OpenAirDocs.org

N398EH

Cancelled 2015
Open the Markdown

Deregistered aircraft · 1976 Bell Helicopter Textron 212 · Pratt & Whitney Canada PT6T-3

Open in FAA registry

© OpenStreetMap
Cancelled
April 10, 2015
Exported to
Canada
Status when cancelled
Valid registration
Serial number
30766
Year built
1976
Type
Rotorcraft
Engine
Turbo-shaft
Airworthiness
Standard, transport
Airworthiness date
June 17, 1997
Certificate issued
February 23, 2015
Last registry action
February 23, 2015
Mode S code
A4A0ED
Owner when cancelled
Copter Lease LLC Trustee
Location
Albuquerque, NM
Owner type
Corporation
Airframe modelBell Helicopter Textron 212TCDS H4SW · ADs, bulletins and aircraft registered nowEngine modelPratt & Whitney Canada PT6T-3TCDS E22EA · Turbo-shaft

From the FAA registry file of October 31, 2026, cancelled registrations. Owners’ street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

NTSB investigations · 1

Matched to this aircraft by N398EH and the event date: up to this one’s cancellation.

NTSB DEN77FA005Accident · Serious injuriesClosedCasper, WYOct 17, 1976 · Substantial damage

FAA incident reports · 1

FAA accident and incident reports matched to this aircraft by N398EH and the event date: up to this one’s cancellation.

Accident 19761017042139APower On Descent (Rotorcraft) · Casper, WYInadvertant and/or unrecognized rotor system over speed. No.4 tail rotor drive shft crit. Spd. LowOct 17, 1976 · Substantial damage

Service difficulty reports · 3

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

SDR SAJF2014062603020Engine · leakingDURING FLIGHT AFTER 5 HOURS AFTER TAKEOFF, THE PILOT OBSERVED LOW OIL QTY ON NR 2 ENG & NORMAL OIL PRESS WAS MAINTAINED. AFTER INTERVAL DISCUSSION, PILOT CHOSE TO DIVERT FOR AN UNEVENTFUL LANDING. DURING GND INSPECTION, OBVIOUS OIL LEAKAGE UNDER COMPRESSOR RJun 16, 2014 · N398EH · Bell 212 · Engine (Turbine/Turboprop)SDR EHA2004F00003Line · chafedHYDRAULIC LEAK FROM AREA OF CARGO HOOK. TRACED TO TAIL ROTOR SAS LINK HYDRAULIC LINE CHAFED BY FUEL VENT LINE. REPLACED LINE, REROUTED AND SECURED FUEL VENT LINE. LEAK CHECKED AND MOC FLIGHT GOOD. (AL03200404250)Jul 13, 2004 · N398EH · Bell 212 · Hydraulic System, MainSDR EHA2002F00005Fire Loop · brokenAPPROX 0.5 HOURS AFTER TAKEOFF, ENROUTE FOR CROSS COUNTRY, THE NR 1 ENGINE FIRE (T) HANDLE ILLUMINATED IN FLIGHT. HANDLE WAS PULLED TO FIRE NR 1 ENGINE MAIN FIRE BOTTLE, NR 1 ENGINE WAS SHUT DOWN AND SECURED, AND HELICOPTER RETURNED TO BASE. UPON INSPECTION Jun 1, 2002 · N398EH · Bell 212 · Fire Detection