# Service difficulty reports: N416QX, cancelled Oct 31, 2018

A list on [N416QX, cancelled Oct 31, 2018](https://openairdocs.org/deregistered/N416QX-2018-10-31.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 8 · 387 reports

- [SDR QXEA2018041600143](https://openairdocs.org/sdr/QXEA2018041600143.md): Light · loose · Apr 15, 2018 · N416QX · Bombdr DHC8402 · Emergency Lighting
  > 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.md): Warning Message · false activation · Feb 15, 2018 · N416QX · Bombdr DHC8402 · Trailing Edge Flap Control System
  > FLAP POWER CAUTION ILLUMINATED DURING FINAL, SELECTING FLAPS FROM 5 TO 10. RAN E & A CHECKLIST, FLAP POWER CAUTION EXTINGUISGED. NO FURTHER ISSUES, FLAPS OPERATED NORMALLY. LANDING UNEVENTFUL. REMOVED FROM SERVICE. PERFORMED OPERATIONAL TEST OF THE WING FLAP
- [SDR QXEA2018021300058](https://openairdocs.org/sdr/QXEA2018021300058.md): Igniter · failed · Feb 13, 2018 · N416QX · Bombdr DHC8402 · APU Start/Ignition System
  > 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 A AND B. APU OPS CHECKED GOOD. RETURNED TO SERVICE.
- [SDR QXEA2018011000012](https://openairdocs.org/sdr/QXEA2018011000012.md): Lamp · inoperative · Jan 10, 2018 · N416QX · Bombdr DHC8402 · Emergency Lighting
  > EMERGENCY LIGHT SWITCH AT FORWARD FA POSITION, BACKGROUND LIGHT APPEARS INOPERATIVE. REMOVED FROM SERVICE. REPLACED THE LAMP IN THE EMERGENCY LIGHT SWITCH. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA2017121100696](https://openairdocs.org/sdr/QXEA2017121100696.md): Engine · failed · Dec 8, 2017 · N416QX · Bombdr DHC8402 · Engine (Turbine/Turboprop)
  > 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 REMOVED FROM SERVICE. REPLACED THE #2 ENGINE, #2 PROPELLER, AND #2 AC GENERATOR. ALL OPS CHECKS GOOD.
- [SDR QXEA2017112800684](https://openairdocs.org/sdr/QXEA2017112800684.md): Lamp · inoperative · Nov 28, 2017 · N416QX · Bombdr DHC8402 · Emergency Lighting
  > EMERGENCY LIGHT PANEL LIGHTS INOPERATIVE. REMOVED FROM SERVICE. REPLACED THE LAMPS IN THE PANEL. BACKLIGHTING NOW ILLUMINATES NORMALLY. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA2017091900576](https://openairdocs.org/sdr/QXEA2017091900576.md): Sensor · malfunctioned · Sep 18, 2017 · N416QX · Bombdr DHC8402 · Landing Gear Position and Warning
  > 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 32-61-06-830-801, AND MCN 632765-01. OPS TESTED GOOD. RETURNED TO SERVICE.
- [SDR QXEA2017080700504](https://openairdocs.org/sdr/QXEA2017080700504.md): Door · binding · Aug 6, 2017 · N416QX · Bombdr DHC8402 · Fixed Inner Doors
  > FORWARD EMERGENCY STOWAGE COMPARTMENT DOOR IS STUCK. REMOVED FROM SERVICE. FREED THE FWD EMERGENCY STOWAGE COMPARTMENT DOOR. CYCLED THE DOOR OPEN AND CLOSE MULTIPLE TIMES AND OPS CHECKED GOOD. NO FURTHER DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO
- [SDR QXEA2017071000460](https://openairdocs.org/sdr/QXEA2017071000460.md): Proximity Sensor · malfunctioned · Jul 8, 2017 · N416QX · Bombdr DHC8402 · Landing Gear Position and Warning
  > DURING CLIMB, A RED NOSE GEAR UNSAFE LIGHT INDICATED. LIGHT WAS INTERMITTENT, ON AND OFF. REMOVED FROM SERVICE. REPLACED NLG PROXIMITY SENSOR. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA2017050800345](https://openairdocs.org/sdr/QXEA2017050800345.md): Switch · malfunctioned · May 6, 2017 · N416QX · Bombdr DHC8402 · Emergency Lighting
  > 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 THE BACK OF THE SWITCH. CHARGED EMERGENCY LIGHT BATTERIES & OPS CHECKED IAW AMM 33-51-00-710-803. O
- [SDR QXEA2017041200249](https://openairdocs.org/sdr/QXEA2017041200249.md): Engine · failed · Apr 11, 2017 · N416QX · Bombdr DHC8402 · Engine (Turbine/Turboprop)
  > 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 LEVEL OFF FLUCTUATIONS CONTINUED AT PROPS 850 (830-870). AFTER 2 OR 3 MIN #2 PEC CAUTION LIGHT ILLUMINA
- [SDR QXEA2017041200248](https://openairdocs.org/sdr/QXEA2017041200248.md): Tire · failed · Apr 10, 2017 · N416QX · Bombdr DHC8402 · Tire
  > 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 05-50-61-210-801 NO DAMAGE FOUND. RETURNED TO SERVICE.
