N362FE

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 77,408 hrs · 28,439 cycles

SUSPECT CRACK ON UPPER AFT T CHORD OF DOOR CUT OUT STATION 535 ON INBD SIDE FROM RIVET HOLE TO EDGE. PERFORMED HFEC ON UPPER AFT T CHORD OF DOOR CUT OUT OF NR 3 PACK BAY DOOR FRAME IAW NTM PT6. CRACK VERIFIED. INSTALLED SUPPORT BRACKET REF MD 10 SRM 51-31-01 VOL2 AND DRAWING ACA0052-6.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,408 hrs · 28,439 cycles

EVIDENCE OF A CRACK IN THE NR 3 PACK BAY DOOR FRAME. NR 3 PACK DOOR FRAME/SKIN DAMAGE REPAIRED REF MD10/DC 10 SRM 53-50-00 FIG A SHEET 3.

Part: SKIN — CRACKED (LT WING) · airframe 77,335 hrs · 28,396 cycles

ON WALK AROUND FOUND POSSIBLE CRACK ON LT WING AT FWD INBD CORNER OF FUEL PNL. CONFIRMED CRACK AT FWD INBD CORNER OF FUEL PNL BY HFEC INSPECTION IAW NDTSPM PT 6. CRACK TERMINATES AT RIVET. STARTED REMOVING DOOR TO ASSIST SHEET METAL. FINISHED REMOVING LT WING REFUEL PNL IAW SMP. REMOVED DAMAGED SKIN USING HALF INCH RADIUS IAW SRM 57-10-00 VOLUME 1 FIGURE 68. REMOVED LT LE PNL 519AB FOR ACCESS TO SKIN REPAIR. FABRICATED DOUBLER & FILLER IAW SRM 57-10-00 FIG 68. OK TO INSTALL. INSTALLED REPAIR PARTS IAW SRM 57-10-00 VOLUME 1 FIGURE 68. APPLIED PROTECTIVE PAINT FINISH IAW SRM 51-21-02.

Part: SPAR CAP — CRACKED (LT WING) · airframe 77,029 hrs · 28,243 cycles

DURING C7, B9 CHECK AT LAX CRACK FOUND IN HOLE B & C IN REAR SPAR LOWER CAP AT XORS 345.75. ADDITIONAL INSPECTION FOUND UPPER SPAR CAP FLANGE TO HAVE A 2.8 INCH CRACK RUNNING BETWEEN HOLES A & C INCLUDING THE B HOLE. IN ADDITION A CRACK WAS FOUND IN THE STANDING LEG OF THE ARB0164-1 DOG BONE STIFFENER. AN EA WAS ISSUED IAW EA 8-5710-T0 306060 TO TEMPORARILY REPAIR DISCREPANT CONDITION. REPAIRED IAW EA 8-5710-T0306060.

Part: WIRE — DAMAGED (E/E COOLING) · airframe 75,359 hrs · 27,394 cycles

ON POST FLIGHT CHECK FOUND NR 3 AVIONICS RACK COOLING BREAKER POPPED. RESET BREAKER AND IT POPPED AGAIN. REMOVED DAMAGED WIRING AND REPAIRED FOLLOWING WIRES. B115-280-14B,B115-12-14C,B115-281-14C,B115-283-14B, B115-284-14C,B115-282-14A,B115-42-12,B115-276-14B, B115-41-12,B115-10-14A WITH SPLICES PER SWPM 20-10-03. CHECKED ALL AFFECTED WIRING FOR INTEGRITY AND OPERATION. ACCOMPLISHED WIRE BUNDLE REROUTE OF ABS9115 AND ABS9102 PER E.A 8-2126-166275.

Part: SKIN — CORRODED (BS 1109) · airframe 74,330 hrs · 26,832 cycles

CORROSION FOUND ON EXTERNAL FUSELAGE SKIN AT BS 1109 AT S46R. REPAIRED SKIN IAW SRM 53-20-00, FIG 6, REPAIR CLASSIFED AS MAJOR.

