# N925TW: 1986 Mcdonnell Douglas DC-9-82(MD-82), registration cancelled 2007-05-10 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: May 10, 2007 - Status when cancelled: Valid registration - Airframe: [Mcdonnell Douglas DC-9-82(MD-82)](https://openairdocs.org/model/mcdonnell-douglas-dc-9-82-md-82) (registry code 3022082) - Engine: [Pratt & Whitney JT8D series](https://openairdocs.org/engine/pratt-whitney-jt8d-series) (registry code 52053) - Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE) (OpenAirDocs) - Serial number: 49357 - Year built: 1986 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: August 15, 1997 - Certificate issued: September 23, 2004 - Last registry action: September 23, 2004 - Mode S code: ACD27B - Owner when cancelled: [American Airlines Inc](https://openairdocs.org/faa-owner/AMERICAN%20AIRLINES%20INC) - Location: [Fort Worth, TX](https://openairdocs.org/faa-place/TX/Fort%20Worth) - Owner type: Corporation - Owner's area on the map: 32.8240° N, 97.0491° W: Placed by OpenAirDocs at the center of ZIP code 76155, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N925TW - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=925TW - Page: https://openairdocs.org/deregistered/N925TW-2007-05-10 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 Mcdonnell Douglas DC-9-82(MD-82): https://openairdocs.org/model/mcdonnell-douglas-dc-9-82-md-82.md ## Service difficulty reports (21) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR ZW0A0303907](https://openairdocs.org/sdr/ZW0A0303907), Apr 2, 2003: SKIN. DAMAGED. THE FUSELAGE SKIN WAS DAMAGED AT STA 596 TO 605, LONGERON 26R AREA. SPLICED IN NEW SECTION OF SKIN PER SRM 53-04, FIG 12C, AND ARA 18438A, REPAIR AREA NUMBER 3. - [SDR ZW0A0303906](https://openairdocs.org/sdr/ZW0A0303906), Apr 2, 2003: SKIN. DAMAGED. THE FUSELAGE SKIN WAS DAMAGED AT STA 601 TO 604, ABOVE LONGERON 26R, 3.25 INCHES BY 2.625 INCH AND 0.070 DEEP. SPLICED IN NEW SECTION OF SKIN PER SRM 53-04, FIG - [SDR ZW0A0303908](https://openairdocs.org/sdr/ZW0A0303908), Apr 2, 2003: SKIN. DAMAGED. THE FUSELAGE SKIN WAS DAMAGED AT STA 591 TO 596, BELOW LONGERON 26R, 6 INCHES BY 5 INCHES AND 0.074 DEEP. SPLICED IN NEW SECTION OF SKIN PER SRM 53-04, FIG 12C, - [SDR ZW0A0303905](https://openairdocs.org/sdr/ZW0A0303905), Apr 2, 2003: SKIN. DAMAGED. THE FUSELAGE SKIN WAS DAMAGED AT STA 588 TO 555, LONGERON 26R TO 26L. SPLICED IN NEW SECTION OF SKIN PER SRM 53-04, FIG 12C, AND ARA 18438A, REPAIR AREA NUMBER - [SDR ZW0A0303904](https://openairdocs.org/sdr/ZW0A0303904), Apr 2, 2003: SKIN. DAMAGED. THE FUSELAGE SKIN WAS DAMAGED AT STA 586 TO 603, LONGERON 26R TO 27R. SPLICED IN A NEW SECTION OF SKIN PER SRM 53-04, FIG 12C, AND ARA 18438A, REPAIR AREA NUMBE - [SDR ZW0A0303903](https://openairdocs.org/sdr/ZW0A0303903), Apr 2, 2003: SKIN. DAMAGED. THE FUSELAGE SKIN WAS DAMAGED AT STA 586 TO 598, LONGERON 25R TO 26R. REPAIRED PER SRM 53-04, FIG 12C, AND AREA NUMBER 1 ON ARA 18438A. CHECK-C 8-15-02 STL. - [SDR ZW0A0303902](https://openairdocs.org/sdr/ZW0A0303902), Apr 2, 2003: SKIN. DAMAGED. THE FUSELAGE SKIN WAS DAMAGED AT STA 576 TO 579, ABOVE LONGERON 26R, 3.75 INCHES BY 3.75 INCHES AND 0.056 IN DEEP. SPLICED IN NEW SECTION OF SKIN PER SRM 53-04, - [SDR