# N795FT: 1969 Douglas DC-8-73F, registration cancelled 2005-10-05

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: October 5, 2005
- Exported to: Brazil
- Status when cancelled: Valid registration
- Airframe: [Douglas DC-8-73F](https://openairdocs.org/model/douglas-dc-8-73f) (registry code 302199F)
- Engine: [CFM International CFM56 series](https://openairdocs.org/engine/cfm-international-cfm56-series) (registry code 13802)
- Data sheets: [TCDS 4A25](https://openairdocs.org/tcds/4A25) (OpenAirDocs)
- Serial number: 46103
- Year built: 1969
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 12, 1984
- Certificate issued: December 11, 2003
- Last registry action: December 15, 2004
- Mode S code: AACB27
- Owner when cancelled: [Aeroturbine Inc](https://openairdocs.org/faa-owner/AEROTURBINE%20INC)
- Location: [Miami, FL](https://openairdocs.org/faa-place/FL/Miami)
- Owner type: Corporation
- Owner's area on the map: 25.8050° N, 80.3151° W: Placed by OpenAirDocs at the center of ZIP code 33122, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N795FT
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=795FT
- Page: https://openairdocs.org/deregistered/N795FT-2005-10-05

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 Douglas DC-8-73F: https://openairdocs.org/model/douglas-dc-8-73f.md

