N6174C1954 Douglas DC-6A
This N-number isn't registered right now. Below is its last known registration, canceled May 18, 2022.
Safety record in brief:No NTSB accidents or incidents since 1982No ADs since 1998 matched43 service difficulty reports
- Registration
- Deregistered
Registration
FAA Aircraft Registry · Oct 17, 2026- Last registered owner
- Everts Air Cargo
- Owner type
- Corporation
- City, state
- Fairbanks, AK
- Certificate issued
- Nov 2, 2009
- Canceled
- May 18, 2022
- Airworthiness
- Standard · Transport
- Airworthiness date
- Aug 23, 2004
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
- Douglas
- Model
- DC-6A
- Year
- 1954
- Serial number
- 44075
- Aircraft type
- Fixed wing multi engine
- Category
- Land
- Certification
- Type Certificated
- Seats
- 96
- Engines
- 4
- Max takeoff weight
- 20,000 and over lb
- Mode S code
- A80BA6
Engine
- Make and model
- P & W R-2800 Series
- Type
- Reciprocating
- Power
- 2000 hp
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- 2009 – 2022Everts Air CargoFairbanks, AK
- 1957 – 1958Individual ownerLos Angeles, CA · different airframe: North American F-51d S/N 44-72718
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 (43)
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.
- Fuselage · doubler · crackedApr 7, 2014
CABIN HEATER EXHAUST SKIN REPAIR CRACKS WERE FOUND ON THE CABIN HEATER EXHAUST STAINLESS STEEL DOUBLER SHIELD. STOP DRILL CRACKS WITH A 5/32 INCHES DRILL MINIMUM, MANUFACTURE DOUBLER FROM STAINLESS STEEL IAW DWG 1420-01 & DC 6 A & B OHM FIG 14 - 7 EO 1420.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Wings · skin · damagedApr 7, 2014
FLAP SKINS REPLACEMENT BETWEEN STATION 64 & 148. REPLACE PUNCTURED & DENTED LOWER FLAP SKINS LOCATED BEHIND THE RT MLG. REMOVE DAMAGED LOWER SKINS BETWEEN STATION 64 & 148, TE CLOSE OUT PIECE BETWEEN STATION 64 & 97. MANUFACTURE NEW SKINS & CLOSE OUT PIECE FROM 2424-T3 0.040 INCHES. INSTALL NEW…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Engine fuel and control · unknown · leakingNov 27, 2013
A FUEL LEAK WAS DISCOVERED ON THE OTBD SIDE OF THE NR 3 NACELLE. THE FUEL LEAK WAS SUSPECTED TO BE FROM LOOSE RIVETS & BAD SEALANT. THE DOUBLER WAS REMOVED, THE AREA INSPECTED FOR DAMAGE & CORROSION & A NEW DOUBLER WAS MANUFACTURED & INSTALLED.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reportsShow fewer reports
- Wings · spar cap · corrodedApr 22, 2013
CORROSION ON LOWER CTR SPAR CAP AT RWS 177, REMOVED CORROSION. PERFORMED VISUAL & HFEC INSPECTIONS, NO CORROSION DETECTED. FOUND WITHIN LIMITS IAW TO 1C-118A-3-1 APPENDIX III FIGURE C-2. TREATED & PRIMED AREA FOR CORROSION PROTECTION. APPLIED SEALANT FOR AERODYNAMIC SMOOTHNESS EO 1321.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Wings · skin · crackedFeb 21, 2013
RE-ENFORCING RING, SKIN & DOUBLER CRACKED AT CTR WING SECTION. CRACKS WERE FOUND IN THE WING SKIN, STATION 60 TO 60 DOUBLER & RE ENFORCING RING FOR PANEL PN 3479163, DOOR, CTR WING FUSELAGE FRAME CUT OUT, IN THE CTR WING SECTION OF THE AIRPLANE. THE CRACK IS AT WS 17R FWD OF STRINGER 20. STATION…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · access panel · crackedFeb 20, 2013
CRACK IDENTIFIED ON NR 1 ALT FUEL TANK ACCESS DOOR DOUBLER. REPLACE DOOR DOUBLER EO 1305.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · skin · corrodedFeb 23, 2012
DURING HEAVY MX FOUND CORRODED SKIN LAP AT FUSELAGE STA 724, STRINGER 13R.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Wings · skin · corrodedFeb 23, 2012
DURING HEAVY MX FOUND CORRODED WING SKIN AND CENTER WING SPAR AT WING STATION 179L OF THE UPPER WING SURFACE.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · skin · corrodedFeb 23, 2012
DURING HEAVY MX, FOUND CORRODED FUSELAGE SKIN AND DOUBLER AT FUSELAGE BS 1030 BETWEEN STR 2L AND 2R.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Wings · skin · crackedFeb 23, 2012
DURING HEAVY MX, FOUND CRACKED LOWER WING SKIN AT CENTER SPAR AFT FLANGE WING STA 211L.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Showing the 10 most recent of 43 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