# N929TW: 1981 Mcdonnell Douglas DC-9-82(MD-82), registration cancelled 2013-06-27 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: June 27, 2013 - Status when cancelled: Sale reported, canceled - 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: 48014 - Year built: 1981 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: March 5, 1998 - Last registry action: May 31, 2006 - Mode S code: ACE157 - Location: [Kansas City, KS](https://openairdocs.org/faa-place/KS/Kansas%20City) - Owner type: Individual - Owner's area on the map: 39.1483° N, 94.6051° W: Placed by OpenAirDocs at the center of ZIP code 66115, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N929TW - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=929TW - Page: https://openairdocs.org/deregistered/N929TW-2013-06-27 From the FAA registry file of November 5, 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 (33) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR ZW0A0213101](https://openairdocs.org/sdr/ZW0A0213101), Dec 30, 2002: LAMP. THE EMERGENCY LIGHT IN THE TAIL COMPARTMENT WAS INOPERATIVE. REPLACED THE LAMP. CHECK-C 2-8-02 STL. --CLOSED-- - [SDR ZW0A0205603](https://openairdocs.org/sdr/ZW0A0205603), May 29, 2002: ACCELEROMETER. MALFUNCTIONED. AFTER TAKEOFF YAW DAMPER OFF LT-YAW KICKS LT-RT UNSKD LANDING AFTER UNCOMMANDED RUDDER INPUT. REMOVED AND REPLACED ACCELEROMETER PER MM 22-19-01 PG 201. ACCOMPL - [SDR ZW0A0104703](https://openairdocs.org/sdr/ZW0A0104703), Jul 2, 2001: WEDGE. DAMAGED. DURING CHECK-C MAINT THE RT WING T/E FLAP T/E WEDGE WAS DAMAGED ON THE BOTTOM SIDE APPROX 6 FT INBD OF THE OTBD END. REMOVED AND REPLACED THE OTBD 13 .75 OF TRA - [SDR ZW0A0103901](https://openairdocs.org/sdr/ZW0A0103901), Jun 19, 2001: FRAME. CRACKED. DURING CHECK-C MAINT FOUND AT CANTED FRAME NUMBER 1497, 11 O'CLOCK POSITION A DOUBLE ROW OF HI-LOKS WERE CRACKED OUT. INSTALLED WEB REPAIR PER SRM 51-70-11 AND - [SDR ZW0A0103709](https://openairdocs.org/sdr/ZW0A0103709), Jun 14, 2001: FLOOR SUPPORT. CORRODED. DURING CHECK-C MAINT FOUND CABIN FLOOR SUPPORT CRACKED AT STA 1098, BETWEEN LONGERON 26R AND 25R. FLOOR SUPPORT WAS REMOVED AND SENT TO SHOP TO BE WELDED PER SS - [SDR ZW0A0103708](https://openairdocs.org/sdr/ZW0A0103708), Jun 14, 2001: FLOOR SUPPORT. CORRODED. DURING CHECK-C MAINT FOUND CORROSION ON CABIN FLOOR SUPPORT AT STA 183, LBL 44. FLOOR SUPPORT REMOVED AND NEW SUPPORT FABRICATED AND INSTALLED PER SPM 6-70-1 AN - [SDR ZW0A0103707](https://openairdocs.org/sdr/ZW0A0103707), Jun 13, 2001: WEB. CORRODED. DURING CHECK-C MAINT IN FWD CABIN FOUND CORROSION ON MEMBRANE AT STA 197 TO 200, UNDER FWD EDGE OF NUMBER 1 CHAIR TRACK. INSTALLED REPAIR PER SRM 51-70-4 ON MEM - [SDR ZW0A0103706](https://openairdocs.org/sdr/ZW0A0103706), Jun 13, 2001: PANEL. DENTED. DURING CHECK-C MAINT ON LT WING FOUND NUMEROUS DENTS ON TRAILING EDGE PANEL IN FRONT OF AILERON. INSTALLED NEW PANEL P/N 5812737-501 PER SPM 6-70-01. INSTALLED - [SDR ZW0A0103705](https://openairdocs.org/sdr/ZW0A0103705), Jun 13, 2001: FLOORBEAM. GOUGED. DURING CHECK-C MAINT A GOUGE WAS FOUND IN THE BOTTOM FLANGE OF THE CABIN FLOORBEAM, STA 408, RBL 2 INCH. BLENDED