N14090
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
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.
14 reports on file, 1997-09-08 – 2000-06-21.
Part: SMOKE DETECTOR — FALSE INDICATION (CARGO BAY) · airframe 97,916 hrs · 24,193 cycles
THE NR 1 FORWARD CARGO SMOKE DETECTOR AND FORWARD CARGO FIRE LIGHTS ILLUMINATED WITH MASTER WARNING WHILE AT FL 310 AFTER DEPARTING LGW. THE LIGHTS EXTINGUISHED WHEN AGENT NR 1 FIRE BOTTLE WAS DISCHARGED. THE AIRCRAFT WAS RETURNED TO LGW WHERE IT LANDED WITHOUT INCIDENT. THE FORWARD CARGO COMPARTMENT WAS INSPECTED WITH NO EVIDENCE OF SMOKE OR FIRE FOUND. THE NR 1 FORWARD CARGO COMPARTMENT SMOKE DETECTOR WAS REPLACED. IN ADDITION, THE FORWARD CARGO COMPARTMENT NR 1 FIRE BOTTLE WAS REPLACED. WORK WAS PERFORMED IAW MM 26-14-01, 26-22-01, AND 26-22-02.
Earlier reports · 1997–1999 · 13 reports
1999
Part: PANEL — CRACKED (LT WING)
INSPECTION FOUND A 1 INCH CRACK IN LT WING UPPER LEADING EDGE PANEL NR 517CT. THE PANEL WAS REPLACED IAW SRM 51-31-01.
Part: PANEL — DELAMINATED (VERTICAL STAB)
INSPECTION FOUND VERTICAL STABILIZER LOWER REAR CENTER PANEL DELAMINATED. A REPAIR WAS INSTALLED IAW ECRA 5533-01002.
Part: FAIRING — CRACKED (FUSELAGE)
INSPECTION FOUND A 1 INCH CRACK IN LT WING I/B FLAP FAIRING O/B SIDE PANEL 549AL. A REPAIR WAS INSTALLED IAW SRM 57-00-01.
Part: SKIN — CRACKED (RT WING)
INSPECTION FOUND A 2 INCH CRACK AND DELAMINATION IN RT WING I/B FLAP VANE T/E SKIN. THE VANE WAS REMOVED AND REPLACED IAW MM 27-50-00.
1997
Part: SUPPORT — CORRODED (BS 1360)
INSPECTION FOUND FAIRING SUPPORT JUST FORWARD OF RT WHEEL WELL AT FS 1360 CORRODED. THE CORROSION WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 51-21-01 AND 53-00-01.
Part: STRAP — CORRODED (WS 417)
INSPECTION FOUND LT WING UPPER SURFACE FILLER STRAP CORRODED ABOVE REAR SPAR AT XORS 417. REPAIRED IAW ECRA 5710-01840.
Part: BRACKET — CORRODED (VERT STAB)
INSPECTION FOUND MOUNT BRACKET FOR VERTICAL STABILIZER PANEL 374ER CORRODED. THE MOUNT BRACKET WAS REMOVED AND REPLACED IAW SRM 51-31-01.
Part: SKIN — CORRODED (WS 814)
INSPECTION FOUND A 1.25 INCH CRACK IN SKIN OF RT WING LOWER SURFACE AT XORS 814, BELOW FUEL CONTROLLER. THE SKIN WAS REPAIRED IAW SRM 51-21-01 AND ECRA 5710-01839.
Part: SKIN — CORRODED (LT WING)
INSPECTION FOUND CORROSION ON INTERIOR SURFACE OF LT WING OUTBOARD HINGE SKIN PANEL NR 536DL. THE CORRODED SKIN LAYER WAS REMOVED IN THREE PLACES IAW SRM 51-43-01. BONDED DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 51-43-01, 51-21-01, AND 57-32-01.
Part: STIFFENER — CRACKED (RT MLG WW)
INSPECTION FOUND A 1 CRACK IN RT WHEEL WELL LOWER AFT BULKHEAD OUTBOARD STIFFENER. THE STIFFENER WAS REMOVED AND A REPLACEMENT STIFFENER WAS FABRICATED AND INSTALLED IAW SRM 51-31-00 AND 51-10-00.
Part: CHANNEL — CRACKED (E/E COMP)
INSPECTION FOUND CHANNEL IN FORWARD E/E COMPARTMENT DENTED AND CRACKED. THE CHANNEL WAS REMOVED AND A NEW CHANNEL WAS FABRICATED AND INSTALLED IAW SRM 51-31-01, 51-43-00, 53-21-00, AND 51-21-01.
Part: PANEL — CORRODED (LT WING)
INSPECTION FOUND CORROSION IN TWO SPOTS ON INTERIOR SURFACE OF LT WING OUTBOARD HINGE PANEL 536DL. THE CORRODED AREAS WERE REMOVED IAW SRM 51-43-01. DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 57-32-01 AND 51-21-01.
Part: BRACKET — CORRODED (VERT STAB)
INSPECTION FOUND VERTICAL STABILIZER PANEL 374ER MOUNT BRACKET CORRODED. THE MOUNT BRACKET WAS REMOVED, A NEW MOUNT BRACKET WAS FABRICATED AND INSTALLED IAW SRM 51-31-01, 55-00-01, 55-32-01, AND 51-21-01.