N317FE

Part: SENSOR — MALFUNCTIONED (N/A) · airframe 91,306 hrs · 25,788 cycles

AT FL 330, THROTTLES CAME TO IDLE, ACFT BEGAN A SLIGHT CLIMB, AND A "AUTOSLAT FAIL" ALERT. ANOTHER SLIGHT PITCH UP, AND CONFIGURATION PAGE SHOWED RT WING FLAPS TRYING TO EXTEND. INDICATION WAS WHITE BOXES BELOW RT WING, BUT NO NUMBERS INDICATING. STICKSHAKER MOMENTARILY ACTIVATED WITH UPPER AMBER FOOT DROPPED TO BOTTOM OF SCALE. DIVERTED. MOMENTARY STICKSHAKER AGAIN PASSING FL 180. REMOVED AND REPLACED TRANSFORMER IAW MM 20-00-00. REMOVED AND REPLACED RIGHT ANGLE OF ATTACK SENSOR AND ADJUSTED. TESTED GOOD IAW AMM 22-00-05-5 AND 27-35-02-4.

Part: WEB — CRACKED (ZONE 400) · airframe 90,553 hrs · 25,481 cycles

HOLES OUT OF LIMITS ON WEB AUB7366-501. R & R UPPER PYLON SPAR WEB IAW DWG AUB7301 AND SRM 51-33-01, VOL. II INSTRUCTIONS.

Part: BULKHEAD — CRACKED (ZONE 400) · airframe 90,553 hrs · 25,481 cycles

NR 1 ENGINE PYLON AFT BULKHEAD UPPER INBD CORNER FLANGE AREA INSIDE HAS A DISCONTINUITY INDICATION WHICH WAS CONFIRMED BEING CRACKED APPROX .5" BY VERIFYING WITH BOROSCOPE INSPECTION AS SEEN THROUGH THE FOOTBALL PANEL. R & R THE AFT PYLON BULKHEAD IAW EA 8-5410-163804 INSTRUCTIONS.

Part: BEAM — CRACKED (FWD CARGO DOOR) · airframe 90,553 hrs · 25,481 cycles

FWD CARGO DOOR BALANCE BEAM CRACKED AND BROKEN. R & R FWD CARGO DOOR BEAM ASSY IAW CMM 52-31-03, STEP 21(D).

Part: DOUBLER — CRACKED (MLG WW BULKHEAD) · airframe 90,553 hrs · 25,481 cycles

WHEEL WELL SUSPECT A CRACK ON LT KEEL BEAM BULKHEAD MACHINED DOUBLER. REMOVED AND REPLACED CRACKED DOUBLER AEA 0526U1

Part: DOUBLER — CRACKED (BS 1386) · airframe 90,553 hrs · 25,481 cycles

WHEEL WELL CRACKED ON RT KEEL BEAM BULKHEAD MACHINED DOUBLER AT BS 1386 AT X 31.5. R & R CRACKED DOUBLER AEA 0526U2, REF SRM 51-33-01, VOL 2.

Part: STRUCTURE — DAMAGED (RT ELEVATOR) · airframe 89,541 hrs · 25,081 cycles

RIGHT ELEVATOR, AT GAP BETWEEN THE INNER AND OUTER ELEVATORS. DAMAGE TO THE T/E PIECE ON THE UPPER AND LOWER SURFACE THAT RUNS APPROX 10" FROM THE INNER EDGE TOWARDS THE OUTER EDGE RELATIVELY PARALLEL TO THE LONGITUDINAL AXIS OF THE ELEVATOR. REPAIRED IAW SRM 55-00-01 FIG.7 (SHEET1) VOL. I.

Part: TRANSDUCER — FAILED (MLG) · airframe 89,234 hrs · 24,936 cycles

SOON AFTER GEAR EXTENSION, RECEIVED A LEVEL 2 'ANTISKID FAIL' ALERT. COMPLIED WITH QRH AND LANDED ACFT. DURING ROLL-OUT, TOWER REPORTED THAT AT LEAST 1 TIRE HAD FAILED. CALLED FOR CRASH TRUCK. THEY REPORTED NO SEVERE DAMAGE, BUT THAT WE HAD 2 FAILED TIRES. ANTI-SKID FAIL IS A REPEAT WRITE-UP. ACFT WAS TRACKING STRAIGHT DOWN THE RUNWAY WHEN TIRES FAILED. REPLACED NR 1 & NR 5 WHEEL SPEED TRANSDUCERS IAW AMM 32-45-03-2.

