT1 TITLE : STRUCTURES - REPAIR CATALOG - REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 87,829 hrs · 22,174 cycles

AGING AIRCRAFT EXISTING REPAIR AT MAIN DECK CARGO SEAT TRACK STATION1310 TO STATION 1390 X = - 27.5. RIGHT HAND SIDE EXISTING REPAIR AT MAIN DECK CARGO SEAT TRACK STATION 1310 TO STATION 1390 X= -27.5. RIGHT HAND SIDE EVALUATED AND FOUND DAMAGED AT STATION 1358. MATERIAL DAMAGE AT CROWN= 0.350". EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. SEAT TRACK REPAIR CARRIED OUT FROM STATION 1310 TO STATION 1390 X= -27.5 IN ACCORDANCE WITH SRM 53-00-52-2R FIGURE 201 REPAIR 1. EO 1-5100-7-5001 B6 PART 1 TITLE: STRUCTURES - REPAIR CATALOG - REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: LONGERON FITTING — CRACKED (FUSELAGE) · airframe 87,829 hrs · 22,174 cycles

CRACK INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION ON EXISTING REPAIR LONGERON FITTING LOWER FASTENER HOLE AT RIGHT HAND SIDE NOSE LANDING GEAR TRUNNION FITTING.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 87,829 hrs · 22,174 cycles

CRACK INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION ON EXISTING REPAIR. LONGERON FITTING LOWER FASTENER HOLE AT RIGHT HAND SIDE NOSE LANDING GEAR TRUNION FITTING RIGHT HAND SIDE NOSE LANDING GEAR TRUNION FITTING STATION 595 LOWER LONGERON. REMOVED AND REPLACED WITH NEW LONGERON AS PER SRM 51-35-01-0G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 87,829 hrs · 22,174 cycles

CABIN, FOUND SEAT TRACK AT STATION 880 X = - 27.5 CROWN DAMAGED. CABIN, AT SEAT TRACK STATION 880 X = - 27.5, DAMAGED CROWN EVALUATED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE101 ALLOWABLE DAMAGE 1. CROWN DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 869 TO STATION 909 X = - 27.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FITTING — CRACKED (NLG TRUNNION) · airframe 87,829 hrs · 22,174 cycles

AGING AIRCRAFT EXISTING REPAIR AT RIGHT HAND NOSE LANDING GEAR TRUNNION FITTING STATION Y=595. EXISTING REPAIR AT RIGHT HAND NOSE LANDING GEAR TRUNNION FITTING STATION Y=595 EVALUATED AND FOUND REPAIRED AREA CRACKED. APPROXIMATE CRACK LENGTH AT 0.300" AND 0.400". REPAIR CARRIED OUT IN ACCORDANCE WITH SRM 53-10-14-2R FIGURE 202 REPAIR 2. EO 1-5100-7-5001 B6 PART 1 TITLE: STRUCTURES - REPAIR CATALOG - REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. DUE TO CAT B REPAIR, REQUIRE INITIAL INSPECTION AT 1,500 FLIGHT CYCLES WITH REPETITIVE INSPECTIONS AT EVERY 1,500 FLIGHT CYCLES AS PER SRM 53-10-14-2R TABLE 201 FIGURE 202 / REPAIR 2.

Part: FITTING — CRACKED (NLG TRUNNION) · airframe 87,829 hrs · 22,174 cycles

AGING AIRCRAFT EXISTING REPAIR AT LEFT HAND NOSE LANDING GEAR TRUNNION FITTING STATION Y=595. EXISTING REPAIR AT LEFT HAND NOSE LANDING GEAR TRUNNION FITTING STATION Y= 595 EVALUATED AND FOUND CRACKED. REPAIR CARRIED OUT IN ACCORDANCE WITH SRM 53-10-14-2R FIGURE 202 REPAIR 2. EO 1-5100-7-5001 B6 PART 1 TITLE: "STRUCTURES - REPAIR CATALOG - REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707" ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. DUE TO CATEGORY B REPAIR, INITIAL INSPECTION IS REQUIRED AT 1,500 FLIGHT CYCLE WITH REPETITIVE INSPECTIONS AT EVERY 1,500 FLIGHT CYCLE AS PER SRM 53-10-14-2R TABLE 201 FIGURE 202 / REPAIR 2.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 87,829 hrs · 22,174 cycles

CABIN, FOUND SEAT TRACK AT STATION 1017, X = - 47.5 CROWN DAMAGED. CABIN, AT SEAT TRACK STATION 1017, X= - 47.5 DAMAGED CROWN EVALUATED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMANT FROM STATION 989 TO EXISTING SPLICE STATION 1069 X = - 47.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 87,829 hrs · 22,174 cycles

CABIN, FOUND SEAT TRACK AT STATION 878, X = 47.5 CROWN DAMAGED. CABIN, AT SEAT TRACK STATION 878, X = 47.5, DAMAGED CROWN EVALUATED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT EXISTING SPLICES STATION 831 TO STATION 929 X = 47.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REFER TO SNRM N00483 FOR WORK DETAILS. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 87,829 hrs · 22,174 cycles

CABIN, FOUND SEAT TRACK AT STATION 886, X = 47.5 WITH CROWN DAMAGED. CABIN, AT SEAT TRACK STATION 886, X = 47.5, DAMAGED CROWN EVALUATED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT EXISTING SPLICES STATION 831 TO STATION 929 X = 47.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: BEAM — CRACKED (R3 DOOR) · airframe 87,829 hrs · 22,174 cycles

CABIN, AT R3 PLUG DOOR NR 1 STOP BEAM FOUND CRACKED AT AFT.

Part: BEAM — CRACKED (R3 DOOR) · airframe 87,829 hrs · 22,174 cycles

CABIN AT R3 PLUG DOOR NR 1 STOP BEAM FOUND CRACKED AT AFT. CABIN AT R3 PLUG DOOR, CRACKED NR 1 STOP BEAM REMOVED AND REPLACED AS PER SRM 51-31-01-0G. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 87,829 hrs · 22,174 cycles

AGING AIRCRAFT - EXISTING REPAIR FOUND AT CENTER CARGO COMPARTMENT FLOORBEAM WEB STATION 1841 BETWEEN X = - 30 TO X = - 57. EXISTING REPAIR AT CENTER CARGO COMPARTMENT FLOORBEAM WEB AT STA 1841 BETWEEN X= -30 TO X= -57 EVALUATED AND FOUND DAMAGE AT WEB AREA STATION 1841 X= -30 TO X= -57. CARRIED OUT REPAIR IN ACCORDANCE WITH SRM 53-00-00-2R FIGURE 211 REPAIR GENERAL. EO 1-5100-7-5001 B6 PART 1 TITLE: STRUCTURES - REPAIR CATALOG - REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — DAMAGED (LT WING) · airframe 87,829 hrs · 22,174 cycles

AGING AIRCRAFT - EXISTING REPAIR AT LEFT HAND WING FIXED LEADING EDGE UPPER SKIN XIS 247. EXISTING REPAIR AT LEFT HAND WING FIXED LEADING EDGE UPPER SKIN XIS 247 EVALUATED AND FOUND EXISTING REPAIR DOUBLER DAMAGED. LEFT HAND WING FIXED LEADING EDGE XIS 247 CARRIED OUT REPAIR IN ACCORDANCE WITH SRM 57-40-02-2R REPAIR 201 REPAIR 8. EO # 1-5100-7-5001 B6 PART 1 TITLE: "STRUCTURES - REPAIR CATALOG - MD11 - REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 12.707" ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: ADC — FAILED (NR 1) · airframe 86,961 hrs · 21,933 cycles

FOLLOWING LIGHT TURBULENCE AND PRECIPITATION AT 370 SIMULTANEOUS AP1 DISCONNECT ACCOMPANIED BY WINDSHEAR DET FAIL, SELECT FADEC ALT, SEL EVEV FEEL MAN SEL FLAP LIM OVRD AND ALT MISCOMPARE ON PFD. RAN QRH AIRSPEED UNRELIABLE CHECK LIST SWAPPED TO AUX ON 1 UPPER MAINT PANEL. APPEARED TO FIX ISSUE (CADA1) BUT AFTER 20 MIN, CADC FAILED. RERAN AIRSPEED UNRELIABLE AND PUT F/O ON 1 (CADA AND FLT DIR) REPLACED NR 1 CADC AND NR 2 CADC PER AMM 34-16-01-4.

Part: TRANSMITTER — FAILED (HYD SYSTEM) · airframe 84,840 hrs · 21,365 cycles

DURING ARRIVAL RECEIVED "HYD 2 OFF" ALERT. QUANTITY WAS LOW,AND QUANTITY WAS 2.8. RAN QRH. CONTINUED APPROACH. AS WE EXTENDED FLAPS TO 35,RECEIVED "HYD 2 QTY LOW",RAN HYD 2 QTY LOW CHECKLIST. LANDED UNEVENTFULLY.LOWEST QUANTITY IN FLIGHT WAS 1.2. REF WRI 29-01/8568 , COMPLIED STEP #1 , #3 , #5, ITEM CLOSED, R & R #2 HYD QTY XMITTER PER AMM 29-32-02-5 , PERFORM HYDRAULIC SYSTEM RESERVOIR QUANTITY INDICATING TRANSMITTER OPERATIONAL TEST PER AMM 29-32-02-5 , TEST OK .

Part: WARNING MESSAGE — FALSE ACTIVATION (AIR SYSTEM) · airframe 84,081 hrs · 21,137 cycles

DURING CLIMBOUT BELOW 18000 FEET RECEIVED LVL 1 AIR SYS OFF ALERT. AT FIRST SYSTEM 2 WENT FROM RED ON SYNOPTIC BUT QUICKLY TURNED AMBER. C/W PNEUMATIC MANIFOLD 2- ESC LRU INOP, RESET IAW AMM-21-08-01-5 AND ECS RTS, TEST PASSED. C/W NR 2 PNEUMATIC SYSTEM DECAY WITH ENGINES IAW AMM-36-00-02-5 NOTED DECAY CHECK IS OK FOR SERVICE. C/W MANIFOLD CONTROLLER RTS IAW AMM-36-23-01-5, TEST PASSED WITH NO CURRENT FAULTS. C/W, NR 2 MANIFOLD FAILURE DETECTION TEST IAW AMM-36-23-00-5. TEST PASSED. C/W FIM-36-23-01 FIGURE 103, STEPS 1-2-3. SYSTEM OK. C/W POWER ASSURANCE TEST FOR NR 2 ENGINE IAW JRH-7-10 ALL TESTS PASSED. COULD NOT DUPLICATE ANY NR 2 MANIFOLD FAILURES. OK FOR CONTINUED SERVICE.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 83,745 hrs · 21,050 cycles

MDIS 602 51-00 8049 14OCT18 MEM OPEN U FASTENER HEAD MISSING ON FUSELAGE REPAIR DOUBLER, NEAR LOWER BEACON. SHGN 14OCT18 15:49 MEM U UPON FURTHER INVESTIGATION, FOUND DOUBLER BULGING, CONTAINING POPPED RIVETS, AND SHEDDING WHITE POWDER FROM THE RIVET HOLE. ONE CAN ASSUME THAT THERE IS CORROSION BENEATH THE DOUBLER. SHGN 14OCT18 21:22 MEM U CORRECT ASSUMPTION, STRINGER BENEATH DOUBLER CONTAINS INTERGRANULAR CORROSION WHICH IS CAUSING THE SKIN TO BULGE PART 15OCT18 03:06 MEM U IDENTIFIED PARTS HAT-EXTRUDED MPN: 1D0554T CPN: 0222366 QTY: 1 PART 15OCT18 03:06 MEM U ORDER PART MPN: 1D0554T CPN: 0222366 QTY: 1 MSN: 1938000 SHGN 15OCT18 22:08 MEM U CUT OUT SECTION OF CORRODED LONGERON PER SRM 53-00-05-2R. ALSO REMOVE

Part: PANEL — CRACKED (RT WING) · airframe 83,279 hrs · 20,926 cycles

RT WING OUTBOARD L/E PANEL 626AB CRACKED AT STA XOS 842. REPAIR CARRIED OUT PER EA 1-5730-T0340910 P1. CRACKED RT WING LE DOOR PANEL SKIN REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 83,279 hrs · 20,926 cycles

MAIN DECK FLOOR CURVE SEAT TRACK AT STA 465, X= - 75.25 FOUND CORROSION. CORROSION REMOVED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIG 101 ALLOWABLE DAMAGE 1. SEAT TRACK REPAIRED AS PER EA 1-5310-T0340599 PT 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 83,279 hrs · 20,926 cycles

MAIN DECK FLOOR CURVE SEAT TRACK AT STA 455, X = - 107 FOUND CORROSION. CORROSION FOUND EXFOLIATED AND EXCEED LIMIT AS PER SRM 53-00-52-1A FIG 101 ALLOWABLE DAMAGE 1. SEAT TRACK R&R FROM STA 414 TO STA 484, X = -107 AS PER SRM 51-31-01-0G. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 83,279 hrs · 20,926 cycles

MAIN DECK AFT FLOOR SUPPORT AT STA 1914-2007, X = 22 FOUND CORROSION MARKED. CORROSION REMOVED AND FOUND EXCEED LIMIT PER SRM 53-00-00-2R FIG 206. FLOOR SUPPORT REMOVED PER SRM 51-31-01-0G. NEW FLOOR SUPPORT FABRICATED PER DRAWING AGA7088 REV B AND INSTALLED PER SRM 51-31-01-0G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 83,279 hrs · 20,926 cycles

MAIN DECK AFT FLOOR SUPPORT AT STA 1887-2007, X = 2 FOUND CRACKED AS MARKED. FLOOR SUPPORT REMOVED AND REPLACED AS PER SRM 51-31-01-0G. NEW FLOOR SUPPORT FABRICATED AS PER DWG AGA7081 REV M. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 83,279 hrs · 20,926 cycles

MAIN DECK AFT FLOOR SUPPORT AT STA 1887-2007, X = - 2 FOUND CORROSION AS MARKED. CORROSION REMOVED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-00-2R FIG 206. FLOOR SUPPORT REMOVED AND REPLACED AS PER SRM 51-31-01-0G. NEW FLOOR SUPPORT FABRICATED AS PER DWG AGA 7080 REV M. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 83,279 hrs · 20,926 cycles

MAIN DECK FLOOR SEAT TRACK AT STA 1282, X=47.5 FOUND CROWN DAMAGED AS MARKED. SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STA 1269 TO STA 1351, X =47.5 AS PER SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. DAMAGE EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIG 101 ALLOWABLE DAMAGE 1.

Part: SUPPORT — CRACKED (WING) · airframe 83,279 hrs · 20,926 cycles

WING UPPER AUX TANK PANEL 142AZ CUTOUT INTERIOR COMPARTMENT UPPER STRINGER SUPPORT CRACKED. STRINGER SUPPORT TEE REMOVED AND REPLACED AS PER SRM 51-33-01-0G. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 83,279 hrs · 20,926 cycles

RIGHT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 613 FOUND CRACK. REPAIR CARRIED OUT ON BEADED DOUBLER AT STA XOS 613 AS PER SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (LT WING) · airframe 83,279 hrs · 20,926 cycles

LT WING FIXED L/E COMPARTMENT STA XOS 791 STRINGER CRACKED. REPAIR CARRIED OUT ON LT WING FIXED L/E COMPARTMENT AT STA XOS 791 STRINGER AS PER SRM 57-40-03-2R FIG 201 REPAIR 2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FORMER — CRACKED (RT WING) · airframe 83,279 hrs · 20,926 cycles

RIGHT WING FIXED LEADING EDGE FORMER AT XOS 584 FOUND CRACK. FORMER REMOVED AND REPLACED AS PER SRM 51-31-01-0G. FORMER FABRICATED AS PER DWG ARB 2931 REV H. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 83,279 hrs · 20,926 cycles

MAIN DECK FLOOR SEAT TRACK AT STA 1641, X= 8.5 FOUND CORROSION AS MARKED. CORROSION REMOVED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIG 101 ALLOWABLE DAMAGE 1. SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STA 1711 TO EXISTING SPLICE AT STA 1571, X= 8.5 AS PER SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PWER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 83,279 hrs · 20,926 cycles

RIGHT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 664 WAS FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R, FIG 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 83,279 hrs · 20,926 cycles

EXISTING REPAIR DOUBLER ON FUSELAGE SKIN ABA 7057-1 AT STA 275 FOUND CRACK. CRACKED EXISTING REPAIR DOUBLER ON FUSELAGE SKIN ABA7075-1 AT STA 275 CARRIED OUT REPAIR AS PER EA 1-5330-T0310125 A PART 3, TITLE: FUSELAGE - PLATES & SKINS. FUSELAGE SKIN TRIMOUT REPAIR AT STA 275. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CHAFED (LE SLAT) · airframe 83,279 hrs · 20,926 cycles

LT WING NR 2 SLAT ASSY I/B LOWER SURFACE FOUND WITH CHAFED MARK AT STA XIS 247 TO STA XIS 253. REPAIR CARRIED OUT ON LT WING NR 2 SLAT ASSY I/B LOWER EDGE SURFACE AT STA XIS 247 TO STA XIS 253 AS PER EA 1-5750-T0340634 P1, TITLE: WINGS-FLIGHT SURFACES LT WING NR 2 SLAT ASSY CHAFE DAMAGE FOUND ON OUTER SKIN, INNER SURFACE BETWEEN STA XIS 247.028 AND STA XIS 253.212. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CORRODED (LT WING) · airframe 83,279 hrs · 20,926 cycles

LT WING UPPER SURFACE DOUBLER FOUND CORRODED. REPAIRED IAW EA 1-5730-T0340596 P1.

Part: DOUBLER — CRACKED (RT WING) · airframe 83,279 hrs · 20,926 cycles

RT WING LE COMPARTMENT STA XOS 906 DOUBLER CRACKED. DOUBLER REMOVED AND REPLACED AS PER SRM 51-31-01-0G. DOUBLER FABRICATED AS PER DWG ARB3954 REV K. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 83,279 hrs · 20,926 cycles

MAIN DECK FLOOR SEAT TRACK AT STA 1141, X= - 8.5 FOUND CROWN DAMAGED AS MARKED. SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STA 1331 TO STA 1451, X= - 8.5 AS PER SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. SEAT TRACK CROWN DAMAGED AT STA 1411, X= - 8.5 EXCEEDED LIMIT AS PER SRM 53-00-52 -1A FIG 101 ALLOWABLE DAMAGE 1.

Part: DOUBLER — CRACKED (RT WING) · airframe 83,279 hrs · 20,926 cycles

RIGHT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 755 FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R FIG 203 REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 83,279 hrs · 20,926 cycles

MAIN DECK FLOOR SEAT TRACK AT STA 1336, X = - 8.5 FOUND CORROSION AS MARKED. CORROSION REMOVED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIG 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STA 1331 TO STA 1451, X= - 8.5 AS PER SRM 53-00-52-2R FIG 201 REPAIR 1. REFER TO SNRM N00451 FOR WORK DETAILS. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 83,279 hrs · 20,926 cycles

RIGHT WING FIXED LEADING EDGE RIB DOUBLER AT XOS 584. FOUND CRACK AFTER REMOVAL OF FORMER. DOUBLER REMOVED AND REPLACED AS PER 51-31-01-0G. DOUBLER FABRICATED AS PER DWG ARB3954 REV K. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FORMER — CRACKED (LT WING) · airframe 83,279 hrs · 20,926 cycles

LT WING FIXED LE COMPARTMENT STA XOS 698 FORMER SUSPECT CRACK. FORMER REMOVED AND REPLACED AS PER SRM 51-31-01-0G. FORMER FABRICATED AS PER DWG ARB2930 REV F. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CORRODED (RT WING) · airframe 83,279 hrs · 20,926 cycles

RT WING UPPER SURFACE DIAMOND DOUBLER SURFACE FOUND CORROSION. REPAIRED AS PER EA 1-5730-T0340753, PT 1.

Part: SKIN — CHAFED (LE SLAT) · airframe 83,279 hrs · 20,926 cycles

LT WING 31 SLAT ASSY O/B LOWER SURFACE FOUND WITH CHAFED MARK AT STA XIS 240 AND STA XIS 246. REPAIR CARRIED OUT ON LT WING NR 1 SLAT ASSY O/B LOWER EDGE SURFACE AT STA XIS 240 AND STA XIS 246 AS PER EA 1-5750-T0340850 P1, TITLE: WINGS-FLIGHT SURFACES-LT WING NR 1 SLAT ASSY SRM REPAIR ON OUTER SKIN ALONG LOWER AFT EDGE, BETWEEN STA XIS 240 AND STA XIS 246. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO WRI 57507811 FOR WORK DETAILS.

Part: DOUBLER — CRACKED (LT WING) · airframe 83,279 hrs · 20,926 cycles

LT WING FIXED L/E COMPARTMENT STA XOS 906 DOUBLER CRACKED. DOUBLER REMOVED AND REPLACED AS PER SRM 51-31-01-0G. DOUBLER FABRICATED AS PER DWG ARB3954 REV K. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 83,279 hrs · 20,926 cycles

MAIN DECK FLOOR SEAT TRACK AT STA 1411, X = 8.5 FOUND CROWN DAMAGE AS MARKED. SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STA 1371 TO STA 1451, X= 8.5 AS PER SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. SEAT TRACK CROWN DAMAGED AT STA 1411, X= 8.5 EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIG 101 ALLOWABLE DAMAGE 1.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 83,279 hrs · 20,926 cycles

MAIN DECK FLOOR SEAT TRACK AT STA 1661, X= - 8.5 FOUND CROWN DAMAGED AS MARKED. DAMAGED CROWN BLEND OUT AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIG 101 ALLOWABLE DAMAGE 1. SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STA 1711 TO EXISTING SPLICE AT STA 1571, X=- 8.5 AS PER SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CHAFED (LT WING) · airframe 83,279 hrs · 20,926 cycles

LT WING I/B FIXED L/E UPPER SURFACE STA XIS 247 FOUND WITH CHAFED MARK. REPAIR CARRIED OUT ON LT WING I/B FIXED L/E UPPER SURFACE AT STA XIS 247 AS PER SRM 57-40-02-2R FIG 201 REPAIR 8. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FORMER — CRACKED (LT WING) · airframe 83,279 hrs · 20,926 cycles

LT WING FIXED L/E COMPARTMENT STA XOS 584 FORMER CRACKED. FORMER ON LT WING FIXED L/E COMPARTMENT AT STA XOS 584 REMOVED AND REPLACED AS PER SRM 51-31-01-0G. FORMER FABRICATED AS PER DWG ARB2931 REV H. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 83,279 hrs · 20,926 cycles

MAIN DECK FLOOR SEAT TRACK AT STA 1511, X = -27.5 FOUND CORROSION AS MARKED. SEAT TRACK CORROSION FOUND EXCEEDED LIMIT PER SRM 53-00-52-1A FIG 101 ALLOWABLE DAMAGE 1. SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STA 1471 TO EXISTING SPLICE STA 1531, X = - 27.5 PER SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: IRU — MALFUNCTIONED · airframe 82,303 hrs · 20,599 cycles

UNABLE RNP ALERT AT CRUISE. ATC ADVISED OF OUR STATUS. ATC LATER INFORMED US WE WERE 40 MILES WEST OFF COURSE. DURING CREW DEBRIEF THE POS OF RNP ACTUAL WAS SHOWING 1.00/6.00 NM. IRS/GNS POS UPON ARRIVAL SHOWED ALL THREE IRUS GREATLY MISCOMPARED LAT/LONG TO EACH OTHER AND TO GNS. DOWNPOWERED IRU'S, RESET FMC CIRCUIT BREAKERS IAW MM 34-63-09, REALLIGNED IRU'S IAW MM 34-43-00-5 WITH ALL IRUS AND GNS'S MATCHING PERFECTLY. NO UNABLE GNS MESSAGE PRESENT. AFTER RESET RNP/ACTUAL WAS READING 1.00/0.02NM. ACFT OK FOR SERVICRE. ACCOMPLISHED R-T-S OF IRU'S PER MM 34-43-00-5, ALL CHECKED NORMAL, OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (R1 DOOR) · airframe 80,709 hrs · 20,166 cycles

DURING A POST FLIGHT INSPECTION, FOUND THE R1 DOOR SLIDE INDICATOR LIGHT INOPERATIVE. R & R THE R1 DOOR INDICATOR ASSEMBLY IAW AMM 25-61-04-4, OPS CHECKED OK.

