# N9406W: 1992 Mcdonnell Douglas DC-9-83(MD-83), registration cancelled 2019-01-10

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: January 10, 2019
- Status when cancelled: Valid registration
- Airframe: [Mcdonnell Douglas DC-9-83(MD-83)](https://openairdocs.org/model/mcdonnell-douglas-dc-9-83-md-83) (registry code 3022083)
- Engine: [Pratt & Whitney JT8D-1](https://openairdocs.org/engine/pratt-whitney-jt8d-1) (registry code 52044)
- Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE), [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs)
- Serial number: 53126
- Year built: 1992
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: November 12, 1992
- Certificate issued: December 13, 2016
- Last registry action: December 13, 2016
- Mode S code: AD1067
- Owner when cancelled: [Tvpx Ars Inc Trustee](https://openairdocs.org/faa-owner/TVPX%20ARS%20INC%20TRUSTEE)
- Location: [North Salt Lake, UT](https://openairdocs.org/faa-place/UT/North%20Salt%20Lake)
- Owner type: Corporation
- Owner's area on the map: 40.8386° N, 111.9179° W: Placed by OpenAirDocs at the center of ZIP code 84054, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N9406W
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=9406W
- Page: https://openairdocs.org/deregistered/N9406W-2019-01-10

From the FAA registry file of November 4, 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-9-83(MD-83): https://openairdocs.org/model/mcdonnell-douglas-dc-9-83-md-83.md

