N832FT
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
279 reports on file, 1995-04-19 – 1996-08-12.
Part: DOUBLER — CORRODED (BS 2240/2280)
CORROSION ON REINFORCEMENT DOUBLER AT FUSELAGE RT SIDE ABOVE PASSENGER DOOR 5 STA 2240 AND UNDER STA 2280. CORROSION REMOVED PER SRM 51-10-01.
Part: FASTENERS — CORRODED (BS 1680)
CORROSION ON HEAD OF HI-LOCK AT STA 1680 BETWEEN STRINGER 3 TO 4 LT. CORRODED RIVETS TAKEN OUT AND INSTALLED NEW HI-LOCKS PER SRM 51-30-02.
Part: BEAM — CRACKED (LT LE FLAP)
LEFT INBOARD KREUGER L/E FLAP PDU AFTER MOUNT BEAM INBOARD EDGE CRACKED. FAB NEW ANGLE PER SRM 57-12-01 AND INSTALLED PER SRM 51-30-02.
Part: CHORD — CORRODED (RT TE MID FLAP)
RT INBOARD MID FLAP WITH PANEL REMOVED SURFACE, CORROSION ON UPPER CTR CHORD OUTBD END, UNDER PANEL. CORROSION REMOVED AND TREATED PER SRM 51-10-01, FOUND WITHIN LIMITS PER SRM 57-10-01.
Part: PLATE — CHAFED (NLG DOOR)
NOSE LANDING GEAR WHEEL WELL LT FWD DOOR, FLAPPER DOOR DEEP CHAFING ON CHAFING PROTECTION PLATE. NEW PLATE FABRICATED PER SRM 52-80-01 AND 51-30-02.
Part: STRINGER — CORRODED (BS 1160-1180)
CORROSION ON STRINGER 8, 10 BETWEEN STA 1160 TO 1180. CORROSION REMOVED PER SRM 51-10-01, FOUND WITHIN LIMITS PER SRM 53-10-01.
Part: STRINGER — CORRODED (BS 1620-1640)
CORROSION ON STRINGER 1, 2, 8 RT BETWEEN STA 1620 TO 1640. REPAIRED PER SRM 51-10-03.
Part: STRINGER — CORRODED (BS 2100)
CORROSION ON FRAME AT STA 2100 NEAR STRINGER 3. CORROSION REMOVED PER SRM 51-10-01, FOUND WITHIN LIMITS PER SRM 53-10-01.
Part: STRINGER — CORRODED (BS 1800-1820)
CORROSION ON STRINGER 49 AND 51 RT SIDE AND STRINGER 47, 48, 49, 50 LT SIDE BETWEEN STA 1800 TO 1820. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01, FOUND WITHIN LIMITS PER SRM 53-10-01.
Part: STRINGER — CORRODED (BS 1760-1780)
CORROSION ON STRINGER 48 TO 49 RT SIDE AND STRINGER 46 TO 51 LT SIDE BETWEEN STA 1760 TO 1780. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01, FOUND WITHIN LIMITS PER SRM 53-10-01.
Part: STRINGER — CORRODED (BS 1700-1720)
CORROSION ON STRINGER 51 LT SIDE BETWEEN STA 1700 TO 1720. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01, FOUND WITHIN LIMITS PER SRM 53-10-01.
Part: STRINGER — CORRODED (BS 2140)
CORROSION ON STRINGER 1 AT STA 2140 LT SIDE. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01.
Part: FRAME — CORRODED (BS 2020)
CORROSION ON FRAME LWR CHORD AREA AT STA 2020 BETWEEN STRINGER 7 TO 8 LT. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01.
Part: STRINGER — CORRODED (BS 1740-1760)
CORROSION ON STRINGER 44 TO 45 RT SIDE AND STRINGER 46 LT SIDE BETWEEN STA 1740 TO 1760. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01 WITHIN LIMITS PER SRM 53-10-01.
Part: STRINGER — CORRODED (BS 2060)
CORROSION ON STA 2060 LT SIDE AT STRINGER 26 AREA. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01.
Part: TIE CLIP — CORRODED (BS 1960)
CORROSION ON TIE CLIP AT STA 1960 NEAR STRINGER 2 RT. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01.
Part: STRINGER — CORRODED (BS 1540)
CORROSION ON STRINGER 1 LT NEAR STA 1540. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01.
Part: FLOOR RIB — DAMAGED (BS 1620-1640)
BENT ON FLOOR RIB BETWEEN STA 1620 TO 1640 AT LBL 28 AREA. REPAIRED AND TREATED PER SRM 51-40-01 AND SRM 51-10-01.
Part: TIE CLIP — CORRODED (BS 2280)
CORROSION ON TIE CLIP AT STA 2280 LT SIDE STRINGER 14. INSTALLED NEW CLIP (P/N 65B38600-160) PER SRM 51-30-02.
Part: RIVETS — FAILED (WS 380)
SHEAR RIVETS ON UPPER WING SKIN RT AT STA 380 FRONT SPAR AREA. INSTALLED NEW RIVETS PER SRM 51-30-02.
Part: RIVETS — SHEARED (WS 480)
SHEARED RIVETS ON UPPER WING SKIN RT AT STA 480 IN FRONT SPAR AREA. INSTALLED NEW RIVETS .1875 PER SRM 51-30-02.
Part: RIVETS — SHEARED (WS 565)
SHEARED RIVETS ON UPPER WING SKIN RT AT STA 565 FRONT SPAR. NEW RIVETS PER SRM 51-30-02.
Part: SKIN — CORRODED (PAX DOOR)
CORROSION AND HOLE ON LWR SIDE OF PASSENGER DOOR LT BETWEEN STA 2260 TO 2280. HOLE RIVETED WITH NAS 78585-7 RIVET BN.08729-96 PER SRM 51-30-02. REMOVED PER SRM 51-10-01.
Part: BRACKET — CRACKED (BS 1940)
CRACKED AND CORROSION, MISSING RIVETS ON BRACKET AT STA 1940 RT SIDE ABOVE STRINGER 40 TO 43. AREA REPAIRED PER SRM 51-40-02 AND 51-40-03.
Part: FRAME — CORRODED (BS 1110)
CORROSION ON FRAME AT STA 1110 STRINGER 1 LT. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01.
Part: STRINGER — CORRODED (BS 1660-1680)
CORROSION ON STRINGER 15 AND 16 BETWEEN STA 1660 TO 1680 RT SIDE. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01.
Part: STRINGER — CORRODED (BS 1880)
CORROSION ON DOUBLER AT STRINGER 19 AREA AND BENT ON BRACKET NEAR STRINGER 16 AT STA 1880 RT SIDE. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01.
Part: STRINGER — CORRODED (BS 1380-1400)
CORROSION ON STRINGER 8, 9, 10 LT BETWEEN STA 1380 TO 1400. CORROSION BLENDED OUT SURFACE, SMOOTHED PER SRM 51-10-01 AND 51-10-02.
Part: TIE CLIP — CORRODED (BS 2160)
CORROSION ON TIE CLIP AT STA 2160 NEAR STRINGER 11 LT. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01.
Part: STRINGER — CORRODED (BS 1780-1800)
CORROSION ON STRINGER 49 RT SIDE AND STRINGER 46, 51 LT SIDE BETWEEN STA 1780 TO 1800. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01, FOUND WITHIN LIMITS PER SRM 53-10-01.
Part: INTERCOSTAL — CORRODED (BS 1760-1780)
CORROSION ON FLOOR INTERCOSTAL BETWEEN STA 1760 TO 1780 AT RBL 42 AREA. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01, FOUND WITHIN LIMITS PER SRM 53-10-01.
Part: STRINGER — CORRODED (BS 2040)
CORROSION UNDER SEALING ON STRINGER 20 AT AREA WINDOW FRAME NEAR STA 2040 RT. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01.
Part: SKIN — CORRODED (BS 1560-1620)
CORROSION ON INTERNAL SKIN BETWEEN STA 1560 TO 1620 AND BETWEEN STRINGER 3 TO 4 RT. CORROSION REMOVED PER SRM 51-10-01, FOUND WITHIN LIMITS PER SRM 53-10-01.
Part: SKIN — CORRODED (BS 2100-2120)
CORROSION ON THE SKIN UNDER SEALING AT STRINGER 19 LAP JOINT BETWEEN STA 2100 TO 2120 RT SIDE. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01.
Part: TIE CLIP — CORRODED (BS 1780)
CORROSION ON TIE CLIP OF STRINGER 3 RT AT STA 1780. CORROSION REMOVED PER SRM 51-10-01, FOUND WITHIN THE LIMITS PER SRM 53-10-01.
Part: STRINGER — CORRODED (BS 1780-1800)
CORROSION ON STRINGER 39 BETWEEN STA 1780 TO 1800 LT SIDE. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01, FOUND WITHIN LIMITS PER SRM 53-10-01.
Part: TIE CLIPS — CORRODED (BS 2140-2160)
CORROSION ON TIE CLIPS AT STA 2140 AND 2160 IN STRINGER 4, 5 RT. CORROSION REMOVED PER SRM 51-10-01, FOUND WITHIN THE LIMITS PER SRM 53-10-01.
Part: SKIN — CORRODED (BS 1720-1740)
CORROSION ON THE SKIN BETWEEN STA 1720 TO 1740 AND BETWEEN STRINGER 48 TO 49 RT SIDE AND BETWEEN STRINGER 51 RT TO STRINGER 51 LT. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01 AND 53-10-01.
Part: STRINGER — CORRODED (BS 1720-1740)
CORROSION ON STRINGER 44, 48, 49 AND 51 RT SIDE AND STRINGER 51 LT SIDE BETWEEN STA 1720 TO 1740. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01, FOUND WITHIN LIMITS PER SRM 53-10-01.
