# N816CK: Mcdonnell Douglas DC-8-61, registration cancelled 2001-07-10 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: July 10, 2001 - Status when cancelled: Sale reported - Airframe: [Mcdonnell Douglas DC-8-61](https://openairdocs.org/model/mcdonnell-douglas-dc-8-61) (registry code 302195B) - Data sheets: [TCDS 4A25](https://openairdocs.org/tcds/4A25) (OpenAirDocs) - Serial number: 45892 - Type of aircraft: Fixed wing multi engine - Last registry action: May 29, 2001 - Mode S code: AB1FE2 - Location: [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis) - Owner type: Individual - Owner's area on the map: 35.0795° N, 89.8454° W: Placed by OpenAirDocs at the center of ZIP code 38119, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N816CK - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=816CK - Page: https://openairdocs.org/deregistered/N816CK-2001-07-10 From the FAA registry file of October 29, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe. ADs and bulletins for the Mcdonnell Douglas DC-8-61: https://openairdocs.org/model/mcdonnell-douglas-dc-8-61.md ## Service difficulty reports (35) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR CKSA98506](https://openairdocs.org/sdr/CKSA98506), Aug 11, 1998: DUCT. MISALIGNED. AT FL330 JUST AFTER LEVEL OFF AND POWER REDUCTION TO CRUISE POWER 3 OF 4 T/C'S: NR 1,2, AND 4 STARTED STALLING AND OVERHEATING, PNEUMATIC SWITCHES WERE ON HIGH, - [SDR CKSA97525](https://openairdocs.org/sdr/CKSA97525), Aug 4, 1997: SEAT TRACK. CORRODED. DURING ROUTINE C-4 CHECK INSPECTION, FOUND LEVEL 2 CORROSION, FUS INTERIOR FLOOR SECOND TRACK RT SIDE, LEVEL 2 CORROSION FROM STA 1460 TO STA 1380. REPLACED FLO - [SDR CKSA97524](https://openairdocs.org/sdr/CKSA97524), Aug 4, 1997: SEAT TRACK. BROKEN. DURING ROUTINE C-4 CHECK INSPECTION, FOUND FUSELAGE INTERIOR FLOOR CENTER TRACK BROKEN FROM STA 1040 TO STA 1060. REPAIRED FLOOR CENTER TRACK AS PER SRM 53-2-3. - [SDR CKSA97523](https://openairdocs.org/sdr/CKSA97523), Aug 4, 1997: SEAT TRACK. CRACKED. DURING ROUTINE C-4 CHECK INSPECTION, FOUND FUSELAGE INTERIOR FLOOR SECOND TRACK RT SIDE CRACKED 2.5 INCHES FROM STA 1040 TO STA 1060. REPLACED FLOOR SECOND TRAC - [SDR CKSA97522](https://openairdocs.org/sdr/CKSA97522), Aug 4, 1997: SEAT TRACK. CRACKED. DURING ROUTINE C-4 CHECK INSPECTION, FOUND FUSELAGE INTERIOR CENTER TRACK CRACKED 2.5 FROM STA 460 TO STA 500. REPAIRED CENTER TRACK AS PER SRM 53-2-3. NON-ROUT - [SDR CKSA97521](https://openairdocs.org/sdr/CKSA97521), Aug 4, 1997: SKIN. CRACKED. DURING ROUTINE C-4 CHECK INSPECTION, FOUND LT WING NR 2 PYLON AFT SIDE