N68050

Part: COMPRESSOR — STALLED (NR 1) · airframe 68,119 hrs · 30,534 cycles

AT ROTATION NR 1 ENG COMPRESSOR STALLED. HEARD A LOUD BANG WITH YAW AND TEMP AT 1097 DEGREES. N2 INDICATION HAD AN X WITH NO INFORMATION SHOWING. REMOVED AND REPLACED THE ENGINE.

Part: SUPPORT — CRACKED (LT WING) · airframe 66,876 hrs · 29,999 cycles

LEFT OTBD FLAP INBD HINGE-FWD FITTING ATTACHED TO THE WING HAS A CRACK ON INBD SIDE. REMOVED CRACKED SUPPORT FITTINGS IAW SRM 51-33-01. WORKED HOLES TO FINAL SIZE .325 ON OTBD FLALP SUPPORT FITTINGS COMPLIED WITH EA 8-5710-125587 FOR MISLOCATED HOLE REPAIR. INSTALLED CLEVIS ARC0538 IAW DO69/05 DWG ARC0501 INSTALLED LT OTBD FLAP INBD HINGE, INBD AND OTBD SUPPORT FITTINGS IAW SRM 51-33-01.

Part: FUEL CONTROL — MALFUNCTIONED (NR 3 ENGINE) · airframe 64,209 hrs · 28,818 cycles

NR 3 ENG ROLLBACK AT FL370, ENG IGN OVERRIDE ON. ENGINE RESTARTED ITSELF AT FL 270 IN CLOUDS -10C WITH ALL ENG ANTI-ICE ON. ROLL BACK RESULTED IN N1 OF 48 PERCENT & FUEL FLOW OF 1000. EGT OF 570. PERFORMED INSPECTION OF NR 3 ENGINE INLET & EXHAUST NO DEFECTS NOTED. TROUBLESHOT PER FIM 71-00-13. NO FUEL LEAKS FOUND. COMPLETED NR 3 ENGINE FUEL PUMP & MECH INSTALLATION PER MM 73-20-01-2. PERFORMED LEAK & IDLE RUN CHECK PER JRH. PERFORMED FLT IDLE CHECK & POWER ASSURANCE CHECK PER JRH CHAP 4 AND 5 ON NR 3 ENG. RECORDED ALL ENG PARAMETERS ON FORM M-3488 AND CHECK'S GOOD. OK FOR CONTINUED SERVICE.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 63,921 hrs · 28,675 cycles

MAIN CARGO DECK SEAT TRACK AT STA 879 TO 919 LBL 107 HAS SEVERAL FASTENER HOLES DAMAGED ON THE OTBD LOWER LEG FROM PREVIOUS REWORK. REMOVED AND REPLACED SEAT TRACK, FAB NEW SEAT TRACK SECTION AND SPLICES IAW SRM 51-31-01, 53-70-00 FIG 1 SHEET 1 AND MAE TRAVELER T8/767563 AND T8/767564. MAJOR REPAIR RII.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 63,921 hrs · 28,675 cycles

MCDECK SEAT TRACK AT STA 1089 LBL 48 IS DAMAGED, REMOVED FLOORBOARDS FOR ACCESS. REMOVED SEAT TRACK, FABRICATED NEW TRACK. INSTALLED NEW TRACK AND REINSTALLED FLOORBOARDS IAW SRM 51-31-01, SRM 53-70-00 AND MAE TRAVELER T8/766008. MAJOR REPAIR AND RII.

Part: UNKNOWN — UNKNOWN · airframe 62,840 hrs · 28,143 cycles

EN ROUTE TO SEA, NOTICED ON PNEUMATIC PNL RED MANF NR 3 LIGHT AND AMBER BLEED OFF LIGHT. PNEUMATIC SYNOPTIC PG SHOWED NR 3 PNEU MANF IN THE RED AND PRESS IN MANF SLOWLY DROPPING. 2 MIN LATER RECEIVED LVL 3 ALERT "AIR MANF 3 FAIL". C/W QRH AND DIVERTED TO BOI. PERFORMED PNEUMATIC SYSTEM PRESSURE DECAY TEST ON NR 3 SYST TEST PASSED MANUALLY CLOSED AND LOCKED RT WING ANTI-ICE VALVE PER MEL 30-11-01. T/S REF FIM, REACTIVATED WING ANTI ICE. EXTENDED LEADING EDGE SLATS, PERFORMED LEAK CHECK ON ANTI ICE DUCTING ON RT WING. NO LEAKS FOUND. PNEUMATIC MANIFOLD RT WING PRESSURE SWITCH FAULT BALL SHOWING. RESET FAULT BALL. REPLACED FAIL DETECTION PRESSURE SWITCH.

