# N866AT: Douglas DC-9-32, registration cancelled 2005-08-12

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: August 12, 2005
- Status when cancelled: Sale reported
- Airframe: [Douglas DC-9-32](https://openairdocs.org/model/douglas-dc-9-32) (registry code 3022066)
- Engine: [Pratt & Whitney JT8D-1](https://openairdocs.org/engine/pratt-whitney-jt8d-1) (registry code 52044)
- Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE), [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs)
- Serial number: 47168
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: April 9, 1987
- Last registry action: August 10, 2005
- Mode S code: ABE533
- Location: [Oklahoma City, OK](https://openairdocs.org/faa-place/OK/Oklahoma%20City)
- Owner type: Individual
- Owner's area on the map: 35.4676° N, 97.5164° W: Placed by OpenAirDocs: center of Oklahoma City, OK, within about 14 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N866AT
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=866AT
- Page: https://openairdocs.org/deregistered/N866AT-2005-08-12

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-9-32: https://openairdocs.org/model/douglas-dc-9-32.md

## Service difficulty reports (52, newest 50)

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

- [SDR AT0200047](https://openairdocs.org/sdr/AT0200047), Apr 9, 2002: ACTUATOR. STICKING. FORWARD NOSE GEAR DOOR REMAINED OPEN ON DEPARTURE/BURNED DOWN FUEL, RETURNED TO BASE. FOUND NOSE GEAR DOOR MANUAL ACTUATOR STICKING, LUBED ACTUATOR AND MANUALLY
- [SDR AT0200028](https://openairdocs.org/sdr/AT0200028), Mar 3, 2002: WIRE. BROKEN. DURING EMERGENCY LIGHTING CHECK OUT FOUND TAIL CONE EMERGENCY RELEASE HANDLE LIGHT INOP. FURTHER INVESTIGATION REVEALED POSITIVE WIRE CUT IN HALF 2 FEET FROM LI
- [SDR AT0100236](https://openairdocs.org/sdr/AT0100236), Nov 29, 2001: BATTERY. DISCHARGED. FOUND EMERGENCY LIGHTS WILL NOT EXTINGUISH. CORRECTIVE ACTION: REMOVED AND REPLACED NICAD BATTERY PACK, D5-28, B5-27. IAW DC9 MM 33-50
- [SDR AT0100176](https://openairdocs.org/sdr/AT0100176), Feb 12, 2001: PROXIMITY SENSOR. OUT OF ADJ. AIRCRAFT WOULD NOT TRANSFER TO FLIGHT MODE. AIRCRAFT WAS FERRIED FOR TROUBLESHOOTING. RIGGED AND ADJUSTED GROUND SENSE MECHANISM AND SERVICED NOSE STRUT IAW DC9
- [SDR AT0100001](https://openairdocs.org/sdr/AT0100001), Jan 12, 2001: STRUT. DISCHARGED. UNABLE TO RAISE GEAR ON TAKEOFF. SUSPECT SQUAT SWITCH PROBLEM. TRIED GEAR LEVER SEVERAL TIMES. SERVICED NOSE STRUT WITH NITROGEN IAW MM 32-21. PERFORMED CHECK O
- [SDR AT0000504](https://openairdocs.org/sdr/AT0000504), Dec 15, 2000: SMOKE DETECTOR. DAMAGED. FOUND JUST AFTER TAKE OFF 'A' LOOP SMOKE DETECTOR IN FORWARD CARGO COMPARTMENT LIGHT ILLUMINATED. RETURNED TO CAK AIRPORT LIGHT EXTINGUISHED AFTER LANDING. CORR
