# N415QX: 2003 Bombardier DHC-8-402, registration cancelled 2019-02-14

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: February 14, 2019
- 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: 4081
- Year built: 2003
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: April 24, 2005
- Certificate issued: June 22, 2004
- Last registry action: June 12, 2017
- Mode S code: A4E827
- 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/N415QX
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=415QX
- Page: https://openairdocs.org/deregistered/N415QX-2019-02-14

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 (272, newest 50)

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

- [SDR QXEA2018060101](https://openairdocs.org/sdr/QXEA2018060101), Jun 1, 2018: POWER SUPPLY. INOPERATIVE. EMERGENCY LIGHTS FOR THE SECONDED AND THIRD EXITS, AND CEILING LIGHT FROM FORWARD WERE INOPERATIVE. REMOVED AND REPLACED THE POWER SUPPLY IAW 33-51-01-000-801/4
- [SDR QXEA2018052900202](https://openairdocs.org/sdr/QXEA2018052900202), May 25, 2018: WIRE HARNESS. DEFECTIVE. AFTER SELECTING GEAR DOWN ON APPROACH THE NOSE WHEEL GEAR DOOR RETRACTED THEN OPENED APPROX 3 TIMES BEFORE REMAINING OPEN WITH NOSE WHEEL DOOR LIGHT ILLUMINATED
- [SDR QXEA2018031900095](https://openairdocs.org/sdr/QXEA2018031900095), Mar 19, 2018: LAMP. INOPERATIVE. ON FORWARD FA PANEL, EMERGENCY LIGHT BUTTON NOT ILLUMINATED. REMOVED FROM SERVICE. REPLACED THE EMERGENCY LIGHT SWITCH. NO OTHER DEFECT NOTED. AIRCRAFT RETURNED
- [SDR QXEA2016013000031](https://openairdocs.org/sdr/QXEA2016013000031), Jan 28, 2018: FLAP SYSTEM. MALFUNCTIONED. WHEN FLAPS SELECTED TO 35 FROM 15 DURING APPROACH, THE FLAP POWER CAUTION ILLUMINATED. FLAPS REMAINED AT 15 - 16 INDICATED ON THE NR 2 MFD. ABORTED APPROACH. UN
- [SDR QXEA2017010200716](https://openairdocs.org/sdr/QXEA2017010200716), Dec 29, 2017: LENS. DETACHED. EMERGENCY EXIT SIGN LENS POPPED OFF. REPLACED THE LENS. NO OTHER DEFECTS NOTED. RETURNED TO SERVICE.
- [SDR QXEA2017121500703](https://openairdocs.org/sdr/QXEA2017121500703), Dec 14, 2017: LIGHT. LOOSE. LUMINESCENT FLOOR STRIP LIGHTING PULLING UP IN FRONT OF SEAT 2D. REMOVED FROM SERVICE. RE SECURED LUMINESCENT STRIP @ 2D. NO FURTHER DEFECTS NOTED. AIRCRAFT RET
- [SDR QXEA2017110200660](https://openairdocs.org/sdr/QXEA2017110200660), Nov 1, 2017: CONTROLLER. MALFUNCTIONED. DURING A DAILY SYSTEMS CHECK, AUTOFEATHER FAILED MESSAGE FOR THE LEFT ENGINE AND ABORT MESSAGE FOR THE RIGHT ENGINE. REMOVED FROM SERVICE. CHECKED CDS FOUND FAU
- [SDR QXEA2017071700474](https://openairdocs.org/sdr/QXEA2017071700474), Jul 14, 2017: BATTERY PACK. INOPERATIVE. BOTH EXIT LIGHTS AT THE RIGHT FORWARD EMERGENCY EXIT DOOR ARE INOPERATIVE. REPLACED THE BATTERY PACKS FOR THE NR 2 POWER SUPPLY. OPS CHECKED GOOD.
