Registered owner
Air Methods LLC
Owner type
LLC
Serial number
9069
Year built
2005
Type
Rotorcraft
Engine
Turbo-shaft
Airworthiness
Standard, transport
Airworthiness date
May 6, 2005
Certificate issued
April 17, 2019
Expires
April 30, 2029
Mode S code
A0B9AC

From the FAA registry file of October 24, 2026.

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Airworthiness directives that may apply · 58

Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.

2007In forceSuperseded2026
ADs by the year they took effect: 68 ADs
20071
20081
20101
20111
20124
20138
20145
20151
20165
20175
20181
20196
20201
20217
20229
20232
20242
20253
20265
See all 68 ADs

Information bulletins that may apply · 3

Advisory, not mandatory.

NTSB investigations

No NTSB investigations matched to N146HCMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Eurocopter Deutschland MBB-BK 117 C-2 aircraft

FAA incident reports

No FAA accident or incident reports matched to N146HCMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Eurocopter Deutschland MBB-BK 117 C-2 aircraft

Service difficulty reports · 5

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

SDR QMLA2024021220015Control Panel · shortedENGAGING THE NVG LIGHTING SWITCH CAUSED A SHORT IN THE OVERHEAD SWITCH PANEL.Feb 9, 2024 · N146HC · Bolkms BK117C2 · Instrument System WiringSDR 2A6R2023102468502Frame · corrodedDURING 800 HOUR INSPECTION, FOUND CORROSION DAMAGE TO THE FUSELAGE STATION 5645 FRAME UPPER T-EXTRUSION (PN: B533K7052-211) WAS IDENTIFIED IN MULTIPLE AREAS ACROSS THE UPPER SURFACE OF THE AFT FLANGE. A REPLACEMENT T-EXTRUSION WAS FABRICATED TO REPLACE THE DASep 26, 2023 · N146HC · Bolkms BK117C2 · Fuselage Main, FrameSDR 2A6R2023102468501Beam · chafedDURING 800 HOUR INSPECTION, FOUND CHAFE DAMAGE TO THE RH ENGINE DECK CENTER BEAM LOWER CAP (PN: 117-22309-38) WAS IDENTIFIED NEAR THE FORWARD EDGE OF THE PART AND IN AN AREA MEASURED TO BE APPROXIMATELY 0.80” X 0.20” IN SIZE WITH THE DEEPEST CHAFE BEING APPROXSep 21, 2023 · N146HC · Bolkms BK117C2 · Fuselage, Powerplant Attach FittingsSDR 2A6R2021111162101Frame · chafedDURING INSPECTION, CHAFE DAMAGE WAS NOTED TO THE AFT BOX BEAM UPPER FRAME INSIDE SKIN (PN: B533K3606-205) IN THE FORM OF CHAFING MEASURING TO BE APPROXIMATELY 0.70” LONG AND 0.020” DEEP FOR BOTH LOCATIONS. THE DAMAGE WAS REPAIRED VIA REPAIR DOUBLERS TO REINFONov 11, 2021 · N146HC · Bolkms BK117C2 · Fuselage Structure (General)SDR QMLA2020090820045Controller · odorFUMES WERE DETECTED IN THE AIRCRAFT UPON DEPARTURE. WE RETURNED FOR LANDING WITHOUT INCIDENT. UPON INVESTIGATION THE PART WAS SMELLING LIKE THE FUMES DESCRIBED. THERE WAS ALSO A FEW DROPS OF WATER, MOST LIKELY FROM A HEAVY RAIN THAT THE AIRCRAFT ENDURED A FSep 4, 2020 · N146HC · Bolkms BK117C2 · Communications System

STCs that may be installed · 111

Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.

See all 111 STCs