N371FE

Part: LIGHT — WRONG PART (L1 DOOR) · airframe 91,670 hrs · 38,459 cycles

EVACUATION SLIDE REMOTE PRESSURE PRESS TO TEST INDICATING SYS IS INOPERATIVE. RELEASED FOR SERVICE IAW MEL. EVAC SLIDE REMOTE PRESS INDICATOR INOPERATIVE. VERIFY & RECORD IN THE AML, EVAC SLIDE SYS PRESS ONCE EACH FLIGHT DAY. T/S AND FOUND L1 SLIDE REMOTE PRESSURE INDICATOR INOP, SWAPPED LIGHT ASSYS FROM R1 SLIDE AND L1 SLIDE AND PROBLEM FOLLOWED, FOUND WRONG LIGHT BULBS INSTALLED IN LIGHT ASSY, RELAMPED BOTH BAD BULBS AND BOTH L1 & R1 REMOTE PRESSURE INDICATOR TEST NORMAL PER M.M. 25-61-03-5, A/C OK FOR SERVICE.

Part: WIRE HARNESS — DAMAGED (EGT) · airframe 91,111 hrs · 38,158 cycles

RTO AT 110KTS FOR, ENG 3 EXCEEDANCE, LVL 1 ALERT. NR 3 EGT SHOWED YELLOW, 1011, FOR EXCEEDANCE, ESTIMATE EXCEEDANCE WAS MOMENTARY. PULLED UP VIA NR 3 ENG EXCEEDANCES. THE ACARS EXCEEDENCE SHOWS IT WAS AN EGT INDICATION PROBLEM. R & R NR 3 ENG TOP LT EGT THERMOCOUPLE HARNESS & PROBES ASSEMBLY. WORK ACCOMPLISHED IAW MM 77-21-01-2. R & R NR 3 ENG RT FWD THERMOCOUPLE LEAD IAW AMM 77-21-02-2. R & R TOP RIGHT, BOTTOM RIGHT & BOTTOM LEFT EGT HARNESS IAW AMM 77-21-01-2. R & R AFT EGT HARNESS IAW AMM 77-21-01-2. PERFORMED STAIC RUN IAW JRH WITH NO DEFECTS NOTED. PERFORMED HI POWER RUN UP FOR NR 3 ENG IAW JRH. ALL PARAMETERS WITHIN LIMITS OUTLINED IN JRH.

Part: PUSH-PULL CABLE — MALFUNCTIONED (NR 2 ENGINE) · airframe 91,052 hrs · 38,128 cycles

ON TOP OF DESCENT NR 2 THROTTLE FROZE AT 92% N1 FROM FL 370 TO 10,000 FT NO MOVEMENT, SHUTDOWN ENG. CREW REPORTED THAT AFTER ARRIVAL AT GATE & SHUTDOWN NR 2 THROTTLE OPERATED NORMALLY. R & R NR 2 ENG THROTTLE PUSH PULL CABLE. RIG & OPERATIONS CHECKED OK IAW AMM 76-11-01-2. STILL REQ IDLE RUN WITHIN 48 HRS DUE TO INFLIGHT SHUTDOWN IAW AMM 72-00-00-6. COMPLIED WITH NR 2 ENG IDLE RUN, ALL INDICATIONS NORMAL.

Part: DOUBLER — CRACKED (MLG WW) · airframe 90,693 hrs · 37,939 cycles

CENTER WHEEL WELL DOUBLER HAS AN APPROXIMATLEY 5 INCH VERTICAL CRACK AT BS 1381. REMOVED AND REPLACED DOUBLER IAW SRM 51-31-01, RIGGED GOOD IAW AMM 27-60-00-05.

Part: DOUBLER — CRACKED (ZONE 700) · airframe 90,117 hrs · 37,626 cycles

WHEN REMOVING EXISTING REPAIR DOUBLER, FOUND ADDITIONAL CRACK IN AEA0161-11 DOUBLER. BS 1391 APPROX 4" DOWN FROM TOP. REPAIRED IAW EA 8-5310-157389, PART 1.

Part: BULKHEAD — CRACKED (ZONE 700) · airframe 90,117 hrs · 37,626 cycles

LEFT BULKHEAD CRACKED 16 INCHES AFT OF FWD BULKHEAD AND 4 INCHES DOWN FROM UPPER BULKHEAD. CRACK END MARKED USING HFEC. REPAIRED IAW EA 8-5310-157389, PART 1.

