N68052

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 74,481 hrs · 33,729 cycles

EMER LIGHT BATTERY 1 LOW ALERT ON POST FLIGHT INSPECTION. R & R EMER BATTERY PACK. OPERATIONS CHECKED NORMAL.

Part: ACTUATOR — MALFUNCTIONED (LT AILERON) · airframe 74,238 hrs · 33,617 cycles

AIRCRAFT TAKES AT LEAST 3.5 DEGREES OF LT DOWN AILERON TRIM FOR LEVEL FLIGHT. REMOVED AND REPLACED LT IBD AILERON ACTUATOR IAW MM.

Part: SENSOR — FAILED (NR 1 ENG OIL) · airframe 74,121 hrs · 33,544 cycles

NR 1 ENGINE OIL TEMP HIGH, 194 DEGREES AT CRUISE. COMPLIED WITH QRH & EVENTUALLY SHUTDOWN NR 1 ENG. R & R NR 1 ENGINE OIL TEMP SENSOR IAW MM 79-32-01-2, FOUND OIL IN CONNECTOR SUSPECT OIL TEMP BULB LEAKING. CLEANED CONNECTOR. RUN CHECK IAW JRH CH 5, OIL TEMP CHECKED GOOD.

Part: MOTOR — CRACKED (RT HORIZ STAB) · airframe 73,663 hrs · 33,285 cycles

PASSING FL190 DURING CLIMB GOT A LEVEL 2 HYD 3 FAIL ALERT, QTY WENT TO ZERO. ALTERNATE GEAR EXTENSION WAS USED IAW QRH. LEAK APPARENTLY COMING FROM REAR STAB COMPARTMENT ACCESS PANEL AREA. TROUBLESHOOTING IN PROGRESS. FOUND LEAK TO BE COMING FROM RT STAB TRIM PRIMARY MOTOR PUMP. R & R NR 1 STAB TRIM MOTOR IAW MM 27-43-01-2 UP TO STEP 3 B 9. ACCOMPLISHED NR 1 STAB TRIM MOTOR LEAK CHECK IAW AMM 27-43-01-2, LEAK CHECK GOOD. OPERATIONS CHECKED NORMAL.

Part: TOWERSHAFT — FAILED (NR 3 ENGINE) · airframe 73,088 hrs · 32,983 cycles

FL 350 CRUISE FLIGHT ENG 3 FLAMED OUT DUE TO HIGH OIL PRESS & 0 ZERO N2 COMPLIED WITH QRH DIVERTED TO KMIA. NR 3 ENG R & R DUE TO TOWER SHAFT FAILURE, OPERATIONS CHECKED GOOD.

Part: STRUCTURE — CORRODED (RT MLG WW) · corrosion level 2 · airframe 72,738 hrs · 32,825 cycles

RT WW SLANT PANEL AREA EDGE MEMBER CORRODED. REMOVED EDGE MEMBER SLANT PANEL. FABRICATED EDGE MEMBER IAW DWG AEA0449. INSTALLED NEW EDGE MEMBER IAW SRM 51-35-01, VOL II.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,738 hrs · 32,825 cycles

RT SLANT PANEL LOWER HORIZONTAL TEE ANGLE CORRODED. REMOVED CORRODED TEE ANGLE. LOCATED AND DRILLED UP HOLES IN NEW TEE ANGLE. INSTALLED NEW TEE ANGLE IAW DWG.

Part: BULKHEAD — CRACKED (BS 1521) · airframe 72,261 hrs · 32,595 cycles

RIGHT W/W HAS A 1 INCH CRACK INNER WALL 30 INCHES FORWARD OF BS 1521 & 2 FEET DOWN. REPAIR WAS ACCOMPLISHED AND INSTALLED REF EA 8-5310-157386, SEQ NR 255. EA 8-5310-157386 FINAL DRAFT SEQ 257 OF WO 58015 FOR MX PERFORMED.

Part: WEB — CRACKED (BS 1381) · airframe 72,261 hrs · 32,595 cycles

WHEEL WELL LEFT BULKHEAD CRACKED 4 INCHES AFT OF BS 1381 AND 3 INCHES DOWN FROM UPPER BULKHEAD. REPAIRED AND INSTALLED IAW EA 8-5310-157385 SEQ 254.

Part: MODULE — FAILED (OXYGEN SYSTEM) · airframe 69,642 hrs · 31,253 cycles

DON OXYGEN MASK HORN AND LIGHT TEST RESET LIGHT MODULE DOES NOT ILLUMINATE. RELAMPED NO HELP, TEMP SWAPPED LENS MODULES, PROBLEM MOVED. REQ LENS MODULE, CENTER PIN SPRING COLLAPSED. PARTS ORDERED. REMOVED AND REPLACED DON OXYGEN MASK TEST LIGHT MODULE PER SWPM CHAP 20. OPS CHECKS GOOD.