Part: FLOORBEAM — CORRODED (BS 895) · corrosion level 2 · airframe 62,721 hrs · 28,083 cycles

FORWARD LOWER CARGO, DOOR TORQUE BOX FORWARD FRAME CORRODED. REMOVED CORROSION FROM FRAME AND SUPPORT BRACKET AND FOUND BOTH TO EXCEED ALLOWABLE LIMITS IAW MD/DC 10 SRM 53-00-01 VOL I FIG 1B. REPAIRED FRAME IAW FED EX EA NR 8-5350-109160 "FUSELAGE FWD LOWER CARGO DOOR JAMB FRAME STA 895 CORD REPAIR". FABRICATED AND INSTALLED NEW SUPPORT BRACKET IAW DAC DWG ADA0233 REV L AND DC/MD10 SRM 51-33-01 VOL II PG 1.

Part: FRAME — CORRODED (BS 1002) · corrosion level 2 · airframe 62,721 hrs · 28,083 cycles

FORWARD LOWER CARGO, DOOR TORQUE BOX FORWARD FRAME CORRODED. REMOVED CORROSION FROM FRAME AND WEB AND FOUND MATERIAL LOSS FOR BOTH TO EXCEED ALLOWABLE LIMITS IAW MD/DC 10 SRM53-00-01 VOL I FIG 1B. REPAIRED FRAME IAW FED EX EA NR 8-5350-109161 "FUSELAGE-FWD LOWER CARGO DOOR JAMB FRAME STA 1002 CORD-REPAIR". REPAIRED WEB IAW MD/DC10 SRM 53-00-01 VOL I FIG 10.

Part: SPAR — CRACKED (HORIZONTAL STAB) · airframe 62,721 hrs · 28,083 cycles

RT HORIZONTAL STABILIZER OUTBOARD LEADING BOTTOM ATTACH ANGLE CRACKED. REPAIRED IAW FEDEX EA NR 8-5510-109166 "STABILIZERS, RT STAB LOWER LEADING EDGE, SPAR CRACK REPAIR".

Part: WEDGE — DENTED (LT ELEVATOR) · airframe 62,721 hrs · 28,083 cycles

LEFT INBOARD ELEVATOR TRAILING EDGE DENTED AT MID-SECTION AREA. REMOVED DAMAGED SECTION OF LEFT INBOARD ELEVATOR PER DC/MD10 SRM 51-31-01 VOL 11. RECEIVED NEW TRAILING EDGE WEDGE SECTION, LOCATED AND DRILLED HOLES PER DC/MD10 SRM 51-31-01 PARAG 2 VOL11. ALODINED AND PRIMED PER DC/MD10 SRM 51-21-01 PARAG 31, VOL 11; 51-21-01 PARAG 24 VOL 11. INSTALLED TRAILING EDGE PER MD/DC10 SRM 51-31-01 VOL 11. PAINTED WEDGED SURFACE PER MD/DC10 SRM 51-21-02 PARAG 2J VOL11.

Part: FITTING — CORRODED (CARGO DOORWAY) · corrosion level 2 · airframe 62,721 hrs · 28,083 cycles

MAIN CARGO DOOR-LOWER JAMB FITTING NR 4 SHOWS CORROSION AT AFT UPPER HOLE. REPAIRED NR 4 LOWER JAMB FITTING AND WEB IAW FEDEX EA 8-5230-110663 REV A. "FUSELAGE-MAIN CARGO DOOR-LOWER JAMB SUPPORT FITTING INSPECTION AND DOOR RIG" LOWER SUPPORT FITTING REPLACED ON JOB CARD N00788.

Part: FITTING — CORRODED (DOOR FRAME) · corrosion level 2 · airframe 62,721 hrs · 28,083 cycles

MAIN CARGO DOOR-LOWER JAMB FITTING NR 5 SHOWS CORROSION AT LOWER FORWARD HOLE. REPAIRED NR 5 LOWER JAMB AND REPLACED SUPPORT FITTING IAW FEDEX EA 8-5230-110663 REV A " FUSELAGE-MAIN CARGO DOOR-LOWER JAMB SUPPORT FITTING INSPECTION AND DOOR RIG".