Part: FLOORBEAM — CORRODED (BS 1540)
CORROSION ON UPPER CHORD FLOORBEAM STA 1540 BETWEEN AREA RBL 35 TO 45. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01.
Part: STRAP — BROKEN (BS 1780-1800)
BROKEN STRAP ON INTERCOSTAL AT CARGO FLOOR BETWEEN STA 1780 TO 1800 RT SIDE ABOVE STRINGER 42. FAB NEW STRAP INST AND RIVETED PER SRM 51-40-02.
Part: DOOR — CORRODED (AC COMPT)
AIR CONDITION BAY DOORS HINGE SUPPORTS ARE CORRODED LT DOORS. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01.
Part: RIVET — CRACKED (BS 1660)
CRACK AND SHEARED RIVET ON STA 1660 LT SIDE ABOVE STRINGER 34. AREA REPAIRED PER SRM 51-40-02.
Part: SKIN — CORRODED (BS 1740-1760)
CORROSION ON THE SKIN BETWEEN STRINGER 41 TO 42 AND BETWEEN STA 1740 TO 1760. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01.
Part: FLOORBEAM — CORRODED (BS 960)
CORROSION ON UPPER CHORD FLOORBEAM AT STA 960 BETWEEN AREA RBL AND LBL 32 TO 45. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01.
Part: WEB — TORN (BS 1800)
TEAR ON THE WEB AT STA 1800 UNDER UPPER CHORD AT AREA LBL 48. AREA REPAIRED PER SRM 51-40-02.
Part: FLOORBEAM — CORRODED (BS 1720)
CORROSION ON UPPER CHORD FLOORBEAM AT STA 1720 BETWEEN AREA LBL 32 TO 45. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01.
Part: KEEL BEAM — CORRODED (FUSELAGE)
CORROSION ON KEEL BEAM OUTER STRINGERS ABOVE RT A/C BAY DOORS. REMOVED CORROSION AND AREA TREATED PER SRM 51-10-01.
Part: STRINGER — CORRODED (BS 1180-1200)
CORROSION ON STRINGER 7, 9 LT BETWEEN STA 1180 TO 1200. CORROSION REMOVED PER SRM 51-10-01, FOUND WITHIN LIMITS PER SRM 53-10-01.
Part: INTERCOSTAL — CORRODED (BS 1960-1980)
CORROSION ON INTERCOSTAL AND STRINGER 44, BETWEEN STA 1960 TO 1980 RT SIDE. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01, FOUND WITHIN LIMITS PER SRM 53-10-01.
Part: KEEL BEAM — CORRODED (BS 1080-1100)
CORROSION ON LWR SIDE OF VERTICAL SUPPORT AT KEEL BEAM WALL LT SIDE ABOVE DOOR 5 LWR FUS BETWEEN STA 1080 TO 1100 MARKED. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01.
Part: SKIN — CHAFED (BS 2120)
CHAFING ON LWR FUSELAGE SKIN RT SIDE NEAR STA 2120 BETWEEN STRINGER 48 TO 49. STRAIGHTEN AND SMOOTHED PER SRM 51-10-01.
Part: FLOORBEAM — CRACKED (BS 820-860)
CRACKS W/STOP HOLE AND SHEARED, LOOSE RIVETS ON SHEET METAL COVER, UNDER FLOORBEAM BETWEEN STA 820 TO 860 BETWEEN AREA RBL 6 TO 25. REPAIRED SHEET METAL COVER PER SRM 51-40-02 AND SRM 51-30-02.
Part: SKIN — CORRODED (WS 2360)
CORROSION AND SHEARED RIVET ON FUSELAGE SKIN RT SIDE STA 2360 BETWEEN STRINGER 18 TO 23. CLEANED CORROSION AND TREATED PER SRM 51-10-01, NEW FASTENERS PER SRM 51-30-02.
Part: BRACKET — BROKEN (WS 669.5)
BROKEN SUPPORT BRACKET OF ENG NR 2 FAIRING NEAR FRONT SPAR LEADING EDGE AT STA 669.50 AREA. FAB NEW SUPPORT BRACKET PER OLD BRACKET, RIVETED PER SRM 51-30-02.
Part: SKIN — CORRODED (BS 2360)
SURFACE CORROSION ON LWR FUSELAGE SKIN AT STA 2360 BETWEEN STRINGER 45 RT TO STRING 46 LT SIDE. CORROSION REMOVED AND TREATED PER SRM 51-10-01.
Part: BRACKET — CRACKED (BS 1000)
CRACK ON BRACKET ON STA 1000 LT SIDE BETWEEN STRINGER 16 TO 17. INSTALLED NEW BRACKET/7075-T6 AND RIVETED PER SRM 51-30-02.
Part: DOORWAY FRAME — CRACKED (BS 2240)
CRACK WITH STOP HOLE ON FRAME ENTRY CARGO DOOR 5 AT STA 2240 AREA LT. PERFORMED REPAIR PER SRM 51-40-02.
Part: STRINGER — CORRODED (BS 220)
DEEP HIT AND CORROSION ON STA 220 LT SIDE AT STRINGER 26 AREA. REMOVED CORROSION AND AREA TREATED PER SRM 51-10-01 AND 51-40-02.
Part: FRAME — CORRODED (BS 1620)
CORROSION ON FRAME AT STA 1620 BETWEEN STRINGER 1 TO2 LT. REPAIRED PER SRM 53-10-03.
Part: DOUBLER — CORRODED (PAX DOOR CUTOUT)
CORROSION ON DOUBLERS AT FUSELAGE RT SIDE UNDER TO PASSENGER DOOR 3. REMOVED CORROSION AND TREATED PER SRM 51-10-01.
Part: SKIN — CORRODED (WS 625)
SWELLING ON UPPER WING SKIN RT AT STA 625 IN FRONT SPAR AREA. CORROSION REMOVED AND TREATED PER SRM 51-10-01, RIVET PER SRM 51-30-02.
Part: WEB — TORN (CARGO COMPT)
FORWARD CARGO COMPARTMENT SHEET METAL TORN ON STA 680 L. SMALL CRACK BLENDED OUT AND TREATED PER SRM 51-10-01, INSTALLED RIVETS PER SRM 51-30-02.
Part: SKIN — CORRODED (BS 1760)
SWELLING ON UPPER FUSELAGE SKIN LT SIDE STA 1760 AREA AT STRINGER 3. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01, INSTALLED NEW RIVET PER SRM 51-30-02.
Part: HINGE — CORRODED (NLG DOOR)
NOSE LANDING GEAR SURFACE CORROSION ON SERVICE CONTROL PANEL DOOR HINGE. INSTALLED NEW HINGE PER SRM 51-30-02.
Part: FLOORBEAM — CRACKED (BS 440)
CRACK ON WEB AND UPPER CHORD AT FLOORBEAM STA 440 RT SIDE NEAR PASSENGER DOOR-1. UPPER CHORD REPAIRED, WEB REINFORCED PER SRM 53-10-07.
Part: STRINGER — CORRODED (BS 1080)
CORROSION ON STRINGER 3 RT AT STA 1080. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01.
Part: SKIN — CORRODED (WS 315)
SWELLING ON UPPER WING SKIN RT AT STA WS 315 IN FRONT SPAR AREA. REMOVED RIVETS AND CLEANED CORROSION PER SRM 51-10-01 AND 51-30-02.
Part: STRINGER — CORRODED (BS 1406)
CORROSION ON STRINGER 1 LT AT STA 1406. CORROSION REMOVED AND TREATED PER SRM 51-10-01.
Part: SUPPORT — CORRODED (BS 1000)
CORROSION ON FAIRING SUPPORT LWR FUSELAGE AT STA 1000 BETWEEN AREA RBL TO LBL 40. REMOVED CORROSION AND AREA TREATED PER SRM 51-10-01 AND 51-40-03.
Part: TIE CLIP — CORRODED (BS 1560/1580)
CORROSION ON HL IN TIE CLIP AT STRINGER 1 TO 3 RT STA 1560, 1580. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01.
Part: FITTING — CORRODED (NR 1 L PAX DOOR)
NR 1L ENTRY DOOR CORROSION ON STOP FITTING FASTENERS ALONG FWD FRAME. CLEANED PER MM 51-21-00.
Part: HINGE — CORRODED (NR 4R PAX DOOR)
NR 4R ENTRY DOOR FUSELAGE DOOR CUTOUT SURFACE CORROSION ON LWR HINGE GUIDE CAM. CLEANED PER MM 51-21-00.
Part: FITTING — CRACKED (DOOR 1R)
CRACK ON FITTING AT CONNECTION UPPER HINGE TO DOOR 1 RT LWR SIDE. INSTALLED NEW FITTING (P/N 65B07922-2) PER SRM 51-30-02.
Part: RIVETS — CORRODED (FUSELAGE)
CORROSION, HITS, SCRATCHES, SHEARED RIVET AND CONNECTION BETWEEN EXISTING REPAIR FASTENER AND SHEET METAL COVER. REPAIRED PER SRM 51-40-02.
Part: WEB — TORN (BS 1860)
TORN ON THE WEB AT STA 1860 RT SIDE ABOVE STRINGER 46, 47. AREA REPAIRED PER SRM 51-40-02.
Part: SUPPORT — WORN (TE FLAPS)
LEFT WING OUTBD T/E FLAP TORQUE TUBE GEAR BOX HAS EXCESSIVE PLAY BETWEEN FLAP TRACK 1 AND 2. TORQUE TUBE SUPPORT REPLACED PER MM 27-51-00.
