# N406QX: 2001 Bombardier DHC-8-402, registration cancelled 2023-04-18

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: April 18, 2023
- Exported to: Canada
- 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: 4048
- Year built: 2001
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: April 26, 2005
- Certificate issued: September 11, 2020
- Last registry action: March 17, 2023
- Mode S code: A4C45F
- Owner when cancelled: [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%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/N406QX
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=406QX
- Page: https://openairdocs.org/deregistered/N406QX-2023-04-18

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 (532, newest 50)

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

- [SDR QXEA2017122700709](https://openairdocs.org/sdr/QXEA2017122700709), Dec 23, 2017: HANDLE. LACK OF LUBE. AFT GALLEY SERVICE DOOR WILL NOT OPEN FROM EXTERIOR, DIFFICULT TO UNLOCK FROM INSIDE. LUBED AFT SERVICE DOOR EXTERNAL HANDLE SHAFT IAW AMM TASK 12-20-01-640-811
- [SDR QXEA2017092900585](https://openairdocs.org/sdr/QXEA2017092900585), Sep 28, 2017: HANDLE. UNSECURE. MAIN CABIN DOOR WILL NOT OPEN FROM INSIDE OR OUTSIDE. FERRIED FOR REPAIRS. REMOVED FWD GALLEY INSERT AND CLOSET SIDEWALL , INSPECTED MCD OPEN - CLOSE MECHANISIM
- [SDR QXEA2017081500518](https://openairdocs.org/sdr/QXEA2017081500518), Aug 14, 2017: GENERATOR. MALFUNCTIONED. AFTER TAKEOFF, INTERMITTENT CAUTION LIGHT FLICKERED ON AND OFF. WOULDN'T STAY ON LONG ENOUGH TO IDENTIFY. FINALLY IDENTIFIED AS NR 2 DC GENERATOR. AND WOULD BRI
- [SDR QXEA2017061300415](https://openairdocs.org/sdr/QXEA2017061300415), Jun 11, 2017: LAMP. INOPERATIVE. FWD F/A'S EMERGENCY LIGHT SWITCH INOPERATIVE. REPLACED THE LAMP.
- [SDR QXEA2017061400420](https://openairdocs.org/sdr/QXEA2017061400420), Jun 10, 2017: SKIN. DAMAGED. LEFT WING OTBD FLAP TRAILING EDGE METAL PEELING BACK AND SECTION MISSING. REMOVED DAMAGED SKIN, COMPLIED WITH RD/8-4-51-475, NO OTHER DAMAGE NOTED.
- [SDR QXEA2017042100316](https://openairdocs.org/sdr/QXEA2017042100316), Apr 4, 2017: BRACKET. CORRODED. AFT ENTRY DOOR NR 2 BEAM FOUND CRACKED BETWEEN CENTER SUPPORT. LOCATED, & DRILLED NEW BEAM IAW SRM 51-40-07. APPLIED CORROSION INHIBITING COMPOUND TO INNER STRU
- [SDR QXEA2017042100318](https://openairdocs.org/sdr/QXEA2017042100318), Apr 2, 2017: SEAT TRACK. CORRODED. SEAT TRACK DAMAGED. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-40-15, SRM 51-40-07, SRM 51-40-07, SRM 51-40-07-02-01, SRM 51-42-05-02-01, 51-41-00-00-01 & D
- [SDR QXEA2017042100320](https://openairdocs.org/sdr/QXEA2017042100320), Apr 1, 2017: SEAT TRACK. CORRODED. SEAT TRACK CORRODED. REMOVED THE DAMAGED SEAT TRACK IAW SRM 51-42-05 & 51-40-15. LOCATED & DRILLED A NEW SEAT TRACK IAW SRM 51-40-07-02-01, AND INSTALLED IAW SR
