# N824AT: 1968 Douglas DC-9-32, registration cancelled 2013-08-22 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: August 22, 2013 - Status when cancelled: Sale reported, canceled - Airframe: [Douglas DC-9-32](https://openairdocs.org/model/douglas-dc-9-32) (registry code 3022066) - Engine: [Pratt & Whitney JT8D-5](https://openairdocs.org/engine/pratt-whitney-jt8d-5) (registry code 52046) - Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE), [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs) - Serial number: 47278 - Year built: 1968 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: September 18, 1968 - Last registry action: November 13, 2003 - Mode S code: AB3FC9 - Location: [Miami, FL](https://openairdocs.org/faa-place/FL/Miami) - Physical address: [Oklahoma City, OK](https://openairdocs.org/faa-place/OK/Oklahoma%20City) - Owner type: Individual - Owner's area on the map: 25.7743° N, 80.1937° W: Placed by OpenAirDocs: center of Miami, FL, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N824AT - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=824AT - Page: https://openairdocs.org/deregistered/N824AT-2013-08-22 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 (39) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR AT0100231](https://openairdocs.org/sdr/AT0100231), Aug 23, 2001: FIRE BOTTLE. DISCHARGED. FOUND FORWARD CARGO FIRE INDICATION ILLUMINATED. CORRECTIVE ACTION: CHECKED FORWARD CARGO AREA, COULD NOT DUPLICATE PROBLEM, AICRAFT WAS FERRIED TO AVBORNE FOR - [SDR AT0100225](https://openairdocs.org/sdr/AT0100225), Jul 15, 2001: SMOKE DETECTOR. MALFUNCTIONED. FORWARD CARGO FIRE DETECTOR LIGHT ILLUMINATED WITH THE MASTER CAUTION LIGHT. EMERGENCY WAS DECLARED AND NR 2 FIRE BOTTLE WAS DISCHARGED AND AFT TAIL CONE SLIDE - [SDR AT0100213](https://openairdocs.org/sdr/AT0100213), Jun 30, 2001: BATTERY PACK. DISCHARGED. FOUND EMERGENCY LIGHTS OUT ON ROWS 23, 25, AND 28. REPLACED BATTERY PACK IAW DC9 MM 33. - [SDR AT0200004](https://openairdocs.org/sdr/AT0200004), May 29, 2001: WARNING SYSTEM. MALFUNCTIONED. CARGO FIRE WARNING TONE SOUNDED WITH MASTER WARNING LIGHT ON DESCENT IN ATL. CONDITION WAS INTERMITTENT, SOUNDED TWICE WAS UNABLE TO DETERMINE WHICH LOOP. CORRE - [SDR AT0100098](https://openairdocs.org/sdr/AT0100098), Feb 22, 2001: ANGLE. CRACKED. FOUND FLOOR SUPPORT ANGLE CRACKED IN FORWARD PIT AT BS 218 LONGERON 28 RIGHT. FABRICATED AND INSTALLED ANGLE SUPPORT IAW DC9 SRM 51-30, 51-10-04, 51-10-03, AND - [SDR AT0100085](https://openairdocs.org/sdr/AT0100085), Feb 16, 2001: SEAT TRACK. CORRODED. FOUND LEFT INBOARD SEAT TRACK AT BS 918 - 965 CORRODED BEYOND LIMITS. REPLACED CORRODED SECTION OF SEAT TRACK IAW DC9 SRM 53-05 FIG 4B & 4F. - [SDR