Part: FITTING — CORRODED (BS 1480)
CORROSION ON FITTING TRACK RBL 25 AT STA 1480 AREA. CORROSION REMOVED AND TREATED PER SRM 51-10-01, FOUND WITHIN LIMITS PER SRM 53-10-01.
Part: ARM — CORRODED (NR 7 LE FLAP)
L/E FLAP 7 INCHES INBOARD ARM SURFACE CORROSION. CORROSION REMOVED FROM SURFACE PER SRM 51-10-01.
Part: TRACKS — CORRODED (LT TE FORE FLAPS)
CORROSION LEFT WING ALL 7 FORE FLAP TRACKS SURFACE. CORROSION REMOVED FROM SURFACE PER SRM 51-10-01.
Part: SKIN — CORRODED (BS 2360)
SURFACE CORROSION ON FUSELAGE SKIN LT SIDE STA 2360 AT STRINGER 23 AREA. CLEANED CORROSION AND TREATED PER SRM 51-10-01.
Part: FLOORBEAM — CORRODED (BS 940)
CORROSION ON UPPER CHORD FLOORBEAM AT STA 940 BETWEEN AREA LBL 32 TO 45. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01.
Part: FLOORBEAM — CORRODED (BS 1800)
CORROSION ON UPPER CHORD FLOORBEAM AT STA 1800 AREA RBL AND LBL 30 TO 45. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01, FOUND WITHIN LIMITS PER SRM 53-10-01.
Part: FITTING — CRACKING (RT WING)
RT WING CRACKED UNDERWING FITTING OF FWD SKIRT ROD ATT, AFT OF DUAL SIDE STRUT FITTING OF NR 3 PYLON. MUST BE REPAIRED BEFORE INST NEW FITTING (P/N 69B12302-6) AND RIVETED PER SRM 51-30-02.
Part: DOUBLER — CORRODED (BS 1480)
CORROSION ON DOUBLER AT SHEET METAL COVER NEAR STA 1480 AT RBL 6. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01.
Part: ANGLE — CORRODED (BS 2240)
CORROSION ON ANGLES NEAR STA 2240 LT SIDE AT STRINGER 26 AREA FLOOR. CORROSION REMOVED PER SRM 51-10-01, FOUND WITHIN LIMITS PER SRM 53-10-01.
Part: FRAME — CORRODED (BS 1800-1820)
CORROSION AND HITS ON AFT ENTRY CARGO FRAME BETWEEN STA 1800 TO 1820 RT ABOVE STRINGER 36 TO 40. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01.
Part: RIVET — CRACKING (BS 1680)
CRACK AND SHEARED RIVET ON INTERCOSTAL AT STRINGER 34 NEAR STA 1680 LT SIDE. AREA REPAIRED PER SRM 51-40-02.
Part: ANGLE — CORRODED (BS 940-960)
CORROSION ON FLOOR ANGLE BETWEEN STA 940 TO 960 BETWEEN AREA RBL 32 TO 45. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01.
Part: LATCH — BROKEN (CARGO DOOR)
BROKEN LATCH AND SHEARED RIVETS ON AFTER CARGO DOOR SERVICE PANEL AND SCRATCHES ON FUSELAGE SKIN RT SIDE BETWEEN STA 1780 TO 1820 AND BETWEEN STRINGER 34 TO 40. INSTALLED NEW LATCH, SMOOTHED SCRATCHES AND AREA TREATED PER SRM 51-30-02 AND 51-10-01.
Part: SKIN — CORRODED (WS 720)
CORROSION ON UPPER WING SKIN RT AT STA WS 720 STA 20 AREA. CORROSION REMOVED AND TREATED PER SRM 51-10-01, FOUND WITHIN LIMITS PER SRM 57-10-01.
Part: CHORD — CRACKED (BS 1920)
CRACK ON STA 1920 AT UPPER CHORD AREA ABOVE STRINGER 42 LT. AREA REPAIRED PER SRM 53-10-04.
Part: SKIN — CORRODED (WS 680)
SWELLING ON UPPER WING SKIN AT STA 680 IN FRONT SPAR AREA. REMOVED CORROSION AND FASTENERS PER SRM 51-10-01, INSTALLED NEW RIVETS.
Part: HINGE COVER — CORRODED (BS 2240)
DENT ON SHEET METAL UPPER HINGE COVER OF PASSENGER DOOR 5 RT AND TORN ON THE SKIN AT DOOR STA 2240. REMOVED SHEET METAL FROM UPPER HINGE AND BLENDED OUT THE TEAR, CLEANED CORROSION AND TREATED PER SRM 51-10-01.
Part: STRINGER — CORRODED (BS 1160-1180)
CORROSION ON STRINGER 6, 7 BETWEEN STA 1160 TO 1180. CORROSION REMOVED PER SRM 51-10-01, FOUND WITHIN LIMITS PER SRM 53-10-01.
Part: KEEL BEAM — CORRODED (BS 1220-1241)
DEEP CORROSION ON LT SPAR AT KEEL BEAM AREA CENTER LWR FUSELAGE BETWEEN STA 1220 TO 1241. REMOVED CORROSION AND AREA TREATED PER SRM 51-10-01.
Part: STRINGER — CORRODED (BS 1080)
CORROSION ON STRINGER 3 RT AT STA 1080. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01.
Part: INTERCOSTAL — CRACKED (BS 1900-1920)
BROKEN, CRACKED AND CORROSION ON FLOOR INTERCOSTAL BETWEEN STA 1900 TO 1920 AND BETWEEN AREA BL 0 TO RBL 30. ALL AREAS REPAIRED PER SRM 51-40-02 AND SRM 51-40-03, TREATED PER SRM 51-10-01.
Part: SKIN — CORRODED (WS 834.5)
SWELLING ON UPPER RT WING SKIN AT REAR SPAR AREA WS 834.50. REMOVED RIVETS CLEANED CORROSION AND TREATED PER SRM 51-10-01, RERIVETED PER SRM 51-30-02.
Part: STRINGER — CORRODED (BS 1580-1600)
CORROSION STRINGER 2 RT BETWEEN STA 1580 TO 1600. CORROSION BLENDED OUT SURFACE, SMOOTHED PER SRM 51-10-01 AND 51-10-02.
Part: STRINGER — CORRODED (BS 1400-1420)
CORROSION ON STRINGER 3 LT BETWEEN STA 1400 TO 1420. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01.
Part: SCUFF PLATE — CORRODED (CARGO DOOR)
DEEP SURFACE CORROSION, DENT AND CRACK ON LWR SCUFF PLATE AT ENTRY BULK AFTER CARGO DOOR BETWEEN STA 198 TO 2040. FAB AND INSTALLED NEW LWR SCUFF PLATE, FASTENERS INSTALLED PER SRM 51-30-02.
Part: COWL FITTING — CRACKED (NR 4 ENGINE)
NR 4 RT MAIN COWL FWD LATCH FORGING FITTING HAS A CRACK IN LATCH CUTOUT. REMOVED RIVETS CLEANED CORROSION AND TREATED PER SRM 51-10-01, INSTALLED NEW RIVETS PER SRM 51-30-02.
Part: KEEL BEEM — CORRODED (BS 1000-1241)
CORROSION SHEET METAL COVER AND BRACKET SUPPORTS AROUND TO KEEL BEAM CUTOUTS AT CENTER LWR FUS BETWEEN STA 1000 TO 1241. CORROSION REMOVED, AREA TREATED PER SRM 51-10-01.
Part: BEAM — CORRODED (LT MLG)
LEFT BODY LANDING GEAR WHEEL WELL AFTER REMOVAL OF SPLICE PLATES CORROSION FOUND IN LANDING GEAR BEAM LOWER CHORD HORIZONTAL FLANGE. ALSO, ON VERTICAL FLANGE INBOARD AFT SIDE. CORROSION REMOVED SB53-2310.
Part: STRINGER — CRACK (BS 1900)
CRACK BEYOND EXISTING REPAIR ON STA 1900 LT SIDE ABOVE STRINGER 41 TO 42. REPAIRED PER SRM 53-10-04.
Part: STRINGER — CORRODED (BS 1640)
CORROSION ON STRINGER 4 RT AT STA 1640. CORROSION REMOVED AND TREATED PER SRM 51-10-01.
Part: STRINGER — CORRODED (BS 1400-1420)
CORROSION STRINGER 5 LT BETWEEN STA 1400 TO 1420. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01.
Part: RIVETS — SHEARED (WS 600)
SHEARED RIVETS ON UPPER WING SKIN RT AT STA 600 IN FRONT SPAR AREA. INSTALLED NEW RIVETS OBTAINED FROM STA STOCK BN 91662-25.
Part: STRINGER — CORRODED (BS 1420-1440)
CORROSION ON STRINGER 7 LT AT STA 1420 TO 1440. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01.
Part: STRINGER — CORRODED (BS 1420)
CORROSION ON STRINGER 5 AT STA 1420. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01.
Part: SKIN — CORRODED (BS 2120-1960)
CORROSION ON THE SKIN UNDER SEALER AT STRINGER 12 LAP JOINT AREA BETWEEN STA 2120 TO 1960 RT SIDE. CORROSION REMOVED AND TREATED PER SRM 51-10-01.
Part: SKIN — CORRODED (BS 1372-1740)
SURFACE CORROSION ON THE SKIN BETWEEN STA 1372 TO 1740 AND BETWEEN STRINGER 12 TO 18 LT SIDE. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01, FOUND WITHIN THE LIMITS PER SRM 53-30-01.