- [SDR AT0000502](https://openairdocs.org/sdr/AT0000502), Oct 29, 2000: SKIN. CRACKED. FOUND CRACKED EXTERIOR SKIN IN LOWER AFT DOOR JAMB CORNER OF FORWARD SERVICE DOOR. CUT OUT CRACKED SECTION, FABRICATED REPAIR DOUBLERS, SHIMS AND FILLERS. IAW D
- [SDR AT0000475](https://openairdocs.org/sdr/AT0000475), Oct 21, 2000: FRAME. CORRODED. FOUND VERTICAL STABILIZER LEADING EDGE UPPER KNEE CUP HAS CORROSION. REMOVED AND REPLACED VERTICAL STABILIZER LEADING EDGE HORSESHOE FORMER IAW DC9 SRM 51-10-02
- [SDR AT0000469](https://openairdocs.org/sdr/AT0000469), Oct 7, 2000: LONGERON. CORRODED. FOUND CORROSION ON LEFT LONGERON NR 20 AT THE OUTBOARD MEMBER SURFACE. CORROSION WAS OUT OF LIMITS, REMOVED CORRODED SECTION. FABRICATED AND INSTALLED LONGERON 
- [SDR AT0000468](https://openairdocs.org/sdr/AT0000468), Oct 6, 2000: FLOORBEAM. CORRODED. FOUND FLOOR SUPPORT BEAM AT BS 1012 RBL 24 TO LBL 24 WAS CORRODED. MECHANICALLY REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. REMOVED LEFT AND RIGHT BEAM AND LO
- [SDR AT0000466](https://openairdocs.org/sdr/AT0000466), Oct 6, 2000: SKIN. CORRODED. FOUND FLOOR BOARD NR 80 CORRODED ON SKIN. REMOVED CORROSION AND FOUND 3 CRACKS. REPAIRED SKIN, REMOVED AND INSTALLED HATS, AND REINSTALLED FLOOR BOARD IAW DC9 M
- [SDR AT0000465](https://openairdocs.org/sdr/AT0000465), Oct 6, 2000: FLOOR PANEL. CRACKED. FOUND FLOORBOARD NR 67 TEMPORARY PATCH INSTALLED. REMOVED FLOOR PANEL NR 67, FABRICATED REPAIR SKIN. REPLACED HAT CHANNELS AND INSTALLED REPAIR SKIN. REINSTALLE
- [SDR AT0000474](https://openairdocs.org/sdr/AT0000474), Oct 5, 2000: FLOOR PANEL. CORRODED. FOUND FLOOR PANEL 4692 CORRODED AND HAT CHANNELS CRACKED. REMOVED FLOOR PANEL AND REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. FABRICATED, TREATED, AND INSTALL
- [SDR AT0000467](https://openairdocs.org/sdr/AT0000467), Oct 5, 2000: FLOOR PANEL. CORRODED. FOUND FLOOR BOARD NR 4695 WAS CORRODED. BLENDED OUT CORROSION, FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED HATS AND FABRICATED AND INSTALLED FLOOR PANEL IAW
- [SDR AT0000490](https://openairdocs.org/sdr/AT0000490), Oct 3, 2000: PANEL. CORRODED. FOUND PANEL 1211 AT RIGHT WING LOWER LEADING EDGE HAS AREA OF CORROSION ON OUTER SURFACE. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS, FORMED REPAIR DOUBLER
- [SDR AT0000125](https://openairdocs.org/sdr/AT0000125), Mar 20, 2000: CONNECTOR. DISCONNECTED. NO RIGHT MAIN LANDING GEAR GREEN LIGHT FOR THE LANDING GEAR DOWN INDICATION. CORRECTIVE ACTION: CORRECTED OPEN WIRE AT RT GEAR DOWN LIMIT CONNECTOR (P1-129).
- [SDR AT0000127](https://openairdocs.org/sdr/AT0000127), Mar 18, 2000: LIGHT. DISLODGED. EMERGENCY PATH LIGHTING IN BUSINESS CLASS IS OUT OF TRACK. CORRECTIVE ACTION: RESECURED LIGHT.
- [SDR AT0000057](https://openairdocs.org/sdr/AT0000057), Jan 25, 2000: LIGHT. FAILED. FOUND TAIL CONE LEFT STAIR EMERGENCY LIGHT WOULD NOT ILLUMINATE. RELAMPED UNIT IAW DC9 MM 33-50.