## Service difficulty reports (205, newest 50)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR RRXA010050](https://openairdocs.org/sdr/RRXA010050), Jun 10, 2001: TRANSMITTER. FAILED. REJECTED T/O AT DAY, GREATER 60 KTS, NR 2 OIL PRESSURE GAUGE SHOWED AT LEAST 15 PSI HIGHER THAN OTHERS, AND APPEARED TO CONTINUE TO CLIMB. REMOVED AND REPLACED 
- [SDR RRXA010012](https://openairdocs.org/sdr/RRXA010012), Feb 16, 2001: CONTROL CABLE. DEFECTIVE. ON TAXI OUT LOST NOSE STEERING AIRCRAFT WAS TOWED BACK TO EMERGENCY RAMP BY AIRPORT DELTA SUPER TUG. GEAR PIN INSTALLED. REMOVED AND REPLACED RIGHT SIDE NOSE ST
- [SDR RRXA003602](https://openairdocs.org/sdr/RRXA003602), Feb 1, 2001: PANEL. DELAMINATED. DURING A MAINTENANCE VISIT FOUND DELAMINATION DAMAGE TO THE L/H WING BOTTOM T/E PANEL AT STA XRS 419 TO XRS 435, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////
- [SDR RRXA010006](https://openairdocs.org/sdr/RRXA010006), Feb 1, 2001: ENGINE. FOD. ON WALK-AROUND FOUND FOD ON NR 3 ENGINE.
- [SDR RRXA010034](https://openairdocs.org/sdr/RRXA010034), Jan 31, 2001: MECHANISM. OUT OF ADJ. AFTER T/O ACFT DIDN'T GROUND SHIFT; COULD NOT RETRACT MLG. ADJUSTED NOSE GEAR GROUND SHIFT MECHANISM IAW DC-8 M/M CH 32-23-01, OP CHKS GOOD.
- [SDR RRXA003799](https://openairdocs.org/sdr/RRXA003799), Jan 17, 2001: FITTING. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LT.WW BATHTUB FITTING AT STA. 960 AND L24L FWD SIDE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECT
- [SDR RRXA003592](https://openairdocs.org/sdr/RRXA003592), Jan 8, 2001: FITTING. CRACKED. DURING A MAINTENANCE VISIT FOUND A CRACK TO THE RT WING #1 GROUND SPOILER O/B MOUNT FITTING, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///
- [SDR RRXA003591](https://openairdocs.org/sdr/RRXA003591), Jan 8, 2001: PANEL. DELAMINATED. DURING A MAINTENANCE VISIT FOUND DELAMINATION DAMAGE TO THE R/H WING BOTTOM T/E PANEL AT STA XRS 340 TO XRS 419, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////
- [SDR RRXA003595](https://openairdocs.org/sdr/RRXA003595), Jan 6, 2001: TRACK. CRACKED. DURING A MAINTENANCE VISIT FOUND A CRACK TO THE "D-PIT" DOOR AFT TRACK (3" CRACK), DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED
- [SDR RRXA003594](https://openairdocs.org/sdr/RRXA003594), Jan 6, 2001: LONGERON. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE UNDER RT LONGERON 24 SUPPORT FITTING AT STA 920 RT W/W Y-920 X-66, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. R
- [SDR RRXA003593](https://openairdocs.org/sdr/RRXA003593), Jan 5, 2001: FITTING. CRACKED. DURING A MAINTENANCE VISIT FOUND A CRACK TO THE #1 GND SPOILER I/B MOUNT FITTING, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED 
- [SDR RRXA003596](https://openairdocs.org/sdr/RRXA003596), Jan 3, 2001: FASTENER. MISSING. DURING A MAINTENANCE VISIT FOUND MISSING FASTENER ON THE RT UPPER WING THRU ACCESS HOLE 505C & THROUGH MID SPAR ACCESS HOLE 560C INSIDE TANK I/B BETWEEN STA 252
- [SDR RRXA003603](https://openairdocs.org/sdr/RRXA003603), Jan 2, 2001: LONGERON. CRACKED. DURING A MAINTENANCE VISIT FOUND A CRACK TO THE TOP ON LONGERON JUST FWD OF 'C' PIT DOOR AT STA 1140 AND L33R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CO
- [SDR RRXA003601](https://openairdocs.org/sdr/RRXA003601), Jan 2, 2001: PANEL. DELAMINATED. DURING A MAINTENANCE VISIT FOUND DELAMINATION DAMAGE TO THE R/H WING BOTTOM T/E PANEL AT STA XRS 5 TO XRS 98, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////COR
- [SDR RRXA003599](https://openairdocs.org/sdr/RRXA003599), Jan 2, 2001: DOOR. DELAMINATED. DURING A MAINTENANC EVISIT FOUND DELAMINATION IN 2 PLACES ON THE LEFT MLG TOP DOOR TO WING, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION////
- [SDR RRXA003598](https://openairdocs.org/sdr/RRXA003598), Jan 2, 2001: ANGLE. CRACKED. DURING A MAINTENANCE VISIT FOUND THE BULKHEAD ATTACH ANGLE BROKEN AND CRACKED ON THE AFT LWR CARGO COMPT AT STA 1320 X35 Z-8, DAMAGE EXCEEDED LIMITATIONS IAW DC
- [SDR RRXA003597](https://openairdocs.org/sdr/RRXA003597), Jan 2, 2001: SKIN. CRACKED. DURING A MAINTENANCE VISIT FOUND A CRACK TO THE AFT LWR CORNER OF THE "D" PIT DOOR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVE
