N254FE

Part: DOOR FRAME — CRACKED (ZONE 200) · airframe 58,500 hrs · 37,443 cycles

LT AFT SERVICE DOOR FWD UPPER CAM ROLLER FRAME HAS A CRACK. REMOVED AND REPLACED FWD FRAME IAW SRM 51-30-2.

Part: SKIN — DENTED (ZONE 100) · airframe 58,500 hrs · 37,443 cycles

EXT FUSELAGE SKIN DENT APPROX STA 1153 BETWEEN S-17L - S-19L, REPAIRED IAW SRM 53-30-3.

Part: WEB — CRACKED (ZONE 200) · airframe 58,500 hrs · 37,443 cycles

CABIN FS 1183 BULKHEAD LT OB FLOOR WEB HAS CRACKS. REMOVED AND REPLACED FLOOR WEB IAW SRM 51-30-2. FABRICATED NEW FLOOR WEB .020 ON TRAVELER T7/1695713 IAW SRM 51-30-6 TABLE 1.

Part: WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 58,500 hrs · 37,443 cycles

FWD CARGO COMPT BETWEEN BS 580-600 S28R OUTER WEB LOWER ANGLE HAS SURFACE CORROSION. REMOVED AND REPLACED WEB IAW SRM 51-30-2. FABRICATED WEB ON TRAVELER T7/695113.

Part: SUPPORT — CRACKED (ZONE 500) · airframe 58,500 hrs · 37,443 cycles

LT WING AT T/E REAR SPAR AREA APROX RS STA 383 UPPER FIXED PANEL LOWER C CHANNEL BRACKET MOUNT SUPPORT HAS A CRACK AT FWD SECTION ABOVE NR 3 TRANS ASSY. REMOVED AND REPLACED C CHANNEL SUPPORT IAW SRM 51-30-2. C CHANNEL SUPPORT, FABRICATED ON TRAVELER NR T7/693316.

Part: SKIN — CRACKED (LT MLG DOOR) · airframe 58,500 hrs · 37,443 cycles

LT MLG FLYING DOOR UPPER MID INNER SKIN EDGE CRACKED REPAIRED IAW SRM 51-40-2.

Part: PANEL — CORRODED (ZONE 600) · corrosion level 2 · airframe 58,500 hrs · 37,443 cycles

RT WING T/E LOWER HINGE PANEL 8506R INNER SURFACE HAS CORROSION AROUND EDGE REPAIRED IAW SRM 51-20-151-7.

Part: RIB — CRACKED (ZONE 600) · airframe 58,500 hrs · 37,443 cycles

RT WING L/E SLAT NR 5 INBD END PORK CHOP SEAL MOUNTING PLATE DEFORMED AND CRACKED. REMOVED CRACKED RIB, FABBED NEW RIB ON TRAVLER T/682663. INSTALLED NEW RIB.

Part: VALVE — LEAKING (NR 1 ENGINE) · airframe 57,871 hrs · 36,916 cycles

NR 1 ENG FAILED DURING FLIGHT. 1ST INDICATION WAS EXCESSIVE NR 1 FUEL FLOW AND 2 KNOB DIFF BETWEEN NR 1 THRUST LEVER AND NR 2/3. JUST PRIOR TO FAILURE, NR 1 EPR 1.6 (2/3 EPRS 1.8). NR 1 N1 80 NR 2/3 N1S 85) N2 86 (NR 2/3 N2S 88/90) NR 1 FF 4000 (2/3 3400). APPROX 30 MI NORTH OF MEM NR 1 CSD FELL OFFLINE AND ENG FAILED. ENG WAS SHUTDOWN IN ACCORDANCE W/QRH. REMOVED AND REPLACED ORIGINAL P&D VALVE WITH NEW O-RINGS AND REPLACED MISSING FARRULE PER PWA ENG MANUAL 73-12-01-450-002 IDLE LEAK CKS OK. ACCOMPLISHED HIGH POWER RUN PER JRH, ALL ENGINE PARAMETERS NORMAL , NO LEAKS NOTED , A/C OK FOR SERVICE.

Part: INDICATOR — INOPERATIVE (COCKPIT) · airframe 56,858 hrs · 36,127 cycles

CAPTAINS AIRSPEED INDICATOR DID NOT INDICATE AIRSPEED ON T/O. ACN RELEASED FOR SERVICE PER MEL/CDL: 20-01 CATEGORY: X RVSM ITEM "MEL 20-01: DO NOT OPERATE AIRCRAFT WITHIN RVSM AIRSPACE." "NO RVSM OPERATIONS". R/R CADC PER M/M 34-12-011-4, OPS CHECK GOOD. DEF. RVSM ON A/C PER MEL 20-01 CONT NR 248485, NO EXP. NOTE: NO RVSM CADC INSTALLED (NIS) PER M.O.C.C. PREMATURE REMOVAL/INSTALLATION OFF MFG 9B-81020-1 POS 1 SRL 40851 TAG 6A8103 ON MFG HG480B13 SRL 91032048 TAG 830290.

