N212AH
Registered owner: ASPEN HELICOPTERS INC, CA (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| Aspen Helicopters Inc (IGAA) | Certificate holder | — | Matched by certificate designator |
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
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.
6 reports on file, 2005-08-08 – 2022-08-15.
Part: HOSE — LEAKING (ZONE 200) · airframe 18,232 hrs
HOSE ASSEMBLY CHAFING DAMAGE RESULTING IN LOSS OF FLUID.
Part: LINK — CRACKED (XMSN MOUNT)
UPON 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 BEYOND LIMITS ALLOWED.
Part: BLADE — CORRODED (TAIL ROTOR)
TAIL ROTOR BLADE DEVELOPED DEEP CORROSION PIT AT BLADE ROOT.
Part: BLADE — CORRODED (TAIL ROTOR)
TAIL ROTOR BLADE DEVELOPED DEEP CORROSION PIT AT BLADE ROOT.
Part: BLADE — CRACKED (MAIN ROTOR)
DURING 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.
Part: FITTING — DETACHED (VALVE)
DURING FLIGHT FITTING BECAME DETACHED CAUSING LOSS OF OIL. FOUND FITTING MADE OF ALUMINUM. NEW FITTING MADE OF STEEL. (K)