# Service difficulty reports: N429QX

A list on [N429QX](https://openairdocs.org/aircraft/N429QX.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 5 · 217 reports

- [SDR QXEA2020080400230](https://openairdocs.org/sdr/QXEA2020080400230.md): Warning Message · illuminated · Jul 31, 2020 · N429QX · Bombdr DHC8402 · Emergency Lighting
  > WHEN TURNING OF AIRCRAFT POWER EMERGENCY LIGHTS ASSOCIATED WITH POWER SUPPLY PS1 ILLUMINATED.
- [SDR QXEA2019011100011](https://openairdocs.org/sdr/QXEA2019011100011.md): Pump · malfunctioned · Jan 10, 2019 · N429QX · Bombdr DHC8402 · Propeller Feathering/Reversing
  > FOUND NR 1 ENG ALT FEATHER PUMP TO BE LEAKING AT THE ASSY. JOINTS. REMOVED AND REPLACED #1 FEATHERING PUMP IAW AMM TASK 61-20-31-000-801 AND 61-20-31-400-801 OPS AND LEAK CHECK GOOD.
- [SDR QXEA2018122400466](https://openairdocs.org/sdr/QXEA2018122400466.md): Light · loose · Dec 21, 2018 · N429QX · Bombdr DHC8402 · Emergency Lighting
  > CREW REPORTS CLEAR PLASTIC COVER ON LH FLOOR LIGHT STRIPS IS LIFTING AT ROW 18AB. REMOVED FROM SERVICE. RESECURED CLEAR PLASTIC COVER ON LH FLOOR LIGHTING STRIP @ 18B. NO OTHER DEFECTS NOTED. RETURNED TO SERVICE.
- [SDR QXEA2018120300446](https://openairdocs.org/sdr/QXEA2018120300446.md): Control Valve · malfunctioned · Dec 2, 2018 · N429QX · Bombdr DHC8402 · Pneumatic Distribution System
  > TAKEOFF ABORTED < 40 KTS FOR #1 BLEED HOT CAUTION. REMOVED FROM SERVICE. FOUND FAULT IN CDS L NAPSOV,PACK FCV. CLEAR FAULT. GROUND RUN #1 & #2 ENG. NO AIR FLOW IN CABIN.FAULT RETURNED IN CDS. REMOVED AND REPLACED #1 NACELLE SHUTOFF VALVE REF AMM TASK 36-11-19-
- [SDR QXEA2018082800315](https://openairdocs.org/sdr/QXEA2018082800315.md): Propeller · out of balance · Aug 27, 2018 · N429QX · Bombdr DHC8402 · Propeller Assembly
  > DURING CRUISE, SLOW AIRSPEED, FIRST NOTICED AT 210 KTS, NOTICEABLE VIBRATION. TRIED PUTTING ANVS ON PAUSE WITH NO CHANGE. VIBRATION WORSENED DURING POWER REDUCTION. PROPS WERE AT 850. TORQUE ABOUT 50%. REMOVED FROM SERVICE. IAW WO 247742, 00001 THROUGH 00
- [SDR QXEA2018082800314](https://openairdocs.org/sdr/QXEA2018082800314.md): Propeller · out of balance · Aug 25, 2018 · N429QX · Bombdr DHC8402 · Propeller Assembly
  > FAIRLY SIGNIFICANT VIBRATION ON THE NR 1 PROPELLER. WHEN POWER LEVERS WERE REDUCED BELOW ABOUT 65%, TORQUE VIBRATION WAS MOST NOTICEABLE. VIBRATION WOULD BECOME LESS NOTICEABLE AFTER SEVERAL SECONDS AND THEN COME BACK WHEN A POWER CHANGE WAS MADE. REMOVED
- [SDR QXEA2018082200301](https://openairdocs.org/sdr/QXEA2018082200301.md): Brake · smoke · Aug 21, 2018 · N429QX · Bombdr DHC8402 · Landing Gear Brake System
  > ON A WALK AROUND, FOUND THE NR 4 BRAKE SMOKING. TEMP READING APPROXIMATELY 117C OUTER BRAKES ARE AROUND 73C. REMOVED FROM SERVICE. COMPLIED WITH INSPECTION AFTER APPLICATION OF EXCESSIVE BRAKING IAW AMM 05-50-56-1-210-801. NO DEFECTS NOTED. NO PARTS REPLACED.