Part: CARGO TRACK — WORN (MAIN DECK) · airframe 74,330 hrs · 26,832 cycles

MAIN DECK CARGO TRACK AT BS 1387.5, LBL 72 HAS TWO WORN AND BROKEN SCALLOP LOBES, REPAIRED CARGO TRACK IAW SRM 53-70-00 FIG 1.

Part: SKIN — TORN (RT WING TE FLAP) · airframe 74,330 hrs · 26,832 cycles

RIGHT OTBD T/E FLAP LOWER SKIN HAS OIL CANNING ABOUT 45" OTBD OF FLAP VANE CARTRIDGE CUT-OUT AND 25" FWD OF T/E. REPAIRED RT WING OTBD T/E FLAP LOWER SKIN IAW SRM 57-10-00, FIG 7, REPAIR CLASSIFIED AS MAJOR.

Part: SKIN — CORRODED (BS 1621) · airframe 74,330 hrs · 26,832 cycles

EXTERNAL FUSELAGE SKIN BULGING AT BS 1621 BETWEEN S47-48R. REPAIRED EXTERNAL FUSELAGE SKIN IAW SRM 53-20-00, FIG 6, SHEET 5 AND 6, REPAIR CLASSIFIED AS MAJOR.

Part: SEAT TRACK — WORN (BS 755) · airframe 74,330 hrs · 26,832 cycles

MAIN DECK SEAT TRACK AT BS 755 AT LBL 47.5 HAS CHIPPED LOBES. REMOVED AND REPLACED MAIN DECK SEAT TRACK BETWEEN BS 725 TO 765 AT LBL 47.5 IAW SRM 51-31-01 AND SRM 53-70-00, FIG. 1, REPAIR CLASSIFIED AS MAJOR.

Part: LIGHT — INOPERATIVE (L1 DOOR SLIDE) · airframe 72,848 hrs · 26,073 cycles

L1 DOOR SLIDE PTT LIGHT INOP. WIRE THAT ATTACHES TO C BATTERY HOUSING BROKEN OFF. RELEASED FOR SERVICE IAW MEL: 25-61-01, PRESS VERIFIED IAW MEL 25-61-01. ACFT OK FOR SERVICE.

Part: ANTENNA — MALFUNCTIONED (ELT) · airframe 72,851 hrs · 26,074 cycles

CONSTANT ELT TONE ON 121.5 BOTH RADIOS. OVERHEAD COCKPIT ELT PANEL RESET NO HELP, RESET AT ELT NO HELP. TONE GOES AWAY THEN COMES BACK AFTER 5 TO 10 MINUTES. WITH ELT SWITCH IN OFF DETENT TONE STILL SOUNDS. WITH ELT SWITCH IN OFF AND ELT 6 INCH ANTENNA REMOVED TONE HAS STOPPED. REQUIRES EA FOR ANTENNA REMOVAL. ANTENNA STOWED IN FIRST AID KIT COMPARTMENT.

Part: WEB — CRACKED (NR 1 SLAT) · airframe 71,591 hrs · 25,449 cycles

NR 1 RT SLAT DAMAGED AT INBD WEB/RIB STRUCTURE R & R FITTING PN ARB701602 IAW DWG ARB 7016 VIEW CC AND SRM 51-31-01, VOL II. R & R WEB PN ARB7128-24 IAW SRM 51-33-01 VOL II AND DRWN ARB7128-24.