- [SDR QXEA2017042100319](https://openairdocs.org/sdr/QXEA2017042100319), Mar 31, 2017: SEAT TRACK. CORRODED. SEAT TRACK CORRODED. REMOVED AND REPLACED THE SEAT TRACK ANGLE IAW SRM 51-42-05, LOCATED A NEW SEAT TRACK IAW SRM 51-40-07 AND INSTALLED THE SEAT TRACK IAW SRM 
- [SDR QXEA2017042100317](https://openairdocs.org/sdr/QXEA2017042100317), Mar 31, 2017: SEAT TRACK. CORRODED. SEAT TRACK 16 CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-42-005 REPAIR -01 & 51-40-15. DRILLING NEW SEAT TRACK IAW SRM 51-40-07-02-01 & DWG 853382
- [SDR QXEA2017042100321](https://openairdocs.org/sdr/QXEA2017042100321), Mar 29, 2017: THRESHOLD. CORRODED. FWD PAX DOOR THRESHOLD MEMBER CORRODED. THE THRESHOLD WAS REMOVED IAW SRM 51-42-05. A NEW FWD THRESHOLD LOCATED AND DRILLED IAW SRM 51-40-09. A NEW DOOR THRESHO
- [SDR QXEA2017030800109](https://openairdocs.org/sdr/QXEA2017030800109), Mar 7, 2017: BOOT. MALFUNCTIONED. DE-ICE PRESSURE CAUTION LIGHT SEGMENT ON RT OUTBOARD TAIL DID NOT ILLUMINATE 21 PSI, 70% TORQUE, BOOT AIR NORM. REMOVED AND REPLACED VERTICAL LEADING EDGE IAW A
- [SDR QXEA2017012300020](https://openairdocs.org/sdr/QXEA2017012300020), Jan 20, 2017: REPAIR. UNSECURE. ON FINAL, FO NOTICED THE RIGHT WING PATCH ON THE BOOT WAS FLAPPING IN THE WIND AND SHOWING RED LINING UNDERNEATH. REMOVED AND REPLACED OUTER WING LEADING EDGE 6
- [SDR QXEA2017012300019](https://openairdocs.org/sdr/QXEA2017012300019), Jan 18, 2017: GOVERNOR. MALFUNCTIONED. NR 2 PROPELLER NOT COMPLETELY FEATHERING ON SHUTDOWN. CHECKED CDS. NO FAULT CODES PRESENT. REMOVED AND REPLACED NR 2 PROP OSG IAW AMM TASK 61-20-26-000-801 AND 
- [SDR QXEA2016112100733](https://openairdocs.org/sdr/QXEA2016112100733), Nov 19, 2016: WIRE. CHAFED. FIRE DETECTION WARNING WITHOUT BELL OR EVIDENCE OF FIRE ON THE T HANDLES. NR 2 ENGINE FIRE DETECT FAULT LIGHT A&B ILLUMINATED AND CIRCUIT BREAKER J7 POPPED. FOU
- [SDR QXEA2016102400675](https://openairdocs.org/sdr/QXEA2016102400675), Oct 24, 2016: SEAL. LOOSE. DITCHING DAM SEAL ON MAIN CABIN DOOR IS LOOSE. SECURED THE SEAL. NO DEFECTS NOTED. RETURNED TO SERVICE.
- [SDR QXEA2016090300566](https://openairdocs.org/sdr/QXEA2016090300566), Sep 3, 2016: LAMP. INOPERATIVE. F/A FORWARD EMERGENCY LIGHT SWITCH, GREEN LIGHT INOPERATIVE. REPLACED THE LAMP. CHECKED GOOD. RETURNED TO SERVICE.
- [SDR QXEA2016072200461](https://openairdocs.org/sdr/QXEA2016072200461), Jul 22, 2016: ESCAPE ROPE. UNSECURE. EMERGENCY ROPE PROTRUDING FROM THE DITCHING DAM ON THE RIGHT FORWARD EMERGENCY EXIT DOOR. SECURED THE ROPE. NO DEFECTS NOTED. RETURNED TO SERVICE.
- [SDR QXEA2016071300451](https://openairdocs.org/sdr/QXEA2016071300451), Jul 13, 2016: PROXIMITY SENSOR. FAULTED. RIGHT MAIN GEAR LIGHT ILLUMINATED, RIGHT GEAR DOOR REMAINS OPEN. FOUND FAULT PROXIMITY SENSOR. REPLACED THE PROXIMITY SENSOR. RETURNED TO SERVICE.
- [SDR QXEA2016061900405](https://openairdocs.org/sdr/QXEA2016061900405), Jun 19, 2016: ACTUATOR. FAILED. AFTER TAKEOFF THE NR 1 ENGINE OIL TEMP CLIMBED TO 114 DEGREES FOR 2 MINUTES. ALL OTHER PARAMETERS NORMAL. OPS CHECK OF OIL COOLER DOOR ACTUATOR FAILED TO OPEN. 