- [SDR QXEA2018082200299](https://openairdocs.org/sdr/QXEA2018082200299.md): Line · leaking · Aug 19, 2018 · N429QX · Bombdr DHC8402 · Hydraulic System, Main
  > DURING CRUISE, RECEIVED A NR 1 HYD ISOLATION VALVE CAUTION, ALONG WITH AN INBD ROLL SPOILER CAUTION. THE NR 1 HYD QTY WAS AT ABOUT 20%. RAN THE CHECKLIST. AT THIS TIME THE NR 1 HYD PRESSURE STARTED TO DROP. THE QTY AND PRESSURE WENT TO 0 % FOR THE NR 1 SY
- [SDR QXEA2018071900262](https://openairdocs.org/sdr/QXEA2018071900262.md): Engine · failed · Jul 17, 2018 · N429QX · Bombdr DHC8402 · Engine (Turbine/Turboprop)
  > CLIMBING THROUGH APPROX 3000' FEET MSL THE NR 1 ENGINE SURGED TWICE THEN SHUT DOWN. THERE WERE NO CAUTION OR WARNING LIGHTS PRIOR TO THE SHUTDOWN. RETURNED TO FIELD. LANDING UNEVENTFUL. REMOVED FROM SERVICE. DEBRIS FOUND IN MAIN OIL FILTER. REF W/O 245318 FOR
- [SDR QXEA2018071200257](https://openairdocs.org/sdr/QXEA2018071200257.md): Propeller · out of balance · Jul 12, 2018 · N429QX · Bombdr DHC8402 · Propeller Assembly
  > NR 1 ENGINE PROP VIBRATION ENROUTE. DIVERTED. LANDING UNEVENTFUL. REMOVED FROM SERVICE. PERFORMED PROPELLER BALANCE ON NR 1 ENGINE IAW 6611001. INITIAL IPS SHOWED.317. APPLIED SOLUTION. PROJECTED IPS ARE.006. WEIGHTS APPLIED AT HOLES 11(30G), 12(50G), 13(50G
- [SDR QXEA2018062500236](https://openairdocs.org/sdr/QXEA2018062500236.md): Proximity Sensor · out of adjust · Jun 22, 2018 · N429QX · Bombdr DHC8402 · Landing Gear Position and Warning
  > NLG DOOR LIGHT FLASHED PERIODICALLY DURING CLIMB AND LEVEL OFF. NO INDICATION DURING LEVEL FLIGHT. NO DOOR CHATTER SOUND ASSOCIATED. REMOVED FROM SERVICE. PERFORMED GVI OF THE NLG DOORS AND HINGES WITH NO DEFECTS NOTED. INTERROGATED PSEU AND FOUND THE NG D
- [SDR QXEA2018061800222](https://openairdocs.org/sdr/QXEA2018061800222.md): Contact · damaged · Jun 15, 2018 · N429QX · Bombdr DHC8402 · Door System Wiring
  > INTERMITTENT FUSELAGE DOORS WARNING. UNABLE TO CONFIRM WHICH DOOR SINCE EACH WARNING WAS VERY SHORT. PRESSURIZATION WAS NORMAL. ALL DOORS APPEARED CLOSED AND SECURE FROM AN INTERIOR VISUAL CHECK BY THE FLIGHT ATTENDANTS. RETURNED TO FIELD. LANDING UNEVENTFU
- [SDR QXEA2018022300069](https://openairdocs.org/sdr/QXEA2018022300069.md): Lamp · inoperative · Feb 23, 2018 · N429QX · Bombdr DHC8402 · Emergency Equipment
  > FORWARD FLIGHT ATTENDANT EMERGENCY LIGHTING GREEN NORMAL LIGHT OUT. REMOVED FROM SERVICE. REPLACED THE LAMP IN THE FWD FLIGHT ATTENDANT EMERGENCY GREEN NORMAL LIGHT. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA2017121900705](https://openairdocs.org/sdr/QXEA2017121900705.md): Lens · separated · Dec 18, 2017 · N429QX · Bombdr DHC8402 · Emergency Lighting
