# N413QX: 2002 Bombardier DHC-8-402, registration cancelled 2019-09-26

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: September 26, 2019
- Status when cancelled: Valid registration
- Airframe: [Bombardier DHC-8-402](https://openairdocs.org/model/bombardier-dhc-8-402) (registry code 1390042)
- Engine: [Pratt & Whitney Canada PW150A](https://openairdocs.org/engine/pratt-whitney-canada-pw150a) (registry code 52167)
- Data sheets: [TCDS A13NM](https://openairdocs.org/tcds/A13NM), [TCDS E00062EN](https://openairdocs.org/tcds/E00062EN) (OpenAirDocs)
- Serial number: 4060
- Year built: 2002
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: February 1, 2002
- Certificate issued: February 22, 2002
- Last registry action: March 4, 2019
- Mode S code: A4E0B9
- Owner when cancelled: [Wells Fargo Trust Co Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20TRUST%20CO%20NA%20TRUSTEE)
- Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City)
- Owner type: Corporation
- Owner's area on the map: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N413QX
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=413QX
- Page: https://openairdocs.org/deregistered/N413QX-2019-09-26

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 Bombardier DHC-8-402: https://openairdocs.org/model/bombardier-dhc-8-402.md

## Service difficulty reports (529, newest 50)

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

- [SDR QXEA2018042600162](https://openairdocs.org/sdr/QXEA2018042600162), Apr 25, 2018: PLUNGER. DIRTY. LANDING GEAR ALT EXTENSION ACCESS DOOR ON FLT DECK FLOOR IS DIFFICULT TO OPERATE. REMOVED FROM SERVICE. CLEANED LANDING GEAR ALTERNATE SELECT VALVE PLUNGER SHAF
- [SDR QXEA2018033000126](https://openairdocs.org/sdr/QXEA2018033000126), Mar 29, 2018: LENS. LOOSE. EMERGENCY LIGHT LENS, ROW 2 FEEL OFF. INSPECTED & FOUND CEILING LIGHT LENS LOOSE. SECURED THE LENS IAW AMM 33-22-00-01, NO OTHER DEFECTS NOTED. RETURNED TO SERV
- [SDR QXEA2018011000022](https://openairdocs.org/sdr/QXEA2018011000022), Jan 19, 2018: SEAL. STICKING. AFT PASSENGER DOOR SEAL STICKS. REMOVED FROM SERVICE. COULD NOT SET AFT PAX DOOR SEAL TO ADJUST.R&R AFT PAX DOOR SEAL IAW 52-12-21-000-802 & 52-12-21-4000-802 1
- [SDR QXEA2018010400003](https://openairdocs.org/sdr/QXEA2018010400003), Jan 4, 2018: DOOR SEAL. LOOSE. CREW REPORTS AFT PAX DOOR HARD TO OPEN CLOSE DUE TO SEAL PINCHING. REMOVED FROM SERVICE. REMOVED & REPLACED AFT PAX DOOR SEAL IAW AMM TASK 52-12-21-000-802 & TA
- [SDR QXEA2017090700550](https://openairdocs.org/sdr/QXEA2017090700550), Sep 7, 2017: CONTROL UNIT. MALFUNCTIONED. ON TAXI OUT FOR TAKEOFF, THE NOSE STEERING CAUTION LIGHT ILLUMINATED. WE CONDUCTED THE APPLICABLE CHECKLISTS AND THE CAUTION LIGHT REMAINED ILLUMINATED. REMOVED
- [SDR QXEA2017082300533](https://openairdocs.org/sdr/QXEA2017082300533), Aug 22, 2017: ECU. MALFUNCTIONED. DURING INITIAL CLIMB, CABIN PACK HOT. RAN CHECKLIST, THEN AIRCRAFT WOULD NOT PRESSURIZE. RETURN TO FIELD. LANDING UNEVENTFUL. REMOVED FROM SERVICE. R & R THE EC