- [SDR QXEA2017071700470](https://openairdocs.org/sdr/QXEA2017071700470), Jul 13, 2017: HANDLE. OUT OF ADJUST. MAIN CABIN DOOR HANDLE STICKS WHEN OPENING THE DOOR FROM INSIDE. REMOVED FROM SERVICE. FERRIED FOR REPAIRS. FOUND THE HANDLE FORCES OUT OF ADJUSTMENT. ADJUSTED 
- [SDR QXEA2017061400421](https://openairdocs.org/sdr/QXEA2017061400421), Jun 13, 2017: WARNING MESSAGE. FALSE ACTIVATION. ABORTED TAKE OFF DUE TO A WARNING. PERFORMED THE CHECKLIST AND AIRCRAFT FAILED TO WARN TEST. PERFORMED TAKE OFF WARNING HORN FIM 31-52-00-810-802 AND OPERATIONA
- [SDR QXEA2017021300056](https://openairdocs.org/sdr/QXEA2017021300056), Feb 9, 2017: ENGINE. FAILED. NR 1 OIL PSI FLUCTUATES ERRATICALLY FROM GREEN INTO YELLOW AND THEN INTO THE RED ARC AS LOW AS 41 PSI ON FINAL. THE NR 1 AC GEN LIGHT ILLUMINATED ITT ON BOTH EN
- [SDR QXEA2016101300651](https://openairdocs.org/sdr/QXEA2016101300651), Oct 13, 2016: BULB. FAILED. AFT F/A STATION LIGHT BULB POPPED. MINOR SMOKE EMITTED. REMOVED BROKEN BULB & DEFRIS FROM AFT GALLEY WORK LIGHT. PERFORMED GVI OF AFT GALLEY WORK LIGHT W/ NO DE
- [SDR QXEA2016092600601](https://openairdocs.org/sdr/QXEA2016092600601), Sep 23, 2016: LIGHT. INOPERATIVE. F/A EMERGENCY LIGHTING SWITCH LIGHT, NORMAL, LIGHT DOES NOT ILLUMINATE, RELAMPED. NO OTHER DEFECTS NOTED. RETURNED TO SERVICE.
- [SDR QXEA2016082100542](https://openairdocs.org/sdr/QXEA2016082100542), Aug 21, 2016: APU. ODOR. RUBBER ODOR COMING FROM THE APU WITH THE BLEEDS ON.
- [SDR QXEA2016082100541](https://openairdocs.org/sdr/QXEA2016082100541), Aug 21, 2016: UNKNOWN. ODOR. RUBBER ODOR COMING FROM THE APU WITH THE BLEEDS SELECTED ON. THE ODOR WENT AWAY WITH THE ENGINES ON. NO FAULTS FOUND IN CDS SYSTEM. RAN APU WITH BLEEDS ON FOR 2
- [SDR QXEA2016072900485](https://openairdocs.org/sdr/QXEA2016072900485), Jul 29, 2016: BRAKE. SMOKE. DURING PREFLIGHT, DISCOVERED RIGHT MAIN INBOARD AND OUTBOARD WHEELS SMOKING. SMOKE IS COMING FROM THE BRAKE AREA OF THE WHEEL. REMOVED NR 3 AND 4 MAIN WHEEL TIR
- [SDR QXEA2016072100460](https://openairdocs.org/sdr/QXEA2016072100460), Jul 21, 2016: TIRE. FAILED. BLOWN LT MAIN GEAR TIRE AFTER TAKEOFF, CAUSED A LOSS OF NR 1 HYD SYSTEM FLUID. DIVERTED. LANDING UNEVENTFUL. REPLACED NR 1 & 2 MLG TIRES, RETORQUE THE TEE FITTI
- [SDR QXEA2016070600444](https://openairdocs.org/sdr/QXEA2016070600444), Jul 6, 2016: WIRE HARNESS. SHORTED. NR 1 AC GENERATOR CAUTION & L AC BUS CAUTION. ABORTED TAKEOFF AT 90 KNOTS. RETURNED TO GATE. FERRIED FOR REPAIRS. FOUND SHORT IN HARNESS. REPLACED NR 1 AC GENER
- [SDR QXEA2016052300332](https://openairdocs.org/sdr/QXEA2016052300332), May 14, 2016: SEAT TRACK. NOT REPORTED. SEAT TRACK NR 23 REQUIRES REPLACEMENT. REMOVED SEAT TRACK NR 23 REF SRM 51-41-00, 51-42-05. INSTALLED SEAT TRACK NR 23, NEW TRACK, REF SRM 51-41-00, 51-42-05, 5
- [SDR QXEA2016052300330](https://openairdocs.org/sdr/QXEA2016052300330), May 14, 2016: SEAT TRACK. NOT REPORTED. SEAT TRACK NR 16 REQUIRES REPLACEMENT, PN 85338210. REMOVED WEB ASSY, PN 85338806-001 COMMON TO SEAT TRACK NR 16 AND NR 23 IAW SRM 51-42-05 AND 51-41-00. RE-INS
