- Registered owner
- Aspen Helicopters Inc
- Location
- Oxnard, CA
- Owner type
- Corporation
- Serial number
- 30959
- Year built
- 1979
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Airworthiness
- Standard, transport
- Airworthiness date
- January 22, 2004
- Certificate issued
- March 16, 2004
- Expires
- October 31, 2029
- Mode S code
- A1C0F8
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Pratt & Whitney Canada PT6T-3 model are included below.
On this page
Airworthiness directives that may apply · 67
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1974 | 3 |
|---|---|
| 1975 | 1 |
| 1976 | 5 |
| 1977 | 3 |
| 1978 | 7 |
| 1979 | 2 |
| 1980 | 3 |
| 1981 | 2 |
| 1990 | 2 |
| 1991 | 1 |
| 1992 | 2 |
| 1993 | 3 |
| 1994 | 2 |
| 1998 | 1 |
| 1999 | 1 |
| 2000 | 2 |
| 2001 | 2 |
| 2002 | 3 |
| 2003 | 1 |
| 2005 | 1 |
| 2007 | 2 |
| 2008 | 1 |
| 2010 | 2 |
| 2011 | 4 |
| 2012 | 2 |
| 2013 | 4 |
| 2014 | 1 |
| 2015 | 1 |
| 2017 | 1 |
| 2018 | 2 |
| 2019 | 1 |
| 2020 | 3 |
| 2021 | 2 |
| 2022 | 7 |
| 2023 | 1 |
| 2024 | 4 |
| 2025 | 1 |
See all 91 ADs
Information bulletins that may apply · 5
Advisory, not mandatory.
Historical bulletins · 1
NTSB investigations
No NTSB investigations matched to N212AHMatched 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 Bell 212 aircraft
FAA incident reports
No FAA accident or incident reports matched to N212AHMatched 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 Bell 212 aircraft
Service difficulty reports · 6
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2022FA0000450Hose · leakingHOSE ASSEMBLY CHAFING DAMAGE RESULTING IN LOSS OF FLUID.SDR DALA2022FA0000429Link · crackedUPON VISUAL INSPECTION OF FRICTION DAMPERS AND TRANSMISSION MOUNTS, FOUND LIFT LINK FITTING CRACK ON THE AFT LUG BUSHING AREA COVERING THE ENTIRE LATERAL (SIDE). TRANSMISSION MOUNTS WERE REMOVED AND INSPECTED FOUND PRESSURE REQUIRED TO DEFLECT MOUNT WAS BEYONDSDR IGAR2016FA0000184Blade · corrodedTAIL ROTOR BLADE DEVELOPED DEEP CORROSION PIT AT BLADE ROOT.SDR IGAR2016FA0000183Blade · corrodedTAIL ROTOR BLADE DEVELOPED DEEP CORROSION PIT AT BLADE ROOT.SDR IGAA2014121200002Blade · crackedDURING ROUTINE MAINTENANCE, CONDUCTING AD2011-23-02 FOR CRACKS AND CORROSION, FOUND A VOID IN THE M/R BLADE AT ABOUT STATION 29.5 ON THE TOP SIDE OF THE BLADE DOUBLER. BLADE WAS REMOVED FROM SERVICE.SDR 2005FA0001139Fitting · detachedDURING FLIGHT FITTING BECAME DETACHED CAUSING LOSS OF OIL. FOUND FITTING MADE OF ALUMINUM. NEW FITTING MADE OF STEEL. (K)
STCs that may be installed · 359
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
See all 359 STCs