N566FE

Part: UPLOCK SENSOR — OUT OF ADJUST (LT MLG) · airframe 85,816 hrs · 32,039 cycles

DURING INTIAL ACCELERATION AND CLIMB AFTER TAKEOFF, RECEIVED INTERMITTENT LEFT MAIN GEAR UNLOCKED INDICATIONS, RED LIGHT BY GEAR HANDLE AND EAD CONFIGURATION PAGE. BEGAN AT 300 KIAS AND WOULD COME ON FOR APPROXIMATELY 2 SECONDS THEN OUT. SLOW TO 260/M. 70 AND LIGHT REMAINED OUT. FOUND THE LEFT GEAR UPLOCK SENSOR OUT OF RIG AND OUT OF LIMITS. RIGGED THE LEFT GEAR UPLOCK SENSOR IAW MM 32-61-15-4. PERFORMED MAIN GEAR PROXIMITY ADJUSTMENT TEST IAW MM 32-61-15-5. INDUCTANCE CHECKED GOOD. OK FOR SERVICE.

Part: INDICATOR — FAILED (L1 DOOR SLIDE) · airframe 85,286 hrs · 31,741 cycles

R1 DOOR SLIDE WILL NOT TEST. REMOVED AND REPLACED SLIDE PRESSURE INDICATOR ASSEMBLY IAW 25-63-03-2 AND PERFORMED OPS CHECKED IAW 25-61-03-5. OPS CHECK IS NORMAL.

Part: SOLENOID — MALFUNCTIONED (L1 DOOR) · airframe 85,227 hrs · 31,704 cycles

L1 DOOR INTERIOR ELECTRIC SWITCH IS INTERMITTANT. REPLACED L1 DOOR SOLENOID S2-730 PER AMM 52-11-13. PERFORMED NUMEROUS NORMAL OPERARATIONS WITH NO DISCREPANCIES. OK FOR SERVICE.

Part: SUPPORT FRAME — CRACKED (NR 3 PYLON) · airframe 85,026 hrs · 31,613 cycles

NR 3 ENGINE PYLON, SUPPORT FRAME IS CRACKED. REPAIRED IAW EA 8-5410-T0330096 AND SRM 54-00-01 FIG 12 VOL 1.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 85,026 hrs · 31,613 cycles

AFT CARGO SHEAR TIE CORRODED STA 1781 RBL, REMOVED AND REPLACED SKIN ATTACH LEG IN REF TO SRM 53-30-00 FIG 9 PAGE 34 VOL1.

Part: BOLT — SHEARED (RT AILERON) · airframe 85,026 hrs · 31,613 cycles

RIGHT INBD AILERON, CENTER ATTACH FITTING BOLT HEAD SHEARED. REMOVED AND REPLACED CENTER ATTACH FITTING BOLT AS REQUIRED IAW AMM 57-44-01-2 AND AILERON OPS CHECKED GOOD IAW AMM 27-10-00-5.

Part: FLOOR SUPPORT — DAMAGED (BS 1701-1721) · airframe 85,026 hrs · 31,613 cycles

CENTER CARGO COMPARTMENT RT OF CENTER ROLLER TRAY FWD END FLOOR BOARD MOUNT HOLES ARE DOUBLE DRILLED CUT OUT DAMAGE SECTION OF FLOOR CHANNEL AND REPAIR IAW SRM 53-70-00 VOL 1, FIG 7, SHEET 3

Part: ATTACH FITTING — CRACKED (LT WING) · airframe 85,026 hrs · 31,613 cycles

LT WING ATTACH TEE FRONT SPAR TO FRAME HAS 2 IN CRACK IN RADIUS STA 1159 X=118 REF SRM 57-20-00 FIG 5. VERIFIED WITH NDT AND MARKED END OF CRACK. REPAIRED ATTACH TEE FRONT SPAR TO FRAME REF SRM 57-20-00 FIG 5 PAGE 19 VOL.1.

Part: ATTACH FITTING — CRACKED (LT WING) · airframe 85,026 hrs · 31,613 cycles

LT WING ATTACH TEE FRONT SPAR TO FRAME HAS 2 IN CRACK IN RADIUS STA 1159 X=118. REF SRM 57-20-00 FIG 5. VERIFIED WITH NDT AND MARKED END OF CRACK. REPAIRED TEE FRONT SPA TO FRAME REF SRM 57-20-00 FIG 5 PAGE 19 VOL 1.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 85,026 hrs · 31,613 cycles

RIGHT INBD FLAP LOWER SURFACE DENTED. REPAIRED IAW SRM 57-10-00. FIG 85, SHT 1, VOL 1

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 85,026 hrs · 31,613 cycles

RIGHT WING TE FLAP LOWER SKIN AT APPROX XIFH 253 HAD TWO DENTS. REPAIRED IAW SRM 57-10-00 FIG 85, SHT 1, VOL 1.

Part: SKIN — CRACKED (LT WING TE FLAP) · airframe 85,026 hrs · 31,613 cycles

LEFT OTBD FLAP UPPER L/E SKIN CRACKED. REPAIRED IAW SRM 57-00-01, FIG 4, SHT 2, VOL 1.

Part: SKIN — CRACKED (LT WING TE FLAP) · airframe 85,026 hrs · 31,613 cycles

LEFT OTBD FLAP UPPER INBD SKIN IS CRACKED. REPAIRED IAW SRM 57-00-01, FIG 4, SHT 2, VOL 1.

Part: SKIN — DAMAGED (BS 959-965) · airframe 85,026 hrs · 31,613 cycles

LOWER FWD CARGO DOOR CUT OUT IS DAMAGED AT THE LOWER AFT CORNER. REPAIRED IAW SRM 53-50-00 FIG.26 SHEET 3 VOL1.