  > EMERGENCY LIGHT STRIP PLASTIC LENS SEPARATED FROM LIGHT. REMOVED FROM SERVICE. REMOVED DAMAGED LIGHT STRIP, REPLACED WITH NEW. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA2017111700669](https://openairdocs.org/sdr/QXEA2017111700669.md): Probe · malfunctioned · Nov 15, 2017 · N429QX · Bombdr DHC8402 · Pitot/Static Anti-Ice System
  > PITOT HEAT NR 2 CAUTION LIGHT. DIVERTED. LANDING UNEVENTFUL. REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 2 PITOT STATIC PROBE IAW AMM 34-11-06-000, 400-801 AND LEAK CHECKED IAW TC 6341102, OPS CHECKED GOOD. PROBE HEATED NORMALLY AND CAUTION LIGHT EXTING
- [SDR QXEA2017091100552](https://openairdocs.org/sdr/QXEA2017091100552.md): Proximity Sensor · out of rig · Sep 10, 2017 · N429QX · Bombdr DHC8402 · Landing Gear Position and Warning
  > NOSE GEAR DOOR LIGHT CYCLED ON AND OFF CONSISTANTLY FOR ROUGHLY 20 MINS IN THE CLIMB OUT. DID NOT NOTICE AT WHAT EXACT POINT IT CAME ON. ONCE DECISION WAS TO TURN AROUND WAS MADE. THE LIGHT DID NOT CYCLE AGAIN. RETURNED TO FIELD. LANDING UNEVENTFUL. AIRCRAFT
- [SDR QXEA2017072700496](https://openairdocs.org/sdr/QXEA2017072700496.md): Pressure Switch · malfunctioned · Jul 27, 2017 · N429QX · Bombdr DHC8402 · Landing Gear Steering System
  > DURING TAXI OUT, THE NOSE WHEEL STEERING MASTER CAUTION ILLUMINATED AND NOSE WHEEL STEERING WASN'T WORKING. AFTER REFERENCING THE E & A CHECKLIST CAUTION CLEARED. OPTED TO CONTINUE. ON TAKEOFF ROLL, APROX 100KTS, THE NOSE WHEEL STEERING CAUTION ILLUMINATED
- [SDR QXEA2017030800107](https://openairdocs.org/sdr/QXEA2017030800107.md): Bleed Valve · failed · Mar 8, 2017 · N429QX · Bombdr DHC8402 · Compressor Bleed Valve
  > CLIMBING THROUGH 10,000 FT, THE NR 1 FADEC CAUTIONED, WITH POWER PLANT MESSAGE. LEVEL AT 14,000FT ENGINE SURGES OF 10 DEGREES, 15 DEGREES TORQUE. DURING DESCENT DID NOT NOTICE ANY ENGINE SURGES. REMOVED AND REPLACED THE NR 1 P2.2 INTERSTAGE BLEED VALVE IAW
- [SDR QXEA2017020800049](https://openairdocs.org/sdr/QXEA2017020800049.md): Unknown · odor · Feb 8, 2017 · N429QX · Bombdr DHC8402 · Air Distribution System
  > F/A REPORTS SMELL COMING FROM THE AIR CYCLE MACHINE. RAN THE APU WITH THE BLEED AIR ON UNTIL THE CABIN TEMP REACHED 80 DEGREES. NO SMELLS NOTED. RETURNED TO SERVICE. COULD NOT DUPLICATE. RETURNED TO SERVICE.
- [SDR QXEA2016112800741](https://openairdocs.org/sdr/QXEA2016112800741.md): Power Supply · inoperative · Nov 28, 2016 · N429QX · Bombdr DHC8402 · Emergency Lighting
  > WITH THE EMERGENCY LIGHTS SELECTED TO ON, THE FORWARD EMERGENCY LIGHTS DO NOT ILLUMINATE. REPLACED THE FORWARD EMERGENCY LIGHT POWER SUPPLY IAW AMM 33-51-01-00-801 AND 33-51-01-400-801. CHECKS GOOD. RETURNED TO SERVICE.