GOUGE IN BOTTOM FLANGE OF CABIN FLOORBEAM, STA - [SDR ZW0A0103703](https://openairdocs.org/sdr/ZW0A0103703), Jun 12, 2001: BULKHEAD. CRACKED. DURING CHECK-C MAINT IN AFT ACCY COMPT FOUND CRACKED WEB APPROX 2 INCHES ON STA 1485 CANTED BULKHEAD, APPROX 10 O'CLOCK POSITION. STOP DRILLED CRACK. REPAIRED W - [SDR ZW0A0103704](https://openairdocs.org/sdr/ZW0A0103704), Jun 12, 2001: FRAME. CRACKED. DURING CHECK-C MAINT FOUND CANTED FRAME AT STA 1463, 2 O'CLOCK POSITION, WAS CRACKED AT HI-LOKS. REPAIRED PER SRM 53-01, FIG 2 SHEET 3. - [SDR ZW0A0103403](https://openairdocs.org/sdr/ZW0A0103403), Jun 8, 2001: FITTING. CRACKED. DURING CHECK-C MAINT THE FWD CARGO DOOR T-ANGLE WAS CRACKED APPROX 16 INCHES FWD OF AFT END AT TOP OF DOOR. REPLACED CRACKED FITTING PER SRM 51-01, PAGE 1, ITEM - [SDR ZW0A0103402](https://openairdocs.org/sdr/ZW0A0103402), Jun 8, 2001: WEB. CRACKED. DURING CHECK-C MAINT FOUND A CRACK IN MEMBRANE AT LONGERON 18R, STA 1302. REMOVED DAMAGED AREA AND REPAIRED PER SRM 53-01 AND 51-30-2. - [SDR ZW0A0103505](https://openairdocs.org/sdr/ZW0A0103505), Jun 7, 2001: LONGERON. CRACKED. DURING CHECK-C MAINT FOUND LONGERON 17L CRACKED AT EACH HI-LOK TO FORMER 217, AT BOTH ATTACH POINTS TO FORMER 313, AT ATTACH POINT TO FORMER STA 256, AT BOTTOM - [SDR ZW0A0103504](https://openairdocs.org/sdr/ZW0A0103504), Jun 7, 2001: FLOORBEAM. CORRODED. DURING CHECK-C MAINT FOUND CORROSION ON CABIN FLOORBEAM, STA 218 CENTERLINE. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-01 PAGE 1. - [SDR ZW0A0103503](https://openairdocs.org/sdr/ZW0A0103503), Jun 7, 2001: FLOOR SUPPORT. CORRODED. DURING CHECK-C MAINT FOUND CABIN FLOOR SUPPORT HAD CORROSION AT STA 180, RBL 9 TO 43. REPLACED SUPPORT PER SPM 6-70-01, PAGE 3 PARAGRAPH 4. - [SDR ZW0A0103006](https://openairdocs.org/sdr/ZW0A0103006), Jun 5, 2001: ANGLE. CORRODED. DURING CHECK-C MAINT FOUND ANGLE CORRODED AT STA 1155, LONGERON 29R TO 28R, AND AT STA 1212, STRINGER 29R TO 28R. REMOVED CORRODED ANGLES AND REPLACED WITH NEW. - [SDR ZW0A0103005](https://openairdocs.org/sdr/ZW0A0103005), Jun 5, 2001: BRACKET. CRACKED. DURING CHECK-C MAINT IN THE FWD CARGO COMPT FOUND CRACK IN TRACK TO FORMER BRACKET, STA 237, FWD SIDE, BETWEEN LONGERON 27 AND 28L, AND BETWEEN LONGERON 27 AND - [SDR ZW0A0103004](https://openairdocs.org/sdr/ZW0A0103004), Jun 4, 2001: BULKHEAD. WORN. DURING CHECK-C MAINT FOUND WORN AREA ON STRINGER 1380, BULKHEAD, UPPER LT SIDE, FWD FACE APPROX 11 O'CLOCK. INSTALLED 0.050 DOUBLER OVER RUB AREA PER SRM 53-01. - [SDR ZW0A0103001](https://openairdocs.org/sdr/ZW0A0103001), May 31, 2001: DOUBLER. CRACKED. DURING CHECK-C MAINT FOUND OLD REPAIR ON MEMBRANE HAD CRACKED, STA 905 TO 927, LONGERON 18R. REPLACED DOUBLER PER SRM 53-01, PAGE 9. - [SDR ZW0A0102515](https://openairdocs.org/sdr/ZW0A0102515), May 31, 2001: SUPPORT. CORRODED. DURING CHECK-C MAINT FOUND CORROSION ON AFT GALLEY GIRT BAR SUPPORTS. REMOVED CORROSION ON FWD GIRT BAR SUPPORT PER SPM 6-80-01, PAGE 2. REPLACED AFT GIRT BAR S - [SDR ZW0A0102514](https://openairdocs.org/sdr/ZW0A0102514), May 30, 2001: RIVET. CRACKED. DURING CHECK-C MAINT ON THE INBD LT ELEVATOR, FWD OF INBD MOUNT, HAD A METAL PLATE