Part: TRANSDUCER — FAILED (MLG) · airframe 89,234 hrs · 24,936 cycles

SOON AFTER GEAR EXTENSION, RECEIVED A LEVEL 2 'ANTISKID FAIL' ALERT. COMPLIED WITH QRH AND LANDED ACFT. DURING ROLL-OUT, TOWER REPORTED THAT AT LEAST ONE TIRE HAD FAILED. CALLED FOR CRASH TRUCK. THEY REPORTED NO SEVERE DAMAGE, BUT THAT WE HAD 2 FAILED TIRES. ACFT WAS TRACKING STRAIGHT DOWN THE RUNWAY WHEN TIRES FAILED. REPLACED NR 1 & NR 5 WHEEL SPEED TRANSDUCERS IAW AMM 32-45-03-2. C/W REJECTED TAKEOFF TEST. REINSTALLED LI, LO, RI, & RO HUBCAPS REF M/M 27-60-00-5 PERFORMED ANTISKID ALERT TEST REF M/M 32-45-03-2. ALL TEST NORMAL. ACFT OK FOR SERVICE.

Part: LEAD — MALFUNCTIONED (ENGINE) · airframe 89,189 hrs · 24,915 cycles

DURING CLIMBOUT ON A REDUCED POWER TAKEOFF, PASSING ABOUT 1500-2000 FT. RECEIVED A NR 1 ENGINE EXCEEDENCE WITH TEMP REACHING ABOUT 970. A MINUTE OR SO LATER RECEIVED A SIMILAR INDICATION WITH DIAL INDICATING A HIGHER TEMP, EVENTUALLY WITH A PEAK AT 1070C AND AT ONE POINT RECEICVED AN "ENG 1 EGT HIGH" MESSAGE. ALL OTHER ENGINE INDICATIONS SEEMED NORMAL, SHUTDOWN NR 1 ENGINE AND RETURNED TO DEPARTURE. DURING DEBRIEF, CREW STATED EGT WAS SPIKING FOR A FEW SECONDS AND WOULD RETURN TO NORMAL AND THEN SPIKE AGAIN, ALSO DID NOT NOTICE ANY FUEL FLOW ABNORMALITIES. CHECKED THERMO COUPLE RESISTANCE NO FAULTS FOUND. REMOVED THERMOCOUPLES AND HARNESSES AS A PRECAUTION. R & R IAW MM 77-21-02-2. INSTALLED NR 1 EGT THERMOCOUPLE AND HARNESS. RAN ENGINE, EGT WAS WITHIN LIMITS AND STEADY. OK FOR SERVICE. IAW AMM 77-21-01-2.

Part: ANTI-SKID SYS — FAILED (MLG) · airframe 83,085 hrs · 22,697 cycles

ANTI-SKID FAIL ALERT AFTER T/O. WOULD NOT TEST AFTER RECYCLE TO OFF THEN ON. PEFORMED ANTI-SKID TEST, IAW 32-45-00-5. OPS CHECKS GOOD. NO HISTORY. OK FOR SERVICE. REMOVED AND REPLACED SKID CONTROL UNIT IAW MM 32-45-01-2. TEST SATISFACTORY. OK TO CONTINUE.

Part: COMPUTER — MALFUNCTIONED (FMS) · airframe 83,085 hrs · 22,697 cycles

LOST ALL TIME, FUEL AND ACFT WEIGHT PREDICTIONS FROM BOTH FMS NR 1 AND NR 2 WHILE ENROUTE. CHK NR 1 AND NR 2 VIA LAST LEG FAULT, NO FAULT REPORTED. PERFORMED R-T-S ON NR 1 AND NR 2 VIA, OPS CHK GOOD IAW MM 31-43-01-5. PRECAUTIONARY PERFORMED, FIM 34-63-01 STEP "C" DUAL FMS FAIL TEST, NR 1 AND NR 2 FMS TEST OK. ACFT OK FOR SVC.

Part: STIFFENER — CRACKED (ZONE 500) · airframe 82,824 hrs · 22,605 cycles

LT WING L/E FOUND STIFFENER WITH CRACK. REPAIRED AREA IAW SRM 57-00-01 FIG 10 VOL I.

Part: RIB — CRACKED (LWS 795) · airframe 82,824 hrs · 22,605 cycles

LT WING OUTBOARD FLAP FOUND CRACK ON OTBD FITTING. REPAIRED AREA IAW EA NR 8-5750-128520.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 82,824 hrs · 22,605 cycles

DURING INSPECTION OF HORIZONTAL STABILIZER CONSTANT AND CUTER SECTION SKIN PANELS FOUND NR 3 PANELS WITH CRACKS. REPAIRED AREA IAW EA NR 8-5510-126253 AND EA NR 8-5510-126254.

Part: SKIN — CRACKED (ZONE 600) · airframe 82,824 hrs · 22,605 cycles

RT WING LEADING EDGE FOUND CRACK ON SKIN L/E LOWER SIDE. REPAIRED SKIN IAW SRM 57-10-00 FIG 68 SHT 2 VOL I.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 82,824 hrs · 22,605 cycles

LOWER AFT COMPT LIGHT CORROSION ON UPPER SIDE FLOORBEAM AND ANGLE SUPPORT FLOOR. REPAIRED AREA IAW SRM 53-00-01 FIG 9 VOL I.