- [SDR QXEA2016062800438](https://openairdocs.org/sdr/QXEA2016062800438.md): Proximity Sensor · faulty · Jun 28, 2016 · N429QX · Bombdr DHC8402 · Landing Gear Position and Warning
  > AFTER GEAR EXTENSION, RT GEAR DOOR CAUTION ON. ON POST FLIGHT RT GEAR DOOR IS OPEN. FERRIED FOR REPAIRS. REMOVED THE PROXIMITY SENSOR ON THE NR 2 MLG STABILIZER BRACE ASSY AND REPLACED WITH A SERVICEABLE 1 FROM STOCK REF AMM TASK NR 32-11-21-000-801 AND 32
- [SDR QXEA2016062100389](https://openairdocs.org/sdr/QXEA2016062100389.md): Channel · damaged · Jun 9, 2016 · N429QX · Bombdr DHC8402 · Aerodynamic Fairings
  > FOUND DAMAGE ON EXTERNAL PANEL 262HT FUSELAGE LANDING, MARKED. REMOVED REAR SPAR WING TO FUSELAGE FAIRING LANDING STRIP STA X 426.974, PN: 85713402-105, REF SRM 51-42-05, REPAIR-01, PARA 4E, 1-3. INSTALLED REPLACEMENT REAR SPAR WING TO FUSE FAIRING LANDING S
- [SDR QXEA2016062100402](https://openairdocs.org/sdr/QXEA2016062100402.md): Stiffener · broken · Jun 2, 2016 · N429QX · Bombdr DHC8402 · Nacelle/Pylon Miscellaneous Structure
  > RIGHT NACELLE PANEL 424AR HAS BROKEN RIB ANGLE. REMOVED DAMAGED STIFFENER, REF SRM 51-42-05. INSTALLED, DRILLED, LOCATED NEW STIFFENER REF SRM 51-42-05. RESTORED FINISH, REF SRM 51-42-05. SEALED STIFFENER REF SRM 51-23-00.
- [SDR QXEA2016062100399](https://openairdocs.org/sdr/QXEA2016062100399.md): Plate · corroded · Jun 1, 2016 · N429QX · Bombdr DHC8402 · Fuselage Miscellaneous Structure
  > MCD THRESHOLD PLATE CORRODED. MCD THRESHOLD PLATE REMOVED REF SRM 51-42-05. THRESHOLD PLATE INSTALLED REF DWG 85329531, REV A 99/09/08 & REF SRM 51-42-05. TEFLON RUB STRIP REMOVED FROM THRESHOLD PLATE, REF SRM 51-42-05. TEFLON RUB STRIP INSTALLED ON THRESH
- [SDR QXEA2016062100390](https://openairdocs.org/sdr/QXEA2016062100390.md): Support Bracket · cracked · May 31, 2016 · N429QX · Bombdr DHC8402 · Wing Miscellaneous Structure
  > RIGHT WING L/E INBD SUPPORT BRACKET FOR PANEL 422CT IS CRACKED. R & R RT WING L/E INBD SUPPORT BRACKET WITH NEW SERVICEABLE 1, FOR PANEL 422CT, REF SRM 51-40-15, REPAIR -01. DOMED, SEALED 5 EA LOCK FASTENERS, REF SRM 51-23-2. REPAIR -1, FIG 202. FILET SEAL
- [SDR QXEA2016062100396](https://openairdocs.org/sdr/QXEA2016062100396.md): Seat Track · damaged · May 27, 2016 · N429QX · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK NR 10, REQUIRES REPLACEMENT. DISPLACED GROUND CABLES COMMON TO SEAT TRACK NR 10 AT FS X-39.0 IAW SRM 51-11-00, STRUCT IDENT -01, PG 1. REINSTALLED GROUND CABLES COMMON TO SEAT TRACK NR 10 AT FS-39.0, REF SRM 51-41-00, STRUCT IDENT -01. PERFORMED
- [SDR QXEA2016062100393](https://openairdocs.org/sdr/QXEA2016062100393.md): Seat Track · corroded · May 26, 2016 · N429QX · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK NR 25, PN 85337843-103, REQUIRES REPLACEMENT. REMOVED SEAT RAIL 25, PN 85337843-103, FS X 697.60 TO X 726.102, Y12.63 LT IAW SRM 51-42-05-02-01 AND 51-42-15-02-01. INSTALLED SEAT RAIL, NR 25, PN 85337843-103, REF DWG 85338806, DATE 98/05/08 & SRM
