N564FE

Part: SENSOR — FAILED (BLEED AIR SYS) · airframe 914 hrs · 31,321 cycles

AT 370 RECEIVED LEVEL 1 HIGH STAGE 3 OFF ALERT, FOLLOWED BY LEVEL 1 MANIFOLD 3 FAIL ALERT. PERFORMED QRH, RAN THROTTLE IN IDLE. REPLACED NR 2 ENG HIGH STAGE TEMP SENSOR IAW AMM 36-11-01-2. OPERATIONS CHECKED GOOD. PERFORMED PSC 1, 2 & 3 RTS IAW AMM 36-10-02-5. ALL TEST PASSED. RAN ENG 2 & 3 IAW JRH & CHECKED PNEUMATIC SYSTEMS IAW AMM 36-00-03-5, SATISFACTORY. REPLACED NR 3 MANIFOLD FAILURE DETECTION PRESS SWITCH IAW MM36-23-03-4.

Part: SLIDING WINDOW — UNSECURE (COCKPIT) · airframe 911 hrs · 31,111 cycles

REJECTED TAKEOFF, AIR NOISE FROM CAPTAIN`S WINDOW. CHECKED LATCH. LATCH APPEARED CLOSED & LOCKED. THE CAPTAIN PUSHED THE LOCKING ARM FWD ABOUT .750 ON HIS SLIDING WINDOW. NO REPORTS FROM THE FLIGHT CREW OF ANY NOISE COMING FROM CAPTAIN`S SLIDING WINDOW. CYCLED CAPTAIN`S SLIDING WINDOWS SEVERAL TIMES. WINDOW STAYED LATCHED & LOCKED. PERFORMED SLIDING CLEAR VIEW WINDOW RIG OPS TEST IAW MM 56-12-00-5-2. OPS CHECKED GOOD.

Part: UNKNOWN — MALFUNCTIONED (OIL SYSTEM) · airframe 911 hrs · 31,110 cycles

LEVEL 2 ENG 1 OIL FILTER ALERT DURING CLIMB PASSING FL 200. ALL OIL PRESS & TEMP INDICATIONS WERE NORMAL, NO VIBRATION. REDUCED THROTTLE TO IDLE. LEVEL 2 ALERT REMAINED. SHUTDOWN NR 1 ENG IAW QRH GUIDANCE, NO OTHER INDICATIONS. ENG 1 CONTINUED TO WINDMILL AT APPROX 24% N2. TROUBLESHOOT IAW FIMM 79-35-00-2-0, PULLED MASTER CHIP DETECTOR, NO CONTAMINATION FOUND. REMOVED AND REPLACE SCAVANGER OIL FILTER IAW AMM 79-20-02/201 AND, LUB SUPPLY FILTER IAW AMM 79-20-01-201. NO EVIDENCE OF CONTAMINATION OF EITHER FILTERS. AS PRECAUTIONARY REMOVED AND REPLACED OIL STRAINER CLOGGING SWITCH IAW AMM 79-35-01-2. RAN ENGINE REF JRH, LEAK CHECK AND OPS CHECK GOOD. A/C OK FOR SERVICE. ALL ENGINE PARAMETERS NORMAL.

Part: SLIDE — BLOWN (R1 DOOR) · airframe 910 hrs · 31,053 cycles

R1 SLIDE BLOWN ON ARRIVAL. REMOVED DEPLOYED SLIDE & RAFT ASSEMBLY AS REQUIRED IAW AMM 25-61-07-4. RESET & SERVICED RI DOOR AIR RESERVOIR AS REQUIRED IAW AMM 51-10-01-2. INSTALLED NEW EVACUATION SLIDE & RAFT ASSEMBLY AS REQUIRED IAW AMM 25-61-01-2. DOOR CHECKED GOOD. SYS OK FOR SERVICE.

Part: WIRE — BROKEN (MLG) · airframe 906 hrs · 30,782 cycles

DURING CLIMB OUT APPROXIMATELY FIVE MINUTES AFTER TAKEOFF RECEIVED A LEVEL 2 BRAKE OVERHEAT ALERT. CONFIGURATION PAGE SHOWED LT TRUCK RT AFT TIRE TEMP, BRAKE NR 6, RISING RAPIDLY THRU 800 DEGREES, THEN WENT TO A X. COMPLIED WITH QRH & EXTENDED GEAR FOR 10 - 15 MINUTES. SUSPECT BAD INDICATOR, NOT STUCK, BECAUSE WE HAD NORMAL ACCELERATION & RUDDER INPUTS ON TAKEOFF ROLL. TROUBLESHOT & FOUND WIRES BROKEN AT CONNECTOR. R & R CONNECTOR & RETERMINATED WIRES IAW WPM 20-31-03. NR 6 BRAKE TEMP SENSOR OPERATIONS CHECK GOOD IAW MM 32-46-02-2.

Part: ANTI-ICE SYSTEM — UNKNOWN · airframe 905 hrs · 30,759 cycles

DURING DESCENT WITH ENGINE & WING ANTI - ICE ON INITIALLY RECEIVED A NR 3 MANIFOLD FAILURE LIGHT SELECTED. WING ANTI - ICE OFF, NR 3 MANIFOLD FAIL LIGHT REMAINED ON, BUT NO LEVEL3, AIR MANIFOLD 3 FAIL ALERT , SYNOPTIC SHOWED RED FAILURE INDICATION OF MANIFOLD 3. AS WE LEVELED OFF & POWER CAME UP THE LEVEL 3, AIR MANIFOLD 3 FAIL ALERT, CAME ON FOR APPROX 3- 5 SECONDS THEN WENT OFF. THE RED, MANIFOLD FAIL LIGHT, OVERHEAD PANEL STAYED ON FOR NEXT 10 MINUTES THEN WENT OUT WHEN THE PACK TEMP & BLEED AIR 3 TEMP DECREASED. HIGHEST PACK TEMP NOTED WAS 170 F. SYSTEM TESTED GOOD IN REFERENCE TO AMM: 36-10-02-5-0. RAN NR 3 ENGINE IN REFERENCE TO JRH. NO FAULTS FOUND.

