# N919TW: 1985 Mcdonnell Douglas DC-9-82(MD-82), registration cancelled 2012-02-28 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: February 28, 2012 - 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: 49368 - Year built: 1985 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: April 26, 1985 - Last registry action: February 28, 2012 - Mode S code: ACB9D8 - Owner when cancelled: [Stewart Industries International LLC](https://openairdocs.org/faa-owner/STEWART%20INDUSTRIES%20INTERNATIONAL%20LLC) - Location: [Guthrie, OK](https://openairdocs.org/faa-place/OK/Guthrie) - Owner type: Corporation - Owner's area on the map: 35.8679° N, 97.4344° W: Placed by OpenAirDocs at the center of ZIP code 73044, within about 9 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N919TW - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=919TW - Page: https://openairdocs.org/deregistered/N919TW-2012-02-28 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 Mcdonnell Douglas DC-9-82(MD-82): https://openairdocs.org/model/mcdonnell-douglas-dc-9-82-md-82.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 AALA20060106](https://openairdocs.org/sdr/AALA20060106), Feb 19, 2006: SWITCH. INOPERATIVE. SMOKE IN CAB IN AND COCKPIT. SOURCE UNDETERMINED. LANDED STL WITHOUT INCIDENT. REPLACED LEFT PACK 130 DEGREE TEMPERATURE LIMIT SWITCH AND BOTH WATER SEPARATORS. - [SDR ZW0A0305101](https://openairdocs.org/sdr/ZW0A0305101), May 25, 2003: BATTERY. INOPERATIVE. THE EGRESS LIGHTS AT THE OVERWING EMERGENCY EXITS, CAME ON IN FLIGHT WITH THE SWITCH IN ARM POSITION. REPLACED THE BATTERIES IN THE BATTERY PACK. CHECK-C 3-28-0 - [SDR TWAA0102005](https://openairdocs.org/sdr/TWAA0102005), Jan 31, 2001: GENERATOR. MALFUNCTIONED. AT FL 330 CAPT INSTRUMENTS WENT DEAD AND FLT GUIDANCE CONTROL PANEL FROZE. LT AND RT GEN VOLTS AND FREQS NORMAL. MADE UNSCHEDULED LANDING AT TPA. AFTER LANDING - [SDR TWAA0100302](https://openairdocs.org/sdr/TWAA0100302), Jan 3, 2001: SMOKE. DETECTED. ON SHORT FINAL SMOKE APPEARED IN THE CABIN WHEN ANTI-ICE WAS TURNED ON. ACCOMPLISHED PACK BURN OUT AND DEACTIVATED APU PER MEL. CHECK-C 5-12-00 MCI. - [SDR TWAA0008204](https://openairdocs.org/sdr/TWAA0008204), May 22, 2000: MOTOR. DAMAGED. DURING DESCENT HAD A CABIN PRESSURIZATION PROBLEM. PASSENGER OXYGEN MASKS DROPPED. FERRY TO MCI FOR CORRECTIONS. AC04 01-28-00 DFW. REPLACED THE OUTFLOW VALVE M - [SDR TWAA0007205](https://openairdocs.org/sdr/TWAA0007205), May 2, 2000: INTERCOSTAL. CORRODED. DURING CHECK-C MAINT INTERCOSTAL AT RBL 16 BETWEEN STA 1307 AND 1323, HAD CORROSION AT BOTH ENDS. REMOVED AND REPLACED INTERCOSTAL AT STA 1322, RBL 15. INSTALLE - [SDR TWAA0007204](https://openairdocs.org/sdr/TWAA0007204), May 2, 2000: FRAME. CORRODED. DURING CHECK-C MAINT, FOUND FORMER FOOT