N991FD

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 86,361 hrs · 44,212 cycles

1L DOOR JAMMED AND WOULD NOT OPEN FROM OUTSIDE. MX CALLED. RELEASED FOR SERVICE PER MEL : 52-11-01-A CATEGORY : B EXPIRATION : 24NOV23 "MEL 52-11-01-A: __L-1 DOOR___ (IDENTIFY L1 OR R1 DOOR OR SLIDE) - __INOP_______ (IDENTIFY INOP OR MISSING)." L-1 DOOR FUNCTIONS NORMALLY FROM THE INSIDE. PERFORMED INSPECTION OF L1 DOOR ESCAPE SLIDE & MECHANISMS WITH NO DEFECTS NOTED IN REF TO B757 AMM 25-66-01-6. REMOVED BODY HINGE TORQUE TUBE COVER PLATE & PERFORMED INSPECTION OF L1 DOOR MECHANISMS WITH NO DEFECTS NOTED IN REF TO B757 AMM 52-11-01-6 & PERFORMED L1 DOOR OPS CHECK IN REF TO B757 AMM 52-11-00-2 & ALL CHECKS WERE NORMAL FROM OUTSIDE AND INSIDE. MULTIPLE OPS CHECKS WERE PERFORMED FROM BOTH INTERNAL AND EXTERNAL POSITIONS AND UNABLE TO DUPLICATE ANY ISSUES. THIS CLEARS MEL, CTRL # 7379611.

Part: POWERPACK — FAILED (MLG) · airframe 86,317 hrs · 44,189 cycles

MDIS 991 32-30 0510 07NOV23 OAK FACT U REF. WRI 32-30/0482 E.O. F-3230-E0376643 REV NO. POS. P1, WHILE ACCOMPLISHING WORK CARD THE POWER PACK FOR THE ALTERNATE EXTENSION SYSTEM DOES NOT OPERATE AT ALL. REASON CODE : PREMATURE REMOVAL/INSTALLATION OFF MPN: S273N401-6 CPN: 3215931 POS: ONL ON MPN: 1FA13050-5 SRL: 1970E6 TAG NBR: 18E721 FACT 07NOV23 23:59 OAK U AMM: 32-35-10-4 AMM: 32-35-00-5 REMOVED AND REPLACED ALTERNATE EXT. SYSTEM POWER PACK, OPS AND LEAK CHECK OK REF. B757 MM 32-35-10-4 AND MM 32-35-00-5.

Part: BEAM — CRACKED (ZONE 200) · airframe 86,193 hrs · 44,083 cycles

MAIN CARGO DOOR FWD BLOWOUT DOOR BOTH HINGES CRACKED. DOOR - CARGO DOOR / HYD SYS - MAIN CARGO DOOR LOWER BEAM DAMAGE AT STA 500 AND 520, DOUBLER REPAIR ACCOMPLISHED STEPS 1-21 PER EA F-5230-T0375382 PT1. MAJOR REPAIR

Part: SKIN — CRACKED (ZONE 200) · airframe 86,193 hrs · 44,083 cycles

WHILE PERFORMING LFEC INSPECTION IAW PT6 NTM 53-00-06 MULTIPLE CRACK INDICATIONS WERE NOTED AT THE UPPER L1 DOOR BEAR STRAP REPAIR AT THE UPPER FORWARD CORNER. FUSELAGE - PLATES AND SKIN - L1 DOOR CUTOUT, UPPER FWD CORNER, REPAIR REPLACEMENT. ACCOMPLISHED STEPS 1-28 PER EA F-5330-T0375235 PT1. MAJOR REPAIR

Part: FRAME — UNKNOWN (ZONE 100) · airframe 86,193 hrs · 44,083 cycles

AFT CARGO AT STA 1300 HAS A EXISTING FRAME REPAIR BETWEEN S-25R AND S-27R FUSELAGE - MAINFRAME - EXISTING FRAME REPAIR FOUND AT BS 1300 BETWEEN S-25R AND S- 27R IN AFT CARGO COMPARTMENT. ACCOMPLISHED EA F-5310-T0375226 STEPS 1, A-G AND 2 WITH NO DEVIATIONS. MAJOR REPAIR

Part: STRINGER — CORRODED (ZONE 100) · airframe 86,193 hrs · 44,083 cycles

AFT CARGO LOWER BILGE AREA BETWEEN STA. 1400-1420 S-29 STRINGER CORRODED. REMOVED & REPLACED STRINGER AT STA 1400-1420 S-29L IAW SRM 51-40-02. FABRICATED STRINGER ON VTMAE TRAVELER T23/1692068 IAW SRM 53-00-03-2R-4. MAJOR REPAIR

Part: FRAME — CRACKED (ZONE 100) · airframe 86,193 hrs · 44,083 cycles

DURING NDT HFEC REVEALED CRACK INDICATION BETWEEN THE PLUGGED LINER HOLE FASTENER AND FITTING FASTENER AT STA 1640 RH. STR 14R & 15R. TITLE: FUSELAGE- MAINFRAME-STA 1640 FRAME, S-15R, SPLICE REPAIR BETWEEN STRINGER I-9F AND S-20R- EO F-5310-E0367020 CRACK INDICATIONS REPAIR- PARTIAL FRAME REPLACEMENT. ACCOMPLISHED STEPS 1-14 WITH NO DEVIATION PER EA # F-5310-T0375101. MAJOR REPAIR

Part: STRINGER — CORRODED (AONE 10) · corrosion level 2 · airframe 86,193 hrs · 44,083 cycles

AFT CARGO LOWER BILGE AREA STRINGER CORRODED BETWEEN STA 1440 AND 1460 LH REMOVED AFT CARGO LOWER STRINGER STA 1400-1460 L-28 IAW SRM 53-00-03-2R. REPAIRED AFT CARGO LOWER STRINGER BETWEEN STA 1400-1460 LH IAW SRM 53-00-03-2R. MAJOR REPAIR

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 86,193 hrs · 44,083 cycles

DURING OKAY TO CLOSE PANEL 222MAF FOUND TWO PUNCTURES AND AN AREA OF DELAMINATION. FABRICATED FLOOR PANEL 222MAF ON VT MAE TRAVELER # T23/1692509 IAW DWG SRZ-25-005 REVISION R. "MAJOR REPAIR"

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 86,193 hrs · 44,083 cycles

MAIN CABIN FLOOR PANEL 231MAF DAMAGED AND DELAMINATED. FABRICATED ZONE 230 FLOORBOARD 231 MAF ON VTMAE TRAVELER # T23/1691345 IAW DWG BRZ- 25-005 REV R. REMOVED AND REINSTALLED MDC FLOOR PANEL 231MAF IAW AMM 25-55-04-4. MAJOR REPAIR

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 86,193 hrs · 44,083 cycles

MAIN CABIN FLOOR PANEL 231MBF DAMAGED AND DELAMINATED. FABRICATED ZONE 230 FLOORBOARD 231MBF ON VTMAE TRAVELER # T23/1691344 IAW DWG SRZ-25-005 REV R. REMOVED AND REINSTALLED MDC FLOOR PANEL 231MBF IAW AMM 25-55-04-4. MAJOR REPAIR.

Part: NONE — NONE (ZONE 200) · airframe 84,967 hrs · 43,208 cycles

R1 DOOR CUTOUT HINGE BOX WE INB SIDE IS DENTED REMOVED FABRICATED AND REPLACED WEB AT R1 HINGE BOX IAW DWG 141N8415 REVJ

Part: SKIN — CRACKED (ZONE 500) · airframe 84,967 hrs · 43,208 cycles

#2 SLAT COVE SKIN CRACKED AT O/B MAIN TRACK REMOVED #2 SLAT COVE SKIN, FABRICATED NEW SKIN AND REINSTALLED NEW SKIN PER BAC DWGS 114N4076 AND 114N4003

Part: NONE — NONE (N/A) · airframe 84,967 hrs · 43,208 cycles

LMLG W/W SUB STRUCTURE IS CRACKED AT THE FASTENER HOLE, APPROX STA 1147 LBL 70 WL 200 REMOVED, FABRICATED, LOCATED AND DRILLED NEW SUPPORT ANGLE IAW B757-200 DWG 149N7222 REV AC, INSTALLED IAW B757-200 DWG 149N7222 REV H

Part: HINGE — CRACKED (L1 DOOR FRAME) · airframe 84,967 hrs · 43,208 cycles

L1 DOOR CUTOUT, HINGE BOX,INBOARD WEB CRACKED REMOVED AND REPLACED WEB WITH NEW WEB IAW BOEING DWG 141N8315 REV M AND FEDEX EA # F-5310-T0364264 : FUSELAGE - MAINFRAME - L1 DOOR CUTOUT HINGE BOX, INBD WEB, ALTERNATE FASTENERS.

