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Aircraft record

N412981974 Piper PA-34-200

DeregisteredUnclaimedSource: FAA, updated Oct 20, 2026

This N-number isn't registered right now. Below is its last known registration, canceled Nov 19, 2012.

Safety record in brief:1 NTSB accident (substantial damage, Nov 1987)6 ADs may apply2 service difficulty reports

Registration
Deregistered
Last based in
La Verne, CA
owner city / state
Engine
I0360 SER · 180 hp
Lycoming
Owners
1
since 1995
NTSB events
1
substantial, 1987
ADs may apply
6
confirm with A&P
Service reports
2
since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026
Last registered owner
Air Desert Pacific Corporation
Owner type
Corporation
City, state
La Verne, CA
Certificate issued
Apr 24, 1995
Canceled
Nov 19, 2012
Airworthiness
Standard · Normal
Airworthiness date
Jan 22, 1974

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
Piper
Model
PA-34-200
Year
1974
Serial number
34-7450106
Aircraft type
Fixed wing multi engine
Category
Land
Certification
Type Certificated
Seats
7
Engines
2
Max takeoff weight
Up to 12,499 lb
Mode S code
A4DF42

Engine

Make and model
Lycoming I0360 Ser
Type
Reciprocating
Power
180 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. 1995 – 2012Air Desert Pacific CorporationLa Verne, 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 (1)

Accident · substantial damage

Nov 14, 1987 · Murfreesboro, TN

THE RT WHEEL BRAKE FAILED WHILE THE AIRPLANE WAS TAXIING ON A PARALLEL TAXIWAY. THE FAILURE OCCURRED NEAR THE END OF THE TAXIWAY, JUST AS THE PLT WAS ABOUT TO TURN THE AIRPLANE ONTO THE RWY. THE PLT SUBSEQUENTLY ATTEMPTED TO TURN THE AIRPLANE USING DIFFERENTIAL POWER. THE AIRPLANE CROSSED THE RWY AND RAN INTO TREES ON THE OPPOSITE SIDE OF THE RWY. THE PLT PULLED THE MIXTURE CONTROLS TO IDLE…

Damage
Substantial
Injuries
None
Report
ATL88LA039

From NTSB records; matched by serial number.Read NTSB report (search CAROL for ATL88LA039)

Accident history for this model

ADs published since 1998 that may apply (6)

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.

ADSubjectEffectiveApplies to
2022-09-13Nose/Tail Landing GearMay 31, 2022Airframe (PA-34-200)Certain serial numbers: PA-34-200 34-7250001–34-7450220
2013-02-13Stabilizer Control SystemMar 11, 2013Airframe (PA-34-200)
2010-15-10Piper Aircraft, Inc. PA-28, PA-32, PA-34, and PA-44 Series AirplanesAug 31, 2010Airframe (PA-34-200)Certain serial numbers: PA-28-140 28-20001–28-26946; PA-28-140 28-7125001–28-7725290; PA-28-150 28-03; PA-28-150 28-1–28-4377; PA-28-150 28-1760A; PA-28-160 28-03; …
2005-13-16The New Piper Aircraft, Inc. PA-34 Series AirplanesAug 8, 2005Airframe (PA-34-200)
97-01-01 R1The New Piper Aircraft, Inc. PA-24, PA- 28R, PA-30, PA-32R, PA-34, and PA-39 Series…Dec 8, 1998Airframe (PA-34-200)Certain serial numbers: PA-28R-180 28R-30002–28R-31135; PA-28R-180 28R-7130001–28R-7130013; PA-28R-200 28R-35001–28R-35820; PA-28R-200 28R-7135001–28R-7635539; PA-28R-201 28R-7737002–28R-7737096; PA-28R-201T 28R-7703001–28R-7703239; …. Only with: All serials of PA-24, PA-24-250, PA-24-260, PA-24-400, PA-30, PA-39; PA-28R, PA-32R, PA-34 models (all serials of PA-34-200) only if not equipped with Piper P/N 78717-02 (or FAA-approved equivalent) main gear sidebrace stud in both main gear sidebrace bracket assemblies.
Show all 6 ADs
ADSubjectEffectiveApplies to
98-04-27The New Piper Aircraft Corporation Models PA-23, PA-23-160, PA-23-235, PA-23-250…Mar 13, 1998Airframe (PA-34-200)

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

Service Difficulty Reports (2)

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.

  • Engine controls · rod end · failedJun 29, 1999

    ROD END CONNECTS THROTTLE CABLE TO ARM AT SERVO. BALL SEPARATED FROM SOCKET. ENGINE WENT TO FULL POWER AND HAD TO BE FEATHERED TO LAND.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Windows · window · departedAug 1, 1997

    PILOT'S LEFT SIDE WINDOW DEPARTED AIRCRAFT DURING FLIGHT. PILOTS REPORTED NO ADVERSE FLIGHT CHARACTERISTICS AFTER WINDOW DEPARTED. PILOT REPORTED THAT WINDOW WAS CRACKED AT WING WINDOW PRIOR TO FLIGHT. SUSPECT CAUSE OF TOTAL FAILURE WAS WING WINDOW LEFT OPEN FOR COOLING AND BROKEN SECTION OF…

    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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