N13088
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.
25 reports on file, 1998-02-09 – 2001-02-04.
Part: SPAR CAP — CRACKED (HORIZONTAL STAB) · airframe 94,902 hrs · 25,192 cycles
INSPECTION FOUND A .75 INCH CRACK AT AFT BARREL NUT HOLE OF UPPER AFT RT REAR SPAR CAP ON HORIZONTAL STABILIZER. THE SPAR CAP WAS REPAIRED IAW ECRA 5511-01041.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 94,899 hrs · 25,191 cycles
INSPECTION FOUND FLOOR SUPPORT ON RT SIDE OF FORWARD CARGO COMPARTMENT CORRODED AT STA 879. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 53-12-01.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 94,899 hrs · 25,191 cycles
INSPECTION FOUND LT AND RT FLOOR SUPPORT BEAMS CORRODED IN GALLEY G5 AREA AT STA 775-899, X = 40R AND AT X = 40L. THE FLOOR SUPPORT BEAMS WERE REMOVED AND NEW FLOOR SUPPORT BEAMS WERE INSTALLED IAW SRM 53-13-01 AND GMM 10-900-01.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 94,899 hrs · 25,191 cycles
INSPECTION FOUND GALLEY NR 7 I/B SUPPORT BEAM CORRODED AT STA Y = 1900-1997, X = 45R. A NEW BEAM WAS INSTALLED IAW SRM 53-16-01.
Part: STRUCTURE — CORRODED (BULKHEAD) · airframe 94,899 hrs · 25,191 cycles
INSPECTION FOUND REAR PRESSURE BULKHEAD T- SECTION CORRODED AT STA 2007, X = 24. THE T-SECTION WAS REPAIRED IAW SRM 53-40-00.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 94,899 hrs · 25,191 cycles
INSPECTION FOUND GALLEY NR 6 INBOARD FLOORBOARD SUPPORT CORRODED AT STA Y = 1887, X = 45L. THE SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW GMM 10-900-01 AND SRM 53-11-01.
Part: CHANNEL — CORRODED (FUSELAGE) · airframe 94,899 hrs · 25,191 cycles
INSPECTION FOUNFD TOP HAT SECTION AT STA 401-459, X = 30L (GALLEY G1) CORRODED. A NEW SECTION WAS INSTALLED IAW SRM 53-11-01.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 94,899 hrs · 25,191 cycles
INSPECTION FOUND I/B GALLEY NR 7 FLOORBOARD SUPPORT CORRODED AT STA Y = 1871, X = 30R. THE SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 53-16-01.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 94,899 hrs · 25,191 cycles
INSPECTION FOUND I/B CENTER FLOOR SUPPORT CORRODED AT STA 1887, X = -30L. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 53-16-01.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 94,899 hrs · 25,191 cycles
INSPECTION FOUND LAV C I/B FLOOR SUPPORT CORRODED AT STA Y = 840-899, X = 60L. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 53-13-01.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 94,899 hrs · 25,191 cycles
INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA Y = 475, X = -19 TO +19. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 53-11-01.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 94,899 hrs · 25,191 cycles
INSPECTION FOUND FLOORBEAM CORRODED AT STA 481. THE FLOORBEAM WAS REMOVED AND A NEW FLOORBEAM WAS INSTALLED IAW SRM 53-11-01.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 94,899 hrs · 25,191 cycles
INSPECTION FOUND LAV D I/B FLOOR SUPPORT CORRODED AT STA Y = 840-899, X = 60R. THE SUPPORT WAS REMOVED AND A NEW ONE WAS INSTALLED IAW SRM 53-16-01.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 94,899 hrs · 25,191 cycles
INSPECTION FOUND NR 3 GALLEY LEFT O/B AND RIGHT O/B SUPPORT BEAMS CORRODED AT STA 475-535, X = +23 AND AT X = -23. THE SUPPORT BEAMS WERE REMOVED AND NEW SUPPORT BEAMS WERE INSTALLED IAW SRM 53-11-01.
