N511AV1986 Dehavilland DHC-8-103
This N-number isn't registered right now. Below is its last known registration, canceled Jan 30, 2021.
Safety record in brief:No NTSB accidents or incidents since 19823 ADs may apply10 service difficulty reports
- Registration
- Deregistered
Registration
FAA Aircraft Registry · Oct 17, 2026- Last registered owner
- Wells Fargo Trust Co NA Trustee
- Owner type
- Corporation
- City, state
- Salt Lake City, UT
- Certificate issued
- Jul 26, 2010
- Canceled
- Jan 30, 2021
- Airworthiness
- Standard · Transport
- Airworthiness date
- Jul 28, 2010
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 dataAirframe
- Manufacturer
- Dehavilland
- Model
- DHC-8-103
- Year
- 1986
- Serial number
- 051
- 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
- A6653A
Engine
- Make and model
- P&W Canada Pw121
- Type
- Turbo-prop
- Power
- 1950 hp
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- 2010 – 2021Wells 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 17, 2026 · SDRs · Oct 16, 2026NTSB 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.
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2014-14-02 | Pratt & Whitney Canada Corp. Turboprop Engines | Aug 15, 2014 | Engine (PW121)Only with: PW120, PW121, PW121A engines with Post SB21610 configuration; PW124B, PW127, PW127E, PW127F engines with Post SB21607 and/or Post SB21705 configuration; PW127G and PW127M engines unconditionally. |
| 2012-26-08 | Pratt & Whitney Canada Corp. Turboprop Engines | Feb 15, 2013 | Engine (PW121)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. |
| 2003-21-03 | Pratt & Whitney Canada Models PW118, PW120, PW120A, and PW121 Turboprop Engines | Nov 20, 2003 | Engine (PW121) |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (10)
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.
- Air conditioning and pressurization · acm · failedSep 9, 2013
DURING DECENT AT FLIGHT IDLE, A BURNING ODOR OCCURED. DUCT TEMPERATURE WAS AT 0 DEGREES, SWITCHED THE TEMP CONTROL TO MANUAL AND INCREASED INPUT TO WARM. ODOR DISSAPTED. DURING ENGINE RUNS BLEEDS OFF, NO ODORS NOTED, WITH NR 2 BLEED ON FULL COLD NOTICE OIL ODOR. TURNED NR 2 BLEED OFF, ODOR…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Air conditioning and pressurization · duct · separatedSep 7, 2013
A/C PACK HOT CAUTION LIGHT CYCLED CONTINUOUSLY. AT 16K. THERE WAS A BURNING ODOR ASSOCIATED WITH THE LIGHT AFTER SEVERAL MINUTES. FOUND DUCT SEPARATED AT CABIN TRIM VALVE BLOWING HOT BLEED AIR INTO AFT ACCESSORY COMPARTMENT. SECURED DUCTING RAN ENGINES BLEEDS HIGH FOR OVER 20 MINUTES NO ODORS OR…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Landing gear · terminal · looseSep 2, 2013
LANDING GEAR DID NOT EXTEND, ACCOMPLISHED ALT GEAR EXTENSION, 3 GREEN LIGHTS. CHECKED CONTINUITY BETWEEN PSEU AND GEAR SELECTOR HANDLE, NO DEFECTS NOTED. FOUND TERMINAL SCREW ON GEAR INHIBIT SWITCH BACKED HALFWAY OUT. RESECURED TERMINAL ON INHIBIT SWITCH SYS OPS CHECKS GOOD IAW DASH 8, MM 32-30-00.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reportsShow fewer reports
- Engine · unknown · unknownDec 21, 2012
AT V1 AND CLIMB OUT NR 2 ENGINE TORQUE FLUCTUATED PLUS OR MINUS 5 PERCENT FROM TORQUE SETTING. FLUCTUATION WAS NOT AN INDICATOR ISSSUE. MALFUNCTION CONTINUED TO OCCUR WITH ENGINE CONTROL UNIT (ECU) SET TO NORMAL. NO OTHER INDICATIONS NOTED. PERFOMRED ENGINE GROUND RUNS AND ENGINE TRIM CHECKS WITH…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Hydraulic power · line · leakingOct 25, 2012
IN FLIGHT, NOTED SLOW LOSS OF NR 2 HYD QUANTITY. RETURNED TO BASE. AFTER LANDING, RECEIVED NR 2 ISOLATION VALVE CAUTION LIGHT. AFTER SHUTDOWN NOTED LARGE HYD LEAK IN NR 2 WHEEL WELL. RESEATED PRESSURE LINE ON FILTER MANIFOLD ASSY; SERVICED HYD SYS AND PERFORMED SATISFACTORY OPS CHECK.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Landing gear · pseu · failedJun 21, 2012
DURING APPROACH, NOSE GEAR RED LIGHT WOULD NOT EXTINGUISH. AFTER COMPLETEING ALTERNATE GEAR EXTENSION RED NLG LIGHT STAYED ILLUMINATED AND FINALLY EXTINGUISHED AFTER A FEW MINUTES. REMOVED AND REPLACED PSEU AND NOSE GEAR DOWNLOCK PROX SENSOR. PERFORMED EXTENSION AND RETRACTION CHECKS. OPS CHECK…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Landing gear · warning system · false activationJun 19, 2012
ON APPROACH, PIC CALLED FOR GEAR DOWN, OBSERVED THE NLG LIGHT WAS RED. INFORMED THE TOWER THE AC WAS GOING AROUND AND TO REVIEW THE QRH. COMPLIED WITH THE QRH FOR ALTERNATE GEAR EXTENSION, BUT THE LIGHT REMAINED ILLUMINATED. ALTERNATE EXTENSION GEAR LIGHT INDICATED ALL 3 GEAR WERE DOWN AND THE…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Landing gear · bracket · crackedSep 2, 2011
LEFT MLG DRAG STRUT AFT FAIRING ATTACHMENT BRACKET CRACKED IN 2 PLACES. R & R ATTACHMENT BRACKET IAW SRM 51-40-11.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Nacelles and pylons · angle · crackedSep 2, 2011
RT OTBD ENGINE AFT NACELLE LOWER STIFFENER ANGLES CRACKED. COMPLIED WITH PERMANENT REPAIR OF BOTH ANGLES, IAW 8-54-310.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Exhaust · heat shield · gougedSep 2, 2011
NR 2 ENGINE FINGERNAIL UPPER SURFACE PATCH (HEAT SHIELD) DAMAGED. R & R FINGERNAIL PATCH IAW RD 8-54-177.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Sources
- FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 17, 2026
- NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
- FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 17, 2026
- FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026