Part: SKIN — CRACKED (LT WING TE FLAP) · airframe 85,026 hrs · 31,613 cycles

LEFT OTBD FLAP UPPER T/E SKIN FOUND CRACKED. REPAIRED IAW SRM 57-00-01 FIG 4 SHT 2 VOL 1.

Part: SHEAR TIE — CRACKED (BS 1661) · airframe 85,026 hrs · 31,613 cycles

MAIN CABIN SHEAR TIE HAS A CRACK AT BS 1661 JUST BELOW STRINGER 18L. REMOVED AND REPLACED THE DAMAGED SECTION OF THE SHEAR TIE IAW SRM 53-30-00 FIG. 10 AND DWG AFA0005.

Part: SKIN — CRACKED (LT WING) · airframe 85,026 hrs · 31,613 cycles

LEFT WING FIXED LEADING EDGE INT UPPER SKIN CRACKED. SEVERAL CRACKS BEYOND PREVIOUS STOP DRILLS. REPAIRED IAW SRM 57-10-00 FIG.71 PAGE 222 VOL 1.

Part: SKIN — CRACKED (LT WING) · airframe 85,026 hrs · 31,613 cycles

LEFT WING FIXED LEADING EDGE UPPER INTERIOR SKIN CRACKED. REPAIRED IAW SRM 57-10-00 FIG 71 PAGE 222 VOL1.

Part: STRUCTURE — CRACKED (L1 DOOR) · airframe 85,026 hrs · 31,613 cycles

L1 DOOR UPPER AFT CORNER HAS DAMAGE. REPAIRED THE L1 DOOR IAW SRM 52-10-00 FIG 12A VOL 1.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 85,026 hrs · 31,613 cycles

RT WING UPPER SKIN AT STRINGER 13, XORS 264, SHOWS CORROSION. REMOVED CORROSION IAW EA 8-5730-T0329998.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 85,026 hrs · 31,613 cycles

RIGHT WING UPPER SURFACE, STRINGER 17, XORS 264, PREVIOUS REPAIR HAS CORROSION. FOUND TO BE OUT OF LIMITS IAW SRM 57-10-00 FIG 59 VOL 1.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 85,026 hrs · 31,613 cycles

RT WING UPPER SURFACE, AT STRINGER 16, XORS 264, 2 FASTENERS SHOW CORROSION. CORROSION REMOVED IAW EA 8-5730-T032-9998.

Part: SKIN — CORRODED (BS 1099-1119) · airframe 85,026 hrs · 31,613 cycles

LOWER FUSELAGE AT BS 1119, RBL 52 SHOWS EVIDENCE OF CORROSION. CUT OUT CORROSION AND REPAIRED IAW SRM 53-20-00 FIG. 6 SHEET 9 PAGE 78 VOL. 1.

Part: SKIN — DELAMINATED (LT WING SPOILER) · airframe 85,026 hrs · 31,613 cycles

LEFT NR 5 SPOILER UPPERR SKIN IS DELAMINATED. REPAIRED IAW SRM 51- 21-02 VOL.II.

Part: SEAT TRACK — WORN (1460) · airframe 85,026 hrs · 31,613 cycles

MAIN DECK SEAT TRACK NEAR BS 1460 LBL 27.50 SHOWS WEAR. REMOVED AND REPLACED THE SECTION OF SEAT TRACK IAW SRM 53-70-00 FIG 1, AND SRM 53-42-01 FIG 4, PAGE 11 VOL 3.

Part: SKIN — DELAMINATED (NR 3 SPOILER LT) · airframe 85,026 hrs · 31,613 cycles

LEFT NR 3 SPOILER UPPER SKIN WAS DELAMINATED. REPAIRED THE SKIN SRM 57-00-01 VOL.I, FIG.4, PG.11.

Part: TEE FITTING — CRACKED (BS 595) · airframe 85,026 hrs · 31,613 cycles

FWD CARGO, BS 595, LONGERON 39L FOUND CRACKED. REMOVED AND REPLACED SECTION OF TEE FITTING BETWEEN LONGERONS 36 AND 40L IAW DWG SR10530064 AND EA 8-5310-T0329315.

Part: TEE FITTING — CRACKED (BS 595) · airframe 85,026 hrs · 31,613 cycles

FWD CARGO RT BS 595 TEE LONGERON 39R FOUND CRACKED. REMOVED AND REPLACED THE TEE IAW DWG SR10530064 AND EA 8-5310-T0329368.

Part: SEAT TRACK — CORRODED (BS 1388) · corrosion level 2 · airframe 85,026 hrs · 31,613 cycles

[MAIN DECK SEAT TRACK BS 1388 RBL 47.50 WORN. REMOVE AND REPLACED THE SEAT TRACK IAW SRM 53-70-00 FIG 1 VOL 1.

Part: ACTUATOR — FAILED (L1 DOOR) · airframe 84,976 hrs · 31,590 cycles

L1 DOOR WILL NOT OPEN ELECTRICALLY. REMOVED AND REPLACED L1 PASSENGER DOOR ELECTRIC ACTUATOR. OPS CHECKED GOOD IAW AMM 52-11-01-2.

Part: SKIN — CRACKED (FUSELAGE) · airframe 84,850 hrs · 31,513 cycles

FOUND SMALL CRACK AT THE UPPER LT CORNER IN THE FUSELAGE JUST ABOVE THE NR 3 PACK BAY DOOR. INSTALLED REPAIR IN REF TO EA 8-5330-T0328078.

