N105AM

BELL HELICOPTER TEXTRON CANADA 407 · 2010 · Valid Registration

Registered owner: AIR METHODS LLC, CO (owner ≠ operator)

Operators of this aircraft

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

OperatorRolePeriodBasis
AIR METHODS LLC (QMLA)Certificate holderMatched by certificate designator

Accident & incident history

No NTSB accidents or incidents on file for this aircraft.

Maintenance disclosures

E · 2024-03-01 Matched by certificate designator
ATA 6210

ENROUTE TO BASE, DEVIATED TO AIRPORT/COMPANY HANGAR DUE TO EXCESSIVE VERTICAL AND LATERAL VIBRATION IN FORWARD FLIGHT AT AND ABOVE 95KIAS. VIBRATION EXPERIENCED IN CRUISE, CLIMB, AND DESCENT.

Source: SDR QMLA2024030120023 · FAA SDRS
E J · 2024-03-01 Matched by certificate designator
ATA 6220

EN ROUTE TO BASE, DEVIATED TO AIRPORT/COMPANY HANGAR DUE TO EXCESSIVE VERTICAL AND LATERAL VIBRATION IN FORWARD FLIGHT AT AND ABOVE 95KIAS. VIBRATION EXPERIENCED IN CRUISE, CLIMB, AND DESCENT. SUPPLEMENTAL INFORMATION.

Source: SDR QMLA2024040220034 · FAA SDRS
O · 2016-08-12 Matched by certificate designator
ATA 7230

CRACK IN THE COMPRESSOR SCROLL, APPROXIMATELY 1 1/4 INCH LONG.

Source: SDR QMLA2016081216093 · FAA SDRS
J · 2015-08-25 Matched by certificate designator
ATA 6320

MAIN TRANSMISSION PN 407-040-006-123, SN A-1061, TT 1436.9 MAKING METAL WAS PULLED FROM THE ACFT & DISASSEMBLED. INSPECTED & FOUND THE DUPLEX BEARING PN 407-340-032-010, SN ZS1127 INSTALLED. HAS TWO BALL BEARINGS STARTED PITTING & FAILING.

Source: SDR 2A6D2015082525391 · FAA SDRS
R J · 2013-07-02 Matched by certificate designator
ATA 7200

ACFT DEPARTED. 7 MINUTES INTO FLIGHT, 1600 FT MSL, CLIMBING TO 2000 FT, FADEC FAULT CAUTION ILLUMINATED. BETWEEN 10 & 15 SECONDS LATER ACFT EXPERIENCED A VIOLENT LEFT YAW OF APPROX 45 DEGREES. AN AUTOROTATIVE DESCENT IMMEDIATELY INITIATED. DURING DESCENT, NR NOTED AT 100 PERCENT & NP AT 80-85 PERCENT. EMERGENCY PROCEDURE FOR ENGINE UNDERSPEED COMPLETED, FADEC PLACED IN MANUAL MODE, NR & NP MATCHED. FLT STABILIZED AT APPROX 400 FT AGL, NO FLUCTUATIONS INDICATED. RETUREND TO BASE. ON FINAL & REDUCTION OF POWER TO INITIATE APPROACH, DISCOVERED THE THROTTLE DID NOT RESPOND APPROPRIATELY. IT TOOK A SIGNIFICANTLY LARGE AMOUNT OF THROTTLE INPUT TO AFFECT THE NP. ACFT LANDED WITHOUT FURTHER INCIDENT.

Source: SDR QMLA2013070213090 · FAA SDRS