Part: CONNECTOR — OUT OF ALIGNMENT (SWITCH) · airframe 80,471 hrs · 20,097 cycles

RIGHT CABIN, FWD DOOR ESCAPE SLIDE BOTTLE PRESSURE LIGHT INOPERATIVE. FOUND LIGHT SWITCH AFT CONNECTOR MISALIGNED, REPOSITIONNED CONNECTOR IAW ELECT PRACTICE. OPS CHECKED OK IAW MM 25-61-06-5.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,836 hrs · 19,594 cycles

FWD CABIN MAIN DECK CARGO FLOOR SUPPORT CORRODED AT BS 494, X -57.0. FWD CABIN, MAIN DECK CARGO COMPARTMENT. CORRODED FLOOR SUPPORT AT RT STA 494, X= -57.0. R & R NEW FLOOR SUPPORT FROM STA 459 TO STA 515 X=-57.0 IAW SRM 51-31-01-0G. NEW FLOOR SUPPORT FABRICATED IAW DWG ACA 7364, REV A. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,836 hrs · 19,594 cycles

CABIN, MAIN DECK CARGO FLOOR PANEL OPENED UP FOR CORRODED CLIP NUT REPLACEMENT. FOUND SEAT TRACK FLANGE CORROSIONS AT RT STA 790, X=-75.25. SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STA 765 TO STA 815 X=-75.25 AS PER SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — DENTED (LE SLAT) · airframe 78,836 hrs · 19,594 cycles

LEFT WING NR 4 SLAT UPPER SURFACE FOUND DENTED AT STA XOS 554.894 TO STA 560.200. DENT EXCEEDED LIMIT OF ALLOWABLE SRM 57-40-02-2R FIG 201 REPAIR 6. DAMAGED AREA TRIM OUT AND REPAIR DOUBLER INSTALLED PER EA 1-5750-T0326476. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO WRI 57504763 FOR WORK DETAILS.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,836 hrs · 19,594 cycles

MAIN DECK FLOOR SEAT TRACK FLANGE LOWER SIDE FOUND CORROSION AT STA 1820, X=-8, OTBD. SEAT TRACK REPAIRED PER SRM 53-00-52-2R FIG 201 REPAIR 1. REFER TO SNRM N00987 FOR WORK DETAILS. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,836 hrs · 19,594 cycles

MAIN DECK FLOOR SEAT TRACK FLANGE LOWER SIDE FOUND CORROSION AT STA 1821-1854, X=-8, INBD. SEAT TRACK REPAIRED PER SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,836 hrs · 19,594 cycles

MAIN DECK FLOOR SEAT TRACK FLANGE LOWER SIDE FOUND CORROSION AT STA 1821-1841, X=8, OTBD. SEAT TRACK REPLACEMENT FROM STA 1771 TO STA 1887 X= 8 PER SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,836 hrs · 19,594 cycles

MAIN DECK, AFT CABIN RT FLOOR SUPPORT AT STA 1887 -STA 2007, X=-57 FOUND CORROSION AS MARKED.

Part: BUSHING — CORRODED (TE FLAP VANE) · corrosion level 2 · airframe 78,836 hrs · 19,594 cycles

LEFT WING OTBD FLAP VANE FITTING C, BUSHING HOLE CORRODED. BUSHING HOLE REWORKED AND FOUND EXCEED LIMIT AS PER SRM 57-50-02-2R FIGURE 201. EXISTING HOLE SIZE 0.856" X 0.597", FINAL HOLE SIZE: 0.997" X 0.704", MAXIMUM ALLOWABLE LIMIT: 0.940" X 0.670". OVERSIZE BUSHING FABRICATED AND INSTALLED PER EA 1-5750-T0326517 PART 1 STEP 2B. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO WRI: 57504768 FOR WORK DETAILS.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 78,836 hrs · 19,594 cycles

MAIN DECK LT FLOOR SEAT TRACK AT STA 755, X= 27.5 FOUND CRACKED AS MARKED. SEAT TRACK REPAIRED PER SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 78,836 hrs · 19,594 cycles

MAIN DECK LT FLOOR SEAT TRACK AT STA 755, X=47.5 FOUND CRACKED AS MARKED. SEAT TRACK REPAIRED PER SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: BUSHING — CORRODED (TE FLAP VANE) · corrosion level 2 · airframe 78,836 hrs · 19,594 cycles

LT WING OTBD FLAP VANE FITTING D, BUSHING HOLE, CORRODED. BUSHING HOLE REWORKED AND FOUND EXCEED LIMIT AS PER SRM 57-50-02-2R FIGURE 201. EXISTING HOLE SIZE 0.876" X 0.580", FINAL HOLE SIZE: 0.953" X 0.660", MAXIMUM ALLOWABLE LIMIT: 0.940" X 0.670". OVERSIZE BUSHING FABRICATED AND INSTALLED PER EA 1-5750-T0326517 PART 1 STEP 2D. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO WRI: 57504768 FOR WORK DETAILS.

Part: WEB — CRACKED (FUSELAGE) · airframe 78,836 hrs · 19,594 cycles

MAIN DECK R3 DOOR AFT JAMB LOWER WEB BOX AT STA 1305.25-STA 1315.42, LONGERON L26R-L27R FOUND CRACKED AS MARKED. WEB BOX REPAIRED PER SRM 53-40-15-2R FIG 201 REPAIR 3. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (TE FLAP) · corrosion level 2 · airframe 78,836 hrs · 19,594 cycles

LEFT WING OTBD FLAP, FLAP SIDE, INBD AFT HINGE PIVOT INBD HOLE BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT CMM 57-52-04. EXISTING HOLE: DIA 1.154", FINAL HOLE: DIA 1.217", MAXIMUM ALLOWABLE HOLE: DIA 1.150". REPAIR BUSHING FABRICATED AND INSTALLED IAW EA1-5750-T0326466, PART 1, STEP 1A. TITLE: WINGS FLIGHT SURFACES, EO 1-5750-7-5002-LT WINGS-OTBD FLAP-INBD HINGE BRACKET ASSY CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100. REF TO WRI: 57504777 FOR WORK DETAILS.

Part: BUSHING — CORRODED (TE FLAP VANE) · corrosion level 2 · airframe 78,836 hrs · 19,594 cycles

LEFT WING OTBD FLAP VANE FITTING F, BUSHING HOLE, CORRODED. BUSHING HOLE CORROSION REWORKED PER SRM 57-50-02-2R FIGURE 201 AND FOUND EXCEED LIMIT. EXISTING HOLE SIZE 0.860" X 0.5655", FINAL HOLE SIZE: 0.9565" X 0.6585", MAXIMUM ALLOWABLE LIMIT: 0.940" X 0.670". BUSHING FABRICATED AND INSTALLED PER EA 1-5750-T0326517 PART 1 STEP 2C. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO WRI: 57504768 FOR WORK DETAILS.

Part: BUSHING — CORRODED (TE FLAP VANE) · corrosion level 2 · airframe 78,836 hrs · 19,594 cycles

LT WING OUTBOARD FLAP VANE FITTING 'B' BUSHING HOLE CORROSION. BUSHING HOLE REWORKED AND FOUND EXCEED LIMIT AS PER SRM 57-50-02-2R FIGURE 201. EXISTING HOLE SIZE 0.935" X 0.650", FINAL HOLE SIZE: 1.0325" X 0.740", MAXIMUM ALLOWABLE LIMIT: 0.940" X 0.670". OVERSIZE BUSHING FABRICATED AND INSTALLED PER EA 1-5750-T0326517 PART 1 STEP 2A. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO WRI: 57504768 FOR WORK DETAILS.

Part: BEAM — CORRODED (R3 DOOR) · airframe 78,836 hrs · 19,594 cycles

CABIN MAIN DECK CARGO COMPARTMENT. R3 DOOR PLUG NR 7 LOWER DOOR BEAM DAMAGED.

Part: BRACKET — CORRODED (TE FLAP) · corrosion level 2 · airframe 78,836 hrs · 19,594 cycles

LEFT HAND WING INBOARD FLAP (FLAP SIDE) OUTBOARD AFT HINGE ACTUATOR OUTBOARD HOLE BORE CORRODED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-52-03. EXISTING HOLE DIA: 1.219", FINAL HOLE DIA: 1.235" MAXIMUM ALLOWABLE HOLE DIA: 1.220". OVERSIZE BUSHING FABRICATED BY MACHINING IAW EA NR 1-5750-127720 B, PART 5, STEP 1B AND INSTALLED IAW EA 1-5750-127720 B, PART 5, STEP 1E. TITLE: WINGS, LT WING INBD FLAP OTBD HINGE, FLAP SIDE, PIVOT BORE-REPAIR. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100. REFER TO WRI: 57504773 FOR WORK DETAILS.

Part: HINGE — CORRODED (TE FLAP) · corrosion level 2 · airframe 78,836 hrs · 19,594 cycles

RIGHT WING INBOARD FLAP (FLAP SIDE) OUTBOARD AFT HINGE PIVOT OUTBOARD HOLE BORE CORRODED. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-52-03. EXISTING HOLE: DIA 1.330", FINAL HOLE: DIA 1.336", MAXIMUM ALLOWABLE HOLE: DIA 1.220". OVERSIZE BUSHING FABRICATED IAW EA :1-5750-127721D, PART 5, STEP 1A AND INSTALLED IAW EA: 1-5750-127721D, PART 5, STEP 1C. TITLE: WINGS-RT WING INBD FLAP, OTBD HINGE, FLAP SIDE, PIVOT BORE REPAIR. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100. REFER TO WRI: 57504774 FOR WORK DETAILS.

Part: SKIN — CRACKED (ZONE 200) · airframe 78,836 hrs · 19,594 cycles

TWO CRACK INDICATIONS APPROXIMATE 2.0 INCHES IN LENGTH FOUND DURING X-RAY INSPECTION AT STA 6-0, LONGERON SPLICE 4R AFT SECTION EDGE.

Part: HINGE — CORRODED (TE FLAP) · corrosion level 2 · airframe 78,836 hrs · 19,594 cycles

LEFT WING INBOARD FLAP (FLAP SIDE) OUTBOARD AFT HINGE PIVOT OUTBOARD HOLE BORE CORRODED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-52-03. EXISTING HOLE DIA: 1.294", FINAL HOLE DIA: 1.327", MAXIMUM ALLOWABLE HOLE DIA: 1.220", OVERSIZE BUSHING FABRICATED AND INSTALLED IAW EA NR 1-5750-127720B, PART 5, STEP 1A AND 1E. TITLE: WINGS-LT WING INBD FLAP OTBD HINGE, FLAP SIDE PIVOT BORE-REPAIR. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100. REF TO WRI: 57504773 FOR WORK DETAILS.

Part: HINGE — CORRODED (LT WING) · corrosion level 2 · airframe 78,836 hrs · 19,594 cycles

LEFT WING OUTBOARD FLAP (WING SIDE) INBOARD FWD HINGE PIVOT HOLE BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-08. EXISTING HOLE DIA: 2.311", FINAL HOLE DIA: 2.317", MAXIMUM ALLOWABLE HOLE DIA: 2.3135". REPAIR BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0326464, PART 1, STEP 1B. TITLE: WINGS, FLIGHT SURFACE, EO 1-5750-7-5002, LT WING OTBD FLAP INBD HINGE ASSY, WING SIDE. CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100. REFER TO WRI: 57504778 FOR WORK DETAILS.

Part: HINGE — CORRODED (TE FLAP) · corrosion level 2 · airframe 78,836 hrs · 19,594 cycles

RIGHT WING INBOARD FLAP (FLAP SIDE) OUTBOARD AFT HINGE PIVOT INBOARD HOLE BORE CORRODED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-52-03. EXISTING HOLE: DIA 1.330", FINAL HOLE: DIA 1.336", MAXIMUM ALLOWABLE HOLE: DIA 1.220". OVERSIZE BUSHING FABRICATED IAW EA:1-5750-127721D, PART 5, STEP 1A AND INSTALLED IAW EA: 1-5750-127721D, PART 5, STEP 1D. TITLE: WINGS-RT WING INBD FLAP OTBD HINGE, FLAP SIDE, PIVOT BORE REPAIR. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100. REFER TO WRI:57504774 FOR WORK DETAILS.

Part: HINGE — CORRODED (LT WING) · corrosion level 2 · airframe 78,836 hrs · 19,594 cycles

LEFT WING OUTBOARD FLAP (WING SIDE) INBOARD FWD HINGE LOWER MOUNT INBOARD HOLE BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-08. EXISTING HOLE: DIA 0.706", FINAL HOLE: DIA 0.728", MAXIMUM ALLOWABLE HOLE: DIA 0.709". REPAIR BUSHING FABRICATED IAW EA 1-5750-T0326464, PART 1 STEP 1C AND INSTALLED IAW EA 1-5750-T0326464, PART 1, STEP 1. TITLE: WINGS, FLIGHT SURFACES, EO 1-5750-7-5002, LT WING, OTBD FLAP, INBD HINGE ASSY, WING SIDE, CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100. REFER TO WRI: 57504778 FOR WORK DETAILS.

Part: HINGE — CORRODED (LT WING) · corrosion level 2 · airframe 78,836 hrs · 19,594 cycles

LEFT HAND WING OUTBOARD FLAP (WING SIDE) INBOARD FWD HINGE LOWER MOUNT OUTBOARD HOLE BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-08. EXISTING HOLE DIA: 0.706", FINAL HOLE DIA: 0.728", MAXIMUM ALLOWABLE HOLE DIA: 0.709". REPAIR BUSHING FABRICATED IAW EA 1-5750-T0326464, PART 1, STEP 1C AND INSTALLED IAW EA 1-5750-T0326464, PART 1, STEP 1. TITLE: WINGS, FLIGHT SURFACE-EO 1-5750-7-5002. LT WING, OTBD FLAP INBD BINGE ASSY, WING SIDE CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100 REF TO WRI 57504778 FOR WORK DETAILS.

Part: HINGE — CORRODED (TE FLAP) · corrosion level 2 · airframe 78,836 hrs · 19,594 cycles

LEFT WING INBOARD FLAP (FLAP SIDE) OUTBOARD AFT HINGE PIVOT INBOARD HOLE BORE CORRODED. HINGE REWORKED AND FOUND EXCEED LIMIT PER CMM57-52-03. EXISTING HOLE DIA: 1.294", FINAL HOLE DIA: 1.327", MAXIMUM ALLOWABLE HOLE DIA: 1.220". OVERSIZE BUSHING FABRICATED AND INSTALLED PER EA 1-5750-127720 B PART 5 STEP 1A AND 1E. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO WRI: 57504773 FOR WORK DETAILS.

Part: HINGE — CORRODED (LT WING) · corrosion level 2 · airframe 78,836 hrs · 19,594 cycles

LEFT WING OUTBOARD FLAP (WING SIDE) INBOARD FWD HINGE UPPER MOUNT OUTBOARD HOLE BORE CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING HOLE DIA: 0.942", FINAL HOLE DIA: 0.950", MAXIMUM ALLOWABLE HOLE DIA: 0.944". REPAIR BUSHING FABRICATED AND INSTALLED IAW EA: 1-5750-T0326464, PART 1, STEP 1A. TITLE: WINGS, FLIGHT SURFACES, EO 1-5750-7-5002, LT WING, OTBD FLAP INBD HINGE ASSY, WING SIDE, CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100. REFER TO WRI: 57504778 FOR WORK DETAILS.

Part: HINGE — CORRODED (LT WING) · corrosion level 2 · airframe 78,836 hrs · 19,594 cycles

LEFT WING OUTBOARD FLAP (WING SIDE) INBOARD FWD HINGE UPPER MOUNT INBOARD HOLE BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-08. EXISTING HOLE DIA: 0.942", FINAL HOLE DIA: 0.950", MAXIMUM ALLOWABLE HOLE DIA: 0.944", REPAIR BUSHING FABRICATED AND INSTALLED IAW EA: 1-5750-T0326464, PART 1, STEP 1A. TITLE: WINGS-FLIGHT SURFACE, EO 1-5750-7-5002, LT WING, OTBD FLAP, INBD HINGE ASSY, WING SIDE, CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 78,836 hrs · 19,594 cycles

MAIN DECK CARGO LT FLOOR SEAT TRACK AT STA 1259, X= 47.5, FOUND CROWN DAMAGED AS MARKED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 78,836 hrs · 19,594 cycles

CENTER CARGO FLOORBEAM UPPER SURFACE FOUND WITH CORROSION AT STA 1701, X=-18 TO X=-24.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 78,836 hrs · 19,594 cycles

MAIN DECK CARGO RT FLOOR SEAT TRACK AT STA 5-53, X=-47.5. FOUND CROWN DAMAGED AS MARKED.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 78,836 hrs · 19,594 cycles

MAIN DECK CARGO LT FLOOR SEAT TRACK AT STA 1801, X= 47.5. FOUND CROWN DAMAGED AS MARKED.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 78,836 hrs · 19,594 cycles

MAIN DECK CARGO LT FLOOR SEAT TRACK AT STA 5-27, X= 47.5. FOUND CROWN DAMAGED AS MARKED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 78,836 hrs · 19,594 cycles

MAIN DECK CARGO RT FLOOR SEAT TRACK AT STA 492, X=-27.5, FOUND CORROSION AS MARKED.

Part: HINGE — CORRODED (LT WING) · airframe 78,836 hrs · 19,594 cycles

LEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, BARREL NUT LOWER HOLE BORE CORRODED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-09. EXISTING HOLE D: 0.420", FINAL HOLE D: 0.423", MAXIMUM ALLOWABLE HOLE D: 0.391". REPAIR BUSHING FABRICATED AND INSTALLED IAW EA NR 1-5750-T0326401, PART 1, STEP 1D. TITLE: WINGS, FLIGHT SURFACE, EO 1-5750-7-5002, LT WING, OTBD FLAP, OTBD HINGE ASSY, WING SIDE, CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100. REFER TO WRI: 57504779 FOR WORK DETAILS.

Part: HINGE — CORRODED (LT WING) · airframe 78,836 hrs · 19,594 cycles

LEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, UPPER MOUNT OTBD HOLE BORE CORRODED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIA: 0.942", FINAL HOLE DIA: 0.946". MAXIMUM ALLOWABLE HOLE DIA: 0.944". REPAIR BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0326401, PART 1, STEP 1A. WINGS, FLIGHT SURFACES EO1-5750-7-5002, LT WING-OTBD FLAP, OTBD HINGE ASSY, WING SIDE CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100. REFER TO WRI: 57504779 FOR WORK DETAILS.

Part: HINGE — CORRODED (LT WING) · airframe 78,836 hrs · 19,594 cycles

LEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, BARREL NUT UPPER HOLE BORE CORRODED. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE: DIA 0.420", FINAL HOLE: DIA 0.423", MAXIMUM ALLOWABLE HOLE: DIA 0.391". REPAIR BUSHING FABRICATED AND INSTALLED IAW EA: 1-5750-T0326401, PART 1, STEP 1D. TITLE: WINGS-FLIGHT SURFACES, EO 1-5750-7-5002, LT WINGS, OTBD FLAP, OTBD HINGE ASSY, WING SIDE, CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100. REFER TO WRI: 57504779 FOR WORK DETAILS.

Part: HINGE — CORRODED (LT WING) · airframe 78,836 hrs · 19,594 cycles

LEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, LOWER MOUNT INBD HOLE SURFACE CORRODED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-09. EXISTING THICKNESS: 0.419", MATERIAL REMOVED: 0.006", FWD FACE; 0.006", AFT FACE, REMAINING THICKNESS: 0.389". MINIMUM ALLOWABLE THICKNESS: 0.408". REPAIR SHIM FABRICATED AND INSTALLED IAW EA: 1-5750-T0326401, PART 1, STEP 1, TITLE: WINGS, FLIGHT SURFACES, EO 1-5750-7-5002-LT WING-OTBD FLAP, OTBD HINGE ASSY, WING SIDE CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR IAW GMM6-2-100. REFER TO WRI: 57504779 FOR WORK DETAILS.

Part: HINGE — CORRODED (LT WING) · airframe 78,836 hrs · 19,594 cycles

LEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, LOWER MOUNT OTBD HOLE SURFACE CORRODED. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING THICKNESS: 0.400", MATERIAL REMOVED: 0.006", FWD FACE; 0.023", AFT FACE, REMAINING THICKNESS: 0.371". MINIMUM ALLOWABLE THICKNESS: 0.408". REPAIR SHIM FABRICATED AND INSTALLED IAW EA: 1-5750-T0326401, PART 1, STEP 1, TITLE: WINGS, FLIGHT SURFACES, EO 1- 5750-7-5002, LT WING, OTBD FLAP, OTBD HINGE ASSY, WING SIDE, CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100. REFER TO WRI: 57504779 FOR WORK DETAILS.

Part: HINGE — CORRODED (LT WING) · airframe 78,836 hrs · 19,594 cycles

LEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE PIVOT HOLE BORE CORRODED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIA: 2.311". FINAL HOLE DIA: 2.316". MAXIMUM ALLOWABLE HOLE DIA: 2.3135". REPAIR BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0326401, PART 1, STEP 1C WINGS, FLIGHT SURFACE, EO 1-5750-7-5002, LT WING-OTBD FLAP, OTBD HINGE ASSY, WING SIDE, CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE — CORRODED (LT WING) · airframe 78,836 hrs · 19,594 cycles

LT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, LOWER MOUNT OTBD HOLE BORE CORRODED. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIA: 0.614", FINAL HOLE DIA: 0.620", MAXIMUM ALLOWABLE HOLE DIA: 0.584". REPAIR BUSHING FABRICATED IAW EA: 1-5750-T0326401, PART 1, STEP 1B AND INSTALLED IAW EA 1-5750-T0326401, PART 1, STEP 1. TITLE: WINGS, FLIGHT SURFACES, EO 1-5750-7-5002, LT WINGS, OTBD FLAP, OTBD HINGE ASSY, WING SIDE, CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100. REFER TO WRI: 57504779 FOR WORK DETAILS.

Part: HINGE — CORRODED (LT WING) · airframe 78,836 hrs · 19,594 cycles

LT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, ACTUATOR INBD HOLE BORE CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09, EXISTING HOLE DIA: 1.249", FINAL HOLE DIA: 1.252" MAXIMUM ALLOWABLE HOLE DIA: 1.220". REPAIR BUSHING FABRICATED AND INSTALLED IAW EA: 1-5750-T0326401, PART 1, STEP 1E. TITLE: WINGS FLIGHT SURFACES-EO 1-5750-5002, LT WING, OTBD FLAP, OTBD HINGE ASSY, WING SIDE, CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100. REFER TO WRI: 57504779 FOR WORK DETAILS.