Part: SWITCH — STUCK (L1 DOOR) · airframe 904 hrs · 30,706 cycles

RAMP CREW REPORTED THAT AFTER CLOSING L1 DOOR, IT WOULD NOT OPEN ELECTRICALLY. ON INSPECTION FOUND DOOR OPEN SWITCH PLUNGER STUCK IN THE OPEN POSITION. LUBED AND CYCLED PLUNGER SEVERAL TIMES. RAN L1 DOOR THROUGH FULL CYCLE SEVERAL TIMES IAW AMM 52-10-01-5-0, OPS CHECKED GOOD.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 90,002 hrs · 30,458 cycles

RIGHT AFT BODY FAIRING AFT SUPPORT SHOWING EXFOLIATION CORROSION. REPAIRED IAW EA 8-5320-T0311923.

Part: SKIN — CORRODED (LT AILERON) · airframe 90,002 hrs · 30,458 cycles

LEFT WING INBD AILERON UPPER SURFACE SHOWS CORROSION. LT INBD AILERON R & R IAW N00135 & MM 27-10-01-4.

Part: SKIN — WORN (RT WING TE FLAP) · airframe 90,002 hrs · 30,458 cycles

RIGHT INBD FLAP VANE LE WORN. REPAIRED IAW SRM 51-71-00 VOL II.

Part: VANE — DELAMINATED (TE FLAP) · airframe 90,002 hrs · 30,458 cycles

LEFT FLAP VANE LE INBD OF NR 3 TRACK HAS SMALL SECTION OF DELAMINATION. REPAIRED IAW SRM 51-71-00 VOL 2.

Part: SKIN — GOUGED (LE SLAT) · airframe 90,002 hrs · 30,458 cycles

LEFT WING NR 5 SLAT LOWER SURFACE HAS DEEP GOUGE BY NR 11 SLAT TRACK. REPAIRED IAW SRM 57-00-01 VOL1 FIG 4 SHEET 2.

Part: SKIN — DENTED (TE FLAP VANE) · airframe 90,002 hrs · 30,458 cycles

LEFT WING INBD FLAP VANE TOP SURFACE HAS SHARP DENT. REPAIRED IAW SRM 51-71-00 VOL 2.

Part: SKIN — DAMAGED (TE FLAP) · airframe 90,002 hrs · 30,458 cycles

RIGHT LOWER FLAP SURFACE SKIN HAS HAIL DAMAGE. FABRICATED DOUBLER IAW SRM 57-10-00 FIG 85 SHEET 2.

Part: DOUBLER — CRACKED (LT WING) · airframe 90,002 hrs · 30,458 cycles

LEFT WING FIXED LE INNER SKIN DOUBLER HAS APPROX 10 INCH CRACK AT STATION XORS 570. INSTALLED .020 TITANIUM DOUBLER IAW SRM 57-10-00 FIG 71 VOL 1.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 90,002 hrs · 30,458 cycles

AFT CARGO COMPARTMENT AT STATION 1781, BULKHEAD TO SKIN SHEAR TIE HAS EXFOLIATION CORROSION AT L48R. R & R SHEAR TIE IAW 51-30-00 VII.

Part: FLOOR SUPPORT — CRACKED (ZONE 100) · airframe 90,002 hrs · 30,458 cycles

LEFT CORNER OF FLOOR SUPPORT HAS A 1.25 INCH CRACK EMANATING FROM TOP FASTENER ON FRAME VERTICAL FWD FLANGE. PERFORMED REPAIR IAW SRM 53-30-00 FIG 7, VOL 1

Part: STRUT — CRACKED (NLG) · airframe 89,420 hrs · 30,134 cycles

FOUND NOSE GEAR LEAKING FLUID. INVESTIGATION FOUND ROUGHLY 15 INCH CRACK IN STRUT FROM TOP OF SERVICE POINT TO DOWN TO FRONT OF STRUT. INSTALLED SERVICEABLE NOSE LANDING GEAR ASSEMBLY IAW AMM 32-21-01-4. OPS & LEAK CHECKED GOOD.TAXIED AIRCRAFT PER JRH. NO DISCREPANCIES NOTED.

Part: MECHANISM — DIRTY (GEAR HANDLE) · airframe 89,312 hrs · 30,085 cycles

HAD 3 GEAR UNSAFE, AFTER 2 CYCLES OF GEAR HANDLE, RAN QRH. ON THIRD ATTEMPT GOT 3 GREEN. FOUND EXCESSIVE FRICTION IN THE LONGITUDINAL AXIS OF THE LG CONTROL LEVER. CLEANED & LUBRICATED THE LG CONTROL MECHANISM IAW MD-10-10 AMM 32-31-02-7.

Part: CONTROL UNIT — FAULTY (ANIT-SKID SYS) · airframe 89,188 hrs · 30,011 cycles

LEFT ANTI-SKID FAIL. CREW STATED DURING DEBRIEF ALERT APPEARED AT GEAR EXTENSION, DID GO AROUND & HAD NO ALERT ON THE SECOND GEAR EXTENSION. ASCU SHOWS ASCU FAULTED AT THE TIME OF THE FIRST GEAR EXTENSION. SYS TESTING NORMAL AT THE GATE WITH NO ALERTS. R & R ANTI-SKID CONTROL UNIT IAW MM 32-45-01-4. OPERATIONS CHECKED NORMAL IAW MM 2-45-00-2.

Part: SLEEVE — DAMAGED (THRUST REVERSER) · airframe 87,506 hrs · 29,126 cycles

ON TAXI, ADVISED BY THE TOWER THAT A PIECE OF OUR ENGINE COWL HAD FALLEN OFF. FOUND NR 2 ENGINE RT THRUST REVERSER COWL DAMAGED AND A LARGE SECTION MISSING. REMOVED NR 2 RT FAN REVERSER HALF IAW W/C 78T3101R-2. INSTALLED NR 2 ENGINE RT REVERSER HALF AND PERFORMED ALL REQUIRED OPS CHECKS IAW WC 78T3701R-2. ACFT OK FOR SERVICE.

Part: SKIN — MISREPAIRED (LT WING NR 6 SLA) · airframe 87,397 hrs · 29,063 cycles

LEFT WING NR 6 SLAT MISREPAIRED. REPAIRED IAW EA 8-5750-160700, REPAIR CLASSIFIED AS MAJOR.

Part: SKIN — CORRODED (RUDDER) · corrosion level 2 · airframe 87,189 hrs · 28,948 cycles

LOWER AFT RUDDER, FWD RT SIDE HAS AREA OF SURFACE CORROSION. REPAIRED LWR AFT RUDDER ON RT SIDE IAW SRM 55-10-00 AND EA 8-5540-157335.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 86,068 hrs · 28,366 cycles

ENTRY DOOR LIGHTED EMERGENCY EXIT SIGN HAS SEVERAL INOPERATIVE BULBS, DIM ILLUMINATION. RELAMPED THE LT EXIT LIGHT'S IAW SMP CHECKED OK.