Part: PROXIMITY SENSOR — OUT OF ADJUST (LT MLG) · airframe 89,372 hrs · 37,217 cycles

ON GEAR RETRACTION RECEIVED A RED LT MAIN GEAR LIGHT ON THE PRIMARY AND SECONDARY INDICATORS. PERFORMED QHR PROCEDURES AND HAD SAME INDICATIONS. DUMPED FUEL TO MAX LANDING WT AND RETURNED TO DEPARTURE. R & R LT MLG CRANK SENSOR SUPPORT FOR THE UP AND LATCHED INDICATION. REF CMM 32-34-03. ADJUSTED MLG UP AND LATCHED PROXIMITY SENSOR TO OBTAIN NECESSARY CLEARANCE REF AMM 32-61-15-4. PERFORMED PSEU RTS TEST, TEST PASSED REF AMM 31-71-01-2. PERFORMED MULTIPLE GEAR SWINGS WITH CORRECT INDICATIONS. REF AMM 32-10-0-5.

Part: FIRE WARNING — ILLUMINATED · airframe 89,118 hrs · 37,076 cycles

A LEVEL 3 CARGO FIRE LOWER FWD ILLUMINATED. PUSHED FLASHING DISCHARGE SWITCH, LANDED & ROLLED OUT TO FULL STOP. FIRE DEPTARTMENT REPORTED SLIGHT HEAT SIGNATURE ON LOWER FORWARD BELLY. ALL CHECKLIST COMPLETED.

Part: DOOR FRAME — CORRODED (CARGO DOORWAY) · airframe 88,392 hrs · 36,697 cycles

AFT CARGO DOOR LWR FWD FRAME CORRODED. REMOVED CORROSION FROM AFT CARGO DOOR LWR FWD INTERIOR JAMB REF SRM53-50-00, VOL 1 FIG 15 AND ER 11-04534. REPAIRED IAW REF EA3 8-5310-153320 AND SR10530057 AND EA 8-5350-156806.

Part: FITTING — CRACKED (CARGO DOOR) · airframe 88,392 hrs · 36,697 cycles

MAIN CARGO DOOR NR6 LATCH SPOOL LOWER FITTING CRACKED FROM INBD FWD SPOOL MOUNT BOLT HOLE. R & R SPOOL FITTING NR 6 REF SRM 51-33-01, VOL II.

Part: PITOT LINE — DAMAGED · airframe 88,059 hrs · 36,510 cycles

ON TAKEOFF AIRSPEED STAGNATED THEN BECAME ERRATIC. COMPLIED WITH QRH. RETURNED TO KIND. R & R 3EA PITOT TUBES IAW MM 34-11-02-2. OPS CHECK REQ'D. PERFORMED A LOW RANGE LEAK TEST ON PITOT AND STATIC SYS. ALL TESTS NORMAL. NO LEAKS IN SYS OR LEAK DOWN. ALL PITOT LINES PURGED PRIOR TO PITOT TUBE CONNECTION AND NO OBSTRUCTIONS NOTED. AIRSPEED AND ALT CHECK NORMAL ON AIR DATA SYS TEST. ACFT OK TO CONTINUE IAW AMM CHAPT 34-16-00-5. ACFT REMAINS RVSM.

Part: PITOT LINE — DAMAGED · airframe 88,059 hrs · 36,510 cycles

ON TAKEOFF, AIRSPEED STAGNATED THEN BECAME ERRATIC. COMPLIED WITH QRH. RETURNED TO FIELD. R & R 3 PITOT TUBES IAW MM 34-11-02-2. PERFORMED A LOW RANGE LEAK TEST ON PITOT AND STATIC SYS. ALL TESTS NORMAL. NO LEAKS IN SYS OR LEAK DOWN. ALL PITOT LINES PURGED PRIOR TO PITOT TUBE CONNECTION AND NO OBSTRUCTIONS NOTED. AIRSPEED AND ALT CHECKED NORMAL ON AIR DATA SYS TEST. ACFT OK TO CONTINUE IAW AMM 34-16-00-5. ACFT REMAINS RVSM IAW GMM CHAPT 6.