- [SDR QXEA2016061700404](https://openairdocs.org/sdr/QXEA2016061700404), Jun 17, 2016: WIRE HARNESS. UNSECURE. WIRE BUNDLE HANGING DOWN ABOVE CAPTAIN'S RT RUDDER PEDAL, AFFECTS USE OF PEDALS. ADJUSTED THE HARNESS, OPERATED THE RUDDER PEDALS THROUGH FULL MOVEMENT, NO DEFE
- [SDR QXEA2016042000273](https://openairdocs.org/sdr/QXEA2016042000273), Apr 20, 2016: GCU. MALFUNCTIONED. 2 AC GENERATOR CAUTION LIGHT ILLUMINATED AFTER TAKEOFF. CHECKLIST DONE + NR 2 AC GENERATOR CYCLED. NR 2 AC GENERATOR WOULD NOT RESET. RETURNED TO FIELD. LANDING
- [SDR QXEA2016022000148](https://openairdocs.org/sdr/QXEA2016022000148), Feb 20, 2016: LIGHT. LOOSE. EMERGENCY LIGHTING STRIP AT MAIN CABIN DOOR CAME OFF. SECURED FLOOR PATH LIGHTING STRIP. RETURNED TO SERVICE.
- [SDR QXEA2015081500431](https://openairdocs.org/sdr/QXEA2015081500431), Aug 15, 2015: BATTERY PACK. FAILED. CEILING LIGHT FOR EMERGENCY LIGHTS AT ROW 2 AND 5 FAILED OPS TEST. REMOVED CEILING PANEL AT ROW 2 AND 5 IAW AMM TASK 25-27-01-000-801. NO DEFECTS NOTED. R & R E
- [SDR QXEA2015062700344](https://openairdocs.org/sdr/QXEA2015062700344), Jun 27, 2015: PROXIMITY SENSOR. OUT OF ADJUST. CLIMBING OUT, FORWARD CARGO DOOR MASTER WARNING FUSELAGE DOOR, IT WOULD CONTINUE TO COME ON AND TURN OFF THEN STAYED ON. PRESSURIZATION NORMAL. RETURNED TO FIEL
- [SDR QXEA2015040600176](https://openairdocs.org/sdr/QXEA2015040600176), Apr 2, 2015: SKIN. SCRATCHED. LEFT OTBD FLAP BELOW INBD ACTUATOR HAS 4" SCRATCH. REMOVED SCRATCH MARKS IAW SRM 51-14-00-02-03. C/W ET INSP + UT THICK TEST ON AREA REF NDTM PT1 51-00-06 & 51-
- [SDR QXEA2015040600181](https://openairdocs.org/sdr/QXEA2015040600181), Apr 1, 2015: SEAT TRACK. UNKNOWN. SEAT TRACK NR 2 REQUIRES REPLACEMENT. REMOVED SEAT TRACK NR 2, PN:85361561-103, REF SRM 51-42-05, REPAIR -01 AND 51-40-15, REPAIR -01. LOCATED AND DRILLED NEW S
- [SDR QXEA2015040600180](https://openairdocs.org/sdr/QXEA2015040600180), Apr 1, 2015: SEAT TRACK. UNKNOWN. SEAT TRACK, NR 11 REQUIRES REPLACEMENT. REMOVED SEAT TRACK SPLICE AT FS X102.5 COMMON TO SEAT TRACK 11 AND 12 IAW SRM'S 51-40-15, PAR 6M, 51-42-05, PAR 4E. INST
- [SDR QXEA2015040600175](https://openairdocs.org/sdr/QXEA2015040600175), Apr 1, 2015: DOOR SILL. CORRODED. FORWARD BAGGAGE DOOR LOWER SILL SURFACE CORROSION ON OUTER EDGE BEAM. REMOVED THRESHOLD PLATE, PN:85329610, REF SRM 51-41-00. INSTALLED THRESHOLD PLATE COMMON T
- [SDR QXEA2015040600179](https://openairdocs.org/sdr/QXEA2015040600179), Mar 31, 2015: DOUBLER. CORRODED. FOUND CORROSION ON LAV SERVICE PORT INTERNAL DOUBLER, PN 85307789-101 AT AFT LOWER CORNER. BLENDED DAMAGE AREA REF SRM 52-42-10, REPAIR-01. C/W ET INSP & UT THI
- [SDR QXEA2015040200169](https://openairdocs.org/sdr/QXEA2015040200169), Mar 29, 2015: PLATE. CORRODED. FWD LAVATORY SERVICE DOOR ADAPTOR PLATE PN 85307781-105 CORRODED. REMOVED CORROSION ON ADAPTOR PLATE, PN: 85307781-105 OF FWD LAVATORY SERVICE DOOR IAW SRM 51-2