Part: LIGHT — INOPERATIVE (SLIDE) · airframe 85,556 hrs · 28,090 cycles

WHILE DOING PREFLIGHT FOUND R1 DOOR SLIDE TEST LIGHT NOT WORKING. REPLACED SLIDE PACK LIGHT SW ASSY, SLIDE LIGHT OPS. GOOD, IAW AMM 25-61-03-2. (CLOSED)

Part: COALESCER BAG — DIRTY · airframe 84,734 hrs · 27,661 cycles

AT FL360, AFTER COCKPIT TEMP ADJUSTMENT-STRONG SMOKE ODOR FOLLOWED BY LARGE AMOUNT OF SMOKE IN COCKPIT. FOLLOWED QUICK REF HANDBOOK FOR SMOKE AND FUMES. EMERGENCY DECLARED AND LANDED. REF MM 21-53-00-7 & JRH C/W PACK BURN ON ALL 3 ACFT. PACKS WITH ENG BLEED AIR FROM ALL 3 ENGINES FOR OVER 60 MIN AND PACKS OPS NORMAL. NO ODOR PRESENT. R & R ALL 3 COALESCER BAGS IAW MM 21-54-03-2 AND AIR COND SYS TESTS NORMAL IAW MM 21-00-01-5 WITH ENG BLEED AIR. FINAL CLOSED.

Part: ANGLE — CORRODED (BS 1761 S51L) · corrosion level 2 · airframe 84,639 hrs · 27,602 cycles

CTR PIT SUMP DRAIN COMPT SHEAR TIE HAS CORROSION AT STA. 1761 APPROX. BETWEEN S- 51L TO S-51R. FOUND CORROSION OUT OF LIMITS AFTER BLENDING, REMOVED AND REPLACED SUPPORT ANGLE, SHEAR TIES IAW SRM 51-31-01, MAJOR REPAIR.

Part: SUPPORT — CORRODED (BS 1841) · corrosion level 2 · airframe 84,639 hrs · 27,602 cycles

AFT CARGO COMPT LOWER FRAME SUPPORT HAS CORROSION AT STA. 1841 BETWEEN S-49R AND S-50R. REMOVED AND REPLACED FRAME SUPPORT AT STA 1841 BETWEEN S-49R AND S-50R IAW SRM 51-21-01 AND SRM 53-01-00 , FIG. 8 MAJOR REPAIR.

Part: SHEAR TIE — CORRODED (BS 1781) · corrosion level 2 · airframe 84,639 hrs · 27,602 cycles

CENTER PIT SUMP DRAIN COMPT. SHEAR TIE IS CORRODED AT AFT SURFACE AT STA. 1781 BETWEEN S-47R TO S-48R. REMOVED AND REPLACED CENTER PIT SUMP DRAIN COMPT. SHEAR TIE IAW SRM 53-30-00, FIG. 10, MAJOR REPAIR.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 84,639 hrs · 27,602 cycles

UPPER CARGO COMPT SEAT TRACK LBL 107 FS 1701 TO 1841 HAS 4 EA LOBES WORN. FABRICATED SEAT TRACK, HAT AND SPLICE USING TRAVELER T10/844703 AND T10/84470544705 FROM MATERIALS 7075-T6511, 7075-T6 .050 AND 7075-T6 EXT. BATCH NUMBERS 0001665654, 0001610155 AND 0061221829 IAW SRM 53-70-00 AND SRM 51-20-00. REMOVED AND RELPACED SEAT TRACK IAW SRM 51-31-01. CLASSIFIED AS A MAJOR REPAIR.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 84,639 hrs · 27,602 cycles

UPPER CARGO SEAT TRACK FS 1731 TO 1721, LBL 28 HAS 2 LOBES PROTRUDING UPWARD AND ADDITIONAL LOBES DISTORTED. R & R DAMAGED SEAT TRACK SECTION AT LBL 28 FS 1721-1771 IAW SRM 51-31-01 AND SRM 53-70-00. CLASSIFIED AS A MAJOR REPAIR.

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 84,639 hrs · 27,602 cycles

MAIN DECK STA 475, LBL 77 TO 107, FLOORBEAM IS CRACKED/DAMAGED. FABRICATED FLOORBEAM SEC REPAIR FROM 7075-T6 .071 BATCH NR 183113 IAW SRM 53-00-01, FIG 9, SHEET 7. TREATED AND PRIMED REPAIR IAW SRM 51-21-01. INSTALLED REPAIR IAW SRM 51-31-01. PAINTED AREA IAW SRM 51-21-02. CLASSIFIED AS A MAJOR REPAIR.

Part: SENSOR — FAILED (N1) · airframe 83,437 hrs · 26,989 cycles

FLT 3707. NR 2 ENGINE ROLLED BACK ON TAKEOFF, MAX N1 WAS 84 PERCENT, ENGINE FAIL LIGHT ON. CKED VIA'S AND HAD NR 2 ENG N1 FAILED MSG -PROBABLE CAUSE ENG 2 TACHOMETER. REPLACED NR 2 ENG FAN SPEED SENSOR/N1 TACH PER AMM 77-11-01-2 OPS CKS NRML, RAN ENG TO T/O PWR PER JRH ALL IND NRML AND WITHIN LIMITS NOTE: NEW SENSOR FAILED AND WAS REPLACED WITH WRI 77-15 3467, HAS FLOWN GOOD WITH 2ND SENSOR.

Part: COALESCER BAG — ODOR (A/C PACKS) · airframe 83,373 hrs · 26,961 cycles

AFTER STARTING APU AND TURNING ON THE PACKS. HAD SMOKE COMING OUT OF DUCTS. R & R NR 3 PACK COALESCER BAGS, RAN APU, CLEARED FUMES FROM AIR CONDITIONING DUCTS. RAN NR 2 PACK IAW AMM AMM 21-00-01-5. NO SMOKE NOTED. RAN ALL 3 ENGINES AT HIGH POWER FOR 45 MINUTES IAW JRH. NO DEFECTS NOTED. R & R NR 2 PACK COALESCER BAG IAW 21-53-00-7.

