# N825AT: 1968 Douglas DC-9-32, registration cancelled 2003-01-29 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: January 29, 2003 - 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: 47319 - Year built: 1968 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: January 4, 1969 - Certificate issued: May 1, 1996 - Last registry action: January 21, 2003 - Mode S code: AB4380 - 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/N825AT - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=825AT - Page: https://openairdocs.org/deregistered/N825AT-2003-01-29 From the FAA registry file of October 28, 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 (41) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR AT0200007](https://openairdocs.org/sdr/AT0200007), Feb 7, 2002: SLIDE. OUT OF POSITION. GIRT BAR WOULD NOT LATCH AT R1 DOOR. REPOSITIONED SLIDE AT R1 DOOR. - [SDR AT0000485](https://openairdocs.org/sdr/AT0000485), Dec 6, 2000: REGULATOR. INOPERATIVE. PASSING THROUGH 260FL, FIRST OFFICER HEARD SURGE FROM PAX O2 SYSTEM. ALL MASKS DEPLOYED. CABIN ALTITUDE WAS AT 7000FT. REMOVED AND REPLACED PAX O2 CYLINDER REGU - [SDR AT0000471](https://openairdocs.org/sdr/AT0000471), Oct 25, 2000: DUCT. BLOWN. EXPERIENCED PRESSURIZATION PROBLEM. CABIN ALTITUDE COULD NOT BE CONTROLLED MANUALLY, O2 MASK DEPLOYED. RETURNED TO ATL. REMOVED AND REPLACED HOSE ASSEMBLY FOR L - [SDR AT0000448R1](https://openairdocs.org/sdr/AT0000448R1), Oct 21, 2000: SWITCH. INOPERATIVE. WHEN RIGHT LANDING LIGHT SWITCH WAS ACTIVATED FOR LANDING, SMOKE CAME FROM SWITCH. REMOVED VELCRO/ADHESIVE GLUE FROM BOTTOM OF LANDING LIGHT SWITCHES, REMOVED G - [SDR AT0000448](https://openairdocs.org/sdr/AT0000448), Oct 21, 2000: SWITCH. SHORTED. WHEN RIGHT LANDING LIGHT SWITCH ACTIVATED FOR LANDING, SMOKE CAME FROM SWITCH. COULD NOT DUPLICATE, PULLED CIRCUIT BREAKER AND COLLARED. - [SDR AT0000375](https://openairdocs.org/sdr/AT0000375), Aug 8, 2000: LIGHT. INOPERATIVE. FOUND AFT EMERGENCY LIGHTING AT AFT ENTRY DOOR WILL NOT ILLUMINATE. REPAIRED WIRE IN GROUND TO AFT EMERGENCY LIGHT IAW DC9 WDM 33-51. - [SDR AT0000305](https://openairdocs.org/sdr/AT0000305), Jun 5, 2000: DUCT. RUPTURED. ON CLIMBOUT, NR 1 ENGINE FIRE WARNING INDICATION SOUNDED, LIGHTS WENT OUT UPON POWER REDUCTION. REMOVED AND REPLACED RUPTURED FUEL HEAT DUCT IAW DC9 MM. - [SDR AT0000246](https://openairdocs.org/sdr/AT0000246), May 9, 2000: SKIN. LIGHTNING STRIKE. FOUND LIGHTNING STRIKE BLENDED BEYOND LIMITS AT RIGHT HAND WINDOW PANEL, BS 775 - 813. FABRICATED, DRILLED AND INSTALLED REPAIR DOUBLER IAW REO L00173. - [SDR AT0000244](https://openairdocs.org/sdr/AT0000244), May 