Part: SKIN — LOOSE (LT ELEVATOR) · airframe 82,824 hrs · 22,605 cycles

LT OTBD ELEVATOR FOUND 150 LOOSE FASTENERS ON LWR SKIN T/E. REPAIRED T/E SECTION AND SKIN IAW DWG ALC7345 & SRM 55-10-00 FIG 8 VOL I.

Part: SKIN — NONE (ZONE 100) · airframe 82,824 hrs · 22,605 cycles

ACFT DOOR PACK NR 2 EXTERNAL SKIN FOUND EXISTING FLUSH REPAIR. REPAIRED AREA IAW EA NR 8-5240-128516.

Part: FRAME — CRACKED (ZONE 100) · airframe 82,824 hrs · 22,605 cycles

AIR COND COMPT FOUND CRACK ON CAP FRAME, REPAIRED AREA IAW SRM 53-00-01 FIG 2, SHT 2, VOL I.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 82,824 hrs · 22,605 cycles

MAIN CABIN INSPECTION FLOOR PANEL AND SEAT TRACKS FOUND CRACKS ON TRACK. REPAIRED AREA IAW SRM 53-70-00 FIG 1, SHT 1 AND 2 VOL I.

Part: FRAME — CRACKED (ZONE 100) · airframe 82,824 hrs · 22,605 cycles

DURING INSPECTION ON AVIONIC COMPT FOUND CRACK ON FRAME. REPAIRED FRAME IAW SRM 53-30-00 VOL I, FIG 5.

Part: STANCHION — NONE (ZONE 100) · airframe 82,824 hrs · 22,605 cycles

CTR CARGO COMPARTMENT EXISTING REPAIR ON STANCHION. REPAIRED AREA IAW EA 8-5310-126251.

Part: STANCHION — NONE (ZONE 100) · airframe 82,824 hrs · 22,605 cycles

CTR CARGO COMPARTMENT EXISTING REPAIR ON STANCHION. REPAIRED AREA IAW EA 8-5310-126252.

Part: STANCHION — UNKNOWN (ZONE 100) · airframe 82,824 hrs · 22,605 cycles

CTR CARGO COMPARTMENT EXISTING REPAIR ON STANCHION. REPAIRED AREA IAW EA 8-5310-126245.

Part: STANCHION — UNKNOWN (ZONE 100) · airframe 82,824 hrs · 22,605 cycles

CTR CARGO COMPARTMENT EXISTING REPAIR ON STANCHION. REPAIRED AREA IAW EA 8-5310-126246.

Part: WEB — CRACKED (ZONE 700) · airframe 82,824 hrs · 22,605 cycles

DURING INSPECTION NLG FOUND CRACK ON VERTICAL WEB. REPAIRED WEB IAW SRM 53-40-00 FIG 34, VOL I.

Part: WEB — CRACKED (NLG WW) · airframe 82,824 hrs · 22,605 cycles

DURING INSPECTION NLG WW FOUND CRACK ON VERTICAL WEB. REPAIRED WEB IAW SRM 53-40-00 FIG 34 VOL I.

Part: STANCHION — UNKNOWN (ZONE 100) · airframe 82,824 hrs · 22,605 cycles

CTR CARGO COMPARTMENT EXISTING REPAIR ON STANCHION. REPAIRED AREA IAW EA NR 8-5310-126247.

Part: FRAME — WORN (ZONE 100) · airframe 82,824 hrs · 22,605 cycles

DURING INSPECTION ON AVIONIC COMPT FOUND DEEP WEAR ON FRAME. REPAIRED AREA IAW SRM 53-30-00 FIG 4 VOL I.

Part: STANCHION — UNKNOWN (ZONE 100) · airframe 82,824 hrs · 22,605 cycles

CTR CARGO COMPARTMENT EXISTING REPAIR ON STANCHION. REPAIRED AREA IAW EA 8-5310-126248.

Part: STANCHION — UNKNOWN (ZONE 100) · airframe 82,824 hrs · 22,605 cycles

CTR CARGO COMPARTMENT EXISTING REPAIR ON STANCHION. REPAIRED AREA IAW EA 8-5310-126250.

Part: STANCHION — UNKNOWN (ZONE 100) · airframe 82,824 hrs · 22,605 cycles

CTR CARGO COMPARTMENT EXISTING REPAIR ON STANCHION. REPAIRED AREA IAW EA 8-5310-126249.

Part: FRAME — CRACKED (ZONE 100) · airframe 82,824 hrs · 22,605 cycles

DURING INSPECTION ON AVIONIC COMPT FOUND CRACK ON FRAME. REPAIRED FRAME IAW SRM 53-30-00 FIG 11 VOL I.

Part: FRAME — UNKNOWN (ZONE 100) · airframe 82,824 hrs · 22,605 cycles

AFT CARGO COMPARTMENT EXISTING REPAIR ON FRAME. REPLACED FRAME IAW DWG AJC7363.