Part: FEEDER CABLE — DAMAGED (ELECTRICAL SYS) · airframe 71,591 hrs · 25,449 cycles

WIRE NR C501-19-00A AT EXTERNAL POWER PLUG PIN "A" HAD OVERHEAT/ARCING DAMAGE AND POWER RECEPTACLE R5-1065 PIN "A" HOLE MELTED DUE TO OVERHEAT CONDITION. WIRE NR C501-23-00A AT LUG A2 OF EXTERNAL POWER BREAKER R2-218 HAD OVERHEAT DAMAGE AND WIRE STRANDS SEPARATED, MELTED, AND BROKEN. 2/0 POWER FEEDER CABLE INSTALLED AT EXTERNAL POWER RECEPTACLE R5-1065 PIN A TO LUG A1 AT EXTERNAL POWER BREAKER R2-218 AND FROM LUG A2 OF EXTERNAL POWER BREAKER TO S3-517, LUG 1. WIRE HOOKUP LIST CALLS FOR 1/0 CABLE TO BE INSTALLED AT THESE LOCATIONS N00691: ACFT WILL NOT ACCEPT EXTERNAL POWER. REPLACED BAD FEEDER CABLES C501-19-00A AND C501-23-00A. OPS CK GOOD IAW DPS 1.834- 1 AND EA 8-2020-137473 AND WDM 24-41-01 SH 2.

Part: RELAY — MALFUNCTIONED (THRUST REVERSER) · airframe 70,879 hrs · 25,105 cycles

REJECTED T/O DUE TO: LEVEL 1 ALERT: REV 1, PRESS FAIL T, DUPLICATED REV 1 PRESS FAULT ON 3 DIFFERENT TAXI/RUN-UP TESTS IAW JRH CHAPT 5 AND CHPT 4-8. REMOVED AND REPLACED NR 1 T/R ACTUATION SYS LOCK RELAY BOX IAW MM 78-33-10-6 AND CHECKED IAW MM 87-33-10-4. TAXI'D AND RAN NR 1 ENGINE TO MAX ASSURANCE POWER SETTINGS IAW JRH CHAPT 5 AND CHPT 4-8. NO REPEAT. PROBLEM CLEARED. OK TO CONTINUE.

Part: CYLINDER — SHEARED (SLAT) · airframe 70,774 hrs · 25,060 cycles

WHILE CONFIGURING FOR LANDING, RECEIVED A LEVEL 2 SLAT DISAGREE ALERT. RAN QRH PROCEDURE WHICH REQUIRED A FLAPS 22/RETRACT LANDING. LANDED ILS 36C CAPTAINS LANDING. REMOVED AND REPLACED LT WING INBD AND OTBD SLAT CYLINDERS REF AMM 27-82-01-2. LEAK CK GOOD.

Part: LINE — LOOSE (NR 2 ENGINE OIL) · airframe 70,083 hrs · 24,729 cycles

NR 2 ENG OIL QTY DROPPED FROM 12 QTS TO 3 QTS IN 2HRS. TEMP/PRESS NORMAL. DECREASED TO 2 QTS AT IDLE WITH DECREASING PRESSURE. SHUTDOWN NR 2. NR 2 ENG AND FOUND LINE LOOSE FROM NR 2 ENG OIL SCAVENGE FILTER BOWL TO THE OIL STRAINER CLOGGING SWITCH.

Part: PUSH-PULL CABLE — DAMAGED (THROTTLE) · airframe 70,079 hrs · 24,727 cycles

AT TOP OF DESCENT NR 2 ENG WOULD NOT RETARD BELOW 74 PERCENT N1. NR 2 THROTTLE WAS AT LEAST TWO KNOB WIDTHS ABOVE NR 1 AND NR 3 THROTTLES. SHUTDOWN NR 2 ENG ON APPROACH. UNEVENTFUL APPROACH AND LANDING. FINISHED REMOVING OLD PUSH-PULL CABLE AND INSTALLED NEW PUSH-PULL CABLE PER MM 76-11-01-2 , ADJ CABLE PER SAME REF. RAN NR 2 ENGINE PER JRH CHAPTER 5, OK FOR SERVICE.

