# Service difficulty reports: N415QX, cancelled Feb 14, 2019

A list on [N415QX, cancelled Feb 14, 2019](https://openairdocs.org/deregistered/N415QX-2019-02-14.md).

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

Page 1 of 6 · 272 reports

- [SDR QXEA2018060101](https://openairdocs.org/sdr/QXEA2018060101.md): Power Supply · inoperative · Jun 1, 2018 · N415QX · Bombdr DHC8402 · Emergency Lighting
  > EMERGENCY LIGHTS FOR THE SECONDED AND THIRD EXITS, AND CEILING LIGHT FROM FORWARD WERE INOPERATIVE. REMOVED AND REPLACED THE POWER SUPPLY IAW 33-51-01-000-801/400-801, REPLACED BOTH BATTERY PACKS AT SAME LOCATION IAW AMM 33-51-00-820-801. OPS TESTED GOOD.
- [SDR QXEA2018052900202](https://openairdocs.org/sdr/QXEA2018052900202.md): Wire Harness · defective · May 25, 2018 · N415QX · Bombdr DHC8402 · Landing Gear System Wiring
  > 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. LANDED UNEVENTFUL. REMOVED AND REPLACED NLG 1 HARNESS. OPS CHECK GOOD. RETURNED TO SERVICE.
- [SDR QXEA2018031900095](https://openairdocs.org/sdr/QXEA2018031900095.md): Lamp · inoperative · Mar 19, 2018 · N415QX · Bombdr DHC8402 · Emergency Lighting
  > ON FORWARD FA PANEL, EMERGENCY LIGHT BUTTON NOT ILLUMINATED. REMOVED FROM SERVICE. REPLACED THE EMERGENCY LIGHT SWITCH. NO OTHER DEFECT NOTED. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA2016013000031](https://openairdocs.org/sdr/QXEA2016013000031.md): Flap System · malfunctioned · Jan 28, 2018 · N415QX · Bombdr DHC8402 · Trailing Edge Flap Control System
  > 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. UNEVENTFUL LANDING SECOND ATTEMPT. IAW FIM 27-50-00-810-802, PERFORMED FAULT CONFIRMATION PROCEDURE.
- [SDR QXEA2017010200716](https://openairdocs.org/sdr/QXEA2017010200716.md): Lens · detached · Dec 29, 2017 · N415QX · Bombdr DHC8402 · Emergency Lighting
  > EMERGENCY EXIT SIGN LENS POPPED OFF. REPLACED THE LENS. NO OTHER DEFECTS NOTED. RETURNED TO SERVICE.
- [SDR QXEA2017121500703](https://openairdocs.org/sdr/QXEA2017121500703.md): Light · loose · Dec 14, 2017 · N415QX · Bombdr DHC8402 · Emergency Lighting
  > LUMINESCENT FLOOR STRIP LIGHTING PULLING UP IN FRONT OF SEAT 2D. REMOVED FROM SERVICE. RE SECURED LUMINESCENT STRIP @ 2D. NO FURTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA2017110200660](https://openairdocs.org/sdr/QXEA2017110200660.md): Controller · malfunctioned · Nov 1, 2017 · N415QX · Bombdr DHC8402 · Propeller Controlling System
  > 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 FAULT CODE 398 B. COMPLIED WITH FIM 61-20-00-810-805. COMPLIED WITH NR 1 PEC. REMOVED AND REPLACED I
- [SDR QXEA2017071700474](https://openairdocs.org/sdr/QXEA2017071700474.md): Battery Pack · inoperative · Jul 14, 2017 · N415QX · Bombdr DHC8402 · Emergency Lighting
  > 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.md): Handle · out of adjust · Jul 13, 2017 · N415QX · Bombdr DHC8402 · Passenger/Crew Doors
  > 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 HANDLE FORCES IAW AMM 52-11-00-820-801. OPERATIONAL TESTS GOOD RETURNED TO SERVICE. NO PARTS REPLACE
- [SDR QXEA2017061400421](https://openairdocs.org/sdr/QXEA2017061400421.md): Warning Message · false activation · Jun 13, 2017 · N415QX · Bombdr DHC8402 · Central Warning
  > 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 OPERATIONAL TESTED THE WARNING SYSTEM IAW AMM 31-52-00-710-801. TAKE OFF WARNING SYSTEM OPS CHECKED PASSED.