Part: SKIN — CRACKED (ZONE 500) · airframe 82,824 hrs · 22,605 cycles

LT WING SLATS, FOUND CRACK AND NR 10 FASTENERS U/S ON CORNER SKIN INTERNAL SIDE SLAT NR 2. REPAIRED AREA IAW SRM 57-10-00 FIG 31, VOL I.

Part: SKIN — DENTED (ZONE 100) · airframe 82,824 hrs · 22,605 cycles

EXT FUSELAGE LWR SURFACE FOUND DEEP DENT ON SKIN 1 INCH BY 1 INCH DEEP .078 INCH. REPAIRED AREA IAW SRM 53-20-00, VOL I, FIG 6, SHT 3-4.

Part: RIB — CRACKED (ZONE 500) · airframe 82,824 hrs · 22,605 cycles

LT WING LEADING EDGE, FOUND CRACK AND RIVETS U/S ON ANGLE SUPPORT REFUEL PANEL. REPAIRED RIB IAW SRM57-00-01 VOL I, FIG 10, SHT 1,3,4.

Part: ANGLE — CRACKED (ZONE 500) · airframe 82,824 hrs · 22,605 cycles

LT WING LEADING EDGE FOUND NR 1 CRACK ON TEE ANGLE. REPAIRED AREA IAW SRM 57-10-00 FIG 49 VOL I.

Part: STANCHION — UNKNOWN (ZONE 100) · airframe 82,824 hrs · 22,605 cycles

FWD CARGO COMPARTMENT EXISTING REPAIR ON STANCHION. REPLACE STANCHION IAW DWG ADA3353.

Part: STANCHION — UNKNOWN (ZONE 100) · airframe 82,824 hrs · 22,605 cycles

FWD CARGO COMPARTMENT EXISTING REPAIR ON STANCHION. REPLACE STANCHION IAW DWG ADA3353.

Part: STANCHION — UNKNOWN (ZONE 100) · airframe 82,824 hrs · 22,605 cycles

FWD CARGO COMPARTMENT EXISTING REPAIR ON STANCHION. REPLACE STANCHION IAW DWG ADA3353.

Part: STANCHION — UNKNOWN (ZONE 100) · airframe 82,824 hrs · 22,605 cycles

FWD CARGO COMPARTMENT EXISTING REPAIR ON STANCHION. REPLACE STANCHION IAW DWG ADA3353.

Part: SKIN — DENTED (ZONE 600) · airframe 82,824 hrs · 22,605 cycles

DURING INSPECTION RT WING LWR SURFACE FOUND SCRATCH 22 INCHES LONG AND DEEP DENT 3 INCHES BY 3 INCHES DEEP .161 INCH ON LWR SKIN OF OUTBD AILERON. DAMAGE IS "NOT/FLIGHT AIRCRAFT STRIKE DAMAGE". REPAIRED AREA IAW SRM 57-10-00 VOL I FIG 2 SHT 2 NOTE 8.

Part: PUMP — FAILED (HYD SYSTEM) · airframe 82,816 hrs · 22,604 cycles

AT CRUISE FLT, NR 2 HYDRAULIC QTY AND PRESSURE WENT TO ZER0. NO HIGH TEMP INDICATED. COMPLIED WITH QRH AND RETURNED TO MEMPHIS. REMOVED AND REPLACED 2/1 NON-REV MOTOR PUMP SHUTOFF VALVE

Part: PUMP — FAILED (HYD SYSTEM) · airframe 82,816 hrs · 22,604 cycles

AT CRUISE FLT, NR 2 HYDRAULIC QTY AND PRESSURE WENT TO ZER0. NO HIGH TEMP INDICATED. COMPLIED WITH QRH AND RETURNED TO MEMPHIS. REMOVED AND REPLACED 2/1 NON-REV MOTOR PUMP SHUTOFF VALVE.

Part: ATTACH FITTING — DAMAGED (TE FLAPS) · airframe 81,695 hrs · 22,028 cycles

DURING DEPARTURE, PRIOR TO FLAPS RETRACTION RIGHT FLAP TAPES MOVED FROM 20 PERCENT TO 28 PERCENT. AIRCRAFT REQUIRED SIGNIFICANT RT AILERON TO KEEP WINGS LEVEL. ON ARRIVAL AT KMEM, A CONTROLLABILITY CHECK WAS PERFORMED WHEN FLAPS WERE EXTENDED TO 22' RIGHT FLAP TAPE INDICATED 30 AND 3/4 RIGHT LATERAL CONTROL WAS REQUIRED TO MAINTAIN WINGS LEVEL. FLAPS WERE RETRACTED AND A O EXT APPROACH AND LANDING WAS ACCOMPLISHED WITHOUT INCIDENT. REMOVED AND REPLACED ATTACH FITTING FROM RT O/B FLAP O/B HINGE BRACKET ASSY IN REF TO SRM 51-31-01 VOL2 51-33-01 VOL2 AND 51-35-01 VOL2.

