N3831

EUROCOPTER AS 350 B3 · 2005 · 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

Accident · 1975-02-15 Unresolved
WINDJAMMER None injuryoperator not yet resolved
Source: NTSB case OAK75DVG44

Maintenance disclosures

O · 2023-05-10 Matched by certificate designator
ATA 5300

CHAFING WAS DISCOVERED IN 2 PLACES ON THE ENGINE DECK (AIRBUS PN 350A21-1239.21) JUST NEAR THE SCUPPER DRAIN HOLE. THE FIRST DAMAGE AREA IS APPROXIMATELY 0.300” LONG, 0.275”WIDE, AND 0.015” DEEP AT THE DEEPEST POINT. THE SECOND DAMAGE AREA IS APPROXIMATELY 0.250” LONG, 0.200”WIDE, AND 0.012” DEEP AT THE DEEPEST POINT.

Source: SDR 2A6D20230510001 · FAA SDRS
O · 2020-04-28 Matched by certificate designator
ATA 5311

THERE IS DAMAGE ON THE TRANSMISSION DECK FRAME JUST INBOARD OF THE SPLICE. DAMAGE MEASURES AT 0.017” IS 13MM WIDE AND 5MM LONG LOCATED AT APPROX. STA 3640, BL 210R, AND WL 1839.

Source: SDR 2A6D20200428001 · FAA SDRS
O · 2020-04-27 Matched by certificate designator
ATA 5311

THERE IS CHAFFING ON THE R/H UPPER FORWARD SECTION OF THE X FRAME MEASURED AT .012” DEEP APPROX. 4MM WIDE AND 3 MM LONG.

Source: SDR 2A6D2020042701301 · FAA SDRS
R J · 2018-04-05 Matched by certificate designator
ATA 7250

DURING DESCENT, AROUND 6500 FEET MSL, RECEIVED AN ENGINE CHIP LIGHT. NOTIFIED APPROACH CONTROL. HEARD A POP FOLLOWED BY A DECREASE ENGINE SOUND, RAPID DESCENT AND LOW ROTOR HORN. LOWERED COLLECTIVE AND CAME MORE AFT CYCLIC AND ENTERED AN AUTO ASSUMING ENGINE FAILURE, NOTIFIED ATC. PERFORMED A FULL DOWN AUTOROTATION ON THE ROAD. WHITE SMOKE STARTED PUSHING PAST THE AIRCRAFT SIDES AND NOSE. PERFORMED AN ENGINE EMERGENCY SHUTDOWN. THE SMOKE DISSIPATED, USED THE FIRE EXTINGUISHER, SAW NO FIRE OR APPARENT DAMAGE TO THE AIRCRAFT DURING INSPECTION. MAINTENANCE DISCOVERED THAT THERE WAS METAL CONTAMINATION ON THE ENGINE ELECTRONIC CHIP PLUG, ENGINE OIL TANK MAGNETIC PLUG, MO1 MAGNECTIC PLUG, AND EXCESSIVE AMOUNTS ON REAR BEARING STRAINER. FURTHER INSPECTION DETERMINED POSSIBLE REAR BEARING FAILURE.

Source: SDR QMLA2018040518041 · FAA SDRS
O · 2012-06-21 Matched by certificate designator
ATA 5302

AFTER ACFT ARRIVAL AT BASE, TROUBLESHOOTING AN UNRELATED DISCREPANCY. DURING WALKAROUND, FOUND A CRACK IN THE UPPER VERTICAL STABILIZER, FWD OF THE SPAR ON THE LOWER FRAME.

Source: SDR QMLA2012062112102 · FAA SDRS