- Registered owner
- United Aeronautical Corp
- Location
- North Hollywood, CA
- Owner type
- Corporation
- Serial number
- 151391
- Year built
- 2010
- Type
- Fixed wing multi engine
- Engine
- Turbo-prop
- Airworthiness
- Restricted, forest
- Airworthiness date
- April 20, 2011
- Certificate issued
- November 7, 2013
- Expires
- November 30, 2029
- Mode S code
- AC6F3F
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 2
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 2014 | 1 |
|---|---|
| 2018 | 1 |
Information bulletins that may apply
Advisory, not mandatory.
No bulletins matched this aircraft’s models
NTSB investigations
No NTSB investigations matched to N900AUMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Aero Union P3A aircraft
FAA incident reports
No FAA accident or incident reports matched to N900AUMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Aero Union P3A aircraft
Service difficulty reports · 2
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR AUCR20110215002Fitting · crackedDURING ANNUAL INSP, A DETAILED ULTRA-SONIC INSP OF THE FUSELAGE WING ATTACH RING FITTINGS WERE INITIATED BY AN INTERNAL SB. A FATIGUE CRACK WAS APPRECIATED IN THE RT AFT FITTING'S VERTICAL OTBD FLANGE.SDR AUCR20110215001Flange · crackedDURING 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 RT FWD FITTING'S VERTICAL OTBD FLANGE.
Reports on N900AU not matched to an aircraft · 2
They name N900AU, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR AUCR200600006Spar Cap · crackedDURING SCHEDULED INSPECTION FOUND CORROSION INDUCED CRACK IN UPPER AFT SPAR CAP EXTENDING OUTBOARD FROM PREVIOUS REPAIR IN THE AREA OF FLAP TRACK 5, WS 346. DURING DISASSEMBLY TO EFFECT REPAIR FOUND ADDITIONAL STRESS CORROSION FRACTURE ON UPPER AFT SPAR CAP ASDR AUC2003F00001Tire · failedWHEEL ASSEMBLY WITH RECAPPED TIRES INSTALLED ON AIRCRAFT. THESE TIRES INSTALLED FOR A TOTAL OF 10 DAY AND OPERATED FOR A TOTAL OF 28 FLIGHT HOURS. UPON TAKE OFF ONE OF THE NOSE WHEELS LOST THE CENTER PORTION OF THE TIRE TREAD. THE FLIGHT CREW EXPERIENCED AN
STCs that may be installed · 4
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Aero Union P3A
STC ST04186ATIncorporation of P3A Airworthiness Limitation Section for aircraft operated in Restricted Category for the special mission of aerial dispensing of liquidsSTC ST00788LAInstallation of a Champion or Unison engine ignition systemSTC ST00792LAInstallation of Retardant Tanks for the special purpose of Forest and Wildlife Conservation.STC ST03718ATIncorporation of P3A Airworthiness Limitation Section for aircraft operated in Restricted Category for the special mission of aerial dispensing of liquids in accordance with Avenger Aircraft and Services Report No. AAS-MDL-09-002, Revision NC dated April 30, 2009, or later FAA approved revision.