Registered owner
Air Methods LLC
Owner type
LLC
Serial number
9072
Year built
2005
Type
Rotorcraft
Engine
Turbo-shaft
Airworthiness
Standard, transport
Airworthiness date
April 22, 2006
Certificate issued
January 13, 2015
Expires
January 31, 2028
Mode S code
A0B643

From the FAA registry file of October 24, 2026.

On this page

Airworthiness directives that may apply · 72

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

2003In forceSuperseded2026
ADs by the year they took effect: 87 ADs
20033
20072
20081
20092
20102
20112
20124
201312
20147
20152
20167
20177
20181
20196
20201
20217
20229
20232
20242
20253
20265
See all 88 ADs

Information bulletins that may apply · 3

Advisory, not mandatory.

NTSB investigations

No NTSB investigations matched to N145LFMatched 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 N145LFMatched 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 · 12

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

SDR QMLA2024121020149Engine · making metalUPON TAKEOFF FROM HOSPITAL PAD #1 ENG CHIP ILLUMINATED ON CAD. #1 ENGINE OIL PRESSURE AND TEMPERATURE INDICATED NORMAL. DEPRESSED FUZZ BURN SWITCH, #1 ENG CHIP CAD LIGHT REMAINED ILLUMINATED. CONTINUED FLIGHT FOR APPROXIMATELY ONE TO TWO MINUTES AND LANDED AT Dec 2, 2024 · N145LF · Bolkms BK117C2 · Engine (Turbine/Turboprop)SDR QMLA2023032220017Frame · unknownDURING THE A 0306 - ZONE 6 AIRFRAME INSPECTION A MISSING RIVET HEAD WAS LOCATED AT THE TRANSITION FROM THE TAILBOOM TO VERTICAL STRUCTURE THRU THE R/H OMEGA STRINGER (P/N 105-30251.26) AT FRAME 10L. AIRBUS MAINTENANCE MANUAL 53-50-00 6-1 (1)(2) AND FIGURE 2 REJan 30, 2023 · N145LF · Bolkms BK117C2 · Fuselage Structure (General)SDR QMLA20190419719Starter Gen · arcedDURING ATTEMPTED ENGINE START, PILOT OBSERVED THE NR 2 ENGINE N1 FAILURE TO INCREASE, AND SUBSEQUEENT FAILURE OF ENGINE TO START. AFTER ABORTING ENGINE START PILOT INSPECTED ENGINE AREA AND FOUND SEVERE ARCING ON POST 'C' OF STARTER GENERATOR. ARCING CAUSED TApr 17, 2019 · N145LF · Bolkms BK117C2 · Starter-GeneratorSDR QMLA2019030519026Wire · burnedSUPPLEMENTAL INFORMATION: THE PILOT REPORTED THAT THE STANDBY ATTITUDE INDICATOR BACKLIGHTING AND THE SUPER NIGHT SCANNER SEARCHLIGHT REMAINED ILLUMINATED IN THE OFF POSITION. THE MECHANIC BEGAN TROUBLESHOOTING THIS PILOT REPORTED SQUAWK (FOUND ON THE GROUND).Mar 5, 2019 · N145LF · Bolkms BK117C2 · Electrical Power System WiringSDR QMLA2019022619020Skin · crackedDURING A PREFLIGHT INSPECTION, THE MECHANIC FOUND A CRACK ON THE LOWER SKIN OF THE LT HORIZONTAL STABILIZER. THE CRACK WAS STOP DRILLED TO PROVIDE TEMPORARY RELIEF UNTIL THE MATERIALS NECESSARY TO ACCOMPLISH THE PERMANENT REPAIR