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Aircraft record

N3582X1980 Piper PA-31-350

DeregisteredUnclaimedSource: FAA, updated Oct 19, 2026

This N-number isn't registered right now. Below is its last known registration, canceled Apr 16, 2021.

Safety record in brief:No NTSB accidents or incidents since 198213 ADs may apply9 service difficulty reports

Registration
Deregistered
Last based in
Pearce, AZ
owner city / state
Engine
TI0-540 SER · 310 hp
Lycoming
Owners
1
since 1990
NTSB events
None
since 1982
ADs may apply
13
confirm with A&P
Service reports
9
since 1995

Registration

FAA Aircraft Registry · Oct 19, 2026
Last registered owner
Airpac Airlines INC
Owner type
Corporation
City, state
Pearce, AZ
Certificate issued
Sep 26, 1990
Canceled
Apr 16, 2021
Airworthiness
Standard · Normal
Airworthiness date
Mar 13, 1980

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-31-350
Year
1980
Serial number
31-8052105
Aircraft type
Fixed wing multi engine
Category
Land
Certification
Type Certificated
Seats
8
Engines
2
Max takeoff weight
Up to 12,499 lb
Mode S code
A40539

Engine

Make and model
Lycoming Ti0-540 Ser
Type
Reciprocating
Power
310 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. 1990 – 2021Airpac Airlines INCPearce, AZ

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 19, 2026 · SDRs · Oct 16, 2026

NTSB events (0)

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

Accident history for this model

ADs published since 1998 that may apply (13)

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
2017-10-20Fuselage--Main BulkheadJun 29, 2017Airframe (PA-31-350)Certain serial numbers: PA-31 31-2–31-900; PA-31 31-7300901–31-8312019; PA-31-300 31-2–31-900; PA-31-300 31-7300901–31-8312019; PA-31-325 31-2–31-900; PA-31-325 31-7300901–31-8312019; …
2016-08-18Engine Fuel and ControlJun 6, 2016Airframe (PA-31-350)Certain serial numbers: PA-31-350 31-5001–31-5004; PA-31-350 31-7305005–31-8452024; PA-31-350 31-8253001–31-8553002. Only with: Equipped with Lycoming LTIO-540-J2B/TIO-540-J2B or LTIO-540-J2BD/TIO-540-J2BD engines and fuel pump hose assemblies Piper P/N 39995-034 or Lycoming P/N LW-12877-6S142.
2016-05-01FuselageApr 15, 2016Airframe (PA-31-350)Certain serial numbers: PA-31 31-2–31-900; PA-31 31-7300901–31-8312019; PA-31-300 31-2–31-900; PA-31-300 31-7300901–31-8312019; PA-31-325 31-2–31-900; PA-31-325 31-7300901–31-8312019; …
2013-10-04Engine ExhaustJul 17, 2013Airframe (PA-31-350)Only with: Applies to turbocharged airplanes.
2009-13-06 R1Piper Aircraft, Inc. AirplanesNov 3, 2011Airframe (PA-31-350)Only with: Equipped with a baggage door in the fuselage nose section (nose baggage door).
Show all 13 ADs
ADSubjectEffectiveApplies to
2000-25-01The New Piper Aircraft, Inc. (formerly Piper Aircraft Corporation) PA-31 Series AirplanesJan 19, 2001Airframe (PA-31-350)Certain serial numbers: PA-31 31-2–31-900; PA-31 31-7300901–31-8312019; PA-31-300 31-2–31-900; PA-31-300 31-7300901–31-8312019; PA-31-350 31-5001–31-5004; PA-31-350 31-7305005–31-8553002; …. Only with: Equipped with Piper P/N 46653-00 or 47529-32 aluminum main landing gear door hinge assemblies (or FAA-approved equivalents); aircraft referred to as PA-31-310 are PA-31 airplanes.
2000-06-06The New Piper Aircraft, Inc. PA-31 Series AirplanesMar 23, 2000Airframe (PA-31-350)Only with: Equipped with pneumatic deicing boots.
99-12-05The New Piper Aircraft, Inc. Models PA- 31, PA-31-300, PA-31-325, PA-31-350, and…Jul 23, 1999Airframe (PA-31-350)Certain serial numbers: PA-31 31-2–31-8312019; PA-31-300 31-2–31-8312019; PA-31-325 31-2–31-8312019; PA-31-350 31-5001–31-8553002; PA-31P-350 31P-8414001–31P-8414050. Only with: Airplanes not equipped with the improved design elevators or elevator spar assemblies specified in the Material Required Table of Piper Service Bulletin No. 998A, dated August 4, 1997.
99-06-01The New Piper Aircraft, Inc. Models PA- 31, PA-31-300, PA-31-325, PA-31-350, and…Apr 20, 1999Airframe (PA-31-350)Certain serial numbers: PA-31 31-2–31-8312019; PA-31-300 31-2–31-8312019; PA-31-325 31-2–31-8312019; PA-31-350 31-5001–31-8553002; PA-31P-350 31P-8414001–31P-8414050
98-09-25The New Piper Aircraft, Inc. Models PA- 31, PA-31-300, PA-31-325, and PA-31-350 AirplanesJun 15, 1998Airframe (PA-31-350)Certain serial numbers: PA-31 31-2–31-8312019; PA-31-300 31-2–31-8312019; PA-31-325 31-2–31-8312019; PA-31-350 31-5001–31-8553002
98-08-18The New Piper Aircraft, Inc. Models PA- 31, PA-31-300, PA-31-325, PA-31-350, and PA-31P…May 26, 1998Airframe (PA-31-350)Certain serial numbers: PA-31 31-2–31-8312019; PA-31-300 31-2–31-8312019; PA-31-325 31-2–31-8312019; PA-31-350 31-5001–31-8553002; PA-31P 31P-1–31P-7730012
98-04-27The New Piper Aircraft Corporation Models PA-23, PA-23-160, PA-23-235, PA-23-250…Mar 13, 1998Airframe (PA-31-350)
96-10-14The New Piper Aircraft, Inc. (Formerly Piper Aircraft Corporation) PA31, PA31P, and…Jun 27, 1996Airframe (PA-31-350)Certain serial numbers: PA31 31-2–31-8312019; PA31-300 31-2–31-8312019; PA31-325 31-2–31-8312019; PA31-350 31-5001–31-8553002; PA31P 31P-2–31P-7730012; PA31P-350 31P-8414001–31P-8414050; …. Only with: Applies to airplanes without improved design MLG forward sidebraces P/N 85165-02/-03 or P/N 85166-02/-03 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 (9)

