# N914TW: 1984 Mcdonnell Douglas DC-9-82(MD-82), registration cancelled 2012-09-06

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: September 6, 2012
- 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: 49185
- Year built: 1984
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: March 23, 1984
- Last registry action: May 31, 2006
- Mode S code: ACA745
- 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/N914TW
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=914TW
- Page: https://openairdocs.org/deregistered/N914TW-2012-09-06

From the FAA registry file of November 3, 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 (45)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR ZW0A0208203](https://openairdocs.org/sdr/ZW0A0208203), Aug 3, 2002: B-NUT. LOOSE. DURING TAKEOFF HIGH TEMP LIGHT IN TAIL COMPARTMENT RESULT IN UNSCHEDULED LANDING/RETURN TO STL. PNEUMATIC PRESS REGULATOR RELIEF LINE LOOSE HEAT EXCHANGE VENTIN
- [SDR ZW0A0204604](https://openairdocs.org/sdr/ZW0A0204604), Apr 23, 2002: CONNECTOR. LOOSE. THE EGRESS LIGHTING ROWS 7 TO 15 WERE INOPERATIVE. RESET THE CONNECTORS.
- [SDR ZW0A0204102](https://openairdocs.org/sdr/ZW0A0204102), Apr 5, 2002: BATTERY. DISCHARGED. THE EMERGENCY EVACUATION LIGHTS IN THE CABIN WERE ILLUMINATED WITH THE SWITCH IN THE ARM POSITION. REPLACED THE BATTERIES IN THE POWER SUPPLY.
- [SDR ZW0A0203901](https://openairdocs.org/sdr/ZW0A0203901), Apr 1, 2002: POWER SUPPLY. DURING CLIMB AND DESCENT THE FIRST CLASS CABIN EGRESS LIGHTS ILLUMINATED. REPLACED THE POWER SUPPLY. CHECK-C 3-4-01 STL. --CLOSED--
- [SDR ZW0A0203303](https://openairdocs.org/sdr/ZW0A0203303), Mar 14, 2002: FRAME. CORRODED. DURING CHECK-C MAINT THE FORMER RING AND REPAIR WERE CORRODED AT STA 1309, LONGERON 27R TO 27L. REMOVED AND INSTALLED NEW FRAME AND INSTALLED REPAIR SPLICES PER
- [SDR ZW0A0203302](https://openairdocs.org/sdr/ZW0A0203302), Mar 14, 2002: CARGO TRACK. CORRODED. DURING CHECK-C MAINT THE LT FLOOR TRACK IN THE AFT CARGO COMPARTMENT WAS CORRODED FROM STA 1211 TO 1320. INSTALLED NEW TRACK IN CARGO COMPARTMENT, LT SIDE, AND 
- [SDR ZW0A0203301](https://openairdocs.org/sdr/ZW0A0203301), Mar 14, 2002: INTERCOSTAL. CORRODED. DURING CHECK-C MAINT THE INTERCOSTAL WAS CORRODED AT STA 1308 TO 1322, BETWEEN LONGERON 27 AND 28, LT SIDE. DRILLED NEW INTERCOSTAL AND END FITTINGS AND INSTALL
- [SDR ZW0A0203102](https://openairdocs.org/sdr/ZW0A0203102), Mar 12, 2002: FLOOR SUPPORT. CORRODED. DURING CHECK-C MAINT IN AFT CABIN FOUND CORROSION ON FLOOR SUPPORT AT STA 1320, LONGERON 23L TO 23R. INSTALLED NEW FLOOR SUPPORT PER SPM 6-70-01, 4B.
- [SDR ZW0A0203104](https://openairdocs.org/sdr/ZW0A0203104), Mar 8, 2002: FLOOR SUPPORT. CORRODED. DURING CHECK-C MAINT FOUND CORROSION ON CAPTAINS KICKPLATE BULKHEAD AND FLOOR PANEL SUPPORT. REMOVED CORROSION PER SPM 6-80-01. FABRICATED NEW SUPPORT AND INSTA
- [SDR ZW0A0203103](https://openairdocs.org/sdr/ZW0A0203103), Mar 8, 2002: SEAT TRACK. CORRODED. DURING CHECK-C MAINT FOUND PILOTS AFT INBD SEAT TRACK WAS CORRODED. REMOVED AND REPLACED TRACK PER SRM 51-01, PAGE 1, ITEM C.