- [SDR QXEA2017021300056](https://openairdocs.org/sdr/QXEA2017021300056.md): Engine · failed · Feb 9, 2017 · N415QX · Bombdr DHC8402 · Engine (Turbine/Turboprop)
  > 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 ENGINES REMAINED NORMAL. NR 1 ENGINE FEATHERED. LANDING UNEVENTFUL. REPLACED NR 1 ENGINE. RETURNED TO
- [SDR QXEA2016101300651](https://openairdocs.org/sdr/QXEA2016101300651.md): Bulb · failed · Oct 13, 2016 · N415QX · Bombdr DHC8402 · Passenger Compartment Lighting
  > 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 DEFECTS NOTED. REPLACED THE BULB. BULB TESTED GOOD, NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE
- [SDR QXEA2016092600601](https://openairdocs.org/sdr/QXEA2016092600601.md): Light · inoperative · Sep 23, 2016 · N415QX · Bombdr DHC8402 · Emergency Lighting
  > 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.md): Apu · odor · Aug 21, 2016 · N415QX · Bombdr DHC8402 · Airborne Auxiliary Power Unit (APU) System
  > RUBBER ODOR COMING FROM THE APU WITH THE BLEEDS ON.
- [SDR QXEA2016082100541](https://openairdocs.org/sdr/QXEA2016082100541.md): Unknown · odor · Aug 21, 2016 · N415QX · Bombdr DHC8402 · Airborne Auxiliary Power Unit (APU) System
  > 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 20 MINUTES WITH NO ODOR DETECTED. COULD NOT DUPLICATE. RETURNED TO SERVICE.
- [SDR QXEA2016072900485](https://openairdocs.org/sdr/QXEA2016072900485.md): Brake · smoke · Jul 29, 2016 · N415QX · Bombdr DHC8402 · Landing Gear Brake System
  > 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 TIRES AND INSPECTED THE BRAKES AND AXLES, NO DEFECTS NOTED. REPLACED NR 3 AND 4 MAIN TIRES IAW T/
- [SDR QXEA2016072100460](https://openairdocs.org/sdr/QXEA2016072100460.md): Tire · failed · Jul 21, 2016 · N415QX · Bombdr DHC8402 · Tire
  > 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 FITTING AND BLEEDING OF THE NR 1 HYD SYS. OK FOR CONTINUED SERVICE.
- [SDR QXEA2016070600444](https://openairdocs.org/sdr/QXEA2016070600444.md): Wire Harness · shorted · Jul 6, 2016 · N415QX · Bombdr DHC8402 · Electrical Power System Wiring
  > 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 GENERATOR CONTROL HARNESS. OPS CHECKED GOOD, CAUTION LIGHTS REMAINED UNILLUMINATED. RETURNED TO SERVI
- [SDR QXEA2016052300332](https://openairdocs.org/sdr/QXEA2016052300332.md): Seat Track · not reported · May 14, 2016 · N415QX · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach Fittings
  > 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, 51-40-07. COMPLETED INSTALLATION OF SEAT TRACK BY INSTALLING, 6 RIVETS ON SUPPORT BLOCK COMMON TO SE
- [SDR QXEA2016052300330](https://openairdocs.org/sdr/QXEA2016052300330.md): Seat Track · not reported · May 14, 2016 · N415QX · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach Fittings
  > 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-INSTALLED WEB ASSY, PN 85338806-001 COMMON TO SEAT TRACK NR 16 AND NR 23 IAW SRM 51-42-05, SRM 51-41-
- [SDR QXEA2016052300328](https://openairdocs.org/sdr/QXEA2016052300328.md): Web · corroded · May 13, 2016 · N415QX · Bombdr DHC8402 · Fuselage Miscellaneous Structure
  > 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-PASSENGER DOOR PART REQUIRES REPLACEMENT. LOCATED DRILLED AND REPLACED MACHINED WEB PN 85329687-1
- [SDR QXEA2016052400344](https://openairdocs.org/sdr/QXEA2016052400344.md): Strap · corroded · May 11, 2016 · N415QX · Bombdr DHC8402 · Fuselage Miscellaneous Structure
  > 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 SRM 53-00-00-02-20, PARA 6 A-B AND FIG 201, SHT 1 AND SHT 3. CW ET/UT INSP REF NDTM 51-00-06 + 51-00
- [SDR QXEA2016052400343](https://openairdocs.org/sdr/QXEA2016052400343.md): Web · corroded · May 11, 2016 · N415QX · Bombdr DHC8402 · Fuselage Miscellaneous Structure
  > 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-FWD PASSENGER DOOR. PARTS REQUIRES REPLACMENT. LOCATED, DRILLED AND REPLACED MACHINED WEB, PN 85329
- [SDR QXEA2016052400323](https://openairdocs.org/sdr/QXEA2016052400323.md): Intercostal · corroded · May 11, 2016 · N415QX · Bombdr DHC8402 · Fuselage Miscellaneous Structure
  > 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 85329342-105 IAW SRM 53-20-17, STRUCT IDENT-01 ITEM 57. ORDERED NEW INTERCOSTAL, PN 85329345-105.
