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Aircraft record

N917AULockheed P-3A

DeregisteredUnclaimedSource: FAA, updated Oct 20, 2026

This N-number isn't registered right now. Below is its last known registration, canceled Nov 2, 2025.

Safety record in brief:No NTSB accidents or incidents since 1982No ADs since 1998 matched5 service difficulty reports

Registration
Deregistered
Last based in
North Hollywood, CA
owner city / state
Owners
1
on record
NTSB events
None
since 1982
ADs may apply
0
confirm with A&P
Service reports
5
since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026
Last registered owner
Individual owner
City, state
North Hollywood, CA
Canceled
Nov 2, 2025
Airworthiness
Restricted · Forest
Airworthiness date
Apr 25, 2011

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
Lockheed
Model
P-3A
Serial number
150510
Aircraft type
Fixed wing multi engine
Category
Land
Certification
Type Certificated
Seats
10
Engines
4
Max takeoff weight
12,500 - 19,999 lb
Mode S code
ACB0BF

Engine

Make and model
Allison T-56-A-10w
Type
Turbo-prop
Power
4500 hp

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

Ownership history

Ownership history from FAA records
  1. until 2025Individual ownerNorth Hollywood, CA

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 2026 · SDRs · Oct 16, 2026

NTSB events (0)

No NTSB accidents or incidents found for this airframe since 1982.

ADs published since 1998 that may apply (0)

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.

No ADs published since 1998 matched this airframe or engine model.

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

Service Difficulty Reports (5)

Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.

  • Fuselage · attach fitting · crackedFeb 15, 2011

    DURING ANNUAL INSPECTION, A DETAILED ULTRA-SONIC INSPECTION OF THE FUSELAGE WING ATTACH RING FITTINGS WERE INITIATED BY AN INTERNAL SB. FATIGUE CRACKS WERE APPRECIATED IN THE RT FWD FITTING'S CHORDWISE FLANGE AT THE UPPER TENSION BOLT.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Wings · panel · crackedDec 1, 2005

    LOCATED LOWER WING PLANK RISER FRACTURE 7 INCHES IN LENGTH LT WING STA. 167. FRACTURE EMANATED ALONG BASE OF RISER EXTENDING IB AND OB SPANWISE. FRACTURE WAS VISUALLY DETECTED DURING SCHEDULED INSPECTION. FRACTURE WAS PROPAGATED BY THE MAIN LANDING GEAR TRUSS RIB ATTACHING STIFFENER AT THE FORWARD…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Wings · spar cap · corrodedDec 1, 2005

    LT WING UPPER REAR SPAR CAP WS178, AT NACELLE AFT ATTACH PLATE. DISSIMILAR METAL CORROSION ATTACK UPPER CROWN AND VERTICAL LEG. CORROSION WAS VISUALLY DETECTED AT DEPOT LEVEL SCHEDULED INSPECTION. CORROSION WAS FOUND TO EXCEED NEGLIGIBLE DAMAGE LIMITS.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 5 reports
  • Wings · spar cap · corrodedDec 1, 2005

    RT WING REAR SPAR UPPER CAP WS178 AT NACELLE AFT ATTACH PLATE. DISSIMILAR METAL CORROSION ATTACKING UPPER CROWN AND AND VETICAL LEG OF THE SPAR CAP. CORROSION WAS VISUALLY DETECTED AT SCHEDULED DEPOT LEVEL INSPECTION. CORROSION EXCEEDED MAXIMUM NEGLIGIBLE LIMITS.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Wings · spar cap · corrodedDec 1, 2005

    RT WING UPPER FORWARD SPAR CAP W.S.73 (PREVIOUS PROCESSING BY PARTY UNKNOWN) OF THE FORWARD FLANGE HAS EXCEEDED MAXIMUM NEGLIGIBLE LIMITS FOR DAMAGE LOCATION. DUE TO THE RELATIVE LOCATION OF THE WING ATTACH CORNER FITTING THIS DAMAGE CANNOT BE REPAIRED AND WILL REQUIRE A SPAR CAP INSERTION.

    From FAA Service Difficulty Reports; matched by N-number and serial number.

Sources

  • FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 20, 2026
  • NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
  • FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 20, 2026
  • FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

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