Part: RELIEF VALVE — FAILED (FUEL SYSTEM) · airframe 86,159 hrs · 35,510 cycles

FUEL SYS AUTO, ON LONG APP WITH MEL 28-22-01-04A. ALL PUMPS WERE ON THAT WERE NOT DEFFERRED. FUEL QTY TANK NR 2 STARTED A SLOW INCREASE AS FUEL QTY TANK NR1 DROPPED FASTER THAN IT SHOULD ON 8 ML FINAL, GOT WARNING OF TANK IMBALANCE AND POSSIBLE FUEL LEAK. ON LANDING FUEL QTY WERE 4.4/11.2/7.5, NO FUEL WAS LEAKING FROM ACFT. T/S, WITH NR 1 AND NR 3 PUMPS RUNNING, IT APPEARS THAT FUEL IS MIGRATING INTO NR 2 TANK ON THE GROUND. ALL WORK ACCOMPLISHED BY TANK VENDORS FFC R/O5100152. R & R NR 2 FILL LINE SURGE RELIEF VALVE IAW AMM 28-21-08-2. RAN NR 1 AND NR 3 TRANSFER PUMPS. NO FUEL MOVEMENT TO NR 2 TANK. LEAK AND OPS CHECK GOOD.

Part: FRAME — CRACKED (ZONE 200) · airframe 83,081 hrs · 34,005 cycles

MAIN CABIN FOUND 1 CRACK ON FRAME STA 1741 STR 14 RT REPAIRED IAW SRM 53-30-00 FIG 5 VOL I AND EA NR 8-5380-111563.

Part: FRAME — CRACKED (ZONE 200) · airframe 83,081 hrs · 34,005 cycles

MAIN CABIN FOUND 1 CRACK ON FRAME STA 1741, STR 14, RT. REPAIRED AREA IAW SRM 53-30-00 FIG 5 VOL I AND EA NR 8-5310-111521, 8-5330-111563.

Part: STRINGER — CRACKED (ZONE 500) · airframe 83,081 hrs · 34,005 cycles

FOUND LOWER CHORD LUGS CRACKED. REPAIRED AREA IAW SRM 57-20-00 FIG 27 SHT 2 VOL I.

Part: LUG — CRACKED (ZONE 600) · airframe 83,081 hrs · 34,005 cycles

FOUND LOWER CHORD LUG CRACKED. REPAIRED AREA IAW SRM 57-20-00 FIG 27 SHT 2 VOL I.

Part: ANGLE — CRACKED (ZONE 100) · airframe 83,081 hrs · 34,005 cycles

LOWER FWD COMPT CRACK ON TEE ANGLE. REPAIRED TEE CAP IAW EA NR 8-5310-111463.

Part: SKIN — CRACKED (ZONE 600) · airframe 83,081 hrs · 34,005 cycles

RT WING DROOPED FOUND CRACK ON UPPER EXTERNAL SKIN. REPAIRED SKIN IAW SRM 57-10-00 FIG 55 VOL I.

Part: LUG — CRACKED (ZONE 600) · airframe 83,081 hrs · 34,005 cycles

AT ACCESS 634 AT FOUND LOWER CHORD LUG CRACKED. REPAIRED AREA IAW EA NR 8-5710-111525A.

Part: LUG — CRACKED (ZONE 500) · airframe 83,081 hrs · 34,005 cycles

FOUND LOWER CHORD LUG CRACKED. REPAIRED AREA IAW EA NR 8-5710-111524A.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 83,081 hrs · 34,005 cycles

CTR CARGO COMPT SEVERE CORROSION WITH EXFOLIATION ON CHANNEL. REPAIRED CHANNEL IAW SRM 53-70-00 VOL I FIG 5 SHT 5.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 83,081 hrs · 34,005 cycles

DURING PERFORMING OK TO CLOSE FLOOR PANELS WITH J/C MD10-53210290-1J FOUND SEAT TRACK CRACK ON MAIN CABIN. REPAIRED AREA IAW SRM 53-70-00 FIG 1 VOL I.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 83,081 hrs · 34,005 cycles

ENTRY WAY ZONE AFTER REMOVAL FLOOR PANEL WITH OAN J/C MD10-600C220-1JR FOUND CRACK ON SEAT TRACK LUG LT SIDE. REPAIRED SEAT TRACK IAW SRM 53-70-00 FIG 1 SHT 1 AND 3 VOL I.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 83,081 hrs · 34,005 cycles

DURING PERFORMING OK TO CLOSE FLOOR PANELS WITH J/C MD10-53210290-1J FOUND SEAT TRACK CRACK ON MAIN CABIN.