ARRIVED. SRM, CHAPTER 51-70-51,Feb 26, 2019 · N145LF · Bolkms BK117C2 · Rotorcraft Tail BoomSDR QMLA2014060214063Chip Detector · contaminatedTAIL ROTOR CHIP CAUTION ILLUMINATED ON CAD DURING POWER UP. REMOVED TAIL ROTOR CHIP PLUG & FOUND ONE TINY SLIVER APPROXIMATELY THE SIZE OF A HAIR & 1 - 2 MM IN LENGTH. CLEANED CHIP PLUG & REINSTALLED. PERFORMED OPERATIONS CHECK & 10 MINUTE GND RUN WITH NO RJun 2, 2014 · N145LF · Bolkms BK117C2 · Tail Rotor Drive Indicating SystemSDR QMLA2014030314022Doubler · crackedDURING ROUTINE PRE-FLIGHT AIRWORTHINESS CHECK A CRACK WAS FOUND ON A SKIN DOUBLER LOCATED ON THE LT BASE OF THE VERTICAL STABILIZER AT STATION 9800, WL 3100, BLL 50. THE CRACK RUNS VERTICAL & MEASURES APPROXIMATELY 2.315 INCHES. THE DOUBLER WAS REMOVED & ANOMar 3, 2014 · N145LF · Bolkms BK117C2 · Rotorcraft Tail BoomSDR QMLA2013041813056Unknown · fumesDURING ACFT STARTING PROCEDURE, BATTERY POWER WAS ENERGIZED AND ACFT SYSTEMS WERE PREPARED FOR STARTING FIRST ENGINE. FUMES WERE NOTICED AND WHEN ATTENTION WAS DIVERTED TO VIEW WHERE THE FUMES WERE EMMINATING FROM, SMOKE WAS RISING FROM BEHIND THE INSTRUMENT Apr 18, 2013 · N145LF · Bolkms BK117C2 · Air Distribution SystemSDR QMLA2012070912113Blower Motor · shortedWHILE ENROUTE, CREWMEMBERS REPORTED SMOKE IN CABIN. SHUT OFF AIR CONDITIONER AND ELECTRICAL GENERATORS, OPENED VENT WINDOWS, AND BEGAN A DESCENT FOR AN EMERGENCY LANDING. DECLARED AN EMERGENCY, PERFORMED AN EMERGENCY SHUTDOWN, AND APPLIED ROTOR BRAKE. Jul 9, 2012 · N145LF · Bolkms BK117C2 · Air Distribution SystemSDR QMLA2010070510026Blower Motor · burnedON DEPARTURE AT 600' AGL, NOTICED SMELL/AROMA OF ELECTRICAL OVERHEATING. NOTIFIED CREW AND IMMEDIATELY BEGAN A 270 DEGREE TURN TO RETURN TO DEPARTURE. DISCONNECTED BOTH GENERATORS, DISENGAGED BOTH BUS TIES, TURNED OFF AIR CONDITIONING UNIT. LANDED WITHOUT INCIJul 5, 2010 · N145LF · Bolkms BK117C2 · Cabin Cooling SystemSDR 907204142008Wire · damagedTHIS REPORT IS THE 3RD OCCURRENCE OF SMOKE/ODOR CAUSED BY AN ELECTRICAL DISCHARGE FAULT IN THE OVERHEAD CIRCUIT BREAKER PANEL. MECHANICS REPLACED THE APPROPRIATE WIRING AND DUMMY CIRCUIT BREAKER INVOLVED IN THE INITIAL FAULT. AIRCRAFT WAS OPS CHECKED AND THEN Apr 14, 2008 · N145LF · Bolkms BK117C2 · Electrical Power System WiringSDR 907204092008Wire · shortedUPON LANDING, STRONG ACRID ODOR IN CABIN AND COCKPIT AREAS. MECHANIC CALLED IN AND UPON INSPECTION OF OVERHEAD CIRCUIT BREAKER PANEL, IT WAS DISCOVERED THAT THE STANDBY ATTITUDE INDICATOR CIRCUIT BREAKER WIRE HAD CONTACTED METAL FRAME RESULTING IN ARCING. MECHApr 9, 2008 · N145LF · Urocop EC135P1 · Electrical Power System Wiring

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