STA YOP320 TO YOP420 CRACKED 8. REPAIRED AFFECTED AREA AS PER SRM 54-2-1. NON-ROUTINE TAS - [SDR CKSA97520](https://openairdocs.org/sdr/CKSA97520), Aug 4, 1997: SEAT TRACK. BROKEN. DURING ROUTINE C-4 CHECK INSPECTION, FOUND FUS INTERIOR FLOOR FIRST TRACK LT SIDE BROKEN 4 INCHES FROM STA 1680 TO STA 1720. REPAIRED FLOOR FIRST TRACK AS PER S - [SDR CKSA97519](https://openairdocs.org/sdr/CKSA97519), Aug 4, 1997: SEAT TRACK. CRACKED. DURING ROUTINE C-4 CHECK INSPECTION, FOUND FUS INTERIOR FLOOR FIRST TRACK RT SIDE CRACKED 2 INCHES FROM STA 1300 TO STA 1320. REPAIRED FLOOR FIRST TRACK AS PER - [SDR CKSA97518](https://openairdocs.org/sdr/CKSA97518), Aug 4, 1997: SEAT TRACK. BROKEN. DURING ROUTINE C-4 CHECK INSPECTION, FOUND FUSELAGE INTERIOR FLOOR FIRST RT TRACK BROKEN FROM STA 1040 TO STA 1060. REPAIRED FLOOR FIRST RT TRACK AS PER SRM 53- - [SDR CKSA97517](https://openairdocs.org/sdr/CKSA97517), Aug 4, 1997: SEAT TRACK. CRACKED. DURING ROUTINE C-4 CHECK INSPECTION, FOUND FUS INT FLOOR CENTER TRACK CRACKED 2 INCHES FROM STA 1340 TO STA 1300. REPAIRED TRACK AT AFFECTED AREA AS PER SRM 53- - [SDR CKSA97516](https://openairdocs.org/sdr/CKSA97516), Aug 4, 1997: SKIN. CORRODED. DURING ROUTINE C-4 CHECK INSPECTION, FOUND LEVEL 2 CORROSION, FUSELAGE SKIN LWR PART SHOWS LEVEL 1 CORROSION STA 1690 LONG 35 RT SIDE. AFTER SECOND INSPECTION W - [SDR CKSA97515](https://openairdocs.org/sdr/CKSA97515), Aug 4, 1997: FRAME. CRACKED. DURING ROUTINE C-4 CHECK INSPECTION, FOUND FWD CARGO COMPARTMENT FRAME DOUBLER CRACKED 1 INCH AT STA 220 STR 27, 28 RT SIDE. REPAIRED FRAME DOUBLER ON FWD CARGO - [SDR CKSA97514](https://openairdocs.org/sdr/CKSA97514), Aug 4, 1997: FRAME. CRACKED. DURING ROUTINE C-4 CHECK INSPECTION, FOUND FWD CARGO COMPARTMENT FRAME DOUBLER CRACKED 1 INCH AT STA 180 AND STR 32 RT. REPAIRED DOUBLER ON FWD CARGO COMPARTMEN - [SDR CKSA97513](https://openairdocs.org/sdr/CKSA97513), Aug 4, 1997: DOUBLER. CRACKED. DURING ROUTINE C-4 CHECK INSPECTION, FOUND FWD CARGO COMPARTMENT FRAME LWR DOUBLER CRACKED .5. REPAIRED DOUBLER ON FWD CARGO COMPARTMENT FRAME AS PER SRM 53-2-0 - [SDR CKSA97512](https://openairdocs.org/sdr/CKSA97512), Aug 4, 1997: DOUBLER. CRACKED. DURING ROUTINE C-4 CHECK INSPECTION, FOUND FWD CARGO COMPARTMENT FRAME DOUBLER CRACKED 1 AT STA 220, STR 32 AND 33 LT SIDE. REPAIRED DOUBLER ON FWD CARGO COMPAR - [SDR CKSA97511](https://openairdocs.org/sdr/CKSA97511), Aug 4, 1997: DOUBLER. CRACKED. DURING ROUTINE C-4 CHECK INSPECTION, FOUND FWD CARGO COMPARTMENT FRAME DOUBLER CRACKED .75 AT STA 180 AND STR 36. REPAIRED DOUBLER ON FWD CARGO COMPARTMENT FRAM - [SDR