Part: BULKHEAD — CRACKED (CLG WW) · airframe 83,081 hrs · 34,005 cycles

CLG WW CENTER CRACKS ON VERTICAL RT BULKHEAD. REPAIRED AREA IAW SRM 53-00-01 FIG 10 VOL I.

Part: SKIN — WORN (RT WING) · airframe 83,081 hrs · 34,005 cycles

RT WING DROOPED FOUND DEEP WEAR ON LWR EXTERNAL SKIN. REPAIRED SKIN IAW SRM 57-10-00 VOL I FIG 39.

Part: STRINGER — CRACKED (LT WING) · airframe 83,081 hrs · 34,005 cycles

AT ACCESS 534 AT FOUND CRACK, ACCOMPLISHED EA NR 8-5710-111526.

Part: SKIN — CRACKED (LT WING) · airframe 83,081 hrs · 34,005 cycles

LT WING DROOPED FOUND CRACK AND DEEP WEAR ON EXT SKIN OUTBOARD SIDE DROOPED. REPAIRED SKIN IAW SRM 57-10-00 VOL I FIG 15 SHT 1.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 83,081 hrs · 34,005 cycles

DURING U/S INSP OF HORIZ STB, FOUND TWO PANEL WITH CRACK IN FLYABLE LIMITS. ACCOMPLISHED EA NR 8-5510-111533.

Part: SKIN — LOOSE (T/E FLAP) · airframe 83,081 hrs · 34,005 cycles

LT WING I/B FLAP UPPER SKIN EXISTING REPAIR. REPAIRED SKIN IAW SRM 57-10-00 FIG 86 VOL I.

Part: STRINGER — CRACKED (ZONE 600) · airframe 83,081 hrs · 34,005 cycles

FOUND 2" CRACK ON RT WING STRINGER NR 40 AT XORS 346. REPAIR PER SRM 57-20-00 VOL 1 FIG 36 CONF.

Part: HINGE — DAMAGED (HORIZONTAL STAB) · airframe 83,081 hrs · 34,005 cycles

HINGE ASSY ITEM 360 BROKEN, REF IPC 55-22-02-01. REPLACE HINGE IAW STD REWORK DWG SR10-55-501.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 83,081 hrs · 34,005 cycles

FOUND 1 CRACK 4" ON SEAT TRACK AT STA 635 X= 67 CUT APPROX AT STA 666 AND 624 AND REPAIR IAW SRM 53-70-00 VOL 1 FIG 1 AND FIG 11.

Part: SKIN — DAMAGED (ZONE 500) · airframe 83,081 hrs · 34,005 cycles

LT WING L/E SKIN LOWER SLAT TRACK CUT OUT NR 8 AT STA XOS 549 EXISTING REPAIR. REPLACED REPAIR PER SRM 57-10-00 VOL.1 FIG 68.

Part: HINGE — DAMAGED (FUSELAGE) · airframe 83,081 hrs · 34,005 cycles

HINGE ASSY ITEM 360 BROKEN (REF IPC 55-22-02-01). REPLACED LATCH IAW FEDEX STD REWORK DWG SR10-55-501.

Part: ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,081 hrs · 34,005 cycles

CTR CARGO COMPT EXFOLIATION CORROSION ON CAP ANGLE AT STA 1541 L NR 52 REPAIR CAP IAW SRM 53-30-00 VOL 1 FIG 8 SHEET 1.

Part: ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,081 hrs · 34,005 cycles

EXFOLIATION CORROSION ON CAP ANGLE AT STA 1561 L NR 52 REPAIR IAW SRM 53-30-00 VOL 1 FIG 8 SHEET 1.

Part: STRINGER — CRACKED (ZONE 600) · airframe 83,081 hrs · 34,005 cycles

RT WING L/E INTERNAL STRUCTURE FOUND 1 CRACK 0,75" LONG ON FIXED TEE AT XOS 906 REPAIR WING LOWER L/E STRINGER DOUBLER IAW SRM 57-10-00 FIG 49 VOL 1.