## Service difficulty reports (71, newest 50)

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

- [SDR AALA20150914005](https://openairdocs.org/sdr/AALA20150914005), Sep 7, 2015: PUMP. INOPERATIVE. CENTER TANK, FUEL BOOST PUMP INOPERATIVE. R & R CTR TANK VOLUTE & REPLACED CTR TANK BOOST PUMP PICKUP LINE PACKING’S.
- [SDR AALA20150903017](https://openairdocs.org/sdr/AALA20150903017), Sep 3, 2015: ACM. FAILED. AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING TAKEOFF, TEMP COMPARTMENT HIGH WARNING ILLUMINATED. FOUND RT ACM FAILED. R & R AC
- [SDR AALA20141112008](https://openairdocs.org/sdr/AALA20141112008), Nov 12, 2014: STOP FITTING. CRACKED. CENTER CARGO DOOR UPPER AFT STOP CRACKED. R & R STOP IAW AARD 51-00-05-1 & DWG 5910141.
- [SDR AALA20141111017](https://openairdocs.org/sdr/AALA20141111017), Nov 10, 2014: SHEAR TIE. CRACKED. SHEAR TIE CRACKED FWD SIDE OF FUSELAGE STATION 1380 AT LONGERON 14 RT. REPAIRED SHEAR TIE IAW AARD53-10-00-20.
- [SDR AALA20141111014](https://openairdocs.org/sdr/AALA20141111014), Nov 10, 2014: SHEAR TIE. CRACKED. SHEAR TIE CRACKED FWD SIDE OF FRAME AT FUSELAGE STATION 1380 & LONGERON 14 LT. REPAIRED IAW AARD 53-10-00-20.
- [SDR AALA20141111013](https://openairdocs.org/sdr/AALA20141111013), Nov 10, 2014: LONGERON. CRACKED. LONGERON 2 RT CRACKED AT AFT SIDE OF FRAME AT FUSELAGE STATION 1418. PERFORMED SPLICE REPAIR IAW SRM 53-02-00-001.
- [SDR AALA20141016007](https://openairdocs.org/sdr/AALA20141016007), Oct 16, 2014: FORMER. CRACKED. LEFT WING LE NR 4 SLAT TRACK INBD FORMER IS CRACKED. INSTALLED LT WING NR 4 SLAT INBD FORMER DOUBLER & HAT BUSHING IAW WORK CARD 57-98-05.
- [SDR AALA20141016006](https://openairdocs.org/sdr/AALA20141016006), Oct 16, 2014: FORMER. CRACKED. RIGHT WING LE NR 4 SLAT TRACK INBD FORMER IS CRACKED. INSTALLED RT WING NR 4 INBD FORMER DOUBLER & HAT BUSHING IAW WORK CARD 57-98-06.
- [SDR AALA20140730004](https://openairdocs.org/sdr/AALA20140730004), Jul 27, 2014: LIGHT. DAMAGED. AFT AIRSTAIR OVERHEAD EMER LIGHT ASSEMBLY DAMAGED. REPLACED AFT AIRSTAIR OVERHEAD EMER LIGHT ASSEMBLY. OPERATIONS CHECKED NORMAL.
- [SDR AALA20140730003](https://openairdocs.org/sdr/AALA20140730003), Jul 27, 2014: WIRE. BROKEN. AFT STAIRWELL OVERHEAD LIGHT PANEL HAS BROKEN WIRE. REPAIRED WIRE FOR OVERHEAD EMER LIGHT. OPERATIONS CHECKED NORMAL.
- [SDR AALA20140613002](https://openairdocs.org/sdr/AALA20140613002), Jun 13, 2014: CSD. FAILED. INFLIGHT CREW REPORTED LT ENG GEN FAULTED. FLIGHT DIVERTED & LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED CONSTANT SPEED DRIVE & LT GEN MPN 976J
- [SDR AALA20140418005](https://openairdocs.org/sdr/AALA20140418005), Apr 18, 2014: CONNECTOR. LEAKING. LAS CREW REPORTED TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED DURING CLIMB OUT. ACCOMPLISHED QRH & LIGHT EXTINGUISHED. EMERGENCY DECLARED FLIGHT RETURNE
- [SDR AALA20130817003](https://openairdocs.org/sdr/AALA20130817003), Aug 16, 2013: SKIN. DAMAGED. LT WING OTBD FLAP UPPER SKIN HAS TWO LIGHTNING STRIKES. ACCOMPLISHED EXTERNAL DOUBLER REPAIR IAW SRM 57-01 FIGURE 3 SHEET 2 & EA MD80-57-031130.
- [SDR AALA20130725002](https://openairdocs.org/sdr/AALA20130725002), Jul 24, 2013: DUCT. RUPTURED. DFW CREW REPORTED LT ENGINE FIRE WARNING JUST AFTER GEAR UP. LIGHT INDICATION WENT OUT WHEN THROTTLE MOVED TO IDLE. EMERGENCY DECLARED FLIGHT LANDED DFW WITHOUT
