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N4282

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2007 Eurocopter AS 350 B3 · Turbomeca ARRIEL-2B1

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Registered owner
Air Methods LLC
Location
Greenwood Village, CO
Owner type
LLC
Serial number
4282
Year built
2007
Type
Rotorcraft
Engine
Turbo-shaft
Airworthiness
Standard, normal
Airworthiness date
August 10, 2007
Certificate issued
March 18, 2013
Expires
March 31, 2029
Mode S code
A51BF5
Eurocopter AS 350 B3Airframe model · 6 seats · 1 engine · 167 registeredTCDS H9EUAirframe · Eurocopter AS 350 B3TCDS E00054ENEngine · Turbomeca ARRIEL-2B1

From the FAA registry file of October 24, 2026.

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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
See all 144 ADs

Information bulletins that may apply · 9

Advisory, not mandatory.

Historical bulletins · 2
SAIB SW-17-23R1Fuel SystemIssued Mar 2, 2018SAIB SW-17-23Fuel SystemIssued Aug 24, 2017

NTSB investigations · 1

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

NTSB WPR10CA164Accident · No injuriesData collectionFinal reportParker, AZThe mechanics' failure to account for all the tools following a maintenance procedure and the pilot's failure to perform a preflight check before a maintenance test flight.Mar 16, 2010 · Substantial damage

FAA incident reports · 1

FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.

Accident 20100316032849AGround/Ramp/Ma · Parker, AZOn 3-16-2010 omniflight helicopter N4282, s/n 4282 located at la paz regional Hospital, Parker, AZ sustained damage to one main rotor blade, right side of tailboom and lower vertical fin. The damage occured due to a 12" crescent wrench being left on or near…Mar 16, 2010 · Substantial damage

Service difficulty reports · 8

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

SDR 2022FA0000034Tail Boom · chafedTAIL BOOM SERVO RH BEAM (PN: 350A23-4015.24) IN THE FORM OF A CHAFE. THE CHAFE DAMAGE WAS MEASURED TO BE APPROXIMATELY 0.50” X 0.10” AND 0.015” DEEP.Jan 18, 2022 · N4282 · Airbus A300* · Rotorcraft Tail BoomSDR 2022FA0000033Skin · chafedTAILBOOM P/N 350A23-0000-0705 S/N TB4490 SKIN DAMAGE AT APPROXIMATELY X1219 RBL 228. THE DAMAGE IS MINOR CHAFING MEASURING 0.005” AT ITS DEEPEST.Jan 18, 2022 · N4282 · Snias AS350B3 · Rotorcraft Tail BoomSDR 2021FA0000426None · dentedDAMAGE TO THE ENGINE DECK (PN: 350A21-1239.21) IN THE FORM OF 3EA DENTS AND A CHAFE. THE CHAFE DAMAGE AREA WAS DISCOVERED TO BE NEAR THE SCUPPER DRAIN HOLE.Dec 27, 2021 · N4282 · Snias AS350B3 · Fuselage Structure (General)SDR 2A6R202001104282Frame · chafedL/H INBOARD SIDE OF AFT LOWER LEG OF THE X-FRAME HAS CHAFFING MEASURING APPROXIMATELY 0.011" DEEP AND 0.3" WIDE BY 2.4".Jan 7, 2020 · N4282 · Snias AS350B3 · Fuselage Main, FrameSDR QMLA2016032116025Support Frame · chafedTHE TRANSMISSION SUPPORT FRAME, PN 350A21-1041-143, HAS CHAFING DAMAGE ON THE LOWER FLANGE FROM AN UNSECURED CABLE, PN 704A34-1302-23. PN 350A38-1040-20 ATTACHES TO PN 350A21-1041-143.Mar 21, 2016 · N4282 · Snias AS350B3 · Fuselage Main, Attach FittingsSDR RMXA383298Blade · damagedUPON APPROACH, ACFT SUSTAINED A BIRD STRIKE ON THE PILOT SIDE WIND SCREEN AND WAS PROJECTED INTO THE TAIL ROTOR DUE TO THE DOWN WASH OF THE MAIN ROTOR SYS TECH INSPECTED WINDSCREEN WITH NO DEFECTS NOTED. TAIL ROTOR BLADE AND SPIDER ASSY HAD EVIDENCE OF THE BIRMay 2, 2011 · N4282 · Snias AS350B3 · Tail Rotor BladesSDR RMXA383295Display · malfunctionedDURING APPROACH TO AIRPORT, ACFT INDICATED AN AMBER GOV LIGHT. DOWNLOADED VEMD FAIL 1 CODE OF 0008 AND A FAIL 2 CODE OF 0200. AFTER CONTACTING MFG REPRESENTATIVE IT WAS VERIFIED THAT THESE DISTURBANCES ARE KNOWN AS NUISANCE CODES. CONNECTOR PLUGS WERE CLEANEDApr 28, 2011 · N4282 · Snias AS350B3 · Central DisplaySDR RMXA363942Potentiometer · malfunctionedACFT INDICATED AN AMBER GOV LIGHT IN FLIGHT, WITH NO ENGINE, MAIN ROTOR, OR TAIL ROTOR FLUCTUATIONS IN FLIGHT. TECH RETRIEVED AN INTERMITTENT FAILURE CODE 122 FOR THE COLLECTIVE POTENTIOMETER. WHEN THE ACFT WAS POWERED BACK UP AFTER LANDING THE AMBER GOV LIGHTMar 5, 2011 · N4282 · Snias AS350B3 · Rotorcraft Flight Control

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