Part: SWITCH — NO TEST (MASTER BATTERY) · airframe 69,383 hrs · 31,136 cycles

EMERGENCY POWER TEST FAIL DURING PRE-FLIGHT. RE-SELECTED BATTERY SWITCH AND FUEL SHUTOFF LEVERS EPT PASSED IAW-FIM-24-24. ACFT OK FOR SERVICE. RE-SELECTED BATTERY SWITCH AND FUEL SHUTOFF LEVERS EPT PASSED IAW FIM-24-24. ACFT OK FOR SERVICE. (CLOSED)

Part: TRANSMITTER — FAILED (ELT) · airframe 69,251 hrs · 31,074 cycles

ELT ON 121.5 FOLLOWED US, SUSPECT ACFT ELT IS ALERTING. FACT 28NOV10 19:44 MEM R R & R EMERGENCY LOCATOR TRANSMITTER IAW 23-25-00-4. OPS CHECK GOOD, OK FOR SERVICE. (CLOSED)

Part: STRUT — FAILED (NLG) · airframe 68,820 hrs · 30,867 cycles

ON POST FLIGHT, FOUND NOSE GEAR COLLAPSED AND LOWER COLLAR OUT OF SHRUT. REMOVED AND REPLACED NOSE LANDING GEAR ASSY IAW WORK CARD 32T2701. OPS, LEAK & RIG CHECKS NORMAL.

Part: ENGINE — FLAMED OUT · airframe 68,341 hrs · 30,629 cycles

ENGINE FLAMEOUT AT FL350. RESTART ATTEMPTED DURING DESCENT/DIVERT. DURING RESTART ATTEMPT, OIL PRESSURE WENT TO "0" (ZERO). "ENGINE FIRE, OR SEVERE DAMAGE" CHECKLIST ACCOMPLISHED. DIVERTED. TO PIT. CHECKED MAIN OIL FILTER CHIP DETECTOR. DETECTOR IS VERY CLEAN WITH NO CHIPS OR FOREIGN MATERIAL AT ALL. DURING DRY MOTOR ENGINE NR 3 N2 IMMEDIATLY CLIMBS TO 45% AND OIL PRESSURE CLIMBS TO 24PSI QUICKLY. ENGINES 1 AND 2 MAX MOTOR AT 20% N2 AND OIL PRESSURE IS AT 10PSI. ALSO DURING DRY MOTOR NOTICED NO N1 ROTATION OF ANY KIND AND NO TURBINE ROTATION. WHILE OBSERVING ALSO NOTICED THAT THERE IS AN ABNORMAL SOUND PRODUCED BY THE ENGINE DURING MOTORING. MOCC NOTIFIED OF THESE IDICATIONS AND WE BELIEVE THAT THE TOWER SHAFT IS SHEARED. REMOVED AND REPLACED NR 3 ENGINE PER MD-10 ENGINE INSTALLATION POSITION NR 3 WORK CARD 71T0701-3 AND MD-10 ENGINE RUN-UP FORM COMPLETED.

Part: PROBE — FAILED (FUEL CELL) · airframe 66,572 hrs · 29,843 cycles

DEPARTING TPA RW 18R AT 392.2 TOGW BETWEEN 200 FT AND 3000 FT MSL IN A RT TURN TO 350' (FLAPS AND SLATS RETRACTED) LAT FUEL UNBALANCE ALERT CAME ON THE EAD. ALSO, FUEL QTY/USED CHK ALERT CAME ON. FUEL OFF SKED ALERT ILLUMINATED ABNORMAL NON ALERT FUEL LEAK. ALSO, ILLUMINATED ON EAD. FOB AT DEP 55.1 AFTER 1ST ALERT ILLUMINATED FOB 43.2. REQ FUEL FOR TRIP WAS 48.1. REPLACED NR 3 OUTBOARD MJP. SEALED ALL TANK ACCESS COVERS AND THE MJP'S THAT WERE INSTALLED. ALL WORK PERFORMED IAW W/O 5081158.

Part: CONTROL VALVE — FAILED (TE FLAPS) · airframe 66,077 hrs · 29,608 cycles

LVL 2 FLAP DISAGREE AFTER TAKEOFF RAN QRH AND MADE NORMAL LANDING. CREW REPORTED IT TOOK 10 MINUTES FOR FLAPS TO EXTEND 35 DEGREES FOR LANDING. REMOVED AND INSTALLED I/B FLAP CNTL VALVE AND SECURED HYD LINES TO OTHER VALVES REF MD10-10 AMM 27-52-02-2. OPS CK AND LEAK CK GOOD. OFF MFG AYG7030-5505MODFX SRL SEM391, ON MFG AYG7030-5511, SRL SEM2176.

