# N913TW: 1984 Mcdonnell Douglas DC-9-82(MD-82), registration cancelled 2013-08-13 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: August 13, 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: 49184 - Year built: 1984 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: March 8, 1984 - Last registry action: May 31, 2006 - Mode S code: ACA38E - 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/N913TW - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=913TW - Page: https://openairdocs.org/deregistered/N913TW-2013-08-13 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 (32) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR ZW0A0111407](https://openairdocs.org/sdr/ZW0A0111407), Nov 19, 2001: CARGO TRACK. CORRODED. DURING CHECK-C MAINT IN THE AFT CARGO COMPT THE RT TIE DOWN WAS CORRODED FROM STA 1212 TO 1322. REPLACED WITH NEW TRACK PER SRM 51-30-1, STA 1212 TO 1322. - [SDR ZW0A0111406](https://openairdocs.org/sdr/ZW0A0111406), Nov 19, 2001: CARGO TRACK. CORRODED. DURING CHECK-C MAINT IN THE AFT CARGO COMPT THE LT TIE DOWN TRACK WAS CORRODED FROM STA 1212 TO 1322. INSTALLED NEW TRACK PER SRM 51-30-2, AND 51-30-8. INSTALLE - [SDR ZW0A0111405](https://openairdocs.org/sdr/ZW0A0111405), Nov 19, 2001: INTERCOSTAL. CORRODED. DURING CHECK-C MAINT IN THE AFT CARGO COMPT FOUND CORROSION ON INTERCOSTAL AT STA 1309 TO 1322, BELOW THE LT CHAIR TRACK. REMOVED CORROSION PER SRM 51-10-3. INS - [SDR ZW0A0111404](https://openairdocs.org/sdr/ZW0A0111404), Nov 16, 2001: FRAME. CORRODED. DURING CHECK-C MAINT IN THE AFT CARGO COMPT FOUND FORMER CORRODED FROM LONGERON 28R TO 28L, STA 1271. REMOVED CORROSION PER SPM 6-80-1 AND SRM 51-10-3. REPAIRED - [SDR ZW0A0111403](https://openairdocs.org/sdr/ZW0A0111403), Nov 15, 2001: FRAME. CORRODED. DURING CHECK-C MAINT FOUND CORROSION IN AFT CARGO COMPT ON FORMER FRAME AT STA 1322, FROM LONGERON 29L TO 29R. REMOVED CORROSION PER SRM 51-10-3. REPAIRED PER S - [SDR ZW0A0111003](https://openairdocs.org/sdr/ZW0A0111003), Nov 12, 2001: THRESHOLD. CORRODED. DURING CHECK-C MAINT THE AFT EMERGENCY DOOR (VAULT DOOR) THRESHOLD PLATE BELOW THE FLOOR LINE WAS HEAVILY CORRODED. REPAIRED AREA PER 51-10-3, 51-30-2, AND 51-3 - [SDR ZW0A0111002](https://openairdocs.org/sdr/ZW0A0111002), Nov 11, 2001: FLOOR SUPPORT. CRACKED. DURING CHECK-C MAINT THE FLOOR SUPPORT HAD A 4 INCH CRACK AT STA 927, LBL 44, BELOW THE OUTBOARD TRACK. INSTALLED BEAM PER DOUGLAS DRAWING 593056, P/N 9915527-5 - [SDR ZW0A0111001](https://openairdocs.org/sdr/ZW0A0111001), Nov 9, 2001: SILL. CORRODED. DURING CHECK-C MAINT THE AFT CARGO COMPT DOOR SILL WAS CORRODED AT STA 1155 TO 1212. INSTALLED NEW BEAM PER SPM 6-70-1, SRM 51-30-2 AND SRM 51-30-5. TREATED ARE - [SDR ZW0A0110804](https://openairdocs.org/sdr/ZW0A0110804), Nov 8, 2001: SEAT TRACK. CORRODED. DURING CHECK-C MAINT, THE NUMBER 1 (LT OUTBOARD) FLOOR TRACK WAS CORRODED BEYOND LIMITS AT STA 797 TO 1003. REPLACED FLOOR TRACK PER SRM 51-30-1 AND SPM 6-70-01 - [SDR ZW0A0110703](https://openairdocs.org/sdr/ZW0A0110703), Nov 6, 2001: SEAT TRACK. CORRODED. DURING CHECK-C MAINT FOUND FLOOR TRACK AT LBL 44, STA 1260 TO 1300, HAD CORROSION. REPLACED TRACK FROM STA 1041 TO 1309 PER SRM 53-05, FIG 4F. - [SDR ZW0A0110702](https://openairdocs.org/sdr/ZW0A0110702), Nov 5, 2001: FLOOR SUPPORT. CORRODED. DURING CHECK-C MAINT FOUND CABIN FLOOR AT L-1 CABIN DOOR, THE OUTBOARD SUPPORT FOR FLOOR PANEL NUMBER 