- [SDR QXEA2017072000482](https://openairdocs.org/sdr/QXEA2017072000482), Jul 18, 2017: ANGLE. CORRODED. FWD PAX DOOR AFT OTBD ANGLE SHOWS EVIDENCE OF CORROSION. REMOVED AND DISCARDED AFT OTBD ANGLE IAW SRM 51-41-05. INSTALLED A NEW AFT OTBD ANGLE IAW DWG 85217008,
- [SDR QXEA2017072000481](https://openairdocs.org/sdr/QXEA2017072000481), Jul 18, 2017: ANGLE. CORRODED. FWD PAX DOOR FWD OUTBOARD ANGLE SHOWS EVIDENCE OF CORROSION. REMOVED AND DISCARDED FWD OTBD ANGLE IAW SRM 51-41-05. INSTALLED A NEW FWD OTBD ANGLE IAW DWG 85217
- [SDR QXEA2017072000480](https://openairdocs.org/sdr/QXEA2017072000480), Jul 18, 2017: ANGLE. CORRODED. FWD PAX DOOR AFT INBD ANGLE SHOWS EVIDENCE OF CORROSION. REMOVED AND DISCARDED AFT INBD ANGLE IAW SRM 51-41-05. INSTALLED A NEW AFT INBD ANGLE IAW DWG 85217008,
- [SDR QXEA2017072000479](https://openairdocs.org/sdr/QXEA2017072000479), Jul 18, 2017: ANGLE. CORRODED. FWD PAX DOOR INBD ANGLE SHOWS EVIDENCE OF CORROSION. REMOVED AND DISCARDED FWD INBD ANGLE IAW SRM 51-45-05. INSTALLED A NEW FWD INBD ANGLE IAW DWG 85217008, REV
- [SDR QXEA2017072000484](https://openairdocs.org/sdr/QXEA2017072000484), Jul 17, 2017: SUPPORT CHANNEL. CORRODED. FOUND CORROSION ON THRESHOLD SUPPORT CHANNEL. BLENDED DAMAGE AREAS ON THRESHOLD CHANNEL REF SRM 53-20-23 REPAIR-01. REMAINING THICKNESS AFTER BLEND 0.033 FOUND 
- [SDR QXEA2017072000483](https://openairdocs.org/sdr/QXEA2017072000483), Jul 16, 2017: FITTING. CORRODED. LEFT NACELLE EMS STRUT A3 ATTACHMENT FITTINGS HAS EVIDENCE OF CORROSION ON THE FWD ATTACHMENT FITTING (IB) AND AFT ATTACHMENT (IB & OB). REMOVED LIGHT SURFACE C
- [SDR QXEA2017080100503](https://openairdocs.org/sdr/QXEA2017080100503), Jul 2, 2017: SEAT TRACK. DAMAGED. SEAT TRACK 11 (PN 85328210-115) REQUIRES REPLACEMENT. REMOVED SEAT TRACK 11 PN: 85328210-115 REF SRM 51-41-00-00-01. INSTALLED BOLTS ON NEW SEAT TRACK 11 AT STA
- [SDR QXEA2017072000478](https://openairdocs.org/sdr/QXEA2017072000478), Jun 29, 2017: SEAT TRACK. DAMAGED. SEAT TRACK NR 8 DAMAGED. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-40-07, SRM 51-42-05, & 51-40-015.
- [SDR QXEA2017072000477](https://openairdocs.org/sdr/QXEA2017072000477), Jun 28, 2017: SEAT TRACK. DAMAGED. SEAT TRACK 15 DAMAGED. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-40-07-02-01, SRM 51-41-00-00-01, AND 51-42-05-02-01.
- [SDR QXEA2016092900623](https://openairdocs.org/sdr/QXEA2016092900623), Sep 27, 2016: LAMP. INOPERATIVE. GREEN NORMAL LIGHT ON THE MAIN CABIN DOOR EMERGENCY LIGHT SWITCH NOT ILLUMINATED. REPLACED THE LAMP NORMAL LIGHT SWITCH. OPERATES NORMALLY. RETURNED TO SERVICE.
- [SDR QXEA2016062400408](https://openairdocs.org/sdr/QXEA2016062400408), Jun 24, 2016: BATTERY PACK. FAILED. EMERGENCY LIGHTS NR 3 CHARGER FAILED 10 MINUTE CHECK. REPLACED BATTERY PACK.
- [SDR QXEA2015121500650](https://openairdocs.org/sdr/QXEA2015121500650), Dec 15, 2015: SIGN. LOOSE. EMERGENCY EXIT SIGN AT EMERGENCY EXIT, PLASTIC COVER FELL OFF. REINSTALLED COVER.