Part: SEAT TRACK — CRACKED (BS 635) · airframe 83,081 hrs · 34,005 cycles

FOUND 1 CRACK 4 INCH ON SEAT TRACK AT STA 635 X= 67 CUT APPROX AT STA 666 AND 624 AND REPAIR IAW SRM 53-70-00 VOL 1 FIG 1 AND FIG 11.

Part: ANGLE — CRACKED (BS 899) · airframe 83,081 hrs · 34,005 cycles

LOWER CTR CARGO DOOR CRACK ON FWD LWR CORNER. REPAIRED AREA IAW SRM 52-10-00 FIG 17 VOL I.

Part: RIB — CRACKED (ZONE 600) · airframe 83,081 hrs · 34,005 cycles

RT WING L/E INT STRUCTURE FOUND CRACK ON UPPER RIB. REPAIRED AREA IAW SRM 57-20-00 FIG 1 SHT 1 VOL I.

Part: RIB — CRACKED (ZONE 600) · airframe 83,081 hrs · 34,005 cycles

RT WING L/E INT STRUCTURE FOUND CRACK ON UPPER RIB. REPAIRED AREA IAW SRM 57-20-00 FIG 1 SHT 1 VOL I.

Part: RIB — CRACKED (ZONE 600) · airframe 83,081 hrs · 34,005 cycles

RT WING L/E INT STRUCTURE FOUND CRACK ON UPPER RIB. REPAIRED AREA IAW SRM 57-20-00 FIG 1 SHT 1 VOL I.

Part: RIB — CRACKED (ZONE 600) · airframe 83,081 hrs · 34,005 cycles

RT WING L/E INT STRUCTURE FOUND CRACK ON UPPER RIB. REPAIRED AREA IAW SRM 57-20-00 FIG 1 SHT 1 VOL I.

Part: RIB — CRACKED (ZONE 600) · airframe 83,081 hrs · 34,005 cycles

RT WING L/E INT STRUCTURE FOUND CRACK ON RIB. REPAIRED AREA IAW SRM 57-20-00 FIG 1 SHT 1 VOL I.

Part: MEMBRANE — CORRODED (ZONE 200) · corrosion level 2 · airframe 83,081 hrs · 34,005 cycles

COCKPIT INT AFTER REMOVAL FLOOR PANEL WITH OAN J/C MD10-0600C210-1JR FOUND SEVERE CORROSION ON 2 HORIZ MEMBRANE: FROM STA 303 TO STA 330 FROM X= 7.50 TO X=17 LT SIDE; FROM STA 303 TO STA 330 FROM X= 27 TO X= 60 LT SIDE. THE FIRST CASE REPLACED MEMBRANE IAW SRM 51-35-01 PAR 1-5 VOL II. THE SECOND CASE REPAIRED MEMBRANE IAW SRM 53-00-01 FIG 10 VOL I.

Part: FRAME — CRACKED (ZONE 200) · airframe 83,081 hrs · 34,005 cycles

MAIN CABIN STRUCTURE HAS CRACK ON FRAME. REPAIRED FRAME IAW SRM 53-30-00 FIG 5 VOL I.

Part: SKIN — CRACKED (ZONE 500) · airframe 83,081 hrs · 34,005 cycles

LT WING FOUND CRACK ON LOWER EXT SKIN L/E. REPAIRED SKIN IAW SRM 57-10-00 FIG 68 SHT 1 VOL I.

Part: SKIN — CRACKED (ZONE 600) · airframe 83,081 hrs · 34,005 cycles

RT WING LWR SURFACE FOUND CRACK ON SKIN. REPAIRED CRACK IAW SRM 57-10-00 FIG 68 SHT 1 VOL I.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 83,081 hrs · 34,005 cycles

FOUND EXTERNAL FUSELAGE SKIN EXISTING DOUBLER. NOT PER SRM. REPAIRED SKIN IAW SRM 53-20-00 VOL I FIG 6.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 83,081 hrs · 34,005 cycles

EXTERNAL FUSELAGE SKIN EXISTING DOUBLER. NOT PER SRM. REPAIRED SKIN IAW SRM 53-20-00 FIG 6 VOL I.

