N373FE

Part: FAIRING — SEPARATED (LT PYLON) · airframe 921 hrs · 39,172 cycles

ELP MX REPORTED PART FOUND ON RUNWAY AFTER TAKEOFF. INSPECTED ACFT FOUND THE NR 2 ENG LT SIDE TAIL PYLON & FAN DUCT RAMP FAIRING. IPC 54-22-15-01 ITEM 720, MISSING. COMPLIED WITH PART 3 OF EA 8-5481-T0321869. REPLACED RAMP PANEL IAW SRM.

Part: LIGHT — INOPERATIVE (L1 DOOR) · airframe 910 hrs · 38,506 cycles

L1 DOOR SLIDE FAILS PRESS TO TEST. RELAMPED L1 DOOR EMER ESCAPE SLIDE PRESSURE, PRESS TO TEST, INDICATOR LAMP AS REQUIRED. OPERATIONS CHECKED NORMAL IAW AMM 25-61-03-05.

Part: WIRE HARNESS — DAMAGED (NR 1 EGT) · airframe 90,847 hrs · 38,382 cycles

DURING INITIAL CLIMB, NR 1 ENGINE EXCEEDED 1051 DEGREES EGT. NO FIRE INDICATIONS, NO ABNORMAL AIRFRAME MOVEMENTS. RAN QRH SHUTDOWN THE ENGINE. TROUBLESHOT IAW SMP AND FOUND HIGH RESISTANCE DURING HARNESS. SHAKE TEST ON UPPER ENGINE EGT HARNESS , REPLACED UPPER EGT HARNESS AND NOW READS WITHIN LIMITS WITH NO FLUCTUATION. COMPLETED HIGH POWER ENGINE RUN WITH NO ABNORMAL EGT READINGS OR FLUCTUATIONS IAW AMM MD-10 77-21-01-2.

Part: ATTACH ANGLE — CRACKED (RT WING) · airframe 90,620 hrs · 38,273 cycles

DURING HIGH FREQUENCY EDDY CURRENT INSPECTION, FOUND A CRACK AT RT WING STRINGER BUTTERFLY CLIP AT XORS 402 STRINGER 39, APPROX 0.5 INCHES IN LENGTH. REMOVED AND REPLACED WITH NEW ATTACH ANGLE IAW SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 90,620 hrs · 38,273 cycles

RIGHT WING INBD FLAP ASSEMBLY AFT HINGE OTBD PIVOT BORE HAS SURFACE CORROSION. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57- 52-01. REPAIRED PER EA 8-5750-T0312232 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SUPPORT FITTING — CORRODED (BS 1361) · corrosion level 2 · airframe 90,620 hrs · 38,273 cycles

AFTER REMOVAL OF CENTER WING TANK, TOP SURFACE SUPPORT FITTING FOUND CORRODED BS 1361 X = 31. SUPPORT FITTING REMOVED AND REPLACED IAW SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SKIN — CRACKED (LT WING LE) · airframe 90,620 hrs · 38,273 cycles

LEFT WING DROOP LE AFT SURFACE FOUND CRACKED. REPAIRED IAW SRM 57-10-00 FIGURE 55 VOLUME I. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FLOORBEAM — CORRODED (BS 959) · corrosion level 2 · airframe 90,620 hrs · 38,273 cycles

FORWARD CARGO BAY SUMP AREA BS 959 RBL 7 FLOORBEAM FOUND CORRODED. FLOORBEAM REMOVED AND REPLACED IAW SRM 51-31-01 VOLUME II. FLOORBEAM REWORKED IAW DRAWING ADA0035 REVISION E. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: ATTACH FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,620 hrs · 38,273 cycles

LEFT WHEEL WELL FWD BULKHEAD PANEL INBD ATTACHMENT FITTING FOUND CORRODED. FITTING REMOVED AND REPLACED IAW SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 90,620 hrs · 38,273 cycles

RIGHT WING LE BEADED DOUBLER AT XOS 908 FOUND CRACKED. REPAIRED IAW SRM 57-10-00 FIGURE 71 VOLUME I. REPAIR CLASIFIED MAJOR IAW GMM 6-2-100.

Part: SKIN — CHAFED (LT WING LE) · airframe 90,620 hrs · 38,273 cycles

RIGHT WING DROP LE OTBD UPPER SURFACE AT XDLE 328 FOUND WITH CHAFED. REPAIRED IAW SRM 57-10-00 FIGURE 97 VOLUME I. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING TE FLAP) · airframe 90,620 hrs · 38,273 cycles

RIGHT WING INBD FLAP ASSEMBLY, ENCLOSURE AREA SIDE LOAD FITTING CUT OUT DOUBLER CRACKED. REPAIRED IAW EA 8-5340-T0312333 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FORMER — CRACKED (RT WING) · airframe 90,620 hrs · 38,273 cycles

RIGHT WING LE COMPARTMENT FIXED LE RIB ATTACHED FORMER AT XOS 584 FOUND CRACKED. CRACKED FORMER REMOVED AND REPLACED IAW DRAWING ARB1162 REVISION S AND SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 90,620 hrs · 38,273 cycles

RIGHT WING LE BEADED DOUBLER AT STATION XOS 665 FOUND CRACKED. REPAIRED IAW SRM 57-10-00 FIGURE 71 VOLUME I. REPAIR CLASIFIED MAJOR IAW GMM 6-2-100.

Part: TEE FITTING — CORRODED (BULKHEAD) · airframe 90,620 hrs · 38,273 cycles

LEFT WW FWD BULKHEAD SLAT PANEL ATTACH TEE FITTING INBD SIDE FOUND WITH CORROSION. REMOVED AND REPLACED IAW AMM 20-50-02 AND DRAWING NPB6072 REVISION AL. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SKIN — CRACKED (BS 1156) · airframe 90,620 hrs · 38,273 cycles

LOWER FUSELAGE SKIN AT BS 1156 CRACKED. REPAIR IAW EA 8-5310-T0312350 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 90,620 hrs · 38,273 cycles

RIGHT WING LE BEADED DOUBLER AT XOS 587 FOUND CRACKED. REPAIRED IAW SRM 57-10-00 FIGURE 71 VOLUME I. REPAIR CLASIFIED MAJOR IAW GMM 6-2-100.

Part: SKIN — CRACKED (RT WING) · airframe 90,620 hrs · 38,273 cycles

RIGHT WING DROOP LE AFT UPPER SURFACE FOUND CRACKED. REPAIRED IAW SRM 57-10-00 FIGURE 55 VOLUME I. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CRACKED (BS 1471) · airframe 90,620 hrs · 38,273 cycles

BS 1471 LBL 27.5 SEAT TRACK FOUND CRACKED. REPAIRED IAW SRM 53-70- 00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: LONGERON — CORRODED (BS 780-790) · corrosion level 2 · airframe 90,620 hrs · 38,273 cycles

FORWARD CARGO BILGE AREA FOUND LONGERON 52 CORRODED BETWEEN BS 780 & 790. REMOVED AND REPLACED THE LONGERON IAW SRM 51-31-01 VOLUME II AND DRAWING ADA8098. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SKIN — CRACKED (LT WING LE SLAT) · airframe 90,620 hrs · 38,273 cycles

LEFT WING NR 3 SLAT LOWER SURFACE AT STATION XOS 418 FOUND CRACKED. REPAIRED IAW SRM 57-10-00 FIGURE 43 VOLUME I AND EA 8-5750-T0312515 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 90,620 hrs · 38,273 cycles

LEFT WING LE BEADED DOUBLER AT XOS 545 FOUND CRACKED. REPAIRED IAW SRM 57-10-00 FIGURE 71 VOLUME I. REPAIR CLASIFIED MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 90,620 hrs · 38,273 cycles

LEFT WING LE BEADED DOUBLER AT XOS 668 FOUND CRACKED. REPAIR CARRIED OUT IAW SRM 57-10-00 FIGURE 71 VOLUME I. REPAIR CLASIFIED MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 90,620 hrs · 38,273 cycles

RIGHT WING LE BEADED DOUBLER AT XOS 668 FOUND CRACKED. REPAIRED IAW SRM 57-10-00 FIGURE 71 VOLUME I. REPAIR CLASIFIED MAJOR IAW GMM 6-2-100..