Part: RIVETS — SHEARED (WS 990)
SHEARED RIVETS ON UPPER WING SKIN RT AT STA WS 990 IN FRONT SPAR AREA. INSTALLED NEW RIVET .1875 PER SRM 51-30-02.
Part: STRIP — TORN (LT AILERON)
LEFT OUTBOARD AILERON UPPER OUTBOARD STRIP IS TORN. TORN STRIP REPLACED PER MM 57-51-00.
Part: STRINGER — CORRODED (BS 1580-1600)
CORROSION STRINGER 7 TO 9 BETWEEN STA 1580 TO 1600 LT. CORROSION REMOVED AND AREA TREATED PER 51-10-01.
Part: INTERCOSTAL — DAMAGED (BS 1920-1940)
DENT ON INTERCOSTAL AT STRINGER 35 BETWEEN STA 1920 TO 1940 LT SIDE. STRAIGHTEN SRM 51-40-01 AND TREATED PER SRM 51-10-01. VISUAL CHECK FOUND OK.
Part: CHORD — CRACKED (BS 1580)
CRACK ON UPPER CHORD STA 1580 RT SIDE ABOVE STRINGER 39 TO 40. REPAIRED PER SRM 53-10-04.
Part: SKIN — CORRODED (BS 2240-2280)
CORROSION ON REINFORCEMENT DOUBLER ON FUS SKIN ABOVE AND LWR PASSENGER DOOR 5 AT STA 2240 AND 2280. CORROSION REMOVED PER SRM 51-10-01.
Part: SKIN — CORRODED (BS 260)
CORROSION ON NOSE SKIN UNDER FWD COCKPIT WINDOW AT STA 260 AREA. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01.
Part: DOME NUTS — CORRODED (NR 3 PAX DOOR)
NR 3L MAIN ENTRY DOOR CORROSION ON DOME NUTS AT UPPER FRAME INNER SURFACE. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01 AND 51-30-02.
Part: CLIP — CRACKED (BS 1820)
CRACK ON TIE CLIP AT STA 1820 IN STRINGER 4 LT AREA. INST NEW CLIP (P/N 65B38600-160) AND RIVETED OBTAINED FROM STA STOCK PER SRM 51-30-02.
Part: SUPPORT — CRACKED (BS 1480)
CRACKS ON FAIRING SUPPORT ANGLES LWR FUS LT SIDE STA 1480. REPAIRED PER SRM 53-50-04.
Part: WINDOW FRAME — CORRODED (BS 1940-1960)
CORROSION WINDOW FRAME UNDER SEALANT AT STRINGER 22 BETWEEN STA 1940 TO 1960 RT. CORROSION REMOVED AND TREATED PER SRM 51-10-01.
Part: STRINGER — CORRODED (BS 1080-1100)
CORROSION ON STRINGER 7, 9 BETWEEN STA 1080 TO 1100. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01.
Part: CHORD — CORRODED (BS 1920)
CORROSION ON PROFILE TEE ABOVE UPPER CHORD STA 1920. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01.
Part: STRINGER — CORRODED (BS 1080-1100)
CORROSION ON STRINGER 1, 4, 5, 6 LT BETWEEN STA 1080 TO 1100. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01.
Part: STRINGER — CORRODED (BS 1920-1940)
CORROSION ON STRINGER 22 AT FRAME WINDOW AREA BETWEEN STA 1920 TO 1940. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01.
Part: SKIN — CORRODED (BS 1372-1394)
CORROSION ON THE SKIN UNDER SEALING AT WINDOW FRAME AREA AT STRINGER 21 AND SHEARED RIVET ON ANCHOR NUT BETWEEN STRINGER 24 TO 25 AND BETW STA 1372 TO 1394 RT SIDE. CORROSION REMOVED AREA TREATED PER SRM 51-10-01 AND 51-30-02.
Part: STRINGER — CORRODED (BS 1394-1416)
CORROSION ON STRINGER 22 UNDER SEALING AT WINDOW FRAME AREA BETWEEN STA 1394 TO 1416 RT SIDE. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01.
Part: STRINGER — CORRODED (BS 1800-1820)
CORROSION ON STRINGER 20 ABOVE PASSENGER WINDOW BETWEEN STA 1800 TO 1820 RT SIDE. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01.
Part: SKIN — CORRODED (BS 1520-1540)
SURFACE CORROSION ON THE SKIN AND ON ANCHOR NUT BETWEEN STA 1520 TO 1540 LT SIDE AND BETWEEN STRINGER 24 TO 25. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01.
Part: SKIN — CORRODED (BS 780-1000)
SURFACE CORROSION ON THE SKIN BETWEEN STA 780 TO 1000 RT SIDE AND BETWEEN STRINGER 12 TO 18. CORROSION REMOVED AND TREATED PER SRM 51-10-01.
Part: STOP — CORRODED (NR 3R DOOR)
NR 3R ENTRY DOOR SURFACE CORROSION ON DOOR STOPS. CLEANED PER MM 51-21-00.
Part: TIE CLIPS — CORRODED (BS 1920)
CORROSION ON TIE CLIPS AT STA 1920 COND STRINGER 3, 11 RT. CORROSION REMOVED PER SRM 51-10-01, FOUND WITHIN THE LIMITS PER SRM 53-10-01.
Part: FRAME — CORRODED (BS 1600)
CORROSION FRAME LWR CHORD AT STA 1600 ABOVE STR 11, 12. CORROSION BLENDED OUT PER SRM 51-10-01 AND 51-10-02.
Part: HOUSING — CORRODED (LT AILERON)
CORROSION LT INBOARD AILERON POWER CONTROL PACKAGE HOUSING SURFACE. CORROSION REMOVED FROM SURFACE PER SRM 51-10-01.
Part: SUPPORT — CORRODED (FUSELAGE)
CORROSION ON BRACKETS ABOVE FAIRING SUPPORT LWR FUS LT SIDE AT AREA LBL 20 TO LBL 60. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01.
Part: SKIN — CORRODED (BS 580-600)
CORROSION ON THE SKIN UNDER SEALING AT STRINGER 23 BETWEEN STA 580 TO 600. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01.
Part: STRINGER — CORRODED (BS 1880-1900)
CORROSION ON STRINGER 7 RT BETWEEN STA 1880 TO 1900. CORROSION REMOVED PER SRM 51-10-01, FOUND WITHIN THE LIMITS PER SRM 53-10-01.
Part: SKIN — CORRODED (BS 1740-1496)
SURFACE CORROSION ON THE SKIN BETWEEN STA 1740 TO 1496 AND BETWEEN STRINGER 19 TO 12. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01.
Part: ANGLE — CRACKED (LT AILERON)
LT INBOARD AILERON L/E ANGLE INBOARD TO INBOARD HINGE CRACKED. FAB NEW ANGLE PER SRM 57-12-00 AND INSTALLED PER SRM 51-30-02.
Part: STRINGER — CORRODED (BS 1820)
CORROSION ON FRAME AT STA 1820 NEAR STRINGER 7 RT. CORROSION REMOVED PER SRM 51-10-01, FOUND WITHIN THE LIMITS PER SRM 53-10-01.
Part: SUPPORT — CORRODED (BS 1060)
CORROSION ON FAIRING SUPPORT LWR FUS AT STA 1060 BETWEEN AREA RBL TO LBL 105. FAB NEW SUPPORT FAIRING PER SRM 51-40-04.
Part: STRINGER — CORRODED (BS 1080)
CORROSION ON STRINGER 1 RT AT STA 1080. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01.
Part: BEAM — CORRODED (RT MLG)
RIGHT BODY LANDING GEAR WHEEL WELL AFTER REMOVAL OF SPLICE PLATES CORROSION FOUND ON L/G BEAM LWR CHORD HORIZ FLANGE. ALSO, SCRATCHES EXIST ON FLANGE AFT EDGE. CORROSION AND DAMAGE REMOVED PER SB53-2310.
Part: ANGLE — CORRODED (BS 2280-2360)
CORROSION AND LOOSE CLIPS ON FLOOR ANGLE BETWEEN STA 2280 TO 2360 LT SIDE. CLEANED CORROSION AND TREATED PER SRM 51-10-01 AND 51-30-02.
Part: ANGLE — BROKEN (BS 1660)
BROKEN ANGLE AND MISSING COLLAR ON HI-LOCK RIVET AT FRAME NEAR STA 1660 LT SIDE AT STRINGER 15 AREA. INSTALLED NEW ANGLE AND RIVETED PER SRM 51-30-02.
Part: STRINGER — CORRODED (BS 1960)
CORROSION ON REINFORCEMENT DBL AT STA 1960 RT SIDE BETW STRINGER 17 TO 18 INCLUDING CORRODED ON STRINGER 17. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01.
Part: STRINGER — CORRODED (BS 1220-1240)
CORROSION ON STRINGER 4 LT BETWEEN STA 1220 TO 1240. REPAIRED STRINGER PER SRM 53-10-03.
Part: FASTENERS — CORRODED (BS 1000)
CORROSION ON HEAD OF HI-LOCK RIVET, ON SPLICE STRINGER 3R, 3L AT STA 1000. CORROSION RIVETS REMOVED AND INSTALLED NEW HI-LOCKS PER SRM 51-30-02.
Part: HI-LOCK RIVET — CORRODED (FUSELAGE)
CORROSION ON HEAD OF HI-LOCK AND OPEN HOLE AT STA 1700 BETWEEN STRINGER 3 TO 5. CORROSION RIVETS TAKEN OUT AND OPEN HOLE AREA INSTALLED NEW HI-LOCKS PER SRM 51-30-02 OBTAINED FROM STA STOCK.
