Aircraft record

N62PJ1997 Mcdonnell Douglas Helicopter 369E

DeregisteredUnclaimedSource: FAA, updated Oct 17, 2026

This N-number isn't registered right now. Below is its last known registration, canceled Nov 6, 2013.

Safety record in brief:1 NTSB accident (substantial damage, Aug 2013)3 ADs may apply

Registration: Deregistered
Last based in: Red Bluff, CA; owner city / state
Engine: 250-C20 SER · 420 hp; Allison
Owners: 1; since 2001
NTSB events: 1; substantial, 2013
ADs may apply: 3; confirm with A&P
Service reports: 0; since 1995

Registration

FAA Aircraft Registry · Oct 17, 2026

Last registered owner: P J Helicopters
Owner type: Corporation
City, state: Red Bluff, CA
Certificate issued: Mar 26, 2001
Canceled: Nov 6, 2013
Airworthiness: Standard · Normal
Airworthiness date: Feb 12, 1997

We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.

Airframe & engine

FAA Registry + type data

Airframe

Manufacturer: Mcdonnell Douglas Helicopter
Model: 369E
Year: 1997
Serial number: 0535E
Aircraft type: Rotorcraft
Category: Land
Certification: Type Certificated
Seats: 4
Engines: 1
Max takeoff weight: Up to 12,499 lb
Type certificate data sheet: H3WE
Mode S code: A81532

Engine

Make and model: Allison 250-C20 Ser
Type: Turbo-shaft
Power: 420 hp

Total time and engine hours aren't public. They appear here once the owner adds logbooks.

Ownership history

Ownership history from FAA records

2001 – 2013P J HelicoptersRed Bluff, CA
1995 – 1997Fox Aircraft CorporationMinden, NV · different airframe: Fox Aircraft Corporation Pj-2 S/N 001

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 17, 2026 · SDRs · Oct 16, 2026

NTSB events (1)

Accident · substantial damage

Aug 12, 2013 · Burns, OR

The total loss of engine power during cruise flight due to the separation of one of the 4th-stage turbine wheel blades due to low-cycle fatigue cracking that had progressed to high-cycle fatigue cracking, which ultimately led to the overload failure of the blade.

Damage: Substantial
Injuries: None
Report: WPR13GA374

From NTSB records; matched by serial number.Read NTSB report (search CAROL for WPR13GA374)

Accident history for this model

ADs published since 1998 that may apply (3)

These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.

AD	Subject	Effective	Applies to
2006-16-04	Rolls-Royce Corporation (Formerly Allison Engine Company, Allison Gas Turbine Division…	Sep 7, 2006	Engine (250-C20 SER)
2006-13-06	Rolls-Royce Corporation (Formerly Allison Engine Company, Allison Gas Turbine Division…	Jul 26, 2006	Engine (250-C20 SER)Only with: Engines with gas producer rotor assembly tie bolt P/Ns A23008020, E23008020 (EXTEX), 23008020, 6843388, 6876991 (RRC), A23008020 (SAP), or 23008020P (Pacific Sky Supply) installed.
2005-10-13	Rolls-Royce Corporation (Formerly Allison Engine Company) 250-B17B, -B17C, -B17D, -B17E…	Jun 22, 2005	Engine (250-C20 SER)Only with: Engines that do not have turbine energy absorbing ring RRC P/N 23035175, or an equivalent FAA-approved serviceable ring, installed.

AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.

Service Difficulty Reports (0)

No Service Difficulty Reports found for this airframe since 1995.

Sources

FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 17, 2026
NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 17, 2026
FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

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