Part: PLUG — LEAKING (HYD PUMP) · airframe 83,373 hrs · 26,961 cycles

WHEN APU WAS STARTED AND APU BLEED TURNED ON, CABIN FILLED WITH SMOKE, TURNED OFF BLEEDS FOUND HYD FLUID RUNNING FROM AFT DRAIN HOLE INTO APU INLET. FOUND REV MOTOR PUMP S/O VALVE M1-165 DRIPPING IN AFT COMPT PN 148995, AIPC 29-12-60-03, FACT 10SEP09 06:58, EWR. FOUND PLUG ON NON REV HYD MOTOR PUMP S/O VALVE LEAKING. REPLACED PACKING ON PLUG. LEAK CK GOOD. REF IPC 29-22-05-05, AND MM 27-26-03-2.

Part: WARNING LIGHT — FALSE ACTIVATION (MLG) · airframe 83,153 hrs · 26,842 cycles

GEAR UNSAFE WARNING DURING GEAR EXTENSION. GA PROCEDURE. ACCOMPLISHED QRH PROCEDURE ACCOMPLISHED WITH NORMAL GEAR EXTENSION - LEFT MAIN. NO CURRENT FAULTS LOGGED, CHECKED RIGGING IN PSEU AND SENSORS ARE WITHIN LIMITS PER AMM 32-61-15-5. PERFOMED R-T-S AND PASSED. CHECKED GAP RIG AT THE DOWNLOCK SENSER AND IS WITHIN LIMITS PER AMM 32-61-15-4. AIRCRAFT OK FOR SERVICE.

Part: PANEL — DAMAGED (NR 2 NACELLE) · airframe 81,889 hrs · 26,187 cycles

NR 2 PYLON APRON HAS EDGE DAMAGE AT THE FWD END WHERE THE LT FAN COWL MATES. REPAIRED NR 2 FAN COWL LT APRON IAW E.A. 8-5480-123629.

Part: VANE — DELAMINATED (TE FLAP) · airframe 81,889 hrs · 26,187 cycles

LEFT OUTBOARD FLAP VANE; INBOARD LOWER SKIN IS DELAMINATED. REMOVED DELAMINATED INBOARD LOWER SKIN ON LEFT OUTBOARD FLAP VANE INBOARD END. FABRICATED SKIN PLUG & REPAIR DOUBLER. PREPPED FOR BONDING; HOT BONDED REPAIR. ALODINED AREA & EDGE SEALED DOUBLER; PRIMED PER DC/MD-10 SRM 51-71-00; VOL II. PAINTED PER DC/MD-10 SRM 51-21-01; VOL II. REMOVED & RE-INSTALLED LEFT WING OUTBOARD FLAP VANE ASSEMBLY IAW MD-10-10 AMM 27-50-03-2.

Part: SKIN — CRACKED (NR 1 SLAT) · airframe 81,889 hrs · 26,187 cycles

RIGHT NR 1 SLAT LOWER SURFACE SKIN IS CRACKED AT A FASTENER HOLE, TRAILING EDGE APPROX 1 INCH FROM THE INBD END. REMOVED RIGHT WING NR 1 SLAT IAW AMM 27-80-01-4. OPENED SKIN FOR ACCESS. REMOVED THE CRACKED SECTION. FABRICATED A REPAIR, INSTALLED REPAIR AND RE-INSTALLED SKIN IAW SRM 57-10-00; FIG 30 AND SRM 51-35-01, VOL II. ALODINED AND PRIMED THE REPAIR IAW SRM 51-21-01; VOL II. RE-INSTALLED, AND ACCOMPLISHED GAP AND OPS CHECKS FOR THE RIGHT WING NR 1 SLAT IAW AMM 27-80-01-4.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 81,889 hrs · 26,187 cycles

FRAME P/N AEA 0273-3 REQUIRES FABRICATION DUE TO EXISTING FRAME BEING CORRODED BEYOND LIMITS AT STA 1501. FABRICATED A NEW FRAME SECTION AND SHEAR TIE IAW DAC DWG AEA 0273; REV "G". LOCATED AND DRILLED AEA 0273-3 FRAME AND AEA 0273-5 SHEAR TIE. ALODINED AND PRIMED IAW SRM 51-21-01; PGS 21 AND 24; VOL II. APPLIED TOP COAT OF PAINT IAW SRM 51-21-02; PG 1; VOL II. PART MARKED NEW PARTS IAW FEDEX GMM 7-0-1001. FRAME SECTION REMOVED AND INSTALLED ON SNRM N00567.

Part: LONGERON — CORRODED (ZONE 100) · corrosion level 2 · airframe 81,889 hrs · 26,187 cycles

LONGERON 51 L RIGHT END FITTING AT STA 1521 IS CORRODED. FABRICATED 1 LONGERON 51 L END FITTING P/N AYB 7020-2 IAW DWG NR AYB 7020.

Part: LONGERON — CORRODED (ZONE 100) · corrosion level 2 · airframe 81,889 hrs · 26,187 cycles

LONGERON 51 L LEFT END FITTING AT STA 1521 IS CORRODED. FABRICATED 1 LONGERON END FITTING P/N AYB 7020-2 IAW BAC DWG NR AYB7020.

Part: LONGERON — CORRODED (ZONE 100) · corrosion level 2 · airframe 81,889 hrs · 26,187 cycles

LONGERON 52 AT STA 1480 IN THE CENTER LANDING GEAR COMPARTMENT HAS CORROSION. REMOVED DAMAGED SECTION OF LONGERON 52 IAW SRM 51-33-01; PG 1; VOL II. LOCATED AND DRILLED NEW SECTION OF LONGERON 52 AND 2 SPLICES IAW DWG AYB 7013 AND SRM 53-00-01; FIG 9; PG 32; VOL I. ALODINED AND PRIMED NEW SECTION OF THE LONGERON AND 2 SPLICES IAW SRM 51-21-01; PGS 21 7 24; VOL II. APPLIED TOP COAT OF PAINT IAW SRM 51-21-01; PG 1; VOL II. PART MARKED NEW LONGERON FX AYB 7013-1 IAW GMM 7-0-1001. INSTALLED NEW SECTION OF LONGERON AND 2 SPLICES IAW SRM 51-33-01; PG 1; VOL II AND SRM 53-00-01, FIG 32; VOL I.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 81,889 hrs · 26,187 cycles

FRAME P/N AEA 0273-3 REQUIRES FABRICATION DUE TO BEING CORRODED BEYOND LIMITS. FABRICATED A NEW FRAME SECTION AND SHEAR TIE IAW DWG AEA 0273; REV "G". LOCATED AND DRILLED AEA 0273-3 FRAME AND AEA 0273-5 SHEAR TIE. ALODINED AND PRIMED IAW SRM 51-21-01; PGS 21 AND 24; VOL II. APPLIED TOP COAT OF PAINT IAW SRM 51-21-02; PG 1; VOL II. PART MARKED NEW PARTS IAW GMM 7-0-1001. FRAME SECTION REMOVED AND INSTALLED ON SNRM N00567.