Part: CHECK VALVE — FAILED (TE FLAPS) · airframe 65,673 hrs · 29,410 cycles

AFTER TAKEOFF, FLAPS UP GOT LEVEL 2 "FLAP DISAG". FLAPS INDICATED 8/7 (LEFT) AND 5/4 RIGHT WING. FLAP HANDLE BACK TO LAST POSITION AND FLAPS WOULD NOT MOVE. HANDLE BACK TO UP NO CHANGE, WHILE MANEUVERING TO LAND FLAPS INDICATED 3/1 AND UP. RETURNED TO MEM. FLAP HINGES, ACTUATORS, CARRIAGES, TRACKS, FLAP VANES, RIG POSITIONS AND IND POSITIONS ALL OKAY. FOUND LT O/B FLAP SPEED SLOWER THAN RT O/B CAUSING A SPLIT. REMOVED RESTRICTOR AND CHECK VALVES ON LT O/B FLAP CONTROL VALVE. FOUND FOD IN CHECK VALVES FILTERS. RESTRICTORS WERE CLEAN. INSPECTED NR 1 AND NR 2 HYDRAULIC ENGINE AND SYSTEM MANIFOLD FILTERS. NO EVIDENCE OF DEBRIS FOUND. REPLACED CHECK VALVES. EXTEND AND RETRACT SPEED NOW MATCH.

Part: WEB — CRACKED (ZONE 700) · airframe 64,627 hrs · 28,946 cycles

LT MLG W/W FOUND CRACK ON VERTICAL WEB. REPAIRED WEB IAW SRM 53-00-01 FIG 10 VOL I.

Part: SKIN — CORRODED (ZONE 300) · corrosion level 2 · airframe 64,627 hrs · 28,946 cycles

RT STAB, INBD ELEVATOR, MODERATE CORROSION BTWN UPPER SKIN AND RIB. REPAIRED AREA IAW SRM 55-10-00 FIG 7 VOL I.

Part: SKIN — CRACKED (ZONE 600) · airframe 64,627 hrs · 28,946 cycles

RT WING OUTBOARD FLAP CRACK ON EXT SKIN UPPER SIDE. REPAIRED AREA IAW SRM 57-10-00 FIG 7 VOL I.

Part: SKIN — CRACKED (ZONE 300) · airframe 64,627 hrs · 28,946 cycles

DURING U/S INSP FOUND PANEL P/N 7206-1 AND 7204-1 OF STAB LOWER SURFACE WITH CRACK IN FLYABLE LIMITS, SEE ATTACHED "INSP FINDING FORM" FOR DETAIL. ACCOMPLISHED EA NR 8-5510-111454.

Part: SKIN — CORRODED (ZONE 300) · corrosion level 2 · airframe 64,627 hrs · 28,946 cycles

RT INBD ELEVATOR LWR SURFACE FOUND SEVERE CORROSION ON SKIN AND SUSPECT CORROSION UNDER SKIN. REPAIRED AREA IAW SRM 55-10-00 FIG 7 VOL I.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 64,627 hrs · 28,946 cycles

CTR CARGO COMPT RT TUNNEL SEVERE CORROSION WITH EXFOLIATION ON FITTING. ACCOMPLISHED EA NR 8-5310-111460.

Part: FLOORBEAM — UNKNOWN (ZONE 200) · airframe 64,627 hrs · 28,946 cycles

FOUND EXISTING REPAIR CTR CARGO COMPARTMENT FLOORBEAM. REPAIRED AREA IAW SRM 53-60-01 FIG 3 VOL I.

Part: RIB — CRACKED (ZONE 500) · airframe 64,627 hrs · 28,946 cycles

FOUND UPPER RIB CAP CRACKED ON LT WING PNL 534AT. REPLACED RIB IAW SRM 57-20-00 FIG 38 SHT 1-2-3 VOL I.

Part: LONGERON — CORRODED (ZONE 100) · corrosion level 2 · airframe 64,627 hrs · 28,946 cycles

CTR CARGO COMPT BILGE, CORROSION WITH EXFOLIATION ON SPLICE AND LONGERON. REPAIRED AREA IAW SRM 53-10-00 VOL I FIG 5.

Part: RIB — CRACKED (ZONE 600) · airframe 64,627 hrs · 28,946 cycles

FOUND UPPER RIB CAP CRACKED ON RT WING PNL 634AT. REPLACED RIB IAW SRM 57-20-00 FIG 38 SHT 1-2-3 VOL I.

Part: SKIN — LOOSE (ZONE 600) · airframe 64,627 hrs · 28,946 cycles

RT WING UPPER SURFACE OUTBD FLAP FOUND 180 EA LOOSE RIVETS ON SKIN. REPAIRED EFFECTED AREAS IAW SRM 57-20-00 VOL I FIG 11 AND WORK IN CONJUNCTION OF NRC N00468.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 64,627 hrs · 28,946 cycles

SEAT TRACK SEVERE CORROSION WITH EXFOLIATION ON SEAT TRACK. REPAIRED SEAT TRACK IAW SRM 53-60-01 FIG 1 VOL I.