- [SDR QXEA2015121000645](https://openairdocs.org/sdr/QXEA2015121000645), Dec 10, 2015: PUMP. FAILED. DURING DESCENT BEFORE GEAR EXTENSION, EXPERIENCED NR 2 HYD ISOLATION VALVE CAUTION WHILE RUNNING THE CHECKLIST NOTED 15 PERCENT NR 2 HYD QTY REMAINING. ACCOMPLI
- [SDR QXEA2015111200588](https://openairdocs.org/sdr/QXEA2015111200588), Nov 12, 2015: SWITCH. BROKEN. FORWARD F/A EMERGENCY LIGHT SWITCH GUARD BROKEN. REPLACED SWITCH AND GUARD. RETURNED TO SERVICE.
- [SDR QXEA2015082900443](https://openairdocs.org/sdr/QXEA2015082900443), Aug 29, 2015: TRANSCEIVER. MALFUNCTIONED. WX RADAR TOOK SEVERAL ATTEMPTS TURNING OFF THEN ON TO WORK. THEN WORKED INTERMITTENTLY. DIVERTED AND ACCOMPLISHED A UNEVENTFUL LANDING. R & R WR TRANCEIVER REF 
- [SDR QXEA2015081200425](https://openairdocs.org/sdr/QXEA2015081200425), Aug 11, 2015: SKIN. DENTED. NINE DENTS ON RT FUSELAGE SKIN BETWEEN BS 291 - 321 AND STRINGERS 17 - 23R. FABRICATED A REPAIR DOUBLER IAW RD8/4-53-6983 AND INSTALLED IAW TC RD8/4-53-6983/3 I
- [SDR QXEA2015081100424](https://openairdocs.org/sdr/QXEA2015081100424), Aug 6, 2015: SKIN. DENTED. DENT ON RT FUSELAGE AT FS -37, STR 14-15. DENT IS WITHIN LIMITS IAW SRM 53-00-00, REPAIR -02.
- [SDR QXEA2015081100423](https://openairdocs.org/sdr/QXEA2015081100423), Aug 6, 2015: SKIN. GOUGED. DENT AND GOUGE AT FRAME, BS-34 RT STR 18-19. DENT IS WITHIN LIMITS IAW SRM 53-00-00, REPAIR-02. BLENDED DENT TO REMOVE GOUGE IAW SRM 53-00-00, REPAIR-02, PROCED
- [SDR QXEA2015081100422](https://openairdocs.org/sdr/QXEA2015081100422), Aug 6, 2015: SKIN. DENTED. DENT ON RT FUSELAGE AT FRAME STA -100, STR 28-29. C/W ET INSP ON DENT AS MARKED, REF NDTM PT1 51-00-06. ITEM 1, CORRECTIVE ACTION ABOVE. DENT MEASURES .70"L X .
- [SDR QXEA2015081100421](https://openairdocs.org/sdr/QXEA2015081100421), Aug 6, 2015: PANEL. CRACKED. AFT CEILING PANEL 245EZ HAS A CRACK ON CLOSE OUT SHROUD, MARKED. REPAIRED CLOSE-OUT SHROUD ON PANEL 245EZ IAW CDP002-07-06 MANUAL, REV:N/C 3/18/02, PAGE 15, SEC
- [SDR QXEA2015081100420](https://openairdocs.org/sdr/QXEA2015081100420), Aug 5, 2015: SKIN. DENTED. ONE DENT ON LT FUSELAGE SKIN BETWEEN STR 4P-5P AT FSX 307.00. RECIEVED RD NR 8/4-53-6987 ISSUE 1, DATED 28 JULY 2015. RECEIVED TASK CARD RD8/4-53-6987/3, W/O 18
- [SDR QXEA2015080400415](https://openairdocs.org/sdr/QXEA2015080400415), Aug 2, 2015: BEAM. CORRODED. FWD BAGGAGE DOOR OUTER EDGE BEAM, PN 85329604-001 IS CORRODED. CORROSION EVALUATION IS NOT REQUIRED. NO CORROSION IS ALLOWED IAW SRM 53-20-25. COMPLIED WITH FOR
- [SDR QXEA2015080400414](https://openairdocs.org/sdr/QXEA2015080400414), Aug 2, 2015: BEAM. CORRODED. FWD BAGGAGE DOOR INNER EDGE BEAM, PN 85329603-103 IS CORRODED. CORROSION EVALUATION IS NOT REQUIRED. NO CORROSION IS ALLOWED IAW SRM 53-20-25. COMPLIED WITH FOR
- [SDR QXEA2015073100408](https://openairdocs.org/sdr/QXEA2015073100408), Jul 29, 2015: SEAT TRACK. NOT REPORTED. SEAT TRACK NR 11 REPLACEMENT REQUIRED. INSTALLED A NEW SEAT TRACK IAW SRM 51-41-00 AND SRM 51-40-15, STEP 6, H.