Part: STRINGER — CRACKED (RT WING) · airframe 90,620 hrs · 38,273 cycles

RIGHT WING LE STRINGER AT XOS 666 FOUND CRACKED. REPAIRED IAW EA 8-5710-T0312188 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: STRINGER — CRACKED (LT WING) · airframe 90,620 hrs · 38,273 cycles

LEFT WING LE STRINGER AT XOS 666 FOUND CRACKED. REPAIRED IAW EA 8-5710-T0312186 PART 1. . REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 90,620 hrs · 38,273 cycles

LEFT WING LE BEADED DOUBLER AT XOS 666 FOUND CRACKED. REPAIR CARRIED OUT IAW SRM 57-10-00 FIGURE 71 VOLUME I. REPAIR CLASIFIED MAJOR IAW GMM 6-2-100.

Part: RIB — CRACKED (LT WING) · airframe 90,620 hrs · 38,273 cycles

LEFT WING LE RIB DOUBLER AT XOS 667 FOUND CRACKED. RIB REMOVED AND REPLACED IAW SRM 51-33-01 VOLUME II. NEW RIB DOUBLER FABRICATED IAW DRAWING ARB1249 REVISION AA. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: CONNECTOR — LOOSE (CABIN) · airframe 90,439 hrs · 38,181 cycles

ON FIGHT CREW PREFLIGHT FOUND EMER LIGHTING SYS INOPERATIVE. FOUND CONNECTOR P1-203 PARTIALLY DISCONNECTED. RECONNECTED P1-203 IAW SWPM. EMER LIGHTS OPERATIONS & TEST GOOD FROM THE OVERHEAD PANEL.

Part: PROXIMITY SENSOR — DEFECTIVE (LANDING GEAR) · airframe 90,096 hrs · 38,013 cycles

PASSING 25K' NOSE GEAR RED UNSAFE CYCLED ON & OFF SEVERAL TIMES THEN HELD STEADY. SLOWED & DESCENDED TO CYCLE GEAR. NOSE UP & LOCKED, BUT MAINS WOULD NOT. SLOWED TO 210 & CYCLED AGAIN & MAINS LOCKED. FAILED OPERATIONS CHECK & ORIGINAL UNIT REINSTALLED DURING TROUBLESHOOTING A SERVICEABLE PSEU WAS INSTALLED FOR COMPARATIVE PURPOSES & WAS FOUND TO BE UNSERVICEABLE IAW AMM 31-71-01-2 CONFIG CODE SHOULD BE 34 - 34 FOR MD10-10 & 33-33 FOR -30. NEW PSEU INDICATED 34 - 34 BUT FAULTED PSEU & CTR GEAR INDICATOR. ORIGINAL UNIT WAS INSTALLED & RTS TEST PASSES. VISUALLY INSPECTED MAIN GEAR, NO PROBLEMS NOTED. REPLACED D1-78 SYS B DOWN SENSOR IAW AMM 32-1-17-4 & CHECKED IAW AMM 32-61-17-5. ALL FUNCTIONS & INDICATIONS NORMAL.

Part: SENSOR — MALFUNCTIONED (NLG) · airframe 90,070 hrs · 37,997 cycles

CLIMBING THROUGH 5000 FT, RECEIVED AN INTERMITTENT, THEN STEADY UNSAFE NLG ON BOTH THE SYNOPTIC & GEAR HANDLE LIGHT. CYCLED GEAR IAW QRH & NLG INDICATED SAFE. REPLACED D1-78 SYSTEM "B" DOWN SENSOR, IAW AMM 32-1-17-4 AND CHECKED IAW AMM 32-61-17-5. ALL FUNCTIONS AND INDICATIONS INDICATIONS NORMAL.

Part: INDICATOR — INOPERATIVE (L1 DOOR SLIDE) · airframe 89,193 hrs · 37,523 cycles

DURING PREFLIGHT, FOUND LEFT ENTRY DOOR EVACUATION SLIDE REMOTE PRESSURE PRESS-TO-TEST INDICATING SYS LIGHT INOPERATIVE. REMOVED AND REPLACED THE L1 DOOR PRESSURE INDICATOR ASSY, OPS NORMAL.

Part: PUMP — FAILED (NR 1 ENGINE) · airframe 88,990 hrs · 37,412 cycles

REJECTED TAKEOFF DUE TO NR 1 ENGINE ROLL BACK AT 95 KTS. R & R THE MEC AND FUEL PUMP.

Part: SWITCH — INOPERATIVE (PRESSURE IND) · airframe 88,979 hrs · 37,406 cycles

L1 DOOR BOTTLE PRESSURE LIGHT DOESN`T TEST. R & R L1 DOOR PRESSURE INDICATOR SWITCH. OPS CHECKED GOOD.

Part: BOTTLE — NO TEST (L1 DOOR) · airframe 88,899 hrs · 37,366 cycles

LIFE RAFT BOTTLE FAILED TEST, DURING PREFLT TEST. INSTALLED CORRECT BULBS,PERFORMED OPS CHECK PER MM 25-61-01-2. SLIDE LIGHT OPS CHECKED GOOD.

Part: SMOKE DETECTOR — FALSE ACTIVATION (CARGO) · airframe 88,886 hrs · 37,358 cycles

CLIMBING THROUGH 18000' TRI-TONE WARNING ANNUNCIATING A "CARGO FIRE LOWER" OCCURED FOR APPROX 5 SECONDS (2 CYCLES OF THE TRI-TONE). HAPPENED FOUR TIMES. INITIATED AN EMERGENCY RETURN TO AIRPORT, DECLARING AN EMERGENCY. THERE WERE NO ADDITIONAL FIRE WARNINGS WHILE ENROUTE TO AIRPORT. NO SMOKE/FUMES EXPERIENCED. LANDING UNEVENTFUL. WARNING WAS FOR THE FWD CARGO BAY. REPLACED ALL FOUR SMOKE DETECTORS IN LWR/FWD CARGO COMPARTMENT. CARGO SMOKE TEST GOOD IAW MM 26-14-01-5 REF MM 26-14-01-4

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 88,351 hrs · 37,070 cycles

CABIN PRESSURE UNCONTROLLABLE AFTER TAKEOFF, RTB. R & R CABIN OUTFLOW ACTUATOR, RIG & FUNCTIONAL CHECK GOOD IAW REF MM 21-31-20-4, MM 21-31-01/501. PERFORMED RTS CPC1 & CPC2 ALL TEAST PASSED. IAW REF MM 21-00-005 PRESSURIZED ACFT FOR OVER 45 MIN, NO LEAKS NOTED IN AREAS IDENTIFIED IN MTIS AND NO FAULTS APPEARED WITH SYS OP CK. ACFT OK FOR SERVICE.

