# N416QX: 2001 Bombardier DHC-8-402, registration cancelled 2018-10-31

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: October 31, 2018
- 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: 4083
- Year built: 2001
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: April 25, 2005
- Certificate issued: June 22, 2004
- Last registry action: June 12, 2017
- Mode S code: A4EBDE
- Owner when cancelled: [Horizon Air Industries Inc](https://openairdocs.org/faa-owner/HORIZON%20AIR%20INDUSTRIES%20INC)
- Location: [Seatac, WA](https://openairdocs.org/faa-place/WA/Seatac)
- Owner type: Corporation
- Owner's area on the map: 47.4466° N, 122.2721° W: Placed by OpenAirDocs at the center of ZIP code 98188, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N416QX
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=416QX
- Page: https://openairdocs.org/deregistered/N416QX-2018-10-31

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

## Service difficulty reports (387, newest 50)

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

- [SDR QXEA2018041600143](https://openairdocs.org/sdr/QXEA2018041600143), Apr 15, 2018: LIGHT. LOOSE. CARPET AND EMERGENCY LIGHT STRIP COMING OFF FLOOR AT SEAT 2D. SECURED THE LIGHT AND CORNER OF CARPET AT ROW 2D. RETURNED TO SERVICE.
- [SDR QXEA2018021600061](https://openairdocs.org/sdr/QXEA2018021600061), Feb 15, 2018: WARNING MESSAGE. FALSE ACTIVATION. FLAP POWER CAUTION ILLUMINATED DURING FINAL, SELECTING FLAPS FROM 5 TO 10. RAN E & A CHECKLIST, FLAP POWER CAUTION EXTINGUISGED. NO FURTHER ISSUES, FLAPS OPERAT
- [SDR QXEA2018021300058](https://openairdocs.org/sdr/QXEA2018021300058), Feb 13, 2018: IGNITER. FAILED. APU FAILED DURING START. SMOKE REPORTED COMING OUT OF THE APU. CLEARED BY INTERROGATED CDS AND FOUND MULTIPLE IGNITER CODES. REMOVED AND REPLACED BOTH IGNITERS 
- [SDR QXEA2018011000012](https://openairdocs.org/sdr/QXEA2018011000012), Jan 10, 2018: LAMP. INOPERATIVE. EMERGENCY LIGHT SWITCH AT FORWARD FA POSITION, BACKGROUND LIGHT APPEARS INOPERATIVE. REMOVED FROM SERVICE. REPLACED THE LAMP IN THE EMERGENCY LIGHT SWITCH. OPS 
- [SDR QXEA2017121100696](https://openairdocs.org/sdr/QXEA2017121100696), Dec 8, 2017: ENGINE. FAILED. ON APPROACH HAS #2 ENGINE FAIL. FOLLOWED BY #2 ENGINE FADEC FAIL WARNING. EMERGENCY DECLARED. LANDING UNEVENTFUL AND TAXI TO GATE UNDER OWN POWER.AIRCRAFT REMOV
- [SDR QXEA2017112800684](https://openairdocs.org/sdr/QXEA2017112800684), Nov 28, 2017: LAMP. INOPERATIVE. EMERGENCY LIGHT PANEL LIGHTS INOPERATIVE. REMOVED FROM SERVICE. REPLACED THE LAMPS IN THE PANEL. BACKLIGHTING NOW ILLUMINATES NORMALLY. AIRCRAFT RETURNED TO SER
- [SDR QXEA2017091900576](https://openairdocs.org/sdr/QXEA2017091900576), Sep 18, 2017: SENSOR. MALFUNCTIONED. DOOR AMBER CAUTION LIGHT ON GEAR PANEL, REMAINED ILLUMINATED AFTER GEAR SELECTION TO GEAR DOWN ON FINAL. REMOVED FROM SERVICE. ADJUSTED NGLK1 SENSOR IAW AMM 32-