CKSA97510](https://openairdocs.org/sdr/CKSA97510), Aug 4, 1997: DOUBLER. CRACKED. DURING ROUTINE C-4 CHECK INSPECTION, FOUND FWD CARGO COMPARTMENT FRAME DOUBLER CRACKED 1 AT STA 200 AND STR 35 RT. REPAIRED ANGLE DOUBLER ON FWD CARGO COMPARTME - [SDR CKSA97509](https://openairdocs.org/sdr/CKSA97509), Aug 4, 1997: ANGLE. CRACKED. DURING ROUTINE C-4 CHECK INSPECTION, FOUND LWR FWD CARGO COMPARTMENT FRAME REINFORCEMENT ANGLE STA 200 STRINGER 31 LT SHOWS CRACK. REPAIRED AFFECTED AREA AS PER - [SDR CKSA97508](https://openairdocs.org/sdr/CKSA97508), Aug 4, 1997: DOUBLER. CRACKED. DURING ROUTINE C-4 CHECK INSPECTION, FOUND FWD CARGO COMPARTMENT FRAME DOUBLER CRACKED 1 STR 31 RT. REPAIRED AFFECTED AREA AS PER SRM 53-2-0. NON-ROUTINE TASK C - [SDR CKSA97507](https://openairdocs.org/sdr/CKSA97507), Aug 4, 1997: DOUBLER. DEFORMED. DURING ROUTINE C-4 CHECK INSPECTION, FOUND FWD CARGO COMPARTMENT FRAME DOUBLER DEFORMED AT STA 280 STR 34 RT TO STR 34 LT. REPAIRED AFFECTED AREA AS PER SRM 53- - [SDR CKSA97506](https://openairdocs.org/sdr/CKSA97506), Aug 4, 1997: DOUBLER. CRACKED. DURING ROUTINE C-4 CHECK INSPECTION, FOUND FWD CARGO COMPARTMENT FRAME DOUBLER CRACKED .75 AT STA 360 STR 31 RT. REPAIRED AFFECTED AREA AS PER SRM 53-2-0. NON-R - [SDR CKSA97505](https://openairdocs.org/sdr/CKSA97505), Aug 4, 1997: DOUBLER. CRACKED. DURING ROUTINE C-4 CHECK INSPECTION, FOUND FWD CARGO COMPARTMENT FRAME DOUBLER CRACKED .5 TO .75 AT STA 380 STR 35 LT AND STR 36. REPAIRED AFFECTED AREA AS PER - [SDR CKSA97504](https://openairdocs.org/sdr/CKSA97504), Aug 4, 1997: DOUBLER. DEFORMED. DURING ROUTINE C-4 CHECK INSPECTION, FOUND FWD CARGO COMPARTMENT FRAME DOUBLER DEFORMED FROM STA 500 TO STA 520. REPAIRED AFFECTED AREA AS PER SRM 53-2-0. NON-R - [SDR CKSA97503](https://openairdocs.org/sdr/CKSA97503), Aug 4, 1997: DOUBLER. CRACKED. DURING ROUTINE C-4 CHECK INSPECTION, FOUND FWD CARGO COMPARTMENT FRAME DOUBLER CRACKED 1 AT STA 340 STR 35 RT. REPAIRED AFFECTED AREA AS PER SRM 53-2-0. NON-ROU - [SDR CKSA97502](https://openairdocs.org/sdr/CKSA97502), Aug 4, 1997: DOUBLER. CRACKED. DURING ROUTINE C-4 CHECK INSPECTION, FOUND FWD CARGO COMPARTMENT FRAME DOUBLER CRACKED 1 AT STA 350 STR 36. REPAIRED FWD CARGO COMPARTMENT FRAME AS PER SRM 53-2 - [SDR CKSA97501](https://openairdocs.org/sdr/CKSA97501), Aug 4, 1997: DOOR. CRACKED. DURING ROUTINE C-4 CHECK INSPECTION, FOUND FWD CARGO COMPARTMENT DOOR INTERIOR CRACKED .75 STA 288 S30R. REPAIRED AFFECTED AREA AS PER SRM 52-2-0. NON-ROUTINE T - [SDR CKSA97500](https://openairdocs.org/sdr/CKSA97500), Aug 4, 1997: DOUBLER. CRACKED. DURING ROUTINE C-4 