Part: WIRE — BROKEN (DOOR SLIDE) · airframe 87,996 hrs · 36,877 cycles

LT DOOR SLIDE INDICATION SYS INOPERATIVE. REMOVED BROKEN PRESS TO TEST LAMP AND PULLED PLUG FROM TEST LIGHT JACK IN L1 DOOR. FOUND BROKEN WIRE ON POWER UNIT ASSY THAT SLIDE JACK PLUGS IN TO. SLIDE CONNECTOR JACK IS UNPLUGGED AND BATTERIES ARE REMOVED DUE TO THE BROKEN WIRE. REMAINS ON MEL. REPAIRED WIRE AND OP CHECKED DOOR REF SSM 25-61-0 AND MM 25-61-01-2. ACFT OK FOR SERVICE. FINAL CLOSED.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 86,530 hrs · 36,082 cycles

DURING COCKPIT SET UP, EMERGENCY LIGHTS TEST RECEIVED A LEVEL ONE ALERT. EMERGENCY LIGHT TEST FUNCTION - INOP. R & R EMERGENCY POWER SUPPLY IAW MM 33-51-4-0. OPS TEST IAW MM 33-51-5-0, NORMAL.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 86,518 hrs · 36,078 cycles

DURING COCKPIT SET UP, EMERGENCY LIGHTS TEST RECEIVED A LEVEL ONE ALERT: EMERGENCY LIGHT BATTERY ONE LOW. REMOVED AND REPLACED EMERGENCY POWER SUPPLY AS PER MM 33-51-4-0. OPS TESTED AS PER MM 33-51-5-0, NORMAL.

Part: RELAY — MALFUNCTIONED (FUEL DUMP) · airframe 86,361 hrs · 35,990 cycles

ATTEMPTED TO DUMP FUEL FOR RTB MEM AT APPROX 35K AT START OF DUMP, COULD NOT GET NORMAL DUMP TO OCCUR, EVEN AFTER SELECTING DUMP A SECOND TIME. GOT FUEL DUMP VALVE LT & RT DISAGREE ALERTS. TRANSFER PUMPS NEVER CAME ON. AFTER SEVERAL ATTEMPTS , NR 2 TRANSFER PUMP CAME ON BUT DUMP VALVES NEVER OPENED AND NO DECREASE IN FUEL QUANTITY OCCURRED. BURNED DOWN TO 15K FOR LANDING. R &R LT DUMP VALVE CONTROL RELAY R2-5871 AND RT DUMP VALVE CONTROL RELAY R2-5886. PERFORMED DUMP VALVES OPS TEST IAW AMM 28-30-02-2. OPS TEST GOOD. VERIFIED DUMP VALVE POSITIONS AND DUMP VALVE RELAY POSITIONS GOOD THRU CFDS FSC SENSOR READOUT. ALL CHECKS GOOD. FINAL CLOSED.

Part: CONTROL CABLE — BINDING (THROTTLE) · airframe 86,092 hrs · 35,849 cycles

NR 2 THROTTLE JAMMED AT CRUISE POWER SETTING. UNABLE TO CONTROL THROTTLE POSITION DURING DESCENT AND APPROACH. SHUTDOWN NR 2 ENG IAW QRH. AFTER LANDING DURING TAXI-IN, WAS ABLE TO MOVE THROTTLE FREELY. ENG WAS SHUTDOWN FOR LAST 10 MINS OF FLIGHT. DEPARTED FROM AIRPORT, WHICH HAD EXPERIENCED SOME RAINFALL- CRUISED.

Part: LANDING GEAR — MALFUNCTIONED (LEFT) · airframe 85,599 hrs · 35,603 cycles

DURING LANDING GEAR RETRACTION, THE LT MLG PRIMARY AND SECONDARY INDICATIONS, INDICATED UNSAFE. CHECK LIST WAS ACCOMPLISHED. GEAR WAS EXTENDED AND RETRACTED. ALL INDICATORS WERE SAFE. LANDED WITHOUT INCIDENT. INSPECTED GEAR UPLOCK SENSORS AND LUBED GEAR UPLOCK ROLLER IAW MM 32-00-00. AT THIS TIME NO DEFECTS NOTED,OK FOR SERVICE. (CLOSED)

Part: SKIN — CRACKED (ZONE 500) · airframe 85,576 hrs · 35,595 cycles

LT WING REAR SPAR LOWER CAP AT XORS 345, HFEC OPEN HOLE INSP. FOUND 01EA FASTENER HOLE WITH CRACKED INDICATION. LEFT HAND WING REAR SPAR LOWER CAP AT XORS 345, 01 EACH FASTENER HOLE WITH CRACKED INDICATION REPAIRED AS PER E.A. 8-5710-143797 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REVISION 111.

Part: SKIN — CRACKED (ZONE 500) · airframe 85,576 hrs · 35,595 cycles

LT WING ANTI ICE TELESCOPIC DUCT CUTOUT FOUND CRACKED. LT WING ANTI ICE TELESCOPIC DUCT CUTOUT CARRIED OUT REPAIR IAW EA NR 8-5710-143470, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.

Part: SKIN — CRACKED (ZONE 600) · airframe 85,576 hrs · 35,595 cycles

RT WING ANTI ICE TELESCOPIC DUCT CUTOUT FOUND CRACKED. RT WING ANTI ICE TELESCOPIC DUCT CUTOUT CARRIED OUT REPAIR IAW NR 8-5710-143471, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.

Part: SKIN — CHAFED (NR 4 SLAT LT) · airframe 85,576 hrs · 35,595 cycles

LT WING SLAT NR 4 UPPER SURFACE FOUND CHAFED. REMOVED AND CLEANED AS PER SRM 57-00-01 FIGURE 1A, VOLUME I, REVISION 96. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100, REVISION 111.

Part: SKIN — CRACKED (ZONE 600) · airframe 85,576 hrs · 35,595 cycles

WHILE CARRYING OUT WALK AROUND CHECK FOUND RT WING FUEL DUMP ISLAND UPPER SURFACE OTBD AREA EDGE WITH CRACK APPROX .5". REPAIRED AS PER EA 8-5750-143479, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100, REVISION 111.

Part: SKIN — CHAFED (ZONE 100) · airframe 85,576 hrs · 35,595 cycles

FWD CARGO DOOR - AFT DOOR CUTOUT STA Y=959 STR 40 TO 41R EXISTING REPAIR DOUBLER FOUND CHAFING. REPAIRED AS PER SRM 53-50-00 FIGURE 26, VOLUME I, REVISION 97. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100, REVISION 111.

Part: SKIN — CRACKED (ZONE 500) · airframe 85,576 hrs · 35,595 cycles

LT WING FIXED L/E FWD INBD SIDE OF PRESSURE REFUEL PANEL CUTOUT FOUND REPAIR DOUBLER CRACKED. CARRIED OUT RECTIFICATION AS PER E.A. 8-5730-143796, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REVISION 111.

Part: SKIN — CHAFED (BS 1780 S40-42R) · airframe 85,576 hrs · 35,595 cycles

LOWER CTR CARGO - AFT DOOR CUTOUT STA Y=1780 STR 40 TO 42R FOUND CHAFING. REPAIRED AS PER SRM 53-50-00 FIGURE 26, VOLUME I, REVISION 97. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100, REVISION 111.

Part: SKIN — DELAMINATED (NR 2 SPOILER LT) · airframe 85,576 hrs · 35,595 cycles

LT WING SPOILER NR 2 UPPER SURFACE FOUND DELAMINATION. LEFT HAND WING SPOILER NO.2 REMOVED AND REPLACED AS PER AMM 27-60-01 REVISION 10.1. OPERATIONAL CHECK CARRIED OUT AS PER AMM 27-60-00-2 REVISION 10.1 FOUND SATISFACTORY. CLEARANCE CHECK CARRIED OUT AS PER AMM 27-60-01-6 FOUND SATISFACTORY.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 82,520 hrs · 34,106 cycles

MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 7 HOLES "C" AND "D" INDICATED CRACKED DURING HFEC INSPECTION REMOVED AND REINSTALLED FRAME , INTERCOSTALLS, BRACKET AND WEB. REMOVED AND REPLACED FITTING. FABRICATED AND INSTALLED BUSHINGS AND REPAIR DOUBLER ALL IAW SRM 51-31-01, SRM 53-50-00 FIG 17, SRM 53-12-01 AND MAE TRAVELER T8/764446. MAJOR REPAIR RII.