- [SDR QXEA2016052300328](https://openairdocs.org/sdr/QXEA2016052300328), May 13, 2016: WEB. CORRODED. EVIDENCE OF CORROSION FOUND ON MACHINED WEB, PN 85329687-101 AT MCD LWR SURROUND X26.70. EVALUATED CORROSION FOUND NO DAMAGE ALLOWED REF TASK CARD 6-53-1160-FWD
- [SDR QXEA2016052400344](https://openairdocs.org/sdr/QXEA2016052400344), May 11, 2016: STRAP. CORRODED. EVIDENCE OF CORROSION FOUND ON STRAP BETWEEN FS 301-321, STR 32P. BLENDED, REMOVED CORROSION ON INTERNAL STRAP BETWEEN FS X 301.0 TO FS X 321.0, STR 32P, REF SR
- [SDR QXEA2016052400343](https://openairdocs.org/sdr/QXEA2016052400343), May 11, 2016: WEB. CORRODED. EVIDENCE OF CORROSION FOUND ON MACHINED WEB, PN 85329688-101 AT MCD LOWER SURROUND X6.70. EVALUATED CORROSION, FOUND NO DAMAGE ALLOWED REF TASK CARD 6-53-1160-F
- [SDR QXEA2016052400323](https://openairdocs.org/sdr/QXEA2016052400323), May 11, 2016: INTERCOSTAL. CORRODED. EVIDENCE OF CORROSION ON MACHINED INTERCOSTAL, PN 85329342-105 AT MCD LOWER SURROUND BETWEEN X 1.00 AND X 32.4, STR 25P. NO REPAIRS ALLOWED ON INTERCOSTAL, PN 8
- [SDR QXEA2016052300325](https://openairdocs.org/sdr/QXEA2016052300325), May 11, 2016: CHANNEL. CORRODED. EVIDENCE OF CORROSION AROUND BOLT HOLES OF MCD THRESHOLD CHANNEL, PN 85329540-001. UPPER SURFACE OF THRESHOLD CHANNEL CAN BE BLENDED TO 0.040", MIN REMAINING TH
- [SDR QXEA2016052300324](https://openairdocs.org/sdr/QXEA2016052300324), May 11, 2016: THRESHOLD. CORRODED. FOUND CORROSION ON THRESHOLD PLATE 85329532-001 FROM BS X 6.700 TO BS X 26.700 ON MCD. REMOVED THRESHOLD PLATE, PN 85329532-001 FROM X6.70 TO X26370 MCD LOWER S
- [SDR QXEA2016052300327](https://openairdocs.org/sdr/QXEA2016052300327), May 10, 2016: SUPPORT ANGLE. CORRODED. EVIDENCE OF CORROSION ON DRAIN TROUGH SUPPORT ANGLES, PN 85329333-103, 2EA AT MCD LOWER SURROUND COMMON TO MACHINED INTERCOSTAL, STR 25P. REMOVED DRAIN TROUGH S
- [SDR QXEA2016052300326](https://openairdocs.org/sdr/QXEA2016052300326), May 10, 2016: DOOR SILL. CORRODED. EVIDENCE OF CORROSION ON LOWER MAIN SILL, STR 25P, BETWEEN X 1.0 AND X 32.4 MCD LOWER SURROUND, PN 85329349-101. EVALUATED CORROSION AND FOUND NO DAMAGE ALLOWED
- [SDR QXEA2016051100306](https://openairdocs.org/sdr/QXEA2016051100306), May 8, 2016: INTERCOSTAL. NOT REPORTED. 3 EA DAMAGED NUT PLATES NEED REPLACEMENT UNDER LOWER TCAS ANTENNA. REMOVED INTERCOSTAL, PN 8533492-101, REF SRM 51-42-05, 4.C. INSTALLED INTERCOSTAL PN 85334920
- [SDR QXEA2016051100305](https://openairdocs.org/sdr/QXEA2016051100305), May 8, 2016: SEAT TRACK. NOT REPORTED. SEAT TRACK NR 11 REQUIRES REPLACEMENT, PN 85328210. REMOVED DRIP ANGLE, PN 85307495-112 AT X 176.0 TO X 49.50 Y 9.250 REF SRM 51-42-05. INSTALLED DRIP ANGLE, PN
- [SDR QXEA2016052300329](https://openairdocs.org/sdr/QXEA2016052300329), May 7, 2016: SEAT TRACK. NOT REPORTED. SEAT TRACK NR 10 REQUIRES REPLACEMENT, PN 85328210. REMOVED 2 EA GROUND CABLES FROM SEAT TRACK NR 10 FWD SIDE OF SEAT TRACK BEHIND BULKHEAD AT X-39.00, 2" AFT O
- [SDR QXEA2016051100301](https://openairdocs.org/sdr/QXEA2016051100301), May 5, 2016: SEAT TRACK. DAMAGED. SEAT TRACK NR 16 OTBD SPLICE. FOUND WITH OVERSIZE HOLES. LOCATED AND DRILLED A NEW SEAT TRACK SPLICE, IAW SRM 51-40-07.