Part: SKIN — DENTED (FUSELAGE) · airframe 81,273 hrs · 21,822 cycles

FUSELAGE SKIN AFT OF CENTER PIT DOOR HAS 3 EACH DENTS REPAIRED AREA AS REQUIRED IAW SRM 53-20-00 FIG 13.

Part: WEB — CRACKED (FUSELAGE) · airframe 81,273 hrs · 21,822 cycles

R-3 DOOR AFT JAMB TORQUE BOX WEB CRACKED AT FLOOR LINE REPAIRED WEB IAW SRM 53-50-00 FIG 19 SHEET 2.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 81,273 hrs · 21,822 cycles

FWD PIT DOOR LOWER SILL AFT AND FWD ENDS BELOW OMNI ROLLERS SUPPORT IS CORRODED REWORKED AREAS AS REQUIRED IAW SRM 53-50-00 FIGURE 15.

Part: TORQUE BOX — CRACKED (FUSELAGE) · airframe 81,273 hrs · 21,822 cycles

R-3 DOOR FWD JAMB TORQUE BOX WEB CRACKED AT FLOOR LINE REPAIRED WEB IAW SRM 53-50-00 FIG 19 SHEET 1.

Part: SEAT TRACK — GOUGED (BS 1079-1099) · airframe 81,273 hrs · 21,822 cycles

MAIN CARGO COMPT SEAT TRACK HAS GOUGED AREA AT F/S 1079-1099 LBL 48 REMOVED AND REPLACED SEAT TRACK SECTION IAW SRM 53-70-00 FIG1 SHEET 1.

Part: SEAT TRACK — CORRODED (BS 515) · corrosion level 2 · airframe 81,273 hrs · 21,822 cycles

MCD - SEAT TRACK AT STA 515 LBL 27.5 IS EXFOLIATED. REMOVE, FABRICATED AND INSTALLED NEW SEAT TRACK IAW SRM 53-70-00 AND 51-31-01.

Part: SEAT TRACK — GOUGED (BS 899-919) · airframe 81,273 hrs · 21,822 cycles

MAIN DECK COMPT SEAT TRACK HAS GOUGED AREAS AT F/S 899-919 LBL 48 REMOVED, FABRICATED AND INSTALLED NEW SEAT TRACK IAW SRM 53-70-00 AND 51-31-01.

Part: NUT — INOPERATIVE (ZONE 700) · airframe 80,550 hrs · 21,515 cycles

CENTER GEAR RT PILLOW BLOCK :FWD BOLT BACKED OFF APPROX 1/2 INCH. AFT BOLT LOOSE AND CAN BE ROTATE BY HAND. UPON DISASSEMBLY FOUND PILLOW BLOCK NUTS DO NOT SELF LOCK. REMOVED LT TRUNNION PILLOW BLOCK AND PERFORMED HFEC AND FPI INSPECTION OF HOLE BORE AND BLOCK ASSY PER NDTSPM, TP-MDC-93K0393. NO DEFECTS WERE NOTED. FABRICATED AND INSTALLED FIVE (5). REPAIR BUSHINGS PER CMM 32-15-01. PERFORMED A BREAK AWAY TORQUE CHECK ON THE FOUR (4) PILLOW BLOCK BOLT NUTS PER NASM25027 3.8.2.2.2 TABLE III PRIOR TO RE-INSTALLATION OF TRUNNION PILLOW BLOCK. RE-INSTALLED LT TRUNNION PILLOW BLOCK AND CENTER LG ASSY PER WC 32T7701.

Part: CYLINDER — CRACKED (MLG) · airframe 80,550 hrs · 21,515 cycles

DURING LAX "B" CHECK VISIT WO 36669; FOUND CENTER GEAR RETRACT CYLINDER CRACKED AT ROD END. [SUP 05-30-07] REMOVED AND REPLACED CENTER GEAR RETRACT CYLINDER PER MM 32-38-01-2. INSTALLED NEW CLG ROD END CLEVIS ON RETRACT ACTUATOR PER MM 32-38-01-2.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 78,622 hrs · 20,619 cycles

CENTER PIT STA 1731 ABOVE L45R TORQUE BOX WEB (SILL AREA) SKIN BULGE AND SHEARED RIVET. REPAIRED IAW FEDEX EA E8-5310-96470. FUSELAGE CENTER CARGO DOOR JAMB FRAME SPLICE AT STA 1708 REPAIR.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 78,622 hrs · 20,619 cycles

CENTER LWR FUSELAGE FRAME SHEAR TIES AND SKIN HAS LIGHT CORROSION FROM STA 1510 TO 1518 STR 47L TO STR 47R. COMPLIED WITH FEDEX EA E8-5330-96467, FUSELAGE CORROSION IN SKIN AND INTERNAL BULKHEAD TEE, STA 1521 REPAIR.