Part: FRAME — CRACKING (BS 2100)
CRACK ON STA 2100 RT SIDE BETWEEN STRINGER 22 TO 23. PERFORMED REPAIR ON FRAME PER SRM 51-40-03.
Part: CHORD — CORRODED (BS 1480)
CORROSION ON UPPER CHORD STA 1480, UNDER MAIN DECK FLOOR BETWEEN AREA LBL TO RBL 25. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01.
Part: STRINGER — CORRODED (BS 2220)
CORROSION ON STRINGER 7 RT AT STA 2220. CORROSION REMOVED PER SRM 51-10-01, FOUND WITHIN LIMITS PER SRM 53-10-01.
Part: SKIN — CORRODED (BS 1820-1840)
CORROSION ON THE SKIN BETWEEN STA 1820 TO 1840 RT SIDE AND BETWEEN STRINGER 45 TO 46. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01.
Part: SKIN — CORRODED (BS 2040-2360)
SURFACE CORROSION ON FUS SKIN RT SIDE BETWEEN STA 2040 TO 2360 AT STRINGER 12 AREA. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01.
Part: STRINGER — CORRODED (BS 1680-1700)
CORROSION ON STRINGER 42 BETWEEN STA 1680 TO 1700 LT SIDE. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01, FOUND WITHIN LIMITS PER SRM 53-10-01.
Part: TIE CLIP — CORRODED (BS 1920)
CORROSION ON TIE CLIP AT STA 1920 BETWEEN STRINGER 2 TO 3. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01.
Part: FRAME — CORRODED (BS 1241)
CORROSION ON FRAME AT STA 1241 NEAR STRINGER 1 LT. CORROSION BLENDED OUT, SURFACE SMOOTHED PER SRM 51-10-01 AND 51-10-02.
Part: SKIN — DAMAGED (BS 660-680)
TORN, HITS, SCRATCHES AND DENT ON FUSELAGE SKIN RT SIDE BETWEEN STA 660 TO 680 BETWEEN STRINGER 34 TO 39. PERFORMED REPAIRS PER SRM 51-10-01.
Part: SKIN — CORRODED (BS 1420-1400)
CORROSION ON INTERNAL SKIN BETWEEN STA 1420 TO 1400 AND BETWEEN STRINGER 1 TO 4 LT. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01.
Part: FLOORBEAM — CORRODED (BS 2360)
CORROSION INBOARD CHORD STA 2360 BETWEEN STRINGER 45 RT TO 45 LT. CORROSION REMOVED AND TREATED PER SRM 51-10-01.
Part: GUTTER — CRACKED (BS 2280-2300)
CRACK AND BENT ON GUTTER AT FUSELAGE LT SIDE ABOVE PASSENGER DOOR 5 BETWEEN STA 228 TO 2300. CRACK BLENDED OUT, CHECKED AND FOUND OK PER SRM 53-10-01.
Part: SUPPORT — CORRODED (BS 1180)
CORROSION FAIRING SUPPORT LWR FUS STA 1180 BETWEEN AREA RBL TO LBL 58. REPAIRED PER SRM 53-50-04.
Part: ANGLE — BROKEN (BS 1480-1500)
BROKEN KYDEX SUPPORT ANGLE ON LT SIDE WALL BETWEEN STA 1480 TO 1500 ABOVE STRINGER 34. NEW KYDEX SUPPORT INSTALLED PER SRM 51-40-03.
Part: FLOOR — CRACKED (BS 780)
CRACK ON FLOOR SHEET METAL AT STRINGER 26 AREA NEAR STA 780 RT SIDE. FAB NEW PART PER SRM 53-10-21 AND 51-30-02.
Part: FLOORBEAM — CORRODED (BS 1700)
CORROSION ON UPPER CHORD FLOORBEAM AT STA 1700 BETWEEN AREA RBL 35 TO 45. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01.
Part: TIE CLIPS — CRACKED (BS 1660)
SMALL CRACK AND BENT ON CLIPS AT STA 1660 LT SIDE BETWEEN STRINGER 35 TO 37. AREA REPAIRED PER SRM 51-40-04.
Part: STRINGER — CORRODED (BS 1260-1320)
CORROSION ON STRINGER 1 BETWEEN STA 1260 TO 1320 LT. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01.
Part: HINGE CUTOUT — CRACKED (RT AILERON)
RT OUTBD AILERON OUTBD HINGE UPPER CUTOUT CRACKED. CUTOUT REWORKED PER SRM 57-10-01, DAMAGE WITHIN THE LIMIT PER SRM 57-10-01.
Part: SKIN — CORRODED (BS 1960)
SURFACE CORROSION ON FUS SKIN RT SIDE STA 1960 AT STRINGER 12 AREA. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01.
Part: INTERCOSTAL — CORRODED (BS 2120-2140)
CORROSION, HIT AND RIVETS IMPROPERLY DRIVEN ON INTERCOSTAL AT STRINGER 36 BETWEEN STA 2120 TO 2140. CORROSION REMOVED AND TREATED PER SRM 51-10-01, DAMAGE BLENDED OUT PER SRM 51-40-01 AND NEW RIVET INSTALLED PER SRM 51-30-02.
Part: STRINGER — CORRODED (BS 1440)
CORROSION ON STRINGER 10 LT AND ON FRAME STA 1440. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01.
Part: PANEL — TORN (CARGO DOOR)
FORWARD CARGO COMPARTMENT DOOR LIFT MANUAL MECH PANEL IS TORN. MANUFACTURED AND INSTALLED NEW PANEL AS ORIGINAL MATERIAL OBTAINED FROM STA STOCK BNR09842-96.
Part: FRAME — CORRODED (BS 1500)
CORROSION ON FRAME AT STA 1500 NEAR STRINGER 3 LT. CORROSION REMOVED AREA TREATED PER SRM 51-10-01.
Part: SKIN — DENTED (BS 2300-2320)
DENT ON FUS SKIN LT SIDE BETWEEN STA 2300 TO 2320 AND BETWEEN STRINGER 15 TO 16. REWORKED PER SRM 51-40-01 AND 53-30-01.
Part: SKIN — CORRODED (BS 140-160)
CORROSION ON HEAD FASTENERS AT FUS SKIN ABOVE AND UNDER PASSENGER WINDOW LT BETWEEN STA 140 TO 160 AND RT SIDE. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01.
Part: STRINGER — CRACKED (BS 460)
FOUND 2 CRACKS IN AFT ROW STA 460 BETWEEN STRINGER 14E AND 15 RT. REPAIRED IAW SB53-2289.
Part: FLOOR — CORRODED (BS 860-880)
HITS AND CORROSION ON SHEET METAL FLOOR COVER BETWEEN STA 860 TO 880 BETWEEN AREA LBL TO RBL 58. AREA SMOOTHED, CORROSION REMOVED AND TREATED PER SRM 51-10-01.
Part: SKIN — CORRODED (BS 1680-1700)
CORROSION ON THE SKIN BETWEEN STRINGER 48 TO 49 AND BETWEEN STA 1680 TO 1700 RT SIDE. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01.
Part: SUPPORT — CORRODED (BS 1540)
CORROSION AND BENT ON FAIRING SUPPORT AT LWR FUS STA 1540 BETWEEN AREA LBL 1000 TO RBL 100. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01.
Part: FAIRING — CORRODED (BS 1120-1140)
CORROSION FAIRING SUPPORT LWR FUS BETWEEN AREA RBL TO LBL 58 AND BETWEEN STA 1120 TO 1140. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01.
Part: FRAME — CORRODED (BS 1860)
CORROSION ON FRAME LWR CHORD AT STA 1860 NEAR STRINGER 7. CORROSION REMOVED PER SRM 51-10-01, FOUND WITHIN THE LIMITS PER SRM 53-10-01.
Part: STRINGER — CORRODED (BS 1620)
CORROSION ON STRINGER 1 AT STA 1620. REPAIRED PER SRM 53-10-03.
Part: STRINGER — CORRODED (BS 1760)
CORROSION ON STRINGER 11 RT AT STA 1760 AND ON HEAD OF HI-LOCK AT STRINGER 1 LT TO 2 RT. CORRISION REMOVED AND TREATED PER SRM 51-10-01 AND 51-30-02.
Part: TRACK — CORRODED (NR 3 TE FLAP)
TRACK NR 3 IS CORRODED AT BEARING MOVING PATHES. SURFACE CORROSION REMOVED PER SRM 51-10-01.
Part: STRINGER — CORRODED (BS 1740)
CORROSION ON STRINGER 13 NEAR STA 1740 RT SIDE. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01.
Part: RIB — DAMAGED (RT TE MID FLAP)
RT INBOARD MID FLAP, L/E END RIB INBOARD OF INBOARD FLAP CARRIAGE ASSY HAS DENT AND DAMAGE. STRAIGHTEN DENT PER SRM 51-40-01, SMOOTHED AND TREATED PER SRM 51-10-02.
Part: WEB — TORN (BS 1880)
TEAR ON THE WEB AT STA 1880 RT SIDE UNDER UPPER CHORD ABOVE STRINGER 48 TO 49. AREA REPAIRED PER SRM 51-40-02.
Part: SKIN — DENTED (NLG DOOR)
NOSE LANDING GEAR W/W RT FWD DOOR HAS DENTS ON INNER SKIN SURFACE. REPAIRED PER SRM 53-10-23 AND 51-30-02.
Part: INTERCOSTAL — DAMAGED (BS 1580-1600)
BENT ON FLOOR INTERCOSTAL BETWEEN STA 1580 TO 1600 AT RBL 28 AREA. DAMAGE BLENDED OUT AND AREA TREATED PER SRM 51-10-01 AND SRM 51-40-01.