- [SDR AT0000038](https://openairdocs.org/sdr/AT0000038), Jan 23, 2000: STRUT. DISCHARGED. FOUND LANDING GEAR UPLATCH RELEASE OR GROUND SHIFT DID NOT WORK AND WOULD NOT RAISE. ON FINAL AT BUF (BUFFALO). GROUND SHIFT OR THE UPLATCH RELEASE WAS HEARD TO
- [SDR AT0000037](https://openairdocs.org/sdr/AT0000037), Jan 21, 2000: STRUT. DISCHARGED. FOUND AFTER TAKEOFF AIRCRAFT WOULD NOT PRESSURIZE AND GEAR WOULD NOT COME UP. RETURNED TO BMI (BLOOMINGTON-NORMAL). STEERING IN AIR WOULD TURN. INSPECTED AIRCRA
- [SDR AT0000008](https://openairdocs.org/sdr/AT0000008), Jan 3, 2000: ENGINE. FOD. ON CLIMB-OUT, NOISE AND VIBRATION WERE NOTED FROM NUMBER 2 ENGINE. NR 2 ENGINE SHUT DOWN, AIRCRAFT RETURNED FOR LANDING. REMOVED AND REPLACED NR 2 ENGINE AND CO
- [SDR AT9900895](https://openairdocs.org/sdr/AT9900895), Dec 21, 1999: GLIDE SLOPE. INOPERATIVE. DURING CLIMB-OUT, NR 2 NAV BECAME INOPERATIVE AND ALL FLOURESCENT LIGHTS FLICKERED. RESEATED NR 2 NAV CONTROL PANEL IAW DC9 MM 34-32 AND TESTED LIGHTING IAW DC9
- [SDR AT9900722](https://openairdocs.org/sdr/AT9900722), Oct 9, 1999: CLAMP. FAILED. INBOUND TO ATL LOST CABIN PRESSURIZATION AT 14,000 FT, PASSENGER OXYGEN MASKS DEPLOYED. BOTH AIR CONDITIONING PACKS QUIT AT THE SAME TIME. BOTH PACKS WERE RESTA
- [SDR AT9900637](https://openairdocs.org/sdr/AT9900637), Sep 5, 1999: RIB. GOUGED. SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND GOUGED ON THE LEADING EDGE NR 3 SLAT RIB AT XOS 288.193. BLEND OUT GOUGED AREA, TREAT, PRIMED, AND REFINISH I
- [SDR AT9900587](https://openairdocs.org/sdr/AT9900587), Aug 14, 1999: SKIN. CORRODED. DURING A ROUTINE INSPECTION AT TIMCO LAKE CITY FL, FOUND EXTERIOR FUSELAGE SKIN HAS BULGE AT BS 990 L25L. REMOVED CORROSION AT BS 976-996. FABRICATED, TREATED, 
- [SDR AT9900586](https://openairdocs.org/sdr/AT9900586), Aug 13, 1999: SKIN. CORRODED. DURING A ROUTINE INSPECTION AT TIMCO LAKE CITY FL, FOUND EXTERIOR FUSELAGE SKIN OF AFT CARGO DOOR AT BS 935 CORRODED. CUT OUT CORRODED AREA. FORMED, DRILLED, CO
- [SDR AT9900570](https://openairdocs.org/sdr/AT9900570), Aug 9, 1999: LONGERON. CHAFED. DURING SCHEDULED INSPECTION AT TIMCO, FOUND FLANGE OF LONGERON AT RT BOTTOM OF BS 1076 CHAFED. BLENDED OUT CHAFED AREA. FABRICATED AND INSTALLED EXTERNAL STRAP 
- [SDR AT9900569](https://openairdocs.org/sdr/AT9900569), Aug 6, 1999: PANEL. CORRODED. DURING SCHEDULED INSPECTION AT TIMCO LAKE CITY FL, FOUND CORROSION ON INNER FLANGE LT PANEL NR 2108A. CLEANED CORROSION ON INNER FLANGE. FABRICATED, TREATED, PR
- [SDR AT9900564](https://openairdocs.org/sdr/AT9900564), Jul 31, 1999: FIXED VANE. CORRODED. DURING SCHEDULED CHECK AT TIMCO LAKE CITY FL, FOUND SPOTS OF CORROSION ON UNDERSIDE OF RT WING FLAP FIXED VANE. REMOVED CORROSION. FABRICATED FILLERS AND DOUBLE
- [SDR AT9900567](https://openairdocs.org/sdr/AT9900567), Jul 29, 1999: FLOOR. CORRODED. DURING SCHEDULED CHECK AT TIMCO LAKE CITY FL, FOUND FWD ENTRY FLOOR PANEL AT BS 160-200 RT CORRODED. FABRICATED NEW PANEL IAW DC9 SRM 53-20-0, 51-10-4.