Part: FITTING — CORRODED (DOOR FRAME) · corrosion level 2 · airframe 62,721 hrs · 28,083 cycles

MAIN CARGO DOOR LOWER JAMB FITTING NR 2 SHOWS CORROSION AT LOWER FORWARD HOLE. REPAIRED LOWER JAMB AND REPLACED SUPPORT FITTING NR 2 IAW FEDEX EA. 8-5230-110663 REV A. " FUSELAGE- MAIN CARGO DOOR-LOWER JAMB SUPPORT FITTING INSPECTION AND DOOR RIG." LOWER SUPPORT FITTING REPLACED ON JOB CARD N00788.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,721 hrs · 28,083 cycles

MAIN CARGO DOOR NR 6 LATCH SPOOL AND FITTING IS CORRODED. REMOVED NR 6 SPOOL IAW DC/MD10 FEDEX EA NR 8-5230-110663 STEPS 5A AND B. CLEANED,TREATED AND PRIMED IAW FEDEX DC/MD10 SRM 51-21-01 VOL 11. INSTALLED NR 6 SPOOL AND FITTING IAW FEDEX EA NR 8-5230-110663. INSTALLED MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING AND RIGGED DOOR IAW FEDEX EA NR 8-5230-110663.

Part: FITTING — CORRODED (DOOR FRAME) · corrosion level 2 · airframe 62,721 hrs · 28,083 cycles

MAIN CARGO DOOR LOWER JAMB FITTING NR 3 SHOWS CORROSION AT FORWARD LOWER HOLE. REPAIRED NR 3 LOWER JAMB AND REPLACED SUPPORT FITTING IAW FEDEX EA 8-5230-110663 REV A "FUSELAGE-MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING INSPECTION AND DOOR RIG."

Part: FITTING — CORRODED (ZONE 800) · corrosion level 2 · airframe 62,721 hrs · 28,083 cycles

COMPLY WITH FEDEX EA NR 8-5230-110663 "FUSELAGE-MAIN CARGO DOOR - LOWER JAMB FITTING INSPECTION AND DOOR RIG". COMPLIED WITH FEDEX EA NR 8-5230-110663 "FUSELAGE- MAIN CARGO DOOR, LOWER JAMB FITTING INSPECTED AND RIGGED."

Part: FITTING — CORRODED (BS 755) · corrosion level 2 · airframe 62,721 hrs · 28,083 cycles

MAIN CARGO DOOR NR 7 LATCH SPOOL AND FITTING IS CORRODED. REMOVED NR 7 SPOOL IAW FEDEX EA NR 8-5230-110663 REV A. " FUSELAGE-MAIN CARGO DOOR - LOWER JAMB SUPPORT FITTING INSPECTION AND DOOR RIG." CLEANED AND TREATED, PRIMED IAW FEDEX MD10 SRM 51-21-01 VOL 11. SPOOL AND FITTING INSTALLED NR 7 SPOOL ON EA 8-5230-110663 REV, A.

Part: FITTING — CORRODED (DOOR FRAME) · corrosion level 2 · airframe 62,721 hrs · 28,083 cycles

MAIN CARGO DOOR-LOWER JAMB FITTING NR 3 SHOWS CORROSION AT AFT LOWER HOLE. REPAIRED NR 3 LOWER JAMB WEB IAW FEDEX EA 8-5230-110663 REV. A. " FUSELAGE, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING INSPECTION AND DOOR RIIG." FITTING(LOWER SUPPORT) REPLACED ON JOB CARD N00788.

Part: FITTING — CORRODED (DOOR FRAME) · corrosion level 2 · airframe 62,721 hrs · 28,083 cycles

MAIN CARGO DOOR-LOWER JAMB FITTING NR 1 SHOWS CORROSION AT LOWER FORWARD HOLE. REPAIRED LOWER JAMB AND REPLACED SUPPORT FITTING NR 1 IAW FEDEX EA 8-5230-110663. "FUSELAGE- MAIN CARGO DOOR - LOWER JAMB FITTING INSPECTION AND DOOR RIG."

Part: FRAME — CRACKED (ZONE 600) · airframe 62,721 hrs · 28,083 cycles

RIGHT WING LEADING EDGE FORMER CRACKED AT XOS625.5 STOP DRILLED CRACK AND INSTALLED REPAIR CLIP PER MD/DC 10-10 SRM 57-20-00 FIG 1 VOL I . FUEL CONTROL PANEL WAS REMOVED. REINSTALLED AND OPS CHECKED TO FACILITATE REPAIR IN REF TO MD10-10 MM 28-00-00-5. OPS CHECK GOOD.