Part: REPAIR — NONE (ZONE 300) · airframe 78,622 hrs · 20,619 cycles

FOUND FLUSH REPAIR LOCATED AT RIGHT HORIZONTAL STAB STA XE98 TO XFS 175 UPPER. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED AND REPLACED DOUBLER IAW DC10-10 SRM 51-31-01 VOL II, 55-00-01 VOL I FIG 3 SHEET 2, 51-35-01 VOL II. MINOR REPAIR.

Part: SKIN — CORRODED (BS 1510-1518) · airframe 78,622 hrs · 20,619 cycles

CENTER LWR FUSELAGE FRAME SHEAR TIES AND SKIN HAS LITE CORROSION FROM STA 1510 TO 1518 STR 47L TO STR 47R. CORRECTIVE ACTION-N00285.

Part: SKIN — DAMAGED (BS 1054 S5L) · airframe 78,622 hrs · 20,619 cycles

ARCHING AT FASTENER HOLE ON EXTERNAL FUSELAGE AT STA 1054, LONGERON 5L. REMOVED DAMAGED AREA, FAB'D DOUBLERS, INSTALLED DOUBLERS IAW DC10-30 SRM 53-20-00 VOL 1, 53-20-00 FIG 6 VOL 1, 51-35-01 VOL II. MINOR REPAIR.

Part: REPAIR — UNKNOWN (ZONE 900) · airframe 78,622 hrs · 20,619 cycles

FOUND REPAIR LOCATED AT RT WING, INB FLAP STA XIFH167, UPPER SKIN. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED EXISTING DOUBLER IAW DC10 SRM 51-35-02 VOL II. FABRICATED NEW DOUBLER IAW DC10 SRM 57-10-00 FIG 85 VOL.I. ALODINED AND PRIMED IAW DC10 SRM 51-21-01 VOL II. INSTALLED DOUBLER IAW DC10 SRM 51-35-02 VOL II. MINOR REPAIR.

Part: REPAIR — UNKNOWN (ZONE 100) · airframe 78,622 hrs · 20,619 cycles

FOUND FLUSH REPAIR LOCATED AT STA 859 L32R. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. FABRICATED DOUBLER IAW DWG 7097 REV.U. FABRICATED FILLER IAW DC10-30 SRM 53-20-00 FIG 13 SHT 4. INSTALLED IAW DC-10-30 SRM 51-21-01 VOL.II. ALODINED, PRIMED, TOPCOATED IAW DC10-30 SRM 51-21-01 VOL.II. MINOR REPAIR.

Part: O-RING — LEAKING (NR 1 ENGINE) · airframe 76,395 hrs · 19,793 cycles

NR 1 ENG EXCESSIVE OIL USAGE OR LOSS, AT ENG START HAD 19 QTS AFTER ENGINE START WAS APPROX 17 QTS. AT 1.5 HRS INTO FLT READ 11 QTS AND STILL DROPPING 7 QTS AT TOUCHDOWN 4 HRS 10 MIN TOTAL TIME. REMOVED NR 10 DRIVE ADAPTER, FOUND O-RING SEAL ON IDLER GEAR SECTION BAD. REMOVED AND REPLACED O-RING. INSTALLED ADAPTER PER DC10-30 MM 72-65-00-8. RECHECKED AREA WITH PRESSURE ADAPTER, NO LEAKS NOTED. REMOVED ADAPTER AND REINSTALLED SHAFTS AND COVERS. REINSTALLED GENERATOR PER DC10-30 MM 24-21-04 AND REINSTALLED CSD PER DC 10-30 MM 24-11-09. RAN ENGINE AT HIGH POWER AND RECHECKED DRAINS, NO LEAKS NOTED.

Part: PROXIMITY SENSOR — MALFUNCTIONED (MLG) · airframe 74,780 hrs · 19,249 cycles

AFTER T/O OF BOSTON GEAR HANDLE WOULD NOT RAISE. AFTER TWO ATTEMPTS GEAR HANDLE WAS RAISED. HOWEVER BOTH MAINS INDICATE UNSAT (RED LIGHTS AT S/O AND PILOTS INDICATORS ILLUMINATED). FOLLOWED QRH DIRECTION, WITH SAME RESULTS. FLEW REMAINING FLIGHT AT < 260 KIAS. T/S AS PER TAFI MANUAL REF 32-30 FAULT CODE -AC-, PERFORMED BITE TEST OF PROXIMITY BOX WITH NO FAULTS NOTED. REMOVED AND REPLACED PROX BOX AS PRECAUTIONS ALL TEST PASS NO FAULTS NOTED REF DC-10 MM REF 32-61-01-2. A/C OK FOR SERVICE. ALL INDICATIONS NORMAL.