Part: UNKNOWN — ODOR · airframe 84,520 hrs · 31,333 cycles

FUME EVENT ON DESCENT PASSING FLIGHT LEVEL 200 WITH ALL PACKS AND BLEEDS ON. ODOR OF MUSTY DIRTY SOCKS. RAN APU. OPERATED PACKS 1, 2, 3 SEPARATELY, THEN OPERATED PACKS TOGETHER ON HOT AND COLD SETTING. TT OF RUNNING PACKS WAS 1 HR. OPEN ALL PACKS BAYS TRY TO ISOLATE ANY SMELLS FROM PACKS. NO HELP, NEEDS MORE TROUBLESHOOTING. REF WRI 21-54-3002 TSI, COMPLIED WITH TSI STEPS 1-4 AS REQUIRED, AFTER COMPLETING TSI STEPS, RAN APU AGAIN WITH PACKS, COULD NOT GET FOUL ODOR FROM PACKS AND VENTS. ALSO RAN ENGINES INDIVIDUALLY, COULD NOT GET FOUL ODOR FROM AIR VENTS AT THIS TIME. ACFT IS OK TO CONTINUE.

Part: COALESCER BAG — DIRTY (AC BAY) · airframe 83,494 hrs · 30,830 cycles

FUMES WHILE DIVERTING, INSPECTION ACCOMPLISHED ON ARRIVAL, CHEM-SPILL ISOLATED TO AAD CONTAINER AT POSITION 2L. NO SEEPAGE TO ACFT NOTED. CONTAINER QUARANTINED FOR EVALUATION. PERFORMED LIQUID CHEM & SPILLAGE MX PRACTICE. R & R ALL THREE PACK COALESCE BAGS, PN 20D10-2. RAN ALL PACKS FOR SEVERAL MINUTES FOR BURN OFF. OK FOR CONTINUED SERVICE.

Part: FIRE WARNING — ACTIVATED (CARGO BAY) · airframe 825 hrs · 30,279 cycles

DURING PREFLIGHT, RECEIVED A FWD CARGO FIRE ALERT & DISCHARGED BOTTLE. R & R NR 1 CARGO FIRE BOTTLE.

Part: BRACKET — CRACKED (LT WING) · airframe 82,179 hrs · 30,088 cycles

LT WING TE BRACKET FOR FLIGHT CONTROL PULLEYS AFT OF PYLON IS CRACKED. REMOVED BRACKET & INSTALLED NEW BRACKET IAW SRM 51-31-01, PN ARB0107-5, MAJOR REPAIR.

Part: SKIN — GOUGED (LT AILERON) · airframe 82,179 hrs · 30,088 cycles

LEFT INBD AILERON LOWER SKIN LE GOUGED. REMOVED OLD LE SKIN PANEL, RECEIVED NEW FABRICATED SKIN PANEL T14 1100803, LOCATED, DRILLED, INSTALLED & TREATED, PRIMED & TOP COATED IAW SRM 51-31-01 & 51-21-01. COMPLIED WITH EA 8-5750-TO313143 REV NO POS P1 WINGS FLIGHT SURFACES LT LOWER LE SKIN REPLACEMENT RSC TRACKING ONLY MAJOR REPAIR.

Part: PANEL — CRACKED (RT PYLON) · airframe 82,179 hrs · 30,088 cycles

RIGHT PYLON PANEL 457BT CRACKED AS MARKED. PANEL RACK WELDED ON T14 1102142 IAW EA 8-5480-T0312625 REV NO PS P 1. NACELLES & PYLON FILLETS FAIRINGS RT PYLON PANEL 457BT CRACKED. MINOR REPAIR.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 82,179 hrs · 30,088 cycles

AFT CARGO FLOORBEAM UPPER CHORD AT STATION 1902 STRINGER 43R HAS HEAVY CORROSION ON LOWER SURFACE. REMOVED DAMAGE, ORIGINAL MATERIAL .063, MATERIAL REMOVED .050 & REMAINING MATERIAL .013 IAW SRM 53-00-01. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01 FIG 1B. INSTALLED FILLER & ANGLE REPAIR IAW SRM 53-00-01 PAGE 29 FIG 28 & SRM 51-31-01. MAJOR REPAIR.

Part: ATTACH BRACKET — CRACKED (NR 3 ENGINE) · airframe 82,179 hrs · 30,088 cycles

NUMBER 3 ENG FAN ACCESSORY INBD SIDE HYD PUMP HOSE LINE ATTACHED BRACKET CRACKED. REMOVED & INSTALLED ATTACHED BRACKET IAW SRM 51-31-01. WELDED ON T14 1103378 IAW EA 8-7210-T0312736 REV NO PS P1 TITLE ENG REDUCTION GEAR & SHAFT NR 3 ENG HYD PUMP. IN REPAIR.

Part: FRAME SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 82,179 hrs · 30,088 cycles

CENTER CARGO COMPARTMENT BILGE AT STATION 1781 BETWEEN LONGERON 48L - 49L LOWER FRAME SPLICE HAS CORROSION. R & R SPLICE STRAP, FABRICATED ON T14 1101840 IAW SRM 51-31-01 & REPAIRED LOWER FRAME CHANNEL STATION 1781 IAW SRM 53-30-00 FIG 5 & INSTALLED IAW SRM 51-31-01. MINOR REPAIR.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 82,179 hrs · 30,088 cycles

AFT CARGO FLOORBEAM UPPER CHORD AT STATION 1902, STRINGER 43R HAS HEAVY CORROSION ON LOWER SURFACE. INSTALLED FILLER & ANGLE REPAIR AT AFT CARGO FLOORBEAM 43R IAW SRM 53-00-01 PAGE 29 FIG 28 & SRM 51-31-01. FLOORBEAM IS OUT OF LIMITS IAW SRM 53-00-01 FIG 1B PAGE 12. MAJOR REPAIR.