- [SDR QXEA2015040200165](https://openairdocs.org/sdr/QXEA2015040200165), Mar 29, 2015: SEAT TRACK. UNKNOWN. SEAT TRACK NR 19 REQUIRES REPLACEMENT. REMOVED FWD SPLICE COMMON TO SEAT TRACK NR 18 AND NR 19 REF SRM 51-40-15 AND SRM 51-42-05. INSTALLED FWD SPLICE COMMON TO
- [SDR QXEA2015040600174](https://openairdocs.org/sdr/QXEA2015040600174), Mar 27, 2015: WEB. CRACKED. WEB CRACKED, LOCATED BETWEEN FS X341.00 AND X361.00 AT STR 23S. REMOVED INTERCOSTAL PN 85361567-102-9 CRACKED WEB, BETWEEN FSX 341.00 AND X 361.00 AT STR 235, R
- [SDR QXEA2015040200162](https://openairdocs.org/sdr/QXEA2015040200162), Mar 25, 2015: SEAT TRACK. UNKNOWN. SEAT TRACK NR 7 REQUIRES REPLACEMENT. REMOVED FWD SEAT TRACK SPLICE COMMON TO TRACK NR 6 & NR 7 FOM REF SRM 51-42-05, 51-40-15. INSTALLED FWD SEAT TRACK SPLICE 
- [SDR QXEA2015040200161](https://openairdocs.org/sdr/QXEA2015040200161), Mar 24, 2015: SEAT TRACK. UNKNOWN. SEAT TRACK, NR 10 REQUIRES REPLACEMENT. SEAT TRACK, NR 10 REMOVED IAW SRM 51-42-05 STEP 4E, 51-41-00, 51-40-15. SEAT TRACK, NR 10 INSTALLED IAW SRM 51-40-07, 51
- [SDR QXEA2015040200164](https://openairdocs.org/sdr/QXEA2015040200164), Mar 23, 2015: THRESHOLD. CORRODED. CORROSION ON FWD PAX DOOR THRESHOLD PLATE. REMOVED CORRODED THRESHOLD PLATE, PN 85329539-105, REF SRM 51-42-05-02-01-4 (E). INSTALLED NEW THRESHOLD PLATE, PN 85
- [SDR QXEA2015040200166](https://openairdocs.org/sdr/QXEA2015040200166), Mar 21, 2015: BEAM. CORRODED. FWD BAGGAGE DOOR SURROUND HAS SURFACE CORROSION ON INNER EDGE BEAM. REMOVED FWD SPLICE COMMON TO SEAT TRACK NR 18 AND NR 19 REF SRM 51-40-15 AND SRM 51-42-05. I
- [SDR QXEA2015040200167](https://openairdocs.org/sdr/QXEA2015040200167), Mar 18, 2015: BEAM. CORRODED. AFT PAX DOOR SURROUND STRUCTURE HAS OUTER EDGE BEAM CORRODED, PN 85339542-101. REMOVED OUTER EDGE BEAM, PN 85339542-101, REF SRM 51-42-05-02-01 STEP 4E. LOCATED
- [SDR QXEA2015040200163](https://openairdocs.org/sdr/QXEA2015040200163), Mar 18, 2015: BEAM. CORRODED. EDGE BEAM, PN 85339512-101, CORRODED TO LIMITS. REMOVE DAMAGED EDGE BEAM, INNER, PN:85339512-11, REF SRM 51-42-05, PARA E, 1-8 AND 51-42-45, PARA H, 1 AND 2. RE
- [SDR QXEA2015040600177](https://openairdocs.org/sdr/QXEA2015040600177), Mar 15, 2015: SKIN. CORRODED. LT FUSELAGE INNER SKIN HAS CORROSION AT AFT PAX DOOR CUTOUT BETWEEN STA X669.3 TO STA 697.6. REMOVED 4 NUTPLATES FOR ACCESS REF SRM 51-42-05 STEP 4E. INSTALLED 
- [SDR QXEA2015031700143](https://openairdocs.org/sdr/QXEA2015031700143), Mar 15, 2015: RIB. CORRODED. AFT PAX DOOR SURROUND STRUCTURE HAS RIB CORRODED AT BS X669.3 AND Z100.032, PN 85339516-101. REMOVED RIB, PN:85339516-101 AT BS X669.3, REF SRM 51-42-05 STEP 4E
- [SDR QXEA2015031700142](https://openairdocs.org/sdr/QXEA2015031700142), Mar 15, 2015: RIB. CORRODED. AFT PASSENGER DOOR SURROUND STRUCTURE HAS CORRODED RIB AT BS X676.45 AND Z100.032, PN 85339514-101. REMOVED RIB, PN:85339514-101 AT BS X676.45, REF SRM 51-42-05
