N106HN

No registry detail on file · not in current registry

Operators of this aircraft

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

OperatorRolePeriodBasis
Air Methods Corp. (QMLA)Operatoron 2009-06-24Operator named in NTSB report

Accident & incident history

Accident · 2009-06-24 Operator named in NTSB report
EUROCOPTER AS 350 B2 No injuries Part 91Air Methods Corp.

Operated by Air Methods Corporation Inc. (per NTSB report)

Source: NTSB case ERA09CA367

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.

3 reports on file, 2007-04-22 – 2013-10-30.

OTHER · 2013-10-30 Matched by certificate designator
ATA 6320

Part: ACTUATOR — BINDING (MAIN ROTOR) · airframe 9,239 hrs · 30,110 cycles

DURING MAINTENANCE GROUND RUN, PILOT INFORMED ONBOARD MECHANIC THAT CYCLIC STICK WAS HARD TO PUSH TO THE RT WHILE PERFORMING FLIGHT CONTROL CHECK. R & R BOTH LATERAL CONTROL SERVO ACTUATORS AND PERFORMED RIG CHECK OF MAIN ROTOR. OPS CHECK FLIGHT WAS SUCCESSFUL.

Source: SDR 2A6R20131105001
OTHER · 2013-10-30 Matched by certificate designator
ATA 6320

Part: ACTUATOR — BINDING (MAIN ROTOR) · airframe 9,239 hrs · 30,110 cycles

DURING MAINTENANCE GROUND RUN, PILOT INFORMED ONBOARD MECHANIC THAT CYCLIC STICK WAS HARD TO PUSH TO THE RT WHILE PERFORMING FLIGHT CONTROL CHECK. R & R BOTH LATERAL CONTROL SERVO ACTUATORS AND PERFORMED RIG CHECK OF MAIN ROTOR. OPS CHECK FLIGHT WAS SUCCESSFUL.

Source: SDR 2A6R20131105002
PARTIAL RPM/PWR LOSS; WARNING INDICATION · 2007-04-22 Matched by certificate designator
ATA 7200

Part: ENGINE — POWER LOSS

APPROXIMATELY 22 MINUTES INTO FLT, PILOT EXPERIENCED INDICATIONS OF ENGINE FAILURE, LOW ROTOR RPM AUDIO CAME ON FOLLOWED AT THE SAME TIME WITH AIRCRAFT YAW. PILOT ENTERED AUTOROTATIONAL DESCENT AND LOOKED FOR LANDING AREA UNDER THE NVGS WHILE MAKING A MAYDAY CALL TO APPROACH CONTROL. FLT MEDIC ALSO MADE MAYDAY CALL TO MEDCOM. AFTER SETTING UP FOR LANDING PILOT HAD TIME TO LOOK AT ENGINE INDICATIONS BRIEFLY AND DETERMINED THAT PARTIAL POWER CONDITION WAS NOW INDICATED. DUE TO LOW ALTITUDE, 250 FT AGL, PILOT FELT THAT THERE WAS LITTLE TIME TO REGAIN ENGINE CONTROL WITH FUEL CONTROL LEVER. AUTO WAS COMPLETED WITH SKID AND CROSSTUBE DAMAGE. NO INJURIES TO CREW OR PATIENT. AIRCRAFT IS BEING REMOVED FROM FIELD AN

Source: SDR 07N106HN01