N13086
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.
9 reports on file, 1998-02-02 – 2000-01-26.
Part: SKIN — DELAMINATED (SPOILER)
INSPECTION FOUND UPPER SKIN OF LT WING SPOILER PANEL NR 3 DELAMINATED. THE SPOILER WAS REPLACED AND ADJUSTED IAW MM 27-60-01.
Part: SKIN — DELAMINATED (LT WING)
INSPECTION FOUND LT WING T/E PANEL 541BB DELAMINATED. A NEW PANEL WAS INSTALLED IAW SRM 51-31-01 AND MM 20-50-02.
Part: FLOORBEAM — CRACKED (BS 939)
INSPECTION FOUND A 4 CRACK IN FLOORBEAM IN FORWARD CARGO AREA AT STA 939, LT SIDE. THE BEAM WAS REPLACED IAW MM 20-50-02.
Part: BEAM — CORRODED (LT MLG)
LEFT MAIN LANDING GEAR SUPPORT BEAM RETRACT CYLINDER SUPPORT FRAME ATTACHMENT BOLT HOLES CORRODED. HOLES REWORKED AND BUSHED PER EC/RA 5743-01012.
Part: BEAM — CORRODED (RT MLG)
RIGHT MAIN LANDING GEAR SUPPORT FRAME ATTACHMENT BOLT HOLES CORRODED. HOLES REWORKED AND BUSHED PER EC/RA 5473-01012.
Part: ASSIST BOTTLE — LOW PRESSURE (L1 DOOR)
L1 DOOR ASSIST BOTTLE PRESSURE LOW. RECHARGED L1 DOOR ASSIST BOTTLE PER MM 52-12-06.
Part: SKIN — CRACKED (RT TE FLAP)
RIGHT OUTBOARD FLAP UPPER SKIN CRACKED IN 4 PLACES, STATION 563.375, 4 AND 2 STATION 569.375, 7 AND STATION 581.377, 2. REMOVED AND REPLACED RIGHT OUTBOARD FLAP UPPER SKIN PER SRM 57-10-00.
Part: CRANK ASSY — CRACKED (CTR PEDESTAL)
THE AUTO SPOILERS WOULD NOT DEPLOY WHEN REVERSE THRUST WAS SELECTED. MAINTENANCE FOUND A 1 INCH CRACK IN THE AUTO SPOILER CRANK ASSEMBLY. THE CRANK ASSEMBLY WAS REPLACED IAW MM 27-62-01.
Part: STIFFENER — CRACKED (BS 1841)
INSPECTION FOUND A 2 X 1 CRACK AT FASTENER HOLE OF STIFFENER ON AFT SIDE OF FRAME IN CENTER CARGO COMPARTMENT AT STA 1841, RBL 42. THE STIFFENER WAS REMOVED IAW SRM 51-30-00. A NEW STIFFENER WAS FABRICATED AND INSTALLED IAW SRM 53-16-01 AND 51-30-00.