Part: LONGERON — CORRODED (ZONE 100) · corrosion level 2 · airframe 64,627 hrs · 28,946 cycles

AIR CONDITIONING COMPT LT SIDE FOUND SEVERE EXFOLIATION CORROSION. REPAIRED AREA IAW SRM 53-10-00 VOL I.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 64,627 hrs · 28,946 cycles

SEAT TRACK BALLMAT AREA CRACKS ON SEAT TRACK. REPAIRED AREA IAW SRM 53-70-00 FIG 1 VOL I.

Part: SKIN — UNKNOWN (ZONE 600) · airframe 64,627 hrs · 28,946 cycles

RT WING L/E SKIN EXISTING DOUBLER. REPLACED DOUBLER IAW SRM 51-30-00 VOL II.

Part: LONGERON — WORN (ZONE 100) · airframe 64,627 hrs · 28,946 cycles

AIR CONDITIONING COMPT LT SIDE ON LONGERON FOUND DEEP WEAR OUT OF LIMITS IAW SRM 53-10-00. REPAIRED AREA IAW SRM 53-10-00 FIG 7 VOL I.

Part: SKIN — DAMAGED (ZONE 600) · airframe 64,627 hrs · 28,946 cycles

RT WING LWR SURFACE OUTBD FLAP FOUND 30 EA LOOSE RIVETS ON SKIN. REPAIRED AREA IAW SRM 57-20-00 VOL I FIG 11.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 64,627 hrs · 28,946 cycles

SEAT TRACK BALLMAT AREA CRACK ON SEAT TRACK. REPAIREED AREA IAW SRM 53-70-00 FIG 1 VOL I.

Part: WEB — CRACKED (ZONE 700) · airframe 64,627 hrs · 28,946 cycles

LT MLG W/W FOUND CRACKS ON VERTICAL WEB. REPAIRED WEB IAW SRM 53-00-01 FIG 10 VOL I.

Part: LONGERON — CORRODED (ZONE 100) · corrosion level 2 · airframe 64,627 hrs · 28,946 cycles

AIR CONDITIONING COMPT LT SIDE FOUND SEVERE EXFOLIATION CORROSION. REPAIRED AREA IAW SRM 53-10-00 FIG 6 VOL I.

Part: SKIN — CRACKED (ZONE 600) · airframe 64,627 hrs · 28,946 cycles

SLAT NR 5 RT : INSTALLING EXTEND CABLE ASSY FOUND NUT PLATE OF BOLT ASSY TRACK CABLE RETAINER ON TRACK SLAT, MISSING. REPAIRED SLAT SKIN IAW SRM 57-00-01 VOL I FIG 4 SHT 2.

Part: PAN — CRACKED (ZONE 800) · airframe 64,627 hrs · 28,946 cycles

CTR LOWER CARGO DOOR CRACK ON FWD JAMB DOOR PAN. REPAIRED AREA IAW SRM 52-00-01 FIG 7 SHT 2 VOL 1.

Part: SKIN — DAMAGED (ZONE 800) · airframe 64,627 hrs · 28,946 cycles

CTR LWR CARGO DOOR, LWR FWD CORNER OF SKIN DEFORMED. REPAIRED AREA IAW SRM 52-10-00 FIG 17 VOL 1.

Part: RIB — CRACKED (ZONE 500) · airframe 64,627 hrs · 28,946 cycles

LT WING INT L/E ON UPPER RIB FOUND CRACK 0.60" LONG. REPAIRED RIB IAW SRM 57-20-00 VOL 1 FIG 1.

Part: SKIN — DEFORMED (ZONE 600) · airframe 64,627 hrs · 28,946 cycles

RT WING T/E LOWER SKIN OF ISLAND DEFORMATION. REPAIRED AREA IAW SRM 57-00-01 VOL 1 SHT 2 FIG 4.

Part: SKIN — UNKNOWN (LT WING) · airframe 64,627 hrs · 28,946 cycles

LT WING TIP EXTERNAL DOUBLER ON SKIN. ACCOMPLISHED EA NR 8-5760-112423.

Part: SKIN — UNKNOWN (RT WING) · airframe 64,627 hrs · 28,946 cycles

RT WING TIP EXTERNAL DOUBLER ON SKIN. ACCOMPLISHED EA NR 8-5760-112423.

Part: BEAM — CORRODED (BS 899) · corrosion level 2 · airframe 64,627 hrs · 28,946 cycles

FWD CARGO COMPT BILGE AREA ON BEAM FOUND SEVERE EXFOLIATION CORROSION. REPAIRED AREA IAW SRM 53-60-01 VOL 1 FIG 3.