Part: BUSHING — LOOSE (RT ELEVATOR) · airframe 62,721 hrs · 28,083 cycles

RT O/B ELEVATOR O/B DAMPER HINGE FITTING HAT BUSHINGS ARE LOOSE. REMOVED AND REPLACED RT O/B ELEVATOR O/B ELEVATOR O/B DAMPNER HINGE FITTING HAT BUSHINGS IAW CMM 55-21-01 AND FEDEX EA 8-5520-109163. TITLE; LT AND RT ELEVATOR HINGE FITTING OVERSIZE HOLE-REPAIR. ORIGINAL ATTACHED TO FEDEX N/R N00836.

Part: BUSHING — CORRODED (RT ELEVATOR) · corrosion level 2 · airframe 62,721 hrs · 28,083 cycles

RT O/B ELEVATOR I/B ACTUATOR MOUNT FITTING (ON ELEVATOR) CORRODED ON I/B SIDE. REMOVED CORROSION/DAMAGE IAW DAC CMM 55-21-01. REMOVED, FABRICATED AND INSTALLED BUSHINGS IAW DAC CMM 55-21-01 AND FEDEX 8-5520-109163. TITLE; " STABILIZER- LT AND RT ELEVATOR HINGE OVERSIZE HOLE-REPAIR".

Part: BUSHING — LOOSE (LT ELEVATOR) · airframe 62,721 hrs · 28,083 cycles

LEFT OUTBD ELEVATOR THIRD HINGE FROM INBD SIDE HAT BUSHINGS LOOSE IN FITTING BORE FOR OUTBOARD DAMPNER. REMOVED AND REPLACED LT O/B ELEVATOR THIRD HINGE FROM I/B SIDE HAT BUSHINGS IAW CMM 55-21-01 AND FEDEX 8-5520-10913-63. ORIGINAL ATTACHED TO FEDEX N/R N00836.

Part: BUSHING — LOOSE (RT ELEVATOR) · airframe 62,721 hrs · 28,083 cycles

RT O/B ELEVATOR I/B DAMPNER HINGE FITTING HAT BUSHINGS ARE LOOSE. REMOVED AND REPLACED RT O/B ELEVATOR I/B DAMPNER HINGE FITTING HAT BUSHINGS IAW CMM 55-21-01 AND FEDEX EA 8-5520-109163. ORIGINAL ATTACHED TO FEDEX N/R N00836.

Part: SKIN — CRACKED (ZONE 300) · airframe 62,721 hrs · 28,083 cycles

RT INBOARD ELEVATOR UPPER SKIN IS CRACKED ON EDGE. CUT OUT DAMAGED SKIN, FABRICATED REPAIR DOUBLER AND FILLER, AND INSTALLED REF. DC/MD 10 SRM 55-00-01 FIG 3 VOL I AND 51-31-01 VOL II. ALODINED AND PRIMERED PER REF MD/DC 10 SRM 51-21-01 VOL II. THIS IS A MINOR REPAIR.

Part: SKIN — CRACKED (ZONE 300) · airframe 62,721 hrs · 28,083 cycles

DURING DENT EVALUATION ON RT OUTBOARD ELEVATOR UPPER SKIN HFEC INSPECTION REVEALED A 1" CRACK. CUT OUT DAMAGED SKIN, FABRICATED REPAIR DOUBLER AND FILLER AND INSTALLED REF. DC/MD10 55-00-01 FIG 3, VOL I. ALODINED AND PRIMERED PER REF DC/MD 10 SRM 51-21-01 VOL II. RECALCULATED WEIGHT AND BALANCE PER REF DC/MD 10 SRM 55-20-00 VOL II. RECORDED NEW BALANCE CONDITION ON BALANCE TAG. THIS WAS A MINOR REPAIR.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 62,721 hrs · 28,083 cycles

AFT LOWER CARGO, CORROSION AT TIEDOWN SEAT TRACK SURFACE AND AT NUT PLATES HOLES UPPER AND LOWER SURFACES, FS 1790-167 LBL 21". REMOVED DAMAGE SEAT TRACK SECTIONS AND FABRICATED NEW SECTIONS AND SPLICES IAW MD/DC 10 SRM 53-70-00 FIG 1 VOL I. ALODINED AND PRIMED IAW MD/DC 10 SRM 51-21-01-VOL II. INSTALLED IAW MD/DC 10 SRM 53-70-00 FIG1 VOL I, AND 51-31-01 VOL II. THIS IS A MAJOR REPAIR.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 62,721 hrs · 28,083 cycles

CABIN FLOOR SEAT TRACK GOUGED AT STA 1161 TO STA 1171 LBL 48. REMOVED AND REPLACED CABIN SEAT TRACK FROM STA 1129 TO STA 1189, LBL 48 IAW DC/MD10 SRM 53-70-00 FIG 1, VOL 1.