- [SDR QXEA2017080700504](https://openairdocs.org/sdr/QXEA2017080700504), Aug 6, 2017: DOOR. BINDING. FORWARD EMERGENCY STOWAGE COMPARTMENT DOOR IS STUCK. REMOVED FROM SERVICE. FREED THE FWD EMERGENCY STOWAGE COMPARTMENT DOOR. CYCLED THE DOOR OPEN AND CLOSE MULT
- [SDR QXEA2017071000460](https://openairdocs.org/sdr/QXEA2017071000460), Jul 8, 2017: PROXIMITY SENSOR. MALFUNCTIONED. DURING CLIMB , A RED NOSE GEAR UNSAFE LIGHT INDICATED. LIGHT WAS INTERMITTENT, ON AND OFF. REMOVED FROM SERVICE. REPLACED NLG PROXIMITY SENSOR. AIRCRAFT RETURNE
- [SDR QXEA2017050800345](https://openairdocs.org/sdr/QXEA2017050800345), May 6, 2017: SWITCH. MALFUNCTIONED. EMERGENCY LIGHTS CYCLING ON AND OFF. REMOVED AND REPLACED THE EMERGENCY LIGHTS SWITCH IAW AMM 33-51-05-000-801 & 33-51-05-400-801. CHECKED SECURITY OF WIRING ON
- [SDR QXEA2017041200249](https://openairdocs.org/sdr/QXEA2017041200249), Apr 11, 2017: ENGINE. FAILED. NR 2 PEC CAUTION LIGHT AT CRUISE. DURING CLIMB WITH PROPS AT 900, NOTED FLUCTUATIONS OF +/- 10 RPM(890-910) FLUCTUATIONS INCREASED TO +/- 20 (880-920) AFTER LEV
- [SDR QXEA2017041200248](https://openairdocs.org/sdr/QXEA2017041200248), Apr 10, 2017: TIRE. FAILED. INBOARD RIGHT MAIN TIRE NR 3 WENT FLAT DURING TAXI IN. REPLACED THE 3 AND 4 WHEEL ASSEMBLIES IAW 6324101. PERFORMED INSPECTION AFTER TIRE FAILURE IAW AMM 05-50-
- [SDR QXEA2017032700177](https://openairdocs.org/sdr/QXEA2017032700177), Mar 26, 2017: SCREW. LOOSE. SIGNIFICANT AIR LEAK DURING CLIMB ALL THE WAY TO FL 230. SEEMED TO ORIGINATE AT FIRST OFFICER`S WINDOW. PRESSURIZATION NORMAL. RETORQUED THE WINDOW IAW AMM 56-1
- [SDR QXEA2017020800045](https://openairdocs.org/sdr/QXEA2017020800045), Feb 6, 2017: PIVOT ASSY. MALFUNCTIONED. AFT REAR BOARDING DOOR (L2) WILL NOT OPEN OR CLOSE FROM THE AFT SIDE. FERRIED FOR REPAIRS. REMOVED & REPLACED AFT PASSENGER DOOR PIVOT ASSY. C/W RIGGING OF AFT 
- [SDR QXEA2017011300010](https://openairdocs.org/sdr/QXEA2017011300010), Jan 12, 2017: LIGHT. LOOSE. EMERGENCY LIGHT LOOSE AT ROW 1AB. SECURED THE LIGHT.
- [SDR QXEA2017010900002](https://openairdocs.org/sdr/QXEA2017010900002), Jan 8, 2017: RELAY. MALFUNCTIONED. FA REPORTS EMERGENCY LIGHTS ARE REMAINING ILLUMINATED. TRIED CYCLING ALL SWITCHES, NO FIX. CYCLED A/C POWER AFTER SHUTDOWN, NOW HALF OF EMERGENCY LIGHTS ON WHEN
- [SDR QXEA2016121600795](https://openairdocs.org/sdr/QXEA2016121600795), Dec 16, 2016: RELAY. MALFUNCTIONED. EMERGENCY LIGHT IN CABIN AND EXTERIOR ALL ON WITH EMERGENCY LIGHT SWITCH IN ARM AND APU NORMAL ELECTRICAL POWER. PERFORMED OPERATIONAL CHECK OF EMERGENCY LIGHT 
- [SDR QXEA2016082600563](https://openairdocs.org/sdr/QXEA2016082600563), Aug 28, 2016: SEAL. FAILED. NR 2 ENGINE TOOK 1.5 MINUTES TO COME OUT OF FEATHER AFTER ENGINE START. REMOVED AND REPLACED THE NR 2 PROPELLER PISTON SEAL. IAW AMM 61-10-00-960-801. OPS TESTE
- [SDR QXEA2016062800440](https://openairdocs.org/sdr/QXEA2016062800440), Jun 28, 2016: BATTERY PACK. FAILED. EMERGENCY BATTERY PACKS IN THE NR 2 POSITION FAIL THE 10 MINUTE TEST. REPLACED BATTERY PACK.