- [SDR ZW0A0203106](https://openairdocs.org/sdr/ZW0A0203106), Mar 6, 2002: SEAT TRACK. CORRODED. DURING CHECK-C MAINT FOUND CORROSION ON NUMBER 6 RH O/B SEAT TRACK, FROM STA 256 TO 313. REPLACED SECTION OF SEAT TRACK USING SEAT TRACK SPLICE AT STA 421. TRAC
- [SDR ZW0A0203105](https://openairdocs.org/sdr/ZW0A0203105), Mar 6, 2002: FRAME. CORRODED. DURING CHECK-C MAINT IN THE AFT CABIN AND CARGO BIN, THE FORMER RING WAS CORRODED AT STA 1271, LONGERON 27L TO 29R. INSTALLED NEW Z FRAME FROM LBL 37 TO RBL 11,
- [SDR ZW0A0202401](https://openairdocs.org/sdr/ZW0A0202401), Feb 25, 2002: WEB. CORRODED. DURING CHECK-C FOUND LT AFT LAV AT STA 1338 TO 1350, STRINGER 18L TO 17L, LBL 50 TO 56, THE FLOORBEAM FRAME AT FUSELAGE SKIN AREA, WEB HAD CORROSION. REMOVED CO
- [SDR ZW0A0202402](https://openairdocs.org/sdr/ZW0A0202402), Feb 20, 2002: ANGLE. CORRODED. DURING CHECK-C MAINT THE LEFT SIDE MOST FORWARD CABIN DOOR JAMB, 2 ANGLES HAD CORROSION AT STA 180 TO 200. FABRICATED AND INSTALLED PER SRM 1-10-02, 1-10-03, 51
- [SDR ZW0A0202204](https://openairdocs.org/sdr/ZW0A0202204), Feb 14, 2002: TRUNNION. CRACKED. DURING CHECK-C MAINT IN THE LT WHEEL WELL, FOUND CRACK IN LT GEAR SUPPORT CASTING ABOVE THE LT INBOARD FLAP TRACK, AND ABOVE THE LT FLAP BUSS CABLE BRACKET. REP
- [SDR ZW0A0202006](https://openairdocs.org/sdr/ZW0A0202006), Feb 13, 2002: BRACKET. CRACKED. DURING CHECK-C MAINT THE MID CARGO DOOR BOTTOM INBOARD BRACKET WAS CRACKED, LOWER SIDE FOR AFT BOTTOM DOOR STOP. FABRICATED NEW BRACKET AND INSTALLED.
- [SDR ZW0A0202005](https://openairdocs.org/sdr/ZW0A0202005), Feb 13, 2002: BRACKET. CRACKED. DURING CHECK-C MAINT IN THE MID CARGO COMPARTMENT, THE AFT BOTTOM DOOR STOP BRACKET WAS CRACKED INSIDE THE DOOR, ON THE FWD FACE. REMOVED AND REPLACED CRACKED B
- [SDR ZW0A0201807](https://openairdocs.org/sdr/ZW0A0201807), Feb 13, 2002: CARGO TRACK. CORRODED. DURING CHECK-C MAINT IN CARGO COMPT FOUND CORROSION ON TIE DOWN TRACK AT STA 785, RT SIDE. REPLACED TRACK WITH NEW AT STA 693 TO 788 PER SPM 6-70-01.
- [SDR ZW0A0201806](https://openairdocs.org/sdr/ZW0A0201806), Feb 12, 2002: TIE CLIP. CORRODED. DURING CHECK-C MAINT THE AFT CABIN STA 1338 TIE CLIP HAD CORROSION AT RBL 57 AREA. INSTALLED NEW CLIP PER SPM 6-70-01.
- [SDR ZW0A0201805](https://openairdocs.org/sdr/ZW0A0201805), Feb 12, 2002: WEB. CORRODED. DURING CHECK-C MAINT THE AFT CABIN STA 1338, RBL 57, WEB HAD HEAVY CORROSION 6 INCHES BELOW FLOORBEAM RT LAV. INSTALLED FILLER DOUBLER PER SRM 51-70-4.