Part: BULKHEAD — CORRODED (MLG WW) · corrosion level 2 · airframe 81,889 hrs · 26,187 cycles

THE CENTER WHEEL WELL SKIN HAS VARIOUS AREAS OF CORROSION FROM STA 1521 THRU 1380; BETWEEN LONGERON 51L TO LONGERON 51R. REPAIRED THE CENTER WHEEL WELL SKIN IAW FEDEX EA 8-5330-117008 " FUSELAGE, UNDER WING BARREL BELLY SKIN CORROSION, REPAIR". REMOVED AND REPLACED LONGERONS L-52 AND L-51L; INTERCOSTALS AT STA 1501 - 1521 AND THE LONGERON END FITTINGS IAW DC/MD-10 SRM 51-31-01; VOL II AND SRM 51-33-01; VOL II. ALODINED; PRIMED AND PAINTED IAW DC/MD-10 SRM 51-21-01; VOL II.

Part: SKIN — CRACKED (ZONE 200) · airframe 81,889 hrs · 26,187 cycles

RIGHT SIDE FUSELAGE SKIN AT STA 322 IS CRACKED 10 INCHES ABOVE THE FINGER DOUBLERS. REMOVED FIRST OFFICERS SEAT IAW AMM 25-11-01-4. REMOVED DAMAGE AND FABRICATED A REPAIR IAW SRM 53-20-00; FIG 6; VOL I. ALODINED AND PRIMED IAW SRM 51-21-01; VOL II. INSTALLED THE REPAIR IAW SRM 53-20-00; VOL II; FIG 6. INSTALLED FIRST OFFICERS SEAT IAW AMM 25-11-01-4; OPS CHECK FOUND TO BE GOOD IAW AMM 25-11-01-4.

Part: LONGERON — CORRODED (ZONE 100) · corrosion level 2 · airframe 81,889 hrs · 26,187 cycles

CORROSION ON LONGERON 51L FROM BODY STA 1441 TO 1461. REMOVED DAMAGED SECTION OF LONGERON 51L FROM FS 1430 TO 1520 IAW SRM 51-33-01; PG 1; VOL II. LOCATED AND DRILLED NEW SECTION OF LONGERON 51L AND 2 EA SPLICES IAW DWG AYB 7013 AND SRM 53-00-01; FIG 9; PG 32; VOL I. ALODINED AND PRIMER NEW SECTION OF LONGERON AND 2 SPLICES IAW SRM 51-21-01; PGS 21 AND 24; VOL II. APPLIED TOP COAT OF PAINT IAW SRM 51-21-02; PG 1; VOL II. PART MARKED NW LONGERON FX AYB 7013-1IAW GMM 7-0-1001. INSTALLED NEW SECTION OF LONGERON AND SPLICES IAW SRM 51-33-01; PG 1; VOL II AND SRM 53-00-01; FIG 9; PG 32; VOL I.

Part: SKIN — CORRODED (LT AILERON) · corrosion level 2 · airframe 81,889 hrs · 26,187 cycles

LEFT OUTBD AILERON LOWER SKIN IS CORRODED/BULGED AROUND THE HINGE FITTING. LEFT WING OUTBD AILERON WAS REPLACED ON SNRM N00728. CORROSION WAS FOUND TO BE OUT OF LIMITS.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 81,889 hrs · 26,187 cycles

LEFT EXTERNAL FUSELAGE SKIN IS BULGED AT FS 1123; LONGERON 46L. REPAIRED SKIN IAW EA NR 8-5330-117009.

Part: DOOR FRAME — CORRODED (ZONE 100) · airframe 81,889 hrs · 26,187 cycles

THE MAIN CARGO DOOR JAMB HAS A CRACK INDICATION AT FITTING NR 7; HOLE "B". REMOVED AND REPLACED THE NR 7 LOWER FITTING, CARGO DOOR LATCH SPOOL P/N AFA 7132-1 AT STA 757L LBL 112 IN REF TO SRM 51-33-01; VOL II, PG 1. INSTALLED REPAIR BUSHING FREEZE PLUG IN HOLE B OF LOWER JAMB UPPER AND LOWER BEAMS AT SAT 757L LBL 112 IN REF TO SRM 53-50-00; VOL I; FIG 17.

Part: STRINGER — GOUGED (ZONE 100) · airframe 81,889 hrs · 26,187 cycles

FWD CARGO COMP LONGERON 52 AT STA 1026 IS MISSING FASTENERS AND IS GOUGED IN THE RADIUS. INSTALLED REPAIR CHANNEL AND REPLACED MISSING FASTENERS IN REFERENCE TO DC/MD-10 SRM 53-10-00; FIG 2-A; VOL I.

Part: STRUCTURE — CORRODED (LT AILERON) · corrosion level 2 · airframe 81,889 hrs · 26,187 cycles

LEFT OUTBD AILERON IS BULDGING AROUND THE RIB ATTACH FASTENERS AT XOA 960. LEFT WING OUTBD AILERON WAS REPLACED ON SNRM N00728. CORROSION WAS FOUND TO BE OUT OF LIMITS.

Part: LONGERON — CORRODED (ZONE 100) · corrosion level 2 · airframe 81,889 hrs · 26,187 cycles

NR 1 AIR CONDITIONING COMP FUSELAGE SKIN, ANGLES; INTERCOSTAL WEB AND FASTENERS ARE CORRODED BETWEEN STA 562 AND STA 593; LONGERON 43L IMMEDIATELY OUTBOARD OF THE EXHAUST BOX. REPLACED CORRODED THROUGH LONGERON SECTION ACA 3353-3 LEFT BY SPLICING IN A NEW PIECE AT STA 561-593 IN REF TO DC/MD-10 SRM 53-00-01; FIG 7 AND EA 8-5310-117022 "FUSELAGE, A/C BAY LONGERON CORROSION AT STA 561-578 - REPAIR". CLEANED SKIN AND INTERCOSTAL AND UPON FURTHER EVALUATION FOUND NO CORROSION PRESENT. ALODINED AND PRIMED ALL BARE METAL IN REF TO DC/MD-10 SRM 51-21-01; VOL II; PGS 9; 21 AND 24. REPLACED 2 CORRODED CLIPS AND CORRODED HARDWARE IN REF TO DAC DWG ACA 3816 AND SRM 51-31-01; VOL II; .

