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Aircraft record

N391FL1955 Convair 340

Registration validUnclaimedSource: FAA, updated Oct 18, 2026

Safety record in brief:No NTSB accidents or incidents since 19821 AD may apply12 service difficulty reports

Registration
Valid
expires Jul 31, 2027
Based in
Waterford, MI
owner city / state
Engine
501-D22 · 4050 hp
Allison
Owners
1
since 1998
NTSB events
None
since 1982
ADs may apply
1
confirm with A&P
Service reports
12
since 1995

Registration

FAA Aircraft Registry · Oct 18, 2026
Registered owner
Ifl Group INC
Owner type
Corporation
City, state
Waterford, MI
Certificate issued
Jun 5, 1998
Expires
Jul 31, 2027
Airworthiness
Standard · Transport
Airworthiness date
Jun 29, 1998

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
Convair
Model
340
Year
1955
Serial number
278
Aircraft type
Fixed wing multi engine
Category
Land
Certification
Type Certificated
Seats
46
Engines
2
Max takeoff weight
20,000 and over lb
Mode S code
A48708

Engine

Make and model
Allison 501-D22
Type
Turbo-prop
Power
4050 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. 1998 – nowIfl Group INCWaterford, MI · current

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 18, 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 (1)

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
2006-25-12Rolls-Royce Corporation 501-D Series Turboprop EnginesJan 23, 2007Engine (501-D22)

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

Service Difficulty Reports (12)

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 indicating · tach generator · strippedMay 13, 2025

    RIGHT ENGINE RPM SPOOLED DOWN IN FLIGHT. ENGINE WAS SHUTDOWN. SUBSEQUENT INSPECTION FOUND THAT TACH GENERATOR DRIVE SHAFT WAS SPRIPPED

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · skin panel · corrodedApr 15, 2022

    CORROSION ON FUSLAGE SKIN AT THE WINDOW CUTOUT BETWEEN STRETCH STA 389.5 AND 409.5 LHS. REPAIRED IN ACCRODANCE WITH ENGINEERING REPAIR R278-053-012-002

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Doors · door frame · crackedApr 15, 2022

    MAIN DECK CARGO DOOR CRACKED ON LOWER EDGE FRAME. REPAIRED IN ACCORDANCE WITH ENGINEERING REPAIR R278-052-003-003

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reports
  • Wings · splice plate · corrodedOct 30, 2021

    RH WING WS 8 LOWER SPLICE PLATE PN:340-1610922-8 BETWEEN STRINGER 12 AND FRONT SPAR, CORRODED.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Air conditioning and pressurization · compressor · failedMar 21, 2018

    COMPLETE LOSS OF PRESSURIZATION INFLIGHT.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Windows · window frame · corrodedJul 8, 2016

    CORROSION FOUND ON RIGHT WINDOW FRAME. REMOVED CORROSION, TREATED AND REPAIRED PER DWG R278-053-010-001.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fire protection · sensing element · failedSep 8, 2012

    FIRE WARNING AFTER TAKE-OFF. FOUND SENSING ELEMENT FAILED.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · beam · crackedAug 24, 2012

    LEFT NOSE LANDING GEAR BEAM UPPER CHORD CRACKED.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Wings · attach fitting · crackedOct 23, 2007

    DURING VISUAL INSPECTION OF WING ATTACH FITTING FOUND CRACKS BETWEEN RIVET HOLES UPPER FWD PORTION OF FITTING (LT AFT WING TO FUSELAGE ATTACH FITTING).

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Wings · attach fitting · crackedOct 23, 2007

    DURING VISUAL INSPECTION OF WING ATTACH FITTING FOUND CRACKS BETWEEN RIVET HOLES UPPER FWD PORTION OF FITTING (LT AFT WING TO FUSELAGE ATTACH FITTING).

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

Showing the 10 most recent of 12 reports.

Sources

  • FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 18, 2026
  • NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
  • FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 18, 2026
  • FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

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