Part: HINGE — CORRODED (LT WING) · airframe 78,836 hrs · 19,594 cycles

LEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, LOWER MOUNT INBD HOLE BORE CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIA: 0.614", FINAL HOLE DIA: 0.620", MAXIMUM ALLOWABLE HOLE DIA: 0.584". REPAIR BUSHING FABRICATED IAW EA: 1-5750-T0326401, PART 1, STEP 1B AND INSTALLED IAW EA: 1-5750-T0326401, PART 1, STEP 1. TITLE: WINGS FLIGHT SURFACES, EO 1-5750-7-5002 LT WING-OTBD FLAP, OTBD HINGE ASSY, WING SIDE, CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100. REFER TO WRI: 57504779 FOR WORK DETAILS.

Part: HINGE — CORRODED (LT WING) · airframe 78,836 hrs · 19,594 cycles

LEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, UPPER MOUNT INBD HOLE BORE CORRODED. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIA: 0.942", FINAL HOLE DIA: 0.946". MAXIMUM ALLOWABLE HOLE DIA: 0.944". REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED IAW EA 1-5750-T0326401, PART 1, STEP 1A. WINGS, FLIGHT SURFACE, EO 1-5750-5002, LT WING-OTBD FLAP, OTBD HINGE ASSY, WING SIDE, CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100. REFER TO WRI: 57504779 FOR WORK DETAILS.

Part: SCREW — DEFECTIVE (L1 DOOR) · airframe 78,836 hrs · 19,594 cycles

CABIN DOOR WOULD NOT ARM AT PUSHBACK. FOUND DOOR CABLE BRACKET LOOSE. REPLACED HARDWARE FOR BRACKET. L1 DOOR OPS CK GOOD AND ARMS. REF AMM 52-11-02-6, FOUND DOOR CABLE BRACKET LOOSE. REPLACED HARDWARE FOR BRACKET. L1 DOOR OPS CK GOOD & ARMS, REF AMM 52-11-02-6. REPLACED 1 SCREW IN SIDE PANEL THAT HOLDS A BRACKET OUT OF THE WAY OF THE CABLE.

Part: COVER — UNSECURE (L1 DOOR) · airframe 78,733 hrs · 19,569 cycles

LEFT ENTRANCE DOOR, L1 WILL NOT ARM, JAMMED LEVER. RESECURED SLIDE COVER IAW MM 25-61-15-4. OPS CHECK GOOD, ACFT OK FOR SERVICE.

Part: BLOCK — WORN (LE SLAT) · airframe 78,684 hrs · 19,549 cycles

INTERMITTENT SLAT DISAGREE ON APPROACH, WENT AROUND. FOLLOWED QRH, NO SLAT & FLAPS 28 DEGREE LANDING. 194 WAS APPROACH SPEED. R & R FWD ATTACH NR 12 BOLT & ATTACHING HARDWARE IAW AMM. R & R L4B SLAT POSITION SENSOR IAW AMM 27-84-03-4. SENSOR STILL REQUIRES WIRES CUT TO LENGTH & TERMINATED. CLEARANCE CHECK STILL NEEDS TO BE DONE. FINISHED INSTALLATION OF SLAT TRACK RUB BLOCKS IAW MM CH 27-80-32-2 & PERFORMED CLEARANCE CHECK IAW MM CH 27-84-03-4. SLATS CHECKED GOOD NO INTERMITTENT SLAT FAULTS NOTED. SYS OK FOR SERVICE.

Part: GIRT BAR — OUT OF ADJUST (EVAC SLIDE) · airframe 78,301 hrs · 19,423 cycles

LEFT CABIN DOOR SLIDE WILL NOT ARM WHEN CLOSED. READJUSTED GIRT BAR IAW MM 52-10-01-2. PERFORMED TEST IAW RMM 52-10-01-2.

Part: PUMP — LEAKING (HYD SYSTEM) · airframe 78,099 hrs · 19,365 cycles

APPROXIMATELY 50 MINUTES INTO FLIGHT, ANNUNCIATION, HYD 3 OFF. HYD 3 SYS SHOWED 2.0 AT THAT TIME. LEVEL CONTINUED TO DECREASE UNTIL 0.0. RECEIVED ANNUNCIATION, HYD 3 FAIL. USED ALTERNATE GEAR EXTENSION. TROUBLE SHOT ITEM & FOUND LEAK COMING FROM INBD STAB TRIM BRAKE. R & R BRAKE & STAB TRIM MOTOR. ALL OPERATIONAL & LEAK CHECK NORMAL. AMM 27-43-04-4, 27-43-30-4 R & R ENG 3, NR 2 EDP. STILL NEEDS OPERATIONS & LEAK CHECK. AMM 29-11-20-4-1 R & R NR 3 ENG 1 HYD PUMP. NEEDS OPERATIONS & LEAK CHECK. AMM 29-11-20-4-1 COMPLETED NR 3 ENG NR 1 & 2 ENG DRIVEN HYD OPERATIONS & LEAK CHECKED IAW AMM 29-11-20-4-1. ALL OPERATIONAL CHECKED NORMAL & NO LEAKS NOTED.

Part: GIRT BAR — OUT OF ADJUST (L1 DOOR) · airframe 77,871 hrs · 19,295 cycles

L1 DOOR EMER SLIDE GIRT BAR WOULD NOT ENGAGE IN DOOR JAMB. UPON INSPECTION, FOUND GIRT BAR DISENGAGED FROM ITS LOCATOR PIN ON SLIDE PACK. RE-CENTERED GIRT BAR, PERFORMED OPERATIONAL TEST OF L1 DOOR SLIDE IAW AMM 52-10-01-2. TESTED OK ACFT OK FOR SERVICE.

Part: PACKING — DETERIORATED (HYDRAULIC SYS) · airframe 77,707 hrs · 19,255 cycles

HYD 1 OFF, LEVEL 1 ALERT 2, 30 HOURS INTO FLIGHT AT FL 380, HYD SYS 1 INDICATING 2.8 GALS. FOUND HYD LEAK AT SYS 1 PRESS TRANSDUCER. FURTHER TROUBLESHOOTING FOUND PACKING DETERIORATED AT FITTING SIDE, REMOVED SYS 1 PRESS TRANSDUCER. R & R PACKING ON FITTING SIDE & REINSTALLED SYS 1 PRESS TRANSDUCER IAW AMM 29-12-46-2. HYD SYS 1 PRESS INDICATION CHECKED NORMAL & NO LEAK NOTED.

Part: GIRT BAR — OUT OF POSITION (L1 DOOR) · airframe 77,249 hrs · 19,099 cycles

UNABLE TO ARM L1 DOOR. REPOSITIONED L1 GIRT BAR IAW AMM 52-10-01-2. ACFT OK FOR SERVICE.

Part: POWER SUPPLY — FAILED (CABIN) · airframe 75,388 hrs · 18,540 cycles

DURING EMER LIGHT TEST, GOT A LEVEL 1 EMER LIGHT BATTERY 1 LOW ALERT. REPLACED EMER EXIT LIGHT POWER SUPPLY IAW MM 33-51-01-4 & TESTED OK PER AMM 33-51-01-5.

Part: ARMING LEVER — OBSTRUCTED (L1 DOOR) · airframe 74,614 hrs · 18,308 cycles

L1 DOOR SLIDE ARM LEVER IS DIFFICULT TO MOVE TO THE ARM POSITION AMM SMP. FOUND CORN NUT DEBRIS IN GIRT BAR TO DOOR FRAME AREA, REMOVED DEBRIS & GND TESTED NORMAL IAW MM.

Part: SKIN — DAMAGED (TE FLAP) · airframe 74,325 hrs · 18,232 cycles

TO COMPLY WITH WORK CARD T1-5750-T0302286 PART 2 TITLE WINGS, FLIGHT SURFACES, RT INBD FLAP SKIN DAMAGE. INSTALL PERMANENT REPAIR. EA 1-5750-T0302286 PART 2 TITLE: "WINGS-FLIGHT SURFACES - RT INBD FLAP SKIN DAMAGE" HAS BEEN COMPLIED WITH. REPAIR CLASSFIED MAJOR AS PER GMM 6-2-100 REVISION 122.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 74,325 hrs · 18,232 cycles

RIGHT WING INBD FLAP UPPER SURFACE FOUND NUMEROUS DENTS. REPAIRED IAW EA 1-5750-T0309945B PT1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 122.

Part: DOUBLER — CRACKED (RT WING) · airframe 74,325 hrs · 18,232 cycles

RIGHT WING LE LOWER ACCESS COMPARTMENT BEADED DOUBLER FOUND CRACKED XORS 695 DURING OTBD SLAT DRIVE CABLE INSPECTION. REPAIRED IAW SRM 57-40-02 FIGURE 203 REPAIR 15 REVISION 56 REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 122.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,325 hrs · 18,232 cycles

LEFT FUSELAGE NR 1 AIR CONDITIONING COMPARTMENT DOOR CUT OUT UPPER AFT CORNER SKIN FOUND CRACK ABOUT 1 INCH IN LENGTH. DOOR CUTOUT UPPER AFT CORNER SKIN CARRIED OUT REPAIR AS PER SRM 53-20-15 REPAIR 3 FIGURE 201 REV 56. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 122 INITIAL INSPECTION REQUIRED AT 4,000 FLIGHT CYCLES, REPETITIVE INSPECTION AT 4,000 FLIGHT CYCLES , METHOD: VISUAL INSPECTION AS PER SRM 53-20-15 REPAIR 3 TABLE 201 REV 56

Part: SEAL — LEAKING (FUEL SYSTEM) · airframe 73,108 hrs · 17,792 cycles

FUEL STREAMING FROM BOTTOM OF NR 1 ENGINE. LEAK COMING FROM BETWEEN NR 1 ENG FUEL PUMP & HEAT EXCHANGER. R & R SEAL BETWEEN FUEL PUMP & FUEL OIL HEAT EXCHANGER. WET MOTOR, NO LEAKS NOTED. RAN NR 1 ENGINE NO LEAKS NOTED IAW MM 73-12-01-4-1 & JRH. DURING LANDING.

Part: LIGHT — INOPERATIVE (R1 DOOR) · airframe 73,065 hrs · 17,775 cycles

R1 DOOR PRESS TO TEST LAMP INOPERATIVE. R & R BULBS IAW AMM CHAPTER 25-61-04-4. OPERATIONS CHECKED GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 72,092 hrs · 17,445 cycles

EMERGENCY POWER OFF LIGHT DOES NOT WORK. REPLACED POWER SUPPLY IAW MM24-08-02-4, PERFORMED OPS TEST OF THE ELEC SYS CONTROL PANEL IAW MM 24-08-02-700-806. ALL CHECKS GOOD AT THIS TIME.

Part: FITTING — CORRODED (RT WING) · corrosion level 2 · airframe 70,213 hrs · 16,853 cycles

RT WING (WING SIDE) OTBD FLAP VANE FITTING 'E' MOUNTING SURFACE FOUND CORROSION. REPAIRED IAW EA 1-5750-162385. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.

Part: SKIN — CORRODED (BS 2163) · corrosion level 2 · airframe 70,213 hrs · 16,853 cycles

RT FUSELAGE SKIN AT BS 2163 BETWEEN LONGERON 33 AND 35 RT, FOUND CORRODED. CORROSION REMOVED AS PER SRM 51-21-01 REVISION 50 FOUND EXCEEDED OF LIMITS AS PER SRM 53-70-01 FIGURE 201 REPAIR 3 REVISION 50. REPAIR CARRIED OUT PER EA 1-5330-163513. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.

Part: HINGE BRACKET — DAMAGED (RT WING TE FLAP) · airframe 70,213 hrs · 16,853 cycles

RIGHT WING OTBD FLAP INBD HINGE LOWER MOUNT OTBD HOLE REPAIR BUSHING FOUND DAMAGED. REPAIRED IAW EA 1-5750-127716, REVISION B, PART 2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.

Part: HINGE FITTING — CORRODED (RT WING) · corrosion level 2 · airframe 70,213 hrs · 16,853 cycles

RIGHT WING TE FLAP, WING SIDE OTBD HINGE FITTING MATING SURFACE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5750-162384 PART 1, STEP 1, 2, 3, 4 AND 7. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.

Part: HINGE FITTING — CORRODED (ZONE 600) · corrosion level 2 · airframe 70,213 hrs · 16,853 cycles

RT WING SIDE OTBD FLAP, OTBD HINGE FITTING FOUND CORRODED. REPAIR ACCOMPLISHED PER EA 1-5750-162384 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.

Part: ATTACH BRACKET — WORN (ZONE 600) · airframe 70,213 hrs · 16,853 cycles

RIGHT WING SIDE FLAP, OTBD HINGE ACTUATOR ATTACHED FITTING WORN. REPAIR ACCOMPLISHED AS PER EA 1-5750-127715 REVISION B PART 2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.

Part: FLOORBEAM — CRACKED (BS 410) · airframe 70,213 hrs · 16,853 cycles

MAIN DECK CABIN FLOORBEAM BS 410, X = 27 TO X = 30 FOUND CRACKED. REMOVED AND REPLACED IAW SRM 51-31-01 REVISION 50. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.

Part: HINGE BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 70,213 hrs · 16,853 cycles

RIGHT WING SIDE OTBD FLAP, OTBD HINGE FITTING FOUND CORRODED. REPAIR ACCOMPLISHED PER EA 1-5750-162384 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.

Part: BUSHING — WORN (ZONE 600) · airframe 70,213 hrs · 16,853 cycles

RIGHT WING SIDE OTBD FLAP HINGE ACTUATOR ATTACHED FITTING BUSHING WORN. REPAIR ACCOMPLISHED AS PER EA 1-5750-127715 REVISION B PART 2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.

Part: HINGE BRACKET — DAMAGED (RT WING TE FLAP) · airframe 70,213 hrs · 16,853 cycles

RIGHT WING OTBD FLAP INBD HINGE LOWER MOUNT INBD HOLE REPAIR BUSHING FOUND DAMAGED. REPAIR ACCOMPLISHED AS PER EA 1-5750-127716, REVISION B, PART 2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.

Part: SKIN — CRACKED (LT WING) · airframe 70,213 hrs · 16,853 cycles

LEFT WING OTBD L/E NR14 SLAT TRACK CUTOUT OTBD CORNER FOUND CRACKED. REPAIRED IAW SRM 57-40-02 FIGURE 201, REPAIR 7, REVISION 50. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.

Part: SKIN — CRACKED (ZONE 500) · airframe 70,213 hrs · 16,853 cycles

LEFT WING OTBD L/E NR 12 SLAT TRACK CUTOUT OTBD CORNER FOUND CRACKED. REPAIRED IAW SRM 57-40-02 FIGURE 201, REPAIR 7 REVISION 50. REPAIR CALSSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.

Part: DOUBLER — CRACKED (ZONE 500) · airframe 70,213 hrs · 16,853 cycles

LEFT WING - L/E CAVITY BEADED DOUBLER AT APPROX STA XOS 585 FOUND CRACKED. REPAIRED IAW SRM 57-40-02, FIGURE 203, REPAIR 15 REVISION 50. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.

Part: ATTACH FITTING — CRACKED (ZONE 500) · airframe 70,213 hrs · 16,853 cycles

LEFT WING T/E LOWER ATTACH FITTING AT APPROX XORS 433 FOUND CRACKED. REPLACED IAW SRM 51-31-01 REVISION 50. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.

Part: SKIN — CRACKED (ZONE 600) · airframe 70,213 hrs · 16,853 cycles

RT WING REFUEL PANEL CUTOUT FORWARD INBD CORNER FOUND CRACKED. REPAIRED IAW SRM 57-40-02, FIGURE 202, REPAIR 7, REVISION 50. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.

Part: CARGO TRACK — CORRODED (BS 1491) · corrosion level 2 · airframe 70,213 hrs · 16,853 cycles

MAIN DECK CARGO TRACK AT BS 1491, X = 107.25 FOUND CORRODED. REPAIRED AS PER SRM 53-00-52 FIGURE 201 REPAIR 5 REVISION 50. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.

Part: CARGO TRACK — CORRODED (BS 1514) · corrosion level 2 · airframe 70,213 hrs · 16,853 cycles

MAIN DECK CARGO TRACK AT BS 1514, X = 805 FOUND CORRODED. REPAIRED AS PER SRM 53-00-52 FIGURE 201 REPAIR 5 REVISION 50. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.

Part: DOUBLER — CRACKED (ZONE 500) · airframe 70,213 hrs · 16,853 cycles

LEFT WING L/E CAVITY BEADED DOUBLER AT APPROX XOS 610 FOUND CRACKED. REPAIRED IAW SRM 57-40-02, FIGURE 203, REPAIR 15, REVISION 50. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.

Part: HINGE BRACKET — CORRODED (ZONE 600) · corrosion level 2 · airframe 70,213 hrs · 16,853 cycles

RIGHT WING OTBD FLAP INBD HINGE SIDE LOAD FITTING LOWER FASTENER HOLE FOUND CORRODED. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08 REVISION 74. EXISTING HOLE DIAMETER = 0.641 INCH, FINAL HOLE DIAMETER = 0.6455 INCH. MAXIMUM HOLE DIAMETER = 0.621 INCH. REPAIR ACCOMPLISHED AS PER EA 1-5750-162383 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.

Part: STRAP — CRACKED (ZONE 600) · airframe 70,213 hrs · 16,853 cycles

RIGHT WING T/E LOWER AT APPROX XORS 433 LOWER STRAP FOUND CRACKED. REMOVED AND REPLACED IAW SRM 51-31-01 REVISION 50. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.

Part: SKIN — CRACKED (ZONE 500) · airframe 70,213 hrs · 16,853 cycles

LEFT WING REFUEL PANEL CUTOUT FORWARD INBD CORNER FOUND CRACKED. REPAIRED IAW SRM 57-40-02 FIGURE 202 REPAIR 7 REVISION 50. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.

Part: DOUBLER — CRACKED (ZONE 500) · airframe 70,213 hrs · 16,853 cycles

LEFT WING L/E CAVITY BEADED DOUBLER AT APPROX XOS 680 FOUND CRACKED. REPAIRED IAW SRM 57-40-02, FIGURE 203, REPAIR 15 REVISION 50. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.

Part: SEAT TRACK — WORN (BS 635) · airframe 70,213 hrs · 16,853 cycles

MAIN DECK CARGO SEAT TRACK AT BS 635, X = -47.5 FOUND WORN. REPAIRED SEAT TRACK IAW SRM 53-00-52, FIG 201, REPAIR 1 REV 50. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 115.

Part: FLOOR SUPPORT — CRACKED (BS 383-401) · airframe 70,213 hrs · 16,853 cycles

FORWARD AVIONICS COMPARTMENT, FLOOR SUPPORT FROM BS 383 TO 401, FOUND A 4 INCH CRACK AT 2 PLACES. REMOVED AND REPLACED AS PER SRM 51-31-01 REVISION 50. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.

Part: SEAT TRACK — CORRODED (BS 640) · corrosion level 2 · airframe 70,213 hrs · 16,853 cycles

MAIN DECK CARGO SEAT TRACK AT BS 640, X = 8.5 FOUND WITH CORRODED. REPAIRED SEAT TRACK FROM IAW SRM 53-00-52, FIG 201, REPAIR 1, REV 50. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 115.

Part: SEAT TRACK — WORN (BS 635) · airframe 70,213 hrs · 16,853 cycles

MAIN DECK CARGO SEAT TRACK AT BS 635, X = -8.5 FOUND WORN. SEAT TRACK REPAIRED IAW SRM 53-00-52, FIG 201, REPAIR 1 REV 50. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 115.

Part: CARGO TRACK — WORN (BS 775) · airframe 70,213 hrs · 16,853 cycles

MAIN DECK CARGO TRACK AT BS 775, X = -47.5, FOUND WORN. REPAIRED CARGO TRACK IAW SRM 53-00-52, FIG 201, REPAIR 1 REV 50. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 115.

Part: SEAT TRACK — WORN (MAIN DECK CARGO) · airframe 70,213 hrs · 16,853 cycles

MAIN DECK CARGO SEAT TRACK AT BS 690, X = 27.5 FOUND WORN. REPAIRED SEAT TRACK IAW SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 50. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.

Part: SEAT TRACK — WORN (BS 760) · airframe 70,213 hrs · 16,853 cycles

MAIN DECK CARGO SEAT TRACK AT BS 760, X = -8.5 FOUND WORN. REPAIRED SEAT TRACK IAW SRM 53-00-52 FIGURE 201, REPAIR 1, REVISION 50. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.

Part: SEAT TRACK — CORRODED (BS 1401) · corrosion level 2 · airframe 70,213 hrs · 16,853 cycles

MAIN DECK CARGO SEAT TRACK AT BS 1401, X= 27.5 FOUND CORRODED. REPAIRED SEAT TRACK IAW SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 50. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.

Part: SKIN — GOUGED (NR 3 PYLON) · airframe 70,213 hrs · 16,853 cycles

NR 3 PYLON, STATION YWN= 264 HYD CASE DRAIN PAN ADJACENT AREA LT SIDE. EXTERIOR SURFACE FOUND GOUGED. REPAIRED IAW EA 1-5450-163511. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 115.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 70,213 hrs · 16,853 cycles

MAIN DECK CARGO SEAT TRACK AT BS 1881, X= 8.5 FOUND CORRODED. REPAIRED SEAT TRACK IAW SRM 53-00-52, FIG 201 REPAIR 1, REV 50. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 115.

Part: LINE — LEAKING (FUEL SYSTEM) · airframe 68,536 hrs · 16,399 cycles

RAMP PERSONNEL UNLOADING THE AFT CARGO BAY, REPORTED STRONG FUEL ODOR. ODOR VERY STRONG COMING FROM THE LEFT WALL VENT. LT AFT AND CENTER CARGO DOORS OPENED FOR VENTILATION. FOUND FUEL LEAKING FROM COUPLING, LT SIDE WALL OF CENTER CARGO COMPARTMENT. LEAKING COUPLER LOCATED ON TAIL TRANSFER FUEL LINE. REMOVED COUPLING AND AJOINING PARTS, R & R O-RINGS ON TAIL TRANSFER LINE COUPLING IAW MM 28-00-00-4. LEAK CHECKED GOOD. RETURNED TO SERVICE.

Part: WIRE — CHAFED (MLG HANDLE) · airframe 66,981 hrs · 15,993 cycles

WHEN GEAR HANDLE WAS RAISED AFTER T/O, 1 SPARK CAME OUT OF GEAR HANDLE MECHANISM. INSTALLED GEAR PINS AND RAISED GEAR HANDLE AND DESCREPANCY REPEATED WITH C/B B1-415 POPPING. REMOVED DISPLAY UNITS 3 AND 4 AS WELL AS GEAR INDICATOR. FOUND WIRE B007-12-22 BROKEN AND SHOWING SIGNS OF ARCING. ALSO FOUND WIRE B007-9-20 DAMAGED. R & R WIRE B007-12-22 AND SPLICED WIRE B007-9-20, APPROX 6 INCHES FROM BACK OF INDICATOR. LIGHTS NOW OPERATE NORMALLY. LANDING GEAR IND. SYS STILL REQUIRES FULL OPS CHECK. RE-INSTALLED NR 3 AND 4 DU'S. REF: AMM 31-61-03-2. OPS CHECK NORMAL. RE-INSTALLED GEAR INDICATOR REF: AMM 32-61-11-4. ACCOMPLISHED LANDING GEAR POSITION INDICATION TEST IAW MM 32-61-00-5. SYS OPS CHECKS OK. ACFT OK FOR SERVICE.