Part: FITTING — CRACKED (ZONE 200) · airframe 82,520 hrs · 34,106 cycles

MAIN CARGO DOOR LOWER JAMB FITTING NR 6 HOLES "A" AND "C" INDICATED CRACKED DURING HFEC INSPECTION REMOVED AND REINSTALLED WEB, INTERCOSTALS AND FRAME. REMOVED AND REPLACED FITTING. FABRICATED AND INSTALLED BUSHINGS ALL IAW SRM 51-31-01, SRM 53-50-00 FIG 17 AND MAE TRAVELER T8/764445. MAJOR REPAIR RII.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 82,520 hrs · 34,106 cycles

MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 3 HOLE "D" INDICATED TWO CRACKS DURING HFEC INSPECTION. REMOVED AND REINSTALLED STRAPS, WEBS, CLIPS AND ANGLES. REMOVED AND REPLACED FITTING. FABRICATED AND INSTALLED BUSHINGS ALL IAW SRM 51-31-01, SRM 53-50-00 FIG 17 AND MAE TRAVELER T8/764441. MAJOR REPAIR RII.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 82,520 hrs · 34,106 cycles

MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 5 HOLE "A" INDICATED CRACKED DURING HFEC INSPECTION REMOVED AND REINSTALLED CLIP, STRAPS AND WEBS. REMOVED AND REPLACED FITTING. FABRICATED AND INSTALLED BUSHING ALL IAW SRM 51-31-01, SRM 53-50-00 FIG 17 AND MAE TRAVELER T8/764443. MAJOR REPAIR RII.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 82,520 hrs · 34,106 cycles

MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 4 HOLES "A" AND "D" INDICATED CRACKED AND HOLE "C" HAS CORROSION. REMOVED AND REINSTALLED STRAPS, CLIP AND WEB. REMOVED AND REPLACED FITTING MANUFACTURED AND INSTALLED BUSHINGS ALL IAW SRM 51-31-01, SRM 53-50-00 FIG 17 AND MAE TRAVELER T8/764442. MAJOR REPAIR RII.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 82,520 hrs · 34,106 cycles

MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 2 HOLES "A", "C" AND "D" INDICATED CRACKED DURING HFEC INSPECTION. REMOVED AND REINSTALLED STRAPS, WEBS, CLIPS AND ANGLES. REMOVED AND REPLACED FITTING. FABRICATED AND INSTALLED BUSHINGS ALL IAW SRM 53-50-00 FIG 17, SRM 51-31-01 AND MAE TRAVELER T8/764410. MAJOR REPAIR RII.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 82,520 hrs · 34,106 cycles

MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 1 HOLES "C" AND "B" INDICATED CRACKED DURING HFEC INSPECTION AND HOLE "D" HAS CORROSION. REMOVED AND REINSTALLED SIDEWALL GRILLS, PANELS, STRAPS, CLIPS, ANGLE AND WEB FOR ACCESS. REMOVED AND REPLACED FITTING. FABRICATED AND INSTALLED REPAIR BUSHINGS AND REPAIR DOUBLER ALL IAW SRM 51-31-01, SRM 53-50-00 FIG 17, SRM 53-00-01, SRM 53-12-01, SRM 51-21-02 AND MAE TRAVELER T8/764409. MAJOR REPAIR RII.

Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 82,520 hrs · 34,106 cycles

MCD SEAT TRACK RBL 28 STA 615 GOUGED AT CROWN REMOVED AND REINSTALLED 5 FLOOR PANEL FOR ACCESS. REMOVED AND REPLACED SEAT TRACK AND SPLICES AT STA 575 THROUGH 630 AT RBL 28 ALL IAW AMM 53-21-08-2, SRM 51-31-01, SRM 53-70-00 FIG 5, MAE TRAVELERS T8/763440 AND T8/763461. MAJOR REPAIR RII.

Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 82,520 hrs · 34,106 cycles

MCD SEAT TRACK AT RBL 46 STA 1341 IS GOUGED. REMOVED AND REPLACED SEAT TRACK AT RBL 46 STA 1331 THROUGH 1351 WITH SPLICES IAW SRM 53-70-00 FIG 5, SRM 51-31-01, AND MAE TRAVELERS T8/763348 AND T8/763347. MAJOR REPAIR RII.

Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 82,520 hrs · 34,106 cycles

MCD SEAT TRACK AT RBL 28 STA 755 IS GOUGED REMOVED AND REINSTALLED 3 FLOOR PANELS FOR ACCESS. REMOVED AND REPLACED SEAT TRACK AT STA 725 THROUGH 850 RBL 28 WITH SPLICES AND FABRICATED TRACK AND SPLICES ALL IAW AMM 53-21-08-2, SRM 51-31-01, SRM 53-70-00 FIG 5 AND MAE TRAVELERS T8/763383 AND T8/763382. MAJOR REPAIR RII.

Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 82,520 hrs · 34,106 cycles

MAIN DECK FLOOR SEAT TRACK HAS 4 GOUGES ON UPPER CROWN AT STA 675 LBL 47. REMOVED AND REINSTALLED FLOOR PANELS FOR ACCESS. REMOVED AND REPLACED SEAT TRACK AND SPLICES AT STA 665 THROUGH 685 LBL 47 AL IAW SRM 53-70-00 FIG 5, SRM 51-31-01, AMM 53-21-08-2 AND MAE TRAVELERS T8/763463 AND T8/763462. MAJOR REPAIR RII.

Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 82,520 hrs · 34,106 cycles

CABIN FLOOR SEAT TRACK AT STA 1119-1180, LBL 47 HAVE SEVERAL GOUGES AROUND CROWN HOLES EDGE BLENDED AREAS FOUND 1129 THROUGH 1180 IN LIMITS. TREATED AND PRIMED IAW SRM 53-70-00 FIG 5 AND SRM 51-21-01. FOUND AREAS AT 1119 THROUGH 1129 OUT OF LIMITS. REMOVED AND REINSTALLED FLOOR PANEL FOR ACCESS. REMOVED SEAT TRACK SECTION AND INSTALLED NEW SEAT TRACK WITH SPLICES ALL IAW SRM 53-70-00 FIG 5, SRM 51-31-01 AND MAE TRAVELERS T8/763092 AND T8/763091. MAJOR REPAIR RII

Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 82,520 hrs · 34,106 cycles

MCD SEAT TRACK AT RBL 46 STA 795 IS GOUGED REMOVED AND REPLACED SEAT TRACK AT STA 765 THROUGH 819 AT RBL 46 IAW SRM IAW SRM 51-31-01, SRM 53-70-00 FIG 5 AND MAE TRAVELER T8/763465. MAJOR REPAIR RII.