AT0100099](https://openairdocs.org/sdr/AT0100099), Feb 14, 2001: LONGERON. CRACKED. FOUND LONGERON IN E&E COMPARTMENT CRACKED AT BS 200 LONGERON 29 RIGHT. INSTALLED LONGERON SPLICES IAW DC9 SRM 53-02 FIG 18. - [SDR AT0100092](https://openairdocs.org/sdr/AT0100092), Feb 14, 2001: FLOOR PANEL. CORRODED. FOUND FORWARD CABIN FLOOR PANEL BS 155 CORRODED BEYOND LIMITS. FABRICATED AND INSTALLED NEW FLOOR PANEL IAW DC9 SRM 51-10-02, 51-10-03, 51-10-04, 53-21 FIG 20 A - [SDR AT0100084](https://openairdocs.org/sdr/AT0100084), Feb 14, 2001: SKIN. DENTED. REPLACE TEMPORARY REPAIR WITH PERMANENT REPAIR AT BS 976. REPLACED REPAIR IAW DC SRM 53-04 FIG 12B, 51-10-03, AND 51-20. - [SDR AT0100102](https://openairdocs.org/sdr/AT0100102), Feb 13, 2001: SKIN. CRACKED. FOUND AFT PIT CARGO DOOR INNER SKIN TORN AT AFT HINGE. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC9 SRM 52-05, 51-30-01, 51-30-02, AND 51-30-05. - [SDR AT0100091](https://openairdocs.org/sdr/AT0100091), Feb 13, 2001: FLOOR PANEL. CORRODED. FOUND FLOOR PANEL 47 CORRODED BEYOND LIMITS. REPLACED FLOOR PANEL IAW DC9 SRM 53-21 AND 51-20-02. - [SDR AT0100101](https://openairdocs.org/sdr/AT0100101), Feb 9, 2001: LONGERON. CRACKED. FOUND LONGERON 27R CRACKED AT BS 258. FABRICATED AND INSTALLED REPAIR SPLICES IAW DC9 SRM 51-10-05, 51-10-04, AND 53-02 FIG 18. - [SDR AT0100096](https://openairdocs.org/sdr/AT0100096), Feb 9, 2001: WEB. DAMAGED. FOUND HOLE AT NUT PLATE IN FORWARD PIT WEB BS 370 LONG 24R. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC9 SRM 51-10-03, 51-10-04, 53-01 FIG 2, 53-30-02, AND R - [SDR AT0100089](https://openairdocs.org/sdr/AT0100089), Feb 9, 2001: PAN. CORRODED. FOUND G4 GALLEY FLOOR PAN CORRODED BEYOND LIMITS. FORMED AND INSTALLED FLOOR PAN AND HAT CHANNELS IAW DC9 SRM 51-10-03, 51-30-02, 53-01 FIG 1, AND 53-20 FIG 5C. - [SDR AT0100088](https://openairdocs.org/sdr/AT0100088), Feb 9, 2001: DOOR FRAME. GOUGED. FOUND FORWARD GALLEY DOOR JAMB GOUGED BEYOND LIMITS. REMOVED GOUGED SECTION AND INSTALLED REPAIR IAW DC9 SRM 53-05 FIG 55, 51-10-02, 51-10-03, 51-10-04, 51-30-0 - [SDR AT0100104](https://openairdocs.org/sdr/AT0100104), Feb 8, 2001: PANEL. CHAFED. FOUND VERTICAL STABILIZER UPPER FAIRING CHAFED OUT OF LIMITS. REPLACED SKIN PANEL IAW DC9 SRM 55-01 FIG 1, 55-31, 51-10-02, 51-10-03, 51-10-04, AND 51-30-02. - [SDR AT0100103](https://openairdocs.org/sdr/AT0100103), Feb 8, 2001: DOOR FRAME. CRACKED. FOUND AFT CARGO DOOR FRAME CRACKED. STOP DRILLED CRACK AND FABRICATED AND INSTALLED DOUBLER IAW DC9 SRM 51-10-02, 51-10-03, 51-10-04, 51-30-02, 51-30-01, AND 52 - [SDR AT0100100](https://openairdocs.org/sdr/AT0100100), Feb 8, 2001: SKIN. GOUGED. FOUND AFT PIT CARGO DOOR SKIN GOUGED BEYOND LIMITS. INSTALLED REPAIR