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.

  • Reciprocating engine · rocker box tab · wornJun 23, 1997

    ROCKER PIN RETAINING TAB ON COVER WORN EXCESSIVELY. THIS ENGINE HAS 180 HOURS TSOH!

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Lights · light · contact burnsAug 14, 1996

    ELECTRICAL CONTACT BUTTON FOR LAMP CENTER ELECTRODE IS INADEQUATE TO SUPPORT HIGH HEAT GENERATED BY HIGH AMPERAGE FLOW THROUGH LAMP. CONTACT BUTTON BURNS AWAY REQUIRING REPLACEMENT OF (EXPENSIVE) LIGHT BASE ASSEMBLY. MULTIPLE FLEET FAILURES.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Engine oil · valve · wornJun 3, 1996

    INSPECTION FOUND THE CENTER SPRING ASSY RETAINING CLIP LOOSE ON THE VERNATHERM BODY.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 9 reports
  • Engine oil · valve · nut looseJun 3, 1996

    THE END RETAINING NUT ON THE VERNATHERM IS LOOSE. LYCOMING SB 518C DOES NOT APPLY TO THIS PART NUMBERED VERNATHERM.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Starting · starter · burnedJan 4, 1996

    ADDENDUM TO SDR DATED 1-4-96. RT ENGINE STARTER MOTOR FIELD WINDINGS FAILED, APPARENTLY WHILE STARTER ENGAGED TO CRANK THE ENG RESULTING IN A SHORT-TO-GROUND OF STARTER POWER CIRCUIT. PILOT HAD NO INDICATIONS OF TROUBLE, AND ENG STARTED NORMALLY AND CONTINUED TO RUN NORMALLY DURING PRE-FLT RUN-UP.…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Turbochargers · bolt · looseDec 4, 1995

    BOLTS THAT SECURE TURBO MOUNT TRUSS TO ENGINE MOUNT PYLONS CONTINUALLY WORK LOOSE. NUTS CHATTER ON THREADS AND WEAR TO A POINT WHERE RE-TORQUING IS NOT POSSIBLE. MAIN PROBLEM IS STEEL BOSS ON TURBO MOUNT EATING INTO ALUMINUM MOUNT PYLON. SUBMITTER SUGGESTS SHOULDERED STEEL BUSHING BE PRESS-FIT…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Engine oil · valve · crimp nut looseNov 15, 1995

    DURIGN INSPECTION PER LYCOMING SB 518C, CRIMP NUT FOUND LOOSE ON SHAFT. NOTE THAT SERIAL NUMBER OF THIS UNIT IS BEYOND RANGE OF SERVICE BULLETIN AND THEORETICALLY, HAS BEEN REDESIGNED TO ELIMINATE THIS PROBLEM.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Engine oil · valve · loose crimp nutSep 28, 1995

    VERNATHERM VALVE WAS REMOVED FROM ENGINE, RETAINING NUT WAS FOUND LOOSE. THIS VERNATHERM DID NOT APPLY TO SB 518C BY SERIAL NUMBER. IT WAS INSPECTED DUE TO PREVIOUS REPORTS OF VERNATHERM FAILURES WHICH MET SB 518C CRITERIA. SUBMITTER STATED POOR DESIGN, RE-DESIGN PART.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Engine oil · vernatherm valve · defectiveJan 29, 1995

    VERNATHERM VALVE DOES NOT MOVE UNTIL OIL TEMPERATURE REACHES 235 DEGREES FAHRENHEIT. RED-LINE IS 245 DEGREES FAHRENHEIT.

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

Sources

  • FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 19, 2026
  • NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
  • FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 19, 2026
  • FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

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