Part: LANDING GEAR — MALFUNCTIONED · airframe 81,462 hrs · 33,609 cycles

LANDING GEAR DID NOT RETRACT AFTER TAKEOFF. WITH HANDLE UP, THE 3 RED GEAR LIGHTS WERE ILLUMINATED ALONG WITH SECONDARY RED LIGHTS ON CONFIG PAGE. FOLLOWED QRH PROCEDURES AND RECYCLED GEAR. ALL CAME UP NORMALLY AND LIGHT WENT OUT. INSPECTED GEAR AREA FOR OBVIOUS DAMAGE OR INTERFERENCE. NO DEFECTS NOTED. PERFORMED RTS AND FAULT REVIEW ON PSEU. NO FAULTS LOGGED. ALSO CHECKED PSEU FOR MARGINAL RIGGING ON ANY GEAR SENSORS. NO MARGINAL RIGGING FOUND FOR ANY GEAR SENSORS FOR ANY PREVIOUS FLIGHTS. ALL GEAR SENSORS CHECK NORMAL FOR NEAR/FAR STATUS AT THIS TIME. SUSPECT BOGIE WAS NOT CENTERED WHEN HANDLE WAS SELECTED UP. AIRCRAFT OK FOR SERVICE, REF M/M 31-71-01-2.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 3 · airframe 80,218 hrs · 33,033 cycles

LT AIR CONDITION COMPT SEVERE CORROSION WITH EXFOLIATION ON FRAME AT STA 495 X=28, REPAIR IAW SRM 53-00-01 FIG 8 VOL 1.

Part: SKIN — CORRODED (BS 1257-1278) · corrosion level 2 · airframe 80,201 hrs · 33,026 cycles

BARREL SECTION STA Y=1257 TO Y=1278 LONG 47L TO 47R FOUND CORROSION ON SKIN, SHEAR TIES, LONGERONS, RIVETS, DRAIN HOLES AND AROUND INLET DUCT REPAIR IAW SRM 53-20-00 FIG 13.

Part: SKIN — CORRODED (BS 1159-1216) · corrosion level 2 · airframe 80,201 hrs · 33,026 cycles

BARREL SECTION STA Y=1159 TO Y=1216 LONG 48L TO 47R FOUND CORROSION ON SKIN, SHEAR TIES, LOMGERONS, RIVETS, DRAIN HOLES AND AROUND INLET DUCT REPAIR IAW SRM 53-20-00 FIG 13 VOL1.

Part: LONGERON — UNKNOWN (BS 1059-1119) · airframe 80,201 hrs · 33,026 cycles

EXISTING LONGERON SPLICE REPAIR ON FWD CARGO COMPT FROM STA 1079 TO STA 1119 LONGERON 44 RT. INSTALL NEW LONGERON SECTION IAW SRM 53-10-00 FIG 1 VOL 1.

Part: BULKHEAD — CRACKED (BS 488-495) · airframe 80,201 hrs · 33,026 cycles

NLG WHEEL WELL NR 6 CRACKS ON LT VERTICAL BULKHEAD FROM STA 488 TO 495 FROM Z=-60 AT Z=-65, REPAIR IAW SRM 53-40-00 VOL 1.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 80,201 hrs · 33,026 cycles

HORIZONTAL STABILIZER LWR INT SKIN PANELS CONSTANT SECTION CRACKED INFLYABLE LIMIT ACCOMPLISH EA 8-5510-96122.

Part: BULKHEAD — CRACKED (ZONE 700) · airframe 80,201 hrs · 33,026 cycles

LT MLG WHEEL WELL INT STRUCTURE AT STA 1505 X=31 Z=-42 ON VERTICAL BULKEAD FOUND NR 2 CRACK AFTER STOP DRILL OF OLD REPAIR REPAIR IAW SRM53-00-01 FOG 10 VOL 1.

Part: BULKHEAD — CRACKED (NLG WW) · airframe 80,201 hrs · 33,026 cycles

NLG WHEEL WELL QTY 6 CRACK ON RT VERTICAL BULKHEAD FROM STA 583 TO 592 FROM Z=-40 TO Z=-52 REPAIR IAW 53-30-00 FIG 6 SH2 VOL 1.

Part: BULKHEAD — CRACKED (BS 580) · airframe 80,201 hrs · 33,026 cycles

NLG WHEEL WEEL LT VERTICAL BULKHEAD CRACK LONG .75" AT STA 580 Z=-47 REPAIR IAW SRM 53-30-00 FIG 6 VOL 1.

Part: WEB — CRACKED (NR 1 SLAT) · airframe 80,201 hrs · 33,026 cycles

RT WING FOUND CRACK QTY 1 ON WEB ON SLAT NR 1 REPAIR IAW SRM 57-00-01 FIG 12 VOL1.

Part: SKIN — DAMAGED (ZONE 100) · airframe 80,201 hrs · 33,026 cycles

LWR NOSE SKIN ACCIDENTAL DAMAGE AT STA 458 X=16 LT TO X=16 RT REPAIR IAW SRM 53-20-00 FIG 6 SH16 VOL1.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 80,201 hrs · 33,026 cycles

RT WING T/E LWR SKIN FOUND SEVERE CORROSION ON BEAVER TAIL AT STA XORS 231. REPAIR IAW EA FEDEX 8-5710-108070.

Part: FRAME — CRACKED (BS 535) · airframe 80,201 hrs · 33,026 cycles

RT AIR COND COMPT FOUND CRACK 5" LONG ON FRAME STA 535. REPAIRED FRAME IAW SRM 53-30-00 FIG 5 AND SRM 53-00-01 FIG 8 VOL 1.

Part: BEAM — CRACKED (BS 1099) · airframe 80,201 hrs · 33,026 cycles

FWD CARGO COMPT CRACK 2" ON LOWER BEAM STA 1099. REPAIRED BEAM IAW SRM 53-60-01 FIG 3 VOL 1.

Part: ANGLE — CRACKED (BS 547) · airframe 80,201 hrs · 33,026 cycles

LT AIR COND COMPT FOUND CRACK 1.5" ON HORIZONTAL ANGLE AT STA 547. REPAIRED JAMB IAW SRM 53-00-01 FIG 8 SHT 2 VOL 1.

Part: SEAT TRACK — CRACKED (BS 1256) · airframe 80,201 hrs · 33,026 cycles

MAIN CABIN FOUND 1 CRACK 4" ON BEAM SUPPORT SEAT TRACK STA 1256. REPAIRED BEAM IAW SRM 53-00-01 FIG 9 VOL 1.

Part: FRAME — CRACKED (BS 1671 S44R) · airframe 80,201 hrs · 33,026 cycles

CENTRAL CARGO COMPT 2 CRACKS 5" AND 7" LONG STA 1671. REPLACE LONG AFA3040-1 AND REPAIRED FRAME IAW SRM 53-30-00 FIG 5 AND 10 VOL 1.

Part: CAP — CRACKED (RT WING) · airframe 80,201 hrs · 33,026 cycles

RT WING L/E FOUND ONE CRACK 1" LONG ON FIXED CAP STA XORS 827. REPAIRED IAW SRM 57-10-00 FIG 49 VOL 1.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 80,201 hrs · 33,026 cycles

FOUND EXISTING FRAME REPAIR AT STA 1701 BETWEEN LONGERONS 11 AND 12 RT. REMOVED RIVETS AND INSTALLED HI LOCKS IAW SRM 53-30-00 FIG 5 SHT 2 VOL 1, USED FIRST OVERSIZE FASTENERS AS REQUIRED IAW SRM 51-33-01 VOL 2.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 80,201 hrs · 33,026 cycles

FOUND EXISTING FRAME REPAIR AT STA 1741 BETWEEN LONGERONS 11 AND 12 LT. REMOVED RIVETS AND INSTALLED HI LOCKS IAW SRM 53-30-00 FIG 5 SHT 2 VOL 1, USED OVERSIZE FASTENERS AS REQUIRED IAW SRM 51-33-01 VOL 2.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 80,201 hrs · 33,026 cycles