Part: SEAT TRACK — MECHANIC ERROR (FUSELAGE) · airframe 82,179 hrs · 30,088 cycles

AFT PIT LT SEAT TRACK HAS DOUBLE DRILLED HOLE BETWEEN STATION 1821 & 1801. REMOVED DAMAGE OF DOUBLE DRILLED HOLES IAW SRM 51-21-04. FABRICATED FILLER & STRAP IAW SRM 53-70-00 FIG 1B ITEM 2. INSTALLED FASTENERS TO FILLER & DOUBLER IAW SRM 51-31-01. MAJOR REPAIR.

Part: ROLLER TRAY — CORRODED (CARGO BAY) · corrosion level 2 · airframe 82,179 hrs · 30,088 cycles

CENTER CARGO COMPARTMENT BETWEEN STATION 1641 - 1661, RT SIDE ROLLER TRAY SEVERAL AREAS HAVE CORROSION & DEFORMED, RBL 54. REPAIRED CTR CARGO COMPARTMENT ROLLER TRAY BETWEEN 1621 - 1661, RBL 54 IAW SRM 53-70-00 FIG 7. MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 82,179 hrs · 30,088 cycles

LOWER FWD CARGO COMPARTMENT STATION 979 BL 0 FLOOR SUPPORT HAS CORROSION. REPAIRED FLOOR SUPPORT AT STATION 979 LBL 9.5 - RBL 8.5 IAW SRM 53-60-01 FIG 3. MAJOR REPAIR.

Part: CARGO TRACK — DAMAGED (BS 1801-1821) · airframe 82,179 hrs · 30,088 cycles

AFT PIT LT SEAT TRACK HAS DOUBLE DRILLED HOLE BETWEEN STATION 1821 & 1801. REMOVED DAMAGE OF DOUBLE DRILLED HOLES IAW SRM 51-21-04. FABRICATED FILLER & STRAP IAW SRM 53-70-00 ITEM 2. INSTALLED SEAT TRACK & FASTENERS TO FILLER & DOUBLER IAW SRM 51-31-01.

Part: FLOOR SUPPORT — CORRODED (BS 979) · airframe 82,179 hrs · 30,088 cycles

LOWER FWD CARGO BAY BS 979 BL 0 FLOOR SUPPORT HAS CORROSION. REPAIRED FLOOR SUPPORT IAW SRM 53-60-01 FIG 3.

Part: SUPPORT CHANNEL — CRACKED (FUSELAGE) · airframe 82,179 hrs · 30,088 cycles

AFT PIT COMPARTMENT FWD BULKHEAD LT SEAT TRACK FWD ATTACH CHANNEL HAS CRACK ON BOTH ENDS. R & R FLOOR SUPPORT IAW SRM 51-31-01. FABRICATED FLOOR SUPPORT UNDER T14 1100289 FROM STATION 1786 LBL 20 - LBL 40.

Part: CARGO TRACK — CRACKED (AFT CARGO BAY) · airframe 82,179 hrs · 30,088 cycles

AFT CARGO BAY FWD BULKHEAD LT SEAT TRACK FWD ATTACH CHANNEL HAS CRACK ON BOTH ENDS. R & R SEAT TRACK IAW 51-31-01.

Part: RIB — CRACKED (RT WING) · airframe 82,179 hrs · 30,088 cycles

RIGHT WING FIXED LE UPPER CHAMBER LOWER SKIN, RIB SUPPORT ABOVE PULLEY HAS A CRACK. R & R SPLICE PLATE, FORMER ON RT WING FIXED LE. FABRICATED FROM 7075-T6 .071 INCHES BATCH NR 2689862 IAW SRM 51-31-01 & DWG NRB1249-12. MAJOR REPAIR.

Part: CHANNEL — CORRODED (BS 1641-1661) · airframe 82,179 hrs · 30,088 cycles

CENTER CARGO BAY BETWEEN BS 1641 - 1661 RT SIDE ROLLER TRAY HAD SEVERAL AREAS CORROSION & DEFORMED. REPAIRED IAW SRM 53-70-00 FIG 7.

Part: SKIN — DAMAGED (LT AILERON) · airframe 82,179 hrs · 30,088 cycles

LEFT INBD AILERON LOWER SKIN HAS DENT 6 INCHES LONG, 32 INCHES FROM INBD END, NEAR THE TE. EVALUATED DENT .070 INCHES DEEP, OUT OF LIMITS IAW SRM 51-80-02 VOL II FIG 1. VERIFIED MAT ID IS 2024-T3 .020 INCHES SKIN & .012 INCHES DOUBLER. FABRICATED REPAIR DOUBLER FROM 2024-T3 .040 INCHES IAW SRM 57-10-00 FIG 85. LOCATED, DRILLED, TREATED & PRIMED IAW SRM 51-80-01 SRM 57-51-01 FIG 1 PG 2 & SRM 51-21-01. INSTALLED REPAIR DOUBLER IAW SRM 57-10-00 FIG 85. WEIGHT & BALANCE NOT REQUIRED ON INBD AILERON IAW SRM 57-00-00 VII.

Part: CARGO TRACK — DAMAGED (UPPER CARGO) · airframe 82,179 hrs · 30,088 cycles

UPPER DECK CARGO TRACK LBL 8 BS 1248 HAS ONE WORN LOBE. BLENDED DAMAGE IAW SRM 53-70-00 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-70-00 FIG 5 SHT 1. REMOVED AND REPLACED THE CARGO TRACK IAW SRM 53-70-00.

Part: FIRE WARNING — FALSE ACTIVATION (CARGO) · airframe 79,948 hrs · 28,898 cycles

RECEIVED "CARGO FIRE LWR FWD" & "DISCH CARGO AGENT" MESSAGES. MANUAL CARGO FIRE TEST & RESETTING CARGO SMOKE DETECTOR & LIGHTS CIRCUIT BREAKER. DID NOT EXTINGUISH FWD 1 AGENT DISCHARGE SWITCH WAS PRESSED, RESULTING IN LOW LIGHTS FOR FWD1 & AFT1. FIREX R & R FIRE EX CONTAINER 1 REF AMM 26-22-01-4 THRU STEP 3.B.(3)(K).AWAITING AVIONICS CHECKS FOR CLOSEOUT.