Part: SEAT TRACK — BROKEN (FUSELAGE) · airframe 62,721 hrs · 28,083 cycles

CABIN FLOOR SEAT TRACK LUG BROKEN OUT AT STA 635 LBL47. REMOVED AND REPLACED CABIN FLOOR SEAT TRACK SECTION FROM STA 622 TO STA 746 LBL47 IAW DC/MD10 SRM 53-70-00 FIG 5 , VOL 1.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 62,721 hrs · 28,083 cycles

MAIN CABIN SEAT TRACK WORN STA 635 BL 8.5. REMOVED AND REPLACED SEAT TRACK REF DC/MD 10 SRM 51-10-01 VOL III PG 85 53-70-00 VOL I FIG 1, 51-31-01 VOL II PG 4 , 51-33-01 VOL II PG 4.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 62,721 hrs · 28,083 cycles

CABIN FLOOR SEAT TRACK GOUGED BETWEEN STA-1019 AND STA 1039 LBL 50. REMOVED AND REPLACED MAIN CABIN FLOOR SEAT TRACK AT LBL 50 FROM STA 1006 TO STA 1046 IAW DC/MD 10 SRM 53-70-00 FIG 1 VOL 1.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,721 hrs · 28,083 cycles

AFT FUSELAGE WASTE TANK COMPT, FRAME LWR FWD AND AFT CHORDS AT LONGERONS ATTACH FASTENERS HAVE CORROSION BETWEEN L49R AND L52 AT STA 1997 REMOVED FASTENERS FROM FRAME STA 1997 L49-52 PER MD/DC 10 SRM 51-31-01 VOL 2. REMOVED CORROSION PER MD/DC10 SRM 51-21-01 VOL II ORIG THICKNESS IS .071 PER DOUGLAS DRAWING 34929209 REV C. REMAINING THICKNESS IS .058 AND IS FOUND TO BE WITHIN LIMITS PER MD/DC10 SRM 53-00-01 FIG 1B VOL 1. DOUBLER WAS FOUND TO BE CORRODED AND REQUIRED TO BE FABED PER MD10/DC10 SRM 53-30-00 FIG 5 VOL1. DRILLED UP PER 51-31-01 PAGE 2 VOL II, ALODINED PER MD/DC10 51-21-01 PAGE 31 VOLII PRIMED PER 51-21- 01 PAGE 24 VOLI. INSTALLED PER 51-31-01 VOL II.

Part: FITTING — CRACKED (FUSELAGE) · airframe 62,721 hrs · 28,083 cycles

MAIN CARGO DOOR-LOWER JAMB FITTING NR 5 SHOWS CRACK/CORROSION AT LOWER HOLE.

Part: FLANGE — CRACKED (HORIZ STAB) · airframe 62,721 hrs · 28,083 cycles

RT HORIZONTAL STAB CENTER LE SECTION OB UPPER ATTACH POINT FLANGE CRACKED AT NUTPLATES. REMOVED AND REPLACED RT HORIZONTAL LE SECTIONS CENTER OUTBOARD UPPER "T" CAP CHORD AT XFS 241, IAW DC/MD 10-10 SRM 51-31-01 VOL II AND 51-33-01 VOL II.

Part: ANGLE — CRACKED (HORIZ STAB) · airframe 62,721 hrs · 28,083 cycles

RT HORIZONTAL L/E CENTER I/B SECTION UPPER I/B ATTACHED FLANGE CRACKED MARKED. REMOVED CRACKED RT HORIZ L/E T-CAP SECTION AT UPPER I/B STA XFS 166 IAW DC/MD 10 SRM 55-00-01 FIG, 6 VOL 1, AND INSTALLED ANGLE REPAIR PER MD/DC10 SRM 55-00-01 FIG, 6 VOL 1.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 62,721 hrs · 28,083 cycles

RT HORIZONTAL STABILIZER I/B L/E SECTION NOSE O/B RIB FLANGE CRACKED XFS108, AND ATTACHED CLIP HAS SHEARED FASTENER. INSTALLED REPAIR ANGLE AND STOP DRILLED CRACK IN RT HORIZONTAL STABILIZER IN/B L/E SECTION FORMER RIB AT XFS 108 AND INSTALLED NEW FASTENERS IAW DC/MD10 SRM 53-00-01 FIG 8, SHIT 1, PG 26B. VOL 1.

Part: SEAT TRACK — BENT (BS 625-775) · airframe 62,721 hrs · 28,083 cycles

MAIN CABIN SEAT TRACK BENT SEVERAL AREAS BETWEEN STA. 625 AND STA. 775, BL107.5. REMOVED BENT AREAS IAW EA NR 8-5310-11060411, (FUSELAGE MAINFRAME-SEAT TRACK BETWEEN STA. 635-765/X=107.25. TRIMMED SEAT TRACK LOBES), ALODINED AND PRIMED IAW SRM 51-21-01 PG.1 VOL 11.