Part: RIB — WORN (ZONE 500) · airframe 64,627 hrs · 28,946 cycles

LT WING L/E AT STA XOS 460 ON LOWER RIB AREA DOOR 513AB FOUND DEEP WEAR REPAIRED TEE IAW SRM 57-00-01 VOL I FIG 9. FABRICATED PARTS IAW SRM 57-00-01 FIG 9 VOL 1.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 64,627 hrs · 28,946 cycles

MAIN CABIN DEEP WEAR ON SEAT TRACK AT STA 1497, X=-47 CUT DAMAGED SECTION OF SEAT TRACK FROM STA 1491 TO 1531. FABRICATED AND INSTALLED NEW SECTION REPAIR AND SPLICE IAW SRM 53-70-00 FIG 1 VOL 1.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 64,627 hrs · 28,946 cycles

MAIN CABIN SEAT TRACK DEEP WEAR ON UPPER SIDE. REPAIRED IAW SRM 53-70-000 FIG 1 VOL 1.

Part: PRESSURE PANEL — CRACKED (ZONE 700) · airframe 64,627 hrs · 28,946 cycles

NLG W/W ON VERTICAL PRESSURE PANEL FOUND CRACKED. REPAIRED WEB IAW SRM 53-40-00 FIG 34 VOL 1.

Part: FLOORBEAM — CRACKED (ZONE 100) · airframe 64,627 hrs · 28,946 cycles

FWD CARGO COMPT BILGE AREA ON BEAM FOUND CRACK. REPAIRED BEAM IAW SRM 53-60-01 VOL 1 FIG 3 SHEET 1-2.

Part: SKIN — DENTED (ZONE 600) · airframe 64,627 hrs · 28,946 cycles

RT WING INBD FLAP EXT SKIN UPPER SIDE FOUND DENT 1.50" BY 1" DEEP .078". REPAIRED SKIN IAW SRM 57-00-01 VOL 1 FIG 4 SHT 2.

Part: SKIN — WORN (ZONE 600) · airframe 64,627 hrs · 28,946 cycles

RT WING SLATS DEEP WEAR ON EXT SKIN ON DROOPED L/E OUTBOARD SIDE. REPAIRED AREA IAW SRM 57-10-00 VOL 1 PAG 39.

Part: FRAME — CRACKED (ZONE 100) · airframe 64,627 hrs · 28,946 cycles

AVIONIC COMPT ON FRAME FOUND CRACKS. REPAIRED AREA IAW SRM 53-30-00 VOL 1 FIG 11.

Part: STIFFENER — CRACKED (ZONE 600) · airframe 64,627 hrs · 28,946 cycles

DURING PERFORM OF OAN J/C 0600B620-2JR, FOUND NR 2 CRACKS 0.50" LONG ON STIFFENERS OF L/E ACCESS PANEL 617CT. REPAIRED STIFFENERS IAW SRM 57-10-00 VOL 1 FIG 10.

Part: SKIN — WORN (ZONE 500) · airframe 64,627 hrs · 28,946 cycles

LT WING L/E ON EXTERNAL SKIN DROPPED FOUND DEEP WEAR. REPAIRED AREA IAW SRM 57-10-00 FIG 39 VOL 1.

Part: STRUCTURE — UNKNOWN (ZONE 100) · airframe 64,627 hrs · 28,946 cycles

EXISTING DOUBLER EXTERNAL FUSELAGE. REPAIRED AREA IAW SRM 53-20-00 FIG 6 VOL 1.

Part: SKIN — CRACKED (ZONE 500) · airframe 64,627 hrs · 28,946 cycles

LT WING L/E EXTERNAL SURFACE LWR SIDE ON SKIN FOUND CRACK 0.40" LONG. REPAIRED SKIN IAW SRM 57-10-00 VOL 1 FIG 68.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 64,627 hrs · 28,946 cycles

AVIONIC COMPT ON FRAME FOUND SEVERE CORROSION WITH EXFOLIATION. REPAIRED FRAME IAW SRM 53-30-00 PAGE 13 FIG 4 VOL 1.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 64,627 hrs · 28,946 cycles

MAIN CABIN SEVERE EXFOLIATION CORROSION ON SEAT TRACK. INSTALLED NEW TRACK AND SPLICE IAW SRM 53-70-00 FIG 1 VOL 1.

Part: FRAME — CRACKED (ZONE 100) · airframe 64,627 hrs · 28,946 cycles

AVIONIC COMPT ON FRAME RT SIDE FOUND CRACK. REPAIRED FRAME IAW SRM 53-30-00 VOL 1 FIG 5.

Part: SKIN — CRACKED (ZONE 100) · airframe 64,627 hrs · 28,946 cycles

EXT FUSELAGE LWR SURFACE FOUND 1 CRACK 0.25" LONG ON SKIN. REPAIRED AREA IAW SRM 53-20-00 FIG 2 VOL 1.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 64,627 hrs · 28,946 cycles

SEAT TRACK BALL MAT AREA CRACK 4" LONG AND SEVERE CORROSION WITH EXFOLIATION ON SEAT TRACK. REPAIRED AREA IAW SRM 53-70-00 FIG 1 VOL 1 7 SRM 53-60-00 FIG 2-11 VOL 1.