Part: SKIN — CRACKED (NR 8 SLAT) · airframe 84,967 hrs · 43,208 cycles

#8 SLAT COVE SKIN IS CRACKED AT I/B MAIN TRACK. REMOVED AND REPLACED COVE SKIN PER DWG # 114N4004 REV F

Part: BRACKET — CRACKED (NR 2 NACELLE) · airframe 84,967 hrs · 43,208 cycles

#2 ENGINE PYLON O/B SIDE ,FWD LOWER SIDE OF HYDRAULIC BAY HAS CRACKED BRACKET REMOVED AND REPLACED BRACKET PER DWG 313N3052 AND B757 SRM 51-40-02-0G.

Part: SKIN — CRACKED (LT WING LE) · airframe 84,967 hrs · 43,208 cycles

LEFT WING FIXED L/E CRACKED AT #3 SLAT INBD TRACK. REPAIRED ALL NOTED AREAS ON L/W FIXED LE BEHIND #3 SLAT IAW B757 SRM 57-41-01-2R FIG 201 SHEET 8 AND SRM 51-70-07-OG AND FIG 10.

Part: SKIN — CRACKED (RT WING LE) · airframe 84,967 hrs · 43,208 cycles

RIGHT WING FIXED L/E CRACKED AT #8 SLAT APROX 2 FT FROM OTBD END REPAIRED RIGHT WING FIXED L/E AT #8 SLAT 2FT FROM O/B END IAW B757 SRM 57-41-01, 57-41-01- 2R FIG 201 SHEET 8 AND 51-70-07-OG.

Part: WIRE — BROKEN (OUTFLOW VALVE) · airframe 84,756 hrs · 43,054 cycles

ENROUTE AT FL340 NOTICED EARS POPPING AND CABIN DIFFERENTIAL NEAR 6 WITH CABIN ALTITUDE AT 9000. 10 MINUTES LATER RECEIVED CABIN ALT HIGH EICAS. DONNED O2 MASKS, RAN QRH AND DESCENDED TO 10000 INITIALLY. EICAS REMAINED. DESCENDED TO 9000 AND EICAS WENT OUT. ONCE AT 9000, CABIN PRESSURIZED TO ~7000 . AT NO POINT DID CABIN ALTITUDE EXCEED 10,000. FOUND FLOW CONTROL VALVE FAULTED LAST FLIGHT. REMOVED AND PARTIALLY INSTALLED FLOW CONTROL VALVE REF AMM 21- 51-01-2. FINISHED INSTALL OF L/H FLOW CONTROL VALVE REF AMM 21-51-01-2 FLO CONTROL FAULT LIGHT REMAINS ON BOX DURING RTS. FOUND BROKEN WIRE TO CANNON PLUG D4128 ON L/H FLOW CONTROL VALVE .RETERMINATED PINS AT CONNECTOR D4128P AND REASSEMBLED IAW B757 SWPM 20-61-00 AND WDM 21-51-12. NEEDS OPS CHECK.COMPLETED OPS CHECK OF L/H FLOW CONTROL VALVE OPS REMOVED AND REPLACED LH PRIMARY AND SECONDARY HEAT EXCHANGERS AND RAM AIR DUCT TO COMPLY WITH TSI 21-50/8611 REF 757 AMM 21-51-02-4.

Part: COLLAR — CRACKED (L1 DOOR) · airframe 83,641 hrs · 42,351 cycles

AFTER BLOCK IN DURING ENTRY DOOR OPENING, FOUND DOOR HOLD OPEN LOCK COLLAR CRACKED. REMOVED AND REPLACED L1 DOOR HOLD OPEN LOCK COLLAR REF AMM 52-11-08-8-0.

Part: COLLAR — CRACKED (L1 DOOR) · airframe 83,641 hrs · 42,351 cycles

AFTER BLOCK IN DURING ENTRY DOOR OPENING, FOUND DOOR HOLD OPEN LOCK COLLAR CRACKED. REMOVED AND REPLACED L1 DOOR HOLD OPEN LOCK COLLAR REF AMM 52-11-08-8-0.

Part: UNKNOWN — MALFUNCTIONED (ENTRY DOOR) · airframe 83,479 hrs · 42,242 cycles

REF. WRI 52-10/7612 RH SIDE CREW ENTRY DOOR SLIDE ARMED LIGHT INOP. GRIT BAR WILL NOT ENGAGE. FACT 05JAN20 02:24 IAD TROUBLESHOT GIRT BAR ENGAGEMENT LIGHT REF B7575 FIM CHAP 25-66-00 FAULT TREE 802 FIGURE 103. GIRT BAR ENGAGEMENT LIGHT OPERATES NORMALLY. CHECKED GIRT BAR PROXIMITY SWITCHES REF B757 AMM CHAP 25-66-11-2. OP CHECK NORMAL.

Part: PROXIMITY SWITCH — OUT OF ADJUST (R1 DOOR) · airframe 83,247 hrs · 42,090 cycles

DURING MX WALKAROUND FOUND R1 DOOR SLIDE LIGHT NOT ILLUMINATED WHILE DOOR WAS ARMED. TROUBLESHOT PER FIM AND WDM 25-66-11, RANG OUT WIRING AND LIGHT ASSY CKS NORMAL. FOUND FWD PROX SWITCH OUT OF ADJUSTMENT AND LOOSE. ADJUSTED AND RESECURED PER 25-66-11-2-0 OPS CKS NORMAL OK FOR SERVICE.

Part: GIRT BAR — DISCONNECTED (EVAC SLIDE) · airframe 83,247 hrs · 42,090 cycles

MDIS 991 25-60 7348 21SEP19 MEM FACT U WHILE PERFORMING POST FLIGHT MX WALKAROUND FOUND R1 DOOR AFT PORTION OF THE GIRT BAR NOT CONNECTED TO DOOR SLIDE AND THE GIRT BAR SLIDE WOULDNT SLIDE INTO THE FLOOR FITTING. FACT 21SEP19 06:24 MEM U REINSTALLED GIRT BAR BACK TO SLIDE AND GIRT BAR SLIDE NOW ENGAGES IN FLOOR FITTING. ARMING OPERATIONAL CHECKS GOOD REF AMM 25-66-10-2. R1 DOOR SLIDE LIGHT INOP STILL REMAINS ON MEL. A/C OK FOR SERVICE.

Part: SKIN — DENTED (RT WING SLAT) · airframe 83,240 hrs · 42,084 cycles

R/H WING L/E SLAT #10 UPPER WEDGE SKIN HAS A DENT AROUND WS 763. ACCOMPLISHED REPAIR ON R/H WING L/E SLAT #10 UPPER WEDGE SKIN IAW B757 SRM 57-43-02 02- 2R AND IAW SRM 51-70-10-2R REP. 4. AND IAW EA T F-5750-T0348977 P1.

Part: STRAP — CRACKED (BS 1520) · airframe 83,240 hrs · 42,084 cycles

REWORK OF NR N00423 DUE TO INCORRECT SRM REFERENCE USED. MAIN CABIN FLOORBEAM LOWER STABILIZER STRAP IS BROKEN AT BS 1520 RBL 24.75". INSPECTED REPAIR OF THE STABILIZER STRAP REPAIR ON STA 1500 TO 1540 AND STRAP SPLICE ON STA 1500 RBL 24.75 FOR CORRECT REPAIR PROCEDURE AND FOUND THE REPAIR WAS ACCOMPLISHED IAW SRM 53-00-51-2R, FIG 201, DETAIL V, REPAIR 12.

Part: STRAP — CRACKED (BS 1260) · airframe 83,240 hrs · 42,084 cycles

MAIN CABIN FLOOR BEAM LOWER STABILIZER STRAP IS CRACKED AT BS 1260 LBL 24.75. REMOVED CRACKED STABILIZER STRAP AREA AT BS 1260, LBL 24.75,FABRICATED AND INSTALLED REPAIR STRAP AND FILLER IAW B 757,SRM 53-00-51-2R FIG 201,REPAIR 12.

Part: SEAT TRACK — CORRODED (BS 900-1030) · corrosion level 2 · airframe 83,240 hrs · 42,084 cycles

MAIN DECK FLOOR SEAT TRACK LBL 58.22(#1 FROM LEFT)HAS EVIDENCE OF CORROSION AT APPROX BS 1022-1030 FOUND SEAT TRACK,CORROSION DAMAGE @ SECTION STA 900 - STA 1030 LBL 58.22 TO HAVE NO ALLOWABLE DAMAGE DATA IAW B 757 SRM 53-00-52-1A,FIG 101 DETAIL VII,REMOVED FABRICATED AND INSTALLED NEW SECTION OF SEAT TRACK IAW B DWG 657N3332 REV - 657N3321 REV - , B 757 SRM 51-40-05-OG,51-10-02-OG AND 51-40-02-OG.