- [SDR QXEA2016052300325](https://openairdocs.org/sdr/QXEA2016052300325.md): Channel · corroded · May 11, 2016 · N415QX · Bombdr DHC8402 · Fuselage Miscellaneous Structure
  > 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 THICKNESS IAW SRM 53-20-23, REPAIR -01. REMAINING MATERIAL THICKNESS ON UPPER SURFACE IS 0.035" OUT O
- [SDR QXEA2016052300324](https://openairdocs.org/sdr/QXEA2016052300324.md): Threshold · corroded · May 11, 2016 · N415QX · Bombdr DHC8402 · Fuselage Miscellaneous Structure
  > 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 SURROUND REF SRM 51-42-05. INSTALLED NEW THRESHOLD PLATE, PN 85329532-001, REF SRM 51-42-05, REPAIR
- [SDR QXEA2016052300327](https://openairdocs.org/sdr/QXEA2016052300327.md): Support Angle · corroded · May 10, 2016 · N415QX · Bombdr DHC8402 · Fuselage Miscellaneous Structure
  > 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 SUPPORT ANGLES, PN 85329333-103 FROM MACHINED INTERCOSTAL AT MCD LOWER SURROUND. REF SRM 51-42-05, 2
- [SDR QXEA2016052300326](https://openairdocs.org/sdr/QXEA2016052300326.md): Door Sill · corroded · May 10, 2016 · N415QX · Bombdr DHC8402 · Fuselage Miscellaneous Structure
  > 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 IAW TASK CARD 6-53-1160-FWD PAX DOOR. PERFORM REPAIR REF SRM 53-20-17, REPAIR -02. REMOVED DAMAGED
- [SDR QXEA2016051100306](https://openairdocs.org/sdr/QXEA2016051100306.md): Intercostal · not reported · May 8, 2016 · N415QX · Bombdr DHC8402 · Fuselage Miscellaneous Structure
  > 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 85334920-101, REF SRM 51-42-05, REPAIR 10. REMOVED INTERCOSTAL, PN 8533499-101, REF SRM 51-42-05 4C. INSTAL
- [SDR QXEA2016051100305](https://openairdocs.org/sdr/QXEA2016051100305.md): Seat Track · not reported · May 8, 2016 · N415QX · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach Fittings
  > 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 8530-7495-112 AT X 176.0 TO X 49.50 Y 9.250 REF SRM 51-42-05 AND DWG 85307401, RELEASE P, REV C.
- [SDR QXEA2016052300329](https://openairdocs.org/sdr/QXEA2016052300329.md): Seat Track · not reported · May 7, 2016 · N415QX · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach Fittings
  > 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 OF BULKHEAD ON SEAT TRACK 10, REF SRM 51-41-00. INSTALLED 2EA GROUND CABLES ON SEAT TRACK NR 10 APPR
- [SDR QXEA2016051100301](https://openairdocs.org/sdr/QXEA2016051100301.md): Seat Track · damaged · May 5, 2016 · N415QX · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach Fittings
  > 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.md): Seat Track · damaged · May 4, 2016 · N415QX · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach Fittings
  > 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 TRACKS 10 & 11 IAW SRM 51-40-07 & DWG 85528201, REV E.
- [SDR QXEA2016051100303](https://openairdocs.org/sdr/QXEA2016051100303.md): Seat Track · damaged · May 4, 2016 · N415QX · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach Fittings
  > 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 & 12 IAW SRM 51-40-07 & DWG 85328201, REV E.
- [SDR QXEA2016052300334](https://openairdocs.org/sdr/QXEA2016052300334.md): Doubler · corroded · May 3, 2016 · N415QX · Bombdr DHC8402 · Fuselage Main, Plate/Skin
  > 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.md): Rib · cracked · May 3, 2016 · N415QX · Bombdr DHC8402 · Wing, Rib/Bulkhead
  > 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 REF SRM 51-42-05, 51-40-15. INSTALLED NEW REPAIR ANGLE BACK INTO L/E PANEL 611AR ON BOTTOM CORNER RE
- [SDR QXEA2016052300322](https://openairdocs.org/sdr/QXEA2016052300322.md): Rib · cracked · May 2, 2016 · N415QX · Bombdr DHC8402 · Wing, Rib/Bulkhead
  > 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 SRM 57-40-00, REPAIR-07, SECTION 7, "PROCEDURE" PG 202, STEPS 3 THROUGH 10, PG 203+204 RESPECTIVELY
- [SDR QXEA2016052300333](https://openairdocs.org/sdr/QXEA2016052300333.md): Doubler · corroded · May 1, 2016 · N415QX · Bombdr DHC8402 · Fuselage Main, Plate/Skin
  > 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.md): Seat Track · not reported · May 1, 2016 · N415QX · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach Fittings
  > 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 51-42-05 REPAIR-01 AND SRM 51-42-45, REPAIR-01.
