N813CKDouglas DC-8-61
This N-number isn't registered right now. Below is its last known registration, canceled Jul 10, 2001.
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
- Memphis, TN
- Canceled
- Jul 10, 2001
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-8-61
- Serial number
- 45893
- 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
- AB14BD
Engine
- Type
- Turbo-jet
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- until 2001Individual ownerMemphis, TN
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.
- Engine fuel and control · fuel pump · failedJan 1, 1999
DURING CRUISE FL 340, NR 1 ENG BEGAN TO LOSE PWR AS EVIDENCED BY DECREASING EPR AND RPM IND. APPLIED ENG AND SCOOP ANTI-ICE, EPR AND RPM'S CONTINUED TO DROP. AFTER 5 MIN RPM DROPPED TO APPROX 85 PERCENT N2. AS RPM DECREASED NR 1 FUEL PRESS IND DROPPED BELOW 0 PSI TO APPROX -5 PSI. OPENED ALL…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Landing gear · uplatch mech · lack of lubeAug 21, 1997
NOSE GEAR EXTENDED ON UPLATCH CHECK, TWICE, THEN STAYED UP. CHECKED UPLATCH MECHANISM FOR CONDITION/SECURITY FOUND OK. GREASED UPLOCK UNIT AND ROLLER JACKED AIRCRAFT NOSE AND ACCOMPLISHED NOSE GEAR FUNCTIONAL CHECK, UPLOCK CHECK SATISFACTORY.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fire protection · insulator · out of positionOct 18, 1996
IN FLIGHT, NR 3 FIRE WARNING WENT OFF. COMPLETED ALL APPROPRIATE CHECKLISTS, VISUALLY INSPECTED NR 3 ENGINE AND NO DEFECTS NOTED. FOUND INSULATOR NR 3 ENGINE FIRE LOOP OUT OF PLACE. REINSTALLED INSULATOR PER DACO DC-8 MM 26-10-1. NR 3 ENGINE FIRE WARNING TESTS GOOD PER DACO DC-8 MM 26-10-0.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 7 reportsShow fewer reports
- Landing gear · strut · brokenNov 1, 1995
MIA - FLT 61556 - REFERENCE MRR NR 95-002, DATED 1-15-95. IN THE PROCESS OF TOWING AIRCRAFT, THE NOSE GEAR LOWER STRUT BROKE OFF APPROXIMATELY 12 INCHES FROM THE BOTTOM OF THE STRUT. UPON DISASSEMBLY AND INVESTIGATION, FOUND CRACK INITIATION WAS ATTRIBUTED TO AN ABUSIVE GRINDING OPERATION OF THE…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · panel · corrodedJun 20, 1995
KYIP - DURING 'C-3' CHECK INSPECTION, FOUND GALLEY FLOOR CORRODED. REMOVED AND CUT OUT CORRODED PORTION OF GALLEY FLOOR AND REPAIRED PER EA NR 95-168.C. (X)
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · angle · corrosionJun 20, 1995
KYIP - DURING 'C-3' CHECK INSPECTION, FOUND CORROSION AT STA 280.0 BETWEEN LONGERONS 32L AND 33L. REMOVED AND REPLACED CORRODED ANGLE IAW EA NR 95-168. (X)
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · floor beam · crackedJun 20, 1995
KYIP - DURING 'C-3' CHECK INSPECTION, FOUND FLOOR BEAM AT STA 798.00 BETWEEN SEAT TRACKS 3 AND 4 WITH END CLIPS CRACKED. REMOVED AND REPLACED END CLIP STA 798.00 BETWEEN SEAT TRACKS 3 AND 4 PER SKA95110-3. INSTALLED PANELS AS REQUIRED. REPAIRED END CLIP STA 798.00 IAW EA NR 95-167.C. (X)
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