- [SDR QXEA2016051100304](https://openairdocs.org/sdr/QXEA2016051100304), May 4, 2016: SEAT TRACK. DAMAGED. SPLICE ON SEAT TRACK NR 10 COMMON TO SEAT TRACK 11 HAS ELONGATED HOLES INBD AND OTBD SEAT TRACK SPLICES. LOCATED AND DRILLED THE SEAT TRACK SPLICES AT SEAT TRAC
- [SDR QXEA2016051100303](https://openairdocs.org/sdr/QXEA2016051100303), May 4, 2016: SEAT TRACK. DAMAGED. SPLICE ON SEAT TRACK NR 11 COMMON TO SEAT 12 HAS ELONGATED HOLES BOTH INBD AND OTBD SEAT TRACK SPLICES. LOCATED & DRILLED SEAT TRACK SPLICES AT SEAT TRACKS 11 &
- [SDR QXEA2016052300334](https://openairdocs.org/sdr/QXEA2016052300334), May 3, 2016: DOUBLER. CORRODED. LOWER TCAS PLATFORM, PN 85335262-105, CORRODED. LOCATED AND DRILLED NEW LOWER TCAS PLATFORM, PN 85335262-105, REF SRM 51-40-07-02-01.
- [SDR QXEA2016052300321](https://openairdocs.org/sdr/QXEA2016052300321), May 3, 2016: RIB. CRACKED. LEADING EDGE 611AR, INBD RIB, EXISTING REPAIR ANGLE AT BOTTOM CORNER FOUND CRACKED. REMOVED CRACKED EXISTING REPAIR ANGLE FROM BOTTOM CORNER OF L/E PANEL 611AR 
- [SDR QXEA2016052300322](https://openairdocs.org/sdr/QXEA2016052300322), May 2, 2016: RIB. CRACKED. CRACK FOUND ON OTBD LOWER DOUBLER ON 511AL L/E RIB. REMOVED CRACKED OB LOWER DOUBLER FROM 511AL L/E RIB. REF SRM 51-42-05, 51-40-15. INSTALLED NEW DOUBLER, REF 
- [SDR QXEA2016052300333](https://openairdocs.org/sdr/QXEA2016052300333), May 1, 2016: DOUBLER. CORRODED. TCAS EXTERNAL DOUBLER CORRODED. LOCATED AND DRILLED NEW TCAS EXTERNAL DOUBLER, PN 85314193-103, REF SRM 51-40-07-02-01.
- [SDR QXEA2016052300331](https://openairdocs.org/sdr/QXEA2016052300331), May 1, 2016: SEAT TRACK. NOT REPORTED. SEAT TRACK, 25 REQUIRES REPLACEMENT, PN 85338210. R & R SEAT TRACK NR 25 WITH NEW SERVICEABLE PN 85337843-103SP, PO T24255, REF DWG 85338806, REV- SHT 1 AND SRM
- [SDR QXEA2016052300320](https://openairdocs.org/sdr/QXEA2016052300320), Apr 27, 2016: BUSHING. UNKNOWN. OVERCENTER SPRING BUSHING ON LIFT AND LATCH MECHANISM OF AFT PAX DOOR REQUIRE REPLACEMENT. REMOVED OVER CENTER SPRING BUSHINGS ON AFT PAX DOOR REF AMM 52-12-11-
- [SDR QXEA2016040500244](https://openairdocs.org/sdr/QXEA2016040500244), Apr 5, 2016: GOVERNOR. NO TEST. DURING OVERSPEED GOVERNOR TEST, NR 1 ENGINE OVERSPEED GOVERNOR FAILED TEST. FOUND FAULT CODE 238 ON NR 1 ENGINE. CLEANED THE CONNECTOR PLUG AND RESECURED. CLEAR
- [SDR QXEA2016021700149](https://openairdocs.org/sdr/QXEA2016021700149), Feb 17, 2016: HOUSING. BROKEN. RIGHT FORWARD EMERGENCY EXIT LOWER EMERGENCY EXIT LIGHT HOUSING CRACKED AND BROKEN. REPLACED HOUSING. CHECKS GOOD.