Part: SUPPORT — CORRODED (BS 1160)
CORROSION FAIRING SUPPORT LWR FUS AT RBL 62 AREA STA 1160. CORROSION BLENDED OUT SURFACE, SMOOTH PER SRM 51-10-01 AND 51-40-03.
Part: RESTRAINT — DAMAGED (CARGO COMPT)
FWD CARGO COMPARTMENT FIXED RESTRAINT DAMAGED AT STA 780R. RESTRAINT REPLACED AS PER MM 25-50-00.
Part: CARRIAGE — CORRODED (TE FLAPS)
WING FLAP CARRIAGES 8 BOOGIES SURFACE CORROSION. REMOVED SURFACE CORROSION PER SRM 51-10-01 AND PROTECTION ACTION CARRIED OUT.
Part: STRINGER — CORRODED (BS 1960)
CORROSION ON STRINGER 12 NEAR STA 1960 RT SIDE. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01.
Part: CHORD — CRACKED (BS 1800)
CRACK WITH STOP HOLES ON UPPER CHORD STA 1800 LT SIDE ABOVE STRINGER 42. REPAIRED PER SRM 53-10-04 AND 51-30-02.
Part: TIE CLIP — CORRODED (BS 1940)
CORROSION ON TIE CLIP AT STA 1940 NEAR STRINGER 1 RT. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01.
Part: WATER DRAIN — CRACKED (BS 1100)
AIR COND BAY RT WATER DRAIN TUBE IS CRACKED ON TWO LOCATION AT B STA 1100R APPROX WATER DRAIN TUBE. REPLACED PER MM 21-10-00.
Part: TIP FAIRING — DAMAGED (RT HORIZ STAB)
RT STABILIZERS T/E TIP IS TORN. INSTALLED NEW FAIRING TIP (P/N 65B03521-34) AND RIVETED PER SRM 51-30-02.
Part: FLOORBEAM — CORRODED (BS 920)
CORROSION ON UPPER CHORD FLOORBEAM AT STA 920 BETWEEN AREA LBL AND RBL 32 TO 45. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01.
Part: SKIN — DENTED (BS 800)
HIT ON PANEL NEAR DOOR 2 UNDER COVER HINGE LWR BETWEEN STA 800 TO 820 LT. SMOOTHED AREA AND TREATED PER SRM 51-10-01.
Part: STRUCTURE — CORRODED (AC COMPT)
CORROSION ON LT AIR CONDITION DOOR SUPPORT STRUCTURE STA 1040. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01.
Part: STRINGER — CORRODED (BS 1520)
CORROSION TIE CLIP AT STA 1520 NEAR STRINGER 2 RT. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01.
Part: CLIP — BROKEN (BS 1800)
BROKEN CLIP ON STA 1800 LT SIDE BETWEEN STRINGER 36 TO 37. NEW CLIP INST PER SRM 51-40-04.
Part: FASTENERS — CORRODED (BS 1560-1620)
CORROSION ON HEAD OF HI-LOCK AT STA 1560 TO 1620 BETWEEN STRINGER 5 LT AND 5 RT. CORRODED RIVETS TAKEN OUT AND INSTALLED NEW HI-LOCKS PER SRM 51-30-02.
Part: RIVETS — FAILED (BS 1680-1720)
SHEARED RIVETS ON CONNECTION FITTING TO LWR ENTRY DOOR FRAME NR 4 AT AREA STA 1680 AND 1720. INSTALLED NEW RIVETS PER SRM 51-30-02.
Part: FASTENERS — CORRODED (BS 1780)
CORROSION ON HEAD HI-LOCK AT STA 1780 BETWEEN STRINGER 2 TO 5 LT. CORRODED RIVETS TAKEN OUT AND INSTALLED NEW FASTENERS PER SRM 51-30-02.
Part: SUPPORT — CORRODED (BS 880)
FOUND LEVEL 2 CORROSION ON FAIRING SUPPORT AT LOWER FUS STA 880 BETWEEN BL 0 TO LBL 15. REPAIRED IAW SRM 53-50-04. CPCP BASE LINE INSPECTION.
Part: SKIRT — CHAFED (NR 1 PYLON)
SKIRT NR 1 FWD BRIDGE ABOVE PRESS MODULE CHAFED. SMOOTHED CHAFED AND AREA TREATED PER SRM 51-40-03.
Part: SKIRT CLAMP — BROKEN (NR 4 PYLON)
SKIRT NR 4 CLAMP UNDER RETURN LINE BROKEN. CLAMP REPLACED PER MM 20-11-24.
Part: PANEL — DENTED (BS 540-560)
FOUND DISTORTION ON PANEL AT FUS SKIN RT BETWEEN STA 540 AND 560 AND BETWEEN STRINGERS 35 TO 36. STRAIGHTENED AND SMOOTHED PANEL IAW SRM 51-40-01.
Part: TIE CLIPS — CORRODED (BS 1940)
FOUND CORROSION ON TIE CLIPS STATION 1940 RT SIDE AT STRINGERS 28, 29, 30, 31, 32. REMOVED LEVEL ONE CORROSION AND TREATED IAW SRM 51-10-01. CORROSION FOUND TO BE WITHIN LIMITS OF SRM 53-10-01.
Part: SUPPORT — CORRODED (BS 840)
FOUND CORROSION ON FAIRING SUPPORT AT LOWER FUSELAGE STATION 840 BETWEEN AREA LBL 15 TO RBL 30 AND SHEARED RIVET AT AREA. REMOVED LEVEL ONE CORROSION FROM FAIRING SUPPORT IAW SRM 51-10-01. CORROSION FOUND TO BE WITHIN LIMITS OF SRM 53-10-01.
Part: SUPPORT — CORRODED (BS 1540)
FOUND LEVEL ONE CORROSION ON FAIRING SUPPORT AT FUSELAGE LT SIDE STATION 1540 BETWEEN STR AREA 28 TO 37. REMOVED CORROSION IAW SRM 51-10-01 AND INSTALLED NEW ANCHOR NUT IAW SRM 51-30-02.
Part: SKIN — CORRODED (BS 1700)
FOUND LEVEL ONE CORROSION AND PROTRUDING HI-LOCK ON FUSELAGE SKIN RT SIDE AT STR 40 AREA STA 1700. REMOVED CORROSION FROM SKIN IAW SRM 51-10-01. INSTALLED NEW HI-LOCK AND RIVET IAW SRM 51-30-02.
Part: HYD FITTING — CORRODED (NR 4 PYLON)
FOUND CORRODED HYDRAULIC FITTINGS IN WING BY NR 4 PYLON. LEVEL ONE CORROSION REMOVED AND TREATED AS PER MM 51-21-03.
Part: DOOR — CORRODED (NR 2R DOOR)
NR 2R ENTRY DOOR SURFACE CORROSION ON DOOR STOPS. CORROSION REMOVED AND TREATED PER MM 51-21-03.
Part: SKIN — CORRODED (WS 294.62)
FOUND LEVEL ONE CORROSION ON UPPER SKIN NEAR FRONT SPAR AT ROOT AREA, WING TO FUSELAGE STA WS 294.62. CORROSION REMOVED AND TREATED AS PER SRM 51-10-01, FOUND WITHIN LIMITS OF SRM 57-30-01.
Part: BRACKET — CORRODED (BS 1660)
FOUND LEVEL ONE CORROSION ON BRACKET AND AROUND GROUNDING BOLT AT FAIRING SUPPORT, FUSELAGE RT SIDE STA 1660, BETWEEN STR 44 TO 45. REMOVED CORROSION IAW SRM 51-10-01, INSTALLED HI-LOCK IAW SRM 51-30-02.
Part: SUPPORT — CORRODED (BS 1540)
FOUND LEVEL ONE CORROSION ON FAIRING SUPPORT AT FS RT SIDE STA 1540 BETWEEN STR AREA 33 TO 36. REMOVED CORROSION IAW SRM 51-10-01. FOUND WITHIN LIMITS OF SRM 53-10-01.
Part: DOOR — CORRODED (NR 2L DOOR)
NR 2L ENTRY DOOR 2 CORROSION SCREWS ON OUTER DOOR HANDLE. CORROSION REMOVED AND TREATED PER MM 51-21-03.
Part: SUPPORT — CORRODED (BS 1580)
FOUND LEVEL ONE CORROSION ON FAIRING SUPPORT AT FUSELAGE LT SIDE STAION 1580 BETWEEN STR AREA 29 TO 40. REMOVED CORROSION IAW SRM 51-10-01 AND INSTALLED NEW ANCHOR NUT IAW SRM 51-30-02.
Part: BRACKET — CRACKED (LT WING)
LEFT WING NR 2 DIAGONAL FITTING BRACKET AT RIGHT SIDE IS CRACKED. FABRICATED NEW BRACKET AND INSTALLED AS PER SRM 51-20-01 AND 51-30-02.
Part: BRACKET — BROKEN (NR 2 PYLON)
FOUND BROKEN BRACKET AT BAY CUTOUT ABOVE PYLON NR 2. NEW BRACKET AND FASTENERS INSTALLED AS PER SRM 51-30-02.
Part: SKIN — CORRODED (WS 1340)
FOUND SWELLING ON UPPER WING SKIN WS 1340 IN FRONT SPAR AREA. REMOVED FASTENERS, LEVEL ONE CORROSION PER 51-10-01 AND FOUND WITHIN LIMITS OF SRM 57-30-01. REPAIRED PANEL IAW SRM 51-40-09.
Part: PANEL — CORRODED (WS 353)
FOUND CORROSION ON UPPER SKIN LEFT WING AT STRINGER 3, ROOT AREA CONNECTION WING TO FUSELAGE, WS 353.02. LEVEL ONE CORROSION REMOVED AND AREA TREATED AS PER SRM 51-10-01, FOUND WITHIN LIMITS OF SRM 57-10-01.
