# N817AT: 1969 Douglas DC-9-32, registration cancelled 2004-09-30 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: September 30, 2004 - Status when cancelled: Triennial form not returned - 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: 47323 - Year built: 1969 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: November 14, 1994 - Certificate issued: December 22, 1994 - Last registry action: January 21, 2003 - Mode S code: AB236F - Owner when cancelled: [Airtran Airways Inc](https://openairdocs.org/faa-owner/AIRTRAN%20AIRWAYS%20INC) - Location: [Orlando, FL](https://openairdocs.org/faa-place/FL/Orlando) - Owner type: Corporation - Owner's area on the map: 28.4315° N, 81.3236° W: Placed by OpenAirDocs at the center of ZIP code 32827, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N817AT - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=817AT - Page: https://openairdocs.org/deregistered/N817AT-2004-09-30 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 (33) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR AT0200069](https://openairdocs.org/sdr/AT0200069), Jul 8, 2002: WIRE. BROKEN. NR 1 LEFT HAND AFT ACCESSORY EMERGENCY LIGHT WILL NOT ILLUMINATE. REPAIRED BROKEN WIRE L795W18 AT VENTRAL STAIR EMERGENCY LIGHTS PER WDM-31-51, OPS CHECK NORMAL - [SDR AT0200012](https://openairdocs.org/sdr/AT0200012), Oct 11, 2001: SKIN. CRACKED. FUSELAGE EXTERNAL SKIN HAS THREE (3) CRACKS AROUND RIVET HEADS AT STA 164 APPROX AND LONGERON 4 LEFT. CUT OUT DAMAGED AREA. NDT VERIFIED AFTER CUT OUT IAW NDT S - [SDR AT0200013](https://openairdocs.org/sdr/AT0200013), Oct 10, 2001: WEB. CRACKED. FORWARD GALLEY AREA AT FS 200/LBL 31 - LBL 40, FOUND CRACKED TO FLOOR WEB ON (2) EXISTING DOUBLER REPAIRS. REMOVED EXISTING DOUBLER AS PER DC-9 SRM 51-30-2. INS - [SDR AT0000443](https://openairdocs.org/sdr/AT0000443), Sep 19, 2000: COUPLER. MISSING. E-PATH MISSING COUPLER AT ROW 21. INSTALLED COUPLER IAW BRUCE INDUSTRIES INC PEEPLES INSTALLATION MANUAL 33-21-27. - [SDR AT0000442](https://openairdocs.org/sdr/AT0000442), Sep 19, 2000: COUPLER. MISSING. E-PATH LIGHTING, RED WIRE HAS NO END AT ROW 17. INSTALLED E-PATH LIGHTING COUPLE IAW 33-21-27. - [SDR AT0000362](https://openairdocs.org/sdr/AT0000362), Jul 19, 2000: BATTERY PACK. DISCHARGED. FOUND EXIT AND EMERGENCY LIGHTS OUT AT ROW 22 AND 19. REMOVED AND REPLACED BATTERY PACK BATTERIES IAW DC9 MM 33-53-00. - [SDR AT0000359](https://openairdocs.org/sdr/AT0000359), Jul 14, 2000: DOUBLER. DAMAGED. FOUND, REMOVED DOUBLER FROM BS 775. INSTALLED NEW DOUBLER IAW REO L00225. - [SDR AT0000366](https://openairdocs.org/sdr/AT0000366), Jul 7, 2000: FITTING. GOUGED. FOUND LEFT WING LEADING EDGE GOUGED AT CENTER RIB FITTING. BLENDED OUT GOUGE AND REPAIRED IAW REO-L00228. - [SDR AT0000368](https://openairdocs.org/sdr/AT0000368), Jul 3, 2000: SKIN. LIGHTNING STRIKE. FOUND LIGHTNING STRIKE AT LEFT HAND WINDOW BELT PANEL AT BS 908 - 937. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC9 MM 25-21-0, 53-05 FIGURE 11 AND REO L0022 - [SDR AT0000367](https://openairdocs.org/sdr/AT0000367), Jul 3, 2000: SKIN. LIGHTNING STRIKE. FOUND LIGHTNING STRIKE AT LEFT HAND WINDOW BELT PANEL AT BS 832 - 870. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC9 MM 25-21-0, 53-05 FIGURE 11 AND REO L0022 - [SDR AT0000358](https://openairdocs.org/sdr/AT0000358), Jul 2, 2000: LAP JOINT. CORRODED. FOUND SKIN LAP FUSELAGE SKIN PITTED BEYOND LIMITS AT L24 - L26. CUT OUT CORRODED SECTION AND INSTALLED REPAIR IAW REO L00229. - [SDR AT0000354](https://openairdocs.org/sdr/AT0000354), Jun 29, 2000: ATTACH ANGLE. CORRODED. FOUND G-2 GALLEY ANGLES CORRODED AT RIGHT SIDE OF G-2. REMOVED CORRODED ANGLES, FABRICATED AND INSTALLED NEW ANGLES IAW DC9 51-10-2, 51-10-3, 51-10-4, 51-30-2. - [SDR AT0000357](https://openairdocs.org/sdr/AT0000357), Jun 25, 2000: SKIN. CRACKED. FOUND FORWARD CARGO DOOR JAMB, LOWER, HAS CRACKS IN EXTERNAL SKIN. REMOVED EXISTING REPAIR, DOUBLER AND FILLER. CUT OUT CRACKED AREA AND FABRICATED 4 FILLERS, F - [SDR AT0000441](https://openairdocs.org/sdr/AT0000441), Jun 23, 2000: SPAR CAP. CORRODED. DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND RIGHT OUTBOARD LOWER SPAR CAP CORRODED BEYOND LIMITS. FABRICATED AND INSTALLED ANGLE REPAIR IAW DC - [SDR AT0000353](https://openairdocs.org/sdr/AT0000353), Jun 23, 2000: SPAR. CORRODED. FOUND RIGHT HAND OUTBOARD LOWER SPAR CAP WAS CORRODED. REMOVED CORROSION, FABRICATED, TREATED, PRIMED AND INSTALLED REPAIR ANGLE IAW DC9 SRM 57-09 FIGURE 11, 51 - [SDR AT0000356](https://openairdocs.org/sdr/AT0000356), Jun 22, 2000: SKIN. BULGED. FOUND BULGING SKIN AT BS 917 - 935, L28R - L26. REMOVED AND REPLACED SKIN IAW REO L00232. - [SDR AT0000355](https://openairdocs.org/sdr/AT0000355), Jun 22, 2000: SKIN. CORRODED. FOUND CORROSION AT BS 973, STRINGER 20 - 24 ON LEFT HAND SIDE. REMOVED CORROSION AND INSTALLED INTERNAL AND EXTERNAL DOUBLER IAW DC9 SRM 51-10-2, 51-30-2 AND RE - [SDR AT0000352](https://openairdocs.org/sdr/AT0000352), Jun 22, 2000: ATTACH ANGLE. CORRODED. FOUND AFT CARGO RIGHT HAND AFT BULKHEAD PANEL UPPER ATTACH ANGLE CORRODED. FORMED, FIT, TRIMMED, DRILLED, TREATED, AND PRIMED REPAIR ANGLE. INSTALLED ATTACH ANG - [SDR AT9900689](https://openairdocs.org/sdr/AT9900689), Sep 17, 1999: DOUBLER. CRACKED. FOUND 3 CRACKS IN FUSELAGE NOSE SKIN AT BS 76R BELOW RIGHT INTERCOSTAL. REMOVED, FABRICATED, AND INSTALLED REPAIR INTERNAL DOUBLERS AND FILLERS AT BS 75R IAW DC - [SDR AT9900437](https://openairdocs.org/sdr/AT9900437), May 26, 1999: SKIN. DENTED. SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND MULTIPLE SKIN DAMAGE (DENTS) ON THE RIGHT SIDE AT BS 229-408 L-18-26R. REMOVED AND REPLACED SKIN DAMAGE SECTI - [SDR AT9900403](https://openairdocs.org/sdr/AT9900403), May 22, 1999: FLOORBEAM. CORRODED. SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND THE PASSENGER CABIN FLOORBEAM IN AFT LAVATORY AREA CHAFED AND CORRODED AT BS 980 BL 0-44L. FORMED NEW FLOORBE - [SDR AT9900389](https://openairdocs.org/sdr/AT9900389), May 19, 1999: FLOOR. CORRODED. SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND THE FORWARD ENTRY FLOOR