- [SDR QXEA2015120300636](https://openairdocs.org/sdr/QXEA2015120300636), Dec 3, 2015: LAMP. INOPERATIVE. FORWARD F/A EMERGENCY SWITCH LIGHT "NORMAL" INDICATION INOPERATIVE. RELAMPED AS REQUIRED.
- [SDR QXEA2015110700591](https://openairdocs.org/sdr/QXEA2015110700591), Nov 7, 2015: LINE. FAILED. ENROUTE DE-ICE PRESSURE CAUTION ILLUMINATED. DIVERTED AND ACCOMPLISHED AN UNEVENTFUL LANDING. REPLACED DEICE BOOT SUPPLY LINE, HOSE AT WING L/E 613AR. RETURNED 
- [SDR QXEA2015090600453](https://openairdocs.org/sdr/QXEA2015090600453), Sep 6, 2015: LIGHT. MALFUNCTIONED. EMERGENCY LIGHTS AT FORWARD RIGHT EMERGENCY EXIT COME ON FOR A MOMENT, THEN GO OFF. CHECKED LIGHTS IAW AMM 33-51-00-710-803, COULD NOT DUPLICATE. NO DEFECTS NOT
- [SDR QXEA2015061800342](https://openairdocs.org/sdr/QXEA2015061800342), Jun 18, 2015: LAMP. INOPERATIVE. "NORMAL" INDICATION, BACK LIGHT INOPERATIVE IN THE F/A EMERGENCY LIGHT SWITCH. RELAMPED SWITCH. OPS CHECKS GOOD.
- [SDR QXEA2015052100263](https://openairdocs.org/sdr/QXEA2015052100263), May 21, 2015: BATTERY. FAILED. POWER SUPPLY/CHARGER NR 2 FAILS THE 10 MINUTE EMERGENCY LIGHT CHECK. LASTED FOR ABOUT 4 MINUTES. REPLACED NR 2 POWER SUPPLY IAW AMM 33-51-01-000-801. NO HELP. R
- [SDR QXEA2015031900145](https://openairdocs.org/sdr/QXEA2015031900145), Mar 19, 2015: SENSOR. MALFUNCTIONED. INTERMITTENT NO OIL TEMP NR 2 INDICATION DURING START AND SHUTDOWN. RETURN TO FIELD. LANDING UNEVENTFUL. INTERROGATED CDS. FAULT CODE 781. CLEARED FAULT CODE. R
- [SDR QXEA2015030100105](https://openairdocs.org/sdr/QXEA2015030100105), Mar 1, 2015: CONTROL UNIT. MALFUNCTIONED. AFTER ENGINE START MOVED BOTH CONDITION LEVERS TO MAX/1020. NR 2 PROP WOULD NOT COME OUT OF FEATHER. R & R 2 OVERSPEED GOVERNOR AND NR 2 PEC. OPS TEST GOOD. NO 
- [SDR QXEA2014110400893](https://openairdocs.org/sdr/QXEA2014110400893), Nov 4, 2014: BATTERY PACK. INOPERATIVE. AFT GALLEY EMERGENCY LIGHTS ILLUMINATE WHEN POWER IS TURNED OFF. REPLACED THE AFT EMERGENCY LIGHTS POWER SUPPLY AND BATTERY PACKS IAW AMM 33-51-00-000-801 AND 3

All 272: https://openairdocs.org/deregistered/N415QX-2019-02-14/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 20160721020669I](https://openairdocs.org/incident/20160721020669I), Jul 21, 2016: Bombardier Inc DHC-8-402 (N415QX), Reno, NV, Minor damage. Qxea flight 2448 experienced left main landing gear #2 tire failure on take off. Aircraft continued to pdx without incident. Aircraft was inspected and found…

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