Part: BEARING — FAILED (MLG WHEEL) · airframe 69,698 hrs · 24,565 cycles

NR 1 TIRE ASSY OUTSIDE BEARING FAILURE. REMOVED WHEEL AND BRAKE ASSY FROM NR 1 AXLE LT MLG TRUCK ASSEMBLY TAG NR 5023BO. REPLACED LEFT MAIN LANDING GEAR TRUCK BEAM AND AXLE ASSY PER M/M REF 32-12-01-2. AIRCRAFT OK FOR FURTHER SERVICE.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 67,511 hrs · 23,523 cycles

CORROSION POSSIBLE ON FUSELAGE SKIN CORROSION LIMITED TO LONGERON DAMAGE WHICH WAS REPAIRED PER 53-10-00 VOL 1 OF MD10-10.

Part: PROXIMITY SENSOR — UNKNOWN (CARGO DOOR) · airframe 67,032 hrs · 23,309 cycles

ON DEPARTURE RECEIVED LVL 2 CARGO DOOR FWD "B" ALERT, RAN QRH AND ALERT DISAPPEARED, MEL 52-40-01-05: CARGO DOOR FWD "B" ALERT INOP. VERIFY DOOR IS CLOSED AND LOCKED PRIOR TO BLOCK-OUT. INSPECTED "B" DOOR WARNING SWITCH FOR FWD LWR CARGO DOOR WARNING FOR CONDITION AND SECURITY. NOTED NO FAULTS. REMOVED AND REPLACED THE LOWER FWD CARGO DOOR WARNING "B" (D1-92) PROXIMITY SENSOR, DOOR WARNING SYSTEM OPS NORMAL. REF MD10-10 AMM 52-70-03-2.

Part: BRACKET — CRACKED (RT WING) · airframe 66,189 hrs · 22,935 cycles

RT O/B SLAT DRIVE O/B BRACKET FWD FLANGE RADIUS IS CRACKED. SEQ CARD 735. REMOVED AND REPLACED RT O/B SLAT DRIVE MECHANISM.

Part: KEELBEAM — CRACKED (ZONE 100) · airframe 63,273 hrs · 21,647 cycles

AUXILIARY POWER UNIT KEEL CAP ASSEMBLY HAS 9 INCH CRACK FROM FUSELAGE STATION 2019 TO STATION 2028 AT STRINGER 45 RIGHT. REPAIRED STRINGER IAW EA 8-5310-83868, FUSELAGE - AFT BODY KEEL CAP SPLICE AT STA 2040 - REPAIR, AND MD 10 SRM 51-31-01 VOL 2 AND 51-31-01 VOL 2.

Part: KEELBEAM — CRACKED (ZONE 100) · airframe 63,273 hrs · 21,647 cycles

AUXILIARY POWER UNIT KEEL CAP ASSEMBLY HAS 9 INCH CRACK FROM FUSELAGE STATION 2019 TO STATION 2028 AT STRINGER 45 RIGHT. REPAIRED STRINGER IAW EA 8-5310-83868, FUSELAGE - AFT BODY KEEL CAP SPLICE AT STA 2040 - REPAIR, AND MD 10 SRM 51-31-01 VOL 2 AND 51-31-01 VOL 2.

Part: DOOR — VIBRATES (NLG) · airframe 62,703 hrs · 21,397 cycles

14000 FT HEAVY VIBRATION SLOWED AND LANDED WITH NO PROBLEM, EVEN WITH GEAR DOWN HAD VIBRATION. "DECLARED EMERGENCY" HAD FIRE TRUCKS STANDING BY. REMOVED AND REPLACED LT NOSE GEAR DOOR PER MM 32-23-01-2. ACCOMLISHED GEAR SWING AND DOOR FIT CHECK PER EA 8-3220-84377 REV POS2 BY EMP NR EJO 476920 AND SOLD TO QA 275049, 11/20/04, JTK183086 RII:275049.