FOUND EXISTING FRAME REPAIR AT STA 1781 BETWEEN LONGERONS 11 AND 12 RT. REMOVED RIVETS AND INSTALLED HI LOCKS FIRST OVERSIZE IAW SRM 53-30-00 FIG 5 SHT 2 VOL 1 AND SRM 51-33-01 PAR 6-10 VOL 2.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 80,201 hrs · 33,026 cycles

FOUND EXISTING FRAME REPAIR AT STA 1761 BETWEEN LONGERONS 11 AND 12 RT. REMOVED RIVETS AND INSTALLED HI LOCKS FIRST OVERSIZE IAW SRM 53-30-00 FIG 5 SHT 2 VOL 1 AND SRM 51-33-01 PAR 6-10 VOL 2.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 80,201 hrs · 33,026 cycles

FOUND EXISTING FRAME REPAIR AT STA 1721 BETWEEN LONGERONS 11 AND 12 LT. REMOVED RIVETS AND INSTALLED HI LOCKS IAW SRM 53-30-00 FIG 5 VOL 1, USED OVERSIZE FASTENERS AS REQUIRED IAW SRM 51-33-00 VOL 2.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 80,201 hrs · 33,026 cycles

MAIN CABIN FOUND NR 1 CRACK 1" LONG ON LOWER SIDE WEB JAMB DOOR L 3 AT STA 1256 LONG NR 26 LT SIDE. REMOVED EXISTING DOUBLER IAW SRM 51-35-01 VOL 2 PAR 1-5. INSTALLED NEW DOUBLER. REPAIRED IAW SRM 53-50-00 FIG 10 VOL 1. FABRICATED PART IAW DETAIL PART TRAVELER I035547/N00547 AND IAW SRM 53-50-01 FIG 10 SHT 1 VOL 1.

Part: DOOR FRAME — MISREPAIRED (FUSELAGE) · airframe 80,201 hrs · 33,026 cycles

FOUND EXISTING REPAIR MAIN CABIN L3 DOOR JAMB FROM STA 1305 TO STA 1315 BETWEEN LONGERONS 26 AND 27 LT. AFTER AN ASSESSMENT OF THIS REPAIRED WAS DETERMINATED DOEN`T COMPLY WITH SRM REQUIREMENTS, THEREFORE, REMOVED AND DISCARDED REPAIRED. FABRICATED AND INSTALLED NEW REPAIR IAW SRM 53-50-00 FIG 19 VOL 1.

Part: DOOR FRAME — UNKNOWN (FUSELAGE) · airframe 80,201 hrs · 33,026 cycles

FOUND EXISTING REPAIR MAIN CABIN R3 DOOR JAMB FROM STA 1305 TO STA 1315 BETWEEN LONGERONS 26 AND 27 RT. REMOVED OLD REPAIR IAW SRM 51-33-01 PAR 6-10 VOL 2. INSTALLED NEW REPAIR DOUBLER IAW SRM 53-50-00 FIG 19 VOL 1. FABRICATED PART IAW DETAIL PART TRAVELER I036055/N01055 AND IAW SRM 53-50-00 FIG 19 DETAIL -9 VOL 1.

Part: FRAME — MISREPAIRED (FUSELAGE) · airframe 80,201 hrs · 33,026 cycles

FOUND EXISTING FRAME REPAIR AFT CARGO COMPARTMENT AT STA 1856 BETWEEN LONGERONS 52 AND 51 RT. PERFORMED INSPECTION OF REPAIR AND NOT FOUND INCOMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001-P2 BECAUSE FOUND 20 RIVETS INSTEAD OF HI LOCKS IAW SRM 53-30-00 PAGE 15 FIG 5 SHT 1 VOL 1. REMOVED RIVETS AND INSTALLED HI LOCKS OVERSIZE IAW SRM 53-30-00 PAGE 15 FIG 5 SHT 1 VOL 1 AND SRM 51-33-01 VOL 2.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 80,201 hrs · 33,026 cycles

MAIN CABIN FOUND NR 1 CRACK 0.40" LONG ON LOWER SIDE WEB JAMB DOOR R 3 AT STA 1256 LONG NR 26 RT SIDE "UNDER EXISTING REPAIR". REMOVED EXISTING DOUBLER IAW SRM 51-35-01 PAR 1-5 / 51-33-01 PAR 6-10 VOL 2. INSTALLED NEW REPAIR DOUBLER IAW SRM 53-50-00 FIG 19 SHT 1 VOL 1. FABRICATED PART IAW DETAIL PART TRAVELER I035540/N00540 AND IAW SRM 53-50-00 FIG 19 SHT 1 VOL 1.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 80,201 hrs · 33,026 cycles

FOUND EXISTING FRAME REPAIR AT STA 1721 BETWEEN LONGERONS 11 AND 12 RT. REMOVED RIVETS AND INSTALLED HI LOCKS IAW SRM 53-30-00 FIG 5 SHT 2 VOL 1, USED OVERSIZE FASTENERS AS REQUIRED IAW SRM 51-33-01 VOL 2.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 80,201 hrs · 33,026 cycles

FOUND EXISTING FRAME REPAIR AT STA 1741 BETWEEN LONGERONS 11 AND 12 RT. REMOVED RIVETS AND INSTALLED HI LOCKS IAW SRM 53-30-00 FIG 5 SHT 2 VOL 1, USED OVERSIZE FASTENERS AS REQUIRED IAW SRM 51-33-01 VOL 2.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 80,201 hrs · 33,026 cycles

RT AIR CONDITIONING COMPT CRACK 1" LONG ON INTERNAL VERTICAL BULKHEAD AT STA 495 Z= -58. REMOVED PORTION OF BROKEN WEB, AND REPAIRED IAW SRM 53-40-00 VOL 1 FIG 34. FABRICATED PARTS IAW DETAIL PARTS TRAVELER I035881/N00881 AND IAW SRM 53-40-00 VOL 1.

Part: RIB — CRACKED (RT WING) · airframe 80,201 hrs · 33,026 cycles

FOUND RT WING L/E INT SIDE FOUND 1 CRACK ON RIB AT STA XORS 923. REPAIRED RIB IAW SRM 57-20-00 PAG 3 FIG 1 VOL 1. FABRICATED PART IAW DETAIL PART TRAVELER I035571-3/N00571-3. REPAIR ANGLE IAW SRM 57-20-00 FIG 20 SHT 2 VOL 1.

Part: RIB — CRACKED (RT WING) · airframe 80,201 hrs · 33,026 cycles

RT WING L/E INT SIDE FOUND 1 CRACK ON RIB AT STA XORS 562. REPAIRED RIB IAW SRM 57-20-00 PAG 3 FIG 1 VOL 1. FABRICATED PART IAW DETAIL PART TRAVELER I035577-3/N00577-3. REPAIR ANGLE IAW SRM 57-20-00 FIG 1 VOL 1.

Part: RIB — CRACKED (RT WING) · airframe 80,201 hrs · 33,026 cycles

RT WING L/E INT SIDE FOUND 1 CRACK ON HORIZONTAL RIB AT STA XORS 548. REPAIRED RIB IAW SRM 57-00-01 VOL 1 FIG 10. FABRICATED PART IAW DETAIL PART TRAVELER I035578-3/N00578-3 REPAIR ANGLE IAW SRM 57-00-01 FIG 10 VOL 1.

Part: ANGLE — CRACKED (BS 594) · airframe 80,201 hrs · 33,026 cycles

FOUND LT AIR CONDITIONING COMPT, CRACK ON STIFFENER AND ANGLE REPAIR OF UPPER BULKHEAD AT STA 594, X= 57. REPAIRED ANGLE IAW SRM 53-00-01 VOL 1 FIG 2 SHT 2. FABRICATED PARTS IAW DETAIL PARTS TRAVELER N00884 AND IAW SRM 53-00-01 FIG 2 SHT 2 VOL 1.