- [SDR RRXA003608](https://openairdocs.org/sdr/RRXA003608), Dec 29, 2000: WEB. CHAFED. DURING A MAINTENANCE VISIT FOUND A CHAFFED WEB IN COCKPIT BETWEEN FRAMES -52 & -67, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW D
- [SDR RRXA003607](https://openairdocs.org/sdr/RRXA003607), Dec 29, 2000: PANEL. DELAMINATED. DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE COCKPIT FLOOR PANEL CAPT'S SIDE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// 
- [SDR RRXA003605](https://openairdocs.org/sdr/RRXA003605), Dec 29, 2000: PRESSURE PANEL. CORRODED. DURING A MAINTENANCE VISIT FOUND 21 SHEAR RIVETS ON THE FINGER DOUBLER AT THE COCKPIT AREA FLOOR BELOW AFT END OF CAPT'S CHAIR, DAMAGE EXCEEDED LIMITATIONS IAW 
- [SDR RRXA003604](https://openairdocs.org/sdr/RRXA003604), Dec 29, 2000: FLOOR PANEL. BROKEN. DURING A MAINTENANCE VISIT FOUND ELONGATED SCREW HOLES BROKEN OUT ON THE FLOOR PANEL 681, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// 
- [SDR RRXA003606](https://openairdocs.org/sdr/RRXA003606), Dec 28, 2000: SKIN. PUNCTURED. DURING A MAINTENANCE VISIT FOUND A PUNCTURE HOLE IN THE OUTER SKIN ON THE FUSELAGE AT STA 220 TO 240 AND L25L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED
- [SDR RRXA003800](https://openairdocs.org/sdr/RRXA003800), Dec 22, 2000: SKIN. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION/SHEARED RIVITS DAMAGE TO DOUBLER AT STA. 1697 AND L29L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACT
- [SDR RRXA003612](https://openairdocs.org/sdr/RRXA003612), Dec 20, 2000: SKIN. CRACKED. DURING A MAINTENANCE VISIT FOUND A CRACK TO THE MOST O/B HOLE ON THE R/H WING LWR SKIN AT STR 64, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTI
- [SDR RRXA003611](https://openairdocs.org/sdr/RRXA003611), Dec 20, 2000: FITTING. CRACKED. DURING A MAINTENANCE VISIT FOUND A CRACK TO THE BATHRUB FITTING BETWEEN STA 1690 & 1700 AND L34L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTI
- [SDR RRXA003610](https://openairdocs.org/sdr/RRXA003610), Dec 20, 2000: FITTING. CRACKED. DURING A MAINTENANCE VISIT FOUND A CRACK TO THE FLOOR STRUT FITTING AFT LWR CARGO COMPT AT STA 1160 AND L27R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////COR
- [SDR RRXA003609](https://openairdocs.org/sdr/RRXA003609), Dec 20, 2000: FLANGE. CRACKED. DURING A MAINTENANCE VISIT FOUND A CRACK TO THE FLOOR BEAM R/H O/B LWR LEG ON FWD SIDE AT STA 920, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACT
- [SDR RRXA003502](https://openairdocs.org/sdr/RRXA003502), Dec 19, 2000: INTERCOSTAL. CRACKED. DURING A MAINTENANCE VISIT FOUND A CRACK TO THE INTERCOSTAL W/W AT STA 940 AND WING STA 69.5 RT W/W, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA003506](https://openairdocs.org/sdr/RRXA003506), Dec 18, 2000: SKIN. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION BLISTERS ON THE SKIN AT STA 1714 AND L29L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA003505](https://openairdocs.org/sdr/RRXA003505), Dec 18, 2000: STRUCTURE. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE REPAIR PATCH RIVETS ON COCKPIT SUB-FLOOR FWD OF L/H AVIONICS RACK, DAMAGE EXCEEDED LIMITATIONS IAW DC-8
- [SDR RRXA003504](https://openairdocs.org/sdr/RRXA003504), Dec 18, 2000: FITTING. CRACKED. DURING A MAINTENANCE VISIT FOUND A CRACK TO THE ANGLE SUPPORT FITTING AT STA 960 R/H, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA003503](https://openairdocs.org/sdr/RRXA003503), Dec 18, 2000: WEB. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE ON WEB ABOVE RT LONGERON 24Y AT STA 879 X=-59 Z=10 INCH, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA003507](https://openairdocs.org/sdr/RRXA003507), Dec 15, 2000: SKIN. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE "D-PIT" DOOR BOTTOM AFT CORNER, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA003513](https://openairdocs.org/sdr/RRXA003513), Dec 14, 2000: SILL. CRACKED. DURING A MAINTENANCE VISIT FOUND A CRACK TO THE REPAIR AFT SIDE OF "C-PIT" DOOR SILL, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////OPEN/////