Part: BATTERY — DISCHARGED (L1 DOOR SLIDE) · airframe 66,586 hrs · 15,904 cycles

L1 DOOR SLIDE REMOTE PRESSURE INDICATOR BATTERIES DEAD. R & R BATTERIES. OPS CHECK GOOD. REF AMM 25-23-07-4-1 AND 25-61-15-4-0. FINAL CLOSED.

Part: WHEEL — FAILED (MLG) · airframe 65,630 hrs · 15,676 cycles

SHORTLY AFTER EXTENDING THE GEAR FOR LANDING, WE RECEIVED A BRAKE DIFF PRESS ALERT. NR 8 TIRE PRESSURE WAS AT 117PSI AND DROPPING RAPIDLY. WITHIN A MINUTE THE PRESSURE WAS AT ZERO AND WE RECEIVED A TIRE FAIL ALERT. THE CAPTAIN TOOK CONTROLL OF THE ACFT AND LANDED THE ACFT ON 18L. THE ACFT WAS STOPPED USING MANUAL BRAKES. THE ACFT WAS TAXIED CLEARED OFF THE RUNWAY WERE WE CONTACTED MX FOR A TOW-IN TO OUR GATE. R & R NR 7 AND NR 8 MW IAW MM 32 41 01 2 VISUALLY INSPECTED BRAKE ASSYS, ATTACHEMENT AND SECURITY IS OK FOR SERVICE. PREMATURE REMOVAL/INSTALLATION OFF MFG ARG7755-503, POS 7, SRL B3017, TAG C74270 ON MFG ARG7755-503, SRL B4179 TAG 8C8851. PREMATURE REMOVAL/INSTALLATION OFF MFG ARG7755-503 POS 8, SRL B4124, TAG 0645C7 ON MFG ARG7755-503, SRL B4021, TAG 74C911. FINAL CLOSED.

Part: LIGHT — DAMAGED (CABIN) · airframe 64,886 hrs · 15,495 cycles

EMERGENCY LIGHT DAMAGED AT DOOR L1 DROP CEILING. R & R LT DOOR HANDLE EMERGENCY LIGHT ASSY AND OPS CHECK CARRIED OUT IAW MM 33-52-02-2, REV 66.0. SATIFACTORY. R/I FROM FACT PREMATURE REMOVAL/INSTALLATION.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 64,885 hrs · 15,494 cycles

MAIN DECK CARGO - UPON REMOVAL OF FLOOR PANELS FOR CORRODED FERRULES. REPLACEMENT FOUND SEAT TRACK X=75 FROM STA 1861 TO 1871 INBD AND OTBD FLANGES CORRODED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1751 TO STATION 1887 X= 75 AS PER SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 45. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100 REVISION 111.

Part: SKIN — DAMAGED (ZONE 200) · airframe 64,885 hrs · 15,494 cycles

MAIN DECK CARGO DOOR LOWER MID CUT OUT AT STA 695 TO STA 700, LONGERON 27 LT FOUND CHIPPED. MAIN DECK CARGO DOOR LOWER MID CUT OUT AT STATION 695 TO STATION 700 LONGERON 27LT, CHIPPED AREA REPAIRED AS PER E.A. 1-5310-143493. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REVISION 111.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 64,885 hrs · 15,494 cycles

MAIN DECK CARGO - UPON REMOVAL OF FLOOR PANEL FOR SLANT PANEL INSPECTION ACCESS FOUND SEAT TRACK STATION 1531 TO STATION 5-33, X= -8 INBOARD FLANGE WITH MULTIPLE SURFACE CORROSION. MAIN DECK CARGO - CORRODED SEAT TRACK AT STATION 1531 TO STATION 5-33 X= -8, REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1531 TO STATION 5-63 X= -8 AS PER SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 45. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 111.

Part: ACCESS PANEL — CRACKED (ZONE 500) · airframe 64,885 hrs · 15,494 cycles

HFEC OPEN HOLE INSP CARRIED OUT ON LT WING ON PSE LOWER SKIN PANEL OUTER WING ACCESS DOOR CUTOUT AT BETWEEN STA XORS= 683.4 AND XORS= 713.6. FOUND 05 EA HOLES WITH CRACK INDICATION. REPAIR CARRIED OUT IAW DWG SG11570004, REV A. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 111.

Part: SKIN — CRACKED (ZONE 600) · airframe 64,885 hrs · 15,494 cycles

HFEC OPEN HOLE INSPECTION CARRIED OUT ON RT WING ON PSE LOWER SKIN PANEL OUTER WING ACCESS DOOR CUTOUT AT BETWEEN STA XORS= 683.4 AND XORS= 713.6. FOUND 15 EA HOLES WITH CRACK INDICATIONS. REPAIR CARRIED OUT IAW DWG SG11570004, REV A. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 111.

Part: WIRE — SHORTED · airframe 60,582 hrs · 14,469 cycles

DURING SERVICE CHK FOUND RAM AIR DOOR CTL FOR PACK NR 3 CB POPPED. ON INVESTIGATION FOUND OVHD CB PANEL WIRE BUNDLE TOUCHING A SCREW ON THE PANEL CAUSING A WIRE TO CHAFE AND SHORT TO GND. PERFORMED INSP ON ASSOCIATED WIRE BUNDLE, FOUND WIRE NR 8201-317-22 CHAFED. NO OTHER WIRES IN BUNDLE WERE DAMAGED. SPLICE REPAIR C/O IAW MD11 AMM 20-30-01-2. OPS CHK FOR RAM AIR DOOR PACK NR3 C/O IAW AMM 21-62-01-5. SYS CHECKS OK. INSTALLED PROTECTIVE SLEEVE AND REPOSITIONED WIRE BUNDLE IAW SWPM 20-00-06 PG205, PARA 13. ACFT OK FOR SERVICE.

Part: FITTING — DAMAGED (ZONE 300) · corrosion level 2 · airframe 59,647 hrs · 14,232 cycles

EXISTING FASTENER HOLE REPAIR AT VERTICAL STABILIZER AT RIGHT AND LEFT NR 4 BANJO FITTING AND PYLON CARRY THRU CAP. EXISTING FASTENER HOLE REPAIR AT VERTICAL STABILIZER AT RIGHT AND LEFT NR 4 BANJO FITTING AND PYLON CARRY THRU CAP EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED AS PER EA NR 1-5530-47423, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FITTING — CRACKED (ZONE 100) · airframe 59,647 hrs · 14,232 cycles

AFT CARGO, WASTE COMPARTMENT STA 1994 LONGERON 47L SHOVEL FITTING CRACKED. REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FITTING — CRACKED (ZONE 100) · airframe 59,647 hrs · 14,232 cycles

AFT CARGO WASTE COMPARTMENT STA 1994 LONGERON 45L SHOVEL FITTING CRACKED. REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: TANK — CORRODED (CENTER) · airframe 59,647 hrs · 14,232 cycles

MAIN DECK, CENTER TANK UPPER SURFACE AT STA 1223, X = -78 FOUND CORROSION. REPAIR CARRIED OUT AS PER E.A. 1-5710-127722. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SKIN — CORRODED (CENTER TANK) · airframe 59,647 hrs · 14,232 cycles

MAIN DECK, CENTER TANK UPPER SURFACE AT STA 1223, X = -75 FOUND CORROSION. COMPLIED WITH E.A. 1-5710-127723, REPAIR. CLASSIFIED AS MINOR REPAIR AS PER FEDEX GMM 6-2-100.

Part: BRACKET — CORRODED (ZONE 500) · airframe 59,647 hrs · 14,232 cycles

LEFT WING INBOARD FLAP OUTBOARD AFT HINGE OUTBOARD PIVOT BORE FOUND WITH CORROSION. OUTBOARD PIVOT BORE HOLE AT LEFT HAND WING INBOARD FLAP OUTBOARD AFT HINGE REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-52-03. NEW BUSHING FABRICATED AND INSTALLED AT LT WING INBOARD FLAP OUTBOARD AFT HINGE OUTBOARD PIVOT BORE AS PER E.A. 1-5750-127720, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: BRACKET — CORRODED (TE FLAPS) · airframe 59,647 hrs · 14,232 cycles

RIGHT WING INBOARD FLAP OUTBOARD AFT HINGE OUTBOARD PIVOT BORE FOUND WITH CORROSION. REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-52-03. NEW BUSHING FABRICATED AND INSTALLED AS PER E.A. 1-5750-127721. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 59,647 hrs · 14,232 cycles

MAIN DECK, FLOOR PANEL SEAT TRACK AT STA 1541, X = 8.5 FOUND WITH CORROSION. REPAIR CARRIED OUT AS PER SRM 53-70-00 FIG 1 VOL I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: BRACKET — CORRODED (TE FLAP) · airframe 59,647 hrs · 14,232 cycles

LEFT WING INBOARD FLAP OUTBOARD AFT HINGE INBOARD PIVOT BORE FOUND WITH CORROSION. INBOARD PIVOT BORE AT LT WING INBOARD FLAP OUTBOARD AFT HINGE REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-52-03. NEW BUSHING FABRICATED AND INSTALLED AS PER E.A. 1-5750-127720, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 59,647 hrs · 14,232 cycles

FUSELAGE EXTERIOR SKIN AT STA 6-90 LONGERON 33R TO 34R FOUND WITH EXISTING DOUBLER REPAIR. EXISTING DOUBLER REPAIR AT FUSELAGE EXTERIOR SKIN AT STA 6-90 LONGERON 33R TO 34R EVALUATED AND FOUND NOT IN ACCORDANCE WITH SRM 53-20-00 FIGURE 2 VOLUME I. REPAIR CARRIED OUT AS PER FEDEX EA NR 1-5310-127727, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: BRACKET — CORRODED (TE FLAP) · airframe 59,647 hrs · 14,232 cycles

RIGHT WING INBOARD FLAP OUTBOARD AFT HINGE INBOARD PIVOT BORE FOUND WITH CORROSION. REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-52-03. NEW BUSHING FABRICATED AND INSTALLED AT RT WING INBOARD FLAP OUTBOARD AFT HINGE INBOARD PIVOT BORE AS PER E.A. 1-5750-127721. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 59,647 hrs · 14,232 cycles

FUSELAGE EXTERIOR SKIN AT STA 6-90 LONGERON 33L TO 34L FOUND WITH EXISTING DOUBLER REPAIR. EXISTING DOUBLER REPAIR AT FUSELAGE EXTERIOR SKIN AT STA 6-90 LONGERON 33L TO 34L EVALUATED AND FOUND NOT IN ACCORDANCE WITH SRM 53-20-00 FIGURE 2 VOLUME I. REPAIR CARRIED OUT AS PER EA NR 1-5310-127727, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STANCHION — CORRODED (THRUST REVERSER) · airframe 59,647 hrs · 14,232 cycles

FORWARD CARGO, DURING POST OPEN UP FOR THRUST REVERSER MODIFICATION, STA 6-70, X = 50, AFT BULKHEAD STANCHION FOUND CORRODED. REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. STANCHION FABRICATED PER DRAWING A6A7094. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: LONGERON — CRACKED (ZONE 100) · airframe 59,647 hrs · 14,232 cycles

AFT CARGO, WASTE COMPARTMENT STA 2007, LONGERON 47L, LONGERON SPLICE FITTING CRACKED. REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 59,647 hrs · 14,232 cycles

MAIN DECK, FLOOR PANEL SEAT TRACK FROM STA 5-20 TO STA 5-60, X = 8.5 FOUND CORROSIONS AT SEVERAL LOCATIONS, MAIN DECK, CORRODED SEAT TRACK FROM STA 5-20 TO STA 5-60, X = 8.5 REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 5-0 TO STA 5-123, X = 8.5 AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — MISREPAIRED (LT WING TE FLAP) · airframe 59,647 hrs · 14,232 cycles

LEFT WING INBOARD TRAILING EDGE FLAP LOWER INBOARD SEGMENT UPPER SURFACE FOUND WITH AN EXISTING REPAIR, LOCATION: 12 INCH FROM TRAILING EDGE AND 88 INCH FROM INBOARD OF FLAP. EXISTING REPAIR AT LEFT WING INBOARD TRAILING EDGE FLAP LOWER INBOARD SEGMENT UPPER SURFACE LOCATION: 12 INCH FROM TRAILING EDGE AND 88 INCH FROM INBOARD OF FLAP EVALUATED AND FOUND NOT CARRIED OUT IN ACCORDANCE WITH SRM 57-10-00 FIGURE 38 VOLUME I. EXISTING REPAIR REMOVED AT LEFT WING INBOARD TRAILING EDGE FLAP LOWER INBOARD SEGMENT UPPER SURFACE AND REPAIR CARRIED OUT AS PER SRM 57-10-00 FIGURE 38 VOLUME I FEDEX E.O. 1-5100-7-5001 PART 1, TITLE: STRUCTURES - REPAIR CATALOG - MD11 REPAIR IDENTIFICATION AND TRACKING REQUIREMENTS 14 CFR 121.707 HAS BEEN ACCOMPLISHED. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SKIN — MISREPAIRED (ZONE 500) · airframe 59,647 hrs · 14,232 cycles

LEFT WING INBOARD TRAILING EDGE FLAP UPPER SURFACE FOUND WITH AN EXISTING REPAIR, LOCATION: 68 INCH FROM TRAILING EDGE AND 70 INCH FROM INBOARD EDGE OF FLAP. LEFT WING INBOARD TRAILING EDGE FLAP UPPER SURFACE EXISTING REPAIR EVALUATED AND FOUND NOT ACCOMPLISHED IAW SRM 57-10-00 FIG 38 VOL I. EXISTING REPAIR REMOVED AND NEW REPAIR CARRIED OUT AS PER SRM 57-10-00 FIG 38 VOL I EO 1-5100-7-5001 PT.1, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: MOUNT — CORRODED (ZONE 600) · airframe 59,647 hrs · 14,232 cycles

RIGHT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE ACTUATOR MOUNT OUTBOARD BORE FOUND WITH CORROSION. COMPLIED WITH E.A. 1-5750-127715. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SKIN — MISREPAIRED (LT WING TE FLAP) · airframe 59,647 hrs · 14,232 cycles

LEFT WING INBOARD TRAILING EDGE FLAP INBOARD LOWER SEGMENT UPPER SURFACE FOUND AN EXISTING REPAIR AT OUTBOARD EDGE AREA. EXISTING REPAIR AT LEFT WING INBOARD TRAILING EDGE FLAP INBOARD LOWER SEGMENT UPPER SURFACE OUTBOARD EDGE AREA EVALUATED AND FOUND NOT CARRIED OUT IN ACCORDANCE WITH SRM 57-10-00 FIGURE 39 VOLUME I. EXISTING REPAIR AT LEFT WING INBOARD TRAILING EDGE FLAP INBOARD LOWER SEGMENT UPPER SURFACE OUTBOARD EDGE AREA. REMOVED AS PER SRM 51-31-01 VOLUME II AND NEW REPAIR CARRIED OUT AS PER SRM 57-10-00 FIGURE 39 VOLUME I EO 1-5100-7-5001 PART 1, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: MOUNT — CORRODED (ZONE 600) · airframe 59,647 hrs · 14,232 cycles

RIGHT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE ACTUATOR MOUNT INBOARD BORE FOUND WITH CORROSION. COMPLIED WITH E.A. 1-5750-127715. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: LONGERON — CRACKED (ZONE 100) · airframe 59,647 hrs · 14,232 cycles

CRACK INDICATION FOUND APPROXIMATELY 2.5 INCH DURING X-RAY INSPECTION AT STA 5-0, LONGERON 2R AFT SECTION EDGE. CRACKED LONGERON 2R AT STA 5-0 REPAIRED AS PER SRM 53-10-00 FIGURE 2 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CHAFED (ZONE 600) · airframe 59,647 hrs · 14,232 cycles

RIGHT WING DROOP LEADING EDGE INBOARD EDGE SKIN WITH CHAFE MARK. REPAIRED AS PER E.A. 1-5750-127877. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SUPPORT FITTING — DAMAGED (DOOR FRAME) · airframe 59,647 hrs · 14,232 cycles

CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSP ON 0.460 INCH HOLES AT MAIN CARGO DOOR LWR JAMB NR 5 SUPPORT FITTING AT HOLES A, B, C AND D. REPAIR CARRIED OUT AS PER SRM 53-50-00 FIG. 10 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: MOUNT — CORRODED (ZONE 500) · airframe 59,647 hrs · 14,232 cycles

LEFT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE AFT LOWER MOUNT NUT SIDE FACE FOUND CORROSION. REPAIRED AS PER E.A. 1-5750-127870, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: MOUNT — CORRODED (ZONE 600) · airframe 59,647 hrs · 14,232 cycles

RIGHT WING OUTBOARD FLAP INBOARD FORWARD HINGE AFT LOWER MOUNT OUTBOARD BORE FOUND WITH CORROSION. COMPLIED WITH E.A. 1-5750-127716. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SUPPORT FITTING — DAMAGED (CARGO DOORWAY) · airframe 59,647 hrs · 14,232 cycles

CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSP ON 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 3 SUPPORT FITTING AT HOLES A, B, C AND D. REMOVED & REPLACED AS PER SRM 51-31-01 VOL.II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: BRACKET — CORRODED (LT WING TE FLAP) · airframe 59,647 hrs · 14,232 cycles

LEFT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE AFT LOWER MOUNT OUTBOARD BORE FOUND WITH CORROSION. REPAIRED AS PER E.A. 1-5750-127870, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: MOUNT — CORRODED (ZONE 500) · airframe 59,647 hrs · 14,232 cycles

LEFT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE INBOARD ACTUATOR MOUNT BORE FOUND WITH CORROSION. COMPLIED WITH E.A 1-5750-127714. CLASSIFIED AS MAJOR REPAIR AS PER GMM 6-2-100.

Part: MOUNT — CORRODED (ZONE 600) · airframe 59,647 hrs · 14,232 cycles

RIGHT WING OUTBOARD FLAP INBOARD FORWARD HINGE AFT LOWER MOUNT INBOARD BORE FOUND WITH CORROSION. COMPLIED WITH E.A. 1-5750-127716. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.

Part: DOOR FRAME — CRACKED (MAIN CARGO DOOR) · airframe 59,647 hrs · 14,232 cycles

CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSP ON 0.460 INCH HOLES AT MAIN CARGO DOOR LWR JAMB NR 7 SUPPORT FITTING AT HOLES A, B , C AND D. REMOVED & REPLACED AS PER SRM 51-31-01 VOL.II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SUPPORT FITTING — CRACKED (DOOR FRAME) · airframe 59,647 hrs · 14,232 cycles

CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 1 SUPPORT FITTING AT HOLES A, B, C AND D. SUPPORT FITTING REMOVED & REPLACED AS PER SRM 51-31-01 VOL.II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SUPPORT FITTING — DAMAGED (DOOR FRAME) · airframe 59,647 hrs · 14,232 cycles

CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSP ON 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 4 SUPPORT FITTING AT HOLES A, B, C AND D. REPAIR CARRIED OUT AS PER SRM 53 -50-00 FIG. 10 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: BRACKET — CORRODED (LT WING TE FLAP) · airframe 59,647 hrs · 14,232 cycles

LEFT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE AFT LOWER MOUNT INBOARD BORE FOUND WITH CORROSION. REPAIRED AS PER E.A. 1-5750-127870, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOOR FRAME — CRACKED (MAIN CARGO DOOR) · airframe 59,647 hrs · 14,232 cycles

CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSP ON 0.460 INCH HOLES AT MAIN CARGO DOOR LWR JAMB NR 6 SUPPORT FITTING AT HOLES A, B, C AND D. REMOVED & REPLACED AS PER SRM 51-31-01 VOL.II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 59,647 hrs · 14,232 cycles

CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 2 SUPPORT FITTING AT HOLES A, B, C AND D. SUPPORT FITTING REMOVED & REPLACED AS PER SRM 51-31-01 VOL II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SKIN — CRACKED (ZONE 600) · airframe 54,481 hrs · 13,078 cycles

WITH REFERENCE TO EA NR 1-5710-90773 DURING ACCOMPLISHMENT OF ALI 57.23.01.2. TWO MOUNTING BORES THE TANKS ACCESS PLATE AT STA XORS = 713.6 GAVE A CRACK INDICATION. THE BORES WERE INCREASED TO 0.310" WHERE CRACK INDICATION CEASED. COMPLIED WITH FEDEX EA NR 1-5710-112360, TITLE: AD 2007-07-04 - WINGS - RIGHT LOWER SKIN PLANK CUT OUT ATT 636AB - FOUR ACCESS DOOR ATTACHMENT BORES WITH CRACK INDICATIONS PSE 57.23.01 ALI - REPAIR. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: LONGERON — DAMAGED (ZONE 100) · airframe 54,481 hrs · 13,078 cycles

LONGERON 37R AT STA 1841 FOUND WITH FASTENER HOLE AS 1/4" SIZE. REPAIR CARRIED OUT PER FEDEX EA 1-5310-114762. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: LONGERON — CRACKED (ZONE 100) · airframe 54,481 hrs · 13,078 cycles

LONGERON 38R AT STA 1863 FOUND CRACKED. CARRIED OUT REPAIR AS PER SRM 53-10-00 FIGURE 2 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: LONGERON — DAMAGED (ZONE 100) · airframe 54,481 hrs · 13,078 cycles

LONGERON 39R AT STA 1857 FOUND WITH FASTENER HOLE ELONGATED. REPAIR CARRIED OUT AS PER FEDEX EA 1-5310-114762, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — DENTED (ZONE 100) · airframe 54,481 hrs · 13,078 cycles

FUSELAGE RT SIDE AT STA 1841-1855 BETWEEN X = 35 AND X = 36 FOUND DENTED. REPAIR CARRIED OUT AS PER FEDEX EA 1-5310-114762. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: LONGERON — DAMAGED (ZONE 100) · airframe 54,481 hrs · 13,078 cycles

LONGERON 38R AT STA 1865 FOUND WITH SHORT PITCHES. REPAIR CARRIED OUT AS PER FEDEX EA 1-5310-114762. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: LONGERON — DAMAGED (ZONE 100) · airframe 54,481 hrs · 13,078 cycles

LONGERON 38R AT STA 1864 FOUND WITH HOLE DIAMETER AS 1/4" SIZE. REPAIR CARRIED OUT AS PER FEDEX EA 1-5310-114762. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 54,481 hrs · 13,078 cycles

MAIN DECK CARGO ALONG CENTER STA 1521 TO 5-93 SEAT TRACK AROUND FASTENER HOLE AREA FOUND WITH CORROSION. [08-02-07] CARRIED OUT REPAIR AS PER SRM 53-70-00 FIGURE 6 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 54,481 hrs · 13,078 cycles

MAIN DECK CARGO ALONG CENTER STA 1501 TO 1521 SEAT TRACK AROUND FASTENER HOLE AREA FOUND WITH CORROSION. [07-30-07] CARRIED OUT REPAIR AS PER SRM 53-70-00 FIGURE 6 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CRACKED (ZONE 500) · airframe 54,481 hrs · 13,078 cycles

CRACK INDICATIONS REVEALED IN 04 EACH FASTENER HOLES TOWARDS EDGE OF ACCESS CUTOUT IN LEFT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN XORS = 683.4 AND XORS = 713.6. [08-06-07] REPAIR CARRIED OUT AS PER FEDEX EA 1-5710-112359, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CRACKED (ZONE 600) · airframe 54,481 hrs · 13,078 cycles