9, 2000: STRUCTURE. MISREPAIRED. FOUND AFT CARGO CUT OUT LOWER SECTION HAS AN EXISTING REPAIR, NOT IAW DC9 SRM OR EO. REMOVED EXISTING REPAIR, FABRICATED AND INSTALLED PERMANENT REPAIR IAW TIMC - [SDR AT0000243](https://openairdocs.org/sdr/AT0000243), May 9, 2000: DOUBLER. CRACKED. FOUND TEMPORARY REPAIR CRACKED AT BS 945. FABRICATED AND INSTALLED PERMANENT PEPAIR IAW TIMCO REO L-00161. - [SDR AT0000270](https://openairdocs.org/sdr/AT0000270), May 8, 2000: SKIN. CORRODED. FOUND FORWARD CARGO COMPARTMENT SKIN UNDER NR 2 DME ANTENNA CORRODED AT BS 427. CUT OUT CORRODED SKIN, REMOVED 2 SPLICES, SHEAR TIES AND FLAPPER VALVE. FABRICAT - [SDR AT0000267](https://openairdocs.org/sdr/AT0000267), May 7, 2000: SKIN. LIGHTNING STRIKE. FOUND LIGHTNING STRIKE AT BS 317 AND BS 323. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW DC9 SRM 53-04 FIGURE 38 AND 12B. - [SDR AT0000266](https://openairdocs.org/sdr/AT0000266), May 2, 2000: SKIN. CRACKED. FOUND FORWARD CARGO COMPARTMENT LOWER AFT DOOR JAMB CORNER WAS CRACKED AT FASTENER HOLE. CUT OUT CRACKED AREA, INSTALLED FILLERS, DOUBLERS AND TRIPLER IAW TIMCO - [SDR AT0000242](https://openairdocs.org/sdr/AT0000242), May 2, 2000: ANGLE. WORN. FOUND BOTTON ANGLE LEFT AFT SIDE OF VERTICAL PANEL WORN BEYOND LIMITS. REMOVED AND REPLACED ANGLE IAW TIMCO SERVICE ORDER 151015-38274. - [SDR AT0000241](https://openairdocs.org/sdr/AT0000241), May 2, 2000: SKIN. GOUGED. FOUND TOP OF VERTICAL STAB PANEL DEEPLY GOUGED ALONG AFT LEFT SIDE, 2 EACH. REMOVED AND REPLACED SKIN IAW TIMCO SERVICE ORDER 151015-36905. - [SDR AT0000303](https://openairdocs.org/sdr/AT0000303), Apr 28, 2000: LONGERON. DAMAGED. FOUND EXISTING REPAIR OUTSIDE LIMITS AT BS 180 TO 207 L-20. REPAIRED TO CORRECT TOLORANCE IAW TIMCO REO L00162. - [SDR AT0000224](https://openairdocs.org/sdr/AT0000224), Apr 27, 2000: SKIN. CORRODED. FOUND CORROSION OF FUSELAGE SKIN OUT OF LIMITS. CUT OUT CORRODED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW SC9 SRM 53-04 FIGURE 38. - [SDR AT0000223](https://openairdocs.org/sdr/AT0000223), Apr 27, 2000: STOP. CRACKED. FOUND CRACK ON 4TH DOOR STOP AFT SIDE OF FORWARD PASSENGER DOOR. CUT OUT CRACK, FABRICATED FILLER DOUBLER AND TRIPLER AND INSTALLED REPAIR IAW EO 09-5310-29-E14 - [SDR AT0000222](https://openairdocs.org/sdr/AT0000222), Apr 21, 2000: SKIN. CRACKED. FOUND 2 CRACKS IN FUSELAGE AT BS 756 L1R. INSTALLED SKIN REPAIR IAW DC9 SRO DWG 9530129. - [SDR AT0000221](https://openairdocs.org/sdr/AT0000221), Apr 21, 2000: SKIN. CRACKED. FOUND CRACK IN FUSELAGE SKIN AT BS 737 L1 & 2R. INSTALLED SKIN REPAIR IAW SRO DWG 9530129. - [SDR