N12

HAWKER BEECHCRAFT CORP C90GTI · 2009 · Fixed-wing multi-engine · 2 engines · 6 seats · Valid Registration

Registered owner: FEDERAL AVIATION ADMINISTRATION, OK (owner ≠ operator)

Operators of this aircraft

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

OperatorRolePeriodBasis
Flight Program Operations (RU3A)Certificate holderMatched by certificate designator

Accident & incident history

BEECH 65 No injuries Part 91operator not named in the NTSB record
Source: NTSB case NYC76AN117

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.

10 reports on file, 2010-07-13 – 2022-07-13.

WARNING INDICATION · 2022-07-13 Matched by certificate designator
ATA 2610

Part: NONE — NONE (ZONE 400)

RIGHT ENGINE FIRELIGHT ILLUMINATED IN FLIGHT. THERE WAS NOT A FIRE. AIRCRAFT RETURNED TO BASE UNEVENTFULLY.

Source: SDR 2022FA0000354
WARNING INDICATION · 2019-08-28 Matched by certificate designator
ATA 2820

Part: UNKNOWN — MALFUNCTIONED (FUEL SYSTEM) · airframe 2,593 hrs · 2,148 cycles

RIGHT NO FUEL XFR (RIGHT NO FUEL TRANSFER) ANNUNCIATOR WARNING LIGHT ILLUMINATED. MAINTENANCE PERFORMED GROUND OPS CHECK. NO DEFECT WAS DISCOVERED.

Source: SDR RU3A20190828045
FALSE WARNING · 2018-07-24 Matched by certificate designator
ATA 7797

Part: WIRE — LOOSE (NR 2 ENGINE) · airframe 2,335 hrs · 1,808 cycles

WHILE IN FLIGHT, CREW OF N12 SHUT DOWN NR 2 ENGINE FOR ITT FLUCTUATIONS AND REDLINING. AFTER ENGINE SHUTDOWN, ITT TEMP WAS STILL MEASURING OVER 900C. ON THE GROUND, TECHNICIAN LOCATED A BAD CRIMP ON A NEW WIRING HARNESS INSTALLED ON THE T5 WIRING HARNESS ON THE NR 2 ENGINE. TECHNICIAN WAS ABLE TO DUPLICATE THE DISCREPANCY BY MOVING THE WIRES. THE FAULTY WIRE WAS RE-CRIMPED. DISCREPANCY WAS CLEARED AND AIRCRAFT RETURNED TO SERVICE.

Source: SDR RU3A20180724032
OTHER · 2013-11-12 Matched by certificate designator
ATA 5420

Part: CHANNEL — CRACKED (NR 2 NACELLE) · airframe 1,123 hrs · 604 cycles

DURING INSPECTION OF THE NR 2 ENGINE, THE FIRE SEAL ASSY OTBD CHANNEL LOWER FLANGE WAS FOUND CRACKED AND DEFORMED AT THE BOLT HOLES.

Source: SDR UA2R20131118015
OTHER · 2013-11-12 Matched by certificate designator
ATA 5420

Part: CHANNEL — CRACKED (NR 2 NACELLE) · airframe 1,123 hrs · 604 cycles

DURING INSPECTION OF THE NR 2 ENGINE, THE FIRE SEAL ASSY INBD CHANNEL LOWER FLANGE WAS FOUND CRACKED AND DEFORMED AT THE BOLT HOLES.

Source: SDR UA2R20131118014
OTHER · 2013-11-12 Matched by certificate designator
ATA 5420

Part: CHANNEL — CRACKED (NR 1 NACELLE) · airframe 1,123 hrs · 604 cycles

DURING INSPECTION OF NR 1 ENGINE, FIRE SEAL ASSY OTBD CHANNEL LOWER FLANGE WAS FOUND CRACKED AND DEFORMED AT THE BOLT HOLES.

Source: SDR UA2R20131114012
OTHER · 2013-11-12 Matched by certificate designator
ATA 5420

Part: CHANNEL — CRACKED (NR 1 NACELLE) · airframe 1,123 hrs · 604 cycles

DURING INSPECTION OF THE NR 1 ENGINE, FIRE SEAL ASSY INBD CHANNEL LOWER FLANGE WAS FOUND CRACKED AND DEFORMED AT THE BOLT HOLES.

Source: SDR UA2R20131118013
OTHER · 2010-07-14 Matched by certificate designator
ATA 3020

Part: FLEX HOSE — CRACKED (INTAKE ANTI-ICE) · airframe 60 hrs · 47 cycles

(UA2R) ANTI-ICE FLEX HOSES (PAIR) ON BOTH ENGINE INLETS CRACKED. R & R. PN IN BLOCK 5(C) BELOW IS LT. RT SN 90-910099-13, ALSO REPLACED.

Source: SDR UA2R1102
SMOKE/FUMES/ODORS/SPARKS · 2010-07-14 Matched by certificate designator
ATA 7500

Part: MANIFOLD — BROKEN (BLEED SYSTEM) · airframe 60 hrs · 58 cycles

DURING MAINT ACTIONS, DISCOVERED ALL BLEED FLEX LINES TO ENGINE INTAKE ANTI/DE-ICE HAD BROKEN ON BOTH ENGINES. NO OTHER DAMAGE NOTED TO NACELLE OR PYLON. REPAIRED AS NECESSARY WITH NEW COMPONENTS.

Source: SDR 2010F00160
SMOKE/FUMES/ODORS/SPARKS · 2010-07-13 Matched by certificate designator
ATA 7510

Part: FLEX DUCT — BROKEN (ENGINE ANTI ICE) · airframe 60 hrs · 58 cycles

BOTH ENGINE INLET ANTI/DE-ICE MANIFOLDS WERE BROKEN ON BOTH ENGINES.

Source: SDR 2010F00157