- [SDR QXEA2016062200406](https://openairdocs.org/sdr/QXEA2016062200406), Jun 22, 2016: LIGHT. PEELING. FLOOR PATH LIGHT STRIP AT FORWARD GALLEY PEELING UP. REPLACED FLOOR STRIP. RETURNED TO SERVICE.
- [SDR QXEA2016052200335](https://openairdocs.org/sdr/QXEA2016052200335), May 22, 2016: WARNING LIGHT. FALSE ACTIVATION. DEICE PRESSURE CAUTION ILLUMINATED ON DESCENT WHEN BOOTS SELECTED TO SLOW. IAW THE CHECKLIST, SET MODE SELECT TO MANUAL AND THEN BACK TO SLOW. THE LIGHT EXTINGU
- [SDR QXEA2016012800079](https://openairdocs.org/sdr/QXEA2016012800079), Jan 28, 2016: LIGHT. LOOSE. FLOOR STRIP AT ROW 2D LOOSE. RESECURED FLOOR STRIP AT 2D. RETURNED TO SERVICE.
- [SDR QXEA2016012600062](https://openairdocs.org/sdr/QXEA2016012600062), Jan 26, 2016: LEAD. DAMAGED. AT 12,000 FT MSL AND -1C OAT, SELECTED PROP DEICE ON IN IMC CONDITIONS ABOUT 3 MINUTES LATER, PROP DEICE CAUTION ILLUMINATED. RAN THE E/A CHECKLIST AND CAUTION 
- [SDR QXEA2015121500649](https://openairdocs.org/sdr/QXEA2015121500649), Dec 15, 2015: HYDRAULIC SYSTEM. LOW. NR 2 HYDRAULIC QUANTITY LOW. DIVERTED AND ACCOMPLISHED UNEVENTFUL LANDING. ACFT CURRENTLY OUT OF SERVICE FOR REPAIRS.
- [SDR QXEA2015120900637](https://openairdocs.org/sdr/QXEA2015120900637), Dec 2, 2015: SEAT TRACK. CORRODED. SEAT TRACK NR 13, PN 85361510-104 REQUIRES REPLACEMENT. QTY 6 DRIP PANS REMOVED FS X=71.2, 116, 176, 236, 301, 361 IAW SRM 51-41-00. INSTALLED 6EA DRIP PANS AT 
- [SDR QXEA2015121600644](https://openairdocs.org/sdr/QXEA2015121600644), Nov 29, 2015: SEAT TRACK. CORRODED. SEAT TRACK NR 6, PN 85328210-111 REQUIRES REPLACEMENT. REMOVED DRIP ANGLE, PN 85307495-113 FROM SEAT TRACK NR 6 COMMON TO SEAT TRACK NR 7 REF SRM 51-42-05-02-01
- [SDR QXEA2015120900638](https://openairdocs.org/sdr/QXEA2015120900638), Nov 29, 2015: SEAT TRACK. CORRODED. SEAT RAIL NR 5, PN 85338210-109 REQUIRES REPLACEMENT. REMOVED SPLICES AT SEAT TRACK NR 5 AND NR 6 FS X102.0, Y9.250, PN 85338216-101 AND 85338215-101. INSTALLED
- [SDR QXEA2015111000583](https://openairdocs.org/sdr/QXEA2015111000583), Nov 5, 2015: SEAT TRACK. CORRODED. SEAT TRACK NR 1, PN 85328261-107, REQUIRES REPLACEMENT. REMOVED SEAT TRACK NR 1 PN: 85328261-107, REF SRM 51-42-05-02-01, SRM 51-42-45-02-01, SRM 51-40-15-002-0
- [SDR QXEA2015121600643](https://openairdocs.org/sdr/QXEA2015121600643), Nov 4, 2015: ATTACH FITTING. CORRODED. ATTACHING CLIP AT AFT SIDE OF FS 116.00 AND STR 24L, UNDER FLOOR LT FUSELAGE HAS POSSIBLE SURFACE CORROSION, MARKED. DETACHED, DISCOVERED FLOOR SUPPORT AT AFT E
- [SDR QXEA2015110300571](https://openairdocs.org/sdr/QXEA2015110300571), Nov 1, 2015: SEAT TRACK. DAMAGED. OUTER SPLICE, PN 85338215-101 COMMON TO SEAT TRACK NR 6 AND NR 7 HAS 1 EA ELONGATED HOLE. DRILLED AND LOCATED OUTER SPLICE COMMON TO SEAT TRACK NR 6 AT FS 279.5
- [SDR QXEA2015110900580](https://openairdocs.org/sdr/QXEA2015110900580), Oct 28, 2015: SEAT TRACK. CORRODED. SEAT RAIL, NR 19, PN 85361561-104, REQUIRES REPLACEMENT. REMOVED SEAT RAIL, NR 19, PN 35361561-104, FS X229.5 TO 571.0, Y40.95 IAW SRM 51-40-15, REPAIR 01, PARA
- [SDR QXEA2015110300572](https://openairdocs.org/sdr/QXEA2015110300572), Oct 28, 2015: SEAT TRACK. CORRODED. SEAT TRACK NR 7, CORRODED. REMOVED AND REPLACED IAW SRM 51-42-05, SRM 51-40-15 AND DWG 85307071.