- [SDR QXEA2017032700177](https://openairdocs.org/sdr/QXEA2017032700177.md): Screw · loose · Mar 26, 2017 · N416QX · Bombdr DHC8402 · Flight Compartment Windows
  > 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 56-10-00-280-801. PRESSURIZED ACFT IAW AMM 21-00-00-863-801. PRESSURIZED GOOD AT.5 PSID. NO LEAKS/NOI
- [SDR QXEA2017020800045](https://openairdocs.org/sdr/QXEA2017020800045.md): Pivot Assy · malfunctioned · Feb 6, 2017 · N416QX · Bombdr DHC8402 · Passenger/Crew Doors
  > 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 DOOR & VENT DOOR IAW TASK 52-00-00-830-801. OPS TEST GOOD.
- [SDR QXEA2017011300010](https://openairdocs.org/sdr/QXEA2017011300010.md): Light · loose · Jan 12, 2017 · N416QX · Bombdr DHC8402 · Emergency Lighting
  > EMERGENCY LIGHT LOOSE AT ROW 1AB. SECURED THE LIGHT.
- [SDR QXEA2017010900002](https://openairdocs.org/sdr/QXEA2017010900002.md): Relay · malfunctioned · Jan 8, 2017 · N416QX · Bombdr DHC8402 · Emergency Lighting
  > 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 SWITCH IS TURNED ON. TROUBLE SHOT EMERG LIGHT SYSTEM AND FOUND LIGHTS ALTERNATE WHEN SWITCHING BETW
- [SDR QXEA2016121600795](https://openairdocs.org/sdr/QXEA2016121600795.md): Relay · malfunctioned · Dec 16, 2016 · N416QX · Bombdr DHC8402 · Emergency Lighting
  > 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 SYSTEM REF TASK 33-51-00-710-803.OP'S CHECK GOOD. DUE TO INTERMITTANT FAILURES R&R 3351 K1 & K2 RELA
- [SDR QXEA2016082600563](https://openairdocs.org/sdr/QXEA2016082600563.md): Seal · failed · Aug 28, 2016 · N416QX · Bombdr DHC8402 · Propeller Controlling System
  > 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 TESTED GOOD, NO FURTHER DEFECTS NOTED AT THIS TIME. RETURNED TO SERVICE.
- [SDR QXEA2016062800440](https://openairdocs.org/sdr/QXEA2016062800440.md): Battery Pack · failed · Jun 28, 2016 · N416QX · Bombdr DHC8402 · Emergency Lighting
  > EMERGENCY BATTERY PACKS IN THE NR 2 POSITION FAIL THE 10 MINUTE TEST. REPLACED BATTERY PACK.
- [SDR QXEA2016062200406](https://openairdocs.org/sdr/QXEA2016062200406.md): Light · peeling · Jun 22, 2016 · N416QX · Bombdr DHC8402 · Emergency Lighting
  > FLOOR PATH LIGHT STRIP AT FORWARD GALLEY PEELING UP. REPLACED FLOOR STRIP. RETURNED TO SERVICE.
- [SDR QXEA2016052200335](https://openairdocs.org/sdr/QXEA2016052200335.md): Warning Light · false activation · May 22, 2016 · N416QX · Bombdr DHC8402 · Airfoil Anti/De-ice System
  > 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 EXTINGUISHED BUT THEN CAME BACK ON. THE MOST OTBD BOOT LIGHT ON LT WING DID NOT ILLUMINATE. DIVERTED AN
- [SDR QXEA2016012800079](https://openairdocs.org/sdr/QXEA2016012800079.md): Light · loose · Jan 28, 2016 · N416QX · Bombdr DHC8402 · Emergency Lighting
  > FLOOR STRIP AT ROW 2D LOOSE. RESECURED FLOOR STRIP AT 2D. RETURNED TO SERVICE.
- [SDR QXEA2016012600062](https://openairdocs.org/sdr/QXEA2016012600062.md): Lead · damaged · Jan 26, 2016 · N416QX · Bombdr DHC8402 · Ice/Rain Protection System Wiring
  > 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 EXTINGUISHED, BUT REILLUMINATED UPON SECOND CYCLE OF PROPS. THEN WENT OUT ON IT'S OWN AND DID NOT
- [SDR QXEA2015121500649](https://openairdocs.org/sdr/QXEA2015121500649.md): Hydraulic System · low · Dec 15, 2015 · N416QX · Bombdr DHC8402 · Hydraulic System, Main
  > NR 2 HYDRAULIC QUANTITY LOW. DIVERTED AND ACCOMPLISHED UNEVENTFUL LANDING. ACFT CURRENTLY OUT OF SERVICE FOR REPAIRS.