CRACK INDICATIONS REVEALED IN 04 FASTENER HOLES TOWARDS EDGE OF ACCESS, CUTOUT IN RIGHT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN XORS = 683.4 AND XORS = 713.6. [08-06-07] REPAIR CARRIED OUT AS PER FEDEX EA 1-5710-112360, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRUCTURE — CORRODED (ZONE 100) · airframe 54,481 hrs · 13,078 cycles

CENTER ACCESSORY COMPARTMENT BILGE AREA AT LONGERON 51R BETWEEN STA 1139 AND STA 1159, FOUND CORROSION. [08-06-07] REMOVED AND REPLACED WITH NEW LONGERON AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 54,481 hrs · 13,078 cycles

MAIN DECK CARGO CENTER STA 635 BETWEEN FLOOR PANELS NR 232FF AND NR 233GF, FOUND SEAT TRACK CROWN AREA CHIPPED OFF. CARRIED OUT REPAIR ON DAMAGED SEAT TRACK AT STA 625 TO STA 645 AS PER SRM 53-70-00 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — DENTED (BS 1851) · airframe 54,481 hrs · 13,078 cycles

WITH REFERENCE TO WORK CARD NR T1-5310-96612 PT2, DENT FOUND IN FUSELAGE AT STA 1851 BETWEEN LONGERON 35R AND LONGERON 36R. [08-06-07] REPAIR CARRIED OUT AS PER FEDEX EA 1-5310-114762, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: VANE — DELAMINATED (TE FLAP) · airframe 54,481 hrs · 13,078 cycles

RIGHT WING OUTBOARD FLAP VANE UPPER SURFACE FOUND DELAMINATED. [07-30-07] COMPLIED WITH FEDEX E.A. 1-5750-112356. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SLAT TRACK — CRACKED (ZONE 600) · airframe 54,481 hrs · 13,078 cycles

FOUND CRACK, RIGHT WING SLAT TRACK NR 14 CUTOUT. [07-30-07] REPAIRED AS PER SRM 57-10-00. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: TRUNNION — CRACKED (NLG) · airframe 54,481 hrs · 13,078 cycles

NOSE LANDING GEAR LEFT TRUNNION FITTING FOUND CRACKED. [08-03-07] CARRIED OUT REPAIR AS PER SRM 53-40- 00 FIGURE 23 VOLUME I. REPETITIVE INSPECTION TO BE CARRIED OUT NOT EXCEEDING 1,500 LANDING INTERVALS. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: TRUNNION — CRACKED (NLG) · airframe 54,481 hrs · 13,078 cycles

NOSE LANDING GEAR RIGHT TRUNNION FITTING FOUND CRACKED. [08-03-07] CARRIED OUT REPAIR AS PER SRM 53-40 -00 FIGURE 23 VOLUME I. REPETITIVE INSPECTION TO BE CARRIED OUT NOT EXCEEDING 1,500 LANDING INTERVALS. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STOP FITTING — CRACKED (ZONE 500) · airframe 54,481 hrs · 13,078 cycles

LEFT WING OUTBOARD FLAP SECONDARY UP STOP FITTING FOUND CRACKED. [08-02-07] REMOVED CRACKED FITTING AND INSTALLED NEW FITTING AT LT WING OUTBOARD FLAP AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: FIRE WARNING — FALSE ACTIVATION (NR 3 ENGINE) · airframe 50,173 hrs · 12,084 cycles

AT APPROX 2000 AT DEPARTURE, GOT NR 3 ENGINE FIRE WARNING LIGHTS AND BELLS. INTERMITTENT AT FIRST 5-10 SEC AND STEADY AT 20 SEC PHASE 1 AND CHECKLIST COMPLIED WITH. SHUTDOWN ENGINE, DISCHARGED BOTTLE. NO FUEL DUMP. NO OTHER ABNORMAL ENGINE INDICATIONS. DIVERT TO SFO. LANDED UNEVENTFULLY. PRECAUTIONARY REMOVED AND REPLACED NR 3 FDCU. REMOVED AND REPLACED NR 3 ENG NR 1 FIREX CONTAINER. UPPER RIGHT A AND B LOOP FAULTED PART NR 224-0153-503 ADDED MPN 224-0153-503, CPN 2610519 QTY 1 DETECTOR MSN 982058.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 49,905 hrs · 12,018 cycles

MAIN DECK BAY FLOOR SUPPORT FOUND WITH CORROSION AT BS 1914 LBL 47-75. MAIN DECK BAY CORRODED FLOOR SUPPORT AT BS 1941 LBL 47-75 REMOVED AND REPLACED BY FABRICATION AS PER DRAWING AGA7085 AND INSTALLED AS PER SRM 51-31 -01 VOLUME II. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SKIN PANEL — CORRODED (ZONE 200) · airframe 49,905 hrs · 12,018 cycles

UPPER CARGO COMPARTMENT UNDER FLOOR AREA, CENTER WING TANK TOP SURFACE FOUND WITH CORROSION FS STA 1219 LBL 95.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 49,905 hrs · 12,018 cycles

FORWARD CABIN COMPARTMENT SEAT TRACK FOUND WITH CORROSION AT STATION 475 LBL 27. FORWARD CABIN COMPARTMENT SEAT TRACK STATION 467 TO STATION 525 LBL 27. REPAIRED AS PER SRM 53-70-00 FIGURE I VOLUME I. FLOOR PANEL 221FF REMOVED AND REINSTALLED AS PER AMM 53-21-04-4. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CORRODED (ZONE 200) · airframe 49,905 hrs · 12,018 cycles

UPPER CARGO BAY UNDER FLOOR AREA, CENTER WING TANK TOP SURFACE FOUND WITH CORROSION FS STA 1239 LBL 02. SURFACE CORROSION ON UPPER CARGO BAY UNDER FLOOR AREA, CENTER WING TANK TOP SURFACE AT STATION 1239 LBL 02 REMOVED AS PER SRM 51-21-01 VOLUME II AND FOUND WITHIN LIMIT AS PER FEDEX E.A 1-5710-95783. MATERIAL ORIGINAL THICKNESS=0.173", MATERIAL REMOVED=0.017", REMAINING THICKNESS=0.156". REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN PANEL — CORRODED (ZONE 200) · airframe 49,905 hrs · 12,018 cycles

UPPER CARGO BAY, UNDER FLOOR AREA, CENTER WING TANK TOP SURFACE FOUND WITH CORROSION BS 1204 RBL 107. SURFACE CORROSION ON UPPER CARGO BAY UNDER FLOOR AREA, CENTER WING TANK TOP SURFACE AT BS 1204 RBL 107 REMOVED AS PER SRM 51-21-01 VOLUME II AND FOUND WITHIN LIMIT AS PER FEDEX EA 1-5710-957831. MATERIAL ORIGINAL THICKNESS=0.164", MATERIAL REMOVED=0.033", REMAINING THICKNESS=0.131". REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 49,905 hrs · 12,018 cycles

MAIN DECK COMPARTMENT SEAT TRACK FOUND WITH CORROSION AT STATION 1724, RBL 72. MAIN DECK COMPARTMENT CORRODED SEAT TRACK AT STATION 1724 RBL 72 REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II FROM STATION 1531 RBL 75 TO STATION 1887 RBL 68. REFER TO SNRM N00553 FOR SEAT TRACK REPLACEMENT. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN PANEL — CORRODED (ZONE 200) · airframe 49,905 hrs · 12,018 cycles

UPPER CARGO COMPARTMENT UNDER FLOOR AREA, CENTER WING TANK TOP SURFACE FOUND WITH CORROSION FS STA 1219 LBL 95. REMOVED AS PER SRM 51-21-01 VOLUME II AND FOUND WITHIN LIMIT AS PER FEDEX E.A 1-5710-95783. MATERIAL ORIGINAL THICKNESS=0.173", MATERIAL REMOVED=0.034", REMAINING THICKNESS=0.139". REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN PANEL — CORRODED (ZONE 200) · airframe 49,905 hrs · 12,018 cycles

UPPER CARGO COMPARTMENT, UNDER FLOOR AREA, CENTER WING TANK TOP SURFACE FOUND WITH CORROSION FS STA 1204 RBL 107.

Part: SKIN PANEL — CORRODED (ZONE 200) · airframe 49,905 hrs · 12,018 cycles

UPPER CARGO COMPARTMENT UNDER FLOOR AREA, CENTER WING TANK TOP SURFACE FOUND WITH CORROSION FS STA 1239 LBL 02.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 49,905 hrs · 12,018 cycles

MAIN DECK COMPARTMENT SEAT TRACK FOUND WITH CORROSION AT STATION 1741 - 1761 LBL 47. MAIN DECK COMPARTMENT CORRODED SEAT TRACK AT STATION 1741 - 1761 LBL 47. REMOVED AND REPLACED FROM STATION 1531 - 1887 LBL 47 AS PER SRM 51-31-01 VOLUME II WITH NEW SEAT TRACK. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 49,905 hrs · 12,018 cycles

MAIN DECK COMPARTMENT FLOOR SUPPORT FOUND WITH CORROSION AT STATION 5-73 RBL 47-75. CORRODED FLOOR SUPPORT AT STATION 5 - 73 RBL 47 - 75 REMOVED AS PER SRM 51-31-01 VOLUME II AND NEW FLOOR SUPPORT INSTALLED AS PER SRM 51-31-01 VOLUME II. NEW FLOOR SUPPORT FABRICATED AS PER DRAWING AEA7326. REPAIR CLASSIFIED AS MINOR PER GMM 6- 2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 49,905 hrs · 12,018 cycles

FORWARD CABIN COMPARTMENT SEAT TRACK FOUND WITH CORROSION AT STATION 457.660 LBL 0. CORRODED EXISTING REPAIR SEAT TRACK ON FWD CABIN COMPARTMENT AT FS STATION 457.660 LBL 0 REMOVED AS PER SRM 51-31-01 VOL II. NEW REPAIR SEAT TRACK FABRICATED AND INSTALLED AS PER SRM 53-70-00, FIG 1, VOL I. CLASSIFIED AS MAJOR REPAIR AS PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 49,905 hrs · 12,018 cycles

MAIN DECK COMPARTMENT SEAT TRACK FOUND WITH CORROSION AT STATION 1667 - 1691 LBL 75. CORROSION AT SEAT TRACK LOBE MAIN DECK COMPARTMENT STATION 1667 TO 1691 LBL 75 TRIMMED OUT AND CARRIED OUT REPAIR AS PER SRM 53-70-00 FIGURE 5 VOLUME I. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 49,905 hrs · 12,018 cycles

MAIN DECK COMPARTMENT SEAT TRACK FOUND WITH CORROSION AT STATION 1239 - 1256 LBL 27. MAIN DECK COMPARTMENT SEAT TRACK STATION 6-100 TO STATION 1269 LBL 27. REPAIRED AS PER SRM 53-70-00 FIGURE I VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 49,905 hrs · 12,018 cycles

SNRM N00923: FORWARD CABIN SEAT TRACK FOUND CORROSION AT STATION 775 LBL 47. CORRECTIVE ACTION: SNRM N00923: CORRODED SEAT TRACK AT STATION 775 LBL 47 REPAIRED AS PER SRM 53-70- 00 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (ZONE 500) · airframe 49,905 hrs · 12,018 cycles

LEFT HAND WING STATION XOS 645 (AFT OF NR 4 SLAT) LEADING EDGE SKIN INTERIOR BEADED DOUBLER FOUND CRACKED AS MARKED. REPAIR CARRIED OUT AS PER FEDEX EA 1-5730-90774. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (ZONE 500) · airframe 49,905 hrs · 12,018 cycles

LEFT HAND WING XOS 660 LEADING EDGE INTERIOR SKIN BEADED DOUBLER FOUND CRACKED AT TWO PLACES AS MARKED. REPAIR CARRIED OUT AS PER FEDEX EA 1-5730-90774.

Part: FRAME — DENTED (ZONE 200) · airframe 49,905 hrs · 12,018 cycles

MAIN DECK COMPARTMENT FRAME FOUND WITH DENT AT STATION 715 BETWEEN STRINGER 12-13R. DECK COMPARTMENT DENT AT FRAME AT STATION 715 BETWEEN STR 12- 13R, REPAIR CARRIED OUT AS PER SRM 53-30-00 FIGURE I VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: DOUBLER — CRACKED (ZONE 500) · airframe 49,905 hrs · 12,018 cycles

LEFT HAND WING STATION XOS 640 (ACCESS FROM PANEL 519CB) LEADING EDGE SKIN INTERIOR BEADED DOUBLER FOUND CRACKED AS MARKED. REPAIRED AS PER FEDEX EA 1-5730-90774. CLASSIFIED AS MINOR REPAIR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 49,905 hrs · 12,018 cycles

FORWARD CABIN COMPARTMENT SEAT TRACK FOUND WITH CORROSION AT STATION 475 LBL 27. REPAIRED AS PER SRM 53-70-00 FIGURE I VOLUME I. FLOOR PANEL 221FF REMOVED AND REINSTALLED AS PER AMM 53-21-04-4. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: WINDOW FRAME — CORRODED (ZONE 200) · airframe 49,905 hrs · 12,018 cycles

FLIGHT COMPARTMENT DURING REMOVAL AND REPLACEMENT OF CAPTAINS WINDSHIELD FOUND WINDOW FRAME FASTENERS HOLE WITH CORROSION AT SEVERAL PLACES. CORROSION BLENDED OUT AS PER SRM 51-21-02 VOL.II. FPI INSPECTION CARRIED-OUT ON REWORKED AREA AND FOUND NO CORROSION & NO CRACK EVIDENT. MAT'L REMOVED: 0.007"; MAT'L REMAINING: 0.479"; ORIGINAL THICKNESS: 0.486"; FOUND WITHIN LIMIT AS PER DWG ABA7003 TOLERANCE. REPAIR CLASSIFIED AS MINOR AS PER FEDEX GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 49,905 hrs · 12,018 cycles

MAIN DECK COMPARTMENT SEAT TRACK FOUND WITH CORROSION AT STATION 1878 LBL 70. REPAIR CARRIED OUT AS PER SRM 53-70-00 FIGURE I VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (ZONE 600) · airframe 49,905 hrs · 12,018 cycles

RIGHT HAND WING LEADING EDGE AT XORS 572 BEADED DOUBLER FOUND CRACKED AS MARKED.

Part: SKIN — DENTED (BS 999) · airframe 49,905 hrs · 12,018 cycles

FWD LOWER CARGO DOOR CUTOUT ON FUSELAGE SKIN AT STA, 999 RT IN BETWEEN LONGERON 40R AND LONGERON 41R FOUND DAMAGED. DAMAGE AT FORWARD LOWER CARGO DOOR CUTOUT ON FUSELAGE SKIN AT STATION 999 RT IN BETWEEN 40R AND LONGERON 41R REPAIRED AS PER SRM 53-50-00 FIGURE 16 VOLUME I. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SKIN — CRACKED (ZONE 600) · airframe 49,905 hrs · 12,018 cycles

HFEC OPEN HOLE INSPECTION CARRIED OUT ON RT LOWER SKINS PANEL/ACCESS DOOR CUT-OUT BETWEEN STA XORS = 683.4 AND XORS = 713.6 - FASTENER HOLES FOUND CRACK INDICATIONS ON QTY: 02 EA. HOLES. REPAIR CARRIED OUT AS PER FEDEX E.A 1-5710-90773.

Part: SKIN — CORRODED (ZONE 100) · airframe 49,905 hrs · 12,018 cycles

FWD LOWER CARGO DOOR CUTOUT ON FUSELAGE SKIN AT STA 899, RT LONGERON, 42R FOUND DAMAGED. DAMAGE AT FUSELAGE FORWARD LOWER CARGO DOOR CUTOUT ON FUSELAGE SKIN STATION 899 RT LONGERON 42R REPAIRED AS PER SRM 53-50-00 FIGURE 16 VOLUME I. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SUPPORT — CORRODED (ZONE 200) · airframe 49,905 hrs · 12,018 cycles

FORWARD CABIN FLOOR SUPPORT FOUND WITH CORROSION AT STATION 435 RBL 27-95. FORWARD CABIN FLOOR SUPPORT CORROSION AT STATION 435 RBL 27-95. REMOVED AND FOUND WITHIN LIMIT AS PER SRM 53-00-01 FIGURE 1A VOLUME I. MATERIAL ORIGINAL THICKNESS= 0.080", MATERIAL REMOVED=0.007", REMAINING THICKNESS=0.073". REWORKED AREA REPROTECTED AS PER SRM 51-21-01 VOLUME II AND PAINT TOUCHED UP AS PER SRM 51-21-02 VOLUME II. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 49,905 hrs · 12,018 cycles

MAIN DECK COMPARTMENT SEAT TRACK FOUND WITH CORROSION AT STATION 1491 RBL 47. CORRODED SEAT TRACK ON MAIN DECK COMPARTMENT BETWEEN STATION 1401 TO STATION 1531, RBL 47 REMOVED AS PER SRM 51-33-01 VOLUME II. NEW REPAIR SEAT TRACK FABRICATED AND INSTALLED AS PER SRM 53-70-00 FIGURE I, VOLUME I. REFER TO SNRM N00529 FOR REPAIR DETAILS. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 49,905 hrs · 12,018 cycles

MAIN DECK COMPARTMENT SEAT TRACK FOUND WITH CORROSION AT STATION 5-33 LBL 75 AS MARKED. REPAIRED AS PER SRM 53-70-00 FIGURE I VOLUME I. FLOOR PANEL 281BS REMOVED AND INSTALLED AS PER AMM 53-21-04-4. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 49,905 hrs · 12,018 cycles

FORWARD CABIN FLOOR SUPPORT FOUND WITH CORROSION AT STATION 435-457 RBL 30. REMOVED AND REPLACED WITH FABRICATED NEW FLOOR SUPPORT AS PER DRAWING ABA8305 AND INSTALLED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 49,905 hrs · 12,018 cycles

MAIN DECK COMPARTMENT SEAT TRACK FOUND WITH CORROSION AT STATION 1305 LBL 27 AS MARKED. CORRODED SEAT TRACK ON MAIN DECK COMPARTMENT AT STATION 1305 LBL 27 TRIMMED OUT AND CARRIED OUT REPAIR AS PER SRM 53-70-00 FIGURE I VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 49,905 hrs · 12,018 cycles

MAIN DECK COMPARTMENT SEAT TRACK FOUND WITH CORROSION AT STATION 1341-1351 RBL 27 AS MARKED. CORRODED SEAT TRACK ON MAIN DECK COMPARTMENT AT STATION 1310-1390 RBL 27 AREA TRIMMED AND CARRIED OUT REPAIR AS PER SRM 53-70-00 FIGURE III VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 49,905 hrs · 12,018 cycles

MAIN DECK COMPARTMENT SEAT TRACK FOUND WITH CORROSION AT STATION 1504 RBL 27. CORROSION AT MAIN DECK COMPARTMENT SEAT TRACK STATION 1504 RBL 27. REMOVED AND PROTECTED AS PER SRM 51-21-01 VOLUME II. MATERIAL ORIGINAL THICKNESS 0.080", REMOVED 0.008", REMAINING THICKNESS 0.072" AND FOUND WITHIN LIMIT AS PER SRM 53-70-00 FIGURE III VOLUME I. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 49,905 hrs · 12,018 cycles

MAIN DECK COMPARTMENT SEAT TRACK FOUND WITH CORROSION AT STATION 1331-1341 RBL 27 AS MARKED. MAIN DECK COMPARTMENT SEAT TRACK AT STATION 1310-1390 RBL 27 CARRIED OUT REPAIR AS PER SRM 53-70-00 VOLUME I. REFER TO SNRM N00776 FOR REPAIR DETAILS. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: LONGERON — CRACKED (ZONE 100) · airframe 49,905 hrs · 12,018 cycles

LONGERON 35R AT STATION 5-11 CRACKED. CRACKED LONGERON AT CENTER CARGO LONGERON 35R STATION 5-11 TRIMMED OUT AND CARRIED OUT REPAIR AS PER SRM 53-10-00 FIGURE I VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 49,905 hrs · 12,018 cycles

MAIN DECK COMPARTMENT SEAT TRACK FOUND WITH CORROSION AT STATION 1385 RBL 27 AS MARKED. MAIN DECK COMPARTMENT SEAT TRACK AT STATION 1310-1390 RBL 27 CARRIED OUT REPAIR AS PER SRM 53-70-00 VOLUME I. REFER TO SNRM N00776 FOR REPAIR DETAILS. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (RT WING) · airframe 49,905 hrs · 12,018 cycles

HFEC INSPECTION FOUND CRACK ON RIGHT HAND WING OUTBOARD END OF STRINGER S-13R APPROXIMATELY 13 INCHES, AS MARKED. REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. LEAK CHECK CARRIED OUT AT REWORKED AREA AS PER AMM 28-00-00 AND FOUND NO LEAK. THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 49,905 hrs · 12,018 cycles

MAIN DECK COMPARTMENT FLOOR SUPPORT FOUND WITH CORROSION AT STATION 1401 RBL 08-27, AS MARKED. REMOVED AS PER SRM 51-31-01 VOLUME II AND NEW FLOOR SUPPORT INSTALLED AS PER SRM 51-31-01 VOLUME II. NEW FLOOR SUPPORT FABRICATED AS PER DRAWING AEA0397. REPAIR CLASSIFIED AS MINOR PER GMM 6- 2-100.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 49,905 hrs · 12,018 cycles

CABIN COMPARTMENT GALLEY INBOARD AFT MOUNTING FLOOR SUPPORT FOUND WITH CORROSION AT STATION 418. REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MINOR PER GMM 6- 2-100.