Part: SKIN — DAMAGED (ZONE 100) · airframe 81,889 hrs · 26,187 cycles

LEFT LOWER FUSELAGE SKIN IS BULGED AT FS 1113, LONGERON 45L. REPAIRED THE SKIN IN REFERENCE WITH DC/MD-10 SRM 53-20-00; VOL I; FIGURE 6; SHEET 7.

Part: SKIN — DENTED (ZONE 100) · airframe 81,889 hrs · 26,187 cycles

THE LOWER FUSELAGE SKIN IS DENTED AT FS 1682, LONGERON 44L. REPAIRED AREA AT STA 1682, LONGERON 44L IN REFERENCE TO SRM 53-20-00; VOL I; FIG 6.

Part: SPAR — SHEARED (ZONE 400) · airframe 81,889 hrs · 26,187 cycles

THE NR 3 PYLON STA YN 417, UPPER SPAR WEB AT THE BULKHEAD HAS 1 SHEARED FASTENER. REPLACED FASTENER IAW MD-10-10 AMM 20-50-02-2. PERFORMED BHEC TEST ON THE NR 3 PYLON UPPER SPAR WEB AT THE BULKHEAD IAW STSPM 06-10-01.003. NO DEFECTS NOTED.

Part: SPAR — WORN (ZONE 400) · airframe 81,889 hrs · 26,187 cycles

THE NR 3 PYLON UPPER SPAR OUTBD AND INBD SPAR ANGLES HAVE 3 BOLTS; FWD TO AFT; BOTH SIDES LOOSE AND 7 FROM INBD TO OUTBD ARE LOOSE ON THE UPPER WEB AT PYLON STA YN 358. COMPLIED WITH FEDEX EA 8-5450-123625.

Part: ANGLE — LOOSE (ZONE 400) · airframe 81,889 hrs · 26,187 cycles

THE NR 3 PYLON AFT BULKHEAD TO SPAR ANGLE, INBD AND OUTBD SIDES HAS 1 EA BOLT PER SIDE LOOSE AT PYLON STA YN 417. REMOVED AND REPLACED 2 EA FASTENER IAW DC/MD-10 SRM 51-31-01; VOL II AND TORQUED IAW DC/MD-10 AMM 20-30-02-2. PERFORMED HFEC EDDY CURRENT INSPECTION. NO CRACKS NOTED.

Part: STRUCTURE — CORRODED (ZONE 100) · airframe 79,329 hrs · 24,858 cycles

CTR WING LWR BARREL STA 1216 LONGERON 48 REWORK OF CORROSION 40 PERCENT. MATERIAL LOSS TO STANDING LEG. CUT OUT CORRODED SECTION OF LONGERON IAW SRM 53-00-01 FIG 7 VOL I GN 16.

Part: FLANGE — CORRODED (ZONE 100) · airframe 79,329 hrs · 24,858 cycles

CTR WING LWR BARREL AT STA 1216 REWORK TO STR 47 BASE FLANGE TO REMOVE CORROSION MATERIAL PLUS 50 PERCENT. REPAIRED LONGERON IAW SRM 53-00-01 FIG 9 VOL I.

Part: SKIN — UNKNOWN (ZONE 100) · airframe 79,329 hrs · 24,858 cycles

FOUND REPAIR AT STA 1159 - 1139 LONGERON 41-48 RT. REPAIRED IAW FEDEX 8-5330-84091A.

Part: BEAM — DAMAGED (CARGO BAY) · airframe 79,329 hrs · 24,858 cycles

FWD CARGO COMPT LT SIDE ON BEAM AT STA 1099 FOUND SPLICE REPAIR WITH NEW SECTION FROM INB'D TO OUT'B AT X=46 Z=-100. REPAIR IAW EA 8-5310-87665.

Part: DOOR FRAME — DAMAGED (CARGO BAY) · airframe 79,329 hrs · 24,858 cycles

AFT CARGO COMPT LOWER SIDE DOOR JAMB STA 1821 FOUND DOUBLER REPAIR ON WEB. REPLACED REPAIR BY NEW DOUBLER IAW SRM 53-50-00 FIG 12 VOL 1 AND EA 8-5310-87666.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 79,329 hrs · 24,858 cycles

RT WING DROP L/E XW=332 EXISTING FLUSH REPAIR DOUBLER ON EXT SKIN. REMOVED OLD REPAIR AND INSTALL NEW REPAIR IAW SRM 57-10-00 FIG 39 VOL 1.

Part: SKIN — DAMAGED (LT WING) · airframe 79,329 hrs · 24,858 cycles

LT WING UPPER SIDE INTERNAL L/E XORS=778 EXISTING REPAIR DOUBLER ON EXT SKIN. REMOVED AND REPLACE EXISTING REPAIR WITH NEW ONE IAW SRM 57-10-00 FIGURE 68 VOL 1.

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 79,329 hrs · 24,858 cycles

RIGHT STAB I/B ELEV XE 61.875 EXISTING 1EA EXT REPAIR DOUBLER ON UPPER DETACHABLE SKIN. REPLACED REPAIR PER SRM 55-00-01 VOL 1 FIG 3 SHT 2 AND SRM 55-00-01 PG 2A, 2B VOL 1.

Part: FRAME — CORRODED (CARGO DOOR) · airframe 79,329 hrs · 24,858 cycles

CTR CARGO COMPT STA 1710 X=-65 JAMB DOOR FWD, AFTER REMOVED RAIL FOUND SEVERE CORROSION WITH EXFOLIATION. REMOVED CORROSION PER SRM 53-00-01 VOL 1 FIG 1B AND REPLACED FRAME PER SRM 51-32-01 PG 59/68, SRM 51-35-01 PG 1/13, SRM 51-33-01 PG 34/47 VOL 2 AND DWG AFAQ3873.

Part: LONGERON — BROKEN (ZONE 100) · airframe 79,329 hrs · 24,858 cycles

CTR CARGO COMPT BILGE AREA ON STA 1671 RT SIDE LONGERON SPLICE BROKEN 6 INCHES LONG ON L44. REPAIR FRAME CAP BETWEEN L45-46 RT IAW SRM 53-30-00 FIG 5 VOL 1 AND REPLACED LONGERON IAW DWG NFA6074.

