# N813AT: 1968 Douglas DC-9-32, registration cancelled 2006-05-16 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: May 16, 2006 - Status when cancelled: Valid registration - 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: 47318 - Year built: 1968 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: December 12, 1968 - Certificate issued: April 20, 2000 - Last registry action: December 15, 2004 - Mode S code: AB1493 - 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/N813AT - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=813AT - Page: https://openairdocs.org/deregistered/N813AT-2006-05-16 From the FAA registry file of October 31, 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 (37) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR AT9900864](https://openairdocs.org/sdr/AT9900864), Dec 2, 1999: LAMP. FAILED. FOUND L1 DOOR OVERHEAD EMERGENCY LIGHT WILL NOT ILLUMINATE. RELAMPED, OPS CHECK NORMAL IAW DC9 MM 33-50. - [SDR AT9900704](https://openairdocs.org/sdr/AT9900704), Oct 2, 1999: BULB. FAILED. FOUND BOTH TAIL CONE SLIDE EMERGENCY LIGHTS WILL NOT ILLUMINATE. REPLACED LAMPS IAW DC9 MM 33-50. - [SDR AT9900272](https://openairdocs.org/sdr/AT9900272), Mar 30, 1999: HARDWARE. MISSING. ON CLIMBOUT, NR 2 ENGINE AT POWER BACK UNABLE TO REDUCE POWER BELOW MAXIMUM CLIMB. THROTTLE MOVEMENT NORMAL BUT POWER REMAINS AT MAXIMUM CLIMB AFTER BEING RETAR - [SDR AT9900275](https://openairdocs.org/sdr/AT9900275), Mar 25, 1999: JAMB. CORRODED. SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE AFT ENTRANCE LOWER DOOR JAMB LEFT CORNER CORRODED. DISASSEMBLE AFT ENTRANCE THRESHOLD AREA, REMOVED CORRODED WE - [SDR AT9900257](https://openairdocs.org/sdr/AT9900257), Mar 24, 1999: SKIN. DENTED. SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE RIGHT HAND FUSELAGE EXTERIOR SKIN WITH NUMEROUS DENTS AND REPAIRS FROM BS 229-598 L-18-26R. REMOVED AND REPLACE - [SDR AT9900256](https://openairdocs.org/sdr/AT9900256), Mar 20, 1999: SKIN. DENTED. SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE AFT VENTRAL STAIRS FUSELAGE SKIN AT YSD 27-98 WITH NUMEROUS DENT WITH CREASES. REMOVED STEPS TO GAIN ACCESS. RE - [SDR AT9900231](https://openairdocs.org/sdr/AT9900231), Mar 19, 1999: SKIN. CORRODED. SCHEDULED INSPECTION AT AERO CORP, FL. FOUND LIGHT SURFACE CORROSION ON BARE METAL 22 INCHES BELOW CUSP WEB AT BS 1142 ON THE LEFT SIDE. FOUND CORROSION ON SKIN - [SDR AT9900233](https://openairdocs.org/sdr/AT9900233), Mar 18, 1999: FITTING. CRACKED. SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE AFT VENTRAL STAIRS LOWER LEFT HAND SIDE CORNER FITTING CORRODED THROUGH OUT. REMOVED AND REPLACED CORRODED AND - [SDR AT9900273](https://openairdocs.org/sdr/AT9900273), Mar 15, 1999: SKIN. DENTED. SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE RIGHT SIDE NR 1 SLAT LOWER EXTERNAL SURFACE DENTED JUST INBOARD OF ANTI-ICE DUCT. CUT INNER SKIN FOR ACCESS, FA - [SDR AT9900232](https://openairdocs.org/sdr/AT9900232), Mar 15, 1999: SKIN. DENTED. SCHEDULED INSPECTION AT AERO CORP, FL. FOUND A GOUGE IN DENT AT BS 235 L-18L OUT OF LIMITS. FABRICATED EXTERNAL AND INTERNAL FINGER DOUBLER AND DOUBLER, DRILLED - [SDR AT9900284](https://openairdocs.org/sdr/AT9900284), Mar 13, 1999: FLOORBEAM. CRACKED. SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE FORWARD PIT BOTTOM OF FLOORBEAM WITH PREVIOUS REPAIR GOUGED, DENTED AND APPEARS TO HAVE A CRACK RUNNING TOWARDS - [SDR AT9900278](https://openairdocs.org/sdr/AT9900278), Mar 13, 1999: STRUCTURE. CORRODED. SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE AFT ENTRY DOORWAY THRESHOLD WEB, JAMB SUPPORT AND SPLICE AND LOWER CHANNEL FRAME CORRODED. REMOVED CORROSION, F - [SDR AT9900211](https://openairdocs.org/sdr/AT9900211), Mar 13, 1999: WEB. CORRODED. SCHEDULED INSPECTION AT AERO CORP, FL, FOUND THE CABIN INTERIOR RIGHT AFT LAVATORY FRAME TO FLOOR BEAM ATTACHMENT EXFOLIATED AT BS 996. FABRICATED WEB AND DOUBL - [SDR AT9900197](https://openairdocs.org/sdr/AT9900197), Mar 13, 1999: SKIN. CRACKED. SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE NR 1 PYLON TRAILING EDGE PANEL LOWER SIDE SKIN REPAIR DISBONDED AND CORNERS CRACKED OFF AT BS 1030 TO 1076. REM - [SDR AT9900258](https://openairdocs.org/sdr/AT9900258), Mar 9, 1999: DOUBLER. OUT OF POSITION. SCHEDULED INSPECTION AT AERO CORP, FL. FOUND AN EXTERNAL DOUBLER THAT INTERFERES WITH WINDOW BELT DOUBLER AT BS 464 L-14 ON THE RIGHT SIDE. REMOVED EXISTING DOU - [SDR AT9900210](https://openairdocs.org/sdr/AT9900210), Mar 8, 1999: ANGLE. CORRODED. SCHEDULED INSPECTION AT AERO CORP, FL, FOUND CORROSION AROUND FASTENER HEADS ON ATTACH ANGLE AND WEB (TOP SIDE) AT BS 130 LBL 54 ON THE E/E BAY CEILING. REMOVED - [SDR AT9900194](https://openairdocs.org/sdr/AT9900194), Mar 7, 1999: SPAR. CRACKED. SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE LEFT HAND REAR SPAR LOWER CHORD AFT TANG HAS A CRACK INDICATION AT INBOARD BUTE DOOR THIRD HOLE FROM OUTBOARD E - [SDR AT9900282](https://openairdocs.org/sdr/AT9900282), Mar 3, 1999: CARGO TRACK. CORRODED. SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE FORWARD PIT TRACK CORRODED ON THE BOTTOM SIDE. FABRICATED, LOCATED, DRILLED, DEBURRED, COUNTERSUNK, PRIMED, TRE - [SDR AT9900277](https://openairdocs.org/sdr/AT9900277), Mar 3, 1999: TRACK. CORRODED. SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE AFT PIT RIGHT SIDE FLOOR TRACK CORRODED ON BOTTOM FULL LENGTH. FABRICATED, DRILLED, DEBURRED, PRIMED, AND TREAT - [SDR AT9900276](https://openairdocs.org/sdr/AT9900276), Mar 2, 1999: TRACK. CORRODED. SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE FORWARD PIT RIGHT HAND TRACK BOTTOM SIDE CORRODED THROUGHOUT. REMOVED CORROSION, LOCATED NEW TRACK, DRILLED, CO - [SDR AT9900209](https://openairdocs.org/sdr/AT9900209), Mar 1, 1999: FLOORBEAM. CORRODED. SCHEDULED INSPECTION AT AERO CORP, FL, FOUND THE FLOORBEAM UPPER CAP CORRODED AROUND FASTENER HOLES AT BS 980 RBL 38 TO 42. REMOVED, FIT, TRIMMED, DRILLED, AND - [SDR AT9900280](https://openairdocs.org/sdr/AT9900280), Feb 27, 1999: FLOOR. CORRODED. SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE FORWARD PIT CENTER FLOOR PANEL CORRODED ALONG THE EDGES AND ELONGATED HOLES WITH NO EDGE DISTANCE. FABRICATED R - [SDR AT9900292](https://openairdocs.org/sdr/AT9900292), Feb 26, 1999: SUPPORT. CORRODED. SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE FORWARD CABIN FLOOR SUPPORT CORRODED ON THE UPPER SURFACE AND ON BOTTOM OF UPPER FLANGE AROUND CLIP NUTS AT BS - [SDR AT9900281](https://openairdocs.org/sdr/AT9900281), Feb 26, 1999: SEAT TRACK. CORRODED. SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE FORWARD CABIN SEAT TRACK AT BS 200 TO 279 RBL 22 CORRODED. REMOVED FLOOR PANELS, FABRICATED NEW SEAT TRACK AND - [SDR AT9900208](https://openairdocs.org/sdr/AT9900208), Feb 26, 1999: SUPPORT. CORRODED. SCHEDULED INSPECTION AT AERO CORP, FL, FOUND THE FORWARD CABIN FLOOR SUPPORT CORRODED AND PART OF UPPER FLANGE HAS BEEN PREVIOUSLY REMOVED AT BS 210 TO 237 LBL - [SDR AT9900286](https://openairdocs.org/sdr/AT9900286), Feb 25, 