Part: PUMP — LEAKING (HYD SYSTEM) · airframe 79,882 hrs · 28,862 cycles

LEAK IN HYDRAULIC SYS NR 3. HYD SYS SELECTED TO MANUAL AND NR 3 HYD PUMP SELECTED OFF AT ABOUT 4.0 INDICATION. SYS QTY CONTINUED TO DROP. AT BLOCK IN NR 3 HYD SYS IS AT 0.2. NO VISUAL LEAKS NOTED. FOUND NR 3 ENGINE LT HYD PUMP LEAKING AT CASE DRAIN LINE. R & R BOTH LT & RT ENGINE DRIVEN PUMPS REF MM 29-11-01-2, NR 3 HYD SYS SERVICED TO FULL REF MM 12-13-02-3. OPS & LEAK CHECKED NORMAL, OK FOR SERVICE.

Part: PUMP — LEAKING (HYD SYSTEM) · airframe 79,879 hrs · 28,861 cycles

LEAK IN HYD SYSTEM NR 3. HYD SYS SELECTED TO MANUAL AND NR 3 HYD PUMP SELECTED OFF AT ABOUT 4.0 INDICATION. SYS QTY CONTINUED TO DROP AT BLOCK IN NR 3 HYD SYS IS AT 0.2. FOUND NR 3 ENGINE LEFT HYDRAULIC PUMP LEAKING AT CASE DRAIN LINE. REMOVED & REPLACED BOTH LEFT & RIGHT ENGINE DRIVEN PUMPS REF MM 29-11-01-2.

Part: SKIN — DAMAGED (BS 695-715) · airframe 79,312 hrs · 28,540 cycles

LIGHTNING STRIKE ON EXTERNAL FUSELAGE SKIN BS 695 -715, LONGERONS 46 - 47L. REPAIRED IAW SRM 53-20-00, FIG 13. MAJOR REPAIR.

Part: SEAT TRACK — DAMAGED (BS 1381) · airframe 79,312 hrs · 28,540 cycles

MAIN DECK SEAT TRACK AT STA 1381, LBL 75 HAS BROKEN SCALLOP. EVALUATED BROKEN SCALLOP, FOUND TO BE OUT OF LIMITS IAW SRM 53-70-00, FIG 5, VOL I, CUT OUT DAMAGE SECTION OF SEAT TRACK IAW SRM 53-70-00, FABRICATED SEAT TRACK, TWO SPLICES, & TWO SPLICE PLATES IAW SRM 53-70-00. LOCATED AND DRILLED REPAIR PARTS IAW SRM 51-31-01 VOL II, AND INSTALLED REPAIR PARTS IAW SRM 53-70-00, FIG 1 VOL I, REPAIR CLASSIFED AS MAJOR.

Part: FUEL CELL — CONTAMINATED (NR 2) · airframe 79,177 hrs · 28,462 cycles

DEBRIS REMOVED FROM NR2 TANK DURING MX. NEED FFC TO INSPECT NR 2 TANK FOR FURTHER DEBRIS. ALSO NEED TO INSPECT PLUMBING FOR 2L AFT PUMP INLET AND PUMP MANIFOLD FOR DEBRIS DUE TO HISTORY. BASKET ASSY CRACKED AND DEFORMED FROM COMPACTED DEBRIS. R & R PICK UP SCREEN AT NR 2 AFT PUMP (LEFT). REMOVED, CLEANED, REINSTALLED NR 2 AFT PICKUP SCREEN (RIGHT). VISUAL INSPECTION FOR FOD PERFORMED. NR 2 LT AND NR 2 RT CLEARED. ALL OTHER AREAS CLEAR. REF AMM 28-00-00-2, PG 11, 12. REF AMM 28-22-01-2.

Part: MOTOR — CRACKED (STAB TRIM) · airframe 79,124 hrs · 28,431 cycles

LEVEL 2 HYD 3 FAIL. R & R INBD STABILIZER TRIM MOTOR IAW AMM 27-43-01-2, OPS AND LEAK CHECKED GOOD, OK FOR SERVICE.

Part: FUSE — FAILED (MLG) · airframe 78,160 hrs · 27,931 cycles

AFTER TAKEOFF GEAR HANDLE WOULD NOT MOVE TO UP POSITION. FOLLOWED QRH, GEAR HANDLE WOULD STILL NOT MOVE TO UP POSITION. REMOVED AND REPLACED MLG TRIM INTERLOCK HYDRAULIC FUSE IAW MD10-10 32-31-06-2. OK FOR SERVICE.

Part: CONNECTOR — INOPERATIVE (TRANSFER PUMP) · airframe 77,911 hrs · 27,798 cycles

TANK 2 RAFT PUMP INOPERATIVE. RELEASED FOR SERVICE IAW MEL: 28-22-01-02-A. REMOVED PUMP AND FOUND ELECTRICAL CONNECTOR R5-1103 BURNED AND PINS BURNED OFF THE PUMP. REMOVED NR 2 RT/AFT BOOST PUMP HARNESS, BOOST PUMP AND CAP. OPS CHECKED GOOD, LEAK CHECKED GOOD, NOTE: A SCREW WAS FOUND LODGED IN THE IMPELLER.