- [SDR QXEA2015073100407](https://openairdocs.org/sdr/QXEA2015073100407), Jul 29, 2015: SEAT TRACK. NOT REPORTED. SEAT TRACK NR 10, REPLACEMENT REQUIRED. INSTALLED A NEW SEAT TRACK IAW SRM 51-41-00 AND SRM 51-40-15, STEP 6, H.
- [SDR QXEA2015072900404](https://openairdocs.org/sdr/QXEA2015072900404), Jul 27, 2015: THRESHOLD. CORRODED. MAIN DECK THRESHOLD PLATE FOUND CORRODED. LOCATED AND DRILLED A NEW THRESHOLD PLATE IAW SRM 51-40-07. INSTALLED THE NEW THRESHOLD PLATE IAW SRM 51-42-05, REPAIR
- [SDR QXEA2015072900403](https://openairdocs.org/sdr/QXEA2015072900403), Jul 27, 2015: THRESHOLD. CORRODED. MAIN DECK THRESHOLD, FOUND CORRODED. REMOVED THE THRESHOLD IAW SRM 51-42-05. LOCATED AND DRILLED A NEW THRESHOLD IAW SRM 51-40-07. INSTALLED A NEW THRESHOLD IAW
- [SDR QXEA2015072900406](https://openairdocs.org/sdr/QXEA2015072900406), Jul 26, 2015: ANGLE. CORRODED. MAIN DECK INTERCOSTAL ANGLE AT X 26.7 FOUND CORRODED. REMOVED THE INTERCOSTAL ANGLE IAW SRM 51-42-05. LOCATED AND DRILLED A NEW INTERCOSTAL ANGLE IAW SRM 51-40-
- [SDR QXEA2015072900405](https://openairdocs.org/sdr/QXEA2015072900405), Jul 25, 2015: ANGLE. CORRODED. MAIN DECK INTERCOSTAL ANGLE AT X 6.7 FOUND CORRODED. REMOVED THE INTERCOSTAL ANGLE IAW SRM 51-42-05. LOCATED AND DRILLED A NEW INTERCOSTAL ANGLE IAW SRM 51-40-0
- [SDR QXEA201507290045](https://openairdocs.org/sdr/QXEA201507290045), Jul 25, 2015: ANGLE. CORRODED. MAIN DECK INTERCOSTAL ANGLE AT FS 6.7 FOUND CORRODED. REMOVED THE INTERCOSTAL ANGLE IAW SRM 51-42-05. LOCATED AND DRILLED THE NEW INTERCOSTAL ANGLE IAW SRM 51-4
- [SDR QXEA2015072900402](https://openairdocs.org/sdr/QXEA2015072900402), Jul 22, 2015: SEAT TRACK. NOT REPORTED. SEAT TRACK NR 8, NEEDS REPLACEMENT. REMOVED THE SEAT TRACK IAW SRM 51-42-05-02-01 AND SRM 51-40-15-02-01 AND SRM 51-41-00-00-01. LOCATED AND DRILLED THE NEW SEA
- [SDR QXEA2015071200382](https://openairdocs.org/sdr/QXEA2015071200382), Jul 12, 2015: LIGHT. FAILED. FORWARD TYPE II EMERGENCY EXIT DOOR FAILED THE BETA LIGHT CHECK. REPLACED THE BETA LIGHT IAW AMM 33-51-00-960-801. TESTS GOOD.
