N806CK1958 Douglas DC-8-54
This N-number isn't registered right now. Below is its last known registration, canceled Dec 29, 2011.
Safety record in brief:No NTSB accidents or incidents since 1982No ADs since 1998 matched7 service difficulty reports
- Registration
- Deregistered
Registration
FAA Aircraft Registry · Oct 20, 2026- Last registered owner
- Individual owner
- City, state
- Tecumseh, MI
- Canceled
- Dec 29, 2011
- Airworthiness
- Standard · Transport
- Airworthiness date
- Apr 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 dataAirframe
- Manufacturer
- Douglas
- Model
- DC-8-54
- Year
- 1958
- Serial number
- 45932
- Aircraft type
- Fixed wing multi engine
- Category
- Land
- Certification
- Type Certificated
- Seats
- 152
- Engines
- 4
- Max takeoff weight
- 20,000 and over lb
- Type certificate data sheet
- 4A25
- Mode S code
- AAF863
Engine
- Make and model
- P & W Jt3d Series
- Type
- Turbo-jet
- Power
- 17,700 lb thrust
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- until 1989Individual ownerdifferent airframe: Douglas Dc-8-51 S/N 45808
- until 2011Individual ownerTecumseh, MI
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 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 (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 (7)
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.
- Communications · plug · mislocatedJun 18, 1998
ON CLIMBOUT, BURNING SMELL NOTED IN COCKPIT. FO'S AUDIO PANEL CB POPPED. AFTER 5 MIN COOL DOWN, CB RESET AN IMMEDIATELY POPPED AGAIN. BURNING SMELL DISIPATED. FOUND FO'S MIC JACK SHORTING OUT DUE TO LOCATION OF MOUNTING BRACKET. RELOCATED AS REQUIRED. SYSTEM OPS CHECK NORMAL AT THIS TIME (C/B DID…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Engine oil · wire · brokenJan 14, 1998
NR 2 OIL LIGHT LOW PRESS CAME ON, T/R AND T/R DOOR LIGHT CAME ON, GEN FAIL LIGHT CAME ON, OIL PRESS THEN DROPPED AS DID OIL QUANTITY. COMPLETED NR 2 ENGINE SHUTDOWN. LATER AT TOD NR 2 ENGINE FIRE WARNING LIGHT (1/2 SYSTEM) CAME ON, FIRED BOTTLE. REPAIRED WIRING ON NR 2 ENGINE PYLON. NR 2 OIL LOW…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Flight controls · lockout cylinder · reqd serviceOct 30, 1996
WHEN 35 DEGREES FLAPS WERE SELECTED, FLAPS CAME DOWN TO 25 DEGREES, MISSED APPROACH. SELECTED FLAPS 35 DEGREES, FLAPS CAME DOWN TO 25 DEGREES UNTIL AIRCRAFT SLOWED TO 145 KIAS, THEN FLAPS LOWERED TO 35 DEGREES. BLED AND SERVICED FLAP LOCKOUT CYLINDER PER MM 27-28-0, FLAPS OPS CHECK NORMAL PER MM…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 7 reportsShow fewer reports
- Fuselage · skin · puncturedOct 23, 1996
ON WALKAROUND, FOUND HOLE IN SIDE OF AIRCRAFT AT STATION 480 JUST AFT OF A-PIT. AIRCRAFT REPAIRED PER SRM 53-4-0, 53-2-1 WITH A CLASS TWO REPAIR, REFERENCE EA 96-296. REINSPECT WITHIN 12,000 CYCLES, REPETITIVE INSPECT AT 4,000 CYCLES THEREAFTER.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Landing gear · link assy · failedOct 26, 1995
KCVG - FLT 68278 - UPON GEAR RETRACTION DURING CLIMB, NOSE GEAR DOOR DID NOT FULLY CLOSE. THIS CAUSED A VIBRATION IN NOSE GEAR DOOR WELL. FLEW ACFT AT 230KIAS/M.65. (UPLATCH FAIL CHECK SPEED). WITH GEAR DOWN, NO VIBRATION NOTED. ALL OTHER GEAR INDICATIONS NORMAL. INSPECTED NOSE GEAR DOORS, FOUND…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · angle · corrosionJul 11, 1995
KOSC - DURING C-CHECK INSPECTION, FOUND INBOARD LOWER AFT ANGLE IN WHEELWELL DOGHOUSE AREA SURFACE CORRODED. REMOVED ANGLE, REMOVED CORROSION IN CENTER WING UPPER SKIN PANEL. CORROSION REMOVAL OUT OF SRM LIMITS. REPAIRED SKIN PER ENGINEERING SKETCH SKA95118-2. SPLICED IN NEW SECTION OF REAR SPAR…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · floor beam · corrosionJul 11, 1995
KOSC - DURING C-CHECK INSPECTION, FOUND CORROSION ON FLOOR BEAM WEB AT LIGHTING HOLE AT RIGHT END STATION 440 'A' PIT. REMOVED CORROSION IAW SRM 51-1-6 FABRICATED AND INSTALLED PART IAW ENGINEERING SKA95118-1. COMPLIED WITH AIA EA95-176. (M)
From FAA Service Difficulty Reports; matched by N-number and serial number.
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