- [SDR QXEA2016052300320](https://openairdocs.org/sdr/QXEA2016052300320.md): Bushing · unknown · Apr 27, 2016 · N415QX · Bombdr DHC8402 · Passenger/Crew Doors
  > 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 52-12-11-000-801, STEP 4AI, 2-8. INSTALLED NEW OVER CENTER SPRINGS ON AFT PAX DOOR REF AMM 52-12-11-400-801,
- [SDR QXEA2016040500244](https://openairdocs.org/sdr/QXEA2016040500244.md): Governor · no test · Apr 5, 2016 · N415QX · Bombdr DHC8402 · Propeller Controlling System
  > 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. CLEARED FAULT AND PERFORMED ANOTHER OVERSPEED GOVERNOR CHECK. PASSED IAW FIM TASK 61-20-05-810-829 AND
- [SDR QXEA2016021700149](https://openairdocs.org/sdr/QXEA2016021700149.md): Housing · broken · Feb 17, 2016 · N415QX · Bombdr DHC8402 · Emergency Lighting
  > RIGHT FORWARD EMERGENCY EXIT LOWER EMERGENCY EXIT LIGHT HOUSING CRACKED AND BROKEN. REPLACED HOUSING. CHECKS GOOD.
- [SDR QXEA2015120300636](https://openairdocs.org/sdr/QXEA2015120300636.md): Lamp · inoperative · Dec 3, 2015 · N415QX · Bombdr DHC8402 · Emergency Lighting
  > FORWARD F/A EMERGENCY SWITCH LIGHT "NORMAL" INDICATION INOPERATIVE. RELAMPED AS REQUIRED.
- [SDR QXEA2015110700591](https://openairdocs.org/sdr/QXEA2015110700591.md): Line · failed · Nov 7, 2015 · N415QX · Bombdr DHC8402 · Propeller/Rotor Anti-Ice/De-Ice System
  > ENROUTE DE-ICE PRESSURE CAUTION ILLUMINATED. DIVERTED AND ACCOMPLISHED AN UNEVENTFUL LANDING. REPLACED DEICE BOOT SUPPLY LINE, HOSE AT WING L/E 613AR. RETURNED TO SERVICE.
- [SDR QXEA2015090600453](https://openairdocs.org/sdr/QXEA2015090600453.md): Light · malfunctioned · Sep 6, 2015 · N415QX · Bombdr DHC8402 · Emergency Lighting
  > 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 NOTED. RETURNED TO SERVICE.
- [SDR QXEA2015061800342](https://openairdocs.org/sdr/QXEA2015061800342.md): Lamp · inoperative · Jun 18, 2015 · N415QX · Bombdr DHC8402 · Emergency Lighting
  > "NORMAL" INDICATION, BACK LIGHT INOPERATIVE IN THE F/A EMERGENCY LIGHT SWITCH. RELAMPED SWITCH. OPS CHECKS GOOD.
- [SDR QXEA2015052100263](https://openairdocs.org/sdr/QXEA2015052100263.md): Battery · failed · May 21, 2015 · N415QX · Bombdr DHC8402 · Emergency Lighting
  > 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. REPLACED THE EMERGENCY BATTERIES IAW AMM 33-51-00-820-801. OPS CHECKS GOOD.
- [SDR QXEA2015031900145](https://openairdocs.org/sdr/QXEA2015031900145.md): Sensor · malfunctioned · Mar 19, 2015 · N415QX · Bombdr DHC8402 · Engine Oil Indicating System
  > INTERMITTENT NO OIL TEMP NR 2 INDICATION DURING START AND SHUTDOWN. RETURN TO FIELD. LANDING UNEVENTFUL. INTERROGATED CDS. FAULT CODE 781. CLEARED FAULT CODE. REPLACED NR 2 MOT SENSOR IAW AMM 79-32-01-000-801 AND 79-32-01-400-801. FUNCTIONAL TESTS GOOD I
- [SDR QXEA2015030100105](https://openairdocs.org/sdr/QXEA2015030100105.md): Control Unit · malfunctioned · Mar 1, 2015 · N415QX · Bombdr DHC8402 · Propeller Controlling System
  > 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 FURTHER DEFECTS NOTED.
- [SDR QXEA2014110400893](https://openairdocs.org/sdr/QXEA2014110400893.md): Battery Pack · inoperative · Nov 4, 2014 · N415QX · Bombdr DHC8402 · Emergency Lighting
  > 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 33-51-00-400-801. CHECKS GOOD.

Next page: https://openairdocs.org/deregistered/N415QX-2019-02-14/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE n_number = 'N415QX' AND deregistration_id = 'N415QX-2019-02-14'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N415QX-2019-02-14/reports

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