- [SDR QXEA2015071100386](https://openairdocs.org/sdr/QXEA2015071100386), Jul 11, 2015: SEAT BACK. LACK OF LUBE. ON TAKEOFF THE CAPTAIN'S SEAT BECAME UNLOCKED AND WENT TO FULLY RECLINED AND WOULD NOT ENGAGE. CLEANED AND LUBED THE SEAT BACK, ADJUSTMENT LINKAGE. NO DEFECTS N
- [SDR QXEA2015041500205](https://openairdocs.org/sdr/QXEA2015041500205), Apr 15, 2015: FAN. FAILED. AFTER ARRIVING AT GATE, NOTICED A STRONG ELECTRICAL BURNING ODOR AND COULD SEE A HAZE ORIGINATING POSSIBLY FROM F/O SIDE OF COCKPIT, IT LASTED 1 TO 2 MINUTES TH
- [SDR QXEA2015032500158](https://openairdocs.org/sdr/QXEA2015032500158), Mar 25, 2015: SIGN. UNSECURE. FORWARD EMERGENCY EXIT SIGN AT ROW 2-3 AT THE EMERGENCY EXIT DOOR CAME OFF. SECURED EXIT SIGN AT THE EMERGENCY EXIT DOOR. NO FURTHER DEFECTS. RETURNED TO SERVIC
- [SDR QXEA2015031700146](https://openairdocs.org/sdr/QXEA2015031700146), Mar 17, 2015: SEAL. LEAKING. FUEL LEAKING FROM INBD PORTION OF THE LT WING L/E. FERRIED ACFT FOR REPAIRS. REPLACED GASKETS AND SPINNING NUTPLATES FOR THE FUEL ACCESS PANELS 522BT AND 522CT.
- [SDR QXEA2015031400144](https://openairdocs.org/sdr/QXEA2015031400144), Mar 14, 2015: WARNING MESSAGE. ACTIVATED. ENCOUNTERED TURBULENCE DURING CLIMBOUT AND GOT A MASTER WARNING FUSELAGE DOORS INDICATION. CHECKLIST WAS RUN AN INITIALLY PRESSURIZATION INDICATED NORMAL FROM 7
- [SDR QXEA2015020600064](https://openairdocs.org/sdr/QXEA2015020600064), Feb 6, 2015: LIGHT. UNSECURE. EMERGENCY LIGHT STRIP BY MCD UNSECURE. SECURED THE LIGHT. RETURNED TO SERVICE.
- [SDR QXEA2015012600036](https://openairdocs.org/sdr/QXEA2015012600036), Jan 26, 2015: COVER. DETACHED. EMERGENCY EXIT LIGHT COVER AT ROW 2 HAS FALLEN OFF. RESECURED LENS COVER AT EMERGENCY EXIT. ILLUMINATION CHECKS GOOD. RETURNED TO SERVICE.
- [SDR QXEA2014112400923](https://openairdocs.org/sdr/QXEA2014112400923), Nov 24, 2014: UNKNOWN. ODOR. SULPHUR TYPE ODOR COMING FROM THE CABIN WHEN THE APU WAS STARTED. APU ALSO AUTO SHUTDOWN. ODOR WENT AWAY AFTER APU WAS SHUTDOWN. RETURNED TO SERVICE.
- [SDR QXEA2014091100776](https://openairdocs.org/sdr/QXEA2014091100776), Sep 11, 2014: LIGHT. MALFUNCTIONED. F/A'S REPORT UNUSUAL ODOR IN THE AFT GALLEY, STRONGEST ON LT SIDE NEAR AFT PAX DOOR. BOTH AFT DOORS WERE CLOSED AND AFT CARGO DOOR CLOSED WHEN ODOR WAS STRONGES
- [SDR QXEA2014071100574](https://openairdocs.org/sdr/QXEA2014071100574), Jul 11, 2014: LIGHT. INOPERATIVE. WITH AUTOFEATHER SELECT BUTTON PRESSED, THE "AF SELECT" DOES NOT APPEAR ON THE ED. FOUND FAULT CODE 494. C/W FIM 61-20-10-810-826 AND 61-20-00-810-805. AUTOFEAT
- [SDR QXEA2014040200286](https://openairdocs.org/sdr/QXEA2014040200286), Apr 2, 2014: LENS. BROKEN. FORWARD EMERGENCY EXIT SIGN LENS WILL NOT STAY ATTACHED, REPLACED THE LENS. RETURNED TO SERVICE.
- [SDR QXEA2014040200271](https://openairdocs.org/sdr/QXEA2014040200271), Apr 2, 2014: LENS. BROKEN. FORWARD EMERGENCY EXIT LENS COVER WILL NOT STAY ON. REPLACED THE LENS. NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE.

All 529: https://openairdocs.org/deregistered/N413QX-2019-09-26/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.

- [Accident 20120904020931A](https://openairdocs.org/incident/20120904020931A), Sep 4, 2012: Bombardier Inc DHC-8-402 (N413QX), Seattle, WA, Substantial damage. During push back operations N448QX and N413 qx sustained impact damage to to both ac's RH elevators.

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