Location
Lewes, DE
Owner type
LLC
Serial number
45378
Year built
1980
Type
Rotorcraft
Engine
Turbo-shaft
Airworthiness
Standard, normal
Airworthiness date
February 22, 1980
Certificate issued
March 7, 2017
Expires
March 31, 2030
Mode S code
A021D3

From the FAA registry file of October 24, 2026.

On this page

Airworthiness directives that may apply · 64

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

1980In forceSuperseded2026
ADs by the year they took effect: 71 ADs
19803
19813
19821
19831
19852
19861
19871
19882
19892
19914
19922
19943
19953
19962
19992
20011
20022
20032
20042
20051
20072
20082
20092
20101
20111
20123
20133
20142
20151
20171
20192
20214
20224
20232
20241
See all 73 ADs

Information bulletins that may apply · 7

Advisory, not mandatory.

Historical bulletins · 1

NTSB investigations · 1

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

FAA incident reports · 3

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

Service difficulty reports · 7

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

SDR ALG2005F00003B-Nut · looseDURING TAKEOFF, AIRCRAFT HAD A COMPRESSOR STALL. MAINTENANCE INSPECTED ENGINE INTAKE AND EXHAUST FOR EVIDENCE OF FOD NO DAMAGE NOTED. PERFORMED AN ENGINE AIR LINE LEAK CHECK AND FOUND THE P/C LINE FROM THE GOVERNOR TO THE FUEL CONTROL WITH A LOOSE B-NUT. TONov 8, 2004 · N1075Y · Bell 206L1 · Fuel Control/Turbine EnginesSDR ALG2004F00072B-Nut · looseAIRCRAFT HAD COMPRESSOR STALL ON TAKE OFF. MAINTENANCE INSPECTED ENGINE INTAKE AND EXHAUST FOR EVIDENCE OF FOD, NO DAMAGE NOTED. PERFORMED AN ENGINE AIR LEAK CHECK AND FOUND THE PC LINE FROM THE GOVERNOR TO THE FUEL CONTROL WITH A LOOSE B-NUT. TORQUE CHECKENov 8, 2004 · N1075Y · Bell 206L1 · Fuel Controlling SystemSDR ALG2004F00049Pump · failedWHILE AT A HOVER, MANEUVERING FOR TAKE OFF, NOTICED N2 DROPPED AND STABILIZED BELOW THE RED LINE AND DID NOT RECOVER UNTIL LANDED. REMOVED AND REPLACED STARTER GENERATOR, DID NOT FIX THE PROBLEM. REMOVED ALL ENGINE AIR LINES AND INSPECTED FOR CRACKS AND LEAKAug 19, 2004 · N1075Y · Engine Fuel PumpSDR 95ZZZX5458Link Idler · wornDAILY INSPECTION FOUND BUSHINGS AND BEARINGS WORN BEYOND LIMITS. PARTS REQUIRING REPLACEMENT: 4 EACH 206-010-338-001 SPACERS, 4 EACH 206-010-337-001 BEARINGS, 2 EACH, 206-010-338-003 BUSHINGS, 2 EACH NAS6605D64 BOLTS, 1 EACH 206-010-470-101 BEARING. WORN PAAug 30, 1995 · N1075Y · Bell 206L1 · Main Rotor Mast/SwashplateSDR 95ZZZX5457Lever Assy · wornDAILY INSPECTION FOUND BUSHINGS AND BEARINGS WORN BEYOND LIMITS. PARTS REQUIRING REPLACEMENT: 4 EACH 206-010-338-001 SPACERS, 4 EACH 206-010-337-001 BEARINGS, 2 EACH, 206-010-338-003 BUSHINGS, 2 EACH NAS6605D64 BOLTS, 1 EACH 206-010-470-101 BEARING. WORN PAAug 30, 1995 · N1075Y · Bell 206L1 · Main Rotor Mast/SwashplateSDR 95ZZZX3341Link Idler · wornDAILY INSPECTION FOUND BUSHINGS AND BEARINGS WORN BEYOND LIMITS. PARTS REQUIRING REPLACEMENT: 4 EACH 206-010-338-001 SPACERS, 4 EACH 206-010-337-001 BEARINGS, 2 EACH 206-010-338-003 BUSHINGS, 2 EACH NAS 6605D64 BOLTS, AND 1 EACH 206-010-470-101 BEARING. NORJun 2, 1995 · N1075Y · Bell 206L1 · Main Rotor Mast/SwashplateSDR 95ZZZX3340Link Assy · wornDAILY INSPECTION FOUND BUSHINGS AND BEARINGS WORN BEYOND LIMITS. PARTS REQUIRING REPLACEMENT: 4 EACH 206-010-338-001 SPACERS, 4 EACH 206-010-337-001 BEARINGS, 2 EACH 206-010-338-003 BUSHINGS, 2 EACH NAS 6605D64 BOLTS, AND 1 EACH 206-010-470-101 BEARING. NORJun 2, 1995 · N1075Y · Bell 206L1 · Main Rotor Mast/Swashplate

STCs that may be installed · 459

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

See all 459 STCs