Part: CONTROLLER — FAILED (PNEUMATIC SYS) · airframe 73,041 hrs · 18,727 cycles

APPROXIMATELY 2.45 HRS INTO FLIGHT, LEVEL AT 33,000 FT EXPERIENCED NR 3 MANIFOLD FAILURE LIGHT. ACCOMPLISHED RED TABS LIGHT WENT OUT. DIVERTED TO INDY. REMAINDER OF FLIGHT UNEVENTFUL. REMOVED AND REPLACED MANIFOLD FAIL CONTROLLER PER DC-10 M/M 36-23-01-2, NO DEFECTS NOTED. PREMATURE REMOVAL/INSTALLATION OFF MFG 35008-2, POS ONL SRL B214, TAG 940710, ON MFG 35008-2 SRL B306, TAG 495125.

Part: DRIVE LINK — DAMAGED (SLATS & FLAPS) · airframe 72,644 hrs · 18,605 cycles

I/B SLAT DRIVE MECHANISM FWD BEARING AFT RETAINER GREASE SEAL IS BLOWN OUT OF POSITION. REMOVED AND REPLACED SLAT DRIVE MECHANISM PER AMM 27-83-01-2.

Part: BRACKET — CRACKED (CARGO DOOR) · airframe 72,058 hrs · 18,403 cycles

AFT CARGO DOOR HAS LWR AFT BRACKET CRACKED. REMOVED AND REPLACED BRACKET IAW DC10 SRM 51-31-01 VOL 2.

Part: FRAME — GOUGED (RT PYLON) · airframe 72,058 hrs · 18,403 cycles

RIGHT PYLON UPPER PANEL 487EL, INNER FRAME GOUGED AND PREVIOUS REPAIR AND L/E CRACKED. CLOSING ACTION ON 04/07/03. REMOVED FRAME IAW SRM 51-35-01. FAB NEW FRAME WITH TRAVEER T2/324411. INSTALLED NEW FRAME IAW SRM 51-31-01 AND SRM 51-31-01.

Part: ANGLE — BROKEN (NR 3 PYLON) · airframe 72,058 hrs · 18,403 cycles

NR 3 PYLON TOP PANEL 487 RT, RT SIDE NUT PLATE L-ANGLE BROKEN. REMOVED BROKEN ANGLE IAW SRM 51-31-01. REMOVED DOUBLER IAW SRM 51-31-01. FABBED NEW DOUBLER IAW DPS 4.710, TREATED AND PRIMED DOUBLER IAW SRM 51-21-01. DRILLED UP NEW ANGLE T2/325729 IAW SRM 51-31-01. TREATED AND PRIMED NEW ANGLE IAW SRM 51-21-01. INSTALLED ANGLE AND DOUBLER IAW SRM 51-31-01.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 72,058 hrs · 18,403 cycles

N 317 MAIN CARGO COMPT, SEAT TRACK IS CRACKED 10 INCHES LONG AT FS 960 LBL 28. REMOVED DAMAGED PORTION OF SEAT TRACK FROM STA 949 TO 989 AND R & R IAW SRM 53-70-00. REPAIR PARTS FABRICATED ON TRAVELER T2/323005 AND T2/323056, PAINTED IAW SRM 51-21-02. INSTALLED REPAIR PARTS IAW SRM 53- 70-00

Part: PIN — LOOSE (TAIL CONE) · airframe 72,058 hrs · 18,403 cycles

TAILCONE LT SIDE MATING FLANGE UPPER ALIGNMENT PIN HOLE FOR THE PIN HAS EXCESSIVE PLAY. REMOVED FILLER AND PIN IAW SRM 51-31-01. FAB NEW FILLER IAW SRM 53-30-00 FIG 1, INSTALLED IAW SRM 51-31-01.

Part: SEAL — CRACKED (TAIL CONE) · airframe 72,058 hrs · 18,403 cycles

NR 655 TAILCONE FWD UPPER LT METAL SEAL CRACKED ANS CHAFED. CLOSING ACTION ON 04/05/03. REMOVED LT FWD UPPER METAL SEALS 2EA. FROM TAILCONE IAW SRM 51-31-01, RECEIVED REPLACMENT SEALS ON ATTACHED TRAVELER NR T2/324508. INSTALLED REPLACEMENT SEALS IAW SRM 51-31-01.

Part: ROLLER TRAY — CRACKED (CARGO AREA) · airframe 72,058 hrs · 18,403 cycles

NR 771 CENTER PIT, STA 1741 AT RBL 45, CARGO ROLLER TRAYS CRACKED BETWEEN OMNI ROLLERS. CLOSING ACTION ON 04/05/03. REMOVED AND REPLACED DAMAGED ROLLER TRACK WITH 60-11325/29 BATCH NR 0000306010. IAW SRM 53-42-01 FIG 13. SRM 51-21-01.

Part: SPAR CAP — CRACKED (HORIZONTAL STAB) · airframe 65,830 hrs · 16,442 cycles

HFEC INSP FOUND CRACK ON RHS OF THE UPPER SURFACE OF THE UPPER OUTER REAR SPAR CAP''S AFT BARREL NUT HOLES. *S/D* REPAIRED PER FEDEX EA 8-5510-52866.