- [SDR AT9900563](https://openairdocs.org/sdr/AT9900563), Jul 29, 1999: FLOOR. CORRODED. DURING SCHEDULED CHECK AT TIMCO LAKE CITY FL, FOUND FLOOR PANEL ON RT SIDE AT BS 280 CORRODED. FABRICATED NEW PANEL AND INSTALLED IAW DC9 SRM 51-21-0, 51-30-1.
- [SDR AT9900562](https://openairdocs.org/sdr/AT9900562), Jul 29, 1999: FIXED VANE. CORRODED. DURING SCHEDULED CHECK AT TIMCO LAKE CITY FL, FOUND OUTBOARD FIXED VANE ON RT WING CORRODED. FABRICATED FILLER AND DOUBLER. INSTALLED IAW DC9 SRM 57-50-1, 51-70
- [SDR AT9900561](https://openairdocs.org/sdr/AT9900561), Jul 29, 1999: PANEL. CORRODED. DURING SCHEDULED CHECK AT TIMCO LAKE CITY FL, FOUND RT WING LOWER LEADING EDGE PANEL CORRODED. REMOVED CORROSION. FABRICATED DOUBLERS, TREATED, PRIMED AND INSTA
- [SDR AT9900541](https://openairdocs.org/sdr/AT9900541), Jul 29, 1999: FITTING. CORRODED. SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND THE FORWARD CABIN GALLEY AREA AT BS 149 L-18R AT CUSP LINE LOWER FRAME WEB AND ATTACH FITTING CORRODED. REMOV
- [SDR AT9900540](https://openairdocs.org/sdr/AT9900540), Jul 29, 1999: WEB. CRACKED. SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND THE LEFT CUSP WEB AT BS 737-756 WITH CORROSION AND CRACKS. FABRICATED NEW CUSP WEB, TRIMMED AND DRILLED TO FI
- [SDR AT9900545](https://openairdocs.org/sdr/AT9900545), Jul 27, 1999: FLOOR. CORRODED. SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND THE FORWARD ENTRY FLOOR PANEL AT BS 180-200 CORRODED. FABRICATED FLOOR BOARD, DRILLED, DEBURRED, COUNTERSUNK,
- [SDR AT9900546](https://openairdocs.org/sdr/AT9900546), Jul 25, 1999: SKIN. CORRODED. SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND THE RIGHT WING LEADING EDGE PANEL NR 1219A CORRODED AND ANGLE SUPPORT CHAFFED. REMOVED CORROSION, BLEND OUT G
- [SDR AT9900565](https://openairdocs.org/sdr/AT9900565), Jul 24, 1999: FITTING. CORRODED. DURING SCHEDULED CHECK AT TIMCO LAKE CITY FL, FOUND LONGERON END FITTING AT BS 990 L-25L CORRODED. DRILLED NEW LONGERON END FITTING IAW DC9 SRM 51-10-2, 51-10-3
- [SDR AT9900535](https://openairdocs.org/sdr/AT9900535), Jul 23, 1999: FLOOR. CORRODED. DURING A SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND FWD ENTRY RT FLOOR PANEL AT BS 200-280 CORRODED. 3 HAT CHANNELS CRACKED, ELONGATED HOLES AND INSULAT
- [SDR AT9900544](https://openairdocs.org/sdr/AT9900544), Jul 22, 1999: SKIN. CORRODED. SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND THE RIGHT WING FLAP 25 AND 27 INCHES OUTBOARD OF INBOARD FLAP ACTUATOR CORRODED. REMOVED FASTENERS, BURNISHED
- [SDR AT9900607](https://openairdocs.org/sdr/AT9900607), Jul 21, 1999: FLOOR. CORRODED. SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND RIGHT FLOOR PANEL AT BS 160-180 CORRODED. FABRICATED FLOORBOARD PANEL, DRILLED, DEBURRED, DIMPLED, ALODINED, 