- [SDR QXEA2015121600642](https://openairdocs.org/sdr/QXEA2015121600642), Oct 26, 2015: ATTACH FITTING. CORRODED. ATTACHING "CLIP" AT AFT SIDE OF FS 94.800 AND STR 24L UNDER FLOOR LT FUSELAGE, HAS POSSIBLE, SURFACE CORROSION, MARKED. REMOVED CLEAT, PN 85328131-123 FROM FRAM
- [SDR QXEA2015103000560](https://openairdocs.org/sdr/QXEA2015103000560), Oct 25, 2015: SEAT TRACK. CORRODED. SEAT TRACK CORRODED. REMOVED SEAT TRACK NR 3 IAW SRM 51-42-05 AND SRM 51-40-15. LOCATED AND DRILLED NEW SEAT TRACK NR 3, IAW SRM 51-40-07. INSTALLED IAW SRM 51-
- [SDR QXEA2015103000559](https://openairdocs.org/sdr/QXEA2015103000559), Oct 25, 2015: DOUBLER. CORRODED. FORWARD LAV OUTSIDE DOUBLER EVIDENCE OF CORROSION. EVALUATED 2 EA AREAS OF CORROSION DAMAGE ON LAV SERVICE PORT INTERNAL DOUBLER, PN 85307789-101, AREA 1 IS LOC
- [SDR QXEA2015103000567](https://openairdocs.org/sdr/QXEA2015103000567), Oct 17, 2015: SPLICE. CORRODED. SPLICES COMMON TO SEAT TRACK NR 5 AND NR 6 HAVE ELONGATED HOLES. DRILLED AND LOCATED HOLES COMMON TO SEAT TRACK NR 5 AND SPLICE MEMBERS REF SRM 51-40-07-02-01. 
- [SDR QXEA2015111000582](https://openairdocs.org/sdr/QXEA2015111000582), Oct 16, 2015: SEAT TRACK. CORRODED. SEAT TRACK NR 2, PN 8536154-103, REQUIRES REPLACEMENT. LOCATED AND DRILLED NEW SEAT TRACK NR 2, PN 85361561-103 DADO PANEL ANGLES INSTALLED REF SRM 51-42-05, QT
- [SDR QXEA2015103000565](https://openairdocs.org/sdr/QXEA2015103000565), Oct 15, 2015: CUP. CORRODED. ATTACHING "CUP" AT AFT SIDE OF FS 156.00 AND STR 24L, UNDER FLOOR, LT FUSELAGE HAS POSSIBLE SURFACE CORROSION, MARKED. REMOVED CLEAT PN:85328131-119 FROM FRAME 
- [SDR QXEA2015103000564](https://openairdocs.org/sdr/QXEA2015103000564), Oct 15, 2015: CUP. CORRODED. ATTACHING "CUP" AT, FWD SIDE, OF FS 71.200 AND STR 24L UNDER FLOOR LT FUSELAGE, HAS POSSIBLE, SURFACE CORROSION, MARKED. REMOVED CLEAT, PN:85328131-120 FROM FRA
- [SDR QXEA2015101300563](https://openairdocs.org/sdr/QXEA2015101300563), Oct 13, 2015: SEAT TRACK. CORRODED. SEAT TRACK CORRODED. REMOVED AND REPLACED IAW SRM 51-42-05.