Part: CONNECTOR — DIRTY (CARGO DOOR) · airframe 56,630 hrs · 35,921 cycles

ON T/O MCD A LIGHTS ON FWD ILLUM. FOLLOWED QRH RED TABS AND RETURNED TO AFW. A LIGHT WENT OUT ON FINAL. MAIN CARGO DOOR WARNING LIGHT SYSTEM (A OR B) INOP. VERIFY DOOR CLOSED AND LOCKED PRIOR TO EACH BLOCK OUT. CLEANED CONNECTOR ON SYS-A MICROSWITCH PER SMP AND RAN DOOR THROUGH SEVERAL CYCLES. OPS CHECK SATISFACTORY IAW NASI SYSTEM DOOR MANUAL FXV-727-MM14. OK FOR SERVICE.

Part: SKIN PANEL — GOUGED (FUSELAGE) · airframe 56,586 hrs · 35,881 cycles

COMPLY WITH EA 7-5330-55484 FUSELAGE, PLATES AND SKIN GOUGE REPAIR AT BS 950E, STR 19R. COMPLIED WITH EA 7-5330-55484 FUSELAGE, PLATES AND SKIN GOUGE REPAIR AT BS 950E, STR 19R. THIS IS A MAJOR REPAIR.

Part: INSULATION — DAMAGED (CABIN) · airframe 56,586 hrs · 35,881 cycles

EQUIPMENT AND FURNISHINGS INSULATION BLANKETS. PARTIAL REPLACEMENT STA 360-1183, MAIN CABIN COMPARTMENT. COMPLIED WITH EA 7-2580-81692.

Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 56,586 hrs · 35,881 cycles

FLOORBEAM LBL 7-RBL 40 UPPER CHORD REQUIRES MAJOR REPAIR. REMOVED AND REPLACED UPPER T-CHORD IAW SRZ 53-034E REPAIR NR 7.

Part: FAIRING — CRACKED (T/E FLAP) · airframe 56,586 hrs · 35,881 cycles

LT WING LOWER T/E FLAP TRACK SKATE FAIRING BEHIND MLG STRUT IS CRACKED. REMOVED AND REPLACED SKATE FAIRING IAW SRM 51-30-2.

Part: RETAINER — CORRODED (NLG DOOR) · corrosion level 2 · airframe 56,586 hrs · 35,881 cycles

LT NOSE GEAR AFT DOOR SEAL RETAINER CORRODED. REMOVED AND REPLACED SEAL RETAINER IAW SRM 51-30-2.

Part: INSULATION — DAMAGED (ACCCESSORY BAY) · airframe 56,586 hrs · 35,881 cycles

COMPLY WITH EA 7-2580-81691 "EQUIPMENT AND FURNISHINGS. INSULATION BLANKETS, PARTIAL REPLACEMENT, STA 178-294, LOWER SECTION 41 INCH.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,586 hrs · 35,881 cycles

STA 740 STR 27R CORROSION FOUND ON LOWER LEG OF ANGLE. REMOVED AND REPLACED ANGLE IAW EA 7-5310-55482 ON N/R CARD S00011.

Part: DOUBLER — CORRODED (BULKHEAD) · corrosion level 2 · airframe 56,586 hrs · 35,881 cycles

FUSELAGE STA 740 BULKHEAD SUPPORT DOUBLER CORROSION. COMPLIED WITH EA 7-5310-55482 FUSELAGE STA 740 BULKHEAD SUPPORT DOUBLER CORROSION AT MAE. THIS IS A MAJOR REPAIR.

Part: CLIP — CORRODED (RT MLG WW) · corrosion level 2 · airframe 56,586 hrs · 35,881 cycles

RT MLG WHEEL WELL ABOVE UPLOCK MECHANISM WEB UPPER SURFACE BETWEEN STA 930 - 940 SURFACE CORROSION. REMOVED AND REPLACED CLIP IAW SRM 51-30-2.

