N13086

No registry detail on file · not in current registry

Operators of this aircraft

Who operated this tail, and how firmly we know it.

No operator established for this aircraft.

Accident & incident history

CESSNA 150 Minor injury Part 91operator not named in the NTSB record
Source: NTSB case CHI77FEK23

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.

OTHER · 2000-01-26 Matched by certificate designator
ATA 5755

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.

Source: SDR CALA0000085
OTHER · 2000-01-26 Matched by certificate designator
ATA 5730

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.

Source: SDR CALA0000084
OTHER · 2000-01-18 Matched by certificate designator
ATA 5315

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.

Source: SDR CALA0000046
OTHER · 1999-01-20 Matched by certificate designator
ATA 5743

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.

Source: SDR CALA9900034
OTHER · 1999-01-20 Matched by certificate designator
ATA 5743

Part: BEAM — CORRODED (RT MLG)

RIGHT MAIN LANDING GEAR SUPPORT FRAME ATTACHMENT BOLT HOLES CORRODED. HOLES REWORKED AND BUSHED PER EC/RA 5473-01012.

Source: SDR CALA9900035
OTHER · 1999-01-17 Matched by certificate designator
ATA 5210

Part: ASSIST BOTTLE — LOW PRESSURE (L1 DOOR)

L1 DOOR ASSIST BOTTLE PRESSURE LOW. RECHARGED L1 DOOR ASSIST BOTTLE PER MM 52-12-06.

Source: SDR CALA9900064
OTHER · 1999-01-16 Matched by certificate designator
ATA 5753

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.

Source: SDR CALA9900061
OTHER · 1998-02-06 Matched by certificate designator
ATA 2760

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.

Source: SDR CALA9800197
OTHER · 1998-02-02 Matched by certificate designator
ATA 5320

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.

Source: SDR CALA9800169