16 WAS CORRODED. REPLACED SUPPORT PER SPM 6-70-01. - [SDR ZW0A0110604](https://openairdocs.org/sdr/ZW0A0110604), Nov 5, 2001: FRAME. CORRODED. DURING CHECK-C MAINT FOUND CORROSION ON FORMER FROM STA 1309 LONGERON TO LONGERON 29L. PREVIOUS FORMER SPLICE REMOVED. TREATED PER SPM 6-50-1 AND SRM 51-10-3. R - [SDR ZW0A0110603](https://openairdocs.org/sdr/ZW0A0110603), Nov 2, 2001: LONGERON. CORRODED. DURING CHECK-C MAINT IN THE AFT CARGO COMPT FOUND CORROSION ON LONGERON 22L, STA 1290. REPLACED CORRODED SECTION OF LONGERON. SPLICED IN NEW SECTION PER SRM 53- - [SDR ZW0A0110602](https://openairdocs.org/sdr/ZW0A0110602), Nov 1, 2001: SKIN. DAMAGED. DURING CHECK-C MAINT THE FUSELAGE SKIN ALONG THE AFT SIDE OF THE FWD CARGO DOOR ENTRY WAY, STA 427, WAS BENT AND DAMAGED. BLENDED DAMAGED AREA PER SRM 51-02-E. - [SDR ZW0A0110307](https://openairdocs.org/sdr/ZW0A0110307), Oct 26, 2001: ANGLE. CRACKED. DURING CHECK-C MAINT IN THE FWD CARGO COMPT FOUND THE FLOOR TO AFT BULKHEAD SUPPORT WAS CRACKED IN THE RADIUS, STA 541 AND LONGERON 29L. REPLACED CRACKED ANGLE - [SDR ZW0A0110306](https://openairdocs.org/sdr/ZW0A0110306), Oct 25, 2001: CARGO TRACK. CORRODED. DURING CHECK-C MAINT THE LT TIE DOWN TRACK WAS CORRODED IN THE MID CARGO COMPT AT STA 636 TO 693. REPLACED TRACK FROM STA 514 TO 790 PER SRM 53-05, FIG 6, AND S - [SDR ZW0A0110305](https://openairdocs.org/sdr/ZW0A0110305), Oct 24, 2001: PLATE. CORRODED. DURING CHECK-C MAINT IN THE FWD CABIN FOUND HEAVY CORROSION 12 INCHES INBOARD OF THE FWD SERVICE DOOR THRESHOLD, ON FLOOR PLATE. REMOVED OLD FLOOR PLATE AND REP - [SDR ZW0A0110304](https://openairdocs.org/sdr/ZW0A0110304), Oct 24, 2001: FLOOR SUPPORT. CORRODED. DURING CHECK-C MAINT FOUND CABIN FLOOR SUPPORT ANGLE AT STA 1155, BETWEEN LBL 27 INCHES TO 45 INCHES, HAD CORROSION. REMOVED RIVETS. IDENTIFIED MATERIAL PER SRM - [SDR ZW0A0110001](https://openairdocs.org/sdr/ZW0A0110001), Oct 23, 2001: FLOORBEAM. CORRODED. DURING CHECK-C MAINT FOUND CORROSION AT STA 1250, LBL 24 INCHES TO LBL 44 INCHES, CABIN FLOOR FRAME. REMOVED AND TREATED CORROSION PER SPM 6-80-01 AND SRM 51-10 - [SDR ZW0A0110303](https://openairdocs.org/sdr/ZW0A0110303), Oct 22, 2001: SEAT TRACK. CORRODED. DURING CHECK-C MAINT THE FLOOR TRACK WAS CORRODED IN SEVERAL AREAS AT LBL 21 INCHES, STA 1136 TO 1309. REMOVED AND REPLACED TRACK PER SRM 53-05 AND SPM 6-30-01, - [SDR ZW0A0106003](https://openairdocs.org/sdr/ZW0A0106003), Jul 27, 2001: DETECTOR. DURING CRUSE FLIGHT 253 HAD A INDICATION OF SMOKE IN THE AFT. CARGO BIN. THE FLIGHT CREW MADE AN UNSCHEDULED LANDING AND FIRED THE AFT CARGO BIN FIRE BOTTLE. CA - [SDR TWAA0103604](https://openairdocs.org/sdr/TWAA0103604), Feb 25, 2001: LATCH. UNLATCHED. STRONG VIBRATION FELT AND HEARD IN FWD PART OF THE AIRCRAFT DURING CLIMB. FLIGHT RETURNED TO STL. THE EXTERNAL POWER DOOR UPPER LATCH WAS NOT SECURED. RESECURED - [SDR TWAA0014504](https://openairdocs.org/sdr/TWAA0014504), Sep 15, 2000: POWER SUPPLY. INOPERATIVE. THE FIRST CLASS OVERHEAD EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED THE POWER SUPPLY. CHECK-C 12-13-99 MCI. - [SDR TWAA0010801](https://openairdocs.org/sdr/TWAA0010801), Jul 9, 2000: DUCT. CRACKED. IN CRUISE LOST CABIN PRESSURIZATION. CREW ACCOMPLISHED AN EMERGENCY DESCENT. PSU MASKS DID NOT DROP. FOUND RT PACK HOT AIR TRIM DUCT CRACKED AND LEAKING. WELDED - [SDR TWAA9917201](https://openairdocs.org/sdr/TWAA9917201), Dec 