Part: SKIN — CRACKED (RT WING TE FLAP) · airframe 83,240 hrs · 42,084 cycles

R/H I/B FLAP, I/B UPPER SKIN INTERNAL HONEYCOMB PUNCTURED AS MARKED ACCOMPLISHED REPAIR ON R/H I/B FLAP, I/B UPPER SKIN INTERNAL HONEYCOMB IAW B757 SRM 57-53-01-2R AND IAW B757 SRM 51-70-10-2R AND IAW WING-FLIGHT SURFACES-RH INBOARD MAIN FLAP UPPER SKIN, INNER SURFACE REPAIR-RSC TRACKING FEDEX EA T F-5750-T0349007 P1

Part: FLOORBEAM — CRACKED (BS 580) · airframe 83,240 hrs · 42,084 cycles

FWD CARGO COMPARTMENT, MAIN FRAME-STA 580 FLOOR BEAM SPLICE SEGMENT UPPER AFT CRACK COMPLIED WITH EA F- 5310- T0348795 P1.

Part: FRAME — PUNCTURED (BS 231) · airframe 83,240 hrs · 42,084 cycles

FWD EQUIPMENT BAY, MAIN FRAME AT BS.231 HAS A PUNCTURE UPPER SUFACE BL.0 JUST ABOVE THE ACCESS DOOR #113AL LATCH FUS. CUTOUT RECEPTABLE. CUT OUT AND REMOVED DAMAGE AREA FRAME BS 231 BL O IAW B757 53-00-07-2R FIG 202 REP 7 DET I. FORMED, LOCATED, DRILLED AND INSTALLED ANGLE REPAIR FILLER AND SHIELD IAW SRM 53-00-07-2R- REP 7 DETAIL I.

Part: BEARING — WORN (L1 DOOR) · airframe 82,742 hrs · 41,735 cycles

FOUND UPPER LATCH CRANK ROLLERS FOR L1 DOOR ARE CHIPPED AND WORN. REMOVED AND REPLACED L1 DOOR FOUR CAM LATCH ROLLERS REF B57 AMM 52-11-00-05.INSTALLED COTTER PINS AND CHECKED ADJUSTMENT OF THE 4 L1 DOOR LATCH ROLLERS REF AMM 52-11-00-5. ALL 4 LATCH ROLLERS FOUND TO BE WITHIN LIMITS. OK FOR SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (TE FLAPS) · airframe 81,239 hrs · 40,673 cycles

DURING APPROACH, GOING FROM FLAPS 20 TO 25. RECEIVED TE FLAP DISAGREE. WENT AROUND. FOLLOWED QRH. LANDED FLAPS 20 WITH NO EVENT. ALSO GOT SPOILERS ALERT WITH THE SPOILERS DOWN. CHECKED SPOILER MODULE FOR EXISTING FAULTS, NON FOUND RESET ALL MODULES FOR PRECAUTION. PERFORMED OPS CHECK AS PER MM 27-61-00. CKS OK CHECKED FSEU FOR CURRENT FAULTS AS PER MM 27-51. FSEU MX PRACTICES. NO CURRENT FAULTS FOUND. CHECKED STORED FAULTS. FSEU 1 SHOWS FLA FAULT LAST FLIGHT. NR 2 AND 3 SHOW OK. CYCLED FLAPS AND PERFORMED OPS CL AS ER MM 27-51-00. CKS OK. SUSPECT SPURIOUS PROBLEM WHICH NO LONGER PRESENT. NOTE: ALTHOUGH NOT REPORTED IN CREW WRITE UP DISCOVERED AN EMERGENCY WAS REPORTED AT GO AROUND. NO PRIOR HISTORY FOUND 30 DAYS. NOTE 2 AT BLOCK OUT, CREW REPORTED HE HAD BEEN ON APPROACH 'HOT' BUT NOT ENOUGH SPEED TO WARRENT AN OVERSPEED ALERT.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 802 hrs · 39,951 cycles

LEFT WING INBD FLAP, LOWER SURFACE HAS A DENT WS 204. OUND TO BE OUT OF LIMITS IAW SRM 57-53-01-1A FIG 101. REPAIRED IAW SRM 51-70-10-2R PARA 20. PRIMED & TOP COATED IAW SRM 51-70-10-2R PARA 20 & AMM 51-21-10-7.

Part: PLACARD — OUT OF ADJUST (R1 DOOR) · airframe 801 hrs · 39,902 cycles

DISARM & ARM PLACARD ON R1 DOOR FELL INSIDE PLASTIC MOLDING. PLACARD IS ACTUALLY THE GREEN & RED PLATE BEHIND THE ARM & DISARM LEVER. REINSTALLED PLATE ON R1 UPPER DOOR LINING.

Part: SEAL — BROKEN (TE FLAP) · airframe 799 hrs · 39,767 cycles

ON CONFIGURING FOR LANDING, WHEN SELECTING FLAP 30 FROM TE DISPLAY, EICAS MSG APPEARED. RAN QRH PROCEDURE & LANDED FLAP 20 DEGREE. RAN THE FLAP HYD FROM 0 TO 30 DEGREES 2 TIMES, RAN THE FLAPS ELEC 0 TO 30, 2 TIMES WITH NO FAULTS. CHECKED ALL 3 FSEU'S NO FAULTS IAW MM 27-00-5-0, FIM 27-51 TREE 803. RT INBD FLAP, INBD JACKSCREW THREADS ROUGH & BALL NUT SEALS BROKEN. REF WRI 27-50 3523 FOR REPLACEMENT, RII & PARTS INFO. FLAP SYS LUBED & XMSN GEARBOXES SERVICED. TORQUE BRAKES CHECKED GOOD. REF WRI 27-50 3517 FOR WORK ACCOMPLISHED. OK FOR SERVICE.

Part: HANDLE — LACK OF LUBE (L1 DOOR) · airframe 79,538 hrs · 39,483 cycles

ON PREFLIGHT WE NOR ACFT MX COULD FULLY CLOSED LT ENTRY DOOR USING OUTSIDE HANDLES. L1 DOOR SLIDE INOPERATIVE, RELEASED FOR SERVICE IAW MEL 52-11-01-A CATEGORY B EXPIRATION 14OCT14. OUTSIDE DOOR HANDLES FEEL LIKE THEY OVER ROTATE, CANNOT PULL HANDLES OUT TO OPEN DOOR WHEN DOOR IS CLOSED FROM THE OUTSIDE. PERFORMED INSPECTION CHECK OF L1 DOOR IAW AMM 56-11-00-6. FOUND EXTERNAL DOOR HANDLES NOT MOVING FREELY WHEN CLOSING DOOR & INTERRUPTING DOOR CLOSING SEQUENCE. LUBRICATED EXTERIOR DOOR HANDLES, NOW DOOR CLOSES PROPERLY USING EXTERNAL DOOR HANDLES IAW AMM 56-11-00-6.

Part: PLACARD — UNSECURE (CABIN) · airframe 79,382 hrs · 39,376 cycles

PLACARD BEHIND SLIDE ARMING LEVER R1 DOOR MISSING, FELL DOWN INSIDE DOOR COVER. REATTACHED PLACARD IAW SMP.

Part: WIRE — BROKEN (SLIDE SENSOR) · airframe 79,084 hrs · 39,169 cycles

L1 DOOR RT SLIDE ARMED LIGHT INOPERATIVE. FOUND WIRE BROKEN AT FWD SENSOR S10214. SPLICED WIRE & BLUE WIRE FROM FWD PROX SENSOR. OPS CHECKED GOOD AMM 25-66-11-2.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 79,011 hrs · 39,114 cycles

R1 SLIDE ILLUMINATION LIGHT INOPERATIVE. RE-LAMPED IAW AMM 33-51-06, OPERATIONS CHECKED GOOD.

Part: PLATE — MISSING (CREW DOOR) · airframe 78,967 hrs · 39,077 cycles

RIGHT CREW ENTRY DOOR SLIDE ARMED OR DISARMED INDICATOR. REG GREEN METAL PLATE MISSING, FELL DOWN INTO DOOR.