- [SDR QXEA2015101300562](https://openairdocs.org/sdr/QXEA2015101300562), Oct 13, 2015: SEAT TRACK. CORRODED. SEAT TRACK CORRODED. DEBURRED AND INSTALLED NEW SEAT TRACK IAW SRM 51-41-00-08-01.
- [SDR QXEA2015103000561](https://openairdocs.org/sdr/QXEA2015103000561), Oct 13, 2015: SEAT TRACK. CORRODED. SEAT TRACK CORRODED. REMOVED AND REPLACED THE SEAT TRACK SRM 51-42-05-02-01 AND SRM 51-40-15-02-01.
- [SDR QXEA2015102300552](https://openairdocs.org/sdr/QXEA2015102300552), Oct 13, 2015: SEAT TRACK. CORRODED. SEAT TAIL NR 20 CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-40-15, STEP 6N & 6M, SRM 51-42-05, STEP 4E.
- [SDR QXEA2015103000566](https://openairdocs.org/sdr/QXEA2015103000566), Oct 11, 2015: SHEAR TIE. CORRODED. SHEAR ANGLE AT FS X1.0 COMMON TO SEAT TRACK NR 5 CORRODED PN 85327581-101. COMPLIED WITH FORM M-184. LOCATED AND DRILLED NEW SHEAR ANGLE, PN 85328851-101, REF S
- [SDR QXEA2015102300550](https://openairdocs.org/sdr/QXEA2015102300550), Oct 10, 2015: SEAT TRACK. CORRODED. 208 SEAT TRACK NR 10 CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW SRM REF 51-42-05-02-01, PARA E/ 51-40-15-02-01, PARA M.
- [SDR QXEA2015101500532](https://openairdocs.org/sdr/QXEA2015101500532), Oct 9, 2015: SEAT TRACK. CORRODED. SEAT TRACK NR 11CORRODED. SEAT TRACK REMOVED AND REPLACED IAW SRM 51-42-05, SRM 51-42-05, 51-41-00, AND DWG NR 85328201, REV-B.
- [SDR QXEA2015102300551](https://openairdocs.org/sdr/QXEA2015102300551), Oct 4, 2015: SEAT TRACK. CORRODED. SEAT TRACK, NR 14 CORRODED. REMOVED CORROSION IAW SRM 53-20-49, REPAIR-02, FIG 201.
- [SDR QXEA2015062700343](https://openairdocs.org/sdr/QXEA2015062700343), Jun 27, 2015: TRANSDUCER. MALFUNCTIONED. DURING CLIMB PASSING THROUGH APPROXIMATELY 5800, PUSHER SYS FAIL CAUTION LIGHT ILLUMINATED. DIVERTED LANDING UNEVENTFUL. INSPECTED AND FOUND R AOA A-C BREAKER T
- [SDR QXEA2015051500243](https://openairdocs.org/sdr/QXEA2015051500243), May 15, 2015: PSEU. FAULTED. ON DEPARTURE, RT MAIN GEAR INDICATOR, GREEN LIGHT, REMAINED ILLUMINATED. ACCOMPLISHED MANUAL GEAR EXTENSION. RETURNED TO FIELD. LANDING UNEVENTFUL. FOUND THE FO
- [SDR QXEA2015012000020](https://openairdocs.org/sdr/QXEA2015012000020), Jan 20, 2015: BEARING. FAILED. RIGHT MAIN GEAR TIRE BLEW OUT ON LANDING. NR 2 MLG AXLE ASSY R & R WITH SERVICABLE. ALL AMM REQUIRED OPS CHECKS GOOD. NR 2 AXLE ASSY REPLACED DUE TO RT OTBD MAI

All 387: https://openairdocs.org/deregistered/N416QX-2018-10-31/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 20110510008359I](https://openairdocs.org/incident/20110510008359I), May 10, 2011: Bombardier Inc DHC-8-402 (N416QX), Yakima, WA, No damage. The aircraft was en-route from boise, id (boi) to seattle, WA (sea) when the flight crew became aware of a #2 engine low oil pressure indication. The flight…

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