Part: STRINGER — CRACKED (RT WING) · airframe 49,905 hrs · 12,018 cycles

HFEC INSPECTION FOUND CRACK ON RIGHT HAND WING OUTBOARD END OF STRINGER S-10R APPROXIMATELY 4 INCHES, AS MARKED. REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. LEAK CHECK CARRIED OUT AT REWORKED AREA AS PER AMM 28-00-00 AND FOUND NO LEAK. THIS REPAIR IS CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: STRINGER — CRACKED (LT WING) · airframe 49,905 hrs · 12,018 cycles

HFEC INSPECTION FOUND CRACK ON LEFT HAND WING OUTBOARD END OF STRINGERS S-13L APPROXIMATELY 7 INCHES, AS MARKED. REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. FUEL LEAK CHECK CARRIED OUT AND FOUND NO LEAK AS PER AMM 28-00-00. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: STRINGER — CRACKED (RT WING) · airframe 49,905 hrs · 12,018 cycles

HFEC INSPECTION FOUND CRACK ON RIGHT HAND WING OUTBOARD END OF STRINGER S-12R APPROXIMATELY 3.5 INCHES, AS MARKED. REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. FUEL LEAK CHECK CARRIED OUT AND FOUND NO LEAK AS PER AMM 28-00-00. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: STRUCTURE — CRACKED (LT WING) · airframe 49,905 hrs · 12,018 cycles

LEFT HAND WING LEADING EDGE ANTI-ICE TELESCOPIC DUCT CUTOUT AT XORS372 FOUND CRACKED, AS MARKED. REPAIRED AS PER FEDEX EA 1-5730-90764. THIS REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 49,905 hrs · 12,018 cycles

MAIN DECK COMPARTMENT FLOOR SUPPORT FOUND WITH CORROSION AT STATION 1901-1921 LBL 56. REMOVED AND REPLACED BY FABRICATION AS PER DWG AGA7551 AND INSTALLED AS PER SRM 51-31-01 VOL.II. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 49,905 hrs · 12,018 cycles

MAIN DECK COMPARTMENT SEAT TRACK FOUND WITH CORROSION AT STATION 1305 LBL 75, AS MARKED. DAMAGED SEAT TRACK REMOVED AS PER SRM 53-70-00 FIGURE I VOLUME I. NEW SEAT TRACK AND SPLICE REWORKED AS PER SRM 53-70- 00 FIGURE I VOLUME I. NEW SEAT TRACK AND SPLICE INSTALLED AS PER SRM 53-70-00 FIGURE I VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (LT WING) · airframe 49,905 hrs · 12,018 cycles

HFEC INSPECTION FOUND CRACK ON LEFT HAND WING OUTBOARD END OF STRINGER S-44L APPROXIMATELY 6.5 INCHES, AS MARKED. REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. LEAK CHECK CARRIED OUT AND FOUND NO LEAK AS PER AMM 28- 00-00. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 49,905 hrs · 12,018 cycles

MAIN DECK COMPARTMENT FLOOR SUPPORT FOUND WITH CORROSION AT STATION 1661 LBL 95. REMOVED AS PER SRM 51-31-01 VOLUME II AND NEW FLOOR SUPPORT INSTALLED AS PER SRM 51-31-01 VOLUME II. NEW FLOOR SUPPORT FABRICATED AS PER DRAWING AFA3853. REPAIR CLASSIFIED AS MINOR PER GMM 6- 2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 49,905 hrs · 12,018 cycles

MAIN DECK COMPARTMENT SEAT TRACK FOUND WITH CORROSION AT STATION 1222 LBL 75, AS MARKED. REMOVED & NEW SEAT TRACK FABRICATED AND INSTALLED AS PER SRM 53-70-00 FIGURE I VOLUME I. REFER TO SNRM N00760 FOR DETAILS. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 49,905 hrs · 12,018 cycles

CABIN COMPARTMENT LAVATORY INBOARD AFT MOUNTING FLOOR SUPPORT FOUND WITH CORROSION. REMOVED AND REPLACED AS PER SRM 51-31-01 VOL.II. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 49,905 hrs · 12,018 cycles

MAIN DECK COMPARTMENT FLOOR SUPPORT FOUND WITH CORROSION AT STATION 1481 RBL 27-47, AS MARKED. REMOVED AS PER SRM 51-31-01 VOLUME II AND NEW FLOOR SUPPORT INSTALLED AS PER SRM 51-31-01 VOLUME II. NEW FLOOR SUPPORT FABRICATED AS PER DRAWING AEA7326. REPAIR CLASSIFIED AS MINOR PER GMM 6- 2-100.

Part: STRINGER — CRACKED (RT WING) · airframe 49,905 hrs · 12,018 cycles

HFEC INSPECTION FOUND CRACK ON RIGHT HAND WING OUTBOARD END OF STRINGER S-14R APPROXIMATELY 13 INCHES, AS MARKED. REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. LEAK CHECK CARRIED OUT AND FOUND NO LEAK AS PER AMM 28-00-00. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 49,905 hrs · 12,018 cycles

MAIN DECK COMPARTMENT SEAT TRACK FOUND WITH CORROSION AT STATION 1276 LBL 75, AS MARKED.

Part: STRINGER — CRACKED (LT WING) · airframe 49,905 hrs · 12,018 cycles

HFEC INSPECTION FOUND CRACK ON LEFT HAND WING OUTBOARD END OF STRINGER S-41L APPROXIMATELY 5.5 INCHES, AS MARKED. REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. LEAK CHECK CARRIED OUT AND FOUND NO LEAK AS PER AMM 28-00-00. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.06FDEA0769.

Part: STRINGER — CRACKED (RT WING) · airframe 49,905 hrs · 12,018 cycles

HFEC INSPECTION FOUND CRACK ON RIGHT HAND WING OUTBOARD END OF STRINGER S-11R APPROXIMATELY 12 INCHES, AS MARKED. REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. LEAK CHECK CARRIED OUT AT REWORKED AREA AS PER AMM 28-00-00 AND FOUND NO LEAK. THIS REPAIR IS CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 49,905 hrs · 12,018 cycles

MAIN DECK COMPARTMENT FLOOR SUPPORT FOUND WITH CORROSION AT STATION 1501 RBL 08-27, AS MARKED. REMOVED AS PER SRM 51-31-01 VOLUME II AND NEW FLOOR SUPPORT INSTALLED AS PER SRM 51-31-01 VOLUME II. NEW FLOOR SUPPORT FABRICATED AS PER DRAWING AEA0397. REPAIR CLASSIFIED AS MINOR PER GMM 6- 2-100.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 49,905 hrs · 12,018 cycles

MAIN DECK COMPARTMENT FLOOR SUPPORT FOUND WITH CORROSION AT STATION 1481 LBL 78, AS MARKED. FABRICATED AS PER DRAWING AEA0364. FLOOR SUPPORT REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 49,905 hrs · 12,018 cycles

MAIN DECK COMPARTMENT FLOOR SUPPORT FOUND WITH CORROSION AT STATION 1853 RBL 75. REMOVED AS PER SRM 51-31-01. VOLUME II AND NEW FLOOR SUPPORT INSTALLED AS PER SRM 51-31-01 VOLUME II. NEW FLOOR SUPPORT FABRICATED AS PER DRAWING AGA3814. REPAIR CLASSIFIED AS MINOR PER GMM 6- 2-100.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 49,905 hrs · 12,018 cycles

MAIN DECK COMPARTMENT FLOOR SUPPORT FOUND WITH CORROSION AT STATION 1741 LBL 91. REMOVED AS PER SRM 51-31-01 VOLUME II AND NEW FLOOR SUPPORT INSTALLED AS PER SRM 51-31-01 VOLUME II. NEW FLOOR SUPPORT FABRICATED AS PER DRAWING AFA3853. REPAIR CLASSIFIED AS MINOR PER GMM 6- 2-100.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 49,905 hrs · 12,018 cycles

MAIN DECK COMPARTMENT FLOOR SUPPORT FOUND CRACKED AT STATION 1219 RBL 70, AS MARKED. REMOVED AS PER SRM 51-31-01 VOLUME II AND NEW FLOOR SUPPORT INSTALLED AS PER SRM 51-31-01 VOLUME II. NEW FLOOR SUPPORT FABRICATED AS PER DRAWING ACA3762. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 49,905 hrs · 12,018 cycles

MAIN DECK COMPARTMENT SEAT TRACK FOUND WITH CORROSION AT STATION 1321 LBL 75, AS MARKED. CORRODED SEAT TRACK ON MAIN DECK COMPARTMENT AT STATION 1321 LBL 75 REPAIRED AS PER SRM 53-70-00 FIGURE I VOLUME I. REFER TO SNRM N00761 FOR DETAILS. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SUPPORT — CORRODED (ZONE 200) · airframe 49,905 hrs · 12,018 cycles

MAIN DECK COMPARTMENT FLOOR SUPPORT FOUND WITH CORROSION AT STATION 1971 LBL 0. MAIN DECK COMPARTMENT STATION 1971 LBL 0 FLOOR SUPPORT CORROSION REMOVED AS PER SRM 51-21-01 VOLUME II. MATERIAL ORIGINAL THICKNESS=0.505", REMOVED=0.020", REMAINING THICKNESS=0.485" AND FOUND WITHIN LIMIT AS PER SRM 53-00-01 VOLUME I. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (LT WING) · airframe 49,905 hrs · 12,018 cycles

HFEC INSPECTION FOUND CRACK ON LEFT HAND WING OUTBOARD END OF STRINGERS S-14L APPROXIMATELY 14 INCHES, AS MARKED. REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. LEAK CHECK CARRIED OUT AND FOUND NO LEAK AS PER AMM 28- 00-00. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 49,905 hrs · 12,018 cycles

MAIN DECK COMPARTMENT FLOOR SUPPORT FOUND WITH CORROSION AT STATION 5-93 RBL 08-27, AS MARKED. REMOVED AS PER SRM 51-31-01 VOLUME II AND NEW FLOOR SUPPORT INSTALLED AS PER SRM 51-31-01 VOLUME II. NEW FLOOR SUPPORT FABRICATED AS PER DRAWING AFA3853. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 49,905 hrs · 12,018 cycles

MAIN DECK COMPARTMENT FLOOR SUPPORT FOUND WITH CORROSION AT STATION 1741 RBL 83. REMOVED AS PER SRM 51-31-01 VOLUME II AND NEW FLOOR SUPPORT INSTALLED AS PER SRM 51-31-01 VOLUME II. NEW FLOOR SUPPORT FABRICATED AS PER DRAWING AFA3853. REPAIR CLASSIFIED AS MINOR PER GMM 6- 2-100.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 49,905 hrs · 12,018 cycles

MAIN DECK COMPARTMENT FLOOR SUPPORT FOUND WITH CORROSION AT STATION 1361 LBL 75-107, AS MARKED. REMOVED AS PER SRM 51-31-01 VOLUME II AND NEW FLOOR SUPPORT INSTALLED AS PER SRM 51-31-01 VOLUME II. NEW FLOOR SUPPORT FABRICATED AS PER DRAWING AEA0394. REPAIR CLASSIFIED AS MINOR PER GMM 6- 2-100.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 49,905 hrs · 12,018 cycles

MAIN DECK COMPARTMENT FLOOR SUPPORT FOUND WITH CORROSION AT STATION 1560 LBL 95. REMOVED AS PER SRM 51-31-01 VOLUME II AND NEW FLOOR SUPPORT INSTALLED AS PER SRM 51-31-01 VOLUME II. NEW FLOOR SUPPORT FABRICATED AS PER DRAWING AFA3853. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 49,905 hrs · 12,018 cycles

MAIN DECK COMPARTMENT FLOOR SUPPORT FOUND WITH CRACK AT STATION 1481 LBL 47 - 75, AS MARKED. REMOVED AS PER SRM 51-31-01 VOLUME II AND NEW FLOOR SUPPORT INSTALLED AS PER SRM 51-31-01 VOLUME II. NEW FLOOR SUPPORT FABRICATED AS PER DRAWING AEA7326. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 49,905 hrs · 12,018 cycles

MAIN DECK COMPARTMENT SEAT TRACK FOUND WITH CORROSION AT STATION 1401 LBL 75, AS MARKED. CARRIED OUT REPAIR AS PER SRM 53-70-00 FIGURE I VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2 -100.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 49,905 hrs · 12,018 cycles

MAIN DECK COMPARTMENT FLOOR SUPPORT FOUND WITH CORROSION AT STATION 5-73 RBL 80. REMOVED AS PER SRM 51-31-01 VOLUME II AND NEW FLOOR SUPPORT INSTALLED AS PER SRM 51-31-01 VOLUME II. NEW FLOOR SUPPORT FABRICATED AS PER DRAWING AFA3853. REPAIR CLASSIFIED AS MINOR PER GMM 6- 2-100.

Part: SEAT TRACK — CORRODED (BS 1741-1821) · airframe 49,905 hrs · 12,018 cycles

MAIN DECK COMPARTMENT SEAT TRACK FOUND WITH CORROSION AT STATION 1741-1821 LBL 107. REMOVED AND REPLACED AS PER SRM 51-31-01 VOL.II. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. REFER TO SNRM N00549 FOR FURTHER DETAILS.

Part: FLOORBEAM — CORRODED (BS 1481) · airframe 49,905 hrs · 12,018 cycles

MAIN DECK COMPARTMENT FLOOR SUPPORT FOUND WITH CORROSION AT STATION 1481 RBL 47-75. CORRODED FLOOR SUPPORT AT STATION 1481 RBL 47-75 REMOVED AS PER SRM 51-31-01 VOLUME II AND NEW FLOOR SUPPORT INSTALLED PER SRM 51-31-01 VOLUME II. NEW FLOOR SUPPORT FABRICATED PER DRAWING AEA 7326. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1821-1871) · airframe 49,905 hrs · 12,018 cycles

MAIN DECK COMPARTMENT SEAT TRACK FOUND WITH CORROSION AT STATION 1821-1871 LBL 101. REMOVED AND REPLACED FROM STA 1531 LBL 107 TO STA 2007 LBL 101 AS PER SRM 51-31-01 VOL.II. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 49,905 hrs · 12,018 cycles

MAIN DECK COMPARTMENT SEAT TRACK FOUND WITH CORROSION AT STATION 1570 - 1661 LBL 107. REMOVED AND REPLACED AS PER SRM 51-31-01 VOL.II. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. REFER TO SNRM N00549 FOR FURTHER DETAILS.

Part: FLOORBEAM — CORRODED (BS 1661) · airframe 49,905 hrs · 12,018 cycles

MAIN DECK COMPARTMENT FLOOR SUPPORT FOUND WITH CORROSION AT STATION 1661 RBL 91. REMOVED AS PER SRM 51-31-01 VOLUME II AND NEW FLOOR SUPPORT INSTALLED AS PER SRM 51-31-01 VOLUME II. NEW FLOOR SUPPORT FABRICATED AS PER DRAWING AFA 3853. REPAIR CLASSIFIED AS MINOR PER GMM 6- 2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 49,905 hrs · 12,018 cycles

MAIN DECK COMPARTMENT SEAT TRACK FOUND WITH CORROSION AT STATION 5-75 LBL 47. MAIN DECK COMPARTMENT SEAT TRACK FROM STA 1531 TO 1887 LBL 47 REMOVED AND REPLACED AS PER SRM 51-31-01 VOL.II. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 49,905 hrs · 12,018 cycles

MAIN DECK COMPARTMENT FLOOR SUPPORT FOUND WITH CORROSION AT STATION 1561 RBL 80. REMOVED PER SRM 51-31-01 VOL.II. NEW FLOOR SUPPORT INSTALLED AS PER SRM 51-31-01 VOL.II. NEW FLOOR SUPPORT FABRICATED AS PER DWG NR AFA3853. REPAIR CLASSIFIED AS MINOR AS PER FEDEX GMM 6-2-100.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 49,905 hrs · 12,018 cycles

MAIN DECK COMPARTMENT FLOOR SUPPORT FOUND WITH CORROSION AT STATION 5-73 LBL 80. REMOVED AS PER SRM 51-31-01 VOLUME II AND NEW FLOOR SUPPORT INSTALLED AS PER SRM 51-31-01 VOLUME II. NEW FLOOR SUPPORT FABRICATED AS PER DRAWING AFA3853. REPAIR CLASSIFIED AS MINOR PER GMM 6- 2-100.

Part: SEAT TRACK — CORRODED (BS 1661-1741) · airframe 49,905 hrs · 12,018 cycles

MAIN DECK COMPARTMENT SEAT TRACK FOUND WITH CORROSION AT STATION 1661 - 1741 LBL 107. REMOVED AND REPLACED AS PER SRM 51-31-01 VOL.II. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. REFER TO SNRM N00549 FOR FURTHER DETAILS.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 49,905 hrs · 12,018 cycles

MAIN DECK COMPARTMENT SEAT TRACK FOUND WITH CORROSION AT STATION 1531 - 1551 LBL 107. REMOVED AND REPLACED AS PER SRM 51-31-01 VOL.II. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. REFER TO SNRM N00549 FOR FURTHER DETAILS.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 49,905 hrs · 12,018 cycles

MAIN DECK COMPARTMENT SEAT TRACK FOUND WITH CORROSION AT STATION 1531 - 5-73 LBL 107. REMOVED AND REPLACED AS PER SRM 51-31-01 VOL.II. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. REFER TO SNRM N00549 FOR FURTHER DETAILS.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 49,905 hrs · 12,018 cycles

MAIN DECK COMPARTMENT SEAT TRACK FOUND WITH CORROSION AT STATION 1685 LBL 47. MAIN DECK COMPARTMENT SEAT TRACK FROM STA 1531 TO 1887 LBL 47 REMOVED AND REPLACED AS PER SRM 51-31-01 VOL.II. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 49,905 hrs · 12,018 cycles

MAIN DECK COMPARTMENT FLOOR SUPPORT FOUND WITH CORROSION AT STATION 1481 RBL 90. REMOVED AS PER SRM 51-31-01 VOLUME II AND NEW FLOOR SUPPORT INSTALLED AS PER SRM 51-31-01 VOLUME II. NEW FLOOR SUPPORT FABRICATED AS PER DRAWING AEA0364. REPAIR CLASSIFIED AS MINOR PER GMM 6- 2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 49,905 hrs · 12,018 cycles

MAIN DECK COMPARTMENT SEAT TRACK FOUND WITH CORROSION AT STATION 1561 LBL 47. MAIN DECK COMPARTMENT SEAT TRACK FROM STA 1531 TO 1887 LBL 47, REMOVED AND REPLACED AS PER SRM 51-31-01 VOL.II. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1471-1521) · airframe 49,905 hrs · 12,018 cycles

MAIN DECK COMPARTMENT SEAT TRACK FOUND WITH CORROSION AT STATION 1471-1521 LBL 75. CARRIED OUT REPAIR AS PER SRM 53-70-00 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 49,905 hrs · 12,018 cycles

MAIN DECK COMPARTMENT SEAT TRACK FOUND WITH CORROSION AT STATION 1491 RBL 47. CORRODED SEAT TRACK ON MAIN DECK COMPARTMENT BETWEEN STATION 1401 TO STATION 1531,RBL 47 REMOVED AS PER SRM 51-33-01 VOLUME II. NEW REPAIR SEAT TRACK FABRICATED AND INSTALLED AS PER SRM 53-70-00 FIGURE I, VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2- 100.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 49,905 hrs · 12,018 cycles

MAIN DECK COMPARTMENT SEAT TRACK FOUND WITH CORROSION AT STATION 1651 LBL 47. CORRECTIVE ACTION: SNRM N00515: MAIN DECK COMPARTMENT SEAT TRACK FROM STA 1531 TO 1887 LBL 47 REMOVED AND REPLACED AS PER SRM 51-31-01 VOL.II. REFER TO SNRM N00512 FOR FURTHER DETAILS. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.

Part: FLOORBEAM — CORRODED (BS 1561 RBL 91) · airframe 49,905 hrs · 12,018 cycles

MAIN DECK COMPARTMENT FLOOR SUPPORT FOUND WITH CORROSION AT STATION 1561 RBL 91. REMOVED AS PER SRM 51-31-01 VOLUME II AND NEW FLOOR SUPPORT INSTALLED AS PER SRM 51-31-01 VOLUME II. NEW FLOOR SUPPORT FABRICATED AS PER DRAWING AFA3853. REPAIR CLASSIFIED AS MINOR PER GMM 6- 2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 49,905 hrs · 12,018 cycles

MAIN DECK COMPARTMENT SEAT TRACK FOUND WITH CORROSION AT STATION 5-20 RBL 75.

Part: SEAT TRACK — CORRODED (BS 1791-1841) · airframe 49,905 hrs · 12,018 cycles

MAIN DECK COMPARTMENT SEAT TRACK FOUND WITH CORROSION AT STATION 1791-1841 RBL 68.

Part: SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 49,905 hrs · 12,018 cycles

MAIN DECK COMPARTMENT FLOOR SUPPORT FOUND WITH CORROSION AT STATION 5-73 RBL 80. CORRODED FLOOR SUPPORT AT STATION 5-73 RBL 80 REMOVED AS PER SRM 51-31-01 VOLUME II AND NEW FLOOR SUPPORT INSTALLED AS PER SRM 51-31-01 VOLUME II. NEW FLOOR SUPPORT FABRICATED AS PER DRAWING AFA3853. REPAIR CLASSIFIED AS MINOR PER GMM 6- 2-100.

Part: DUCT — CRACKED (ZONE 600) · airframe 49,905 hrs · 12,018 cycles

RIGHT HAND WING LEADING EDGE ANTI-ICE TELESCOPIC DUCT CUTOUT AT XORS372 FOUND CRACKED AS MARKED. REPAIRED AS PER FEDEX EA 1-5730-90763.

Part: SEAT TRACK — CORRODED (BS 1561-1661) · airframe 49,905 hrs · 12,018 cycles

MAIN DECK COMPARTMENT SEAT TRACK FOUND WITH CORROSION AT STATION 1561-1661 RBL 75.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 45,476 hrs · 10,992 cycles

CABIN SEAT TRACK - LBL 47 STA 965 FOUND WORN BEYOND LIMITS. CABIN SEAT TRACK - LBL 47 STA 965 AREA REPAIR CARRIED OUT AS PER SRM 53- 70-00 FIG.1 VOL I AND SRM 51-33-01 VOL II.

Part: SPLICE — CRACKED (ZONE 100) · airframe 45,476 hrs · 10,992 cycles

FORWARD CARGO COMPARTMENT - STA 755 TO 775 STR 43L SPLICE FOUND CRACKED. FORWARD CARGO COMPARTMENT - STA 755 TO 775 STR 43L AREA SPLICE REMOVED AND REPLACED AS PER SRM 51-31-01 & 51-33-01 VOL II.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 45,476 hrs · 10,992 cycles

CABIN SEAT TRACK FOUND WORN BEYOND LIMITS AT STA 1090 LBL 47. REPAIRED AS PER SRM 53-70-00 FIG 1, VOL I & SRM 51-33-01 VOL II.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 45,476 hrs · 10,992 cycles

CABIN SEAT TRACK FOUND WORN BEYOND LIMITS AT STA 998 AND 1026 RBL 47. SEAT TRACK REPAIRED AS PER SRM 53-70-00 FIG1 VOL 1 AND SRM 51-33-01 VOL 2.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 45,476 hrs · 10,992 cycles

CABIN SEAT TRACK FOUND WORN BEYOND LIMITS AT STA 1372-1376 LBL 47. WORN SEAT TRACK ON CABIN AT STA 1372-1376, LBL 47 REPAIRED AS PER SRM 53-70-00, SHEET 1, FIG 1 VOL II.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 45,476 hrs · 10,992 cycles

CABIN SEAT TRACK AT STA 1369 RBL 75 FOUND CORRODED. CABIN SEAT TRACK AT STA 1369 RBL 75 CORROSION AREA REPAIR CARRIED OUT AS PER SRM 53-70-00 FIG 1 VOL I AND SRM 51-33-01 VOL II.

Part: TEE FITTING — CORRODED (ZONE 600) · airframe 45,476 hrs · 10,992 cycles

RIGHT HAND WING, INBOARD FLAP VANE INBOARD SUPPORT FITTING, INBOARD AFT HOLE CORRODED AND OUTBOARD HOLE (03 OFF) CORRODED. ALL BORES ARE NOT WITHIN EO LIMITS. RIGHT HAND WING, INBOARD FLAP VANE INBOARD SUPPORT FITTING, REMOVED AND REPLACED AS PER AMM 27-50-24 FUNCTIONAL TEST CARRIED OUT FOUND SATISFACTORY AS PER AMM 27-50-00-860-801.

Part: SUPPORT FITTING — CORRODED (ZONE 600) · airframe 45,476 hrs · 10,992 cycles

RT WING - INBOARD FLAP VANE, OUTBOARD SUPPORT FITTING INBOARD HOLES (03 OFF) ARE CORRODED. ALL BORES ARE NOT WITHIN EO LIMITS. SUPPORT FITTING REPLACED AS PER AMM27-50-24 AND FUNCTIONAL TEST CARRIED OUT AS PER AMM 27-50-00-860-801.