Part: DOOR — OBSTRUCTED (CABIN) · airframe 78,925 hrs · 39,049 cycles

L1 DOOR DIFFICULT TO OPEN & CLOSE. HAD TO ENTER FROM R1 DOOR, RESET & OPEN L1 DOOR FROM INSIDE. CLOSING L1 DOOR FROM OUTSIDE, DOOR AGAIN GETS OUT OF SYNC & UNABLE TO OPEN. FOUND EVIDENCE OF WATER & DEBRIS IN DOOR JAMB AREA AT ROLLER & CHANNELS. CLEANED & SPRAYED WITH WATER DISPLACING SPRAY, THEN CLEANED AREA IAW SMP. OPERATIONS CHECKED DOOR SEVERAL TIMES FROM INSIDE & OUT IAW 52-11-00-2 WITH NO ISSUES.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 78,909 hrs · 39,038 cycles

ON LG EXTENSION RECEIVED AN EICAS, GEAR DOORS, ALERT. PERFORMED GO AROUND TO READ QRH & PERFORM REQUIRED ACTIONS. DOOR LIGHT & EICAS MESSAGE SUBSEQUENTLY WENT OUT. INSPECTED MLG DOORS IAW MM 32-12-00-6, MLG DOORS CHECKED NORMAL, NO DEFECTS NOTED. INSPECTED NLG DOORS IAW MM 32-22-00-0, NLG DOORS CHECKED NORMAL IAW CREW DEBRIEF GEAR DOORS OPERATED NORMALLY DURING REMAINDER OF APPROACH.

Part: ACTUATOR — INOPERATIVE (RT MLG DOOR) · airframe 78,870 hrs · 39,012 cycles

WHEN GEAR EXTENDED FOR LANDING, GOT GEAR DOORS EICAS MESSAGE & GEAR DOORS WARNING LIGHT. RT MLG GEAR DOOR OPEN UPON ARRIVAL EWR. GND CYCLED DOORS USING MAINT PANEL, OPERATIONS OK ON GND. FURTHER TROUBLE SHOOTING REQUIRED. R & R RT MAIN GEAR DOOR ACTUATOR IAW 757 MM 32-32-12-4. OPERATIONS CHECKED GOOD, ACFT OK FOR SERVICE.

Part: SKIN — GOUGED (BS 1692-1720) · airframe 78,643 hrs · 38,829 cycles

SCRIBE LINES IDENTIFIED AT BS 1692 - 1695, S14L, BS 1710 - 1720, S14L AND BS 1701.5 - 1707, S14L. COMPLIED WITH EA F-5330-T0301773.

Part: INTERCOSTAL — CRACKED (BS 400) · airframe 78,643 hrs · 38,829 cycles

BS 400 INTERCOSTAL IS CRACKED AT FASTENER HOLE, RBL 24. REMOVED DAMAGED INTERCOASTAL, FABRICATED NEW INTERCOASTAL AND INSTALLED IAW SRM 51-40-02, MM 20-60-02-2, DWG 141N5150, FAS ER 2-37153-801A, REV D, SRM 51-40- 05, SRM 51-20-01, AMM 51-21-10-7 AND SRM 51-40-02 AND SRM 53-10-51, FIG 1.

Part: SKIN — GOUGED (FUSELAGE) · airframe 78,643 hrs · 38,829 cycles

R2 DOOR UPPER HINGE CUTOUT GOUGED. REPAIRED IAW SRM 51-40-02 AND SRM 52-10-02, REP1.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 78,286 hrs · 38,591 cycles

RECEIVED EICAS LT WING SLIDE ON FINAL APPROACH. LIGHT WENT OUT BEFORE LANDING. COULD NOT FIND IN QRH. MESSAGE WAS CLEARED BY TIME GOT TO GATE. GAINED ACCESS AND DID VISUAL INSPECTION OF LT DOOR NO DEFECTS NOTED. NO HISTORY.

Part: LAMP — INOPERATIVE (R1 DOOR SLIDE) · airframe 77,926 hrs · 38,345 cycles

R1 DOOR SLIDE ILLUMINATION LIGHT INOPERATIVE. LAMPED IAW AMM 33-51-06-2-1.

Part: WIRE — DAMAGED (SLATS) · airframe 77,891 hrs · 38,327 cycles

DURING CLIMBOUT FL 210 L/E SLAT ASYM EICAS LIGHT AND L/E CAUTION LIGHT CAME ON. PRIOR TO LIGHTS FLAPS WERE UP, FLAP HANDLE UP AND FLAP INDICATOR INDICATED FLAPS UP. REDUCED SPEED TO 240 IAS LIGHTS STAYED ON DURING FLIGHT. NEEDED TO USE QRH PROCEDURES TO CONFIGURE FOR LANDING. EMERGENCY LANDING WAS DECLARED INTO IND ACFT LANDED WITH OUT INCIDENT. THE LT WING OTBD SLAT LOSS SWITCH WIRE W3326-1001-20 APPEARS TO BE SHORTED TO THE SHIELD BETWEEN CONNECTOR D41392J AND SPLICE SP1112. WIRE NEEDED IS CPN 0200167. R & R WIRE WIRE W3326-1001-20 BETWEEN D41392J AND S10341 IAW WDM 27-81-31. LT OTBD SLAT LOSS SWITCH REQUIRES OPS CK. PERFORMED OPS CHECK OF L/E SLAT SYS REF M/M 27-81-00-5 SLATS AND INDICATION CHECKED GOOD. OK FOR SERVICE.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 77,634 hrs · 38,153 cycles

DURING TRANSIT CHECK, FOUND RT EMERGENCY LIGHT OUT. R & R BULB ASSY IAW AMM 33-51-06. OPS CHECKED GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 77,579 hrs · 38,118 cycles

EMERGENCY EXIT LIGHTS UNARMED LIGHT HAS BULB BURNED OUT. RELAMPED EMERGENCY EXIT UNARMED LIGHT IAW MM REF: 33-13-00-2-0. OPS CHECKED GOOD. OK FOR SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 77,574 hrs · 38,112 cycles

R1 SLIDE LIGHT INOPERATIVE. RELAMPED IAW AMM 33-51-06-2-1. OPS CHECKED GOOD.

Part: HANDLE — WORN (L1 DOOR EXTERIOR) · airframe 77,558 hrs · 38,099 cycles

L1 DOOR DOES NOT COMPLETELY CLOSE USING EXTERIOR HANDLES. DOOR OPENS AND CLOSES NORMALLY USING INTERIOR HANDLE. IF CLOSED USING INTERIOR HANDLE DOOR INDICATIONS ALSO NORMAL. FOUND THAT THE OUTSIDE DOOR HANDLE BUTTERFLIES EARLY, HAS EXCESSIVE PLAY, AND OVER ROTATES WITH DOOR CLOSED BUT DOES NOT CAUSE THE INNER HANDLE TO LATCH CLOSED & LOCKED. REMOVED L1 DOOR INTER HANDLE ASSY AND OUTER HANDLE ASSY AMM 52-11-13-2, FOUND CLUTCH PAWL WORN AND OUTER HANDLE SHAFT SPREAD ALLOWING OUTSIDE HANDLE TO SLIP PAST STOPS BEFORE ACTUALLY LOCKING THE DOOR. INSTALLED L1 DOOR HANDLE IAW MM 52-11-13-2. OPENED AND CLOSED L1 DOOR SEVERAL TIMES FROM OUTSIDE HANDLE, L1 DOOR CLOSED NORMAL IAW MM 52-11-13-2.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 77,553 hrs · 38,096 cycles

R1 SLIDE LIGHT INOPERATIVE. RELAMPED IAW AMM 33-51-06-2-1. OPS CHECKED GOOD.

Part: WINDSHIELD — FAILED (COCKPIT) · airframe 77,533 hrs · 38,083 cycles

F/O WINDSHIELD BEGAN TO ARC FROM LOWER LT CORNER, THEN SPREAD THROUGHOUT WINDSHIELD. TURNED OFF WINDOW HEAT, ENTIRE OUTER LAYER OF WINDSHIELD CRACKED. COMPLIED WITH QRH PROCEDURES. R & R WINDSHIELD IAW MM 56-11-01-4 AND EA F-5610-160380. ACFT OK FOR SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 77,478 hrs · 38,053 cycles

DOOR SLIDE ILLUMINATION LIGHT INOPERATIVE. RELAMPED IAW AMM 33-51-06-2-1. OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 77,399 hrs · 38,009 cycles

R1 EXIT EXTERIOR EMERGENCY LIGHT BURNED OUT. RELAMPED R1 EXTERIOR EMERGENCY LIGHT IAW MM 33-51-06-2-1. OPS CHECKED GOOD, ACFT OK TO CONTINUE. FINAL CLOSED.