- [SDR QXEA2015120900637](https://openairdocs.org/sdr/QXEA2015120900637.md): Seat Track · corroded · Dec 2, 2015 · N416QX · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach Fittings
  > 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 BS X71.2, 116, 176, 236, 301 & 361 MID FUSELAGE. REF SRM 51-41-00, PN 82570102-003/005. DRIP ANGL
- [SDR QXEA2015121600644](https://openairdocs.org/sdr/QXEA2015121600644.md): Seat Track · corroded · Nov 29, 2015 · N416QX · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach Fittings
  > 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. INSTALLED FABRICATED ANGLES, PN 85307495-115 AND PN 85307495-119 COMMON TO SEAT TRACK NR 6 AND N
- [SDR QXEA2015120900638](https://openairdocs.org/sdr/QXEA2015120900638.md): Seat Track · corroded · Nov 29, 2015 · N416QX · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach Fittings
  > 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 SPLICES AT SEAT TRACK NR 5 AND NR 6 AT FS X102.0, Y9.250, PN 85338216-101 AND PN 85338215-101, RE
- [SDR QXEA2015111000583](https://openairdocs.org/sdr/QXEA2015111000583.md): Seat Track · corroded · Nov 5, 2015 · N416QX · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach Fittings
  > 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 51-40-15-002-01. INSTALLED 21 ON LOCK FASTENER COMMON TO SEAT TRACK NR 1 AND VERTICAL WEB BETWEEN FS X 32.4 AND X
- [SDR QXEA2015121600643](https://openairdocs.org/sdr/QXEA2015121600643.md): Attach Fitting · corroded · Nov 4, 2015 · N416QX · Bombdr DHC8402 · Fuselage Main, Attach Fittings
  > 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 END TO FOM, BS X 47.975, REF SRM 51-42-05. REATTACHED FLOOR SUPPORT AT AFT AND FS X 47.975 IAW SRM
- [SDR QXEA2015110300571](https://openairdocs.org/sdr/QXEA2015110300571.md): Seat Track · damaged · Nov 1, 2015 · N416QX · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach Fittings
  > 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, Y-9.250 IAW SRM 51-40-07. COMPLETED LOCATING & DRILLING NEW OUTER SPLICE COMMON TO SEAT TRACK NR
- [SDR QXEA2015110900580](https://openairdocs.org/sdr/QXEA2015110900580.md): Seat Track · corroded · Oct 28, 2015 · N416QX · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach Fittings
  > 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 5.M 1-8 AND SRM 51-42-05 PARA 4.E 1-8. SEAT TRACK, NR 19 DRILLED AND LOCATED FROM APPROXIMATELY B
- [SDR QXEA2015110300572](https://openairdocs.org/sdr/QXEA2015110300572.md): Seat Track · corroded · Oct 28, 2015 · N416QX · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach Fittings
  > 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.md): Attach Fitting · corroded · Oct 26, 2015 · N416QX · Bombdr DHC8402 · Fuselage Main, Attach Fittings
  > 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 FRAME BS X94.800, STR 24 REF SRM 51-42-05. INSTALLED NEW CLEAT PN 85328131-175 ON FS X 94.800 STR 24L,
- [SDR QXEA2015103000560](https://openairdocs.org/sdr/QXEA2015103000560.md): Seat Track · corroded · Oct 25, 2015 · N416QX · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach Fittings
  > 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 51-42-05 AND DWG 85338251, REV A.