- [SDR AT9900536](https://openairdocs.org/sdr/AT9900536), Jul 21, 1999: FRAME. CORRODED. DURING A SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND CANTED FRAME AT BS 1074 CORRODED ON FWD SURFACE BELOW L-2L. REMOVED OLD WEB. FABRICATED WEB REPAIR. 
- [SDR AT9900534](https://openairdocs.org/sdr/AT9900534), Jul 21, 1999: FLOOR. CORRODED. DURING A SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND FLOOR PANEL NR 4693 AT BS 180-200 CORRODED ON TOP SIDE OF PANEL AND INSULATION TORN. REMOVED CORROSI
- [SDR AT9900560](https://openairdocs.org/sdr/AT9900560), Jul 20, 1999: FITTING. CORRODED. DURING SCHEDULED CHECK AT TIMCO LAKE CITY FL, FOUND LONGERON END FITTING CORRODED AT BS 990 L24L. OBTAINED NEW END FITTING. DRILLED AND DEBURRED IAW SRM 51-10-2
- [SDR AT9900513](https://openairdocs.org/sdr/AT9900513), Jul 19, 1999: FLOOR. CORRODED. SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND FLOOR PANEL AT BS 200-280 LEFT CORRODED ALONG EDGE UPPER AND LOWER FLANGE. CRACKS ON END HOLES IN PANEL. HAT 
- [SDR AT9900543](https://openairdocs.org/sdr/AT9900543), Jul 18, 1999: SEAT TRACK. CORRODED. SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND THE CABIN RIGHT INBOARD SEAT TRACK AT 198-206 RBL-22 CORRODED. REMOVED SEAT TRACK, LOCATED AND DRILLED, TRIMM
- [SDR AT9900542](https://openairdocs.org/sdr/AT9900542), Jul 18, 1999: SEAT TRACK. CORRODED. SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND THE FORWARD CABIN OUTBOARD SEAT TRACK AT BS 198-205 RBL-44 CORRODED. REMOVED SEAT TRACK, CUT, DRILLED, TRIMME
- [SDR AT9900640](https://openairdocs.org/sdr/AT9900640), Jul 17, 1999: PAN. CORRODED. SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND THE RIGHT SIDE AFT CARGO PIT DOOR CUT OUT CORRODED. REPAIRED THE AFT CARGO DOOR FUSELAGE CUT OUT PAN AFT CORN
- [SDR AT9900599](https://openairdocs.org/sdr/AT9900599), Jul 17, 1999: PANEL. CORRODED. DURING A ROUTINE INSPECTION AT TIMCO LAKE CITY FL, FOUND EXTERIOR FUSELAGE LT SIDE AT BS 237-303 HAS SPOTS OF SURFACE CORROSION AROUND WINDOW FRAME BELT. HFEC A
- [SDR AT9900337](https://openairdocs.org/sdr/AT9900337), Apr 27, 1999: DUCT. LOOSE. TAIL COMPARTMENT TEMPERATURE HIGH LIGHT CAME ON AFTER TAKEOFF, LIGHT WENT OUT WHEN LEFT THROTTLE PULLED BACK TO IDLE. AIR RETURN. RESECURED DUCT BEFORE LEFT HAN

All 52: https://openairdocs.org/deregistered/N866AT-2005-08-12/reports.md

## 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 20000123001169I](https://openairdocs.org/incident/20000123001169I), Jan 23, 2000: Doug DC932 (N866AT), Buffalo, NY. (-23) On Sunday, January 23, 2000, at 0713 local, an air tran airways DC-9 returned and landed at buf on runway 23 due to an unsafe gear indication. The ARFF…

## Other aircraft with N866AT

- [Registered now](https://openairdocs.org/aircraft/N866AT): Piper PA-44-180, S/N 4496624, built 2025

---
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.