Part: LANDING GEAR — MALFUNCTIONED · airframe 77,670 hrs · 27,678 cycles

GEAR HANDLE WOULD NOT COME UP AFTER T/O , TRIED OVERRIDE SWITCH NO JOY. RAN QRH CAME BACK AND LANDED CHECKED BOTH TRIM CYLINDERS FOR LEAKAGE NO EXTERNAL LEAKS NOTED, PINNED GEAR AND RAISED GEAR HANDLE WHILE WATCHING TRIM INTERLOCK CYLIDER , GEAR HANDLE GOES TO THE UP POSITION WHILE HOLDING OVERIDE BUTTON. PERF BITE ON PSEU NO CURRENT OR LAST FLT FAULTS LOGGED, ALL WORK IAW AMM 32-10-00-5 . BLED LT & RT MLG TRIM CYLINDERS AND RESET AND SAFETIED INTERLOCK FUSE REF AMM 32-37-01-2. DISCONNECTED NLG TEE LINKS REF AMM 32-21-02-02 AND CHECKED MLG CONTROL MECHANISM INTERLOCK REF AMM 32-31-02-2. INTERLOCK OPS NORMAL WITH ACFT IN FLT MODE. RECONNECTED NOSE GEAR TEE LINKS REF AMM 32-21-02-2. RETRACTED GEAR SEVERAL TIMES WITH NO PROBLEMS, PER 32-30-00-5.

Part: FIRE DETECTOR — FALSE ACTIVATION (NR 1 NACELLE) · airframe 76,901 hrs · 27,275 cycles

AFTER STARTING ALL 3 ENGINES AND BLOCKING OUT, POWER WAS APPLIED FOR TAXI NR 1 ENGINE INDICATED MOMENTARY FIRE. ENGINE SHUTDOWN AND ALL INDICATIONS RETURNS TO NORMAL. OPS CHECK NR 1 ENG AT GATE CHECKED GOOD, NR 1 B-LOOP, OPS CHECK NORMAL IAW MEL-26-11-01-01 ACFT OK FOR SERVICE.

Part: HINGE FITTING — CRACKED (LT WING TE FLAP) · airframe 76,667 hrs · 27,151 cycles

FOUND 2 EA. CRACKS EMANATING FROM FASTENER HOLES ON THE LT WING, OUTBOARD FLAP, INBOUND FORWARD FLAP TO WING FITTING (MARKED) HFEC INSPECTION VERIFIED INDICATION OF CRACK. REMOVED CRACKED OB FLAP IB HINGE WING FITTINGS 2EA. ARB2431 TRANSFERED HOLES TO NEW SERVICABLE FITTINGS PER NRB6013 INSTALLED FITTINGS 2EA. PER B/P NRB6013 AND SRM 51-33-01

Part: HINGE FITTING — CRACKED (LT WING TE FLAP) · airframe 76,667 hrs · 27,151 cycles

FOUND 1 EA CRACK EMANATING FROM FASTENER HOLE ON THE LT WING, OTBD FLAP, INBD FWD FLAP TO WING FITTING. HFEC INSP VERIFIED INDICATION OF CRACK. REMOVED CRACKED LT OB FLAP IB HINGE WING FITTING ARB2431 TRANSFERED HOLES TO NEW SERVICABLE FITTINGS PER NRB6013 INSTALLED FITTING. PER B/P NRB6013 AND SRM 51-33-01

Part: HINGE FITTING — CRACKED (RT WING TE FLAP) · airframe 76,667 hrs · 27,151 cycles

RIGHT WING, OUTBOARD FLAP.INBD HINGE, WING TO FLAP HINGE FITTING IS CRACKED.(MARKED) REMOVED CRACKED RT OB FLAP IB HINGE WING FITTINGS 2EA. ARB2431 TRANSFERED HOLES TO NEW SERVICABLE FITTINGS PER NRB6013 INSTALLED FITTINGS 2EA. PER B/P NRB6013 AND SRM 51-33-01

Part: FAN — FAILED (CABIN) · airframe 74,830 hrs · 26,240 cycles

ABOUT 1 HOUR INTO FLIGHT AT FL340, NOTICED A BURNING ELECTRICAL ODOR ALONG WITH VISIBLE "HAZEY" SMOKE IN COCKPIT. COMPLIED WITH QRH. AFTER SECURING PACKS AND CABIN BUSS SWITCH, SMOKE AND ODOR SEEMED TO SUBSIDE. BURNING ODOR WAS DEFINITELY ELECTRICAL. REMOVED AND REPLACED AVIONICS RACK COOLING FAN CONTROL RELAY R2-5895 OPS CHECK OF NR 1PACK FAN NORMAL PER 21-26-02. AS PER CONFERENCE CALL WITH MOCC, RAN ALL 3 ENGINES WITH PACKS 1,2, AND 3 RUNNING USING ENGINE AIR. ALSO, HAD ENGINE GENERATORS POWERING ACFT. NO NOTICEABLE ODORS IN COCKPIT. RAN ENGINES AS PER JRH.

Part: UPLOCK SENSOR — MALFUNCTIONED (LT MLG) · airframe 72,600 hrs · 25,206 cycles

AFTER LEVEL OFF, THE LT MAIN GEAR LIGHT INDICATED RED. AS A PRECAUTIONARY MEASURE, SLOWED TO 230KTS FOR REMAINDER OF FLIGHT. DID ATTEMPT ONE RECYCLE OF GEAR HANDLE WHICH DID NOT CHANGE STATUS WITH GEAR HANDLE UP. STATUS PAGE SHOWED "PSEU FAULT". REMOVED LT MLG PROX UP AND LATCHED SENSOR B (D1-81) PER MD10 AMM 32-61-15-4.