- [SDR QXEA2015103000559](https://openairdocs.org/sdr/QXEA2015103000559.md): Doubler · corroded · Oct 25, 2015 · N416QX · Bombdr DHC8402 · Fuselage Miscellaneous Structure
  > 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 LOCATED AT AFT EDGE OF PORT 3.750 ABOVE THE LOWER EDGE, AREA 1 HAS EXFOLIATION DAMAGE 0.053 D AND 0.50
- [SDR QXEA2015103000567](https://openairdocs.org/sdr/QXEA2015103000567.md): Splice · corroded · Oct 17, 2015 · N416QX · Bombdr DHC8402 · Fuselage Main, Attach Fittings
  > 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. DRILLED AND LOCATED HOLES COMMON TO SEAT TRACK NR 6 AND SPLICE MEMBERS AT FS 102.5 AND Y-9.250 REF
- [SDR QXEA2015111000582](https://openairdocs.org/sdr/QXEA2015111000582.md): Seat Track · corroded · Oct 16, 2015 · N416QX · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach Fittings
  > 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, QTY 7. LOCATED AND DRILLED DADO PANEL ANGLES, QTY 7 ON NEW SEAT TRACK, REF SRM 51-40-07. SOLID RIVE
- [SDR QXEA2015103000565](https://openairdocs.org/sdr/QXEA2015103000565.md): Cup · corroded · Oct 15, 2015 · N416QX · Bombdr DHC8402 · Fuselage Miscellaneous Structure
  > 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 BS X156.00, STR 24, REF SRM 51-42-05. INSTALLED NEW CLEAT AT FRAME BS X156.0, STR 24P, PN:85328131
- [SDR QXEA2015103000564](https://openairdocs.org/sdr/QXEA2015103000564.md): Cup · corroded · Oct 15, 2015 · N416QX · Bombdr DHC8402 · Fuselage Miscellaneous Structure
  > 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 FRAME STN.X71.200, STR 24, REF SRM 51-42-05. INSTALLED, NEW, CLEAT AT FRAME BS X71.2, STR 24P REF SRM
- [SDR QXEA2015101300563](https://openairdocs.org/sdr/QXEA2015101300563.md): Seat Track · corroded · Oct 13, 2015 · N416QX · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK CORRODED. REMOVED AND REPLACED IAW SRM 51-42-05.
- [SDR QXEA2015101300562](https://openairdocs.org/sdr/QXEA2015101300562.md): Seat Track · corroded · Oct 13, 2015 · N416QX · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK CORRODED. DEBURRED AND INSTALLED NEW SEAT TRACK IAW SRM 51-41-00-08-01.
- [SDR QXEA2015103000561](https://openairdocs.org/sdr/QXEA2015103000561.md): Seat Track · corroded · Oct 13, 2015 · N416QX · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach Fittings
  > 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.md): Seat Track · corroded · Oct 13, 2015 · N416QX · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach Fittings
  > 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.md): Shear Tie · corroded · Oct 11, 2015 · N416QX · Bombdr DHC8402 · Fuselage Internal Mounting Structure
  > 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 SRM 51-40-078, REPAIR 01. APPLIED TOP COAT TO NEW SHEAR ANGLE REF SRM 51-25-15, REPAIR 01. R & R SHEA
- [SDR QXEA2015102300550](https://openairdocs.org/sdr/QXEA2015102300550.md): Seat Track · corroded · Oct 10, 2015 · N416QX · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach Fittings
  > 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.md): Seat Track · corroded · Oct 9, 2015 · N416QX · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach Fittings
  > 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.md): Seat Track · corroded · Oct 4, 2015 · N416QX · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK, NR 14 CORRODED. REMOVED CORROSION IAW SRM 53-20-49, REPAIR-02, FIG 201.
- [SDR QXEA2015062700343](https://openairdocs.org/sdr/QXEA2015062700343.md): Transducer · malfunctioned · Jun 27, 2015 · N416QX · Bombdr DHC8401 · Stall Warning System
  > DURING CLIMB PASSING THROUGH APPROXIMATELY 5800, PUSHER SYS FAIL CAUTION LIGHT ILLUMINATED. DIVERTED LANDING UNEVENTFUL. INSPECTED AND FOUND R AOA A-C BREAKER TRIPPED. R & R RT AOA TRANSDUCER IAW AMM 27-33-26-000-801 AND 27-33-26-400-801 LLM RTS C/W T/C 627
- [SDR QXEA2015051500243](https://openairdocs.org/sdr/QXEA2015051500243.md): Pseu · faulted · May 15, 2015 · N416QX · Bombdr DHC8402 · Landing Gear Position and Warning
  > ON DEPARTURE, RT MAIN GEAR INDICATOR, GREEN LIGHT, REMAINED ILLUMINATED. ACCOMPLISHED MANUAL GEAR EXTENSION. RETURNED TO FIELD. LANDING UNEVENTFUL. FOUND THE FOLLOWING RELATED FAULTS IN PSEU, FAULT HISTORY D/N01A FAILED AND D/N02A FAILED, NO CURRENT RELATED F
- [SDR QXEA2015012000020](https://openairdocs.org/sdr/QXEA2015012000020.md): Bearing · failed · Jan 20, 2015 · N416QX · Bombdr DHC8402 · Main Landing Gear Strut/Axle/Truck
  > 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 MAIN WHEEL ASSY BEARING FAILURE, NR 4. RETURNED TO SERVICE.

Next page: https://openairdocs.org/deregistered/N416QX-2018-10-31/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 = 'N416QX' AND deregistration_id = 'N416QX-2018-10-31'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N416QX-2018-10-31/reports

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