Part: STIFFENER — DAMAGED (ZONE 100) · airframe 79,329 hrs · 24,858 cycles

AFT CARGO COMPT BILGE AREA RT SIDE ON L49 ONE EXISTING SPLICE ON STIFFENER AT STA 1781 TO 1801. REPAIR PER SRM 53-10-00 FIG 2A SHT 1-3 VOL 1.

Part: SHEAR TIE — CRACKED (ZONE 600) · airframe 79,329 hrs · 24,858 cycles

RT WING XORS 130 ABOVE STR 36 BEHIND A LOWER PIPE SUPPORT BRACKET THE BULKHEAD WEB HAS A 1.250" CRACK LONG. REPAIR IAW SRM 57-00-01 FIG 12 SHT 4 VOL 1.

Part: SKIN — DAMAGED (ZONE 100) · airframe 79,329 hrs · 24,858 cycles

LWR FUSELAGE AT STA 1781 BETWEEN L38-41 RT EXISTING TWO EXTERNAL REPAIR DOUBLER ON SKIN. INSTALLED REPAIR DOUBLER PER SRM 53-50-00 FIG 26 VOL 1.

Part: ANGLE — CRACKED · airframe 79,329 hrs · 24,858 cycles

PERFORMED PENETRANT INSPECTION ON LT LWR CAP ANGLE AT STA 2122.881 FOUND 2 INCH CRACK LONG. REPAIRED ANGLE IAW SRM 53-40-00 FIG 6 PG 25 VOL 1.

Part: SKIN — DAMAGED (ZONE 600) · airframe 79,329 hrs · 24,858 cycles

RIGHT WING SLAT 6 CENTRAL TRACK EXISTING EXTERNAL REPAIR DOUBLER ON LWR SKIN. REPAIR PER SRM 57-10-00 FIG 31 VOL 1.

Part: CHANNEL — DAMAGED (ZONE 100) · airframe 79,329 hrs · 24,858 cycles

FWD CARGO COMPT RT SIDE ON CHANNEL AT X=-58 FOUND AN EXISTING SPLICE REPAIR Y=1019 Z=-100. REPAIR PER SRM 53-70-00 FIG 8, SHEET 1-3 VOL 1.

Part: PRESSURE PANEL — CRACKED (ZONE 100) · airframe 79,329 hrs · 24,858 cycles

ON STA 1510 CTR W/W ON WEB X=31.5 Z=-36 FOUND CRACK 1,75". REPAIR PER SRM 53-00-01 FIG 10 SHEET 5, 6, 7 VOL 1.

Part: SKIN — DAMAGED (ZONE 600) · airframe 79,329 hrs · 24,858 cycles

RIGHT WING T/E OUTBOARD FLAP I/B HINGE XORS 562 EXISTING EXTERNAL REPAIR DOUBLER ON LWR SKIN. REPAIR PER SRM 57-00-01 FIG 4 SHEET 2 VOL 1.

Part: SKIN — DAMAGED (TE FLAP) · airframe 79,329 hrs · 24,858 cycles

LEFT WING O/B FLAP XOF 513 EXT REPAIR DOUBLER ON LWR SKIN. REPLACE REPAIR PER SRM 57-10-00 FIG 85 VOL 1.

Part: FRAME — CRACKED (RT DROOP) · airframe 79,329 hrs · 24,858 cycles

RIGHT DROOP L/E INTERNAL SIDE FOUND CRACKED FORMER ON UPPER EDGE AT XORS 299. REPAIR PER SRM 53-00-01 FIG 8 SHEET 1, 3, 4.

Part: SKIN — DAMAGED (LT WING) · airframe 79,329 hrs · 24,858 cycles

LEFT WING XOS UPPER EXT L/E SIDE, EXISTING REPAIR DOUBLER ON SKIN. REMOVED SLAT TRACK DOOR AND REMOVED AND REPLACED AND REINSTALLED TRACK SLAT DOOR IAW MM 57-21-01-2, SRM 51-35-02 VOL 2 AND SRM 57-10-00 FIG 68 VOL 1.

Part: SKIN — DAMAGED (RT WING) · airframe 79,329 hrs · 24,858 cycles

RIGHT WING XORS 506 L/E TRACK NR 8 EXISTING 1EA EXT REPAIR DOUBLER ON SKIN. REPLACED REPAIR PER SRM 57-10-00 FIG 68 SHT 1-3 VOL 1.

Part: BEAM — DAMAGED (CARGO BAY) · airframe 79,329 hrs · 24,858 cycles

CTR CARGO COMPT ON BEAM AT STA 1701 RT SIDE FOUND OLD REPAIR AT X=-38 BROKEN. REPLACED BEAM PER DWG AFA0043-3 AND SRM 51-33-01 PG 34/47 AND SRM 51-35-01 PG 1/13.

Part: CHANNEL — DAMAGED (ZONE 100) · airframe 79,329 hrs · 24,858 cycles

FWD CARGO COMPT LT SIDE ON CHANNEL AT STA 999 , X=28, Z=-100 FOUND 1EA SPLICE REPAIR. REPAIR PER SRM 53-70-00 FIG 7 SHEET 3, 6 VOL 1.

Part: STRUCTURE — CORRODED (ZONE 100) · airframe 79,329 hrs · 24,858 cycles

LWR FUSELAGE LT SIDE AIR CONDITION COMPT ON INLET EXHAUST VALVE SYS NR 2 DOUBLER WITH CORROSION AT Y=515 LONGERON 46. REMOVED CORROSION PER SRM 51-21-001 VOL 2 PAR 34 AND REPAIRED PER SRM 53-20-00 FIG 2 VOL 1.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 79,329 hrs · 24,858 cycles

UPPER FUSELAGE STA 265 UPPER FWD PRESSURE BULKHEAD EXISTING 1EA REPAIR DOUBLER ON EXTERNAL SKIN. REPAIR PER SRM 53-00-01 VOL 1 FIG 4 SHEET 2.

Part: SKIN — DAMAGED (LT STAB) · airframe 79,329 hrs · 24,858 cycles

LT STAB, XE 101 I/B ELEV, EXISTING 1 EXT REPAIR DOUBLER ON UPPER SKIN. REPLACE REPAIR PER SRM 55-00-01 VOL 1 SHT 2A, 2B FIG 3 SHT 2.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 79,329 hrs · 24,858 cycles

ON EXTERNAL SKIN AT STA 1139 LONGERON 47-48 LT SIDE FOUND TWO RIVETS LOOSE. REPAIR SKIN IAW EA 8-5330-84901A PT 2.