CORRODED AT STA 1287, AT LONGERON 20L. REMOVED CORROSION PER SPM 6-80-01. - [SDR TWAA0006913](https://openairdocs.org/sdr/TWAA0006913), May 1, 2000: FRAME. CORRODED. DURING CHECK-C MAINT, FOUND CORROSION ON LOWER FLANGE OF FORMER STA 1307, LONGERON 25L TO 28R. SPLICED IN NEW FORMER PER DOUGLAS DRAWING 9912243 AND SRO 9530057 - [SDR TWAA0008307](https://openairdocs.org/sdr/TWAA0008307), Apr 27, 2000: OUTFLOW VALVE. CORRODED. DURING CC24C, FOUND INTERGRANULAR CORROSION ON THE OUTFLOW VALVE CASTING (SUGAR SCOOP) LOWER AFT SIDE. REPLACED DOUBLER MANUFACTURE NUMBER 5914558-5012 VING TWA - [SDR TWAA0007003](https://openairdocs.org/sdr/TWAA0007003), Apr 27, 2000: CARGO TRACK. CORRODED. DURING CHECK-C MAINT, THE RT AFT CARGO COMPT TIE DOWN TRACK HAD NUMEROUS PLACES OF CORROSION AT TOP AND BOTTOM OF CLIP NUT LOCATIONS FROM STA 1212 TO 1320. REMO - [SDR TWAA0006609](https://openairdocs.org/sdr/TWAA0006609), Apr 24, 2000: FRAME. CORRODED. DURING CHECK-C MAINT, FOUND CORROSION IN LOWER FLANGE OF FORMER 1271, BETWEEN LONGERON 28L AND 30. REMOVED CORROSION PER SRM 53-10-03. REPAIRED PER SRM 53-03, P - [SDR TWAA0006309](https://openairdocs.org/sdr/TWAA0006309), Apr 23, 2000: FLOOR SUPPORT. CORRODED. DURING CHECK-C MAINT, FOUND CORROSION BEYOND LIMITS ON FLOOR SUPPORT STA 1322, LONGERON 23R TO 23L. FABRICATED NEW FLOOR SUPPORTS FROM 0.040 2024 PER SPM 6-70-0 - [SDR TWAA0006308](https://openairdocs.org/sdr/TWAA0006308), Apr 21, 2000: SKIN. DAMAGED. DURING CHECK-C MAINT, THE FWD LT PAX DOOR SKIN ALONG THE BOTTOM EDGE WAS DISTORTED. REPAIRED SKIN ALONG BOTTOM EDGE BY STRENGHTENING AND REPAIRED PER SRM 52-05, - [SDR TWAA0006307](https://openairdocs.org/sdr/TWAA0006307), Apr 20, 2000: CASTING. CRACKED. DURING CHECK-C MAINT, THE LT WING FWD END OF GROUND SPOILER ATTACH CASTING WAS CRACKED BOTH I/B AND O/B SIDE OF ACT ATTACH FWD END. STOP DRILLED CRACKS PER SRO - [SDR TWAA0006306](https://openairdocs.org/sdr/TWAA0006306), Apr 20, 2000: ACTUATOR. CRACKED. DURING CHECK-C MAINT, THE RT WING FWD END OF GROUND SPOILER ACTUATOR ATTACH CASTING WAS CRACKED I/B AND O/B SIDE AT FWD END, PER BOEING DAC SB 57-180 VIEW DD CO - [SDR TWAA0006305](https://openairdocs.org/sdr/TWAA0006305), Apr 19, 2000: STRUCTURE. BENT. DURING CHECK-C MAINT, THE FWD ENTRY DOOR WAS BENT AT THE BOTTOM FWD AND AFT ENDS. REPAIRED SKIN PER SRM 52-05 PAGE 32, AND 52-03 PAGE 1. - [SDR TWAA0006304](https://openairdocs.org/sdr/TWAA0006304), Apr 18, 2000: DOME NUT. CORRODED. DURING CHECK-C MAINT, FOUND RT FUSELAGE CORROSION AROUND DOME NUT HOLES AT STA 769 TO 807, AREA OF LONGERON 28R. REMOVED CORROSION PER SPM 6-80-01. CHECKED MATE - [SDR TWAA0006303](https://openairdocs.org/sdr/TWAA0006303), Apr 18, 2000: SEAT TRACK. CORRODED. DURING CHECK-C MAINT, THE RT CHAIR TRACK HAD CORROSION FROM STA 1079 TO 