Part: PANEL — CRACKED (COCKPIT) · airframe 56,586 hrs · 35,881 cycles

BELOW CAPTAINS PEDALS RACEWAY (PANEL) HAVE CRACKS. REMOVED AND REPLACED RACEWAYS (PANELS) IAW SRM 51-30-2.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 56,586 hrs · 35,881 cycles

SEAT TRACK BL 0 STA 720F HAS AN EXISTING SPLICE REPAIR AND DOES NOT MEET REQUIREMENTS OF DWG 2902. REMOVED DAMAGED SECTION OF SEAT TRACK AND INSTALLED NEW SECTION OF TRACK WITH REPAIR ANGLES IAW SRM 51-10-5 FIG 1.

Part: BRACKET — CRACKED (CARGO DOOR) · airframe 56,586 hrs · 35,881 cycles

UPPER AFT DOOR BEARING GUIDE BRACKET ON AFT LWR CARGO DOOR FRAME IS CRACKED. REMOVED AND REPLACED DOOR GUIDE BRACKET IAW SRM 51-30-2.

Part: HINGE — CRACKED (RT T/E FLAP) · airframe 56,586 hrs · 35,881 cycles

RIGHT WING NR 8 FLAP TRACK FAIRING AFT I/B END IS CRACKED AND FWD FITTING IS GOUGED. REMOVED AND REPLACED FITTING IAW SRM 51-30-2.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 56,586 hrs · 35,881 cycles

LEFT WING LOWER FIXED T/E PANEL SUPPORT ANGLE CRACKED AT STA WS 522. REMOVED AND REPLACED SUPPORT ANGLE IAW SRM 51-30-2.

Part: GATE — CORRODED (GALLEY DOOR) · corrosion level 2 · airframe 56,586 hrs · 35,881 cycles

GALLEY DOOR LWR FLAPPER ASSY INNER STRUCTURE HAS CORROSION (MAG ALLOY ASSY). REMOVED AND REPLACED GALLEY DOOR LWR GATE IAW OHM 52-16-01.

Part: FLOORBEAM — DAMAGED (CARGO BAY) · airframe 56,586 hrs · 35,881 cycles

EVALUATE PREVIOUS REPAIR STA 1070 MCD FLOORBEAM RBL 12--RBL 62 UPPER CHORD FOR REPAIR STATUS (MAJOR/MINOR) AND FAA APROVAL. EVALUATED PREVIOUS REPAIR, FOUND TO BE IAW SR 27-53-034 REP NR 5 AND A MAJOR REPAIR IAW FED EX GMM 6-2-100.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,586 hrs · 35,881 cycles

CORROSION, STRINGER END TO FWD LWR FUEL TANK CHORD FITTING STA 740 STR 26L. REMOVED DAMAGED AREA IAW SRM 53-10-3 FIG 1 MATERIAL BAC 1498- 147-7075-T6 BATCH 27819 AND SPLICE MAT BMC 1498-131-7075-T6 BATCH 32659. LOCATED AND DRILLED IAW SRM 51-30-5, INSTALLED REPAIR PARTS IAW SRM 53-10-3 FIG 1.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 56,586 hrs · 35,881 cycles

EVALUATE PREVIOUS REPAIR STA 1120 STR 22 FOR REPAIR STATUS (MAJOR/MINOR) AND FAA APPROVAL. REMOVED DAMAGE SECTION OF STRINGER, FABBED FILLER AND SPLICES AND INSTALLED REPAIR IAW SRM 53-10-3 FIG 1 DETAIL I. THIS IS A MAJOR REPAIR ON N/R N00228 AT MAE.

Part: SKIN — GOUGED (FUSELAGE) · airframe 56,586 hrs · 35,881 cycles

FUSE SKIN AT BS 1228 STR 22L HAS DEEP GOUGED MARK MEASURED 1.5 INCH LONG. FABBED REPAIR PLATE IAW SRM 53-30-3 FIG 1 AND INSTALLED REPAIR PLATE IAW SRM 51-30-2. THIS IS A MAJOR REPAIR AT MAE ON N/R N00818.

Part: STRAP — CRACKED (FUSELAGE) · airframe 56,586 hrs · 35,881 cycles

SUBFLOOR BEAM STRAP STA 312-344 RBL 25 IS CRACKED 3EA PLACES. REMOVED AND REPLACED STRAP IAW SRM 51-30-2.

Part: MOUNT BRACKET — CRACKED (NR 1 SLAT) · airframe 56,586 hrs · 35,881 cycles

NR 1 SLAT OUTBOARD TRACK MOUNT BRACKET CRACKED. REMOVED AND REPLACED BRACKET IAW SRM 51-30-2.

Part: RETAINER — CRACKED (NR 3 SLAT) · airframe 56,586 hrs · 35,881 cycles

NR 3 SLAT INBOARD MOLDED SEAL RETAINER CRACKED ON SEVERAL AREAS. REMOVED AND REPLACED SEAL RETAINER IAW SRM 51-30-2.