Part: FITTING — CORRODED (ZONE 600) · airframe 45,476 hrs · 10,992 cycles

RT WING IB FLAP VANE, OB TEE FITTING BORE HOLES HAVE CORROSION. CORROSION REMOVED AS PER SRM 51-21-01 VOL 2 AND REPAIRED AS PER FEDEX EA 1-5750-81570.

Part: SUPPORT — CORRODED (ZONE 500) · airframe 45,476 hrs · 10,992 cycles

LT WING - INBOARD FLAP VANE, OUTBOARD SUPPORT FITTING INBOARD HOLES (03 OFF) ARE CORRODED AND OUTBOARD HOLES FWD AND CENTER ARE CORRODED. ALL BORES ARE NOT WITHIN EO LIMITS. SUPPORT FITTING REPLACED AS PER AMM27-50-24 AND FUNCTIONAL TEST CARRIED OUT AS PER AMM 27-50-00-860-801.

Part: BRACKET — CORRODED (ZONE 600) · airframe 45,476 hrs · 10,992 cycles

RIGHT WING INBOARD FLAP VANE, INBOARD TEE FITTING HOLES HAVE CORROSION AND FORWARD HOLE BORE IS NOT WITHIN EO LIMITS. CORROSION REMOVED AS PER SRM 51-21-01 VOL 2 AND REPAIRED AS PER FEDEX EA 1-5750-81569 TITLE: WINGS TRAILING EDGE FLAPS, RIGHT HAND I/B FLAP VANE, I/B TEE FITTING BORES, CORROSION REPAIR.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 45,476 hrs · 10,992 cycles

MAIN DECK - ATTIC AREA STA 5-116 LONGERON 9R LONGERON SPLICE FOUND CRACK. NEW LONGERON SPLICE FABRICATED AS PER DWG A5A7112. CRACKED LONGERON SPLICE REMOVED & REPLACED AS PER SRM 51-31-01 VOL 2.

Part: STRUCTURE — CORRODED (ZONE 300) · airframe 45,476 hrs · 10,992 cycles

EMPENNAGE, UPPER VERTICAL STAB AT AFT CTR SPAR APPROX ZFR 564 RT EXTRUSION. EXTERIOR SURFACE FOUND CORRODED. CORROSION REPAIRED AS PER FEDEX EA 1-5530-81578.

Part: SUPPORT FITTING — CORRODED (ZONE 500) · airframe 45,476 hrs · 10,992 cycles

LT WING INBOARD FLAP VANE INBOARD SUPPORT FITTING INBOARD HOLES (03 OFF) ARE CORRODED AND OUTBOARD AFT HOLE IS CORRODED. ALL BORES ARE NOT WITHIN EO LIMITS. SUPPORT FITTING REPLACED AS PER AMM27-50-24 AND FUNCTIONAL TEST CARRIED OUT AS PER AMM 27-50-00-860-801.

Part: VANE — CORRODED (ZONE 500) · airframe 45,476 hrs · 10,992 cycles

LT WING IB FLAP VANE, IB TEE FITTING BORES HAVE CORROSION AND AFT HOLE IS NOT WITHIN EO LIMITS. CORROSION REMOVED AS PER SRM 51-21-01 VOL2 AND REPAIRED AS PER FEDEX EA 1-5750-81571.

Part: TEE FITTING — CORRODED (FLAP VANE) · airframe 45,476 hrs · 10,992 cycles

LEFT HAND WING - INBOARD FLAP VANE, OUTBOARD TEE FITTING BORES FOUND CORROSION ARE NOT WITHIN EO LIMITS. TEE FITTING REPLACED AS PER AMM27-50-22 AND OPERATIONAL TEST CARRIED OUT AS PER AMM 27-50-00.

Part: SPAR CAP — CORRODED (ZONE 300) · airframe 45,476 hrs · 10,992 cycles

EMPENNAGE, UPPER VERTICAL STAB AT FWD CTR SPAR APPROX BETWEEN ZFR 300 TO 340 RT SKIN EXTERIOR SURFACE FOUND CORRODED. EMPENNAGE, UPPER VERTICAL STAB AT FWD CTR SPAR APPROX BETWEEN ZFR 300 TO 340 RT SKIN EXTERIOR SURFACE CORROSION AREA REPAIRED AS PER FEDEX EA NR 1- 5530-81579, TITLE: STABILIZERS, UPPER VERTICAL STABILIZER, RT FORWARD CENTER SPAR CAP, CORROSION REPAIR.

Part: LONGERON SPLICE — CRACKED (FUSELAGE) · airframe 45,476 hrs · 10,992 cycles

MAIN DECK - ATTIC AREA STA 1538 LONGERON 6R LONGERON SPLICE FOUND CRACK. NEW LONGERON SPLICE FABRICATED AS PER DWG NR A5A7112. CRACKED LONGERON SPLICE REMOVED & REPLACED AS PER SRM51-33-01 VOL 2.

Part: SPAR — CORRODED (ZONE 300) · airframe 45,476 hrs · 10,992 cycles

EMPENNAGE, UPPER VERTICAL STAB AT FRONT SPAR BETWEEN ZID 92.50 TO ZFR 424.219 LT SKIN EXTERIOR SURFACE FOUND CORRODED. REMOVED & REPAIRED AS PER FEDEX EA 1-5530-81581.

Part: SPAR — CORRODED (ZONE 300) · airframe 45,476 hrs · 10,992 cycles

EMPENNAGE, UPPER VERTICAL STAB AT BETWEEN FWD CTR SPAR TO AFT CTR SPAR, ZID 92.50 LT SKIN EXTERIOR SURFACE FOUND CORRODED. CORROSION AREA REPAIRED AS PER FEDEX EA 1-5530-81582.

Part: SPAR — CORRODED (ZONE 300) · airframe 45,476 hrs · 10,992 cycles

EMPENNAGE, UPPER VERTICAL STAB AT BETWEEN FWD CTR SPAR TO AFT CTR SPAR ZFR 328.0 LT SKIN EXTERIOR SURFACE FOUND CORRODED. CORROSION REMOVED & WITHIN LIMIT AS PER SRM55-00-01VOL1.

Part: SPAR — CORRODED (ZONE 300) · airframe 45,476 hrs · 10,992 cycles

EMPENNAGE, UPPER VERTICAL STAB AT FRONT SPAR BERWEEN ZFR 400.681 TO 424.219 LT EXTRUSION EXTERIOR SURFACE FOUND CORRODED. FOUND WITHIN LIMIT AS PER FEDEX EA #1-5530-81581.

Part: SPAR — CORRODED (ZONE 300) · airframe 45,476 hrs · 10,992 cycles

EMPENNAGE, UPPER VERTICAL STAB AT AFT CTR SPAR BERWEEN ZFR 389.681 TO 424.219 LT EXTRUSION EXTERIOR SURFACE FOUND CORRODED. CORROSION REMOVED AND REPAIRED AS PER EA 1-5530-81580.

Part: STRUCTURE — CORRODED (STABILIZER) · airframe 45,476 hrs · 10,992 cycles

EMPENNAGE, UPPER VERTICAL STAB AT REAR SPAR ZFR 510 RT EXTRUSION, EXTERIOR SURFACE FOUND CORRODED. REMOVED AS PER SRM 51-21-01 VOL II & REPAIRED AS PER FEDEX EA NR 1-5530-81577.

Part: FRAME — CRACKED (ZONE 400) · airframe 45,476 hrs · 10,992 cycles

ENG NR 1 LEFT HAND T/R COWL TOP AT FORWARD FRAME FOUND CRACKED. FRAME CRACKED REPAIR AS PER DRAWING SRZ78-002.

Part: COWLING — CRACKED (ZONE 400) · airframe 45,476 hrs · 10,992 cycles

ENG NR 3 LEFT HAND T/R COWL AT UPPER SLIDER TRACK END FOUND CRACKED. UPP SLIDER TRACK REPAIRED AS PER FAA FORM 8130-3 TRACKING NR 5590 (J009773-000).

Part: COWLING — CRACKED (THRUST REVERSER) · airframe 45,476 hrs · 10,992 cycles

ENG NR 2 LT HAND T/R COWL AT UPPER SLIDER TRACK END CRACKED. ENG NR 2 LEFT HAND T/R COWL UPPER SLIDER TRACK REPAIRED IAW ROHR AERO SERVICES - ASIA ENGINEERING REPAIR NR 'RASA-040560'. (WITH FAA FORM 8130-3, TRACKING 5586, J009768-000).

Part: FITTING — CRACKED (ZONE 600) · airframe 45,476 hrs · 10,992 cycles

RIGHT HAND WING FOUND OUTBOARD FLAP INBOARD STOP FITTING CRACKED, DURING DVI. STOP FITTING REMOVED & REPLACED AS PER SRM51-31-01VOL2 & SRM 51-33-01 VOL2.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 45,476 hrs · 10,992 cycles

FORWARD CABIN, MOST OUTBOARD LEFT SIDE SEAT TRACK AT APPROX STA 430-450 FOUND TOP SURFACES WITH CORROSION. SNRM N0083, FORWARD CABIN, STA 430-450 MOST OUTBOARD LEFT SIDE SEAT TRACK. CORROSION REMOVED AND REPLACED AS PER SRM 51-31-01 VOL II AND SRM 51-33-01 VOL II..

Part: HINGE — CRACKED (ZONE 500) · airframe 40,937 hrs · 9,947 cycles

SNRM N1069 : LT WING FOUND LT OUTBOARD FLAP, INBOARD AFT HINGE FITTING TO FLAP LOWER AFT, FWD MOST HOLE QTY 01 EACH WITH SUSPECTED CRACK. LT WING OUTBOARD FLAP REMOVED AND REPLACED AS PER MM 27-50-30-4. FLAP RIGGING AND OPERATIONAL CHECK CARRIED-OUT AS PER MM 27-50-00-5, FOUND SATISFACTORY. COMPLIED WITH FEDEX EA 1-5750-66425 - WINGS - LT OUTBOARD FLAP - TRACKING OF RECONFIGURED FLAP.

Part: STRUCTURE — CORRODED (HORIZ STAB) · airframe 40,937 hrs · 9,947 cycles

HORIZONTAL STAB CENTER BOX LT 31L BORE EXISTING BUSHING REMOVED FOUND BORE SIDEWALL AND BEARING SURFACE WITH CORROSION. REPAIR CARRIED-OUT AS PER FEDEX EA 1-5510-69213 - STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE REWORK/REPAIR.

Part: STRUCTURE — CORRODED (HORIZ STAB) · airframe 40,937 hrs · 9,947 cycles

HORIZONTAL STAB CENTER BOX RT 31R BORE EXISTING BUSHING REMOVED FOUND SIDEWALL AND BEARING SURFACE WITH CORROSION. REAM BORE TO 1.181 INCH MAX CORROSION STILL PRESENT ON SIDEWALL SURFACE. REPAIR CARRIED-OUT AS PER FEDEX EA 1-5510-69213 - STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE REWORK/REPAIR.

Part: HINGE — CORRODED (RT WING TE FLAP) · airframe 40,937 hrs · 9,947 cycles

RT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE TO FLAP LOWER SURFACE WITH HOLES FLAP SIDE QTY 4 EACH CORRODED. REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-69251 - WINGS - OUTBOARD FLAP HINGE FITTINGS OVERSIZE HOLES - REPAIR.

Part: HINGE — CORRODED (T/E FLAP) · airframe 40,937 hrs · 9,947 cycles

RT WING, OUTBOARD FLAP, OUTBOARD FWD HINGE WITH ACTUATOR HOLES CORRODED. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-69243 WINGS- TRAILING EDGE AND TRAILING EDGE DEVICES - LT AND RT OUTBOARD FLAP OUTBOARD HINGE BRACKET REPAIRS.

Part: HINGE — DAMAGED (ZONE 600) · airframe 40,937 hrs · 9,947 cycles

HFEC INDICATION FOUND IN INBOARD & OUTBOARD PIVOT HOLE BORE SURFACE ON OUTBOARD FLAP, OUTBOARD HINGE (FLAP SIDE) RT WING. REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-66421 - WINGS - RIGHT OUTBOARD FLAP - OUTBOARD HINGE AFT SUPPORT BORE CORRODED.

Part: HINGE — CORRODED (LT WING TE FLAP) · airframe 40,937 hrs · 9,947 cycles

LT WING, FOUND OUTBOARD FLAP, OUTBOARD HINGE FLAP SIDE AT FLAP LOWER SURFACE AFT HOLE QTY 2 EACH WITH CORROSION. LT WING OUTBOARD FLAP REMOVED AND REPLACED AS PER MM 27-50-30-4. FLAP RIGGING AND OPERATIONAL CHECK CARRIED-OUT AS PER MM 27-50-00-5, FOUND SATIS. COMPLIED WITH FEDEX EA 1-5750-66425 - WINGS - LT OUTBOARD FLAP - TRACKING OF RECONFIGURED FLAP.

Part: STRUCTURE — CORRODED (TE FLAPS) · airframe 40,937 hrs · 9,947 cycles

RT WING, FOUND OUTBD FLAP, INBOARD MOST HINGE LOCATION FLAP SIDE MOUNT HOLES QTY. 5 EACH LOCATION WITH CORROSION. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-69251 WINGS- OUTBOARD FLAP HINGE FIIRINGS OVERSIZE HOLES- REPAIR.

Part: STRUCTURE — CORRODED (TE FLAP) · airframe 40,937 hrs · 9,947 cycles

O/B FLAP O/B HINGE ATTACHMENT TO FLAP (LOWER FWD HOLE, 5 EACH) FOUND CORRODED. LT WING OUTBOARD FLAP REMOVED AND REPLACED AS PER MM 27-50-30-4. FLAP RIGGING AND OPERATIONAL CHECK CARRIED-OUT AS PER MM 27-50-00-5, FOUND SATIS. COMPLIED WITH FEDEX EA 1-5750-66425 - WINGS - LT OUTBOARD FLAP - TRACKING OF RECONFIGURED FLAP.

Part: HINGE — CORRODED (LT WING TE FLAP) · airframe 40,937 hrs · 9,947 cycles

LT WING, FOUND OUTBOARD FLAP, OUTBOARD HINGE FLAP SIDE AFT HOLES LOCATION QTY 2 EA WITH CORROSION. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-69244 WINGS- TRAILING EDGE & TRAILING EDGE DEVICES - LT OUTBD FLAP / OUTBD FLAP HINGE BRACKET - STRUT REPAIR.

Part: HINGE FITTING — CORRODED (ZONE 600) · airframe 40,937 hrs · 9,947 cycles

RT WING FOUND OUTBOARD FLAP, INBOARD MOST HINGE FITTING FLAP SIDE, AFT MOST HOLE LOCATION QTY. 1 EACH OUTBOARD MOST FACE WITH CORROSION. REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-69246 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RH OUTBOARD FLAP/INBOARD FLAP HINGE SUPPORT - REPAIR.

Part: HINGE — CORRODED (TE FLAP) · airframe 40,937 hrs · 9,947 cycles

LT WING, FOUND OUTBOARD FLAP, INBOARD HINGE FITTING FLAP SIDE TO FLAP MOUNTING HOLES LOCATION CORRODED. CORROSION ON LH WING, O/B FLAP I/B HINGE FITTING FLAP SIDE TO FLAP MOUNTING HOLES REMOVED AS PER SRM 51-21-01, VOL II. AND SRM 51-31-01, VOL II. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-69254 WING - LT OUTBOARD FLAP INBOARD AFT HINGE OVERSIZE HOLES - REPAIR.

Part: HINGE — CORRODED (TE FLAP) · airframe 40,937 hrs · 9,947 cycles

LT WING, FOUND OUTBOARD FLAP, INBOARD HINGE FITTING, FLAP SIDE TO FLAP MOUNTING HOLES LOCATION QTY 6 EACH CORRODED. CORROSION ON LH WING , O/B FLAP I/B HINGE FITTING, FLAP SIDE TO FLAP MOUNTING HOLES REMOVED AS PER SRM 51-21-01 VOL II & SRM 51-31-01 VOL II. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-69254 WINGS- LT OUTBOARD FLAP INBOARD AFT OVERSIZE HOLES- REPAIR.

Part: HINGE — CORRODED (LT WING TE FLAP) · airframe 40,937 hrs · 9,947 cycles

LT WING: O/B FLAP I/B HINGE ATTACHMENT TO FLAP LOWER AFT HOLE (2 EACH) FOUND CORRODED. LT WING OUTBOARD FLAP REMOVED AND REPLACED AS PER MM 27-50-30-4. FLAP RIGGING AND OPERATIONAL CHECK CARRIED-OUT AS PER MM 27-50-00-5, FOUND SATIS. COMPLIED WITH FEDEX EA 1-5750-66425 - WINGS - LT OUTBOARD FLAP - TRACKING OF RECONFIGURED FLAP.

Part: HINGE — CORRODED (LT WING TE FLAP) · airframe 40,937 hrs · 9,947 cycles

LT WING, FOUND OUTBOARD FLAP, OUTBOARD HINGE WING SIDE LINK ATTACHMENT HOLE LOCATION QTY 2 EACH CORRODED. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-69243 WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - LH & RH OUTBD FLAP OUTBD HINGE BRACKET REPAIRS.

Part: HINGE — CORRODED (LT WING TE FLAP) · airframe 40,937 hrs · 9,947 cycles

LT WING: OUTBOARD FLAP INBOARD HINGE ATTACHMENT TO FLAP LOWER FWD HOLE (4 EACH) FOUND CORRODED. LT WING OUTBOARD FLAP REMOVED AND REPLACED AS PER MM 27-50-30-4. FLAP RIGGING AND OPERATIONAL CHECK CARRIED-OUT AS PER MM 27-50-00-5, FOUND SATIS. COMPLIED WITH FEDEX EA 1-5750-66425 - WINGS - LT OUTBOARD FLAP - TRACKING OF RECONFIGURED FLAP.

Part: RIB — CRACKED (RT WING TE FLAP) · airframe 40,937 hrs · 9,947 cycles

RT WING, FOUND OUTBOARD FLAP, INBOARD STOP BOLT SUPPORT ISLAND WITH CRACK. REMOVED AND REPLACED AS PER 51-31-01 VOL. I.

Part: SPAR CAP — CORRODED (LT WING) · airframe 40,937 hrs · 9,947 cycles

LT WING, FOUND WING REAR SPAR UPPER CAP UPPER SURFACE WITH CORROSION FROM XORS 830 TO XORS 1090. OUTER LT WING/REAR SPAR TRAILING EDGE - LT REAR SPAR UPPER CAP REPAIRED FROM XORS 830 TO XORS 1090 AS PER FEDEX EA 1-5720-69229, SRM 57-20-00 FIG. 16 VOL. I AND FEDEX EA 1-5720-69230.

Part: SPAR — CORRODED (ZONE 500) · airframe 40,937 hrs · 9,947 cycles

LT WING FOUND REAR SPAR LOWER CAP WITH CORROSION AT XORS 1090.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 40,937 hrs · 9,947 cycles

HORZ STABILIZER CENTER BOX LT NR 1 BARREL NUT HOLE FOUND WITH CORROSION. REAM BORE UP TO 1.549 INCH CORROSION STILL PRESENT ON THE SIDE OF BEARING SURFACE. REPAIR CARRIED-OUT AS PER FEDEX EA 1-5510-69213 - STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE REWORK/REPAIR.

Part: STRUCTURE — CORRODED (ZONE 500) · airframe 40,937 hrs · 9,947 cycles

LT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE) PIVOT BORE HOLE FOUND CORRODED.

Part: STRUCTURE — CORRODED (ZONE 500) · airframe 40,937 hrs · 9,947 cycles

LT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE) UPPER ATTACHMENT FITTING TO WING REAR SPAR BORE HOLE (2 EACH) CORRODED. CORROSION ON LT WING OUTBOARD FLAP INBOARD HINGE (WINGSIDE) UPPER ATTACHMENT FITTING TO WING REAR SPAR BORE HOLES (2 EACH) REMOVED AND REPAIR CARRIED-OUT AS PER CMM 57-44-08, FIG. 401.

Part: FLAP TRACK — CHAFED (ZONE 500) · airframe 40,937 hrs · 9,947 cycles

LT WING OUTBOARD FLAP INBOARD TRACK (ON WING)FOUND WITH CHAFING MARKS. TRAILING EDGE & TRAILING EDGE DEVICES - LT OUTBOARD FLAP / INBOARD FLAP TRACK REPAIRED AS PER EA 1-5750-69241.

Part: STRUCTURE — CORRODED (ZONE 500) · airframe 40,937 hrs · 9,947 cycles

LT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE) ACTUATOR FITTING (2 EACH) BORE HOLE FOUND CORRODED. REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-69242 - WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET REPAIRS.

Part: STRUCTURE — CORRODED (ZONE 500) · airframe 40,937 hrs · 9,947 cycles

LT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE) ACTUATOR ATTACH POINT BORE HOLE (2 EACH) FOUND CORRODED. REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-69243 - WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - LH AND RH OUTBOARD FLAP OUTBOARD HINGE BRACKET REPAIRS.

Part: STRUCTURE — CORRODED (ZONE 500) · airframe 40,937 hrs · 9,947 cycles

LT WING INBOARD FLAP OUTBOARD HINGE (WING SIDE) PIVOT BORE HOLE FOUND WITH CORROSION. SURFACE CORROSION ON LT WING INBOARD FLAP OUTBOARD HINGE PIVOT BORE HOLE REMOVED AND REPAIR CARRIED OUT AS PER CMM 57-44-07, FIG. 401.

Part: HINGE — CORRODED (LT WING TE FLAP) · airframe 40,937 hrs · 9,947 cycles

LT WING: O/B FLAP O/B HINGE (WING SIDE) LWR ATTACHMENT TO WING REAR SPAR FOUND WITH HOLE (2 EACH) CORRODED. REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-69243 - WINGS - TRAILING EDGE & TRAILING EDGE DEVICES LT AND RT OUTBOARD FLAP OUTBOARD HINGE BRACKET REPAIRS.

Part: STRUCTURE — CORRODED (ZONE 500) · airframe 40,937 hrs · 9,947 cycles

LT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE) FITTING BORE HOLE FOUND CORRODED. CORROSION ON LH WING OUTBOARD FLAP INBOARD HINGE (WINGSIDE) FITTING PIVOT BORE HOLE REMOVED AND REPAIR CARRIED OUT AS PER CMM 57-44-08 FIG. 401.

Part: STRUCTURE — CORRODED (ZONE 500) · airframe 40,937 hrs · 9,947 cycles

LT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE) UPPER ATTACHMENT TO WING REAR SPAR HOLE (2 EACH) FOUND CORRODED. CORROSION ON LH WING, OUTBD FLAP, OUTBD HINGE (WINGSIDE) UPPER ATTACHMENT TO WING REAR SPAR HOLES (2 EACH) AREA REMOVED AS PER CMM 57-44-09 PAGE 403 AND FOUND WITHIN LIMIT AS PER DWG. NO. ARC0503.

Part: STRUCTURE — CORRODED (ZONE 500) · airframe 40,937 hrs · 9,947 cycles

LT WING OUTBOARD FLAP INBOARD HINGE ATTACHMENT TO WING REAR SPAR LOWER FITTING BORE HOLE (2 EACH) FOUND CORRODED. CORROSION ON LH WING OUTBOARD FLAP INBOARD HINGE ATTACHMENT TO WING REAR SPAR LOWER FITTING BORE HOLE ( 2 EACH )AREA REMOVED AND FOUND WITHIN LIMITS AS PER CMM 57-44-08 FIG. 401 AND DWG NO. ARC0502. REPAIR CARRIED OUT AS PER CMM 57-44-08 FIG. 401.