Part: SKIN — CRACKED (ZONE 500) · airframe 64,627 hrs · 28,946 cycles

LT WING T/E OUTBD FLAP ON SKIN UPPER SURFACE FOUND 3 EA CRACKS 0.50" LONG. INSTALLED REPAIR DOUBLER IAW SRM 57-10-00 FIG 85 VOL 1.

Part: SKIN — CRACKED (ZONE 600) · airframe 64,627 hrs · 28,946 cycles

RT WING L/E CRACK .50" LONG ON EXTERNAL SKIN LOWER L/E ( SLAT TRACK NR 7). REPAIRED AREA IAW SRM 57-10-00 VOL 1FIG 68 SHT 1 & 3.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,686 hrs · 28,441 cycles

BARREL, CORROSION, FUSELAGE-SKIN AND L52 BETWEEN STA 1341-1321, BETWEEN L52-L51. REPAIRED CUT SKIN STA 1337-1341 L52 IAW DC10 SRM 53-40-01 VOL I. MAJOR REPAIR.

Part: CAP — CORRODED (LT WING) · corrosion level 2 · airframe 63,683 hrs · 28,437 cycles

LEFT WING AT STA XW 341 AND STA XW318 CAP IS CORRODED TRAILING EDGE BEAM. COMPLIED WITH FEDEX EA 8-5710-100757. FABRICATED T- CAP SECTION AND SPLICES IAW DAC DWG ARC0293 AND FEDEX EA 8-5710-100757. INSTALLED T-CAP SECTION AND SPLICES IAW FEDEX EA8-5710-100757 AND DC-10 SRM 51-31-01 VOL II. THIS IS A MAJOR REPAIR FOR REFERENCE SEE FEDEX SNRM N00847.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 63,683 hrs · 28,437 cycles

AFT PIT FLOORBEAM STA1887 UPPER AND LOWER SURFACE CORRODED FROM LONGERON 42L TO 42R. FAB ANGLE IAW DC-10-10 SRM 53-16-01 PAGE 26D FIG 6, PAGE 26E VOL III. FAB REPAIR CHANNEL IAW DC10-10 SRM 53-30-00 PAGE 13-16 VOL I ALODINE AND PRIME IAW DC10-10 SRM 51-21-01 VOL II. INSTALLED ANGLE, REPAIR CHANNEL IAW DC10-10 SRM 51-35-01, 51-33-01 VOL II AND 53-30-00 PAGE 13-16 VOL I. THIS IS A MAJOR REPAIR MECH, 96389 QC 311, SEE FEDEX SNRM N00166 OV W/O 00032325.

Part: FITTING — CORRODED (ZONE 500) · airframe 61,130 hrs · 27,175 cycles

COMPLY WITH EA 8-5750-82057. WINGS LT IB FLAP VANE ASSY, REPAIR OF O SIZED HOLES IN CHANNEL FITTINGS CLOSING ACTION ON 10/12/04.ON N/R S00010. COMPLIED WITH EA 8-5750-82059.

Part: VANE — CORRODED (ZONE 600) · airframe 61,130 hrs · 27,175 cycles

WINGS, RT INBD FLAP VANE ASSY, REPAIR OF OVERSIZED HOLES ON CHANNEL FITTINGS. COMPLIED WITH EA 8-5750-82058.

Part: WIRE — INOPERATIVE (NR 1 PNEUMATIC) · airframe 58,574 hrs · 26,052 cycles

WITH NR 1 PNEUMATIC SYSTEM DEFERRED UNDER 36-01-A NR 1 SYSTEM IS STILL PROVIDING AIR TO RUN A-PACK WITH ISOL VALVES CLOSED & PNEUMATIC NR 1 SELECTOR OFF. WHILE DESCENDING WITH ALL THROTTLES IDLE, THE NR 1 PNEUMATIC PRESSURE WAS 15 PSI. PUSHED NR 1THROTTLE UP & PSI WENT TO 45 PSI. FOUND BROKEN WIRE ON CONNECTOR. CHANGED BROKEN CONNECTOR IAW SMP CHAPTER 20 DC10AMM.

Part: CONTROL CABLE — CUT (LEFT WING SLAT) · airframe 58,479 hrs · 25,995 cycles

LT WING NR 7 SLAT EXTEND CABLE HAS ALL BUT ONE STRAND CUT AT O/B PULLY. FOUND ON W/C 57SI5502-02 AND TRANSFERRED TO N/R N00275. REMOVED AND REPLACED NR 7 SLAT EXTEND CABLE, TENSIONED LT NR 7 SLAT EXTEND AND RETRACT CABLE AND OP'S CHECK GOOD, ALL IAW M/M 27-80-00-5-2.

