Location
Billings, MT
Owner type
Corporation
Serial number
51212
Year built
1987
Type
Rotorcraft
Engine
Turbo-shaft
Airworthiness
Standard, normal
Airworthiness date
August 25, 1987
Certificate issued
September 30, 2014
Expires
September 30, 2027
Mode S code
A4100E

From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Allison 250-C30 model are included below.

On this page

Airworthiness directives that may apply · 74

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

1979In forceSuperseded2026
ADs by the year they took effect: 82 ADs
19791
19802
19821
19831
19841
19853
19866
19871
19883
19892
19914
19922
19943
19953
19962
19993
20011
20021
20033
20042
20053
20062
20072
20082
20092
20101
20111
20123
20133
20142
20151
20171
20181
20192
20214
20224
20232
20241
See all 84 ADs

Information bulletins that may apply · 8

Advisory, not mandatory.

Historical bulletins · 2

NTSB investigations

No NTSB investigations matched to N361ALMatched 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 Bell 206L-3 aircraft

FAA incident reports

No FAA accident or incident reports matched to N361ALMatched 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 Bell 206L-3 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 3HCR20110927002Shaft · crackedUNIT FAILED TO LIGHT OFF. INSPECTED AND FOUND TORSION SHAFT LEAKING.Sep 27, 2011 · N361AL · Bell 206L3 · Fuel Control/Turbine EnginesSDR 3HCR20110927001Fuel Control · failedAIRCRAFT FAILED TO LIGHT OFF. INSPECTED AND FOUND CUT-OFF UNSERVICABLE.Sep 27, 2011 · N361AL · Bell 206L3 · Fuel Control/Turbine EnginesSDR ALGA096402Blade · separatedFOUND CORROSION AND SEPARATION AT SKIN/SPAR INTERFACE NEAR LOWER OB GRIP FINGER DOUBLER. REMOVED AND REPLACED DEFECTIVE BLADE WITH NEW BLADE. SCRAPPED DEFECTIVE BLADE.Jul 20, 2004 · N361AL · Bell 206L3 · Main Rotor BladesSDR ALG2004F00043Bleed Valve · failedWHILE HOVERING AND IN A RT PEDAL TURN PREPARING FOR TAKE OFF A LOUD BANG WAS HEARD AND AIRCRAFT YAWED MOMENTARILY LT THEN RT. RETURNED TO MAINTENANCE PAD AND SHUT DOWN AND NOTIFIED MAINTENANCE. MAINTENANCE REMOVED BLEED VALVE PN 23005366A, SN FF43547 AND INSJun 25, 2004 · N361AL · Bell 206L3 · Compressor Bleed ValveSDR ALG2004F00038Compressor · stalledAIRCRAFT HAD COMPRESSOR STALL DURING TAKEOFF. MAINTENANCE INSPECTED ENGINE INLET AND COMPRESSOR AREA, FOUND EVIDENCE OF FROG INGESTION. INSPECTED ENGINE COMPRESSOR FOR DAMAGE NO DAMAGE WAS FOUND. PERFORMED ENGINE CHEMICAL WASH AND ENGINE POWER CHECK. OPS CJun 7, 2004 · N361AL · Bell 206L3 · Turbine Engine Compressor SectionSDR ALG2003F00100Compressor · malfunctionedAT HOVER. DURING INITIAL HOVER PRIOR TO TAKE-OFF THE PILOT NOTICED A HIGH PITCH SCREECHING NOISE THAT WAS EVIDENT ONLY DURING HOVER, AT FLAT PITCH THE NOISE GOES AWAY. MAINTENANCE WAS NOTIFIED AND THE MECHANIC CHANGED THE COMPRESSOR, TURBINE AND GEARBOX ASSEOct 7, 2003 · N361AL · Bell 206L3 · Turbine Engine Compressor SectionSDR ALGA085104Fuel Nozzle · defectiveENGINE LOW MOANING/ BURBLING NOISE WITH N1 OSCILLATIONS AT FLIGHT IDLE.Mar 6, 2003 · N361AL · Bell 206L3 · Fuel Injector Nozzle

STCs that may be installed · 471

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

See all 471 STCs