Part: SKIN — CRACKED (RT WING) · airframe 80,201 hrs · 33,026 cycles

RT WING L/E EXT FOUND 1 CRACK 1.50" LONG ON SKIN AT STA XORS 506. REMOVED REFUELING DOOR IAW MM 20-50-02-2 AND DWG ARB1067. REMOVED PLATE SP10240168 IAW SRM 51-31-01 VOL 2 PAR 6. REMOVED EXISTING DOUBLER AND INSTALLED A NEW ONE IAW SRM 57-10-00 VOL 1 FIG 68. REINSTALLED PLATE IAW SRM 51-31-01 VOL 2 PAR 6. REINSTALLED REFUELING DOOR IAW MM 20-50-02-2 AND DWG ARB1067. FABRICATED PARTS IAW DETAIL PARTS TRAVELER N00580 AND IAW SRM 57-10-00 FIG 68 VOL 1.

Part: RIB — CRACKED (LT WING) · airframe 80,201 hrs · 33,026 cycles

LT WING L/E INT SIDE FOUND 1 CRACK 1" LONG ON HORIZONTAL RIB AT STA XORS 570. REPAIRED RIB IAW SRM 57-00-01 FIG 10 SHT 1 VOL 1. FABRICATED PART IAW DETAIL PART TRAVELER I035526/N00526 AND SRM 57-00-01 VOL 1.

Part: ANGLE — CRACKED (SLAT) · airframe 80,201 hrs · 33,026 cycles

LT WING L/E DURING INSPECTION FOUND 1 CRACK 2" LONG ON ANGLE OF SLAT NR 2 AT STA XORS 264. REPAIRED ANGLE IAW SRM 57-00-01 FIG 3 VOL 1. FABRICATED PART IAW DETAIL PART TRAVELER I035530-3/N00530-3 AND IAW SRM 57-00-01 FIG 3 VOL 1.

Part: WEB — CRACKED (NLG WW) · airframe 79,797 hrs · 32,819 cycles

NOSE WHEEL WELL RT SIDE X= 24.00 STATION 475.00 CENTER OF WEB SKIN CRACK IN SKIN OVER 1 INCH LONG. MULTIPLE AIRCRAFT FOUND WITH SIMILAR CRACKS IN SAME AREA. CRACKED MATERIAL REMOVED AND SRM REPAIR DOUBLER INSTALLED PER SRM 53-30-00 VOLUME 1 FIGURE 6, SHEET 4.

Part: ATTACH FITTING — BROKEN (T/E FLAP VANE) · airframe 79,626 hrs · 32,717 cycles

ON FINAL APPROACH AS FLAPS WERE EXTENDED INCREASINGLY MORE RIGHT WING DOWN AILERON WAS NEEDED TO MAINTAIN WINGS LEVEL FLIGHT YOKE NEEDED TO BE HELD AT APPROX 30 DEGREES RIGHT WING DOWN AS PICTURED. FOUND LEFT WING INBOARD FLAP VANE IN THE RETRACTED POSITION WITH FLAP EXTENDED. FOUND LEFT INBOARD FLAP VANE SPRING CARTRIDGE TRACK ATTACH FITTING BROKEN. REMOVED AND REPLACED LT WING INBOARD FLAP VANE SPRING CARTRIDGE AND TRACK FITTING IAW DC-10-10 AMM 27-51-04-2. OPS CHECK GOOD. OK TO CONTINUE.

Part: LONGERON — CORRODED (ZONE 100) · corrosion level 2 · airframe 78,298 hrs · 32,035 cycles

CORROSION FOUND IN VERTICAL LEG OF LONGERON 47L STATION 1764, LEAVING A HOLE .5 HIGH BY 3.0 LONG AFTER CORROSION REMOVAL WITH REDUCED MATERIAL THICKNESS ON BOTH SIDES OF SUBJECT HOLE. COMPLIED WITH FED EX EA 8-5310-91240 FUSELAGE LONGERON 47L STA 1764 CORROSION, REPAIR.

Part: PRESSURE SWITCH — FAILED (ANTI ICE SYSTEM) · airframe 77,441 hrs · 31,587 cycles

NR 3 MANIFOLD FAIL LIGHT ILLUMINATED SHORTLY AFTER TURNING ON WING ANTI ICE. RAN RED TABS; FAULT LIGHT WENT OUT IMMEDIATELY. AFTER TURNING OFF NR 3 ENG PNEU SUPPLY SELECTOR. CHECK RT WING ANTI-ICE DUCTING FOR LEAKS NO LEAKS NOTED. CHECKED MANIFOLD FAIL DETECTOR CONTROLLER FOR FAULTS. FOUND FAULT BALL FOR RT WING PRESSURE SWITCH. REPLACED PRESSURE SWITCH IAW AMM 36-23-03-4. RAN ENGINE AGAIN WITH WING ANTI-ICE. NO LEAKS NOTED AND FAULT DID NOT RETURN. OPS CHECK GOOD.

Part: PSEU — MALFUNCTIONED (MLG) · airframe 76,764 hrs · 31,226 cycles

ON FIRST GEAR EXTENSION RIGHT MAIN GEAR INDICATED UNSAFE. ANTI-SKID WOULD NOT TEST EITHER. RECYCLED GEAR AND RIGHT MAIN GEAR ON F/O PANEL STILL INDICATED UNSAFE. S/O PANEL INDICATED ALL THREE GEAR DOWN AND LOCKED. ANTI-SKID TESTED OK. F/O RESEATED RIGHT MAIN GEAR LIGHT AND GOT POSITIVE GEAR DOWN INDICATION (GREEN LIGHT). LANDED WITH NO FURTHER PROBLEMS. INSPECTED RIGHT MAIN GEAR PROX SWITCHES AND LINKAGES, NO FAULTS FOUND. TESTED PROX BOX, BOX INDICATED FAULT IN 31 RIGHT POSITION. REPLACED PROX BOX AND TESTED OK PER TAFI 32-30-00. ANTI-SKID TESTED OK PER M/M 32-44-00.

Part: FITTING — GOUGED (L-1 DOOR) · airframe 76,292 hrs · 30,982 cycles

LOWER FWD AND AFT STOPS LUGS HAVE GOUGES ON L-1 DOOR. REMOVED DAMAGED LUGS AND INSTALLED SERVICABLE LUGS/STOPS IAW SRM 51-31-01 AND 51-33-01 AT MAE ON N/R N00825.

Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 76,292 hrs · 30,982 cycles

ZONE 20, FS 475 FWD SIDE OF DOOR 115 AZ CLIPS AND ANGLES CORRODED FROM LBL 15 TO RBL 5. REMOVED AND REPLACED 2 STIFFENERS AND CLIPS IAW SRM 51-31-01 AT MAE ON N/R N00628.

Part: PIPE — DAMAGED (NR 2 ENG DRAIN) · airframe 76,292 hrs · 30,982 cycles

COMPLY WITH EA 8-7160-73881. POWERPLANT - ENGINE DRAINS MINOR DEVIATION TO FEDEX EO 8-7160-7-5000. POWERPLANT - ENGINE DRAINS - MINOR DEVIATION TO FEDEX EO 8-7160-7-5000 COMPLIED WITH AT BFM/MAE.

Part: HOUSING — GOUGED (NR 2 ENG GEARBOX) · airframe 76,292 hrs · 30,982 cycles

COMPLY WITH EA 8-7260-75573. ENGINE DRAIN - TRANSFER GEARBOX HOUSING DAMAGE INTERIM REPAIR. COMPLIED WITH EA 8-7260-75573.