Part: HARNESS — SHORTED (CARGO BULKHEAD) · airframe 63,830 hrs · 16,442 cycles

EXTERNAL PWR FEEDER CABLES FOUND SHORTED AND BURNT WHICH CAUSED FIRE AT FWD CARGO BULKHEAD AREA. *S/D* REMOVED AND REPLACED PER WDM STANDARD MAINTENANCE PRACTICES 20-10-01, 20-20-01 & WDM 24-41-01. EXT PWR OPS CK SAT PER 24-53-01.

Part: HARDWARE — LOOSE (NR 1 PYLON)

12 OFF MOUNTING BOLTS LOOSE AND 3 OFF NUTS MISSING FROM SHEAR WEB FORGINGS ON AFT NR 1 PYLON FRAME, ADJACENT TO SPHERICAL BEARING FITTING. REMOVED AND REPLACED PER MM 70-00-00-2.

Part: CONTROL CABLE — BROKEN (NR 6 LE SLAT)

LT WING NR 6 SLAT EXTEND CABLE FOUND SNAPPED OFF. REMOVED AND REPLACED IAW MM 27-89-11-4. CABLES RE-RIGGED AND FUNCTIONAL TEST CARRIED OUT IAW MM 27-80-00-05. FOUND SATISFACTORY.

Part: SWITCH — INOP (AC DOOR)

AT FL 180 AIR COND DOOR LIGHT CAME ON. A/C REMAIN PRESS, RETURN TO MEM. *S/D* REMOVED AND REPLACED BOTH LEFT SIDE ACCESS DOOR SWITCH IAW MM 52-70-07. REMOVED AND REPLACED RING TERMINAL, P1-1618 AND RE-TERMINATED WIRES IAW MM CHAPTER 20. AIR COND DOOR LIGHT CK GOOD IAW MM 52-70-07.

Part: HYD FUSE — BLOWN (RT MLG WW)

GEAR HANDLE W/N COME UP AFTER T/O, STEERING HANDLE CENTERED, GROUND TENSION CHECKED OK ON TAT. PRESSED HANDLE RELEASE AND HANDLE STILL W/N COME UP. REMOVED AND REPLACED TRIM CYLINDER INTERLOCK FUSE, SYS OPS CK NORMAL PER MM 32-31-06-02.

Part: WARNING SYST — MALFUNCTION (CABIN DOOR)

AFTER TAKEOFF, AIRCRAFT WOULD NOT PRESSURIZE. DISCOVERED 6 FT AFT CABIN DOOR OPEN APPROX 2.5 INCHES. DUMPED FUEL AND LANDED VCP WITHOUT INCIDENT. RESET DOOR PER M/M 52-10-01-2 ARMS OK. CHECKED FOR ELECTRICAL ANOMOLIES TO LOCK PIN RELEASE AND ACTUATOR. FOUND NO POWER COMING OUT OF AFT DOOR LIMIT SWITCH IN THE DOOR STOW POSITION. OK TO CONTINUE ON PREVIOUS DEFERRED. INSTALLED DOOR WARNING LIGHT STRIKER PLATE, POSITION SWITCH PER M/M 52-70-00, DOOR INDICATION OPS CHECK GOOD PER M/M 52-70-00.

Part: BULKHEAD PANEL — CORRODED (CTR MLG WW)

SNRM N00944, CENTER GEAR WHEEL WELL, LT BULKHEAD ACCESS PANELS 146AN AND 146BN PANEL LAND CORRODED. *S/D* REWORKED PER EA WORK INSTRUCTIONS, EA NR 8-5310-31745, STEPS 1 TO 5 FOR AFT ACCESS PANEL 146 IN, AND STEPS 1 TO 3 FOR FWD ACCESS PANEL 146BN FWD ACCESS PANEL 146BN. FOLLOW-UP ACTION PERMANENT REPAIR TO BE ACCOMPLISHED DURING NEXT SCHEDULED C-CHECK.

Part: FRAME — CRACKED (CRT MLG DOORWAY)

SNRM N 00335, CENTER GEAR LT DOOR FRAME HAS AN EIGHT INCH CRACK ALONG FORWARD FACE AT THE FORWARD INBOARD CORNER. *S/D* REMOVED DAMAGED BUTT RIB, INSTALLED NEW BUTT RIB, INSTALLED NEW FRAME AS PER SRM 51-00-00 PG 2 ITEM C, COMPLETED 10/31/96.

Part: FLT CONT CABLES — BROKEN (CTR GEAR WW)

DURING REPLACEMENT OF HYD REVERSABLE MOTOR PUMP SHUTOFF VALVE, BROKEN FLIGHT CONTROL CABLES WERE FOUND IN CENTER GEAR WELL. REMOVED AND REPLACED BOTH FLAP INPUT AILERON LOCKOUT CABLE RUNS. ADJUSTED AS PER 27-10-00 PAGE 515, RII REQUIRED. OPS CK GOOD, (P/N S4913810AS13117), (S4913801AS112404), (S4916997AS04808).