Part: ANTENNA — CORRODED (LOWER VHF) · corrosion level 2 · airframe 56,586 hrs · 35,881 cycles

LOWER AFT VHF ANTENNA HAS CORROSION ON ITS BASE. REMOVED AND REPLACED LWR AFT VHF ANTENNA IAW MM 23-21-031-2, OPS CHECKS GOOD.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,586 hrs · 35,881 cycles

CORROSION ON LEFT TRANS PANEL FWD PIT STA 540-545. REMOVED AND REPLACED TRANSITIONAL PANEL IAW SRM 51-30-2 AT MAE ON N/R N00892.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 56,586 hrs · 35,881 cycles

SEAT TRACK STA 244 TO 480 RBL 45, HAS EXISTING BLEND REPAIRS AND AN EXISTING SPLICE REPAIR AND REQUIRES REPLACEMENT PER 7-5340-7-5002. REMOVED SEAT TRACK IAW SRM 51-30-2. FAB'D SEAT TRACK ON TRAVELER NR T5/510065. LOCATED AND DRILLED IAW SRM 53-10-5 FIG 3. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED SEAT TRACK IAW SRM 51-30-2.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 56,586 hrs · 35,881 cycles

SEAT TRACK, STA 344 - 480 HAS EXISTING BLEND REPAIRS AND REQUIRES REPLACEMENT PER 7-5340-7-5002, LBL 45. REMOVED SEAT TRACK STA 344 - 480 LBL 45 IAW SRM 51-30-2. FABRICATED NEW SEAT TRACK PER TRAVELER NR T5/510063, BATCH NR 888841, PO NR MST0017183. LOCATED AND DRILLED SEAT TRACK IAW SRM 51-10-4 AND 51-30-8. INSTALLED NEW SEAT TRACK IAW SRM 51-30-2.

Part: STRAP — CHAFED (FRAME) · airframe 56,586 hrs · 35,881 cycles

MAIN DECK CARGO, AT STA 1030 AND 1050 STR 6L, LINER FRAME ASSY HAS CHAFED INTO THE FRAME STRAP'S AND HARDWARE. GOUGE OUT OF LIMITS IAW BOEING SRM 53-10-1. REMOVED AND REPLACED STRAP IAW BOEING SRM 51-30-2.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 56,586 hrs · 35,881 cycles

SEAT TRACK, STA 344, LBL 24 HAS EXISTING BLEND REPAIRS AND REQUIRES REPLACEMENT PER 7-5340-7-5002. REMOVED SEAT TRACK STA 344 - 480 IAW SRM 51-30-2. FABRICATED NEW SEAT TRACK PER TRAVELER NRT5/510064, BATCH NR 888841, P.O. NR MST0017183. LOCATED AND DRILLED NEW SEAT TRACK IAW SRM 51-10-4. INSTALLED NEW SEAT TRACK IAW SRM 51-30-2.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 54,584 hrs · 34,249 cycles

CORROSION ON SHEAR TIE BS 580 JUST O/B OF STR 28R. R&R SHEAR TIE PER SRM 51-30-2, 51-10-6, 51-20-1, 51-30-5.

Part: FRAME — CORRODED (FUSELAGE) · airframe 54,584 hrs · 34,249 cycles

CORROSION ON FRAME BS 420, STR 23R. R&R FRAME PER SRM 51-40-3.

Part: KEELBEAM — DAMAGED (FUSELAGE) · airframe 54,584 hrs · 34,249 cycles

COMPLY WITH EO REV C1 PT5 KEELBEAM CHORD REPAIR BS 980-1007, STR 29L. REPAIRED KEELBEAM BS 980-1007, STR 29L IAW EO.

Part: FRAME — CORRODED (FUSELAGE) · airframe 54,584 hrs · 34,249 cycles

CORROSION ON FRAME BS 720E, STR 27R TO 28R. R&R FRAME PER SRM 53-10-4 FIG 11.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 54,584 hrs · 34,249 cycles

CORROSION ON STR 29L, BS 1000 TO 1018. R&R STRINGER PER EO 7-5310-7-2356.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 54,584 hrs · 34,249 cycles

CORROSION ON KEELBEAM BS 1000, STR 29L. R&R KEELBEAM PER EO 7-5310-7-2356.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 54,584 hrs · 34,249 cycles

CORROSION ON FLOORBEAM LOWER CHORD BS 1070, RBL 46, WL 200. REPAIRED FLOORBEAM IAW SRM 53-10-8 FIG 8.

