Registered owner
Air Methods LLC
Owner type
LLC
Serial number
7158
Year built
2011
Type
Rotorcraft
Engine
Turbo-shaft
Airworthiness
Standard, normal
Airworthiness date
February 24, 2012
Certificate issued
March 2, 2022
Expires
March 31, 2029
Mode S code
A263A3

From the FAA registry file of October 24, 2026.

On this page

Airworthiness directives that may apply · 98

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

1985In forceSuperseded2026
ADs by the year they took effect: 141 ADs
19851
19902
19991
20003
20012
20026
20038
20043
20052
20063
20076
20081
20092
20109
20114
20125
201311
20147
20154
20162
20175
20186
20193
20205
202116
20227
20232
20241
20254
202610
See all 144 ADs

Information bulletins that may apply · 9

Advisory, not mandatory.

Historical bulletins · 2

NTSB investigations

No NTSB investigations matched to N253LFMatched 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 American Eurocopter AS350B3 aircraft

FAA incident reports

No FAA accident or incident reports matched to N253LFMatched 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 American Eurocopter AS350B3 aircraft

Service difficulty reports · 7

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

SDR 2A6D2021101409003None · chafedRING FRAME CHAFING DAMAGE AT APPROXIMATELY STA 4918, WL 1759, AND BL 320L MEASURING 0.92” LONG X 0.08” WIDE AND IS 0.008” AT ITS DEEPESTOct 14, 2021 · N253LF · Snias AS350B3 · Fuselage Structure (General)SDR 2A6D2021092409002Deck Plate · chafedDENT AND CHAFING WAS DISCOVERED ON THE ENGINE DECK (AIRBUS PN 350A21-1239.21) JUST NEAR THE SCUPPER DRAIN HOLE. THE DENT WAS MEASURED TO BE 0.20” X 0.10” AND 0.040” DEEP, AND THE CHAFE WAS MEASURED TO BE 1.0” X 0.40” AND 0.005” DEEPSep 24, 2021 · N253LF · Snias AS350B3 · Fuselage Structure (General)SDR QMLA2021070220035Unknown · odorAT 8 MINUTES IN TO FLIGHT FLI FAILED WITH ELECTRICAL SMELL IN COCKPIT. ON 6/30/2021 I WAS CALLED OUT FOR A VEMD FLI FAILURE. UPON ARRIVAL I INSPECTED PANEL AND ENGINE HARNESS FOR SIGNS OF OVERHEATING AND VISUAL CHECK WITH ELECTRICAL POWER APPLIED TO SEE IF ANYJun 30, 2021 · N253LF · Snias AS350B3 · Air Distribution SystemSDR QMLA2019042629042Unknown · odor15 MINS INTO FLIGHT, CREW NOTIFIED THEY SMELLED BURNING ELECTRICAL IN THE CABIN, LANDED WITH NO OTHER ISSUES. MECHANIC AND PILOT RAN UP AIRCRAFT CHECKED SYSTEMS AND COULD NOT DUPLICATE. AIRCRAFT WAS VISUALLY CHECKED AND NO DISCREPANCIES WE NOTED.Apr 22, 2019 · N253LF · Snias AS350B3 · Air Distribution SystemSDR QMLA2018012318010Skin · dentedA DENT WAS FOUND ON THE RT SIDE OF TAILBOOM JUST ABOVE HORIZONTAL STAB APPROXIMATELY 5 INCHES IN LENGTH.Jan 23, 2018 · N253LF · Snias AS350B3 · Rotorcraft Tail BoomSDR QMLA2016112616135Fastener · missingPILOT BEGAN EXPLAINING THE PROBLEM HE ENCOUNTERED. REMOVING THE PANELS FOR FURTHER INSPECTION OF THE PEDAL ASSEMBLIES. THE PILOT AND MYSELF NOTICED THE CLEAR CIRCUIT BREAKER COVER WASN'T SECURED IN PLACE AND WAS INTERFERING WITH THE PEDAL TRAVEL. IT WAS DETERMNov 26, 2016 · N253LF · Snias AS350B3 · Rudder Control SystemSDR QMLA2012080512129Fire Detector · faultyDURING PRESTART CHECK, FIRE LIGHT WAS ILLUMINATED. PRESTART CHECKLIST WAS ABORTED AND MX WAS CALLED. MX TROUBLESHOT THE SWITCH AND FOUND NO DISCREPANCIES. THEY THEN REPLACED ALL 3 FIRE DETECTORS. THE FIRE LIGHT WENT OUT. NO FURTHER ISSUES OR DISCREPANCIES WERAug 5, 2012 · N253LF · Snias AS350B3 · Fire Detection

STCs that may be installed · 401

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

See all 401 STCs