Part: BULKHEAD — DAMAGED (ZONE 600) · airframe 79,329 hrs · 24,858 cycles

RIGHT WING XORS 372 FWD OF STR 12 BULKHEAD CAP CRACKED BETWEEN FASTENERS. REPAIR PER EA 8-5710-84863.

Part: ACCESS PANEL — DAMAGED (ZONE 500) · airframe 79,329 hrs · 24,858 cycles

LEFT WING ACCESS PANEL PRESSURE REFUEL AREA AT XOS 611 EXISTING EXTERNAL REPAIR DOUBLER ON SKIN. REPAIR IAW SRM 57-10-00 FIG 68 VOL 1.

Part: BEAM — DAMAGED (ZONE 100) · airframe 79,329 hrs · 24,858 cycles

FWD CARGO COMPT RIGHT SIDE STA 1099 FOUND EXISTING SPLICE REPAIR WITH NEW SECTION OF BEAM X=-46 Z=-100. REPAIR PER SRM 53-60-01 FIG 3 VOL 1.

Part: LONGERON — CRACKED (CARGO BAY) · airframe 79,329 hrs · 24,858 cycles

CTR CARGO COMPT ON STA 1521 X=-50 RT SIDE 1EA CRACK LONG 10" ON EXISTING REPAIR AT Z=97.350. REPLACE TEE LONGERON IAW SRM 51-35-01 PG 1-13 VOL 2 AND DWG AEA0344 AND SRM 51-33-01 PG 34-47 VOL 2.

Part: ANGLE — DAMAGED (LT WING) · airframe 79,329 hrs · 24,858 cycles

LEFT WING FWD INT L/E XOS 667 EXISTING REPAIR ANGLE ON INTERNAL STIFFENER. REPAIR IS IN COMPLIANCE WITH SRM 51-00-01 FIG 100 VOL 1.

Part: ANGLE — DAMAGED (ZONE 500) · airframe 79,329 hrs · 24,858 cycles

LT WING SLAT 2 XDLE 309 EXISTING REPAIR ANGLE ON CLOSURE ANGLE. REPLACE REPAIR PER SRM 57-00-01 FIG 10 VOL 1.

Part: SKIN — DAMAGED (NR 1 SLAT) · airframe 79,329 hrs · 24,858 cycles

RIGHT WING, SLAT NR 1, EXT TRACK FITTING, ONE EXT REPAIR DOUBLER ON LWR SKIN. REPAIR PER SRM 57-10-01 FIG 4 SHT 2 VOL 1, SRM 51-35-02 VOL 2 PG 3/9.

Part: SKIN — DAMAGED (ZONE 500) · airframe 79,329 hrs · 24,858 cycles

LEFT WING DROOP L/E FLUSH REPAIR SKIN ON EXTERNAL SKIN. REPLACED OLD REPAIR PER SRM 57-00-01 FIG 4 VOL 1 SHEET 2.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 79,329 hrs · 24,858 cycles

RT SIDE AT STA 1119 FROM L NR 44 TO 50 FOUND 1EA NEW FRAME ABOUT 33 INCHES LONG WITH TWO SPLICE ANGLES. ACCOMPLISH REPAIR PER EA 8-5310-87669.

Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 79,329 hrs · 24,858 cycles

AT STA 919, X=58, Z=-97 AFTER REMOVED OLD CHANNEL WITH NRC N01214, FOUND FLOORBEAM DAMAGED ON OLD REPAIR. REPAIR BEAM PER SRM 53-60-01 VOL 1 FIG 3.

Part: RIB — CRACKED (ZONE 600) · airframe 79,329 hrs · 24,858 cycles

SLAT 2 R O/B SIDE ON RIB FOUND 1EA CRACK 2" LONG. REPAIR PER SRM 57-00-01 VOL 1 FIG 10 SHT 2 AND SRM 51-35-01 PAR 1-5 VOL 2.

Part: SKIN — DAMAGED (NR 1 SLAT) · airframe 79,329 hrs · 24,858 cycles

RIGHT WING SLAT NR 1 XCW 118 EXISTING 1 EA REPAIR DOUBLER ON UPPER SKIN. REPLACED REPAIR PER SRM 57-10-00 FIG 84 SHEET 2 VOL 1.

Part: ACCESS PANEL — DAMAGED (ZONE 500) · airframe 79,329 hrs · 24,858 cycles

LEFT WING ACCESS PANEL SLAT DRIVE MECHANISM LOWER EXTERNAL L/E XOS 487 EXISTING EXTERNAL REPAIR DOUBLER ON SKIN. REPAIR PER SRM 57-10-00 FIG 68 VOL 1.

Part: SKIN — DAMAGED (ZONE 500) · airframe 79,329 hrs · 24,858 cycles

LT WING SLAT 2 XORS 231 EXISTING FLUSH REPAIR DOUBLER ON LWR SKIN. REPAIR PER SRM 57-10-00 FIG 29 VOL 1.

Part: SKIN — DAMAGED (ZONE 100) · airframe 79,329 hrs · 24,858 cycles

AFTER CARGO DOOR STA 1791 EXTERNAL SKIN EXISTING 1EA REPAIR DOUBLER ON LWR FWD CORNER. REPAIR PER SRM 52-10-00 FIG 17 VOL 1.

Part: SHEAR TIE — CORRODED (FS 1741) · airframe 79,329 hrs · 24,858 cycles

CTR CARGO COMPT BILGE FOUND CORROSION ON SHEAR CLIP AT STA 1741 FROM STR 52 TO 51 LT. REMOVED CORROSION PER SRM 51-21-01 VOL 2 PAGE 28. TREATED AREA PER SRM 51-21-01 PG 21-24-25 VOL 2. REPAIRED SHEAR CLIP PER SRM 53-30-00 VOL 1 FIG 10, SRM 51-35-01 PG 1/13 AND SRM 51-33-01 PG 34-47 VOL 2.

Part: SKIN — DAMAGED (ZONE 500) · airframe 79,329 hrs · 24,858 cycles

LEFT WING SLAT 1 XORS 130 EXISTING FLUSH REPAIR DOUBLER ON LWR SKIN. ACCOMPLISH EA 8-5710-84123.

Part: CAP — CRACKED (ZONE 500) · airframe 79,329 hrs · 24,858 cycles

LT WING XORS 402 BULKHEAD CAP CRACKED FWD OF STR 15. REPAIR IAW EA 8-5710-84859.