Part: DOOR — CORRODED (CARGO DOOR) · airframe 62,721 hrs · 28,083 cycles

FWD PIT HAS CORROSION IN THE AFT CORNER BETWEEN DOOR SEAL AND BEAM. [SUP 05-30-07] REMOVED CORROSION FROM RAIL AND FOUND MATERIAL LOSS TO WITHIN ALLOWABLE LIMITS IAW DC/MD 10 SRM 53-50-00 VOL I FIG. 15A. ALODINED AND PRIMED REWORK AREA IAW DC/MD 10 SRM 51-21-01, VOL II PG 21 AND24. REMOVED CORROSION FROM FRAME AND WEB AND FOUND MATERIAL LOSS FOR BOTH TO EXCEED ALLOWABLE LIMITS IAW DC/MD 10 SRM 53-00-01 VOL I FIG 1B. REPAIRED FRAME IAW FED EX EA 8-5350- 109161 "FUSELAGE-FWD LOWER CARGO DOOR JAMB FRAME STA 1002 CORD-REPAIR" REPAIRED WEB IAW DC/MD10 SRM 53-00-01 VOLI FIG 10.

Part: BEAM — CORRODED (CARGO DOORWAY) · airframe 62,721 hrs · 28,083 cycles

FWD PIT HAS CORROSION IN THE FORWARD LOWER CORNER BETWEEN DOOR SEAL AND BEAM. [SUP 05-30-07] REMOVED CORROSION FROM RAIL, VERIFIED BLEND OUT AND REMAINING THICKNESS, PER FEDEX EA 8-5350-109152.

Part: HANDLE — WORN (ZONE 200) · airframe 62,721 hrs · 28,083 cycles

R1 DOOR EMERGENCY HANDLE BACKLOCK DOES NOT HOLD HANDLE ONCE HANDLE IS MOVED TO EMERGENCY POSITION. FOUND OVERRIDE LEVER BINDING WITH BACKLOCK. REPLACED BUSHING, SEAL AND LEVER IAW MD10-10 MM 52-11-14-2 AXIAL PLAY CK GOOD. PERFORMED PNEUMATIC TEST TO CK BACK LOCK, OPS CK GOOD IAW MD10-10-MM 52-10-01-2.

Part: SKIN — GOUGED (LT WING TE FLAP) · airframe 62,721 hrs · 28,083 cycles

LT WING O/B FLAP O/B LOWER SKIN GOUGED ON INTERIOR SIDE. CUT OUT DAMAGED PART REF; DC/MD10-10 SRM 57-10-00 FIG 85 VOL 1. FABBED DOUBLER REF; DC/MD10-10 SRM 57-10-00 VOL1. ALODINED AND PRIMED REF; DC/MD10-10 SRM 51-21-01 VOL 11. INSTALLED DOUBLER REF; DC/MD10-10 SRM 51-35-01 VOL 11. TOUCH UP PAINT REF; DC/MD10-10 SRM 51-21-02 VOL11.

Part: SKIN — GOUGED (LT WING TE FLAP) · airframe 62,721 hrs · 28,083 cycles

LT WING O/B FLAP O/B LOWER SKIN GOUGED ON INTERIOR SIDE. CUT OUT DAMAGE REF; DC/MD10-10 SRM 57-10-00 FIG 85 VOL 1. FABBED REPAIR DOUBLER. [SUP 04-30-07] REF; DC/MD10 -10 SRM 57-10-00 VOL 1. ALODINED AND PRIMED REF; DC/MD10-10 SRM 51-21-01 VOL 11. INSTALLED DOUBLER REF; DC/MD10-10 SRM 51-35-01, VOL 11. TOUCH UP PAINT REF; DC/MD10-10 SRM 51-21-02 VOL 11.

Part: SHUTOFF VALVE — INOPERATIVE (ANTI-ICE SYSTEM) · airframe 61,456 hrs · 27,565 cycles

LEVEL 3 MANF FAIL SYS 1 RAN QRH, DIVERTED TO SMF PER CREW VERBAL, ALERT APPEARED WHEN WING ANTI-ICE MEL. ACN RELEASED FOR SERVICE PER MEL/CDL: 30-11-01 CATEGORY: C EXPIRATION: 09SEP06 "MEL 30-11-01: (LEFT) WING A/I SHUTOFF VALVE(S) - INOP. DO NOT OPERATE A/C IN ICING."