20, 1999: BATTERY PACK. DISCHARGED. THE AFT SECTION OF CABIN EGRESS LIGHTS WERE INOPERATIVE. REPLACED THE BATTERY PACK. CHECK-C 12-20-99. - [SDR TWAA0000112](https://openairdocs.org/sdr/TWAA0000112), Dec 15, 1999: BULKHEAD. CHAFED. DURING CHECK-C MAINT, THE AFT ACCESSORY COMPARTMENT AT STA 1380 BULKHEAD, HAD WORN AREA THROUGH WEB BELOW LONGERON 4L. REPAIRED BULKHEAD PER SRM 53-01, FIG 2 SH - [SDR TWAA9905901](https://openairdocs.org/sdr/TWAA9905901), Apr 21, 1999: RIVET. LOOSE. A .25 INCH PULLED RIVET WAS FOUND AT STA 50, LONGERON 20. EDDY CURRENT SHOWED NO CRACK. INSTALLED .25 INCH IN SOLID RIVET PER SRM 53-01, FIG 1. CHECK-C 1-10-99 - [SDR TWAA9820201](https://openairdocs.org/sdr/TWAA9820201), Dec 30, 1998: FAN. FAILED. SOME SMOKE AND SLIGHT BURNING ODOR REPORTED IN THE CABIN. THE -C- PHASE 50 AMP CB, AND A COUPLE OTHER BREAKERS, POPPED. FLIGHT DIVERTED TO IND. FOUND THE RECIRC - [SDR TWAA9811402](https://openairdocs.org/sdr/TWAA9811402), Jul 15, 1998: ROD. BROKEN. A CATERER REPORTED BEING UNABLE TO OPEN THE R-1 CABIN DOOR. FOUND A BROKEN CONTROL ROD FOR THE DOOR LOWER GATE. REPLACED ROD. CHECK-C 12-30-97 MCI. ACFT TT: 45, - [SDR TWAA9810704](https://openairdocs.org/sdr/TWAA9810704), Jul 6, 1998: SWITCH. FAILED. DCA - FLT 209 - AT 6,000 FEET WHEN EXTENDING AND TURNING ON WING LANDING LIGHTS, SMOKE CAME FROM UNDER CAPTAIN'S GLARE SHIELD. TURNED SWITCHES OFF IMMEDIATELY. - [SDR TWAA9803809](https://openairdocs.org/sdr/TWAA9803809), Mar 16, 1998: INDICATOR. WORN. STL - FLT 715 - OVERHEAT ODOR IN CABIN AND COCKPIT WHILE ON APPROACH. NO OVERHEAT INDICATION. WING AND ENGINE ANTI-ICE ON. GAUGES DID NOT INDICATE HOT, SOME SMO - [SDR 96ZZZM973](https://openairdocs.org/sdr/96ZZZM973), May 4, 1996: TURBINE. DAMAGED. MCI - DURING CRUISE, SHUT DOWN NR 1 ENGINE, S/N 3208, DUE TO RAPID DETERIORATION OF ENGINE PARAMETERS. FOUND TURBINE DAMAGE. CHANGED ENGINE. ENGINE OPERATION TH ## FAA accident and incident reports (5) 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 19891011055129I](https://openairdocs.org/incident/19891011055129I), Oct 11, 1989: Doug DC982 (N913TW), St Louis, MO. Hydraulic pressure lost on final approach. Landed safely. O rings seal to spoiler pressure reducer valve had failed - [Incident 19880621034809I](https://openairdocs.org/incident/19880621034809I), Jun 21, 1988: Doug DC982 (N913TW), St Louis, MO. Pilot aborted takeoff when spoiler deployed light came on during takeoff roll. No malfunction found. - [Incident 19880527032889I](https://openairdocs.org/incident/19880527032889I), May 27, 1988: Doug DC982 (N913TW), St Louis, MO. Tail compartment temp. High light came on. Returned. Landed ok. Found leak at a clamp on left side heat exchanger. - [Incident 19871225077159I](https://openairdocs.org/incident/19871225077159I), Dec 25, 1987: Doug DC982 (N913TW), St Louis, MO. Power loss and loud noises NR1 engine. Engine shut down. Returned. Found damage to first stage fan. - [Incident 19850819050269I](https://openairdocs.org/incident/19850819050269I), Aug 19, 1985: Doug DC982 (N913TW), St Louis, MO, Minor damage. Unsafe gear indication on right main. Manual extension. Safe landing. Repaired gear door. ## Other aircraft with N913TW - [Registered now](https://openairdocs.org/aircraft/N913TW): Textron 680A, S/N 680A0221, built 2020 --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). 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