N11UQ

AIRBUS HELICOPTERS EC 130 T2 · 2015 · Rotorcraft · 1 engine · 8 seats · 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 Corp. (QMLA)Certificate holderMatched 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.

3 reports on file, 2023-07-24 – 2025-06-02.

OTHER · 2025-06-02 Matched by certificate designator
ATA 5310

Part: XMSN DECK — CHAFED (ZONE 200) · airframe 8,923 hrs · 12,837 cycles

GOUGING- TOOL DAMAGE WAS DISCOVERED ON THE LH SIDE OF THE TRANSMISSION DECK. THE DEPTH IS APPROXIMATELY 0.026". THE MAXIMUM APPROXIMATE LENGTH IS .6 AND WIDTH IS 0.85".

Source: SDR 2A6D20250502001
WARNING INDICATION · 2023-10-16 Matched by certificate designator
ATA 6520

Part: CHIP DETECTOR — UNKNOWN (T/R GEARBOX) · airframe 8,263 hrs

WHILE ENROUTE FROM HCNMC TO HLBB WHILE @ 5500MSL, 2000'AGL, 110KIAS; EXPERIENCED A FLICKERING TRGB CHIP CAUTION LIGHT. THIS OCCURRED 3 TIMES; PILOT MOVED COLLECTIVE THE LAST TIME AND THE LIGHT FLASHED AS HE MOVED THE COLLECTIVE. PILOT CONFIRMED THE LIGHT HAD FLICKERED WITH OTHER CREWMEMBERS AND DECIDED TO DO A PRECAUTIONARY LANDING AT THE NEAREST AIRPORT. F98 WAS APPROXIMATELY 8 MILES NORTH OF THE AIRCRAFT AT THIS TIME. NORMAL APPROACH WAS MADE TO PREPARED RUNWAY, AND TAXI'D OFF INTO A PARKING AREA AND CONDUCTED A NORMAL SHUTDOWN. MECHANIC REMOVED CHIP PLUG NOTED FINE HAIR LIKE PARTICAL ON CHIP PLUG, CLEANED PLUG DRAINED OIL FROM GEARBOX, REPLACED OIL RININSTALLED CHIP PLUG, PEFORMED PENELTY RUN, CHECKED PLUGS, NO DEFECTS, WORK DONE IAW EC130T2 MM 05-50-00, 6-1. ACFT IN AIRWORTHY CONDITION.

Source: SDR QMLA2023101920093
OTHER · 2023-07-24 Matched by certificate designator
ATA 5510

Part: STABILIZER — CRACKED (UPPER AFT SKIN) · airframe 8,100 hrs · 11,030 cycles

UPON DAILY INSPECTION, THE HORIZONTAL STABILIZER WAS FOUND CRACKED ON THE RIGHT HAND SIDE OF THE UPPER SKIN JUST PAST THE UPPER REINFORCEMENT SPAR.

Source: SDR QMLA2023072520054