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Aircraft record

N833EX1991 Dehavilland DHC-8-106

DeregisteredUnclaimedSource: FAA, updated Oct 20, 2026

This N-number isn't registered right now. Below is its last known registration, canceled Sep 18, 2006.

Safety record in brief:No NTSB accidents or incidents since 19823 ADs may apply19 service difficulty reports

Registration
Deregistered
Last based in
New York, NY
owner city / state
Engine
PW120 · 1800 hp
P&W Canada
Owners
1
since 2004
NTSB events
None
since 1982
ADs may apply
3
confirm with A&P
Service reports
19
since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026
Last registered owner
Cit Capital USA INC
Owner type
Corporation
City, state
New York, NY
Certificate issued
Oct 27, 2004
Canceled
Sep 18, 2006
Airworthiness
Standard · Transport
Airworthiness date
Jul 22, 1991

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-8-106
Year
1991
Serial number
282
Aircraft type
Fixed wing multi engine
Category
Land
Certification
Type Certificated
Seats
44
Engines
2
Max takeoff weight
20,000 and over lb
Mode S code
AB63F9

Engine

Make and model
P&W Canada Pw120
Type
Turbo-prop
Power
1800 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. 2004 – 2006Cit Capital USA INCNew York, NY

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
2014-14-02Pratt & Whitney Canada Corp. Turboprop EnginesAug 15, 2014Engine (PW120)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.
2012-26-08Pratt & Whitney Canada Corp. Turboprop EnginesFeb 15, 2013Engine (PW120)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.
2003-21-03Pratt & Whitney Canada Models PW118, PW120, PW120A, and PW121 Turboprop EnginesNov 20, 2003Engine (PW120)

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

Service Difficulty Reports (19)

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.

  • Electrical power · generator · inoperativeJul 26, 2006

    ABORTED TAKEOFF- NR 2 AIRCRAFT GENERATOR ILLUMINATED DURING TAKEOFF ROLL. REMOVED AND REPLACED NR 2 DC GENERATOR/STARTER IAW MM. OPS CHECK NORMAL MM. (K)

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Propellers · wire harness · groundedJun 26, 2004

    FLIGHT NR 3765 HAD TO RETURN TO GATE DUE TO HAVING THE NR 1 PROP FEATHER WHEN THE AUTOFEATHER SELECT SWITCH WAS SELECTED TO TEST. MAINTENANCE FOUND THE NR 2 ENGINE INTERFACE HARNESS SHOWING A STRAY GROUND TO THE TORQUE SIGNAL CONDITIONING UNIT. HARNESS WAS REPLACED. AIRCRAFT WAS GROUND RUN, ALL…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Lights · battery pack · inoperativeFeb 7, 2003

    DURING SCHEDULED MAINTENANCE VISIT EMERGENCY LIGHTS WOULD NOT TURN OFF WHEN SELECTED TO OFF POSITION IN COCKPIT. LIGHTS WOULD ONLY REMAIN OFF IN ARM POSITION. EMERGENCY LIGHTING SYSTEM TROUBLESHOT. ALL 6 BATTERY PACKS, FLIGHT COMPARTMENT SWITCH, AND POWER CONTROL BOX WERE REPLACED. OPERATIONAL…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reports
  • Hydraulic power · line · leakingJan 26, 2003

    LGA-ITH FLIGHT 3799 CREW REPORTED NR 2 HYDRAULIC QUANTITY LOSS ON TAKEOFF. ISOLATION VALVE LIGHT ILLUMINATED, GEAR PARTIALLY RETRACTED, AND ROLL SPOILER OUTBOARD HYDRAULIC CAUTION LIGHT ILLUMINATED. MAINTENANCE REPLACED BLUE FLEX LINE AT DRAG STRUT ACTUATOR. HYDRAULIC SYSTEM SERVICED AND BLED.…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Lights · battery pack · dischargedJan 29, 2002

    DURING ROUTINE MAINTENANCE VISIT LEFT AFT FUSELAGE AND TWO CENTER OVERHEAD EMERGENCY LIGHTS FOUND TO BE INOPERATIVE. BATTERY PACK AT POSITION 300 REPLACED. AIRCRAFT RETURNED TO SERVICE.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Landing gear · cap · crackedNov 18, 2001

    DURING ROUTINE MAINTENANCE VISIT, PISTON CAP FOR NOSE LANDING GEAR SHOCK STRUT FOUND BROKEN AT BOTTOM FLANGE. NOSE GEAR SHOCK STRUT PISTON CAP, AND LOWER PIN AND BUSHING FOR NOSE GEAR LOWER LINK REPLACED. WORK COMPLETED IN ACCORDANCE WITH COMPONENT MAINTENANCE MANUAL AND ALLEGHENY JOB CARD…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Lights · wire · brokenSep 22, 2001

    DURING ROUTINE MAINTENANCE VISIT, FOUND FORWARD EMERGENCY EXIT PATH RED LIGHT INOPERATIVE. BROKEN WIRE REPAIRED IN PATH LIGHT TRACK. ALSO REPOSITIONED LAMP HOLDER LENS ASSEMBLY TO CORRECT POSITION. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Stabilizers · rivet · looseJul 29, 2001

    DURING ROUTINE MAINTENANCE VISIT LEFT ELEVATOR FOUND TO HAVE ONE NR 4 RIVET WORKING AND ONE TIGHT NR 6 FASTENER. FASTENERS REPLACED IN ACCORDANCE WITH DEHAVILLAND REPAIR DRAWING RD8-55-324 AND 8110-3 FORM FROM CALLAHAN REPAIR SERVICES CAS-AAL-03. AIRCRAFT RETURNED TO SERVICE.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · structure · crackedAug 4, 2000

    MDT - DURING A SPOT INSPECTION THE REAR FUSELAGE STRUCTURE WAS FOUND CRACKED, LEFT AND RIGHT SIDES AT FRAME 4 STRINGER 4. REPAIRS WERE MADE IAW DHC RD8-55-199. AIRCRAFT WAS RETURNED TO SERVICE.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Engine · valve · malfunctionedJul 1, 1999

    FLT 3635 - BWI, IN FLIGHT AFTER CRUISE POWER LEVERS WERE BROUGHT BACK TO IDLE, AN ELECTRICAL ODOR WAS NOTICED. MAINTENANCE RAN ACFT AND ISOLATED NR 2 ENGINE. INSPECTED ENGINE, NO LEAKS NOTED. REMOVED AND CLEANED AIR SWITCHING VALVE. REINSTALLED VALVE IAW P&W M/M 72-30-00. RAN ACFT, OPS CHECK OK.

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

Showing the 10 most recent of 19 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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