Part: RIB — DAMAGED (NR 6 SLAT) · airframe 58,479 hrs · 25,995 cycles

LT WING NR 6 SLAT OUTBOARD RIB REPAIR AT XOS=889.0, PN ABR 1818.

Part: STRINGER CLIP — CRACKED (ZONE 600) · airframe 58,479 hrs · 25,995 cycles

RIGHT WING NR 3 FUEL TANK HAS A CRACKED UPPER BUTTERFLY CLIP AT STA XORS 402. THIS WAS FOUND DURING A ROUTINE INSPECTION.

Part: FITTING — CRACKED (WING) · airframe 58,479 hrs · 25,995 cycles

N 831 DURING ROUTINE INSPECTION ON W/C 28C1501-02, ON THE LT WING JUST INSIDE TANK PLATE 534 AT, STA. XORS 402 SPAR STATION S-37 FOUND A CRACKED SPAR TO RIB FITTING TO BE WORKED AT MAE, UNDER W/O 13338. REPLACED FITTING IAW SRM ON SNRM N00831, W/O 13338 AT MAE.

Part: RIB — CRACKED (RT WING) · airframe 58,479 hrs · 25,995 cycles

RIGHT WING NR 3 FUEL TANK HAS A CRACKED RIB (APPOX. 5 INCHES LONG) INSIDE TANK PLATE NR 634 AT STATION XORS 402, ALONG LARGE OVAL FLAPPER CHECK VALVE. REMOVED FLIPPER DOOR FOR ACCESS IAW SRM 51-31-01, REMOVED FLIPPER DOOR HINGE IAW SRM 51-35-01, REMOVED STIFFENER IAW SRM.51-31-01. TRIMED CRACK AND CUT-OUT HOLE IAW SRM 51-31-01. FAB DOUBLER IAW SRM 52-20-00 FIG 33. OUT OF 7075-T6FAB DOUBLER ON TRAVELER T2/319454. NDT CRACK AND REINSTALLED DOUBLER IAW SRM 51-31-01. INSTALLED STIFFENER IAW SRM 51-31-01. INSTALLED FLIPPER DOOR HINGE IAW SRM 51-31-01. INSTALLED FLIPPER DOOR IAW SRM 51- 31-01.

Part: FITTING — DAMAGED (MLG) · airframe 58,553 hrs · 26,043 cycles

COMPLY WITH EA 8-5740-68748 WINGS-MLG ATTACH FITTING OVERSIZED HOLE REPAIR FACT 13MAR03 18:11 COMPLIED WITH EA 8-5740-68748 WING -MLG ATTACH FITTING OVERSIZED HOLE REPAIR (RIGHT SIDE) BUSHING FABBED ON MAE TRAVELER T2/31970. INSTALLED BUSHING IAW SRM 57-20-00 & EA 8-5740-68748 AT MAE/BFM.

Part: BLOCKER DOOR — DELAMINATED (THRUST REVERSER) · airframe 58,479 hrs · 25,995 cycles

DURING A ROUTINE INSPECTION OF THE NR 1 INBOARD THRUST REVERSER W/C NR 78C3501, IT WAS FOUND THAT BLOCKER DOOR NR 6, THE DRIVE LINK ATTACH FITTING HAD DISBONDED. REMOVED AND REPLACED BROKEN BLOCKER DOOR NR 6 I/B T/R IAW M/M 78-32-06-2, OP'S CHECK GOOD.

Part: FITTING — CRACKED (RT WING) · airframe 58,479 hrs · 25,995 cycles

RIGHT WING NR 3 TANK HAS A CRACKED SPAR TO RIB FITTING AT STATION XORS 402, SPAR STATION S37 INSIDE TANK PLATE 634AT. THIS WAS FOUND DURING ROUTINE INSP. ON W/C 28C1503-02 AT MAE, AND WILL BE WORKED ON N/R N00838, UNDER W/O 13338 REMOVED AND REPLACED FITTING IAW SRM 51-31-01. ORDERED NEW FITTING, DRILLED AND INSTALLED FITTING I.A.W. SRM 51-31-01.

Part: CONTROL CABLE — BROKEN (NR 7 SLAT) · airframe 58,479 hrs · 25,995 cycles

AT MOBILE AEROSPACE ENGINEERING (VENDOR) BFM FOUND DURING C-CHECK INSPECTION THE NR 7 SLAT EXTEND CABLE LT WING, UNRAVELED, ALL STRANDS BROKEN EXCEPT FOR ONE. REMOVED AND REPLACED NR 7 SLAT EXTEND CABLE. TENSIONED LT NR 7 SLAT AND EXTEND RETRACT CABLE, AND OPS CHECKED GOOD, ALL IAW MM 27-80-00-5.