AT0000269](https://openairdocs.org/sdr/AT0000269), Apr 18, 2000: BULKHEAD. CRACKED. FOUND BULKHEAD WEB AT BS 965 CRACKED. FABRICATED REPAIR WEB AND INSTALLED IAW EO 9-5310-29-E1466, REV A. - [SDR AT0000245](https://openairdocs.org/sdr/AT0000245), Apr 18, 2000: FRAME. CRACKED. FOUND FRAME AT BS 718 CRACKED. REMOVED FRAME, DRILLED NEW FRAME AND INSTALLED IAW EO 15-5311-29-B1044 OPTION 2, DC9 SRM 51-30-2, 51-30-5, 51-30-8 AND 53-05 FIGU - [SDR AT0000240](https://openairdocs.org/sdr/AT0000240), Apr 17, 2000: CAP. CRACKED. FOUND RIGHT WING AT BS 58.5 HAS CORROSION AND CRACK ON T-CAP BETWEEN STRINGER 15 AND 16. REMOVED CORROSION, DRILLED, SEALED, AND INSTALLED 6 REPAIR CLIPS IAW RE - [SDR AT0000302](https://openairdocs.org/sdr/AT0000302), Apr 16, 2000: ATTACH FITTING. GOUGED. FOUND RIGHT MLG ATTACH FITTING LUG FOR SIDE BRACE GOUGED. REPAIRED GOUGED RIGHT HAND MAIN LANDING GEAR FITTING ASSEMBLY LUG IAW TIMCO REO L00163. - [SDR AT0000220](https://openairdocs.org/sdr/AT0000220), Apr 15, 2000: LONGERON. CRACKED. FOUND LONGERON 6R WAS CRACKED AT BS 718. REMOVED SECTION OF CRACKED LONGERON, CUT DRILLED, TREATED, PRIMED AND INSTALLED SPLICES IAW DC9 SRM 53-02 FIGURE 18, 51 - [SDR AT0000268](https://openairdocs.org/sdr/AT0000268), Apr 14, 2000: SKIN. CORRODED. FOUND SKIN BELOW LEFT AFT LAVATORY SERVICE PANEL BLENDED BEYOND LIMITS. CUT OUT BLENDED AREA OF SKIN BELOW LAVATORY SERVICE PANEL, FABRICATED SKIN FILLER AND EX - [SDR AT0000250](https://openairdocs.org/sdr/AT0000250), Apr 13, 2000: SKIN. LIGHTNING STRIKE. FOUND LIGHTNING STRIKE AT BS 165 LONGERON 29 - 30R. FABRICATED, DRILLED, COUNTERSUNK, REPAIR DOUBLER AND FILLER. INSTALLED DOUBLER AND FILLER IAW TIMCO REO L001 - [SDR AT0000149](https://openairdocs.org/sdr/AT0000149), Mar 22, 2000: LIGHT. INOPERATIVE. FOUND TAILCONE EMERGENCY FLOOD LIGHT WILL NOT ILLUMINATE. CORRECTIVE ACTION: RELAMPED, IAW DC9 MM 33-50 - [SDR AT0000086](https://openairdocs.org/sdr/AT0000086), Feb 6, 2000: LANYARD. DISENGAGED. FOUND ON TAXI OUT, R1 DOOR SLIDE LANYARD FELL OUT. STRAIGHTENED ARM AND ATTACHED PACK, REATTACHED PIN IAW DC9 MM 25-62-00. - [SDR AT9900378](https://openairdocs.org/sdr/AT9900378), May 16, 1999: BATTERIES. DISCHARGED. FOUND BOTH AFT OVERHEAD EXIT EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERIES IAW MM 33-53-0. - [SDR AT9900377](https://openairdocs.org/sdr/AT9900377), May 16, 1999: BATTERY. DISCHARGED. THREE OVERHEAD EMEGENCY LIGHTS INOPERATIVE, TWO IN ROW 20 AND ONE IN BETWEEN ROWS 19 AND 20. REMOVED AND REPLACED BATTERIES IAW MM 33-53-0. - [SDR AT9900139](https://openairdocs.org/sdr/AT9900139), Feb 12, 1999: FLOORBEAM. CORRODED. SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE FLOORBEAM AT STA 965 HAS CORROSION AND BLUE WATER STAINS ON LOWER LEG AND AROUND NUT PLATES HOLES LEFT HAND LAV - [SDR AT9900116](https://openairdocs.org/sdr/AT9900116), Feb 11, 1999: SKIN. DENTED. SCHEDULED INSPECTION AT AERO CORP, FL, FOUND THE LOWER RIGHT FUSELAGE SKIN FROM STA 389 TO STA 598 L-18R TO L-26R WITH DENTS IN DIFFERENT AREAS. REMOVED AND REP - [SDR AT9900143](https://openairdocs.org/sdr/AT9900143), Jan 22, 1999: FLOOR TRACK. CORRODED. SCHEDULED INSPECTION AT AERO CORP, FL. FOUND FLOOR TRACKS AT THE AFT PIT STA 756 TO 780 AND ON THE RIGHT LOWER SIDE AT STA 935 TO 996 WITH CORROSION. MECHANICAL - [SDR AT9900144](https://openairdocs.org/sdr/AT9900144), Jan 14, 1999: BRACKET. CORRODED. SCHEDULED INSPECTION AT AERO CORP, FL. FOUND VARIOUS LOCATION WITH CORROSION. FIRST, THE CABIN FLOOR PANEL NR 89 ON THE UNDER SIDE AT FORWARD END. SECONDLY, THE - [SDR AT9900130](https://openairdocs.org/sdr/AT9900130), Jan 14, 1999: STRUCTURE. CORRODED. SCHEDULED INSPECTION AT AERO CORP, FL. FOUND VARIOUS LOCATIONS WITH CORROSION. FIRST, AT STA 602 LONGERON L-29L. SECONDLY, THE AFT PIT FORWARD SIDE AT STA 382 B - [SDR AT9900259](https://openairdocs.org/sdr/AT9900259), Jan 13, 1999: FAIRING. DELAMINATED. SCHEDULED INSPECTION AT AERO CORP, FL. FOUND DELAMINATION ON INBOARD AND OUTBOARD SIDES OF LEFT HAND UPPER HORIZONTAL STABILIZER FAIRING. REMOVED INNER SKIN AND - [SDR AT9900146](https://openairdocs.org/sdr/AT9900146), Jan 13, 1999: SUPPORT. CRACKED. SCHEDULED INSPECTION AT AERO CORP, FL. FOUND VARIOUS FLOOR FRAME AT DIFFERENT LOCATIONS CRACKED. FIRST, THE FORWARD CARGO FLOOR FRAME SCREW HOLE CRACKED/ELONGAT - [SDR AT9900137](https://openairdocs.org/sdr/AT9900137), Jan 13, 1999: LONGERON. DENTED. SCHEDULED INSPECTION AT AERO CORP, FL. FOUND A DENT OUT OF LIMITS AT STA 361R L-28R. REMOVED FASTENERS, COLD WORKED DENT, HFCE INSPECTED DENT WITH NO CRACKS NOT - [SDR AT9900145](https://openairdocs.org/sdr/AT9900145), Jan 12, 1999: SUPPORT. CORRODED. SCHEDULED INSPECTION AT AERO CORP, FL. FOUND VARIOUS LOCATION CORRODED AND CRACKED. FIRST, THE AFT PIT LOWER SIDE WALL TIEDOWNS COVER ON THE LOWER SIDE. SECONDL - [SDR AT9900140](https://openairdocs.org/sdr/AT9900140), Jan 12, 1999: FAIRING. CRACKED. SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE NR 2 AFT INBOARD UPPER THRUST REVERSER ACTUATOR FAIRING IS CRACKED. REMOVED THE THRUST REVERSER FAIRING, WELDED ## Other aircraft with N825AT - [Registered now](https://openairdocs.org/aircraft/N825AT): Costruzioni Aeronautiche Tecna P2004 BRAVO, S/N 084, built 2006 --- 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.