PANEL NR 4692 AT BS 200 BL 0-65R CORRODED. FABRICATED PARTS AND INSTALLED IAW DC9 SRM - [SDR AT9900439](https://openairdocs.org/sdr/AT9900439), May 15, 1999: FLOOR. CORRODED. SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND THE FORWARD ENTRY FLOOR PANEL NR 4693 AT LBL 45-65 CORRODED. REMOVED FLOOR PANEL, FABRICATED, COUNTERSUNK, DE - [SDR AT9900391](https://openairdocs.org/sdr/AT9900391), May 15, 1999: BLKHD FRAME. CORRODED. SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND ON THE CABIN LEFT FORWARD PYLON BULKHEAD AFT SIDE LOWER FRAME/FLOOR AT BS 965 CORRODED. CUT, DRILLED, AND DEB - [SDR AT9900402](https://openairdocs.org/sdr/AT9900402), May 14, 1999: FLOOR. CORRODED. SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND THE CABIN FLOOR PANEL NR 90 CORRODED AROUND THE EDGES. REMOVED, FIT, TRIMMED, DRILLED, TREATED, AND PRIMED RE - [SDR AT9900390](https://openairdocs.org/sdr/AT9900390), May 14, 1999: FLOORBEAM. CORRODED. SCHEDULED INSPECTION AT TIMCO, FL, FOUND PASSENGER CABIN FLOORBEAM RIGHT SIDE AFT LAVATORY AT BS 996 RBL 17-54R CORRODED. REMOVED UPPER CAP, LOCATED, DRILLED, A - [SDR AT9900376](https://openairdocs.org/sdr/AT9900376), May 13, 1999: FLOORBEAM. CORRODED. SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND PASSENGER CABIN FLOORBEAM CHAFED AND CORRODED AT BS 965 BL-30L. FORMED, FIT, TRIMMED, DRILLED AND INSTALLED R - [SDR AT9900375](https://openairdocs.org/sdr/AT9900375), May 12, 1999: FLOOR. CORRODED. SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND THE FORWARD FLOOR PANEL NR 4691 AT BS 160 TO 200 BL 0-45L CORRODED. FABRICATED NEW FLOOR PANEL, FIT, DRILLED - [SDR AT9900371](https://openairdocs.org/sdr/AT9900371), May 10, 1999: FLOORBEAM. CORRODED. SCHEDULED INSPECTION AT TIMCO, FL. FOUND THE CABIN FLOORBEAM UPPER FLANGE CORRODED AT BS 196 BL 0. REMOVED FLOORBEAM, CUT, DRILLED, DEBURRED, ALODINED, PRIMED A - [SDR AT9900440](https://openairdocs.org/sdr/AT9900440), May 8, 1999: SUPPORT. CORRODED. SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND THE CABIN ENTRY FLOOR SUPPORT UPPER FLANGE AT BS 196 BL 0-10L CORRODED. REMOVED, FORMED, DRILLED AND INSTALLE - [SDR AT9900473](https://openairdocs.org/sdr/AT9900473), May 7, 1999: SUBFLOOR. CORRODED. SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND CABIN ENTRY SUBFLOOR AT BS 160 TO 200 RBL 55 CORRODED. FABRICATED AND INSTALLED REPAIR IAW DC9 SRM 53-21-0, 5 - [SDR AT9900438](https://openairdocs.org/sdr/AT9900438), Apr 29, 1999: DOUBLER. CORRODED. SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND THE INTERNAL DOUBLER AT BS 580 STRINGER 30. REMOVED LEADING EDGE WING TO FUSELAGE FILLET PANELS, BLEED AIR DU - [SDR AT9900093](https://openairdocs.org/sdr/AT9900093), Feb 8, 1999: LIGHT. OUT OF POSITION. EMERGENCY FLOOR LIGHTING WILL NOT STAY ON. REPLACED FLOOR COVER AND WIRING SPLICES AT ROW NR 1. OPERATIONAL TEST NORMAL IAW MM 33-50. ## Other aircraft with N817AT - [Registered now](https://openairdocs.org/aircraft/N817AT): Piper PA-44-180, S/N 4496536, 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.