- [SDR RRXA003512](https://openairdocs.org/sdr/RRXA003512), Dec 14, 2000: FRAME. BROKEN. DURING A MAINTENANCE VISIT FOUND THE AFT SIDE FWD FRAME BROKEN OFF "C-PIT" DOOR SILL, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA003511](https://openairdocs.org/sdr/RRXA003511), Dec 14, 2000: SILL. CRACKED. DURING A MAINTENANCE VISIT FOUND A CRACK TO THE "C-PIT" DOOR SILL REPAIR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA003510](https://openairdocs.org/sdr/RRXA003510), Dec 14, 2000: WEB. CRACKED. DURING A MAINTENANCE VISIT FOUND A CRACK IN WEB AT RT. CUSP AT STA 1300 Y=1300 X-66 Z-0, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA003509](https://openairdocs.org/sdr/RRXA003509), Dec 14, 2000: FLOOR PANEL. DAMAGED. DURING A MAINTENANCE VISIT FOUND TORN OUT SCREW HOLES ON THE COCKPIT FLOOR PANEL BETWEEN PILOT & CO-PILOTS SEAT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA003508](https://openairdocs.org/sdr/RRXA003508), Dec 14, 2000: WEB. TORN. DURING A MAINTENANCE VISIT FOUND A TORN STRUCTURE ON 'A' PIT DOOR INTERNAL WEB, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA003518](https://openairdocs.org/sdr/RRXA003518), Dec 13, 2000: TRACK. CRACKED. DURING A MAINTENANCE VISIT FOUND A CRACK TO THE "C-PIT" DOOR DOOR COVER AT TRACK, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA003517](https://openairdocs.org/sdr/RRXA003517), Dec 13, 2000: FLOOR PANEL. CRACKED. DURING A MAINTENANCE VISIT FOUND A CRACK AND TORN OUT SCREW HOLES ON THE COCKPIT FLOOR PANEL PILOTS SEAT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA003516](https://openairdocs.org/sdr/RRXA003516), Dec 13, 2000: FLOOR PANEL. CRACKED. DURING A MAINTENANCE VISIT FOUND A CRACK TO THE FLOOR PANEL 678, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA003515](https://openairdocs.org/sdr/RRXA003515), Dec 13, 2000: SKIN. CRACKED. DURING A MAINTENANCE VISIT FOUND 2 CRACKS ALONG BOTTOM OF MAIN CARGO DOOR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA003514](https://openairdocs.org/sdr/RRXA003514), Dec 13, 2000: FITTING. CRACKED. DURING A MAINTENANCE VISIT FOUND A CRACK TO THE RT LONGERON 24 SUPPORT FITTING FWD EDGE AT STA 902, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////OPEN/////
- [SDR RRXA003806](https://openairdocs.org/sdr/RRXA003806), Dec 12, 2000: DOOR FRAME. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO A-PIT DOOR FRAME AT STA. 300, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC
- [SDR RRXA003522](https://openairdocs.org/sdr/RRXA003522), Dec 12, 2000: THRESHOLD. CRACKED. DURING A MAINTENANCE VISIT FOUND A CRACK AND DENTED EDGES TO THE "D-PIT" THRESHOLD/KICK PLATE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////OPEN/////
- [SDR RRXA003521](https://openairdocs.org/sdr/RRXA003521), Dec 12, 2000: DOUBLER. CRACKED. DURING A MAINTENANCE VISIT FOUND 'C-PIT' DOOR HAS REPAIR CRACKING OFF, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA003520](https://openairdocs.org/sdr/RRXA003520), Dec 12, 2000: BULKHEAD. DAMAGED. DURING A MAINTENANCE VISIT FOUND GILLINER ATTACH ANGLE & BULKHEAD ATTACH HOLES BROKEN OUT ON THE AFT LWR CARGO BILGE AT STA 1320 AND L31L TO L31R, DAMAGE EXCEED
- [SDR RRXA003519](https://openairdocs.org/sdr/RRXA003519), Dec 12, 2000: FRAME. CRACKED. DURING A MAINTENANCE VISIT FOUND A CRACK TO THE "C-PIT" DOOR FWD FRAME (DOOR COVER), DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA003529](https://openairdocs.org/sdr/RRXA003529), Dec 11, 2000: BRACKET. WORN. DURING A MAINTENANCE VISIT FOUND A WORN "T-BOLT" RETAINING BRACKET (TOP SIDE) NR 5 BOTTOM, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.

All 205: https://openairdocs.org/deregistered/N795FT-2005-10-05/reports.md

## FAA accident and incident reports (2)

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 19900103003219I](https://openairdocs.org/incident/19900103003219I), Jan 3, 1990: Doug DC873F (N795FT), Dayton, OH, Minor damage. NR1 main gear wheel and tire assembly departed on touch and go landing. Retaining nut on axle failed.
- [Incident 19810507031129I](https://openairdocs.org/incident/19810507031129I), May 7, 1981: Doug DC863F (N795FT), Chicago, IL. Aborted takeoff due to unsafe door light. Maintenance found a dirty micro switch.

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