Part: BOTTLE — DISCHARGED (L1 DOOR) · airframe 77,044 hrs · 37,804 cycles

L1 DOOR DISCHARGE BOTTLE GAUGE SHOWS EMPTY. REMOVED AND REPLACED L-1 DOOR EMERGENCY POWER RESERVOIR REF AMM 52-11-30-4.

Part: MECHANISM — BINDING (L1 DOOR) · airframe 77,004 hrs · 37,771 cycles

WHILE WORKING ACFT, FOUND THAT ON 1L DOOR, UPPER AND LOWER FLAPPER DOORS WILL NOT CLOSE COMPLETELY FROM THE OUTSIDE. DOOR WILL CLOSE FROM THE INSIDE; HOWEVER, WHEN REOPENED A BINDING NOISE IS HEARD. REMOVED DOOR LINER, REF MM 52-11-02-4 AND INSPECTED AREA FOR DAMAGE REF MM 52-11-01-6-0. FOUND DOOR HANDLE CAM ASSY COVER MISSING, PHENOLIC SPACERS AND RUBBING CAM ALSO FOUND ESCAPE SLIDE COVER DISLODGED. REINSTALLED SPACERS REF MM 52-11-13-2-0 AND CORRECTLY POSITIONED SLIDE COVER, OPS CHECK REF MM 52-11-00-2 DOOR OPERATES NORMAL. REINSTALLED, REMOVED DOOR LINER. FINAL CLOSED.

Part: HINGE — DAMAGED (L1 DOOR) · airframe 76,999 hrs · 37,766 cycles

PRIOR TO PUSH TRYING TO SECURE 1L DOOR CLOSED DOOR WOULD NOT SHUT ALL THE WAY, RAMP AGENT NOTICED PROBLEM WITH HINGE. RELEASED FOR SERVICE IAW CDL: 52-11-01.

Part: SKIN — CORRODED (ZONE 100) · airframe 76,985 hrs · 37,745 cycles

HORIZONTAL STAB CENTER COMPARTMENT BS 1844 AFT AREA, CORROSION ON SKIN BETWEEN STR'S 23, 25L. A SKIN REPAIR WAS ACCOMPLISHED ON MAE W/C 46130440001 & MAE EA 757- 5381- 16-F3411, REV- DATED 07/28/2011 AT STA 1844 B/T STR'S 23L- 25L. THIS NON ROUTINE IS FOR TRACKING PURPOSES ONLY. REF EA F-5330-152640 ISSUED FOR TRACKING OF MAJOR REPAIR. MAJOR REPAIR.

Part: SKIN — DENTED (BS 1665 S27-28R) · airframe 76,985 hrs · 37,745 cycles

BS 1665 BETWEEN S27-28R, PROTRUDING DENT. DENT FOUND OUT OF LIMITS IAW SRM 53-00-01 FIG. 101 DET. III, REPAIRED IAWSRM 53-00-01 FIG. 201 REPAIR 16 CLASS B REPAIR MAJOR.

Part: SKIN — DAMAGED (BS 676) · airframe 76,985 hrs · 37,745 cycles

FOUND SCRIBE LINE AT BS 676.613 THROUGH BS 680.125 AND S14L LAP JOINT. ACCOMPLISHED EA F-5330-147696, MAJOR REPAIR.

Part: ANGLE — MISMANUFACTURED (ZONE 100) · airframe 76,985 hrs · 37,745 cycles

REWORK REQUIRED DUE TO INCORRECT MATERIAL USED IN REPAIR. REACCOMPLISH REPAIR IAW EA F-5310-152605 ACCOMPLISHED EA F-5310-152605. MAJOR REPAIR.

Part: ANGLE — MISMANUFACTURED (ZONE 100) · airframe 76,985 hrs · 37,745 cycles

REWORK REQUIRED DUE TO INCORRECT MATERIAL USED IN REPAIR. REACCOMPLISH REPAIR IAW EA F-5310-152604. REMOVED REPAIR ANGLE IAW SRM 51-40-02. ACCOMPLISHED EA F-5310-152604. MAJOR REPAIR.

Part: SKIN — DAMAGED (ZONE 200) · airframe 76,985 hrs · 37,745 cycles

FOUND SCRIBE LINE AT BSTA 1533 THROUGH 1534.25 S4L LAP JOINT ACCOMPLISHED EA F-5330-147690 PART 1 ONLY, VERIFICATION OF NO ADDITIONAL SCRIBELINES AT BUTT JOINT STA 1459 TO STA 1621 ALONG S-4L. PART 2 OF EA REQUIRED AT 1500 FC AFTER PART 1 AND PART 3 OF EA REQUIRED AT 1500FC AFTER PART 2. MAJOR REPAIR.

Part: SKIN — DAMAGED (ZONE 200) · airframe 76,985 hrs · 37,745 cycles

FOUND SCRIBE LINE AT BSTA 1681.8 THROUGH 1700.55 S-10L LAP JOINT. ACCOMPLISHED EA F-5330-147692 PART 1 ONLY, VERIFICATION OF NO ADDITIONAL SCRIBLINES AT BUTT JOINT STA 1621 TO 1720 ALONG S-10L. PART 2 REQUIRED AT 1500FC AFTER PART 1 AND PART 3 OF EA REQUIRED AT 1500 FC AFTER PART 2. MAJOR REPAIR.

Part: FRAME — MISREPAIRED (BS 1520 S29L/R) · airframe 76,985 hrs · 37,745 cycles

FRAME REPAIR LOCATED AT BS 1520 S29R TO S29L DOES NOT CONFORM TO CURRENT SRM REQUIREMENTS. FRAME REPAIR REPLACED IAW EA. F-5310-147719.

Part: MOUNT — CORRODED (NR 2 ENGINE) · airframe 76,985 hrs · 37,745 cycles

NR 2 PYLON FWD ENG MOUNT STRUT FITTING WITH CORROSION ON LOWER SURFACE FWD AND AFT MOUNT MATING. REMOVED CORROSION BY BLENDING AREA PER SRM-54-51-90 PG.104 FIG.101 DET.VII, REMOVED AND REPLACED FWD. STRUT MOUNT FITTING, PER SRM-51-40-02.

Part: SKIN — MISREPAIRED (BS 1680 S20L) · airframe 76,985 hrs · 37,745 cycles

SKIN REPAIR LOCATED AT STA 1680, S-20L DOES NOT CONFORM TO CURRENT SRM CONFIGURATION.

Part: FRAME — MISREPAIRED (BS 1240) · airframe 76,985 hrs · 37,745 cycles

REPAIR AT BS 1240 BETWEEN S25L AND 26L DOES NOT CONFORM CURRENT S/F CONFIGURATION ACCOMPLISHED EA F 5310-152610. FUSELAGE EXISTING FRAME REPAIR REPLACEMENT AT BS 1240 AND S24L-S26L. MAJOR REPAIR.

Part: FRAME — MISREPAIRED (BS 1200 S27R) · airframe 76,985 hrs · 37,745 cycles

FRAME REPAIR AT STA 1200, S27R DOES NOT CONFORM TO CURRENT SRM S/F CONFIGURATION. ACCOMPLISHED EA F-5310-147708.

Part: FITTING — CORRODED (CARGO BAY) · corrosion level 2 · airframe 76,985 hrs · 37,745 cycles

FWD CARGO COMPT, CARGO TIE DOWN FITTING CORRODED AT STA 845, S-26L CENTER PLUG. REMOVED CORROSION STA 845 S-26L TIE DOWN FITTING IAW SRM 51-10-02. ORIG MAT .180 REMAINING .147 OUT OF LIMITS IAW SRM 53-00-53 FIG 101, DET V. REMAINING THICKNESS ACCEPTABLE IAW EA, ACCOMPLISHED EA F5310-147700. FUSELAGE - MAIN FRAME- SECTION 43- LOWER CARGO COMPARTMENT CARGO TIE DOWN FITTINGS. MAJOR REPAIR.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 76,985 hrs · 37,745 cycles

FWD CARGO COMPT, CARGO TIE DOWN FITTING CORRODED AT STA 680, STR 26R. REMOVED CORROSION TIE DOWN FITTING IAW SRM 51-10-02. BLENDED AREA ORIG. MAT .180 REMAINING .146 OUT OF LIMITS IAW SRM 53-00-53, FIG 101, DET V. ACCOMPLISHED EA F5310-147700. MAJOR REPAIR.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 76,985 hrs · 37,745 cycles

FWD CARGO COMPT, CARGO TIE DOWN CORRODED AT STA 640, STR 26R. REMOVED CORROSION TD FITTING IAW SRM 51-10-02. BLENDED AREA ORIG MAT .180 REMAINING .159 OUT OF LIMITS IAW SRM 53-00-53, FIG 101, DET V. ACCOMPLISHED EA F5310-147700. BLEND OUT ACCEPTABLE IAW EA. MAJOR REPAIR.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 76,985 hrs · 37,745 cycles

FWD CARGO COMPT, CARGO TIE DOWN FITTING CORRODED AT STA 760, STR 26R. REMOVED CORROSION FROM TD FITTING STA 760, 26R IAW SRM 51-10-02. ORIG MAT .180 REMAINING .141 OUT OF LIMITS IAW SRM 53-00-53, FIG 101, DET V. REMAINING THICKNESS ACCEPTABLE IAW EA. ACCOMPLISHED EA F5310-147700, FUSELAGE - MAIN FRAME - SECTION 43- LOWER CARGO COMPARTMENT CARGO TIE DOWN FITTINGS. MAJOR REPAIR.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 76,985 hrs · 37,745 cycles

FWD CARGO COMPT, CARGO TIE DOWN FITTING CORRODED AT STA 720 STR 26R. REMOVED CORROSION TD FITTING IAW SRM 51-10-02. BLENDED AREA ORIG MAT .180 REMAINING .150 OUT OF LIMITS IAW SRM 53-00-53, FIG 101, DET V. ACCOMPLISHED EA F-5310-147700. BLEND OUT ACCEPTABLE IAW EA MAJOR REPAIR.