- [SDR AALA20130202006](https://openairdocs.org/sdr/AALA20130202006), Feb 2, 2013: POWER SUPPLY. MALFUNCTIONED. DFW - FLIGHT ATTENDANTS REPORTED BURNING SMELL IN THE CABIN AFTER TAKEOFF. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM
- [SDR AALA20120129LAX01](https://openairdocs.org/sdr/AALA20120129LAX01), Jan 28, 2012: ACTUATOR. INOPERATIVE. LAX - CREW REPORTED AIRCRAFT WOULD NOT PRESSURIZE AFTER TAKE OFF. NUMBER 2 CABIN PRESSURE CONTROLLER CURRENTLY ON PLACARD. FLIGHT RETURNED LAX LANDED WITHOUT IN
- [SDR AALA20110714LGA03](https://openairdocs.org/sdr/AALA20110714LGA03), Jul 14, 2011: CONNECTOR. DISCONNECTED. SEAT ROW 32 EMERGENCY EGRESS LIGHT INOPERATIVE DURING FUNCTIONAL TEST. FOUND CONNECTOR DISCONNECTED AT SEAT ASSEMBLY. RECONNECTED AND RE-SECURED WIRING. OPS CHE
- [SDR AALA20110714LGA02](https://openairdocs.org/sdr/AALA20110714LGA02), Jul 14, 2011: CONNECTOR. SEPARATED. SEAT 19 EMERGENCY EGRESS FLOOR LIGHTING INOPERATIVE. FOUND CONNECTOR PINS PULLED OUT. REPINNED CONNECTOR AND SECURED WIRING. OPS CHECK NORMAL.
- [SDR AALA20110714LGA01](https://openairdocs.org/sdr/AALA20110714LGA01), Jul 14, 2011: LIGHT. INOPERATIVE. ROW 20 LEFT CEILING EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR ROW 20 CEILING EMERGENCY LIGHT. OPS CHECK NORMAL.
- [SDR AALA20100728TUL01](https://openairdocs.org/sdr/AALA20100728TUL01), Jul 28, 2010: MEMBRANE. CORRODED. EMERGENCY EQUIPMENT COMPARTMENT HAS CORROSION ON LOWER SURFACE OF CABIN FLOOR WEBBING AT G1 GALLEY SERVICE PAN. COMPLETED INSTALLATION OF SUBFLOOR DOUBLER FROM 
- [SDR AALA20100703DFW03](https://openairdocs.org/sdr/AALA20100703DFW03), Jul 3, 2010: PUMP. LEAKING. DFW - IN-FLIGHT SJD-ORD. CREW REPORTED AIRCRAFT LOSING FUEL AT RAPID PACE. EMERGENCY DECLARED DIVERTED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVIC
- [SDR AALA20100318SJC01](https://openairdocs.org/sdr/AALA20100318SJC01), Mar 18, 2010: OIL FILTER. CLOGGED. SJC - CREW REPORTED RIGHT ENGINE OIL FILTER CLOGGED INDICATION ILLUMINATED ON CLIMBOUT. EMERGENCY DECLARED RETURNED SJC LANDED WITHOUT INCIDENT. INSPECTED RIGHT
- [SDR AALA20091021DFW09](https://openairdocs.org/sdr/AALA20091021DFW09), Oct 21, 2009: PUMP. FAILED. INFLIGHT SJD TO ORD. IN CLIMB AND CRUISE, CENTER FUEL PRESSURE LOW WARNING INDICATION ILLUMINATED FOLLOWED BY INLET FUEL PRESSURE LOW LIGHT INDICATION. CREW ALS
- [SDR AALA20090417TUL03](https://openairdocs.org/sdr/AALA20090417TUL03), Jan 28, 2009: FITTING. CRACKED. RIGHT MAIN LANDING GEAR WHEEL WELL, BRACKET ABOVE DOOR ACTUATOR FITTING CRACKED AT RADIUS AFT INBOARD AREA. REPAIRED PER ESO 80559 DATED 1/26/09.
- [SDR AALA20071374](https://openairdocs.org/sdr/AALA20071374), Jul 30, 2007: WIRE HARNESS. INOPERATIVE. ORD INFLIGHT T346/30JUL - FORWARD CENTER FUEL BOOST PUMP CIRCUIT BREAKER TRIPPED AFTER TAKEOFF. UNABLE TO BURN CENTER FUEL. RETURNED TO ORD AND LANDED WITHOUT I
- [SDR AALA20040965](https://openairdocs.org/sdr/AALA20040965), Sep 18, 2004: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHTS AT L2 637 THROUGH 639 INOPERATIVE. REPLACED BATTERY PACK AT B528 FOR EMERGENCY LIGHTS AT L2 637 THROUGH 629. SYSTEM GROUND CHECKED NORMAL OPERA