- [SDR QXEA2016062100397](https://openairdocs.org/sdr/QXEA2016062100397.md): Seat Track · damaged · May 26, 2016 · N429QX · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK NR 11, REQUIRES REPLACEMENT. REMOVED 2 EA PLASTIC DRIP TRAY'S AT FS X71.2 AND FS X 116.0 IAW SRM 51-41-00 STRUCT IDENT -01, PG 1. INSTALLED 2 EA PLASTIC DRIP TRAYS AT FS X71.2 AND X116.0 SRM 51-41-00, STRUCT ID -01. DISPLACED METAL DRIP ANGLE COM
- [SDR QXEA2016062100394](https://openairdocs.org/sdr/QXEA2016062100394.md): Seat Track · damaged · May 24, 2016 · N429QX · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK NR 15, PN 85338210-115, REQUIRES REPLACEMENT. REMOVED FWD SPLICE OTBD, PN:85338215-101 COMMON TO SEAT TRACK NR 13 REF SRM 51-42-005-02-01 AND 51-40-15-02-01. INSTALLED FWD OTBD SPLICE, PN:85338215-101 COMMON TO SEAT TRACK 13, REF SRM 51-42-05-02-0
- [SDR QXEA2016062100392](https://openairdocs.org/sdr/QXEA2016062100392.md): Splice · damaged · May 24, 2016 · N429QX · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach Fittings
  > OUTER SPLICE, PN 85338215-101 AT FS X 612.0-Y 9.250 COMMON TO SEAT TRACK NR 14 AND NR 15 HAS ELONGATED HOLES. LOCATED AND DRILLED NEW OTBD SPLICE, PN:85338215-101, REF SRM 51-40-07-02-01. INSTALLATION ACCOMPLISHED ON JOB 5416121, OP 196, ITEM 2.
- [SDR QXEA2016062100398](https://openairdocs.org/sdr/QXEA2016062100398.md): Seat Track · damaged · May 24, 2016 · N429QX · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK 14, REQUIRES REPLACEMENT. REMOVED FWD SPLICE OTBD, PN 85338215-101 COMMON TO SEAT TRACK NR 13 REF SRM 51-42-005-02-01 AND 51-40-15-02-01. INSTALLED FWD OTBD SPLICE, PN 85338215-101 COMMON TO SEAT TRACK 13, REF SRM 51-42-05-02-01, 51-40-15-2-01 AND
- [SDR QXEA2016032900225](https://openairdocs.org/sdr/QXEA2016032900225.md): Roller · out of adjust · Mar 29, 2016 · N429QX · Bombdr DHC8402 · Galley Doors
  > UNABLE TO OPEN THE GALLEY SERVICE DOOR FROM THE OUTSIDE, AND DIFFICULT TO OPEN FROM INSIDE. FERRIED AIRCRAFT FOR REPAIRS. ADJUSTED UPPER GUIDE ROLLERS. FUNCTIONAL TESTS GOOD.
- [SDR QXEA2016030900175](https://openairdocs.org/sdr/QXEA2016030900175.md): Warning Message · illuminated · Mar 9, 2016 · N429QX · Bombdr DHC8402 · Door Warning System
  > AFTER TAKEOFF CLIMBING THROUGH 2000FT, STARTED TO ENCOUNTER MODERATE TURBULENCE AND AT THAT TIME THE MASTER WARNING CHIMED AND FUSELAGE DOORS WARNING STAYED ON FOR A FEW SECONDS. THE MASTER WARNING WENT AWAY ALONG WITH THE FUSELAGE DOOR WARNING. ON MFD DOOR
- [SDR QXEA2015122900668](https://openairdocs.org/sdr/QXEA2015122900668.md): Light · unsecure · Dec 29, 2015 · N429QX · Bombdr DHC8402 · Emergency Lighting
  > EMERGENCY LIGHT STRIP AT ROW 1 A/B IS LOOSE. SECURED EMERGENCY LIGHT STRIP. RETURNED TO SERVICE.