Part: HINGE BRACKET — CORRODED (ZONE 500) · airframe 60,603 hrs · 20,423 cycles

LT OUTBOARD FLAP INBOARD HINGE BRACKET, CORROSION REPAIR (P/N ARC0502-11) LT O/B FLAP I/B HINGE BRACKET CORROSION REPAIR,P/N ARC,0502-11 CLOSED ON 09/09/2003 FEDEX N/R S00031.

Part: HINGE BRACKET — CORRODED (ZONE 600) · airframe 60,603 hrs · 20,423 cycles

RT OUTBOARD FLAP- OB HINGE BRACKET CORROSION REPAIR (P/N ARC0503) COMPLIED WITH EA 8-5750-72274_WINGS RT O/B FLAP-O/B HINGE BRACKET CORROSION REPAIR P/N ARC, 0503 CLOSED ON 09/09/2003 FEDEX NR S00018

Part: CASE — GOUGED (ZONE 400) · airframe 60,603 hrs · 20,423 cycles

GOUGES IN EXTERIOR OF NR 2 FAN FRAME CASE. COMPLIED WITH E.A. 8-7220-72285 ENGINES-DISPOSITION OF GOUGES IN EXTERIOR OF NR 2 ENGINE FAN FRAME CASE.

Part: ARM — CORRODED (ZONE 600) · airframe 60,603 hrs · 20,423 cycles

WINGS-OUTBOARD FLAP REWORK OF CARRAGE SUPPORT ARM P/N ARC 2177. COMPLIED WITH E.A. 8-5740-72289. WINGS-OUTBD FLAPS REWORK OF CARRAGE SUPPORT ARM P/N ARC 2177.

Part: BOLT — INACCURATE (ZONE 500) · airframe 60,603 hrs · 20,423 cycles

WINGS-RIBS AND BULKHEADS-LT OUTBOARD FLAP HINGE STUD BOLT SUBSTITUTION. COMPLIED WITH E.A.8-5710-72287. WINGS-RIBS AND BKHDS- FLAP HINGE STUD BOLT SUBSTITUTION.

Part: SUPPORT — CRACKED (THRUST REVERSER) · airframe 60,603 hrs · 20,423 cycles

THRUST REVERSER-SUPPORT ASSY TORQUE BOX WEB REPAIR. COMPLIED WITH E.A.8-7830-72283. EXHAUST-THRUST REVERSER-SUPPORT ASSY TORQUE BOX WEB REPAIR.

Part: WEB — CRACKED (THRUST REVERSER) · airframe 60,603 hrs · 20,423 cycles

EXHAUST SYSTEM THRUST REVERSER SUPPORT WEB CRACK REPAIR. COMPLIED WITH E.A.8-7830-72281. EXHAUST SYSTEM THRUST REVERSER SUPPORT ASSY WEB CRACK REPAIR.

Part: SUPPORT — CRACKED (NR 1ENG STATOR) · airframe 60,603 hrs · 20,423 cycles

COMPLY WITH E.A. 8-7210-72270- ENGINE-BASIC- FAN STATOR SUPPORT HALF, CRACK REPAIR. ENGINE-BASIC FAN STATOR SUPPORT HALF CRACK REPAIR. CLOSED ON 08/25/2003 FEDEX .

Part: THRUST REVERSER — CRACKED (NR 2 ENGINE) · airframe 60,603 hrs · 20,423 cycles

COMPLY WITH EA 8-7832-72265 EXHAUST-THRUST REV- FIXED BODY UPPER ANGLE CRACK REPAIR. EXHAUST-THRUST REV FIXED BODY UPPER ANGLE CRACK REPAIR.

Part: SUPPORT ANGLE — CRACKED (T/E FLAP) · airframe 60,603 hrs · 20,423 cycles

LEFT WING I/B FLAP FAIRING PANEL SUPPORT STRUCTURE ANGLE IS CRACKED. REMOVED AND REPLACED ANGLE IAW SRM 51-31-01 AT MAE ON N00420 WO 23696.