- [SDR AALA20031472](https://openairdocs.org/sdr/AALA20031472), Dec 25, 2003: CHARGER. INOPERATIVE. CENTER SECTION OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED CENTER SECTION EMERGENCY LIGHT BATTERY CHARGER AND BATTERIES. SYSTEM GROUND CHECKED NORMAL OPERAT
- [SDR ZW0A0107002](https://openairdocs.org/sdr/ZW0A0107002), Aug 16, 2001: CSD. OVERTEMP. THE RH CSD OIL TEMP INCREASED. THE CSD WAS DISCONNECTED AND APU STARTED. SEVERAL MINUTES LATER THE FREQUENCY STARTED TO FLUCTUATE AND APU SPEED DROPPED. MADE UN
- [SDR ZW0A0106101](https://openairdocs.org/sdr/ZW0A0106101), Jul 29, 2001: ENGINE. FAILED. DURING CLIMB OUT NUMBER 2 ENGINE FAILED. CAUSE-UNKNOWN. CHANGED NUMBER 2 ENGINE. LAST CHECK C 012201 JFK ---OPEN---
- [SDR ZW0A0105302](https://openairdocs.org/sdr/ZW0A0105302), Jul 17, 2001: BLADE. FRACTURED. DURING CLIMB OUT NUMBER ONE ENGINE FAILED. FLIGHT RETURNED TO MIA FOUND TURBINE DAMAGE. CHANGED NUMBER ONE ENGINE. A FIRST STAGE TURBINE BLADE FRACTURED DUE TO 
- [SDR TWAA0103601](https://openairdocs.org/sdr/TWAA0103601), Feb 23, 2001: ELEVATOR. JAMMED. DURING FLIGHT CONTROL CHECK FOLLOWING FWD MOVEMENT OF ELEVATOR, SUBSEQUENT REARWARD MOVEMENT JAMMED CONTROL COLUMN IN NEUTRAL POSITION ONLY ALLOWING THE CONTROL
- [SDR TWAA0017401](https://openairdocs.org/sdr/TWAA0017401), Nov 8, 2000: LIGHT. INOPERATIVE. THE EGRESS LIGHTING WAS INOPERATIVE AT ROWS 29 AND 30. REPLACED THE LAMP AT BOTH LOCATIONS. CHECK-C 3-21-00 MCI.
- [SDR TWAA0004301](https://openairdocs.org/sdr/TWAA0004301), Mar 14, 2000: CARGO TRACK. CORRODED. DURING CHECK-C MAINT, THE AFT CARGO BIN CARGO TIE DOWN TRACK, LT SIDE STA 1081 TO 1318, HAD CORROSION IN NUMEROUS PLACES. REMOVED CORRODED TRACK FROM STA 1081 T
- [SDR TWAA0004225](https://openairdocs.org/sdr/TWAA0004225), Mar 13, 2000: PAN. CRACKED. DURING CHECK-C MAINT, THE MID CARGO DOOR INNER PAN WAS CRACKED ABOVE THE FWD LATCH CUTOUT. FABRICATED AND INSTALLED REPAIR PER ARA 16541-A.
- [SDR TWAA0004224](https://openairdocs.org/sdr/TWAA0004224), Mar 12, 2000: PAN. CRACKED. DURING CHECK-C MAINT, THE UPPER INNER DOOR PAN ON THE C3 CARGO DOOR HAD CRACKS AND WEAR DAMAGE. REPLACED PAN PER DOUGLAS DRAWING 5910141 AND SPM 6-70-01 PARA 4 
- [SDR TWAA0004223](https://openairdocs.org/sdr/TWAA0004223), Mar 10, 2000: ANGLE. CORRODED. DURING CHECK-C MAINT, THE AFT CARGO BIN ATTACH ANGLE ON FRAME AT STA 1148 O/B OF LONGERON 30, RBL 6 IN, WAS CORRODED. FABRICATED NEW ATTACH ANGLE AND INSTALLED 
- [SDR TWAA0004222](https://openairdocs.org/sdr/TWAA0004222), Mar 10, 2000: CARGO TRACK. CORRODED. DURING CHECK-C MAINT, THE CARGO TIE DOWN TRACK HAD CORROSION IN NUMEROUS PLACES RT SIDE AFT TRACK FRONT STA 1212 TO 1318. REMOVED CORRODED TRACK AND REPLACED WI
- [SDR TWAA0004221](https://openairdocs.org/sdr/TWAA0004221), Mar 10, 2000: CARGO TRACK. CORRODED. DURING CHECK-C MAINT, THE AFT CARGO BIN FLOOR FITTING WAS CORRODED AT STA 1150, ABOVE STRINGER 29R. REMOVED CORRODED FLOOR FITTING AND INSTALLED NEW FLOOR FITTI
- [SDR TWAA0004220](https://openairdocs.org/sdr/TWAA0004220), Mar 9, 2000: FRAME. CORRODED. DURING CHECK-C MAINT, FOUND CORROSION ON FRAME AT STA 1306, FROM LONGERON 30 TO 29R. REPLACED CORRODED FRAME PER SRM 53-03 FIG 2A, SHEET 1 TO 5.
- [SDR TWAA0004219](https://openairdocs.org/sdr/TWAA0004219), Mar 9, 2000: DOOR FRAME. CORRODED. DURING CHECK-C MAINT, THE AFT CARGO COMPT LOWER AFT CARGO DOOR JAMB HAD NUMEROUS CORRODED INSERTS. REMOVED CORROSION PER TWA SPM 6-80-01 PAGE 1-2. REPLACED BEAM