1999: BULKHEAD ANGLE. CORRODED. SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE LEFT HAND AFT PIT BULKHEAD LINER SUPPORT ANGLE CORRODED AND GILLINER PANEL MISSING. FORMED SUPPORT ANGLE, CUT, - [SDR AT9900279](https://openairdocs.org/sdr/AT9900279), Feb 24, 1999: WEB. CORRODED. SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE LEFT CUSP WEB AT BS 229 L-18 CORRODED. REMOVED CORRODED PORTION OF WEB, REMOVED SUPPORT FITTING FOR ACCESS AND - [SDR AT9900283](https://openairdocs.org/sdr/AT9900283), Feb 21, 1999: CHANNEL. CORRODED. SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE AFT COMPARTMENT LEFT HAND HAT CHANNEL ADJACENT TO THE LOWER BULKHEAD PRESSURE CAP CORRODED AT BS 996 ON THE LOW - [SDR AT9900294](https://openairdocs.org/sdr/AT9900294), Feb 20, 1999: BRACKET. CORRODED. SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE LEFT FORWARD LOWER FLOOR PANEL BRACKET CORRODED AT BS 218 LBL 42. REMOVED BRACKET, CUT, DRILLED, TRIM, ALODINED - [SDR AT9900290](https://openairdocs.org/sdr/AT9900290), Feb 20, 1999: BRACKET. CRACKED. SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE GILLINER ATTACH ANGLE CRACKED AT BS 237 L-24. PERFORMED HFEC TO VERIFIED CRACK. REMOVED CRACKED ATTACH ANGLE, W - [SDR AT9900288](https://openairdocs.org/sdr/AT9900288), Feb 20, 1999: FLOORBEAM. CRACKED. SCHEDULED INSPECTION AT AERO CORP, FL. FOUND UPPER CAP CRACKED AND CORRODED ON FLOORBEAM WEB AT BS 996 RBL 54. REMOVED PULLEY TOWERS, REMOVED FLOOR UPPER BEAM C - [SDR AT9900287](https://openairdocs.org/sdr/AT9900287), Feb 20, 1999: BRACKET. CORRODED. SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE AFT CARGO COMPARTMENT FUEL SHUT OFF BRACKET AT BS 935 CORRODED. RELIEVED CABLE TENSION, REMOVED AND REPLACED BR - [SDR AT9900293](https://openairdocs.org/sdr/AT9900293), Feb 19, 1999: BRACKET. CORRODED. SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE SIDE ROLLER BEARING FITTING CORRODED ON THE INBOARD LEFT SIDE OF THE HORIZONTAL STABILIZER. REMOVED AND REPLACE - [SDR AT9900285](https://openairdocs.org/sdr/AT9900285), Feb 19, 1999: FLOOR. CORRODED. SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE G-4 FLOOR PAN SKIN CORRODED. REMOVED FLOOR PAN HAT SECTION, FABRICATED NEW SKIN, TREATED, PRIMED, INSTALLED SKI - [SDR AT9900295](https://openairdocs.org/sdr/AT9900295), Feb 18, 1999: SKIN. CRACKED. SCHEDULED INSPECTION AT AERO CORP, FL. FOUND LIGHTNING STRIKES ON THE LEFT SIDE NOSE AT Y-69.550 AND RIGHT SIDE NOSE AT Y-69.550 AND Y-76.550. REMOVED E/E ACCES - [SDR AT9900221](https://openairdocs.org/sdr/AT9900221), Feb 17, 1999: SKIN. CORRODED. SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE FUSELAGE SKIN BULGE AT BS 275 L-18L. STRIPPED AREA, REMOVED FASTENERS, FOUND CORROSION. REMOVED SECTION OF SKIN - [SDR AT9900005](https://openairdocs.org/sdr/AT9900005), Jan 6, 1999: AIR DIST. ODOR. DURING FLIGHT, THE AFT LAVATORY SMOKE DETECTOR SOUNDED FLIGHT ATTENDANT REPORTED NO SMOKE, BUT VERIFIED SMOKE ALARMS DID SOUND. AIR CONDITIONING SMOKE PROCEDURE ## 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 19990410017629I](https://openairdocs.org/incident/19990410017629I), Apr 10, 1999: Doug DC932 (N813AT), Buffalo, NY. On Saturday, April 10, 1999 at 1710 EDT, a Douglas DC-9, N813AT, flight 552, operated by airtran airways, inc., on a flight from atlanta, Georgia to Buffalo,… ## Other aircraft with N813AT - [Registered now](https://openairdocs.org/aircraft/N813AT): Daniel J Thompson RV-9A, S/N 90097, built 2023 --- 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.