Part: FLOOR SKIN — CORRODED (ZONE 200) · corrosion level 2 · airframe 83,081 hrs · 34,005 cycles

FOUND SEVERE CORROSION ON 2 COCKPIT MEMBRANES 1 WEB REPAIRED IAW SRM 53-00-01 FIG 10 VOL 1. THE OTHER WEB IS WITHIN LIMITS AFTER CORROSION REMOVAL IAW SRM 53-00-01 FIG1 VOL1:TREATED AREA IAW SRM 51-21-01.

Part: SKIN — CRACKED (ZONE 600) · airframe 83,081 hrs · 34,005 cycles

RT WING UPPER SURFACE FOUND 1 CRACK REPAIR SKIN IAW SRM 57-10-00 VOL1 FIG 68 SHT 1, 2.

Part: SKIN — CRACKED (RT WING) · airframe 83,081 hrs · 34,005 cycles

RT WING LWR SURFACE FOUND 1 CRACK 2" LONG ON SKIN. REPAIRED CRACK IAW SRM 57-10-00 FIG 68 SHT 1 VOL 1.

Part: DOUBLER — CRACKED (ZONE 500) · airframe 83,081 hrs · 34,005 cycles

LT WING L/E CRACK 1" ON TEE ANGLE FIXED PANEL REPAIRED WING LOWER L/E STRINGER DOUBLER IAW SRM 57-10-00 FIG 49.

Part: LONGERON — CRACKED (ZONE 100) · airframe 83,081 hrs · 34,005 cycles

LWR FWD COMPT FOUND CRACK .50" LONG ON LONGERON. REPAIRED AREA IAW SRM 53-10-00 FIG 5 VOL 1.

Part: SKIN — CORRODED (BS 1039 L52R) · corrosion level 2 · airframe 83,081 hrs · 34,005 cycles

LOWER EXT FUSELAGE PERFORMED INSPECTION AFTER ADF ANTENNA REMOVAL WITH OAN J/C SP10240167-7004-1JR. FOUND SEVERE CORROSION WITH EXFOLIATION ON EXT SKIN C/L. REPAIRED AREA IAW SRM 53-20-00 VOL 1 FIG 6 SHT 3-4.

Part: ANGLE — CRACKED (ZONE 100) · airframe 83,081 hrs · 34,005 cycles

AFT CARGO COMPT AT STA 1997.750 L NR 52 CRACK 1" ON CAP ANGLE REPAIR IAW SRM 53-00-01 VOL 1 FIG 8.

Part: HINGE — CORRODED (LT INBD FLAP) · corrosion level 2 · airframe 79,191 hrs · 31,937 cycles

BFM CLOSE R COMPLY WITH EA 8-5750-82054 WINGS, INBD FLAP REWORK OF UPSTOP MOUNT HOLES IN ARC0154 HINGE ASSY ENT BY: 497234 RPT BY: 497234 FACT 14OCT04 05:49. BFM U COMPLIED WITH EA 8-5750-82054 WINGS INBD FLAP REWORK OF UPSTOP MOUNT HOLES IN ARC0154 HINGE ASSY AT MAE ENT BY: 497234 RPT BY: 497234.

Part: STOP — BROKEN (ZONE 800) · airframe 79,191 hrs · 31,937 cycles

COMPLY WITH E.A.8-5210-82059.REWORK OF ABA7188-1 FITTING TO REPLACE ABA7156-501 FOR R1 DOOR. CLOSING ACTION ON 10/11/04. ON N/R S00024. COMPLIED WITH EA 8-5210-82059

Part: STOP — CORRODED (ZONE 600) · airframe 79,191 hrs · 31,937 cycles

RT WING INBD FLAP REWORK OF UPSTOP MOUNT HOLE IN ARC0154 HINGE ASSY. COMPLIED WITH E.A.8-5750-82056.

Part: HINGE — CORRODED (ZONE 600) · airframe 79,191 hrs · 31,937 cycles

COMPLY WITH EA 8-5750-82050 RT INBOARD FLAP MOUNTED HINGE PIVOT BORE REPAIR. COMPLIED WITH EA8-5750-82050.

Part: SUPPORT — CORRODED (TE FLAP) · airframe 79,191 hrs · 31,937 cycles

LT/RT OB FLAPS-FLAP VANE SUPPORTS CORROSION REWORK. CLOSING ACTION ON 10/04/04. ON N/R S00018. COMPLIED WITH EA 8-5750-82049.