ZW0A0301801](https://openairdocs.org/sdr/ZW0A0301801), Feb 8, 2003: POWER SUPPLY. DISCHARGED. THE TAIL CONE EMERGENCY LIGHT WAS INOPERATIVE. REPLACED THE POWER SUPPLY. - [SDR ZW0A0210101](https://openairdocs.org/sdr/ZW0A0210101), Sep 26, 2002: POWER SUPPLY. DISCHARGED. THE EMERGENCY ESCAPE PATH LIGHTING ILLUMINATED DURING FLIGHT IN FIRST CLASS CABIN. REPLACED EGRESS POWER SUPPLY NUMBER 2 AT ROWS 7 AND 8. - [SDR ZW0A0210001](https://openairdocs.org/sdr/ZW0A0210001), Sep 25, 2002: POWER SUPPLY. DISCHARGED. THE ESCAPE PATH LIGHTING IN THE FIRST CLASS SECTION CAME ON IN FLIGHT AND STAYED ON WITH SWITCH IN ARM POSITION. REPLACED THE POWER SUPPLY FOR FIRST CLASS. - [SDR ZW0A0106503](https://openairdocs.org/sdr/ZW0A0106503), Aug 8, 2001: POWER SUPPLY. THE EGRESS LIGHT STRIP ROWS 7 TO 14 CAME ON INTERMITTENTLY. REPLACED THE POWER SUPPLY. CHECK-C 7-29-01 STL. --CLOSED-- - [SDR ZW0A0106502](https://openairdocs.org/sdr/ZW0A0106502), Aug 8, 2001: LIGHT. INTERMITTENT. THE EGRESS LIGHTS ROWS 7 TO 14 CAME ON INTERMITTENTLY. OPERATIONAL TEST NORMAL. - [SDR ZW0A0106501](https://openairdocs.org/sdr/ZW0A0106501), Aug 7, 2001: BATTERY PACK. THE CENTER SECTION OF EGRESS LIGHTS ILLUMINATED WITH THE SWITCH IN EITHER ARMED OR ON POSITION. REPLACED THE BATTERY PACK. CHECK-C 7-29-01 STL. --CLOSED-- - [SDR TWAA0104101](https://openairdocs.org/sdr/TWAA0104101), Mar 3, 2001: POWER SUPPLY. MALFUNCTIONED. THE EGRESS LIGHTS AT ROWS 16 TO 23 CAME ON IN FLIGHT. REPLACED THE POWER SUPPLY. CHECK-C 11-2-00 MCI. - [SDR TWAA0017510](https://openairdocs.org/sdr/TWAA0017510), Oct 1, 2000: PANEL. DELAMINATED. DURING CHECK-C MAINT, THE LT WING UPPER OUTBOARD PANEL FWD OF GROUND SPOILER HAD DELAMINATION ABOUT 11 RIVETS AT OUTBOARD EDGE. REPLACED PANEL PER SRM 6-70-01. - [SDR TWAA0011801](https://openairdocs.org/sdr/TWAA0011801), Jul 24, 2000: RIB. CRACKED. THE RT WING NUMBER 4 SLAT O/B NUMBER 12 SLAT RIB WAS CRACKED. REPLACED THE SLAT PER M99-27-02. CHECKK-C 8-21-99 STL. - [SDR TWAA9914707](https://openairdocs.org/sdr/TWAA9914707), Oct 30, 1999: SPLICE. CRACKED. DURING LS, FOUND STATION 240 LONGERON L19 SPLICE IS CRACKED. INSTALLED NEW SPLICE IN ACCORDANCE WITH SRM 53-02 FIG 18. - [SDR TWAA9908003](https://openairdocs.org/sdr/TWAA9908003), Jun 5, 1999: TURBINE. DAMAGED. THE RT ENGINE SHUT ITSELF DOWN WHILE EGT INDICATION INCREASED. CREW ACCOMPLISHED THE ENGINE SHUT DOWN PROCEDURE AND MADE UNSCHEDULED LANDING AT IND. FOUND TURBI - [SDR TWAA9816801](https://openairdocs.org/sdr/TWAA9816801), Oct 19, 1998: DEFLECTOR. OUT OF POSITION. NOSE GEAR FAILED TO RETRACT ON TAKEOFF. RECYCLED GEAR ONCE NO HELP. RETURNED TO STL. FOUND SOME HARDWARE MISSING FROM THE NLG SPRAY DEFLECTOR, ALLOWING THE DEFL - [SDR TWAA9801406](https://openairdocs.org/sdr/TWAA9801406), Jan 26, 1998: GYRO. WORN. STL - FLT 455 - STARTING DESCENT INTO OMA, BOTH FLIGHT DIRECTORS FAILED. RETURNED TO FLIGHT ORIGINATION STATION, STL. REPLACED NR 1 VERTICAL GYRO. CHECK-C, 8-17 - [SDR TWAA9715401](https://openairdocs.org/sdr/TWAA9715401), Dec 30, 1997: DOOR. NOT CLOSED. STL - FLT 468 - AFTER TAKEOFF DURING CLIMB, AIRCRAFT WOULD NOT PRESSURIZE. FOUND MID-CARGO BEARER PIN HOLDING DOOR OPEN. REMOVED PIN AND SECURED DOOR. 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