Part: SKIN — DENTED (FUSELAGE) · airframe 54,584 hrs · 34,249 cycles

DENT IN ETERNAL FUSELAGE SKIN AT BS 1045 JUST BELOW STR 20L. R&R SKIN PER SRM 53-30-3.

Part: FRAME — DENTED (FUSELAGE) · airframe 54,584 hrs · 34,249 cycles

DENT ON FRAME AT STR 23R ASSOCIATED WITH E&E CATWALK. REPAIRED FRAME IAW SRM 51-40-3.

Part: STRINGER — DENTED (FUSELAGE) · airframe 54,584 hrs · 34,249 cycles

DENT IN STR AT BS 392. REPAIRED STR 23R BS 392 IAW SRM 53-10-3, 51-10-2.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 54,584 hrs · 34,249 cycles

CORROSION ON SHEAR TIE AT BS 720C+1 BETWEEN STR 18L - 28R. R&R SHEAR TIE PER SRM 51-30-2, 51-20-1.

Part: SKIN — CORRODED (FUSELAGE) · airframe 54,584 hrs · 34,249 cycles

CORROSION ON SKIN BS 720C+1 BETWEEN STR 28L-28R. REPAIRED SKIN BS 720C+1, STR 28L-28R IAW EA.

Part: RELAY — MALFUNCTIONED (STAB TRIM)

WHEN THROTTLE RETARD AUTO PILOT KICKED OFF AND TRIM RAN AWAY NOSE DOWN. INSTALL NEW STAB TRIM TRANSFER RELAY 5591 FOR PRECAUTION PER MM 27-40-0. OK FOR SERVICE.

Part: DUCT — LOOSE (PRECOOLER)

THREE MINUTES AFTER TAKEOFF WITH CLIMB POWER SELECTED 90 PERCENT, ENG NR 1 STRUT OVERHEAT LIGHT ILLUMINATED. ACCOMP RED TAB PROCEDURES AND LIGHT EXTINGUISHED, SYS TESTS GOOD AND NO FURTHER PROBLEMS. INSP STUB WING TEMP SENSORS VALVES AND DUCTS. FOUND LOOSE CLAMP ON DUCT FROM PRECOOLER TO OVER BOARD DUCT. SECURED SAME, RAN ENG AT HIGH RPM, NO LEAKAGE.

Part: ANGLE — CRACKED (WS 656.5)

RT WING WS 656.6 S14 LWR ANGLE CRACKED AT RIB ATTACH FASTENER. STOP DRILLED END OF CRACK. HFEC CONFIRMED CRACK ENDS AT STOP DRILL. INSTALLED REPAIR ANGLES PER SRM 57-10-4 AND SB 727-57A 159 FIG 18.

Part: ANGLE — CRACKED (WS 656.5)

RT WING WS 656.5 S13 LWR ANGLE CRACKED AT RIB ATTACH FASTENER. STOP DRILLED CRACK. HFEC CONFIRMED CRACK ENDS AT STOP DRILL. INSTALL REPAIR ANGLES PER SRM 57-10-4 AND SB 57A 159 FIG 18.

Part: ANGLE — CRACKED (WS 656.5)

RT WING WS 656.5, S12 LWR ANGLE CRACKED AT RIB ATTACH FASTENER. HFEC CONFIRMED CRACK RUNS FROM FASTENER HOLE TO AFT EDGE OF ANGLE. INSTALLED REPAIR ANGLES PER SRM 57-10-4 PG 37 FIG 11, REF SB 727-57A159.

Part: ENGINE — FLAMED OUT (NR 3)

NR 3 ENG FLAMED OUT ON T/O PASSING 4000 FT AGL 220 KIAS. ATTEMPTED RESTART UNSUCCESSFUL, ENG SHUTDOWN CHECKLIST COMPLIED WITH. CHECKED NR 3 ENG, IGN SYS CK'D NORMAL, OPS CK'D NR 3 FUEL HEAT VALVE CK'D NORMAL. REPLACED NR 3 ENG MAIN FUEL FILTER. RAN ENG LEAK CK'D GOOD, INSPECTED MOISTURE TRAP AND CDP AIR LINE ALL CK'D GOOD. ENG INLET, AND EXHAUST VISUALLY INSPECTED GOOD. COMPLIED W/FLAME OUT TROUBLESHOOTING PER MM 72-00-07A, PWA AND SUMPED NR 3 MAIN FUEL TANK, NO WATER FOUND. RAN NR 2 ENG TO T/O PWR, CK'D NORMAL, OK TO CONTINUE.