DOUBLER IAW DC9 SRM 52-05 FIG 3, 52-01 FIG 1, 51-10-04, 51-10-02, AND 51-10-03. - [SDR AT0100097](https://openairdocs.org/sdr/AT0100097), Feb 8, 2001: ANGLE. CORRODED. FOUND RIGHT NOSE LANDING GEAR WHEEL WELL LOWER ANGLE CORRODED BEYOND LIMITS AT BS 109 RBL 27. INSTALLED REPAIR IAW REO-L00405. - [SDR AT0100093](https://openairdocs.org/sdr/AT0100093), Feb 8, 2001: FLOOR SUPPORT. CORRODED. FOUND FORWARD CABIN FLOOR SUPPORT AT BS 200 CORRODED. REPLACED FLOOR SUPPORT IAW DC9 SRM 53-21, 53-11-01, AND 53-30-05. - [SDR AT0100087](https://openairdocs.org/sdr/AT0100087), Feb 7, 2001: DOOR FRAME. CORRODED. FOUND AFT CARGO DOOR JAMB CORRODED BEYOND LIMITS. INSTALLED NEW DOOR JAMB IAW DC9 SRM 53-05 FIG 44, 51-30-01, 51-30-02, 51-30-04, 51-10-03, 51-30-05, AND RES 01 - [SDR AT0100086](https://openairdocs.org/sdr/AT0100086), Feb 7, 2001: WEB. CRACKED. FOUND R-1 DOOR JAMB LOWER CORNER SKIN CRACKED. CUT OUT CRACK AND INSTALLED REPAIR IAW EO 09-5310-29-E1472. - [SDR AT0100090](https://openairdocs.org/sdr/AT0100090), Feb 6, 2001: CARGO TRACK. CORRODED. FOUND FORWARD PIT CARGO TRACK BS 239 - 340 CORRODED BEYOND LIMITS. INSTALLED NEW SECTION OF CARGO TRACK IAW DC9 SRM 51-10-03, 51-10-04, 53-05 FIG 4C, AND 53-21. - [SDR AT0200002](https://openairdocs.org/sdr/AT0200002), Dec 22, 2000: CONTROLLER. MALFUNCTIONED. CABIN CLIMBED TO 11,000 FT AND MASKS (OXYGEN) DEPLOYED. REPACKED MASK GOOD FOR SERVICE. - [SDR AT0100004](https://openairdocs.org/sdr/AT0100004), Dec 20, 2000: LIGHT. INOPERATIVE. FOUND FORWARD EMERGENCY FLOOR LIGHT INOPERATIVE. CRIMPED BROKEN WIRE IAW 33-21. - [SDR AT0000276](https://openairdocs.org/sdr/AT0000276), May 18, 2000: BATTERY PACK. DISCHARGED. FOUND RIGHT ENGINE NACELLE EMERGENCY LIGHT NOT ILLUMINATING. REMOVED AND REPLACED BATTERY PACK IAW DC9 MM 33-50. - [SDR AT0000021](https://openairdocs.org/sdr/AT0000021), Dec 24, 1999: WEB. CORRODED. FOUND SURFACE CORROSION AND SEVERAL CRACKS IN LT CUSP WEB OUTBOARD EDGE AT BS 897 TO BS 965. REMOVED SECTION OF CUSP WEB AT BS 889-965. INSTALLED NEW CUSP WEB I - [SDR AT9900914](https://openairdocs.org/sdr/AT9900914), Dec 23, 1999: SKIN. LIGHTING STRIKE. FOUND LIGHTNING STRIKE AT FS 536 BETWEEN LONGERON 21R AND 22R ON FUSELAGE SKIN. CUTOUT STRIKE AREA. FABRICATED AND INSTALLED DOUBLER REPAIR IAW TIMCO EO 99-1445 - [SDR AT9900913](https://openairdocs.org/sdr/AT9900913), Dec 23, 1999: SKIN DOUBLER. CORRODED. FOUND INTERNAL DOUBLER CORRODED AT BS 900 BETWEEN LONGERONS 21L AND 22L. CUTOUT CORRODED AREA. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW TIMCO EO 9 - [SDR AT0000019](https://openairdocs.org/sdr/AT0000019), Dec 21, 1999: SKIN. LIGHTNING STRIKE. FOUND LIGHTNING STRIKES AT LT CABIN WINDOW CUTOUT NR 17. FABRICATED AND INSTALLED WINDOW CUTOUT DOUBLER IAW TIMCO EO 99-1432 AND SERVICE REWORK DRAWING SR095300 - [SDR AT0000068](https://openairdocs.org/sdr/AT0000068), Dec 20, 1999: TEE CAP. CORRODED. FOUND TEE CAP IN LT WING BETWEEN STRINGER 12 AND 17 CORRODED. FABRICATED AND INSTALLED REPAIR CLIPS IAW SB 57-98R8. - [SDR AT0000020](https://openairdocs.org/sdr/AT0000020), Dec 20, 1999: SEAT TRACK. CORRODED. RT INBOARD SEAT TRACK CORRODED AT BS 900 TO 965. REMOVED AND REPLACED SEAT TRACK FROM BS 878 TO 965 IAW DC9 SRM 51-10-3, 53-05 FIG 4 AND 53-20-1. - [SDR AT9900912](https://openairdocs.org/sdr/AT9900912), Dec 13, 1999: FLOOR PANEL. CORRODED. FOUND CORROSION AROUND FASTENER HOLES ON FLOOR PANEL NR 71. FABRICATED AND INSTALLED REPAIR IAW SRM 53-3 AND 51-30-2. - [SDR AT0000018](https://openairdocs.org/sdr/AT0000018), Dec 13, 1999: FLOOR BEAM. CHAFFED. FLOORBEAM AT BS 598 LBL 12 HAS 5 CHAFFED SPOTS. FABRICATED AND INSTALLED 1 DOUBLER, 3 SHIMS, 3 WEAR STRIPS IAW TIMCO EO 99-1415. - [SDR AT9900911](https://openairdocs.org/sdr/AT9900911), Dec 8, 1999: SUPPORT. CORRODED. FOUND FLOOR SUPPORT AT BS 160 - 218 AND BL 0 CORRODED. REMOVED CORRODED FLOOR SUPPORT. FABRICATED, TRIMMED, FORMED, DRILLED, DEBURRED, TREATED, PRIMED AND INSTA - [SDR AT0000372](https://openairdocs.org/sdr/AT0000372), Dec 3, 1999: STRINGER. CORRODED. DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND FORWARD SIDE OF STRINGER 23 TO HAVE EXFOLIATED CORROSION. REMOVED CORRODED AREA IAW EO 99-1426 REV - [SDR AT0000067](https://openairdocs.org/sdr/AT0000067), Dec 3, 1999: FLOORBEAM. CORRODED. FOUND FLOOR SUPPORT AT BS 197 BL 0 TO LBL 44 HAD EXFOLIATION CORROSION. REMOVED FLOOR SUPPORT, FABRICATED, TRIMMED, DRILLED, DEBURRED, TREATED, PRIMED AND INSTA - [SDR AT0000373](https://openairdocs.org/sdr/AT0000373), Dec 1, 1999: WEB. CRACKED. DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND CRACK IN AFT CARGO BIN DOOR IN NR 5 WEB BEAM. STOP DRILLED CRACK, FABRICATED AND INSTALLED DOUBLER - [SDR AT9900639](https://openairdocs.org/sdr/AT9900639), Sep 16, 1999: O RING. DAMAGED. ON TAKEOFF, NOTICED STRONG ODOR. FLIGHT ATTENDANT REPORTED FUMES AND SMOKE OR HAZE IN CABIN, AS ODOR DISSIPATED HAZE REMAINED. FOUND CUT O-RING ON LEFT FUEL PRO ## 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 20010716020979I](https://openairdocs.org/incident/20010716020979I), Jul 16, 2001: Doug DC932 (N824AT), Moline, IL. (-23) During descent into mli the aircraft experienced a forward cargo fire detection. Crew initiated emergency procedures and discharged #1 fire bottle. Crew… ## Other aircraft with N824AT - [Registered now](https://openairdocs.org/aircraft/N824AT): Piper PA-44-180, S/N 4496549, built 2022 --- 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.