Part: WEB — CORRODED (FUSELAGE)
FOUND TWO AREAS ON THE WEB WITH CORROSION. CORROSION REMOVED, CHECKED AND FOUND LOSS OF 7 PERCENT OF MATERIAL ONLY PER SRM 57-10-01.
Part: SPAR — CRACKED (WS 669)
FOUND CRACK ON UPPER CHORD AT STATION 669 NEAR THE FRONT SPAR. REMOVED AND REPLACED CHORD IAW SB 57-2273.
Part: SKIN — CORRODED (WS 750)
FOUND SWELLING ON UPPER WING SKIN WS 750 IN FRONT SPAR AREA. REMOVED FASTENERS, LEVEL ONE CORROSION IAW SRM 51-10-01 AND FOUND WITHIN LIMITS OF SRM 57-30-01. REPAIRED PANEL IAW SRM 51-40-09.
Part: SKIN — CORRODED (BS 2180)
FOUND SURFACE CORROSION ON LOWER FUSELAGE SKIN AT STA 2180 BETWEEN STR 46 RT TO 46 LT. REMOVED LEVEL ONE CORROSION FROM SKIN, TREATED AREA IAW SRM 51-10-01. CORROSION FOUND WITHIN LIMITS OF SRM 53-10-01.
Part: STRINGER — CORRODED (BS 1980-2000)
FOUND CORROSION ON STRINGER 42 BETWEEN STA 1980 TO 2000 RT SIDE. REMOVED LEVEL ONE CORROSION AND TREATED AREA AS PER SRM 51-10-01. CORROSION FOUND TO BE WITHIN LIMITS OF SRM 53-10-01.
Part: STRINGER — CORRODED (BS 1940-1960)
FOUND CORROSION ON STRINGER 51 BETWEEN STA 1940 TO 1960 RT SIDE. REMOVED LEVEL ONE CORROSION AND TREATED AREA IAW SRM 51-10-01. CORROSION FOUND TO BE WITHIN LIMITS OF SRM 53-10-01.
Part: BRACKET — CHAFED (NR 2 PYLON)
FOUND TRIANGLE BRACKET UNDER NR 2 PYLON AFT FAIRING CHAFED. INSTALLED NEW BRACKET WITH RIVET AS PER SRM 51-30-02.
Part: SKIN — DENTED (BS 720-820)
FOUND DENTS, SCRATCHES AND CORROSION ON HEAD OF RIVETS AT FUS SKIN BETWEEN STA 720 TO 820, BETWEEN STRINGERS 26 TO 28 LT. STRAIGHTENED AND SMOOTHED PANEL, REMOVED LEVEL ONE CORROSION IAW SRM 51-10-01. CORROSION WITHIN LIMITS OF SRM 53-10-01.
Part: ROD — CORRODED (NR 3 PYLON)
FOUND CORRODED ROD BEHIND HYDRAULIC TANK IN WING NEAR ATTACH TO NR 3 PYLON. LEVEL ONE CORROSION REMOVED AND TREATED AS PER MM 51-21-03.
Part: FITTING — CORRODED (NR 3 PYLON)
FOUND HYDRAULIC FITTINGS CORRODED IN WING NEAR ATTACHMENT TO NR 3 PYLON. LEVEL ONE CORROSION REMOVED AND TREATED AS PER MM 51-21-01.
Part: SKIN — CORRODED (WS 1270)
FOUND SWELLING ON UPPER WING SKIN STA WS 1270 IN FRONT SPAR AREA. REMOVED FASTENERS, LEVEL ONE CORROSION IAW 51-10-01 AND FOUND WITHIN LIMITS OF SRM 57-30-01. REPAIRED PANEL IAW SRM 51-40-09.
Part: SKIN — CORRODED (WS 800)
FOUND SWELLING ON UPPER WING SKIN WS 800 IN FRONT SPAR AREA. REMOVED FASTENERS, LEVEL ONE CORROSION IAW SRM 51-10-01 AND FOUND WITHIN LIMITS OF SRM 57-30-01. REPAIRED IAW SRM 51-40-09.
Part: SKIN — CORRODED (WS 580)
FOUND LEVEL ONE CORROSION ON UPPER WING SKIN STA 580 IN MID SPAR AREA. REMOVED CORROSION IAW SRM 51-10-01, FOUND WITHIN LIMITS OF SRM 57-30-01. TREATED AREA IAW SRM 51-10-02.
Part: ACCESS PANEL — CRACKED (RT WING)
FOUND CRACKED ACCESS PANEL AND ATTACH ANGLE IN WING L/E TO INBOARD RIB IN NR 4 PYLON CAVITY. REPAIRED IAW SRM 51-40-03 AND SRM 51-40-02.
Part: BRACKET — CHAFED (RT WING)
FOUND LEFTHAND FORWARD MOUNTING BRACKET CHAFED AND ONE ANCHOR NUT MISSING NEAR NR 4 PYLON. FABRICATED NEW BRACKET AND INSTALLED BRACKET AND ANCHOR NUT IAW SRM 51-30-02.
Part: SUPPORT — CORRODED (BS 1480)
FOUND LEVEL ONE CORROSION ON CENTER FAIRING SUPPORT AT LOWER FUSELAGE BETWEEN STATIONS 1480 TO 1660. REMOVED CORROSION IAW SRM 51-10-01 AND INSTALLED NEW ANCHOR NUT IAW SRM 51-30-02.
Part: BRACKET — CORRODED (BS 920-960)
FOUND LEVEL ONE CORROSION ON SUPPORT BRACKET AT CENTER LOWER FUSELAGE BETWEEN STA 920 TO 960. REMOVED CORROSION AND TREATED AREA IAW SRM 51-10-01. REPAIRED IAW SRM 51-40-03.
Part: STRINGER — CORRODED (BS 1920)
FOUND LEVEL ONE CORROSION ON STRINGER 47 NEAR STATION 1920 RT SIDE. REMOVED CORROSION AND TREATED AREA IAW SRM 51-10-01.
Part: SKIN — CORRODED (WS 1020)
FOUND SWELLING ON UPPER WING AT WS 1020 IN FRONT SPAR AREA. REMOVED FASTENERS, LEVEL ONE CORROSION IAW SRM 51-10-01 AND FOUND WITHIN LIMITS OF SRM 57-30-01. REPAIRED IAW SRM 51-40-09.
Part: SUPPORT — CORRODED (BS 1580)
FOUND LEVEL ONE CORROSION ON FAIRING SUPPORT AT LOWER FS 1580 BETWEEN AREA RBL 100 TO LBL 100. REMOVED CORROSION IAW SRM 51-10-01. FOUND WITHIN THE LIMITS OF SRM 53-10-01.
Part: ANGLE — CRACKED (WS 670)
FOUND CRACK ON SUPPORT ANGLE AT WS 670 AT ATTACHMENT OF FRONT SPAR. NEW ANGLE INSTALLED PER SB 57-2159.
Part: SKIN — CORRODED (WS 1340-1380)
FOUND SWELLING AND PROTRUDING RIVET ON UPPER WING SKIN, STA 1340 TO 1380 IN FRONT SPAR AREA. REMOVED FASTENERS, LEVEL ONE CORROSION IAW SRM 51-10-01 AND FOUND WITHIN LIMITS OF SRM 57-30-01. REPAIRED PANEL IAW SRM 51-40-09.
Part: SKIN — CORRODED (WS 1230)
FOUND SWELLING ON UPPER WING WS 1230 IN FRONT SPAR AREA. REMOVED FASTENERS, LEVEL ONE CORROSION IAW SRM 51-10-01 AND FOUND WITHIN LIMITS OF SRM 57-30-01. REPAIRED IAW SRM 57-30-01.
Part: MOUNT BOLTS — CORRODED (L2 DOOR)
LEVEL 1 CORROSION ON MOUNT BOLTS NR 2 ENTRY DOOR. REMOVED AND TREATED CORROSION PER BOEING SRM 51-21-03.
Part: SKIRT — CORRODED (NR 4 PYLON)
SKIRT NR 4 SUPPORT RODS EYEBOLTS CORROSION. CORROSION REMOVED AND TREATED PER MM 51-21-03.
Part: CLIP — BROKEN (BS 2020)
BROKEN CLIP ON STA 2020 LT SIDE ABOVE STRINGER 40 TO 41. NEW ANGLE CLIP INSTALLED PER SRM 51-40-03 AND RIVET PER SRM 51-30-02.
Earlier reports · 1995 · 26 reports
1995
Part: ENGINE — FAILED (NR 1)
NR 1 ENGINE STALL WHILE CLIMBING FROM 34.0 TO 35.0. ALL PARAMETERS SLOW AFTER STALL, EGT DID NOT EXCEED 760 DEGREES. ON LANDING IN KHV, FOUND METAL IN TAILPIPE. ENGINE TO BE CHANGED IAW POLAR WORK CARDS M7100-002 AND M7100-002A.
Part: SEAT TRACK — BROKEN (F/O'S SEAT)
ON TAKEOFF FROM CHICAGO, F/O'S LEFT AFT SEAT TRACK BROKE. ALSO, UPON ARRIVAL AT ANCHORAGE, MAINTENANCE DISCOVERED RIGHT FWD TRACK CRACKED. REPLACED BOTH SEAT TRACK ASSEMBLIES, PART NR 812168-8 AND 811371-412, IAW MM 25-11-01.