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 60,510 hrs · 27,146 cycles

UNSAFE GEAR IND RT MAIN AFTER T/O PRI AND SEC DISPLAY. FOLLOWED CHECKLIST TO SAFE GEAR UP CONDITION. FACT INSP RT GEAR AND DOOR AREA FOR DAMAGE OR DEFECTS WITH NONE FOUND. CHECKED PSEU NO CURRENT FAULTS OR FAULTS ON THE INBD LEG. FAULTS ON LEGS 7 AND 8 FOR "R GEAR UP AND LATCHED A/B SENSOR DISAGREE". JACKED A/C IN HGR AMM 07-11-00-2. SWUNG LANDING GEAR, REF AMM 32-30-00-5. UNABLE TO DUPLICATE. A/C GEAR SWINGS NORMAL. REMOVED AND REPLACED D1-80 R MAIN GEAR DOOR UPLATCH SENSOR. INSP RT MLG DOOR AND FOUND SPRING LOADED ROLLER FOR UP LOCK MECHANISM STIFF. ADJ BOLT AND LUBED. ARM OPERATES NORMAL. CYCLED GEAR AND ROLLER ENGAGES HOOK AS REQ. AMM 32-14-01-2 AND 32-34-03-2.

Part: FINGER DOUBLER — CORRODED (LT OB AILERON) · corrosion level 2 · airframe 60,443 hrs · 27,114 cycles

LT OUTBOARD AILERON, I/B UPPER SKIN FINGER DOUBLERS DELAMINATED WITH CORROSION. FABRICATED AND INSTALLED NEW SKIN IAW DC 10 SRM 51-35-01 VOL II AND DAC DWG ARC1110, AND EA 8-5710-92633 WINGS - LT AILERON SKIN CORRODED.

Part: REPAIR — UNKNOWN (NR 1 SLAT)

FLUSH REPAIR LT WING NR1 SLAT STA. XORS 60, LE, MARKED NR 93. REPAIR REQUIRES EVALUATION FOR MAJOR/ MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. VISUALLY INSPECTED REPAIR L/W NR 1 SLAT STA. XORS 60 L/E, MARKED NR 93. FOUND TO BE WITH- IN EA NR 8-5710-96350 TITLE (WINGS- LT SLAT NR 1 HAS EXSTING REPAIR-EVALUATED) LIMITS WITH RESPECT TO SIZE, SHAPE, SPACING AND EDGE DISTANCE. THIS REPAIR WAS NOT REMOVED FOR THIS INSPECTION.

Part: REPAIR — MISINSTALLED (BS 740) · airframe 60,443 hrs · 27,114 cycles

EXTERIOR FUSELAGE SKIN STA 740 BETWEEN L44R-L45R HAS NON-SRM REPAIR. SRM REPAIR ACCOMPLISHED ON FEDEX NR N00765. MAJOR REPAIR

Part: SKIN — CRACKED (TE FLAPS) · airframe 60,443 hrs · 27,114 cycles

LEFT WING O/B FLAP UPPER SKIN CRACKED. PERFORMED HEFC IAW DC10 NDT SPM 06-10-01. 601. REMOVED DAMAGED AREA IAW DC10-10 SRM 57-10-00 VOL I FIG 85. FAB DOUBLER & FILLER IAW DC10-10 SRM 57-10-00 VOLI FIG 85. ALODINED & PRIMED IAW DC10-10 SRM 51-21-01 VOLII PG 21 & PG 25 AND INSTALLED DOUBLER & FILLER IAW DC10-10 SRM 57-10-00 VOLI FIG 85 & DC10-10 SRM 51-53-02 VOLII PG 3.

Part: REPAIR — MISINSTALLED (FUSELAGE) · airframe 60,443 hrs · 27,114 cycles

N00765 EXTERIOR FUSELAGE SKIN STA 725-730 BETWEEN L44R-L45R HAS NON-SRM REPAIRS. REMOVED EXSISTING REPAIRS FS 725-760 L44R-L45R, FABR. EXTERNAL DOUBLERS AND FINGER DOUBLERS AND INSTALLED IAW DC10 SRM 53-20-00 FIG. 6 SHT 3 AND SHT 5 VOL I AND DC10SRM 51-33-01 FIG 1 VOL II. MAJOR REAPIR.

Part: REPAIR — MISINSTALLED (BS 760) · airframe 60,443 hrs · 27,114 cycles

EXTERIOR FUSELAGE SKIN STA 760 BETWEEN L44R-L45R HAS NON-SRM REPAIR.

