N888PV1979 Dehavilland DHC-6-300
This N-number isn't registered right now. Below is its last known registration, canceled Oct 17, 2022.
Safety record in brief:No NTSB accidents or incidents since 1982No ADs since 1998 matched28 service difficulty reports
- Registration
- Deregistered
Registration
FAA Aircraft Registry · Oct 17, 2026- Last registered owner
- Tvpx Aircraft Solutions INC Trustee
- Owner type
- Corporation
- City, state
- North Salt Lake, UT
- Certificate issued
- Jun 7, 2022
- Canceled
- Oct 17, 2022
- Airworthiness
- Standard · Normal
- Airworthiness date
- Aug 17, 2021
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-6-300
- Year
- 1979
- Serial number
- 620
- Aircraft type
- Fixed wing multi engine
- Category
- Land
- Certification
- Type Certificated
- Seats
- 22
- Engines
- 2
- Max takeoff weight
- Up to 12,499 lb
- Mode S code
- AC3CE6
Engine
- Make and model
- P & W Pt6a-27
- Type
- Turbo-prop
- Power
- 680 hp
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- 2022Tvpx Aircraft Solutions INC TrusteeNorth Salt Lake, 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.
Accident history for this modelADs published since 1998 that may apply (0)
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.
No ADs published since 1998 matched this airframe or engine model.
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (28)
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.
- Fire protection · terminal · unsecureSep 5, 2013
RT FIRE WARNING LIGHT AND BELL ON IN FLIGHT. SECURED RING TERMINAL ON RT OTBD FIRE DETECTION. OPS CHECKED SATISFACTORY. OPEN
From FAA Service Difficulty Reports; matched by N-number and serial number. - Wings · skin · dentedAug 20, 2013
BIRD STRIKE ON LT WING, STA 322.8. INSPECTED ADJACENT AREAS FOR SECONDARY DAMAGE. R & R L/E IAW SRM 57-30-00 AND AC 43.13-B1. PRIMED AND REPAINTED AREA.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Wings · strut · corrodedMay 26, 2009
LT WING STRUT BOTTOM FITTING CORRODED BEYOND LIMITS. REMOVED AND REPLACED, LT WING STRUT IAW DH6-300 MM CHAPTER 57-00.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reportsShow fewer reports
- Wings · skin · crackedFeb 13, 2009
AFTER REMOVING OTBD PLANK DOUBLERS AT WS 118 TO 138 OF THE RT WING, FOUND TWO CRACKS IN THE UPPER WING SKIN. ONE .7500 CRACK AT WS 123.5 AND 47 INCHES AFT OF NOSE SPAR AND ONE .5 INCH CRACK AT WS 123.5 AND 43 INCHES AFT OF THE NOSE SPAR. ACCOMPLISHED REPAIRS IAW SRM 57-30-00 FIG 6 PAGES 6 AND 7.…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Wings · doubler · corrodedFeb 9, 2009
RIGHT WING EXHAUST TRAIL DOUBLERS CORRODED. REMOVED AND REPLACED EXHAUST TRAIL DOUBLERS IAW RD6-57-618. ALL SURFACES CLEANED, TREATED, AND PRIMED IAW 1-GEN-5 CHAPTER 5.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Stabilizers · spar · corrodedFeb 9, 2009
FORWARD SEA FIN MOUNT CORRODED ON LEFT STABILIZATION. REMOVED AND REPLACED LEFT OUTBOARD STABILIZER FORWARD SPAR WITH FACTORY NEW PART.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Power plant · mount · corrodedFeb 9, 2009
RT WING, RT ENGINE MOUNT BRACKET CORRODED. REMOVED AND REPLACED RT ENGINE MOUNT ADAPTOR IAW RD6-54-006. (K)
From FAA Service Difficulty Reports; matched by N-number and serial number. - Nacelles and pylons · longeron · crackedAug 2, 2008
RT HAND NACELLE INBOARD LONGERON CRACKED 10 1/2 INCHES AFT OF THE FWD END. REMOVED AND REPLACED RT HAND INBD LONGERON IAW AC 4313-1B CH 4, RD 6-54-036 AND VERIFIED MOD 6/1655 IS INSTALLED PER AD 80-13-12 R1. (A)
From FAA Service Difficulty Reports; matched by N-number and serial number. - Wings · channel · corrodedApr 14, 2008
DURING CAMP INSPECTION, FOUND LT AILERON OB WEIGHT BALANCE CHANNEL CORRODED. REMOVED AND REPLACED WEIGHT AND BALANCE CHANNEL, AND STATIC BALANCED AILERON IAW SRM 57-50-21 PAGE 3 AND SRM RD6-57-085.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Flight controls · control rod · corrodedFeb 22, 2008
125 HR INSPECTION, EMERGENCY MEASURES EXECUTED, NO, AC GROUNDED. NO CORROSION FOUND ON RT FLAP INTERCONNECT ROD UNDER FLEXIBLE BOOT. ON IB END. REMOVED AND REPLACED CONTROL ROD.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Showing the 10 most recent of 28 reports.
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