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Aircraft record

N808WP1986 Dehavilland DHC-8-103

DeregisteredUnclaimedSource: FAA, updated Oct 19, 2026

This N-number isn't registered right now. Below is its last known registration, canceled Sep 8, 2017.

Safety record in brief:No NTSB accidents or incidents since 19823 ADs may apply41 service difficulty reports

Registration
Deregistered
Last based in
Honolulu, HI
owner city / state
Engine
PW120 · 1800 hp
P&W Canada
Owners
1
since 2010
NTSB events
None
since 1982
ADs may apply
3
confirm with A&P
Service reports
41
since 1995

Registration

FAA Aircraft Registry · Oct 19, 2026
Last registered owner
Hawaii Island Air INC
Owner type
Corporation
City, state
Honolulu, HI
Certificate issued
Nov 8, 2010
Canceled
Sep 8, 2017
Airworthiness
Standard · Transport
Airworthiness date
Jun 8, 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-8-103
Year
1986
Serial number
026
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
AB0197

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. 2010 – 2017Hawaii Island Air INCHonolulu, HI

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 19, 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 (41)

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 · bolt · shearedJun 29, 2009

    ON SELECTION OF GEAR UP AFTER TAKEOFF, THE LANDING GEAR FAILED TO RETRACT AND THE NR 2 HYD ISO VLV CAUTION LIGHT ILLUMINATED. EMERGENCY DECLARED AND AIRCRAFT RETURNED TO OGG. (MX) REPLACED THE NLG DOOR SOLENOID SEQUENCE VALVE. NOTE: 2 OF 4 HOUSING BOLTS ON THE SOLENOID VALVE FAILED.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fire protection · smoke detector · malfunctionedSep 11, 2008

    ON APPROACH, "SMOKE" WARNING LIGHT CAME ON, REMAINED ON FOR 3 SECONDS THEN WENT OUT. AFTER LANDING LIGHT CAME ON AGAIN THEN WENT OUT AFTER A FEW SECONDS. VISUALLY INSPECTED NR 1 AND NR 2 SMOKE DETECTORS, NO DEFECTS NOTED. PERFORMED OPS CHECK OF SMOKE DETECTION SYSTEM GOOD IAW MM 26-12-00, PG 201.…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fire protection · smoke detector · false activationSep 11, 2008

    ON APPROACH, "SMOKE" WARNING LIGHT CAME ON, REMAINED ON FOR 3 SECONDS THEN WENT OUT. AFTER LANDING LIGHT CAME ON AGAIN THEN WENT OUT AFTER A FEW SECONDS. VISUALLY INSPECTED NR 1 AND NR 2 SMOKE DETECTORS, NO DEFECTS NOTED. PERFORMED OPS CHECK OF SMOKE DETECTION SYSTEM GOOD IAW MM 26-12-00, PG 201.…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reports
  • Fire protection · smoke detector · false activationNov 29, 2007

    (PIREP) SMOKE WARNING LIGHT ILLUMINATED BRIEFLY INFLIGHT. NO SMOKE DETECTED. PAX IN REAR OF PLANE HAD CELL PHONE ON. (MX) OPS CHECK GOOD. IT WAS DETERMINED CELL PHONE IN BACK SEAT IN FLIGHT WITNESSED BY OFF DUTY WP PILOT.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fire protection · smoke detector · false activationOct 13, 2007

    (PIREP) SMOKE MASTER WARNING CAME ON DURING TAXI. F/A VERIFIED THERE WAS NO SMOKE. (MX) PERFORMED MASTER WARNING CAUTION LIGHT TEST IAW DHC-8 MM 26-12-05. ADDITIONAL NOTES: TWO DIFFERENT P/N SMOKE DETECTORS ON BOARD THIS AIRCRAFT. NR 1 - P/N 30-231-3, S/N 35007 TIME SINCE REPAIR 174.8 HR. NR 2…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fire protection · smoke warning · intermittentSep 12, 2007

    INTERMITTENT SMOKE WARNING LIGHT ILLUMINATED DURING FLIGHT. (MX) INSPECTED SMOKE WARNING SYSTEM AND FOUND CELL PHONE RINGING IN BAGGAGE COMPARTMENT. PERFORMED SMOKE WARNING SYSTEM TEST IAW MM 26-12-00 PG. 201, NO DEFECTS NOTED.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Ignition · igniter · missingAug 3, 2007

    (PIREP) NR 2 ENGINE INBOARD AIR VENT BURNED OFF 5 OF 9 SLATS & PAINT AROUND THE AREA BURNED AS WELL. (MX) PERFORMED VISUAL INSPECTION OF NR 2 NACELLE, FOUND INBOARD IGNITER NOT INSTALLED ON ENGINE. RE-INSTALLED IGNITER IAW DHC-8 MM 72-01-20 SEC 5B PG 402. ALSO FOUND INBOARD NACELLE AFT DOOR…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Landing gear · selector panel · malfunctionedOct 14, 2006

    NOSE GEAR DOWN AND LOCK LIGHT DID NOT COME ON INTO LNY. FLOOR DOWN AND LOCKED INDICATOR SHOWED NOSE GEAR DOWN AND LOCKED. REMOVED AND REPLACED LANDING GEAR PANEL AND PERFORMED OPS CHECK IAW DHC-8 MM 32-30-05 PG 201-202.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Landing gear · door · openOct 2, 2006

    GEAR UNSAFE LIGHT ON AFTER GEAR UP SELECTION. CLEARED VIA CHECKLIST, FOUND ALTERNATE RELEASE DOOR NOT FULLY CLOSED. VERIFIED WITH CAPTAIN THAT LANDING GEAR ALTERNATE RELEASE DOOR NOT FULLY CLOSED DURING FLIGHT. NO DEFECTS NOTED.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Hydraulic power · packing · leakingMar 11, 2006

    (PIREP) NR 1 HYDRAULIC LEAK. MX CONFIRMED HYDRAULIC LEAK NR 1 NACELLE, RIGHT SIDE BULKHEAD BEHIND FLAP POST COVER. REPLACED BAD PACKING STA Y163.40 LT. RAN ENGINE FOR LEAK CHECK GOOD. SERVICED HYDRAULIC RESERVOIR PER DHC-8 MM 29-00-00 PG 201-202.

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

Showing the 10 most recent of 41 reports.

Sources

  • FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 19, 2026
  • NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
  • FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 19, 2026
  • FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

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