- [SDR ZW0A0202002](https://openairdocs.org/sdr/ZW0A0202002), Feb 8, 2002: STOP FITTING. CRACKED. DURING CHECK-C MAINT IN MID CARGO COMPT THE AFT BOTTOM DOOR STOP BRACKET, INSIDE THE DOOR, IS CRACKED ON AFT SIDE. REMOVED AND REPLACED CRACKED BRACKET AND REPL
- [SDR ZW0A0202001](https://openairdocs.org/sdr/ZW0A0202001), Feb 8, 2002: FLOORBEAM. CORRODED. DURING CHECK-C MAINT FOUND CORROSION IN RT FLOORBEAM BETWEEN STA 636 AND 693. REMOVED CORROSION PER SPM 6-80-01. INSTALLED REPAIR ANGLE AND FILLER PER SRM 53-05
- [SDR ZW0A0201804](https://openairdocs.org/sdr/ZW0A0201804), Feb 7, 2002: BRACKET. CRACKED. DURING CHECK-C MAINT THE FORWARD CARGO COMPARTMENT DOOR HAD A SMALL BRACKET CRACKED LOCATED INSIDE THE SECOND LIGHTENING HOLE FROM THE AFT END, AT LOWER EDGE OF
- [SDR ZW0A0201803](https://openairdocs.org/sdr/ZW0A0201803), Feb 7, 2002: CARGO TRACK. CORRODED. DURING CHECK-C MAINT IN THE AFT CARGO COMPARTMENT FOUND CORROSION ON FLOOR TRACK AT STA 1211 TO 1320, RT TRACK. REPLACED TRACK PER SPM 6-70-01-4B, AND SRM 51-30
- [SDR ZW0A0201802](https://openairdocs.org/sdr/ZW0A0201802), Feb 7, 2002: CARGO TRACK. CORRODED. DURING CHECK-C MAINT IN THE AFT CARGO COMPARTMENT FOUND CORROSION ON THE LT TIE DOWN TRACK FROM STA 1003 TO 1231. INSTALLED NEW TIE DOWN TRACK PER SPM 6-70-01-4
- [SDR ZW0A0201602](https://openairdocs.org/sdr/ZW0A0201602), Feb 7, 2002: KEELBEAM. CRACKED. DURING CHECK-C IN LT WHEEL WELL, FOUND ANGLE CRACKED FWD OF HINGE CASTING AT KEEL BEAM. REMOVED AND REPLACED CRACKED ANGLE PER SPM 6-70-01.
- [SDR ZW0A0201601](https://openairdocs.org/sdr/ZW0A0201601), Feb 7, 2002: FRAME. CORRODED. DURING CHECK-C FOUND CABIN STA 1338 LONGERON 18R, FRAME HAS CORROSION FROM FLOOR LEVEL TO 6 INCHES UP THE FWD SIDE. CORROSION WAS REMOVED PER SPM 6-80-01.
- [SDR TWAA0104605](https://openairdocs.org/sdr/TWAA0104605), Mar 10, 2001: BATTERY PACK. DISCHARGED. THE EMERGENCY LIGHTS CAME ON DURING FLIGHT AT ROW 5 THRU 15. REPLACED THE BATTERY PACK. CHECK-C 2-13-01 STL.
- [SDR TWAA0104603](https://openairdocs.org/sdr/TWAA0104603), Mar 10, 2001: BATTERY PACK. DISCONNECTED. THE EGRESS LIGHTS AT ROW 5 THRU 15 CAME ON DURING FLIGHT. ALL THE LIGHTS WENT OUT WITH THE EMERGENCY LIGHT SWITCH TURNED OFF. RECONNECTED THE BATTERY PACK AT RO
- [SDR TWAA0104604](https://openairdocs.org/sdr/TWAA0104604), Mar 9, 2001: BATTERY. DISCHARGED. THE EGRESS LIGHTS COME ON AT ROW 5 TO 15. REPLACED THE EMERGENCY LIGHT BATTERIES. CHECK-C 2-13-01 STL.
- [SDR TWAA0104501](https://openairdocs.org/sdr/TWAA0104501), Mar 8, 2001: BATTERY. DISCHARGED. A SECTION OF EGRESS LIGHTING IN THE FIRST CLASS CABIN ILLUMINATED DURING TAXI AND WOULD NOT RESET. REPLACED THE BATTERIES IN THE POWER SUPPLY. CHECK-C 2-13-01 S
- [SDR TWAA0104403](https://openairdocs.org/sdr/TWAA0104403), Mar 7, 2001: BATTERY PACK. DISCHARGED. THE EGRESS LIGHTS ON CABIN FLOOR AND AT THE LEFT SIDE NUMBER 2 CABIN DOOR OCCASIONALLY ILLUMINATED IN FLIGHT. REPLACED THE BATTERY PACK. CHECK-C 2-13-01 STL.
- [SDR TWAA0104402](https://openairdocs.org/sdr/TWAA0104402), Mar 7, 2001: LIGHT. INTERMITTENT. THE FIRST SECTION OF CABIN EGRESS LIGHTS REPORTED TO INTERMITTENTLY STAY ILLUMINATED. RESET THE EMERGENCY LIGHT ARM AND CHARGE CIRCUIT BREAKER AND LIGHTS OPERAT
- [SDR TWAA0100902](https://openairdocs.org/sdr/TWAA0100902), Jan 14, 2001: SWITCH. INOPERATIVE. THE EGRESS LIGHTING WAS INOPERATIVE FROM CABIN ROWS 5 TO 14. RECYCLED THE EMERGENCY LIGHT SWITCH. CHECK-C 2-3-00 STL.