Part: SUPPORT FITTING — CORRODED (ZONE 500) · airframe 60,443 hrs · 27,114 cycles

LEFT WING OUTBOARD FLAP VANE NR 1 SUPPORT FITTING CORRODED. REMOVED AND REPLACED SUPPORT FITTING PART NUMBER ARC1495-505 IAW EO E8-5750-7-5004.

Part: SENSOR — MALFUNCTIONED (NR 1 FAN SPEED) · airframe 58,723 hrs · 26,348 cycles

CLIMB-OUT PASSING 3000 FT ENG 1 EXCEEDANCE N1 168.6. PULL THROTTLE NR 1 BACK. ALSO ATS OFF. ALL OTHER INST NORM, NO VIB. REENGAGED ATS AS SOON AS NR 1 WAS CLIMB POWER IMMEDIATELY JUMPED TO RED EXCEED OF 168.6 AND DISCONNECTED ATS. NR 1 THROTTLE BACK TO IDLE AND LAND AT OAK. INSPECTION FAN INLET COWL, FAIRINGS, FAN CASE, ACOUSTICAL PANELS, FAN BLADES, SPINNER AND ADJACENT AREAS. NO DEFECTS NOTED. REMOVED AND REPLACED FAN SPEED SENSOR REF MD-10 MM 77-11-01- 2. VIA 1,2 AND 3, SHOWED N1 SPIKES WAY OUT OF RANGE AND N2 AND EGT INDICATIONS WERE IN LIMITS PER JRHCH4. RAN NR 1 ENGINE PER JRH CH5,4 AND 6. ALL INDICATIONS FROM IDLE TO MAX POWER IN NORMAL RANGE, NO SPIKES. A/C OK FOR SERVICE.

Part: RIB — CRACKED (ZONE 600) · airframe 58,247 hrs · 26,148 cycles

WINGS - RT WING RIB UPPER CAP CRACKS AT XORS 372 AROUND CUTOUTS FOR STRINGER 12 AND 13. TRIMMED OUT AND ROUNDED CRACKS, INSTALLED REPAIR ANGLE AND DOUBLER TO RESTORE STRENGTH IAW FEDEX AE 8-5710-75716.

Part: RIB — CRACKED (ZONE 500) · airframe 58,247 hrs · 26,148 cycles

WINGS - LT WING RIB UPPER CAP CRACKS AT XORS 372 AROUND CUTOUTS FOR STRINGER 12 AND 13. TRIMMED OUT AND ROUNDED CRACKS, INSTALLED REPAIR ANGLE AND DOUBLER TO RESTORE STRENGTH IAW FEDEX AE 8-571-75732.

Part: SKIN PANEL — CRACKED (ZONE 300) · airframe 58,247 hrs · 26,148 cycles

HORIZONTAL STABILIZER - CONSTANT SECTION, UPPER AND LOWER SKIN CRACKS WITHIN FLYABLE LIMITS. PANELS REPLACEMENT PER SB 55-16 IAW FEDEX EA 8-5510-73237.

Part: SEAL — LEAKING (COCKPIT) · airframe 54,868 hrs · 24,740 cycles

F/O WINDOW LOCKING BOLT WAS OUT OF POSITION DURING INITIAL CLIMB-OUT. LOUD NOISE FROM AIR LEAK. RETURNED TO LAND AT MSP, DUMPED 10,000 LBS FOR LANDING WEIGHT. REINSTALLED RT SLIDING WINDOW SEAL PER STD PRAC & DC10-10 AMM 56-12-00-4. OPERATIONAL CHECK OF RT SLIDING WINDOW NORMAL PER DC10-10 AMM 56-12-00-4 & 56-12-00-5. A/C OK FOR SERVICE.

Part: SIDEWALL — CORROSION (BS 1210)

SNRM 345, CORROSION FOUND ON TOP OF CTR TANK, BELOW MAIN CABIN FLOOR, LT SIDEWALL AREA, STA 1210. *S/D* CLEANED CORROSION REF SRM 53-00-01. NDT MEASURED REMAINING SKIN THICKNESS. COMPLIED WITH HFEC INSP, NO DEFECTS NOTED.

Part: CTR WING SECT — CORROSION (BS 1210)

SNRM 345. CORROSION FOUND ON TOP OF CTR TANK, BELOW MAIN CABIN FLOOR, LT SIDEWALL AREA, STA 1210. CLEANED CORROSION REF. SRM 57-20-00. COMPLIED WITH HFEC INSP. NO DEFECTS NOTED. MEASURED REMAINING SKIN THICKNESS. REWORKED PER EA 8-5710-31746 WORK INSTRUCTIONS. 11/08/96.