Part: BLOCKER DOOR — DAMAGED (THRUST REVERSER) · airframe 71,398 hrs · 24,641 cycles

NR 2 REVERSER WOULD NOT STOW AFTER LANDING. FOUND NR 2 LT REV TRANSLATING COWL MISSING. AFW MX REPORTS AIRCRAFT BLOCKED IN WITH LT THRUST REVERSER TRANSLATING COWL MISSING. IT APPEARS THERE ARE ALSO BLOCKER DOORS THAT WERE TOWN OFF WITH THE COWL. THIS MOST LIKELY HAPPENED ON LANDING AND TR DEPLOYMENT. THE AIRPORT AUTHORITY FOUND TRANS COWL AND ATTACHING PARTS ON RUNWAY. ALL DEBRIS REMOVED. INITIAL EVALUATION LOOKS LIKE THE AIRCRAFT WILL REQUIRE A TR HALF. REPLACED NR 2 LT THRUST REVERSER. NR 2 THRUST REV, OPS CKS NORMAL.

Part: SPOOL — CRACKED (CARGO DOOR) · airframe 71,172 hrs · 24,527 cycles

MAIN CARGO DOOR NR 3 SPOOL FITTING HAS CRACK INDICATIONS. NR 3 SPOOL FITTING HAS CRACK INDICATIONS ON FWD INBD HOLE. REAMED HOLE TO .453 IAW DC/MD10 SRM 53-50-01 FIG 17, VOL 1. PERFORMED BHEC IAW NDT SPM 06-10-01.003. NO CRACKS NOTED. DOOR TO BE RIGGED ON FEDEX, N/R N00712.

Part: FLOORBEAM — CORRODED (BS 1841) · airframe 71,172 hrs · 24,527 cycles

AFT PIT TOP OF FLOORBEAM CORRODED AT STA 1841 RBL 17 TO 23. REMOVED AND REPLACED FLOORBEAM AGA3874-3, AND AFT ATTACHED ANGLE AGA3874-9 IAW DAC DWG AGA3874 REV B, AND MD/DC10 SRM 51-33-01 PG 1 VOL 11. MD/DC10 RSM 51-35-01 PG 1 VOL 11.

Part: FITTING — CRACKED (CARGO DOOR) · airframe 71,172 hrs · 24,527 cycles

MAIN CARGO DOOR NR 7 SPOOL FITTING HAS CRACK INDICATION. REMOVED NR 7 SPOOL FITTING (BACK OF FITTING) IAW DC/MD10 SRM 51-33-01 VOL 11, PG 47. LOCATED AND DRILLED NEW FITTING IAW DAC DWG AFA7132 REV B. INSTALLED NEW FITTING IAW DC/MD10 SRM 51-33-01 VOL11 PG 34. SPOOL FITTING TO BE RIGGED ON N/R N00712.

Part: BRACKET — CRACKED (NR 2 ENGINE) · airframe 71,172 hrs · 24,527 cycles

NR 2 ENG RT LOWER FORWARD FLANGE SHIP STAND ATTACHED POINT CRACK PAST STOP DRILL BOTH SIDES OF FLANGE. REMOVED GROUND HANDLING BRACKET IAW MD/DC 10 SRM 51-33-01 VOL 11. WELDED CRACK IN NR 2 ENG RT LOWER FORWARD FLANGE SHIP STAND IAW GE COMMERCIAL ENGINE STANDARD PRACTICE MANUAL 72-23-01 REPAIR 1 STEP 1-4. REINSTALLED BRACKET IAW MD/DC 10 SRM 51-33-01 VOL 11.

Part: FITTING — CRACKED (CARGO DOOR) · airframe 71,172 hrs · 24,527 cycles

MAIN CARGO DOOR NR 6 SPOOL FITTING HAS CRACK INDICATION. REMOVED SPOOL FITTING IAW MD/DC10 SRM 51-33-01 VOL11 PR=G,47. BHEC WAS PERFORMED IAW NDTSPM 06-10-01. ON NR 6 LOWER JAMB WEB HOLES. NO CRACKS FOUND. LOCATED AND DRILLED NEW FITTING IAW DAC DWG AFA7132 REV B. INSTALLED NEW SPOOL FITTING IAW MD/DC10 SRM 51-33-01 VOL 11 PG, 34 PARAG 6.

Part: SEAT TRACK — DAMAGED (BS 1086-1095) · airframe 71,172 hrs · 24,527 cycles

UPPER CARGO DOOR COMPARTMENT SEAT TRACK SCALLOPS DAMAGED BETWEEN STA 1086 AND STA 1095, RBL 48. REMOVED DAMAGED SEAT TRACK IAW DC/MD10-10 SRM 51-31-01 VOL 11 PG 1. FAB`D NEW SEAT TRACK IAW DC/MD10-10 SRM 53-70-00 VOL 1 AND DWG SP10S10179 REV`D, ALODINED AND PRIMED NEW SEAT TRACK IAW DC/MD10-10 SRM 51-21-01 VOL2 PG 2. INSTALLED NEW SEAT TRACK IAW DC/MD10-10 SRM 53-70-00 VOL 1 AND DWGSP10S10179 REV D.

Part: SEAT TRACK — CRACKED (BS 1079-1089) · airframe 71,172 hrs · 24,527 cycles

MAIN CABIN COMPT SEAT TRACK AT STA 1079, RBL 27.5 IS CRACK. REMOVED DAMAGED SECTION OF SEAT TRACK AND SPLICED IAW DC10/MD10 SRM 53-70-00. FAB`D NEW EXTRUSION IAW DRG ADA8019 REV J. INSTALLED EXTRUSION IAW DC10/MD10 SRM 51-33-01 VOL. 11. ALODINED AND PRIMED IAW DC10 SRM 51-21-01 VOL11. INSTALLED REMOVED FLOOR PANELS IAW DC10 SRM 51-31-01 VOL 11.