WITH RIVET CRACKED OUT. REPLACED METAL PLATE PER SRM 55-20-0 AND 51-30-02. - [SDR TWAA0105701](https://openairdocs.org/sdr/TWAA0105701), Mar 28, 2001: POWER SUPPLY. DISCHARGED. THE EGRESS LIGHTS BEHIND ROW 29 WERE FLASHING. REPLACED THE POWER SUPPLY. CHECK-C 3-30-00 STL. - [SDR TWAA0104401](https://openairdocs.org/sdr/TWAA0104401), Mar 7, 2001: LIGHT. INTERMITTENT. THE EMERGENCY EXIT LIGHTS AT THE REAR OF THE AIRCRAFT WERE REPORTED TO FLICKER IN FLIGHT. MAINTENANCE FOUND THE EMERGENCY LIGHTS OPERATED NORMALLY PER MAINT MAN - [SDR TWAA0101003](https://openairdocs.org/sdr/TWAA0101003), Jan 16, 2001: BATTERY. DISCHARGED. THE FIRST CLASS OVERHEAD EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED THE POWER SUPPLY IN NUMBER 3 POSITION (P/N 60-0304-516B), AND REPLACED BATTERIES IN NUMBER - [SDR TWAA0100903](https://openairdocs.org/sdr/TWAA0100903), Jan 13, 2001: BATTERY. OVERHEATED. WHILE AT THE GATE SMOKE WAS SEEN COMING FROM THE ELECTRONIC COMPARTMENT. SHIPS BATTERY WAS HOT TO TOUCH AND EVENTUALLY SPARKING. AMPS WERE CHARGING THEN DISCHAR - [SDR TWAA0014001](https://openairdocs.org/sdr/TWAA0014001), Sep 8, 2000: TRANSCEIVER. SHORTED. ON PREFLIGHT, CREW NOTICED NUMBER 3 VHF CIRCUIT BREAKER TRIPPED. RESET CB AND A STRONG ELECTRICAL BURNING SMELL WAS NOTICED. PULLED CB E-24 AND SMELL WENT AWAY. - [SDR TWAA0012301](https://openairdocs.org/sdr/TWAA0012301), Aug 2, 2000: BATTERY. DISCHARGED. BOTH COCKPIT EMERGENCY LIGHTS FAILED TO ILLUMINATE WHEN EMERGENCY LIGHTS WERE SWITCHED ON. REPLACED THE BATTERIES IN THE POWER SUPPLY. CHECK-C 3-30-00 STL. - [SDR TWAA0009502](https://openairdocs.org/sdr/TWAA0009502), Jun 14, 2000: BATTERY PACK. INOPERATIVE. DURING ROUTINE INSPECTION, FOUND LEFT AND RIGHT AFT OVERWING EGRESS LIGHTS AND EXIT LIGHTS INOP. REPLACED BATTERY PACK. AC05 04-01-00 JFK. - [SDR TWAA0005104](https://openairdocs.org/sdr/TWAA0005104), Apr 2, 2000: BATTERY PACK. WORN. THE AFT CABIN EGRESS LIGHTS FROM THE AFT GALLEY TO REAR OF THE AIRCRAFT INTERMITTENTLY ILLUMINATED DURING FLIGHT. REPLACED BATTERY PACK AT ROW 29. CHECK-C 3-17- - [SDR TWAA0005103](https://openairdocs.org/sdr/TWAA0005103), Apr 1, 2000: BATTERY PACK. INOPERATIVE. THE AFT CABIN EGRESS LIGHTS WERE ILLUMINATING. REPLACED THE BATTERY PACK AT ROW 23. CHECK-C 3-17-00 STL. - [SDR TWAA9814801](https://openairdocs.org/sdr/TWAA9814801), Sep 14, 1998: GENERATOR. FAILED. AIRCRAFT WAS DISPATCHED WITH THE RT ENG GENERATOR INOPERATIVE PER MEL. AT FL310, THE APU SHUT DOWN. APU RESTARTED AT FL 240. ELECTED TO DIVERT TO MCI. THE RT EN - [SDR TWAA9806102](https://openairdocs.org/sdr/TWAA9806102), Feb 19, 1998: SOCKET. CRACKED. MCI - DURING MODIFICATION VISIT, FOUND LT FORWARD OVERWING EXIT FORWARD LOCK PIN SOCKET CRACKED ON THE LOWER OVERWING EXIT FRAME. REPAIRED PER SRM 53-05, FIG 32 ## 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 20020827028019I](https://openairdocs.org/incident/20020827028019I), Aug 27, 2002: Doug DC982 (N929TW), St Louis, MO. (-23) Aircraft N929TW during takeoff out of st. Louis, Missouri had #2 engine turbine failure. Maintenance removed and replaced the #2 engine. --- 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.