1155, WL 200. REMOVED CORRODED TRACK AND INSTALLED NEW TRACK USING SCREWS NAS 7103, WASH - [SDR TWAA0006005](https://openairdocs.org/sdr/TWAA0006005), Apr 14, 2000: SEAT TRACK. CORRODED. DURING C CHECK, THE LT OTBD SEAT TRACK WAS BLENDED BEYOND LIMITS, STA 1231 TO 1240, LONGERON 54. REPLACED SEAT TRACK AT STA 1231 TO 1309 PER DRAWING 5930566. -- - [SDR TWAA0006004](https://openairdocs.org/sdr/TWAA0006004), Apr 14, 2000: FLOOR SUPPORT. CORRODED. DURING C CHECK, IN AFT CARGO BAY, STA 1211, LONGERON 29 LT, AFT FACE OF SUPPORT HAD CORROSION ON FLOOR SUPPORT AT STA 1211, LONGERON 29 RT TO 30 RT. REPLACED FL - [SDR TWAA0006110](https://openairdocs.org/sdr/TWAA0006110), Apr 11, 2000: FORGING. CRACKED. DURING C CHECK, AT CABIN STA 1338, LONGERON 18 RT, WHERE 3 LEGGED FORGING ATTACHES TO FRAME TO FLOORBEAM, THE VERTICAL LEG WAS CRACKED AND CORRODED. REPLACED FI - [SDR TWAA0005803](https://openairdocs.org/sdr/TWAA0005803), Apr 7, 2000: FLOORBEAM. CRACKED. DURING C CHECK, MAINT FOUND CRACK IN FLOORBEAM CAP AT STA 237, RBL 4, CARGO CEILING AREA. FABRICATED NEW FLOORBEAM CAP PER SPM 6-70-01 AND SRM 51-10-03. ---CLOS - [SDR TWAA0004002](https://openairdocs.org/sdr/TWAA0004002), Mar 10, 2000: LINK. BROKEN. ON LANDING GEAR RETRACTION, THE RT GEAR UNSAFE LIGHT AND GEAR DOOR WARNING LIGHT WERE ON. SLOWED TO 180 KTS AND CYCLED GEAR, NO HELP. FLIGHT RETURNED TO STL. RE - [SDR TWAA0003403](https://openairdocs.org/sdr/TWAA0003403), Feb 29, 2000: LIGHT. INOPERATIVE. THE LEFT SIDE FORWARD CABIN DOOR PORTABLE EMERGENCY LIGHT ON-OFF SWITCH WAS BROKEN. REPLACED THE LIGHT ASSY. CHECK-C 5-5-99 MCI. - [SDR TWAA9906801](https://openairdocs.org/sdr/TWAA9906801), May 10, 1999: LINK. BROKEN. AFTER TAKEOFF AND GEAR RETRACTION THE LEFT GEAR RED UNSAFE LIGHT AND GEAR DOOR OPEN LIGHT REMAINED ON. RECYCLED THE GEAR, NO HELP. FLIGHT RETURNED TO STL. FOUND - [SDR TWAA9902902](https://openairdocs.org/sdr/TWAA9902902), Feb 18, 1999: BEAM. CRACKED. FOUND THE FORWARD RIGHT CABIN DOOR HAD THE BOTTOM DOOR BEAM CRACKED. INSTALLED NEW DOOR BEAM PER SRM 51-30-2. CHECK-C 8-27-98 STL. - [SDR TWAA9817101](https://openairdocs.org/sdr/TWAA9817101), Oct 22, 1998: BATTERIES. DISCHARGED. OVERHEAD EMERGENCY EXIT LIGHTS AND COCKPIT EMERGENCY LIGHTS WERE REPORTED INOPERATIVE. REPLACED BATTERIES IN FWD POWER SUPPLY. CHECK-C 8-27-98 STL. - [SDR TWAA9814001](https://openairdocs.org/sdr/TWAA9814001), Aug 24, 1998: BULKHEAD TEE. CREASED. DURING CHECK-C MAINT, FOUND CREASE ON BULKHEAD TEE STA 1338, BETWEEN LONGERON 29R AND 29L. REMOVED AND REPLACED TEE PER SRM 53-03, FIG 37A. - [SDR TWAA9809701](https://openairdocs.org/sdr/TWAA9809701), Jun 17, 1998: COMPRESSOR. STALLED. DCA - FLT 797 - AT FL 330 TO 350 RT ENGINE HAD SEVERAL STALLS. REDUCED THROTTLE TO IDLE AND STALLS STOPPED. DECLARED EMERGENCY AND