Part: SUPPORT — GOUGED (ZONE 500) · airframe 76,292 hrs · 30,982 cycles

COMPLY WITH EA 8-5750-73880 WINGS - INBOARD FLAP ACTUATOR SUPPORT ASSY BARREL NUT HOLE GOUGED. REPAIR P/N ARC0329-1. COMPLIED WITH EA 8-5750-73880.

Part: BRACKET — CRACKED (NR 3 ENGINE) · airframe 76,292 hrs · 30,982 cycles

NR 3 ENGINE I/B TRAILING EDGE LOWER BALL SCREW G/B SUPPORT BRACKET IS CRACKED. REMOVED DAMAGED BRACKET IAW SRM 51-35-01. RECEVIED NEW BRACKET P/N 311OM24POO1A. LOCATED AND DRILLED IAW SRM 51-31-01. INSTALLED BRACKET ACTUATOR IAW SRM 51-31-01 AND 51-31-01.

Part: RIB — DAMAGED (THRUST REVERSER) · airframe 76,292 hrs · 30,982 cycles

COMPLY WITH EA 8-7830-73868 EXHAUST SYSTEM -THRUST REVERSER Z-RIB REPAIR P/N 9152M45P004A. COMPLIED WITH EA 8-7830-73868 EXHAUST SYSTEM - THRUST REVERSER Z-RIB REPAIR P/N 9152M45P004A AT BFM.

Part: RIB — DAMAGED (THRUST REVERSER) · airframe 76,292 hrs · 30,982 cycles

COMPLY WITH EA 8-7830-73868 EXHAUST SYSTEM -THRUST REVERSER Z-RIB REPAIR P/N 9152M45P004A. COMPLIED WITH EA 8-7830-73868 EXHAUST SYSTEM - THRUST REVERSER Z-RIB REPAIR P/N 9152M45P004A AT BFM.

Part: BUMPER BLOCK — CRACKED (THRUST REVERSER) · airframe 76,292 hrs · 30,982 cycles

NR 1 ENGINE OUTBOARD THRUST REVERSER MOST FWD UPPER BUMPER ASSY CRACKED. REMOVED AND REPLACED BUMPER ASSY IAW SRM 51-31-01 AT MAE ON N/R N01145.

Part: SUPPORT — CORRODED (MLG) · airframe 76,292 hrs · 30,982 cycles

MAIN LANDING GEAR ATTACHMENT SUPPORT CORROSION REPAIR (P/N ARB0622). WINGS - MAIN FRAME- MAIN LANDING GEAR ATTACHMENT SUPPORT CORROSION REPAIR (P/N ARB0622).

Part: SUPPORT — CORRODED (MLG) · airframe 76,292 hrs · 30,982 cycles

MAIN LANDING GEAR ATTACHMENT SUPPORT OVERSIZE HOLE REPAIR. COMPLIED WITH EA 8-5740-73874 WINGS - MAIN FRAME - MAIN LANDING GEAR ATTACHMENT SUPPORT OVERSIZE HOLE REPAIR.

Part: HINGE — CORRODED (ZONE 500) · airframe 76,292 hrs · 30,982 cycles

COMPLY WITH EA 8-5750-73872. WINGS - LT OUTBD FLAP, INBD HINGE ASSY ARC1984, PIVOT BORE REWORK. CLOSING ACTION ON 01/30/04, ON N/R S00013. COMPLIED WITH EA 8-5750-73872.

Part: FAIRLEAD — CRACKED (ZONE 100) · airframe 76,292 hrs · 30,982 cycles

COMPLY WITH EA 8-5310-73870. FUSELAGE-REPAIR OF CONTROL CABLE FAIRLEAD AT STA 575 AND LBL 41.5. CLOSING ACTION ON 01/25/04.ON N/R S00011.COMPLIED WITH EA 8-5312-73870.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 73,567 hrs · 29,663 cycles

HORIZ PRESS BULKHEAD LT ANGLE PIN CRACKED FROM BS 555-575 AT LONGERON 30L. REMOVED AND REPLACED PER EA 8-5310-57067.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 73,567 hrs · 29,663 cycles

HORIZ PRESS BULKHEAD RT OUTBOARD ANGLE IS CRACKED FROM BS 535-555. REMOVED AND REPLACED ANGLE PER EA 8-5310-57067.

Part: ENGINE — MALFUNCTIONED (NR 1) · airframe 73,314 hrs · 29,527 cycles

NR 1 ENGINE FAILED AFT THROTTLES REDUCTION. SHUT DOWN. REMOVED AND REPLACED CIT SENSOR AND PERF BORESCOPE PER STALL REQ. RAN ENG OK FOR SERVICE.

Part: LINE — CRACKED (BS 1960)

N3671 - HYD SYS NR 2 PRESSURE LINE PN AJK7011-1 CRACKED AND LEAKING LOCATED AT BS 1960 IN AFT CARGO TUNNEL AREA. REPAIRED IAW DC10 MM 20-10-01-2 AND DPS 3.80-10.

Part: LINE — CRACKED (BS 1995-2004)

N3668 - SYS 2 HYD LEAK DETECT PRESSURE LINE, PN AGK7002-514, RUPTURED. LOCATED BETWEEN BS 1995 AND 2004 LT SIDE. REPAIRED IAW DC 10 MM 20-10-01-2 AND DPS 3.20-10.

Part: LINE — CRACKED (LT MLG WW)

N3477 - HYD LINE PN APK7002-536 IS CRACKED AND LEAKING LOCATED IN LT WHEEL WELL, NR 3 SYS TO MLG. REPAIRED HYD LINE IAW DC10 MM 20-10-01-2 AND DPS 3.80-10.

Part: LINE — CRACKED (BS 1278)

N3489 - SYS NR 3 HYD LINE PN APK7002-518 IS CRACKED AND LEAKING LOCATED ON LT SIDE AT STA 1278 IN ACCESS AREA BETWEEN MLG W/W. REPAIRED IAW DC 10 MM 20-10-01-2 AND DPS 3.80-10.

Part: LINE — CRACKED (BS 1720)

N3483 - HYD LINE P/N AFK7002-541 IS CRACKED AND LEAKING LOCATED IN LT CTR CARGO TUNNEL AREA AT BS 1720. REPAIRED HYD LINE IAW DC10 MM 20-10-01-2 AND DPS 3.80-10.

Part: LINE — CRACKED (BS 1989)

N 3478 - HYD LINE PN AJK7004-589 IS CRACKED AND LEAKING, LOCATED IN AFT PIT AT BS 1989 LT SIDE. REPAIRED HYD LINE IAW DC10 MM 20-10-01-2 AND DRS 3-80-10.

Part: LINE — CRACKED (BS 1995)

HYD LINE P/N AGK7002-565, CRACKED AND LEAKING AT BS 1995 IN AFT WASTE COMP TUNNEL AREA ON LT SIDE. REPAIRED IAW DC10 MM 20-10-01-2 AND DPS 3.80-10.

Part: LINE — CRACKED (BS 1721)

N3481 - HYD LINE SYS 2 PN AGK7002-513 CRACKED AND LEAKING LOCATED AT BS 1721 LT SIDE. REPAIRED IAW DC10 MM 20-10-01-2 AND 3.80-10.

Part: LINE — CRACKED (NR 2 HYD SYS)

N3472 NR 2 HYD SYS RETURN LINE CRACKED. LOCATED IN AFT CARGO COMP RT SIDE AT SM 2.000. REPAIRED HYD LINE IAW DC10 MM 20-10-01-5 AND DPS 3.80-10.