- [SDR TWAA0017001](https://openairdocs.org/sdr/TWAA0017001), Oct 31, 2000: BATTERY PACK. WORN. THE FIRST CLASS OVERHEAD EMERGENCY LIGHT AND ONE SECTION OF COACH FLOOR EGRESS LIGHTS WERE INOPERATIVE. REPLACED THE BATTERY PACK AT ROW 3 AND THE FEEDER STRIP 
- [SDR TWAA0015606](https://openairdocs.org/sdr/TWAA0015606), Oct 5, 2000: COMPRESSOR. FOD. CREW ABORTED TAKEOFF AT 65 KTS DUE TO RT ENGINE STALL WITH VIBRATION ON RT FUEL CONTROL LEVER. ENGINE WAS SHUT DOWN AND FLIGHT RETURNED TO THE GATE. COMPRESSOR 
- [SDR TWAA9917001](https://openairdocs.org/sdr/TWAA9917001), Dec 15, 1999: VHF RADIO. CONTAMINATED. THE NUMBER 1 AND 2 VHF COMM RADIOS WERE INOPERATIVE AFTER TAKEOFF. STATIC WAS TRANSMITTED ON ANY FREQUENCY SELECTED. FLIGHT RETURNED TO STL. FOUND MOISTURE IN T
- [SDR TWAA9916901](https://openairdocs.org/sdr/TWAA9916901), Dec 14, 1999: LIGHT. INOPERATIVE. THE CABIN EGRESS LIGHTS WERE INOPERATIVE FROM ROW 4 TO 16. FOUND FEEDER CABLE BROKEN AND SPLICED CABLE TOGETHER. CHECK-C 2-13-99 MCI.
- [SDR TWAA9906401](https://openairdocs.org/sdr/TWAA9906401), Apr 3, 1999: TURBINE. FAILED. DURING TAKEOFF, THERE WAS A LOUD NOISE FROM THE NUMBER 1 ENG FOLLOWED BY HIGH EGT INDICATION. THE ENG WAS SHUT DOWN AND THE FLIGHT RETURNED TO STL. FOUND THE TU
- [SDR TWAA9819301](https://openairdocs.org/sdr/TWAA9819301), Dec 4, 1998: COFFEEMAKER. FAILED. THE NUMBER 3 GALLEY COFFEEMAKER CAUSED SPARKS. CREW PULLED CIRCUIT BREAKER. MAINT REPLACED THE COFFEEMAKER. CHECK-C 2-28-98 MCI.
- [SDR TWAA9812501](https://openairdocs.org/sdr/TWAA9812501), Aug 3, 1998: BOOST PUMP. WORN. ABOVE FL 300 COULD NOT PUMP FUEL FROM CENTER TANK. TURNED OFF LEFT TANK PUMPS AND DESCENDED IN ALTITUDE AND CENTER TANK STARTED FEEDING. RETURNED TO MCI. REPLAC
- [SDR 96ZZZM1202](https://openairdocs.org/sdr/96ZZZM1202), Jul 10, 1996: BULB. FAILED. SFO - DURING GEAR EXTENSION RIGHT MAIN LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE. REMOVED AND REPLACED LIGHT BULB IN LIGHT ASSEMBLY. OPERATIONAL CHECK NORMAL.
- [SDR 96ZZZM46](https://openairdocs.org/sdr/96ZZZM46), Dec 23, 1995: STRUT SEALS. FAILED. TPA - DURING LANDING, UNABLE TO LOWER NOSE GEAR. CYCLED LANDING GEAR. NOSE STRUT SEALS REPLACED, REPACKED NOSE STRUT. CYCLED GEAR AND OPERATIONS ARE NORMAL.
- [SDR 95ZZZX3411](https://openairdocs.org/sdr/95ZZZX3411), Jun 22, 1995: BLADE. FAILED. DEN - FLT 427 - DURING DESCENT, SHUT DOWN LEFT ENGINE DUE TO SPOOLED DOWN WITH INCREASING EGT. FOUND METAL PARTICLES IN TAILPIPE. CHANGED ENGINE, S/N 1205. ENGI
- [SDR 95ZZZW339](https://openairdocs.org/sdr/95ZZZW339), Mar 20, 1995: RETRACT SYS. REQ'D LUBE. BOS - AFTER TAKEOFF NOSE LANDING GEAR DID NOT RETRACT. CYCLED LANDING GEAR, AND NOSE LANDING GEAR RETRACTED. INSPECTED NOSE LANDING GEAR AND LUBRICATED. JACKED 

## 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 19910831046709I](https://openairdocs.org/incident/19910831046709I), Aug 31, 1991: Doug DC982 (N914TW), Pittsburgh, PA. Left engine oil quantity decreasing during climb. Diverted for landing. Oil line leaking at pressure switch.
- [Incident 19880807048169I](https://openairdocs.org/incident/19880807048169I), Aug 7, 1988: Doug DC982 (N914TW), Ontario, CA. Engine failure during takeoff. Aborted takeoff roll. Cause not given.

## Other aircraft with N914TW

- [Registered now](https://openairdocs.org/aircraft/N914TW): Head Balloons AX9-118, S/N 517, built 2024

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