Earlier reports · 1998–1999 · 11 reports
1999
Part: SKIN — CRACKED (LT TE FLAP)
INSPECTION FOUND A 5 INCH CRACK ON UPPER SURFACE SKIN OF LT INBOARD FLAP. A REPAIR WAS INSTALLED IAW SRM 57-00-01, FIGURE 4, SHEET 2 AND ECRA 5752-01028.
1998
Part: ACTUATOR VALVE — LEAKING (RT SPOILER)
THE AIRCRAFT LOST HYDRAULIC QUANTITY ON SYSTEM NR 1 WHILE EN ROUTE. THE LOSS WAS ACCOMPANIED BY ILLUMINATION OF LOW PRESSURE LIGHTS. THE AIRCRAFT WAS APPROXIMATELY 20 MINUTES FROM MAN WHEN THE FLUID LOSS OCCURRED. FUEL WAS DUMPED AND THE AIRCRAFT WAS DIVERTED TO MAN WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE RT SPOILER DRIVE SERVO ACTUATOR/VALVE LEAKING. THE SPOILER DRIVE SERVO ACTUATOR/VALVE WAS REMOVED AND REPLACED IAW MM 27-61-05, PAGE 201. THE NR 1 HYDRAULIC SYSTEM WAS SERVICED TO FULL. LEAK AND OPERATIONAL CHECKS WERE GOOD.
Part: BATTERY CHARGER — INOPERATIVE (CABIN)
MAINTENANCE REPORTED THAT THE EMERGENCY LIGHT TEST WAS INOPERATIVE. THE BATTERY CHARGER AND PACK AT DOOR 3L WERE REMOVED AND REPLACED.
Part: TR PANEL — DELAMINATED (NR 2 ENGINE)
INSPECTION FOUND A 10 INCH AREA OF DELAMINATION AT NR 2 ENGINE LEFT THRUST REVERSER LOWER SIDEWALL PANEL (FAN AIR BYPASS AREA). THE C-DUCT ASSEMBLY WAS REPLACED IAW MM 78-32-11.
Part: PANEL — DAMAGED (RT HORZ STAB)
THE RT HORIZONTAL STABILIZER LEADING EDGE PANEL SUSTAINED DAMAGE ON FOUR CORNERS WHEN IT WAS DROPPED DURING REMOVAL. THE PANEL WAS REPAIRED IAW SRM 55-12-01 AND ECRA 5510-01390.
Part: RIVETS — SHEARED (NR 1 LE FLAP)
INSPECTION FOUND A ROW OF SHEARED RIVETS AND A BROKEN BRACKET ON LT WING NR 1 LEADING EDGE SLAT LOWER EDGE INBOARD SKIN SURFACE. REPAIR ANGLES WERE FABRICATED AND INSTALLED IAW SRM 51-21-01 AND 51-31-01.
Part: FITTING — CRACKED (VERT STAB)
INSPECTION FOUND A 0.160 INCH CRACK ON VERTICAL STABILIZER NR 4 BANJO FITTING. A REPAIR WAS PERFORMED IAW SRM 55-20-00, FIGURE2, PAGE 28-29 AND 55-20-00, FIGURE 7, PAGE 40.
Part: TRACK — HOLE (BS 1841)
INSPECTION FOUND A HOLE ON FLOOR TRACK IN AFT CARGO BILGE AREA AT STA 1841, RBL 25. A NEW SPLICE ANGLE AND STRAP WERE FABRICATED AND INSTALLED IAW MF MAN D10-53-86784.
Part: PANEL — CANNED (LT WING)
INSPECTION FOUND LT WING TOP SURFACE PANEL OUTBOARD OF INBOARD AILERON OIL CANNING. THE OIL CANNED AREA WAS TRIMMED AND BLENDED OUT. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-21-01 AND 51-31-01.
Part: FLOORBEAM — CRACKED (BS 1275)
INSPECTION FOUND A 1 INCH CRACK ON FLOORBEAM UNDER LOWER JAMB OF R-3 DOOR AT STA 1275. A REPAIR WAS FABRICATED AND INSTALLED IAW ECRA 5320-01500.
Part: BOLT — SHEARED (DOOR 4R)
INSPECTION FOUND A SHEARED BOLT IN AFT FRAME OF DOOR 4R AT LONGERON 15R. THE BOLT WAS REPLACED IAW MM 20-50-02.