Part: CONTROLLER — FAILED (ELECTIRCAL SYS) · airframe 56,910 hrs · 25,317 cycles

GEN BUS 1 FAILURE AT FL 280 (LAS) COMPLIED W/ RED TABS -ONLY RESTORED FOR 5-10 SEC AT BUS FAULT, ATTEMPTED CHECKLIST 2ND TIME AFTER APU STARTED/SAME, ATTEMPTED CHECKLIST 3RD TIME AFTER GEN 1 DISCONNECT/SAME, SHOT RAW DATA APP F/O SIDE. UNEVENTFUL LANDING WITH EMERGENCY POWER ON LAST 15 MIN.

Part: FUEL PUMP — MALFUNCTION (NR 2 ENGINE)

AT 27,000 FT THE NR 2 ENGINE WOULD NOT RESPOND TO THROTTLE MOVEMENT. AT DESCENT INTO SMF AT 8,000 FT THE NR 2 ENGINE FLAMED OUT. REMOVED AND REPLACED ENGINE FUEL PUMP AND MEC AS PER M/M 73-20-01-2 AND 73-12-01. FUEL PUMP AND MEC BLEED LEAK CK AND VSV RIG CHECKS GOOD. ENG RUN IAW JRH 6-7, ALL PARAMETERS WITHIN LIMITS.

Part: CONTROL CABLE — OUT OF POSITION (TE FLAPS)

DISCREPANCY: GOT FLAP DISAGREE FLAG ON TOUCHDOWN, DID NOT RETRACT FLAPS. CORRECTIVE ACTION: FOUND LEFT FLAP CABLE OFF TRACK. REMOVED AND REPLACED LEFT BUS CABLES RIGGED PER MM 27-50-00. OPERATION CHECKED OK, I/B O/B OPERATIONALLY CHECKS NORMAL.

Part: TRUNNION FITTING — CORROSION (RT MLG)

RT MAIN GEAR TRUNNION SUPPORT FTG FWD ATTACH FWD LUG, EXHIBITS CORROSION INSIDE INTERNAL BORE REF NR7048.

Part: TRUNNION FITTING — CORROSION (RT MLG)

RIGHT MAIN GEAR TRUNNION SUPPORT FTG FWD ATTACH, AFT LUG, EXHIBITS HEAVY CORROSION WITH PITTING ON FWD FACE WITH CORROSION INSIDE INTERNAL BORE. REF NR7049. CORROSION REMOVED AND BUSHING REPLACED PER SRM 57-20-00, PAGE 71.

Part: TRUNNION PIN — CORROSION (RT MLG)

RT MAIN GEAR FWD TRUNNION PIN REMOVED, FOUND TO BE CORRODED WITH 4 CIRCUMFERENTIAL CORROSION GROOVES .040 TO .080 DEEP THROUGH HARD CHROME PLATE, REF NR7040. INSTALLED NEW PIN ON WORK CARD 32T-1501, PAGE 12 STEP 1. NEW BUSHINGS WERE INSTALLED IN BOTH POSITIONS OF THE FWD TRUNNIONS ON NR 6126, 6127, 6128, 6131, 6132.

Part: SKIN — CRACKED (RT HORIZ STAB)

RT HORIZ STAB FWD UPPER PANEL HAS CRACK IND AT 2 FASTENER HOLES, FWD UPPER SPAR CAP AFT TANG, I/B OF CLOSING RIB PLANE, BEING THE 2ND AND 3RD HOLES. CRACK LENGTHS ARE APPROX .0937 TO .1875 INCH LONG AT THE PERIPHERY. C/W HFEC ON FWD SPAR UPPER REAR TANG NO DEFECTS NOTED. REPAIRED PER EA 8-5510-27090.

Part: WEB — CRACKED (BS 1500)

LEFT WHEEL INBOARD VERTICAL WALL AT STA 1500 NEAR UPPER TEE CHORD, THERE IS A 3 INCH CRACK IN WEB SKIN JUST FORWARD OF VERTICAL STIFFENER; ALSO, ON CENTER GEAR WELL, 3 EACH FASTENER HOLES ARE CRACKED ATTACHING WEB TO TEE CHORD STA 1500. ***S/D*** COMING.

Part: PLANK — CRACKED (LT HORIZ STAB)

LT HORIZ STAB FWD UPPER PLANK CRACKED JUST INBOARD OF CLOSING RIB, FROM FWD EDGE AFT THROUGH FASTENER HOLE 1.5 TOTAL CRACK CONTINUES PAST HOLE. REMOVED FASTENERS AND TRIMMED OUT CRACKED AREA. NDT AT CRACKED AREA AND OPEN HOLES C/W. COLD WORKED HOLES FINAL REAM. INSTALLED CONCOL WASHER, FABRICATED DOUBLER PER SRM 55-20-00. INSTALLED DOUBLER PER SRM 55-20-22.