DIVERTED TO DCA. REPLACED ENG - [SDR TWAA9808301](https://openairdocs.org/sdr/TWAA9808301), May 25, 1998: OVEN. MALFUNCTIONED. STL - FLT 100 - DURING CRUISE, THE COACH GALLEY OVEN L2 EMITTED STRONG ELECTRICAL FUMES. REPLACED THE AFT GALLEY L2 OVEN MFG P/N 50381. (M) - [SDR TWAA9803102](https://openairdocs.org/sdr/TWAA9803102), Mar 3, 1998: TARGET. MISSING. OMA - FLT 38 - AFT CARGO DOOR LIGHT ILLUMINATED AFTER TAKEOFF. RETURNED TO OMA. DOOR INDICATION PLACARDED PER MEL. ON ACFT LAYOVER, THE DOOR SENSOR WAS REPLACED - [SDR TWAA9802402](https://openairdocs.org/sdr/TWAA9802402), Feb 16, 1998: BEARING. FAILED. MEM - FLT 1226 - DURING FLIGHT, THE LEFT ENGINE, SPOOLED DOWN. MADE UNSCHEDULED LANDING AT MEM. REPLACED ENGINE. ENGINE WAS DISASSEMBLED AND FOUND NR 3 BEARING - [SDR TWAA9714101](https://openairdocs.org/sdr/TWAA9714101), Dec 3, 1997: PRESSURE REG. FAILED. JFK - FLT 783 - AFTER TAKEOFF ROTATION, RIGHT AIRCONDITIONING TEMPERATURE SUPPLY HIGH INDICATION LIGHT CAME ON. REPLACED THE PILOT PRESSURE REGULATOR. (M) - [SDR TWAA9807909](https://openairdocs.org/sdr/TWAA9807909), Aug 14, 1997: LONGERON. CORRODED. MCI - DURING OP 15 MAINTENANCE CHECK, FOUND CORROSION AT STATION 200 TO 218, LONGERON 18L FORWARD AND AFT OF LAV VENT. CLEANED CORROSION PER SRM 51-10-3, PAR 31 - [SDR TWAA9807908](https://openairdocs.org/sdr/TWAA9807908), Aug 14, 1997: FRAME. DAMAGED. MCI - DURING OP 15 MAINTENANCE CHECK, FOUND FORMER RING STATION 1380 BELOW LONGERON 4L WITH GOUGE WORN INTO FORMER BY IMPROPERLY INST AIR VALVE. REMOVED DAMAGED - [SDR 95ZZZX4256](https://openairdocs.org/sdr/95ZZZX4256), Aug 4, 1995: FILTER. DIRTY. ICT - FLT 65 - DURING CRUISE, SHUT DOWN NR 1 ENGINE, SN 1206, DUE TO HIGH OIL PRESSURE AND INCREASING OIL TEMPERATURE. REPLACED ENGINE OIL FILTER AND ENGINE OIL - [SDR 95ZZZX547](https://openairdocs.org/sdr/95ZZZX547), Jan 13, 1995: ENGINE. FAILED. JFK - FLT 481 - DURING CLIMB, SHUT DOWN LEFT ENGINE DUE TO LOUD BANG AND INCREASING EGT. FOUND METAL PARTICLES IN TAILPIPE. REPLACED ENGINE, SN 3218. GROUND RUN ## FAA accident and incident reports (2) 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 19900917059119I](https://openairdocs.org/incident/19900917059119I), Sep 17, 1990: Doug MD88 (N919TW), Covington - Cin, OH. Burning odor from air conditioning ducts after takeoff. Returned. Found APU oil in ducts. - [Incident 19870419015399I](https://openairdocs.org/incident/19870419015399I), Apr 19, 1987: Doug DC982 (N919TW), Wichita, KS. Cockpit cleared of smoke when left air conditioning pack was turned off en route. Placarded inop to termination. ## Other aircraft with N919TW - [Registered now](https://openairdocs.org/aircraft/N919TW): Kubicek Factory S R O BB45Z, S/N 2306, built 2024 --- 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.