Part: STRUCTURE — CORRODED (ZONE 600) · airframe 40,937 hrs · 9,947 cycles

RT WING FOUND INBOARD FLAP, OUTBOARD HINGE WING SIDE WITH PIVOT HOLE WITH MINOR CORROSION. MINOR CORROSION ON RT WING, INBOARD FLAP, OUTBOARD HINGE WING SIDE, PIVOT HOLE REMOVED AND REPAIR CARRIED OUT AS PER CMM 57-44-07, FIG. 401.

Part: SKIN — CRACKED (ZONE 600) · airframe 40,937 hrs · 9,947 cycles

UPON REMOVAL OF RT NR 2 LEADING EDGE OUTBOARD MOST SEAL FOUND SLAT UPPER SKIN TRAILING EDGE AFT MOST HOLE CRACKED. RT WING NR 2 LEADING EDGE OUTBOARD SLAT UPPER SKIN TRAILING EDGE REMOVED AND REPLACED AS PER SRM 51-35-01 VOL. II AND DWG NRB6225.

Part: HINGE BRACKET — CORRODED (T/E FLAP) · airframe 40,937 hrs · 9,947 cycles

RIGHT WING FOUND OUTBOARD FLAP, INBOARD HINGE WING SIDE WITH ACTUATOR HOLE LOCATION INBOARD MOST WITH CORROSION. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-69242 WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - LT & RT OUTBOARD FLAP INBOARD HINGE BRACKET REPAIRS.

Part: STRUCTURE — CORRODED (ZONE 500) · airframe 40,937 hrs · 9,947 cycles

LT WING INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT HOLE (1 EACH) FOUND WITH CORROSION. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-69223 WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - LH INBD. FLAP HINGE BRACKET REPAIR.

Part: FITTING — CORRODED (ZONE 500) · airframe 40,937 hrs · 9,947 cycles

LEFT OUTBOARD FLAP VANE, INBOARD NR 1 VANE TRACK FITTING FWD MOUNT HOLE CORRODED. REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-69349 - WINGS - OUTBAORD FLAP VANE INBOARD SUPPORT CORROSION - REPAIR.

Part: STRUCTURE — CORRODED (ZONE 600) · airframe 40,937 hrs · 9,947 cycles

RT WING FOUND OUTBOARD FLAP, INBOARD HINGE WING SIDE WITH PIVOT HOLE LOCATION CORRODED. CORROSION ON RT WING, OUTBOARD FLAP, INBOARD HINGE WING SIDE, PIVOT BORE HOLE REMOVED AND REPAIR CARRIED OUT AS PER CMM 57-44-08, FIG.401.

Part: STRUCTURE — CORRODED (TE FLAP) · airframe 40,937 hrs · 9,947 cycles

RT WING FOUND OUTBOARD FLAP, OUTBOARD HINGE WING SIDE WITH PIVOT HOLE LOCATION WITH CORROSION. CORROSION ON RT WING, OUTBOARD FLAP, OUTBOARD HINGE WING SIDE, PIVOT HOLE REMOVED AND REPAIR CARRIED OUT AS PER CMM 57-44-09, FIG.401.

Part: HINGE — CORRODED (RT WING TE FLAP) · airframe 40,937 hrs · 9,947 cycles

RT WING, FOUND OUTBOARD FLAP, INBOARD HINGE WITH MOUNTING HOLES QTY 6 EACH WITH CORROSION. REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-69242 - WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET REPAIRS.

Part: RIB — CRACKED (LT WING TE FLAP) · airframe 40,937 hrs · 9,947 cycles

LT OUTBOARD FLAP ASSY LEADING EDGE, NOSE RIB SUPPORT ISLAND WITH CRACK. LT OUTBOARD FLAP ASSEMBLY LEADING EDGE, NOSE RIB SUPPORT ISLAND REMOVED AND REPLACED AS PER SRM 5-31-01 VOL. II.

Part: STRUCTURE — CORRODED (ZONE 500) · airframe 40,937 hrs · 9,947 cycles

LT WING INBOARD FLAP OUTBOARD HINGE OUTBOARD PIVOT HOLE (1 EACH) FLAP SIDE FOUND WITH CORROSION. REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-69223 - WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - LT INBD FLAP HINGE BRACKET REPAIR.

Part: FITTING — CORRODED (HORIZONTAL STAB) · airframe 40,937 hrs · 9,947 cycles

HORIZONTAL STABILIZER CENTER BOX LT SIDE BARREL NUT HOLE NR 26 FOUND FITTING WITH CORROSION (BOTTOM & BEARING SURFACE). HORIZONTAL STABILIZER CENTER BOX LT SIDE BARREL NUT HOLE NR 26L FITTING REMOVED AND REPLACED AS PER FEDEX EA 1-5510-69219 - STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE 26 LT FITTING FABRICATION.

Part: STANCHION — CORRODED (FUSELAGE) · airframe 40,937 hrs · 9,947 cycles

LOWER FORWARD CARGO AFT BULKHEAD STANCHION P/N A6A7094-17 AT STA X = -9.0 FOUND CORROSION (6 PLACES) ON FASTENERS HOLES.

Part: STRUCTURE — CORRODED (ZONE 500) · airframe 40,937 hrs · 9,947 cycles

LT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE) ACTUATOR FITTING HOLE (2 EACH) FOUND CORRODED. REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-69216 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP OUTBOARD HINGE BRACKET REPAIR.

Part: SEAT TRACK — CORRODED (BS 6-90) · airframe 40,937 hrs · 9,947 cycles

CABIN SEAT TRACK CORRODED AT STA 6-90 LT X = 75.25. SEAT TRACK REPAIRED AS PER SRM 53-70-00 FIG. 1 VOL. I.

Part: STANCHION — CORRODED (FUSELAGE) · airframe 40,937 hrs · 9,947 cycles

LOWER FORWARD CARGO AFT BULKHEAD STANCHION P/N A6A7094-9 AT STA X = 9.0 FOUND CORROSION (4 PLACES) ON FASTENERS HOLES.

Part: SKIN — DENTED (TE FLAP) · airframe 40,937 hrs · 9,947 cycles

LT INBOARD FLAP LOWER SKIN SURFACE LOWER SECTION FOUND WITH SEVERAL DENTS (BETWEEN 54 - 66 INCHES FROM INBOARD EDGE). LT INBOARD FLAP LOWER SKIN SURFACE LOWER SECTION DENT SKIN REPAIRED AS PER SRM 57-10-00 VOL. II.

Part: STRUCTURE — CORRODED (TE FLAP) · airframe 40,937 hrs · 9,947 cycles

LT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) FITTING HOLE (2 EACH) FOUND CORRODED. REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-69217 - WINGS - TRAILING EDGE & TRAILING EDGE DEVICES LH OUTBOARD FLAP INBOARD HINGE BRACKET REPAIR.

Part: STRUCTURE — CORRODED (TE FLAP) · airframe 40,937 hrs · 9,947 cycles

RT WING FOUND OUTBOARD FLAP, INBOARD MOST HINGE, OUTBOARD & INBOARD HOLE WITH CORROSION (FLAP SIDE PIVOT HOLE). REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-69218 - WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - RH OUTBOARD FLAP INBOARD HINGE BRACKET REPAIR.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 40,937 hrs · 9,947 cycles

LOWER FORWARD CARGO BILGE AREA LONGERON 52 FOUND WITH CORROSION BETWEEN STA Y = 6-70 TO 6-90. LOWER FORWARD CARGO BETWEEN STA Y=6-70 TO 6-90 LONGERON 52 REPAIRED AS PER SRM 53-10-00, FIG.1, VOL.I.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 40,937 hrs · 9,947 cycles

CABIN SEAT TRACK AT RT X = 47.5 STA 1321 - 1361 CORRODED. CABIN - STA 1270 TO STA 1390 RT X=47.5 SEAT TRACK REPAIRED AS PER SRM 53-70-00, VOL I, FIG 1.

Part: FITTING — CORRODED (ACTUATOR) · airframe 40,937 hrs · 9,947 cycles

LT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) ACTUATOR FITTING (2 EACH) FOUND CORRODED. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-69217 WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - LT OUTBD FLAP INBD HINGE BRACKET REPAIR.

Part: STRUCTURE — CORRODED (TE FLAP) · airframe 40,937 hrs · 9,947 cycles

RT WING FOUND INBOARD FLAP, OUTBOARD HINGE, INBOARD & OUTBOARD HOLE WITH CORROSION (FLAP SIDE PIVOT HOLE). CORROSION ON RT WING, INBOARD FLAP, OUTBOARD HINGE, INBOARD AND OUTBOARD HOLE REMOVED AND REPAIR CARRIED OUT AS PER EA 1-5750-69224.

Part: STRUCTURE — CORRODED (TE FLAP) · airframe 40,937 hrs · 9,947 cycles

LT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE) FITTING HOLE (2 EACH) FOUND CORRODED. REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-69216 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP OUTBOARD HINGE BRACKET REPAIR.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,937 hrs · 9,947 cycles

FORWARD TAIL CONE MOST AFT MAIN FRAME LT SIDE FOUND WITH CRACK. FWD TAIL CONE MOST AFT MAIN FRAME LH SIDE CRACK REPAIRED AS PER DWG. AKC7539 AND SRM 53-00-01, VOL.II.

Part: FITTING — CRACKED (ZONE 500) · airframe 40,937 hrs · 9,947 cycles

LT WING L/E SLAT TRACK NR 16 INBOARD FITTING FOUND CRACKED. LT WING LEADING EDGE SLAT TRACK NR 16 INBOARD FITTING REMOVED AND REPLACED AS PER SRM 51-33-01 VOL. II AND DWG ARB2850.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 40,937 hrs · 9,947 cycles

CABIN SEAT TRACK CRACKED AT STA 635 LBL 8.5 BETWEEN FLOOR PANELS 233FF AND 233EF. CABIN STA 635 TO STA 655 LBL 8.5 SEAT TRACK REPAIRED AS PER SRM 53-70-00, FIG.1, VOL.1.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 40,937 hrs · 9,947 cycles

CABIN SEAT TRACK CRACKED AT STA 755 LBL 47.5 BETWEEN FLOOR PANELS NR 241BF, 241CF AND 241JF. CABIN STA 645 TO STA 765 LBL 47.5 SEAT TRACK REPAIRED AS PER SRM 53-70- 00, VOL.I, FIG.1.

Part: SKIN — CORRODED (LT WING) · airframe 40,937 hrs · 9,947 cycles

LT WING UPPER SURFACE ABOVE WING TRAILING EDGE SPAR STA XORS 1090 FOUND BULGED. WINGS - OUTER WING/REAR SPAR TRAILING EDGE - LT REAR SPAR UPPER CAP REPAIRED AS PER FEDEX EA 1-5720-69230.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 40,937 hrs · 9,947 cycles

CABIN SEAT TRACK AT RT 47.5 STA 1199 - 1280 CRACKED AND CROWN AREA WORN. SEAT TRACK REPAIRED AS PER SRM 53-70-00 FIG. 1 VOL. I.

Part: FITTING — CRACKED (RIGHT WING) · airframe 40,937 hrs · 9,947 cycles

RIGHT WING FOUND L/E NR 16 TRACK INBOARD SUPPORTING FITTING CRACKED. RT WING LEADING EDGE NR 16 TRACK INBOARD SUPPORTING FITTING REMOVED AND REPLACED AS PER SRM 51-33-01 VOL. II AND DWG ARB2850.

Part: VALVE — LEAKING (A/C PACK) · airframe 39,951 hrs · 9,725 cycles

DECLARED INFLIGHT EMERGENCY, SMOKE IN COCKPIT. SOURCE OF SMOKE WAS BELIEVED TO BE AIR CONDITIONING SYSTEM. NOTICED A DIRTY SOCK ODOR DURING TAXI. IN FLIGHT, THE SMOKE KEPT INCREASING, RETURNED TO BASE. USED EMERGENCY ESCAPE SLIDE TO EGRESS ON RUNWAY. FIRE DEPARTMENT ACCIDENTLY DEPLOYED THE OTHER ESCAPE SLIDE. FOUND NR 1 PACK ANTI ICE VALVE LEAKING INSTALLED NR 1 PACK ANTI ICE VALVE PER MD11 M.M. 21-53-27-2 OK FOR SERVICE PERFORMED PER MD11 MM 21-53-00-7 PARA 2 CLEANING AIR CONDITIONING PACK AND DISTRIBUTION APPROX 5 TIMES NO SMOKE AND NO OIL ODOR AT THIS TIME

Part: SUPPORT FITTING — CORRODED (T/E FLAP) · airframe 38,129 hrs · 9,295 cycles

RT WING INBOARD FLAP - OUTBOARD FWD HINGE SUPPORT FITTING LWR INBOARD BOLT AT ATTACH POINT IS EMITTING RUST BETWEEN MATTING SURFACES.

Part: SUPPORT FITTING — CORRODED (T/E FLAP) · airframe 38,129 hrs · 9,295 cycles

RT WING INBOARD FLAP - OUTBOARD FWD HINGE SUPPORT FITTING LWR OUTBOARD BOLT AT ATTACH POINT IS EMITTING RUST AT MATTING SURFACE.

Part: BOLT — LOOSE (LANDING GEAR) · airframe 36,639 hrs · 8,961 cycles

CTR L/G TRUNNION FITTING LT & RT AFT BOLT LOOSE. CTR L/G TRUNNION FITTING LT & RT AFT BOLT REMOVED. GENERAL VISUAL INSP CARRIED OUT AND FOUND SATISFACTORY. CTR L/G TRUNNION FITTING LT & RT AFT BOLT INSTALLED AND NUT REMOVED AND REPLACED AS PER MM 32-15-01-4.

Part: SKIN — CORRODED (RT WINGLET) · airframe 36,639 hrs · 8,961 cycles

RT WING UPPER WINGLET UPPER O/B SURFACE DENT MARK AND CORROSION. RT WING UPPER WINGLET UPPER O/B DENT MARK MEASURED WITHIN LIMIT PER SRM 57-00-01 VOL 1. CORROSION SKIN REPAIRED AS PER SRM 57-00-01 FIG 7 VOL 1. REWORK AREA NDT INSP NO CRACK AS PER NDT SPM PART 06-10-01-001.

Part: ENGINE — MAKING METAL (NR 2) · airframe 36,084 hrs · 8,830 cycles

NR 2 ENG N1 FAILED TO ATTAIN T/O THRUST. MAINTENANCE FOUND METAL IN THE TAILPIPE.

Part: COMPUTER — FAILED (BLEED AIR SYS)

ON CLIMBOUT LEVEL 3 EMERGENCY ALERT AIR MANIFOLD NR 2 FAIL. REMOVED AND REPLACED MFC & ALL SENSORS IN ZONE 15.

Part: MANIFOLD — FAILED (PNEUMATIC SYS)

AIR MANF NR 2 FAIL ALERT NR 2 PACK OFF. REMOVED AND REPLACED MFC & RTS PER MM 36-23-01-4. CLOSED NR 2 COWLING & PLATFORM PER 71-00-00.

Part: BEAM — CRACKED (PAX DOOR) · airframe 32,355 hrs · 7,987 cycles

MAIN DECK - L3 DOOR FOUND SUPPORT BEAM CRACK ON THE AFT END DOOR STOP NR 2. *S/D* REMOVED AND REPLACED PER EA 1-5210-53268.

Part: FUEL TANK — CORRODED (CENTER WING) · airframe 32,355 hrs · 7,987 cycles

MAIN DECK - OVERWING FUEL TANK AREA LEFT SIDE UNDER FLOOR SPACE FOUND 3 SECTIONS OF CORROSION AT BS 1297, 1321, & 1346 X=103.5 LT. *S/D* REMOVED AND REPLACED PER EA 1-5750-53269.

Part: SEAT TRACK — CRACKED (CABIN) · airframe 32,355 hrs · 7,967 cycles

MAIN DECK - SEAT TRACK FOUND CRACKED FROM BS 789 TO BS 801, X=8.5 LT 12 INCHES LONG. *S/D* REMOVED AND REPLACED PER SRM 53-70-00 FIG 1 VOL 1.

Part: BRACKET — BROKEN (RT MLG) · airframe 31,868 hrs · 7,887 cycles

AFT T/O, RT GEAR UNSAFE LIGHT ILLUM. FOUND BRACKET BROKEN. ALSO FOUND 2 GUIDES BROKEN. CHECKED NORMAL PER 32-61-15-5.

Part: FITTING — CRACKED (VERT STAB)

DURING EDDY CURRENT INSP ON RT BANJO NR 4 FOUND INNER FWD FLANGE WITH .5 INCH CRACK AT RADIUS AREA FWD CTR FASTENER HOLE DIA 0.371 IN AND LWR FWD FASTENER HOLE DIA 0.325 IN WITH SHORT EDGE MARGIN AND CRACK=FREE COND-585., FOUND FOR UPPER AND LWR FASTENER HOLE WITH CRACKS AND ALL 3 FWD HOLES LARGER THAN 0.275 DIA. -600. *S/D* REPAIRED AS PER EA 1-5530-47423.

Part: SEAT TRACK — CRACKED (BS 483)

FWD CABIN FLOOR TRACK ASSY FOUND CRACKED. FWD CABIN FLOOR TRACK ASSY FOUND CRACKED. FWD CABIN FLOOR TRACK ASSY FOUND CRACKED. *S/D* REPAIR CARRIED OUT PER SRM 53-70-00.

Part: SEAT TRACK — CRACKED (BS 635)

MAIN DECK SEAT TRACK CRACKED AT BS Y=635, INTERSECTION OF X=27.5 APPROX 3 IN & X=47.5 APPROX 3 IN. *S/D* MAIN DECK SEAT TRACK BS Y=635, X=27.5 & X=47.5. REPAIR CARRIED OUT PER SRM 53-70-00 VOL 1.

Part: TUBE ASSY — CRACKED (NR 3 ENGINE)

97-0147 CDG - 30 MINUTES INTO FLT, NR 3 HYD RAPIDLY LEAKED ALL FLUID. FOUND HYD LEAK FROM NR 3 ENG CASE DRAIN RETURN LINE CRACKED ON LEFT ENGINE DRIVEN PUMP. CHECKED BOTH CASE DRAIN FILTERS AND FOUND BOTH CONTAMINATED, R/R FILTERS. ALSO, R/R NR 3 RT EDP, AND CAPPED OFF CRACKED LINE TO LEFT EDP LEFT PUMP IS ON A/C LINE IS IN STOCK MEM.

Part: HYDRAULIC LINE — BROKEN (LT ENGINE)

NOTICED STEADY LEAK IN HYDRAULIC SYSTEM NR 3. SHUTOFF SYSTEM NR 3 PUMPS, QUANTITY CONTINUED TO GO DOWN TO 0.0 GALLONS. HYDRAULIC NR 3 FAIL ALERT ILLUMINATED. COMPLIED WITH CHECKLIST, UNEVENTFUL LANDING AND ROLLOUT. FOUND FLUID LEAKING FROM NR 3 LEFT HAND ENGINE DRIVEN HYDRAULIC PUMP CASE RETURN LINE. REMOVED AND REPLACED THE LINE. ALSO, REPLACED HYDRAULIC FILTERS. RAN ENGINE AND OPERATIONAL CHECK GOOD.

Part: GEAR DOOR — CRACKED (CTR MLG)

SNRM N00842 LT CENTER LANDING GEAR FWD DOOR IS CRACKED AT FWD RADIUS AT CORNER. SUBMITTER STATES, THIS IS THE 2ND TIME CRACK FAILURE OF THIS PART. ODR SENT 1/12/96 CONTROL NR 96FDEA0053.

Part: SWITCH — OUT OF ADJUST (REFUELING PANEL)

AFTER T/O, RECEIVED A TAIL FUEL FORWARD FOLLOWED SHORTLY BY A CROSSFEED DISAGREE. CYCLED FSC AND TRIED TO MANAGE FUEL IN MANUAL, COULD NOT TRANSFER FUEL INTO THE MAINS. IT APPEARS IF FUEL WAS IN FACT BEING TRANSFERRED EVEN THOUGH THERE WAS NO INDICATION ON THE SYNOPTIC PAGE. ALSO, FUEL OFF SCHEDULE ALERT. ON TAXI IN, FOUND REFUELING DISPLAYED ON SYNOPTIC. FOUND POWER APPLIED TO REFUELING PANEL, SWITCH S1-108 NOT DEPRESSED WITH REFUELING DOOR CLOSED. ADJUSTED STRIKER WITH SHIMS FOR SAME SWITCH ALL AT REFUELING PANEL, OPS NORMAL.

Part: HYD LINE — FAILED (NR 3 HYD SYS)

EN ROUTE AT 12.40Z NR 3 HYD SYS LOSS/FAILURE OCCURED ALL FLUID LOST. ALL ABNORMAL CHECKLIST AND PROCEDURES COMPLETED. REPLACED PRESS LINE THAT GOES FROM THE ENG DRIVEN PUMP TO THE FILTER MODULE. THIS WAS DONE ON EA 1-2910-23270. FINAL FIX WAS DONE IN EWR 6-13-96 WHERE THE HOSE WAS REPLACED.

Part: ENGINE — FAILED (NR 1)

DURING CLIMB OUT, NR 1 ENGINE COMPRESSOR STALLS. THROTTLE WAS RETARDED, ENGINE CONTINUED TO STALL, FLIGHT CREW SHUT DOWN NR 1 ENGINE. THE AIRCRAFT RETURNED TO MEMPHIS. POWER PLANT LINE FOUND METAL IN THE TAIL PIPE. C/A FOUND METAL IN TAILPIPE. BOPED HPT CONFIRMED NR 1 ENGINE CHANGE DUE. REMOVED AND REPLACED NR 1 ENGINE PER W/C 71T0101 AND W/C 71T0701. ENGINE RUN AND LEAK CHK GOOD. PART 7100191 OFF 702757 POS 01 RSN 02.

Part: STRINGER — CRACKED (FS 545)

FORWARD END OF STRINGER 35L CRACKED FROM RIVET HOLE TO FWD END LENGTH. APPROXIMATELY .1250 INCH FS 545 CONFIRMED BY HFEC. FABRICATED STRINGER 35L PER SAMPLE AND INSTALLED STRINGER PER SRM 51-00-01.

Part: STRINGER — CRACKED (FS 545)

FOUND STRINGER 34L SEVERED FWD OF PREVIOUS SKIN CRACK STATION FS 545. FABRICATED STRINGER 34L PER SAMPLE AND INSTALLED PER SRM 51-00-01.

Part: DOOR — CRACKED (LT MLG DOOR)

LT MLG DOOR HAS 2 INCH CRACK AT UPPER MID HINGE AREA, LWR SKIN.

Part: DOOR — CRACKED (CTR GEAR DOOR)

CENTERLINE LANDING GEAR DOOR, LT FWD DOOR IS CRACKED AT LOWER FWD CORNER AT RADIUS. REMOVED LOWER CORNER SECTION LOCATED NEW FRAME, INSTALLED NEW FRAME PER SRM 51-00-01.

Part: FRAME — CRACKED (CTR GEAR DOOR)

CENTERLINE LANDING GEAR DOOR, RT FWD DOOR IS CRACKED AT LOWER FWD CORNER AT RADIUS. REMOVED CRACKED FRAME AND INSTALLED NEW FRAME PER SRM 51-00-01.