Part: SKIN — DAMAGED (BS 661 19R) · airframe 76,985 hrs · 37,745 cycles

FOUND 2EA VERTICAL SCRIBE LINES RUNNING INTO LAP SEAM AT S19R AND BUTT JOINT AT BS 661. ACCOMPLISHED EA F-5330-152621, MAJOR REPAIR.

Part: STRINGER SPLICE — FAILED (BS 1460) · airframe 76,985 hrs · 37,745 cycles

AFT CARGO AREA AT BS 1460, STRINGER S29R, WITH DEEP GOUGE ON SPLICE. REMOVED STRINGER SPLICE IAW SRM 51-40-02 AND STRINGER CLIP IAW SRM51-40-02, REPLACED SPLICE IAW SRM 51-40-02 AND INSTALLED STR CLIP IAW SRM 51-40-02. MAJOR REPAIR.

Part: ANGLE — FAILED · airframe 76,985 hrs · 37,745 cycles

L-2 DOOR UPPER HINGE CUTOUT DAMAGED. ACCOMPLISHED EA F-5210-152619. MAJOR REPAIR.

Part: SKIN — MISREPAIRED (BS 470 S22-23R) · airframe 76,985 hrs · 37,745 cycles

PREVIOUSLY INSTALLED SKIN REPAIR AT BS 470 BETWEEN S22R-S23R DOES NOT COMPLY WITH CURRENT SRM REQUIREMENTS. REMOVED REPAIR, COMPLIED IAW EA F- 5330-147725. MAJOR REPAIR.

Part: FRAME — MISREPAIRED (ZONE 100) · airframe 76,985 hrs · 37,745 cycles

FRAME REPAIR AT STA 780 S-28L TO S-28R DOES NOT CONFORM TO CURRENT SRM CONFIGURATION. REMOVED REPAIR AND COMPLIED WITH EA F-5310-147694 FUSELAGE MAIN FRAME EO F5100-7-5001, REPAIR REWORK STA 70 BETWEEN S-28L TO S-28R. MAJOR REPAIR.

Part: SKIN — MISREPAIRED (BS 450 S23-24R) · airframe 76,985 hrs · 37,745 cycles

PREVIOUSLY INSTALLED SKIN REPAIR AT BS 450 BETWEEN S23R- S24R DOES NOT COMPLY WITH CURRENT SRM REQUIREMENTS. REMOVED REPAIR COMPLIED IAW E.A. F-5330-147725. MAJOR REPAIR

Part: SKIN — CRACKED (BS 1787.45) · airframe 76,985 hrs · 37,745 cycles

FUSELAGE SKIN ABOVE PRODUCTION DOUBLER HAS A CRACK ABOUT 1.3" LONG AT BS 1787.45, S-17L, WL 208. ACCOMPLISHED E.A. F 5330-152606. FUSELAGE STAB SEAL FAIRING SKIN CRACKED MAJOR REPAIR.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 76,985 hrs · 37,745 cycles

AFT CARGO AREA AFTER REMOVAL OF DOUBLER FOUND AT STA 140 BETWEEN S-29R TO S-30 SHEAR TIE WORN AND HAS CORROSION. REMOVED CORROSION AT AFT CARGO SHEAR TIE STA 1400 BETWEEN S-29R TO S-30 IAW SRM 51-10-02. BLENDED AREA L=1 W=.5 D=.010 ORIGINAL MATERIAL .050 AFTER REWORK .040 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07, FIG 101 DETAIL II. R & R SHEAR TIE IAW SRM 51-40-02. CATEGORY "A" MAJOR REPAIR.

Part: FRAME — INOPERATIVE (BS 1220) · airframe 76,985 hrs · 37,745 cycles

THE PREVIOUSLY INSTALLED FRAME REPAIR LOCATED AT STA 1220 BETWEEN S24L TO S26L REQUIRES REPLACEMENT ACCOMPLISHED EA F-5310-147710, FUSELAGE-MAIN FRAME-EO F-5100-7-5001-EXISTING REPAIR. REWORK STA 1220 S-24L TO S-26L.

Part: FRAME — MISREPAIRED (BS 1580) · airframe 76,985 hrs · 37,745 cycles

FRAME REPAIR LOCATED AT STA 1580 BETWEEN S24L AND S25L MISREPAIRED. ACCOMPLISHED EA F5310-152611. MAJOR REPAIR.

Part: SKIN — MISREPAIRED (BS 400-420) · airframe 76,985 hrs · 37,745 cycles

SKIN REPAIR AT BS 400-420 BETWEEN S20L-S21L DOES NOT COMPLY WITH CURRENT SRM REQUIREMENTS. ACCOMPLISHED E.A. F5330-147718. MAJOR REPAIR

Part: FRAME — DAMAGED (BS 1640 S6-7R) · airframe 76,985 hrs · 37,745 cycles

FRAME LOCATED AT STA 1640,S-6R-S-7R DAMAGED. ACCOMPLISHED E.A. F5310-152613.

Part: STRINGER SPLICE — GOUGED (ZONE 100) · airframe 76,985 hrs · 37,745 cycles

AFT CARGO AREA AT BS 1460, STRINGER S29L WIYH GOUGE ON SPLICE. REMOVED SPLICE AT BS 1460, STRINGER 29L IAW SRM 51-40-02. REPLACED SPLICE AT BS 1460, STRINGER 29L IAW SRM 51-40-02, PN 146N3820. REPAIR A , MAJOR REPAIR.

Part: FRAME — MISREPAIRED (BS 1260) · airframe 76,985 hrs · 37,745 cycles

FRAME AT STA 1260 BETWEEN S-25R AND S-26R MISREPAIRED. REMOVED EXISTING REPAIR ANGLE IAW EA F-5310-147706. MAJOR REPAIR.

Part: FRAME — DAMAGED (ZONE 100) · airframe 76,985 hrs · 37,745 cycles

FRAME LOCATED AT BS 1320 BETWEEN S-23R DAMAGED.

Part: FRAME — DAMAGED (BS 1400) · airframe 76,985 hrs · 37,745 cycles

FRAME LOCATED AT BS 1400 BETWEEN S-25L TO S-26L DAMAGED. REPAIRED IAW F-5310-146538. CATEGORY "A" MAJOR REPAIR.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 76,985 hrs · 37,745 cycles

AFT CARGO COMPT STRINGER CORRODED AND GOUGED AT STA 1460 TO 1470, STR 29R REMOVED STRINGER STA 1460 THRU 1490 STR 29R IAW SRM 51-40-02, REMOVED GOUGES AND CORROSION IAW SRM 51-10-02 CHECKED LIMITS OF BLENDED AREA L= .60, W= .50, D= .050 ORIGINAL MATERIAL .090 AFTER REMAINING MATERIAL .040 OUT OF LIMITS IAW SRM 53-00-03 FIG 101, DET II. REPAIRED STRINGER AT STA 1460 TO 1490, STR-29R IAW SRM 53-00-03 REPAIR 2. INSTALLED REPAIR STRINGER PN FX-SRM 53-00-07-1 AND REPAIR HAT CHANNEL FILLER PN FX-SRM 53-00-07-2. MAJOR REPAIR.

Part: SKIN — CORRODED (BS 720-770) · airframe 76,985 hrs · 37,745 cycles

CORROSION UNDER LAP SEAM FROM STA 720 TO 770 STR 19R. REMOVED CORROSION FROM LAP SEAM IAW SRM 51-10-02. ORIG MATERIAL .056 REMAINING .031 OUT OF LIMITS IAW SRM 53-00-01, FIG 101, DETAIL III. ACCOMPLISHED EA F-5330-147695. MAJOR REPAIR.

