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Aircraft record

N337EN1991 Boeing Of Canada/Dehav Div DHC-8-311

DeregisteredUnclaimedSource: FAA, updated Oct 20, 2026

This N-number isn't registered right now. Below is its last known registration, canceled Oct 5, 2023.

Safety record in brief:No NTSB accidents or incidents since 19823 ADs may apply133 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
133
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 18, 2007
Canceled
Oct 5, 2023
Airworthiness
Standard · Transport
Airworthiness date
Feb 15, 2002

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
Boeing Of Canada/Dehav Div
Model
DHC-8-311
Year
1991
Serial number
284
Aircraft type
Fixed wing multi engine
Category
Land
Certification
Type Certificated
Seats
39
Engines
2
Max takeoff weight
20,000 and over lb
Mode S code
A3B041

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 – 2023Wells 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 (133)

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.

  • Landing gear · brake · defectiveMay 1, 2018

    UNDER MODERATE BRAKE ACTION, A/C SHUDDERS WITH ANTI-SKID ON DURING SLOWER TAXI SPEEDS. R&R NR 3 AND NR 4 BRAKE ASSY IAW 32-42-11. OPS CHECK GOOD. CLEAR MEL.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Lights · wire harness · brokenMar 21, 2018

    BROKEN FLOOR EMERGENCY LIGHT, ROW 1. MANUFACTURED WIRE HARNESS IAW WIRING DIAGRAM 33-52-01.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Hydraulic power · line · failedJan 12, 2018

    NR 2 HYDRAULIC QTY ZERO AFTER TAKE OFF. RETURNED TO FIELD. R & R THE RT NOSE GEAR DRAG STRUT ACTUATOR LINE, SERVICED AND BLED THE HDYRAULIC SYSTEM . GROUND RUNS AND LEAK CHECKED GOOD.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reports
  • Air conditioning and pressurization · unknown · odorDec 20, 2017

    ACRID ODOR PRESENT IN CABIN. SEEMS TO BE FROM FORWARD OVERHEAD AIR VENT. INSPECTED THE CENTER CEILING AREA FOR SIGNS OF OVERHEAT. GROUND RAN THE ACFT AND OPERATED THE BLEED SYSTEM AND CYCLED THE INVERTERS. NO DEFECTS OR ODORS PRESENT. OKAY FOR SERVICE.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Lights · light · inoperativeAug 24, 2017

    ONE WHITE EMERGENCY FLOOR LIGHT AT ROW 4 IS INOPERATIVE. R & R THE EMERGENCY LIGHT. OPS CHECKED GOOD. OK FOR SERVICE.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Navigation · computer · failedAug 14, 2017

    NR 2 AHRS FAILED INFLIGHT. CREW REPORTED ASSOCIATED SYSTEM FAILURES AS WELL. R & R THE NR 2 AHRS COMPUTER IAW MM 34-20-01. OPS CHECKED GOOD.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Communications · electronic unit · failedAug 5, 2017

    BURNING ODOR IN CABIN AND FLIGHT DECK WITH LOSS OF INTERPHONE. CAPTAIN PULLED THE CIRCUIT BREAKER M1 AS A PRECAUTION. RESET CIRCUIT BREAKERS M1 & J1, AND FOUND ALL PA INTERPHONE LIGHTS ILLUMINATED WITH AN AUDIO POP SOUND OVER ALL SPEAKERS. INSPECTED WIRING AT BOTH F/A STATIONS, PA AMPLIFIER & PA…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Hydraulic power · indicator · inoperativeJul 18, 2017

    NR 1 MAIN HYD PRESSURE INDICATOR READS 0 WITH NO ASSOCIATED ADVISORY LIGHTS ILLUMINATED. R & R THE NR 1 HYD PRESSURE INDICATOR, GROUND RAN THE ACFT. OPS CHECKED GOOD. OK FOR SERVICE.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Lights · socket · inoperativeJul 14, 2017

    RED FLOOR EMERGENCY LIGHT FROM FRONT IS INOPERATIVE. INSTALLED A NEW EMERGENCY LIGHT. IAW AMM 20-45-07. OPS CHECKED GOOD.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Propellers · propeller · malfunctionedJun 4, 2017

    WHEN PROPELLER LEVERS AT MAX FOR LANDING, RPM SPLIT MORE THAN 30 RPM. NR 1 ENGINE 1175 AND NR 2 AT 1120 RPM. GROUND RAN AIRCRAFT IAW GROUND RUN UP MANUAL AT MIN AND MAX POWER ALL PARAMETERS WITHIN LIMITS, OPS CHECKED GOOD, OK FOR SERVICE.

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

Showing the 10 most recent of 133 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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