CHECK INSPECTION, FOUND FWD CARGO COMPARTMENT FRAME DOUBLER CRACKED 1 AT STA 160 AND STR 28 AND 29 LT SIDE. REPLACED FWD CARGO COMPARTMENT FR - [SDR CKSA97499](https://openairdocs.org/sdr/CKSA97499), Aug 4, 1997: DOUBLER. CRACKED. DURING ROUTINE C-4 CHECK INSPECTION, FOUND FWD CARGO COMPARTMENT FRAME DOUBLER CRACKED 1 AT STA 180 AND STR 33 RT. REPLACED FWD CARGO COMPARTMENT FRAME DOUBLER - [SDR CKSA97498](https://openairdocs.org/sdr/CKSA97498), Aug 4, 1997: DOUBLER. CRACKED. DURING ROUTINE C-4 CHECK INSPECTION, FOUND FWD CARGO COMPARTMENT FRAME DOUBLER CRACKED .5 AT STA 180 AND STR 35 LT. REPLACED FWD CARGO COMPARTMENT FRAME DOUBLER - [SDR CKSA97497](https://openairdocs.org/sdr/CKSA97497), Aug 4, 1997: SEAT TRACK. BROKEN. DURING ROUTINE C-4 CHECK INSPECTION, FOUND FUSELAGE INTERIOR FLOOR TRACK RT SIDE BROKEN FROM STA 440 TO STA 400. REPAIRED FLOOR TRACK AS PER SRM 53-2-3. NON-ROU - [SDR CKSA97496](https://openairdocs.org/sdr/CKSA97496), Aug 4, 1997: DOOR FRAME. BROKEN. DURING ROUTINE C-4 CHECK INSPECTION, FOUND LOWER FORWARD CARGO COMPARTMENT DOOR FRAME AT STA 282 RT SHOWS BREAKAGES (3 BY .25 BY .5 BY .25). REPAIRED AFFECTED A - [SDR CKSA97495](https://openairdocs.org/sdr/CKSA97495), Aug 4, 1997: SEAT TRACK. ELONGATED. REFERENCE CARRY OVER NR 56, F/E FWD SEAT TRACK HOLES ARE ELONGATED AND WORN. REMOVED AND REPLACED FE'S FWD SEAT TRACK AS REQUIRED AS PER DC8 SRM 53-2-3, FE SEAT - [SDR CKSA96053](https://openairdocs.org/sdr/CKSA96053), May 27, 1996: ACTUATOR. FAILED. KNGU - UPON GEAR RETRACTION, HYDRAULIC PRESSURE DROPS TO 800 PSI, 'GEAR NOT LATCHED' LIGHT AND 'GEAR DOOR' LIGHT ILLUMINATED. (SECONDARY GEAR WARNING LIGHTS SHO - [SDR CKSA95037](https://openairdocs.org/sdr/CKSA95037), Jun 14, 1995: RETRACT MECH. MALFUNCTIONED. KBUF - FLT 64648 - AFTER TAKEOFF, LOUD NOISE WAS HEARD FROM NOSE GEAR. RECYCLED GEAR, NO CHANGE. RETURNED TO BUF. MAINTENANCE INSPECTED NOSE GEAR WHEELWELL DOOR - [SDR CKSA95004](https://openairdocs.org/sdr/CKSA95004), Jan 25, 1995: SKIN. CORROSION. YIP - DURING B-CHECK, INSPECTION FOUND EVIDENCE OF SKIN CORROSION AT STA 140 BETWEEN STRINGERS 26 AND 27R. REMOVED CORROSION AND INSTALLED REPAIR PER DC-8 SRM 5 ## FAA accident and incident reports (1) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Incident 19990812032359I](https://openairdocs.org/incident/19990812032359I), Aug 12, 1999: Doug DC861 (N816CK), Fort Wayne, IN. (-23) On landing roll at Fort Wayne international airport. It appears that fire was coming out of the number 4 engine. Emergency equipment called out. The… --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.