- [SDR QXEA2015031700141](https://openairdocs.org/sdr/QXEA2015031700141), Mar 15, 2015: RIB. CORRODED. AFT PASSENGER DOOR SURROUND STRUCTURE HAS RIB CORRODED AT BS X683.45 AND Z100.032, PN 85339514-101. REMOVED RIB, PN:85339514-101, REF BS X683.45, REF SRM 51-42-
- [SDR QXEA2015031700140](https://openairdocs.org/sdr/QXEA2015031700140), Mar 15, 2015: RIB. CORRODED. AFT PAX DOOR SURROUND STRUCTURE HAS RIB CORRODED AT BS X690.45 AND Z100.032, PN 85339515-101. REMOVED RIBS AT BS X690.45, PN:85339515-101 REF SRM 51-42-05, STEP
- [SDR QXEA2015031700139](https://openairdocs.org/sdr/QXEA2015031700139), Mar 15, 2015: RIB. CORRODED. AFT PAX DOOR SURROUND STRUCTURE HAS RIB CORRODED AT STA X 697.600 AND Z100.032, PN 85339517-101. REMOVED RIB, PN:85339517-101 REF SRM 51-42-05, STEP 4E AT STA X
- [SDR QXEA2014102500854](https://openairdocs.org/sdr/QXEA2014102500854), Oct 25, 2014: SLEEVE. LOOSE. FORWARD CARGO DOOR INDCATED OPEN DURING CLIMBOUT, MASTER CAUTION FOR FUSELAGE DOORS. RETURNED TO FIELD. LANDING UNEVENTFUL. IAW FIM TASK 52-70-00-810-801 FOUND 
- [SDR QXEA2014090400768](https://openairdocs.org/sdr/QXEA2014090400768), Sep 4, 2014: AUTOFEATHER SYS. NO TEST. AUTOFEATHER WILL NOT TEST. PERFORMED OPS TEST OF THE PROPELLER AUTOFEATHER AND UPTRIM REF AMM TASK 61-20-00-710-801. OPS TEST GOOD. RETURNED TO SERVICE.
- [SDR QXEA2014090400740](https://openairdocs.org/sdr/QXEA2014090400740), Sep 4, 2014: AUTOFEATHER SYS. NO TEST. AUTOFEATHER WILL NOT TEST. PERFORMED OPS TEST IAW AMM 61-20-00-710-801. CHECKS GOOD, NO DEFECTS. RETURNED TO SERVICE.
- [SDR QXEA2014080100644](https://openairdocs.org/sdr/QXEA2014080100644), Aug 1, 2014: LAMP. INOPERATIVE. EMERGENCY LIGHT SWITCH FOR CABIN "NORMAL" MODE IS NOT ILLUMINATED. REPLACED THE LAMP FOR THE BACKLIGHTING. OPS CHECKED GOOD. RETURNED TO SERVICE.
- [SDR QXEA2014070700557](https://openairdocs.org/sdr/QXEA2014070700557), Jul 7, 2014: LAMP. FAILED. FORWARD EMERGENCY EXIT DOOR BETA LAMP FAILED FUNCTIONAL CHECK. REPLACED THE BETA LAMP IAW AMM 33-51-00-960-801.

All 532: https://openairdocs.org/deregistered/N406QX-2023-04-18/reports.md

## 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 20071022825489I](https://openairdocs.org/incident/20071022825489I), Oct 22, 2007: Bombdr DHC8402 (N406QX), Pasco, WA, No damage. (-23) Qxea flt 2268 pdx to boi was in cruise flight when the pilots noticed a severe reduction of power on the #1 engine. The engine was secured, procedures…
- [Incident 20061209026129I](https://openairdocs.org/incident/20061209026129I), Dec 9, 2006: Bombdr DHC8402 (N406QX), Redding, CA, Minor damage. (-23) On extended approach to runway 16 (rdd) aircraft was hit by a large bird (duck) at approximately 200 knots. Landing was normal with no flight deck signs…

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