Part: SKIN — DENTED (RT WING) · airframe 71,172 hrs · 24,527 cycles

RT WING O/B FLAP O/B END LOWER SKIN DENTED, JUST I/B OF EXISTING REPAIR. REMOVED DAMAGED DOUBLER IAW MD10/DC10 SRM 51-31-01 VOL11 MAT ID FOR REPAIR DOUBLER 2024-T3 0.040 IAW DC10/MD10 SRM 57-52-01 VOL 111. PO NR 557785.5 AND PO NR 541694.2. FAB`D PARTS IAW MD10/DC10-10 SRM 57-10-00. ALODINED AND PRIMED PARTS IAW MD10/DC10-10 SRM 51-21-01 VOL 11. INSTALLED REPAIR IAW MD10/DC10-10 SRM 57-10-00 VOL 1.

Part: SEAT TRACK — DAMAGED (BS 908-949) · airframe 71,172 hrs · 24,527 cycles

FOUND UPPER FUSELAGE CABIN SEAT TRACK AT LBL 47 STA 910 GOUGED. REMOVED DAMAGED SEAT TRACK SECTION AND INSTALLED NEW SEAT TRACK SECTION FROM STA 908 TO STA 949, LBL 47 IAW DC10/MD10 SRM 53-70-00 FIG 1 VOL 1, AND D RW SP10510179 REV D ZONE F-8.

Part: FITTING — CRACKED (CARGO DOOR) · airframe 71,172 hrs · 24,527 cycles

FOUND MAIN CARGO DOOR NR 7 SPOOL FITTING HAS CRACK INDICATION.

Part: FITTING — CRACKED (CARGO DOOR) · airframe 71,172 hrs · 24,527 cycles

FOUND MAIN CARGO DOOR NR 2 SPOOL FITTING HAS CRACK INDICATION. REMOVED AND REPLACED FITTING IAW DC/MD10 SRM 51-33-01 VOL.II,DAC AFA 7132 REV J. MAJOR REPAIR.

Part: FITTING — CRACKED (CARGO DOOR) · airframe 71,172 hrs · 24,527 cycles

FOUND MAIN CARGO DOOR NR 3 SPOOL FITTING HAS CRACK INDICATION.

Part: FITTING — CRACKED (CARGO DOOR) · airframe 71,172 hrs · 24,527 cycles

FOUND MAIN CARGO DOOR NR 6 SPOOL FITTING HAS CRACK INDICATION.

Part: FITTING — CRACKED (CARGO DOOR) · airframe 71,172 hrs · 24,527 cycles

FOUND MAIN CARGO DOOR NR 1 SPOOL FITTING HAS CRACK INDICATION. REMOVED SPOOL FITTING IAW DC10/MD10 SRM 51-33-01 VOL 2 DRILLED UP NEW FITTING IAW DAC DWG AFA 7132 REV J INSTALLED FITTING IAW DC10/MD10 SRM 51-33-01 VOL 2 DOOR TO BE RIGGED ON FEDEX N/R N00712.

Part: CASE — SPLIT (TURBINE) · airframe 65,364 hrs · 21,935 cycles

DURING TO AT 300 FT, NR 3 EGT "X'ED" OUT. EAD SHOWED ENG NR 3 EXCEEDANCE. EGT X WENT AWAY AND SHOWED NORMAL EGT. EGT THEN SPIKED INTO THE RED SHOWING 1027 EGT. THROTTLE WAS RETARDED AND ALL INDICATIONS (N1, EGT, N2, AND FUEL FLOW) WERE NORMAL, NO OTHER INDICATIONS WERE ABNORMAL. RETURNED FOR LANDING. FOUND OPEN FROM PIN A LT SIDE JUNCTION AND PIN A OF RT SIDE JUNCTION, ALSO FOUND CRACKED HARDLINE AT BOTTOM OF ENGINE. FOUND LOWER TURBINE CASE SPLIT LINE STUD BROKEN AT THE SIX O`CLOCK POSITION. HARNESS IS ON THE ENG BUT NOT COMPLETELY INSTALLED. REPLACED BROKEN STUD, AND RESECURED THE AFT THERMOCOUPLE. RAN NR 3 ENGINE TO OPS CHECK NR 3 EGT SYSTEM. CHECKS NORMAL,

Part: VALVE — FAILED (ANTI-SKID SYS) · airframe 63,948 hrs · 21,217 cycles

WHEN LOWERING THE GEAR FOR LANDING GEAR WAS DOWN AND LOCKED. WE HAD ANTI-SKID FAIL WARNING ON CONFIG PAGE. WENT AROUND RECYCLED GEAR DID NOT GET THE WARNING THE SECOND TIME. ALSO TRIED RECYCLING ANTI SKID SWITCH WITH GEAR DOWN DID NOT PUT THE WARNING LIGHT OUT. REMOVED AND REPLACED UPPER (C) ANTI-SKID VALVE ON LT MLG IAW AMM. OPS CHECK IAW 32-45-00-2 PARA 2A/B. AIRCRAFT OK FOR CONTINUED SERVICE.

Part: FLAP TRACK — DAMAGED (TE FLAP VANE) · airframe 63,601 hrs · 21,038 cycles

EXCESSIVE LT WING DOWN INPUT REQUIRED TO HOLD LEVEL FLIGHT ON APPROACH AFTER FLAPS 50 SELECTED. AIRCRAFT WOULD ROLL AGGRESSIVELY TO RT IF PILOT RELEASE PRESSURE ON YOKE. WINDS 110 AT 4KTS LANDING 16L AT AFW. DIRECTIONAL CONTROL WAS POSSIBLE BUT CREW ALSO NOTED LEVEL 3 STAB TRIM ALERT AFTER LANDING AND 11.1 ANU UNITS BOXED AMBER. STAB RAN W/O CREW INPUT AT TOUCHDOWN. *S/D* REMOVED AND REPLACED ALL THREE FLAP VANE TRACK ASSY AND REINSTALLED INBOARD FLAP VANE TO INBOARD FLAP, REMOVED AND REPLACED INBOARD FLAP SPRING CARTRIDGE AND ADJUSTED VANE PER MM 27-50-03-2.