Part: SUPPORT FITTING — GOUGED (NR 1 PYLON) · airframe 76,985 hrs · 37,745 cycles

LT WING NR 1 PYLON FWD AND INBD STRUT SUPPORT FITTINGS HAVE A GOUGE. BLENDED DAMAGED AREA IAW SRM 57-20-90, FIG 101, DETAIL V. COMPLIED WITH EA F-5740-146537 WING-(FITTING AD 2003-18-05/EO F-5450-7-5010) NR 1 PYLON INBD SIDE LOAD FITTING REWORK. MAJOR REPAIR.

Part: FRAME — WORN (BS 984 S1-3L) · airframe 76,985 hrs · 37,745 cycles

FRAME, STA 984, STR 1 TO 3L HAS HOLES THAT ARE OUT OF LIMITS. REMOVED DAMAGED FRAME AREA FROM STR 1 TO STR 7L STA 984 LT IAW SRM 53-00-07. LOCATED AND DRILLED 2 EA ANGLES AND NEW FRAME IAW SRM 51-40-05. TREATED AND PRIMED REPAIR PARTS IAW SRM 51-20-01. INSTALLED NEW FRAME AND 2EA ANGLES AT STA 984, STR 1 TO STR 7L IAW SRM 51-40-02, AND 53-00-07, FIG 201, REPAIR 3. CAT- "B", NEXT INSP AT 10,000 F/C, THEN DO A HFEC INSP EVERY 12,000 F/C. MAJOR REPAIR.

Part: SKIN — MISREPAIRED (BS 1360 S1-2R) · airframe 76,985 hrs · 37,745 cycles

THE PREVIOUSLY INSTALLED SKIN REPAIR LOCATED AT BS 1360 S-1 TO S-2R (SKY RADIO ANTENNA CUT OUT ) DOES NOT CONFORM TO CURRENT S/F SRM. ACCOMPLISHED E.A. F-5330-147691.

Part: SKIN — DAMAGED (BS 1540-1560) · airframe 76,985 hrs · 37,745 cycles

SKIN REPAIR AT STA 1540-1560, BL0 HAS TOOL DAMAGE. ACOMPLISHED EA F-5330-146543. MAJOR REPAIR.

Part: FLOORBEAM — MISALIGNED (ZONE 200) · airframe 76,985 hrs · 37,745 cycles

STA 480, RBL 52, FLOORBEAM UPPER CHORD HAS A DOUBLE DRILL HOLE. REPAIRED FLOOR BEAM UPPER CHORD IAW SRM 53-00-51, REPAIR NR 3, CUT OUT DAMAGE ON FLOORBEAM UPPER CHORD IAW SRM 53-00-51, REPAIR NR 3. FABRICATED REPAIR PARTS FOR UPPER CHORD IAW SRM 53-00-51, REPAIR NR 3. INSTALLED REPAIR PARTS FLOORBEAM UPPER CHORD IAW SRM 53-00-51, REPAIR NR 3. AT STA 480, RBL 52, CATEGORY "A", REPAIR NR 3. MAJOR REPAIR.

Part: SKIN — MISREPAIRED (BS 215-233) · airframe 76,985 hrs · 37,745 cycles

SKIN REPAIR AT BS 215- 233, S29- 30L DOES NOT CONFORM TO CURRENT S/F CONFIGURATION. REMOVED AND REPLACED DOUBLER BS 215-233, S29- 30L IAW SRM 53-00-01 FIG 201 DETAIL I, II, REPAIR 16, CATEGORY "B", TABLE II. MAJOR REPAIR.

Part: FLOORBEAM — DAMAGED (ZONE 200) · airframe 76,985 hrs · 37,745 cycles

STA 460, RBL 52, FLOORBEAM UPPER CHORD HAS A DOUBLE DRILL HOLE. CUT OUT DAMAGE ON FLOORBEAM UPPER CHORD IAW SRM 53-00-51 REPAIR NR3. FABRICATED REPAIR PARTS FOR UPPER CHORD REPAIR IAW SRM 53-00-51. INSTALLED REPAIR PARTS, FLOORBEAM UPPER CHORD REPAIR IAW SRM 53-00-51 AT STA 460, RBL 52, CATEGORY A. MAJOR REPAIR.

Part: FRAME — DAMAGED (BS 1260) · airframe 76,985 hrs · 37,745 cycles

FRAME LOCATED AT STA 1260 BETWEEN S-26L AND S-25L DAMAGED. COMPLIED IAW EA F- 5310-147706. MAJOR REPAIR.

Part: SKIN — MISREPAIRED (BS 395-718) · airframe 76,985 hrs · 37,745 cycles

THE PREVIOUSLY INSTALLED SKIN REPAIR AT BS 395-418 S18-19R DOES NOT COMPLY WITH CURRENT SRM S/F CONFIGURATION. REMOVED PREVIOUSLY INSTALLED SKIN DOUBLER AT STA BS 395 -BS 418, STR 18R TO 19R IAW SRM 51-40-02. HFEC INSPECTED CUT OUT IAW NDTM DT6 51-00-11, NO CRACKS NOTED, HFEC INSPECTED ALL OPEN HOLES IAW NDTM DT6 51-00-16 NO CRACK INDICATION NOTED. FABRICATE 1 EA REPAIR DOUBLER FROM 7075-T6.071 BATCH 1947941, 1 EA REPAIR FILLER FROM 7075-T6 .063 BATCH NR 1947994 IAW SRM 53-00-01 REPAIR 15. INSTALLED REPAIR DOUBLER AND FILLER AT BS 395-BS 418, STR 18R - STR 19R IAW SRM 53-00-01 REPAIR 15. THIS IS CATEGORY B REPAIR. MAJOR REPAIR.

Part: FRAME — DAMAGED (BS 1480) · airframe 76,985 hrs · 37,745 cycles

FRAME DAMAGED LOCATED AT STA 1480 BETWEEN S-25L AND S-26L. COMPLIED IAW EA F-5310- 152612. MAJOR REPAIR.

Part: FRAME — DAMAGED (BS 1420) · airframe 76,985 hrs · 37,745 cycles

FRAME DAMAGED, LOCATED AT STA 1420 BETWEEN S-24L AND S-26L. COMPLIED IAW EA F-5310- 152620. MAJOR REPAIR.

Part: SKIN — MISREPAIRED (BS 1300-1320) · airframe 76,985 hrs · 37,745 cycles

SKIN REPAIR AT BS 1300 TO 1320 S3L DOES NOT COMPLY WITH CURRENT SRM REQUIREMENTS. REMOVE REPAIR DOUBLER, COMPLIED IAW EA F-5330-147699. MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 76,985 hrs · 37,745 cycles

SEAT TRACK, BS 1080-1080-1180, LBL 45,50, CORRODED AND GOUGED IN NUMEROUS PLACES. REMOVED SEAT TRACK IAW SRM 51-40-02. REMOVED CORROSION AND DAMAGED AREA. ORIG MAT .080 AFTER REWORK .030 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, FIG 101. DETAIL VII AND VIII. INSTALLED NEW SEAT TRACK AT STA 1080-1180, LBL 45.5. CATEGORY "A" MAJOR REPAIR.

Part: SKIN — DENTED (BS 435) · airframe 76,985 hrs · 37,745 cycles

EXTERIOR FUSELAGE SKIN HAS A DENT AT STA 435, BETWEEN S21-22R. FOUND OUT OF LIMITS IAW-SRM-53-00-01 FIG 101, DET III . REPAIRED DENT IAW-SRM-53-00-01 FIG 201, REPAIR 16. THIS IS A CLASS B REPAIR.

Part: FRAME — MISREPAIRED (BS 1340 S26-27R) · airframe 76,985 hrs · 37,745 cycles

FRAME REPAIR LOCATED AT STA 1340 BETWEEN STR 26R AND STR 27R DOES NOT CONFORM TO CURRENT SRM CONFIGURATIONS. ACCOMPLISHED EA F5310-147704. MAJOR REPAIR.

Part: FRAME — MISREPAIRED (BS 1340 S25-27L) · airframe 76,985 hrs · 37,745 cycles

FRAME REPAIR LOCATED AT STA 1340 BETWEEN STR 25L AND STR 27L DOES NOT CONFORM TO CURRENT SRM CONFIGURATIONS. REPAIRED IAW EA F5310-147704.