- [SDR TWAA0003920](https://openairdocs.org/sdr/TWAA0003920), Mar 3, 2000: FLOORBEAM. CORRODED. DURING CHECK-C MAINT, FOUND CORROSION ON CABIN MEMBRANE AREA, LONGERON 18R, FROM STA 1174 TO 1193. REPLACED WEB PN 9930612-21 PER SPM 6-70-01 AND SSRM 53-10-111
- [SDR TWAA0003919](https://openairdocs.org/sdr/TWAA0003919), Mar 3, 2000: FLOORBEAM. CORRODED. DURING CHECK-C MAINT, FOUND CORROSION ON CABIN MEMBRANE AREA, LONGERON 18R FROM STA 1193 TO 1212. REPLACED MEMBRANE PER SSRM 53-10-111. PAINTED PER SRM 51-10-03
- [SDR TWAA0003924](https://openairdocs.org/sdr/TWAA0003924), Mar 2, 2000: FLOORBEAM. CORRODED. DURING CHECK-C MAINT, FOUND CORROSION ON CABIN MEMBRANE AREA AT LONGERON 18R, STA 1098 TO 1117. REPLACED MEMBRANE PER SPM 6-70-01, PAGE 3, AND DOUGLAS DRAWING 9
- [SDR TWAA0003923](https://openairdocs.org/sdr/TWAA0003923), Mar 2, 2000: FLOORBEAM. CORRODED. DURING CHECK-C MAINT, FOUND CORROSION ON CABIN MEMBRANE AREA, LONGERON 18R, FROM STA 1117 TO 1136. REPLACED MEMBRANE PER SPM 6-70-01, PAGE 3, AND DOUGLAS DRAWIN
- [SDR TWAA0003922](https://openairdocs.org/sdr/TWAA0003922), Mar 2, 2000: FLOORBEAM. CORRODED. DURING CHECK-C MAINT, FOUND CORROSION ON CABIN MEMBRANE AREA LONGERON 18R, FROM STA 1136 TO 1155. REPLACED MEMBRANE PER SPM 6-70-01, PAGE 3, AND DOUGLAS DRAWING
- [SDR TWAA0003921](https://openairdocs.org/sdr/TWAA0003921), Mar 2, 2000: FLOORBEAM. CORRODED. DURING CHECK-C MAINT, CORROSION WAS FOUND ON CABIN MEMBRANE AREA, LONGERON 18R FROM STA 1155 TO 1174. REPLACED MEMBRANE PER SPM 6-70-01, PAGE 3, AND DOUGLAS DRA
- [SDR TWAA0003808](https://openairdocs.org/sdr/TWAA0003808), Feb 29, 2000: GALLEY TRACK. CRACKED. DURING CHECK-C MAINT, NR 4 GALLEY TIE DOWN TRACK HAD A CRACK FWD INBD TRACK TIE DOWN STA 1174 LEFT. REPLACED SEAT TRACK PER SPM 6-70-01, PAGE 2 AND 3. INSTALLED
- [SDR TWAA0003807](https://openairdocs.org/sdr/TWAA0003807), Feb 29, 2000: GALLEY TRACK. CORRODED. DURING CHECK-C MAINT, NUMBER 3 GALLEY TIE DOWN TRACK HAD CORROSION ON INBD TRACK, STA 1117 TO 1155. REPLACED TRACK USING TWA PART 16-0794 PER SPM 6-70-01, PAGE 
- [SDR TWAA0003806](https://openairdocs.org/sdr/TWAA0003806), Feb 28, 2000: GALLEY TRACK. CORRODED. DURING CHECK-C MAINT, THE NUMBER 4 GALLEY TIE DOWN AREA TRACK HAD CORROSION ON THE OTBD TRACK, FWD AND AFT, STA 1155 TO 1193. REPLACED TRACK PER SRM 53-05, PAGE
- [SDR TWAA0003805](https://openairdocs.org/sdr/TWAA0003805), Feb 28, 2000: GALLEY TRACK. CORRODED. DURING CHECK-C MAINT, THE NUMBER 3 GALLEY TIE DOWN TRACK AREA HAD CORROSION ON OTBD TRACK, FWD AND AFT OF STA 1117 TO 1155. REPLACED TRACK PER SRM 53-05, PAGE 1

All 71: https://openairdocs.org/deregistered/N9406W-2019-01-10/reports.md

## 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 20010717020489I](https://openairdocs.org/incident/20010717020489I), Jul 17, 2001: Doug DC983 (N9406W), Miami, FL. (.19) On July 17, 2001, about 1413 eastern daylight time, a Mcdonnell Douglas MD-83, N9406W, operated by trans world airlines inc., operating as a title 14 CFR…

## Other aircraft with N9406W

- [Cancelled (date not recorded)](https://openairdocs.org/deregistered/N9406W-undated): Piper PA-28-235, S/N 2811112. Triennial form not returned

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