Part: OVERHEAT SWITCH — DEFECTIVE (NR 4 HYD SYSTEM)
DURING TAXI, NR 4 HYDRAULIC OVERHEAT LIGHT ILLUMINATED NR 4 SYSTEM. REMOVED AND REPLACED NR 4 HYDRAULIC OVERHEAT SWITCH IAW MM 29-41-00.
Part: CLEVIS ASSY — CRACKED (LT MLG)
LANDING GEAR DOOR FITTING BROKEN AND CRACKED. REMOVED AND REPLACED CLEVIS ASSEMBLY ON LEFT HAND MAIN BODY GEAR OUTBOARD DOOR IAW MM 20-11-27.
Part: LINER — CRACKED (APU)
CRACKED APU EXHAUST PIPE INNER LINER. REMOVED AND REPLACED LINER IAW MM 49-81-03.
Part: TE SKIN — DEBONDED (LT ELEVATOR)
DEBONDED ELEVATOR, LEFT HAND INBOARD ELEV TRAILING EDGE. REPAIRED WITH POTTING COMPOUND AND FIBERGLASS OVERLAY IAW SRM 51-41-00. PRIMED AND PAINTED IAW SRM 51-24-11.
Part: FAN COWL — DELAMINATED (NR 2 ENGINE)
DELAMINATION AND PUNCTURE OF NR 2 ENGINE RIGHT FAN COWL. REPAIRED IAW SRM 51-40-06.
Part: DRAIN PANEL — CORRODED (FWD LAV)
FOUND CORRODED WASHERS, WHICH ARE BULGING SKIN AT FORWARD LAV SERVICE PANEL DRAIN CUTOUT. REPLACED CORRODED WASHERS IAW SRM 51-10-01 AND REPAIRED PANEL IAW SRM 51-10-01.
Part: DOOR — PUNCTURED (LT MLG)
PUNCTURED LEFT HAND WING GEAR, LOWER OUTBOARD FLYING DOOR INNER SKIN. REPAIRED AND PAINTED AREA IAW SRM 51-40-15.
Part: FAIRING — BULGING (E/E DOOR)
BULGING FAIRING BEHIND CTR E AND E DOOR. REMOVED FAIRING AND FOUND SHIM MISSING. INSTALLED SHIM AND INSTALLED FAIRING IAW SRM 51-30-02.
Part: SKIN — CORRODED (E/E DOOR)
SURFACE CORROSION OF CENTER E AND E DOOR INNER SKIN. REMOVED SURFACE CORROSION WITH NEGLIGIBLE MATERIAL LOSS AND REPAIRED IAW 51-10-01.
Part: RADOME — DELAMINATED (NOSE)
NOSE RADOME HIT BY BIRD ON LANDING. THE TOP SECTION BS 114, 9 INCH DIAMETER OF DELAMINATION, NO BROKEN SKIN INSIDE OR OUT. ENGINEERING REVIEWED OK FOR FLIGHT TO MAINTENANCE BASE FOR RADOME REPLACEMENT.
Part: SENSOR — SHORTED (LT MLG)
ON TAXI OUT, CREW FOUND AUTOSPOILER LIGHT ILLUMINATED AND FOUND THE LANDING GEAR ALTERNATE CONTROL CIRCUIT BREAKER OPEN. RESET CIRCUIT BREAKER, 20 TO 30 SECONDS BREAKER OPENED. FOUND LEFT WING GEAR ALTERNATE DOWN AND LOCK SENSOR TO BE AT FAULT. DEACTIVATED PER MEL AND DISPATCHED AIRCRAFT.
Part: FIRE WARN — MALFUNCTIONED (WHEEL WELL)
ON CLIMB OUT, WHEELWELL FIRE LIGHT CAME ON, RETURNED TO SYD. TROUBLESHOT THE FIRE WARNING SYSTEM, UNABLE TO LOCATE POSITIVE CAUSE. NO AIR LEAKS PLACARDED, FIRE WARNING SYSTEM PER MEL 26-06.
Part: DUCT — BLOWN (APU)
PRIOR TO TAKEOFF, APPLIED POWER AND WHEELWELL FIRE WARNING LIGHT CAME ON. LIGHT WENT OUT WHEN RETURNED TO IDLE, RETURNED TO BLOCKS. ON LEAK CHECK BY MAINTENANCE, APU SUPPLY DUCT BURST. INSTALLED BLOCKING PLATE AND PLACARDED APU INOPERATIVE.
Part: SWITCH — OUT OF ADJUST (CARGO DOOR)
MAINTENANCE FERRY FLIGHT NR 832 OUT OF JFK (UNPRESSURIZED) LOWER AFT CARGO DOOR LIGHT CAME ON DURING CLIMB-OUT. RETURNED TO JFK. ADJUSTED VENT DOOR SWITCH.
Part: WHEEL — FAILED (NR 6 TIRE)
GRU - DURING TAKEOFF AT V1, MASTER FIRE WARNING LIGHTS AND WW FIRE WARNING ILLUMINATED. CONTINUED TAKEOFF. UNABLE TO RETRACT BODY GEAR AND WW DOOR WARNING LIGHT REMAINED ILLUMINATED, THEN THE NR 1 HYDRAULIC SYSTEM QUANTITY WARNING LIGHT CAME ON. AFTER FUEL JETTISON, RETURNED TO GRU. INITIAL GROUND INSPECTION REVEALED DAMAGE TO NR 1 HYDRAULIC SYSTEM PLUMBING, APU PNEUMATIC DUCT, LT BODY GEAR WW DOOR AND NR 6 ML6 TIRE BLOWN. REPLACED WHEEL AND TIRE ASSEMBLIES NR 6 AND NR 7, DAMAGED HYDRAULIC LINES, APU PNEUMATIC DUCT, WHEELWELL FIRE LOOP, BROKEN ROD AND REPAIRED DOOR. INSPECTED WHEELWELL PRESSURE WEB, NO DISCREPANCIES.
Part: TIRE CAP — DEPARTED (NR 6 WHEEL)
ON TAKEOFF, NR 6 TIRE CAP CAME OFF DAMAGING THE LEFT BODY GEAR DOOR FIXED ROD THE ROD DAMAGED NR 1 HYDRAULIC SYSTEM LINES (7 EACH), WHEEL WELL FIRE WARNING LOOP, AND APU PNEUMATIC DUCTING CAUSING LOSS OF NR 1 HYDRAULIC SYSTEM AND APU PNEUMATIC AIR. REPLACED DAMAGED LINES, WHEEL WELL FIRE LOOP, APU DUCT, DOOR ROD, AND WHEEL ASSEMBLY IN ACCORDANCE WITH BOEING MAINTENANCE MANUALS.
Part: DOOR — DELAMINATED (RT MLG)
RIGHT WING LOWER OUTBOARD STRUT DOOR DELAMINATED. REPAIRED IAW BOEING SRM 51-40-02. TOTAL CYCLES 18,464.
Part: DOOR — DELAMINATED (LT MLG)
LEFT WING LANDING GEAR LOWER OUTBOARD STRUT DOOR DELAMINATED. REPAIRED IAW WITH BOEING SRM 51-40-09. TOTAL CYCLES 18,464.
Part: LOCK ARM — CRACKED (CARGO DOOR)
AT JFK, WHILE OPENING MAIN DECK CARGO DOOR, FOUND NR 11 AND NR 12 DOOR LATCH LOCK ARMS CRACKED. REPLACED LOCK ARMS PER GATX MM 52-32-00. AIRCRAFT RELEASED FOR SERVICE.
Part: SKIN — CREASED (NR 4 LE FLAP)
DURING ROUTINE MAINTENANCE CHECK, GROUND DAMAGE OCCURRED TO THE FOLDING NOSE SKIN OF THE NR 4 LEADING EDGE VARIABLE CAMBER FLAP. FLAP REPAIRED PER 747 SRM 57-50-03. REPAIR DEVIATED FROM SRM. DER APPROVED REPAIR FOR 50 HOUR LIMIT. FOLDING NOSE ASSY REPLACED IN JFK ON 4-27-95. AIRCRAFT RELEASED FOR SERVICE.
Part: SKIN — DELAMINATED (LT ELEVATOR)
DURING SERVICE CHECK, FOUND OUTBOARD ELEVATOR UPPER SKIN DELAMINATED. REPAIRED PER SRM 51-40-09 FIG B-200 DEGREES WET LAYUP. REPAIR IS CLASSIFIED AS TIME LIMITED. PERMANENT REPAIR MUST BE ACCOMPLISHED PER SRM 51-40-12 AT NEXT C-CHECK NOT TO EXCEED 18 MONTHS. (M)
Part: STRINGER — CORRODED (BS 1595)
DURING INSPECTION/REPAIR PER AD 95-01-04, FOUND CORROSION STRINGER 4L AT BS 1595, LEVEL 2. REPLACED STRINGER SECTION PER BOEING SRM 53-10-3 FIGURE 5.
Part: STRINGER — CORRODED (BS 1539)
DURING INSPECTION/REPAIR PER AD 95-01-04, FOUND CORROSION BETWEEN FASTENER HOLES STRINGER 4L AT BS 1539. CLEANED CORROSION AND FOUND WITHIN LIMITS PER BOEING SRM 53-30-01 FIG 1 DETAIL 2, ALODINED AND PRIMED.
Part: SKIN — CORRODED (FUSELAGE)
DURING INSPECTION AND REPAIR PER AD 94-01-04, FOUND SEVERAL AREAS OF CORROSION IN THE UPPER AND LOWER LAP JOINTS AT STRINGER 4L. REMOVED LIGHT SURFACE CORROSION WITHIN LIMITS PER BOEING SRM 53-30-01 FIG 1 DETAIL 2, LEVEL 1.