Part: FRAME — MISREPAIRED (BS 1340 S25-27L) · airframe 76,985 hrs · 37,745 cycles

FRAME REPAIR LOCATED AT STA 1340 BETWEEN STR 25L AND 27L DOES NOT CONFORM TO SRM CONFIGURATION.

Part: FLOORBEAM — DAMAGED (ZONE 200) · airframe 76,985 hrs · 37,745 cycles

MAIN CABIN FLOOR AREA AT STA 1520, LBL 14 FLOORBEAM WITH FASTNER HOLE ELONGATED REPAIRED FLOORBEAM AT STA 1520 IAW SRM 53-00-51, REPAIR 5 CATEGORY "A" MAJOR REPAIR.

Part: STRINGER — CRACKED (BS 1650-1670) · airframe 76,985 hrs · 37,745 cycles

STRINGER 23R IS CRACKED AT A FASTNER HOLE IN THE LOWER WEB AT APPROX STA 1660. REPAIRED STR 23R, STA 1650-1670 IAW SRM 53-00-03, FIG 201, REPAIR NR 2 USING BAC 1498-203 TCH 2031079 AND T11/883136. A MAJOR REPAIR NO FOLLOW UP INSP REQUIRE.

Part: SEAT TRACK — CRACKED (BS 640) · airframe 76,985 hrs · 37,745 cycles

SEAT TRACK AT STA 640, LBL 24.75 IS CRACKED. REMOVED DAMAGE SECTION IAW SRM 53-00-52. FABRICATED REPAIR SECTION IAW SRM 53-00-52 REPAIR 1 FIG 201. INSTALLED REPAIR SECTION IAW SRM 53-00-52 REPAIR 1 AT STA 640 LBL 24.75. CATEGORY "A" MAJOR REPAIR

Part: SKIN — MISREPAIRED (BS 1684 S27L) · airframe 76,985 hrs · 37,745 cycles

SKIN REPAIR AT STA 1684, S-27 L DOES NOT COMPLY WITH CURRENT SRM REQUIREMENTS. REMOVED REPAIR AND FILLER IAW SRM 51-40-02. REPLACED REPAIRE AND REINSTALLED FILLER IAW SRM 51-40-02 FIG 201 REPAIR 15. THIS IS CLASS B REPAIR, MAJOR REPAIR.

Part: SKIN — MISREPAIRED (ZONE 200) · airframe 76,985 hrs · 37,745 cycles

SKIN REPAIR AT BS 1560 BETWEEN STR 1R TO S-2R DOES NOT COMPLY WITH CURRENT SRM REQUIREMENTS. REMOVED REPAIR DOUBLER AT SKIN BS 1560 BETWEEN S-1R TO S-2R IAW SRM 51-40-02, INSTALLED REPAIR DOUBLER IAW SRM 53-00-01, FIG 201, REPAIR NR 16 THIS IS CLASS "B" REPAIR, MAJOR REPAIR. FOLLOW UP ACTION REQUIRE, FREQ 25,000 F.C., INTERVAL/SUB 6,000 F.C.

Part: SKIN — DENTED (ZONE 100) · airframe 76,985 hrs · 37,745 cycles

EXTERIOR FUSELAGE SKIN HAS DENT AT STA 1422, BETWEEN S28L AND S29L EVALUATED DENT AT EXTERIOR FUSELAGE SKIN STA 1422 BETWEEN S28L AND S29L A=.040 Y=.020 A/Y=20 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01, FIG 101, DET III, PAGE 104. REPAIRED DENT IAW SRM 53-00-01, FIG 201, REPAIR NR 15. THIS REPAIR IS A CLASS B, MAJOR REPAIR.

Part: SKIN — MISREPAIRED (ZONE 200) · airframe 76,985 hrs · 37,745 cycles

PREVIOUSLY INSTALLED SKIN REPAIR AT STA 1700 BETWEEN S-15L TO S-16L DOES NOT COMPLY WITH CURRENT SRM REQUIREMENTS REMOVED DOUBLER AT STA 1700 BETWEEN S-15L TO S-16L ON THE SKIN IAW SRM 51-40-02. INSTALLED NEW DOUBLER IAW SRM 53-00-01 FIG 201 REPAIR 16. CLASSIFIED CATEGORY "B" MAJOR REPAIR.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 76,985 hrs · 37,745 cycles

PREVIOUSLY INSTALLED SKIN REPAIR AT STA 1625 BETWEEN S-27L TO S-28L DOES NOT COMPLY WITH CURRENT SRM REQUIREMENTS. REMOVED DOUBLER AT STA 1625 BETWEEN S-27L TO S-28L ON THE SKIN IAW SRM 51-40-02. REPAIRED AREA IAW SRM 53-00-01, FIG 201, REPAIR 16. CLASSIFIED CATEGORY "B" MAJOR REPAIR.

Part: DOUBLER — CRACKED (ZONE 100) · airframe 76,985 hrs · 37,745 cycles

MAIN AVIONICS ACCESS DOOR CRACKED AS MARKED. CUT AND REMOVED DAMAGE PORTION IAW SRM 51-70-13, FABRICATED REPAIR DOUBLER FROM 20-24-T3 .050 IAW SRM 51-70-13, INSTALLED NEW REPAIR DOUBLER AT MAIN AVIONICS DOOR IAW SRM 51-70-13, DETAIL I, FIG 1. CATEGORY "A" REPAIR. MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 76,985 hrs · 37,745 cycles

MAIN CABIN AREA BETWEEN STA 470-660, LBL 45 SEAT TRACK HAS CORROSION SEAT TRACK STA 470-660, LBL 45 FOUND OUT OF LIMITS IAW SRM 53-00-52, FIG 101, DETAIL V. ORIG MATERIAL .165 AFTER REWORK .085. L=2.1 W=.750. R & R SEAT TRACK IAW SRM 51-40-02. CLASSIFIED MAJOR REPAIR

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 76,985 hrs · 37,745 cycles

MAIN CARGO FLOORBEAM UPPER CHORD IS CORRODED AT BL 0 TO RBL 58 AT STA. 1640 REMOVED AND REPLACED STA 1640 FLOORBEAM IAW DWG 146N8722 AND SRM 51-40-02.

Part: SKIN — DENTED (BS 1735 S29R) · airframe 76,985 hrs · 37,745 cycles

EXTERNAL FUSELAGE SKIN HAS A OUTER DENT AT STA 1735 S-29R EVALUATEED DENT IAW SRM 53-00-01 FIG. 101 PG. 104 & FOUND OUT OF LIMITS, REPAIRED DENT IAW SRM 53-00-01 REPAIR 16 THIS A CLASS "B" MAJOR REPAIR.

Part: SKIN — DENTED (BS 710 S24-25L) · airframe 76,985 hrs · 37,745 cycles

EXTERNAL FUSELAGE SKIN HAS A OUTER DENT AT STA 710 BETWEEN S-24L TO S-25L. EVALUATED DENT IAW SRM 53-00-01 FIG.101 PG. 104 DET. III. A=.700 Y=.037 A/Y=16.2, FOUND OUT OF LIMITS. REPAIRED DENT AT ST. 710 STR. 24L-25L IAW SRM 53 -00-01 REPAIR 16. THIS IS A CLASS "B" REPAIR MAJOR REPAIR.

Part: FRAME — CORRODED (BS 1460 S29-30L) · airframe 76,985 hrs · 37,745 cycles

AFT LOWER CARGO FLOOR FRAME AT STA 1460 STR 29L TO 30 CORRODED AT LOWER SECTION OF FRAME. REMOVED CORROSION ON FRAME STA 1460. BLENDED AREA ORIG MATERIAL .063 MATERIAL LOSS .015 REMAINING .048. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07, FIG 101, DETAIL II AND SRM 51-10-02. R & R FRAME STA 1460 BETWEEN S-25L TO S-26R IAW SRM 51-40-02. MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 76,985 hrs · 37,745 cycles

MAIN CABIN STA 365, BL-0 FLOORBEAM CORRODED UPPER FLANGE. REMOVED CORROSION IAW SRM 51-10-02. ORIGINAL MATERIAL .125 AFTER REWORK .098. EXCEEDED MAX ALLOWABLE DAMAGE REMOVAL OF .107 IAW SRM 53-00-51 FIG 101 DETAIL III. AREA OUT OF LIMITS. REMOVED DAMAGED AREA OF BEAM REPAIR IAW SRM 51-40-02. FABRICATED NEW TEE, REPAIR ANGLES AND REPAIR STRAPS IAW SRM 51-40-02 AND SRM 53-00- 51 TABLE 1. INSTALLED REPAIR CHORD, ANGLES AND STRAPS IAW SRM 51-40-02. CLASSIFED CATEGORY "A" MAJOR REPAIR