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Aircraft record

N336EN1992 Dehavilland DHC-8-311

DeregisteredUnclaimedSource: FAA, updated Oct 20, 2026

This N-number isn't registered right now. Below is its last known registration, canceled Mar 20, 2020.

Safety record in brief:No NTSB accidents or incidents since 19823 ADs may apply147 service difficulty reports

Registration
Deregistered
Last based in
Salt Lake City, UT
owner city / state
Engine
PW123 · 2142 hp
P&W Canada
Owners
1
since 2007
NTSB events
None
since 1982
ADs may apply
3
confirm with A&P
Service reports
147
since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026
Last registered owner
Wells Fargo Trust Co NA Trustee
Owner type
Corporation
City, state
Salt Lake City, UT
Certificate issued
Jan 10, 2007
Canceled
Mar 20, 2020
Airworthiness
Standard · Transport
Airworthiness date
Sep 29, 2000

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
Dehavilland
Model
DHC-8-311
Year
1992
Serial number
336
Aircraft type
Fixed wing multi engine
Category
Land
Certification
Type Certificated
Seats
61
Engines
2
Max takeoff weight
20,000 and over lb
Mode S code
A3AC8A

Engine

Make and model
P&W Canada Pw123
Type
Turbo-prop
Power
2142 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. 2007 – 2020Wells Fargo Trust Co NA TrusteeSalt Lake City, UT

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 (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.

ADSubjectEffectiveApplies to
2013-15-08Pratt & Whitney Canada Corp. Turboprop EnginesSep 17, 2013Engine (PW123)Serial numbers per Table 1 of the Appendix of P&WC Service Bulletin No. PW100-72-21823, Revision 3. Only with: First-stage power turbine blade P/N 3120973-01, 3120983-01, or 3054053-01 installed with a serial number listed in the referenced SB table.
2012-26-08Pratt & Whitney Canada Corp. Turboprop EnginesFeb 15, 2013Engine (PW123)Serial numbers per P&WC ASB No. PW100-72-A21813 Rev 3, PW100-72-A21802 Rev 4, and PW100-72-A21798 Rev 5. Only with: Engines with propeller shafts having serial numbers listed in the referenced P&WC ASBs.
2004-20-01Pratt & Whitney Canada Models PW123, PW123B, PW123C, PW123D, PW123E, PW123AF, PW124B…Nov 5, 2004Engine (PW123)Only with: Mechanical fuel controls (MFCs) P/Ns 3244841-21, 3244853-17, 3244855-15, 3244857-14, 3244858-23, 3244871-5, 3244873-4, and 3244874-4 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 (147)

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.

  • Doors · skin · erodedJan 14, 2020

    AFT CARGO DOOR SKINAT FS 639 TO HAVE EROSION DAMAGE IN 2 LOCATIONS. AFTER DAMAGE REMOVAL THE FWD DAMAGE MEASURES .8"L X .140"W, AND THE AFT DAMAGE MEASURES 2.1"L X .308"W. THE 2 DAMAGE LOCATIONS ARE SEPARATED BY 2.058".THE DAMAGED AREAS HAVE THE DAMAGE REMOVED AND NDT VERIFYING NO CRACKS OR…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Doors · proximity sensor · out of adjustApr 25, 2018

    SERVICE DOOR OPEN INDICATION ILLUMINATED SHORTLY AFTER TAKEOFF ROLL WAS INITIATED. ADJUSTED AND TESTED THE SERVICE DOOR PROXIMITY SENSOR IAW MM 52-70-00, OPS CHECKED GOOD.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Navigation · stall warning · false activationMar 23, 2018

    NR 2 STALL SYSTEM FAIL AND PUSHER SYSTEM FAILED. CAUTION LIGHTS ILLUMINATED ON TAKEOFF ROLL. CYCLED SWSP COMP CIRCUIT BREAKERS, STALL SYSTEM 1 AND 2 TESTED NORMALLY.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reports
  • Autoflight · controller · failedNov 6, 2017

    AFCS CONTROLLER INOPERATIVE MESSAGE ON 802 PANEL. R & R AFCS CONTROLLER IAW AMM 22-10-01. OPS CHECKED BAD.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Propellers · propeller · vibrationOct 6, 2017

    MODERATE VIBRATION FROM THE RT PROPELLER. CONSTANT AND WORSENS WITH PROPELLER SPEED CHANGES. R & R THE NR 200 PROPELLER ASSY IAW CARD 61-10-06R, RAN ACFT IAW MOM. OPS CHECKED GOOD NO DEFECTS AT THIS TIME.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Propellers · control unit · malfunctionedSep 20, 2017

    REJECTED TAKE OFF. AUTOFEATHER FAILED TO ARM DURING TAKEOFF. TORQUE WAS AT 88%. R & R THE NR 2 TSCU IAW IAW MM 72-01-10. RAN AIRCRAFT, OPS CHECKED GOOD IAW PDT-8 RUN MANUAL AND W/C 61-21-04Q.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Propellers · circuit breaker · malfunctionedSep 15, 2017

    REJECTED TAKEOFF AT 88 PERCENT TORQUE. AUTOFEATHER WOULD NOT ARM. RETURNED TO GATE. R & R THE RT TORQUE CONDITIONING CIRCUIT BREAKERS. RAN ENGINES IAW MANUAL CHECKING AUTOFEATHER. PERFORMED AUTOFEATHER STATIC CHECK MULTIPLE TIMES. AUTOFEATHER ARMS AT 60 PERCENT TORQUE AND REMAINS THROUGHOUT THE…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Propellers · wire harness · malfunctionedSep 14, 2017

    ABORTED TAKEOFF DUE TO AUTOFEATHER WOULD NOT ARM. COMPLIED WITH FLIGHT CREW PROCEDURES. REMOVED AND RANG OUT THE NR 2 ENGINE STRUT HARNESS AND REINSTALLED . CHECKED GOOD IAW PDT -8 RUN MANUALS. R & R THE NR 1 ENGINE STRUT HARNESS IAW MM 72-01-10.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Propellers · autofeather sys · malfunctionedSep 13, 2017

    AUTO FEATHER FAILED TO ARM AT 65 KTS. REJECTED T/O AND RETURNED TO THE GATE. R & R THE NR 1 ENGINE, COMPLIED WITH AUTO FEATHER AND AUX FEATHER RUNS, IAW SRT MANUAL, OPS CHECKED GOOD.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Propellers · actuator · failedSep 8, 2017

    AUTO FX WOULD NOT ARM. ABORTED TAKE OFF. R & R ACTUATORS FOR 6121-S10,11 FOR BEING FLAT SPOTTED. R & R CIRCUIT BREAKERS FOR LT G-10 & RT G10. CHECKED AUTO FX POWER LVR POTS FOR SERVICEABILITY, CHECKED GOOD. AUTO FX ARMING & STATIC TESTS GOOD IAW SRT MANUAL.

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

Showing the 10 most recent of 147 reports.

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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