Part: HINGE — GOUGED (ZONE 800) · airframe 79,191 hrs · 31,937 cycles

COMPLY WITH EA 8-5240-82048. TAILCONE-PATIO DOOR HINGE REPAIR P/N AKC7011. CLOSING ACTI0N ON 10/05/04. ON N/R S00019 COMPLIED WITH EA 8-5240-82048.

Part: DOOR — CHAFED (TAILCONE) · airframe 79,191 hrs · 31,937 cycles

COMPLY WITH EA8-5240-82045, TAILCONE PATIO DOOR HINGE REPAIR P/N ARC7011-2. CLOSING ACTION ON 10/01/04. ON N/R S00013. COMPLIED WITH EA 8-5240-82045.

Part: FITTING — CORRODED (RT OB FLAP) · airframe 79,191 hrs · 31,937 cycles

COMPLY WITH 8-5750-82047- RIGHT O/B HINGE LUG CORROSION REPAIR. COMPLIED WITH EA 8-5750-82047 RIGHT O/B FLAP O/B HINGE LUG CORROSION REPAIR (P/N ARC 1991-2). AT MAE ENT BY: 497234 RPT BY: 497234

Part: WARNING LIGHT — ILLUMINATED (COCKPIT) · airframe 75,281 hrs

ON GEAR RETRACT GEAR HANDLE UP PILOT'S PANEL LT RED UNSAFE LIGHT REMAINED ON W S/O RT RED UNSAFE LIGHT ON. R/R PROX BOX MFG P/N 8-061-25 SN 237

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 69,890 hrs · 27,518 cycles

AT CLIMB CABIN PRESS EXCEEDED 10,000. AC RELEASE PER MEL AUTO AND SEMI AUTO CABIN ALTITUDE CONTROL SYSTEM INOP.

Part: TERMINAL BLOCK — OVERHEATED (RT WINDSHIELD)

ELECTRICAL FUMES IN FLT ISOLATED SOURCE FROM AC BUS 1 PULLED CB. REMOVED AND REPLACED TERMINAL BLOCK, FILTER AND CONTROLLER FOR RT WINDSHIELD PER DC10-10 MM CHAPTER 30-41-01-2 AND 30-41-03-4. CHECKS GOOD ON TEST. RESET NR 1 AC BUSS.

Part: ENGINE — FLAMED OUT (NR 1)

DURING T/O, NR 1 ENG N1 BEGAN TO DECAY. RETURN TO MEM. THROTTLES RETARDED, ENGINE FLAMED OUT. REMOVED AND REPLACED BOTH GASKETS BETWEEN THE P&D VALVE AND MEC PER DC10-10 MM 73-13-05-2 AND ENG PWR INSUR. CK PER JRH 6-31 AND ENG CK GOOD.

Part: LINE — FAILED (NR 1 ENGINE)

ON DEPARTURE ON T/O PWR, NR 1 ENGINE ROLLED BACK TO 5000 FUEL FLOW WITH CORRESPONDING PWR IND. *S/D* REMOVED AND REPLACED CDP LINE FROM FIRE SHIELD TO 13 STAGE CANNED FROM AC 058 NR 1 ENG IN HRGR, REF MM 71-00-00. RAN ENG AND DATA CHECK GOOD PER JRH.

Part: UPLOCK TARGET — BROKEN (RT MLG DOOR)

AFT T/O RETRACTED GEAR AND BOTH PILOT & S/O REQ GEAR RED LIGHT ILLUM WITH HANDLE UP. PERF RED TABS AND BOTH RED LIGHT REMAINED ILLUM. DUMP FUEL TO 375,000 LBS GROSS WT AND MADE NORMAL LANDING. REPLACED TARGET WITH (P/N ARG7531-501) AND COMPLETED LANDING GEAR RETRACTION/EXT TEST IAW DC10 MM 32-10-00-5.

Part: FRAME — CRACKED (BS 1721)

UPPER INTERNAL FUSELAGE BS 1721, LONG 13 RT SIDE, FOUND 1 CRACK ABOUT 5 INCHES LONG ON FRAME. REPAIR ACCOMPLISHED WITH INSTALLATION OF REPAIR FRAME SECTION AND NEW SPLICES IAW SRM 53-10-00, FIG 5. (28 AUGUST 1998).