N921AUAero Union Corp P3A
This N-number isn't registered right now. Below is its last known registration, canceled Nov 29, 2025.
Safety record in brief:No NTSB accidents or incidents since 1982No ADs since 1998 matched3 service difficulty reports
- Registration
- Deregistered
Registration
FAA Aircraft Registry · Oct 20, 2026- Last registered owner
- Individual owner
- City, state
- Hay River
- Canceled
- Nov 29, 2025
- Airworthiness
- Restricted · Forest
- Airworthiness date
- Apr 21, 2011
We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.
Airframe & engine
FAA Registry + type dataAirframe
- Manufacturer
- Aero Union Corp
- Model
- P3A
- Serial number
- 151385
- Aircraft type
- Fixed wing multi engine
- Category
- Land
- Certification
- Type Certificated
- Seats
- 2
- Engines
- 4
- Max takeoff weight
- 20,000 and over lb
- Mode S code
- ACC1F4
Engine
- Make and model
- Allison T-56-A-10w
- Type
- Turbo-prop
- Power
- 4500 hp
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- until 2025Individual ownerHay River
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 2026 · SDRs · Oct 16, 2026NTSB events (0)
No NTSB accidents or incidents found for this airframe since 1982.
ADs published since 1998 that may apply (0)
These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.
No ADs published since 1998 matched this airframe or engine model.
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (3)
Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.
- Fuselage · attach fitting · crackedFeb 15, 2011
DURING ANNUAL INSPECTION, A DETAILED ULTRA-SONIC INSPECTION OF THE FUSELAGE WING ATTACH RING FITTINGS WERE INITIATED BY AN INTERNAL SB. A FATIGUE CRACK WAS APPRECIATED IN THE LT FWD FITTING, VERTICAL OTBD FLANGE APPROX 6" ABOVE UPPER TENSION BOLT.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · fitting · crackedFeb 15, 2011
DURING ANNUAL INSPECTION, A DETAILED ULTRA-SONIC INSPECTION OF THE FUSELAGE WING ATTACH RING FITTINGS WERE INITIATED BY OUR BY OUR INTERNAL SB. A FATIGUE CRACK WAS APPRECIATED IN THE RT FWD FITTING JUST BELOW THE UPPER MOST AFT HOLE ON THE VERTICAL OTBD FLANGE.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Wings · spar cap · fracturedOct 24, 2008
DURING INSPECTION TO DETERMINE THE SOURCE OF A FUEL LEAK A FRACTURE WAS FOUND IN THE LOWER FORWARD RIGHT SPAR CAP AT WING STA 75 EMANATING FROM NUT PLATE FASTENER HOLE ON FORWARD FLANGE TO THE EDGE OF FLANGE MEMBER WITH SLIGHT ENCROACHMENT AFT FROM SAME HOLE, APPROX .125 INCH. SECOND FRACTURE…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Sources
- FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 20, 2026
- NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
- FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 20, 2026
- FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026