- [SDR QXEA2015122900664](https://openairdocs.org/sdr/QXEA2015122900664.md): Trim Panel · malfunctioned · Dec 29, 2015 · N429QX · Bombdr DHC8402 · Rudder Tab Control System
  > RUDDER TRIM RUNAWAY AFTER LEVEL OFF AT FL 240 WITH UNCOMMANDED RT RUDDER TRIM ACTIVATION. ATTEMPTS TO MOVE RUDDER TRIM TO THE LT, RESULTED IN FURTHER RUDDER TRIM TO THE RT. RUD TRIM ACT CB, F7, LT ESS PULLED IAW THE CHECK LIST COORDINATED FLIGHT MAINTAINED W
- [SDR QXEA2015040600186](https://openairdocs.org/sdr/QXEA2015040600186.md): Switch · malfunctioned · Apr 6, 2015 · N429QX · Bombdr DHC8402 · Emergency Lighting
  > EMERGENCY LIGHTS REMAIN ILLUMINATED IN THE CABIN. REPLACED THE F/A EMERGENCY LIGHT SWITCH. RETURNED TO SERVICE.
- [SDR QXEA2015011200011](https://openairdocs.org/sdr/QXEA2015011200011.md): Controller · failed · Jan 12, 2015 · N429QX · Bombdr DHC8402 · Windshield/Door Rain/Ice Removal
  > AFTER SELECTING WINDSHIELD HEAT TO NORMAL, WINDSHIELD CONTROL & WINDSHIELD HOT CAUTIONS BOTH ILLUMINATED. RETURNED TO FIELD. LANDING UNEVENTFUL. FOUND FAULT IN CDS LT WINDSHIELD CONTROL. R & R NR 1 AIC IAW AMM 30-41-01-000-801, 30-41-01-400-801. NO HELP. C/W
- [SDR QXEA2014093000815](https://openairdocs.org/sdr/QXEA2014093000815.md): Lamp · inoperative · Sep 30, 2014 · N429QX · Bombdr DHC8402 · Emergency Lighting
  > CABIN EMERGENCY LIGHT SWITCH NOT ILLUMINATED. REPLACED THE LAMP. ILLUMINATES NORMALLY. RETURNED TO SERVICE.
- [SDR QXEA2014060600463](https://openairdocs.org/sdr/QXEA2014060600463.md): Door · out of rig · Jun 6, 2014 · N429QX · Bombdr DHC8402 · Passenger/Crew Doors
  > F/A & RAMP REPORTED MAIN CABIN DOOR DIFFICULT TO OPEN. PERFORMED FUNCTIONAL TEST OF FWD PAX DOOR IAW AMM 52-11-00-720-802. PAX DOOR FAILED FUNCTIONAL TEST. INTERNAL HANDLE UNLOCK FORCE REQUIRED 45-50 LBF TO UNLOCK, OUT OF LIMITS IAW STEP 3A (1)(B). INTERNA
- [SDR QXEA2014032700250](https://openairdocs.org/sdr/QXEA2014032700250.md): Handle · unsecure · Mar 27, 2014 · N429QX · Bombdr DHC8402 · Passenger/Crew Doors
  > AFT PAX DOOR WARNING ILLUMINATED DURING FLIGHT. RESET MASTER CAUTION, DOOR WARNING STOPPED FLASHING. RETURN TO FIELD, LANDED UNEVENTFUL. INSPECTED AFT PAX DOOR, FOUND AFT PAX DOOR HANDLE OUT APPROX.2500". PUSH IN, LIGHT EXTINGUISHED. OP'S CHECKED A/P DOOR
- [SDR QXEA2014031400225](https://openairdocs.org/sdr/QXEA2014031400225.md): Lamp · inoperative · Mar 14, 2014 · N429QX · Bombdr DHC8402 · Emergency Lighting
  > F/A REPORTED FWD EMERGENCY LIGHT SWITCH GREEN LIGHTS ARE INOPERATIVE. REPLACED LAMPS. SWITCH ILLUMINATED NORMALLY. RETURNED TO SERVICE.
- [SDR QXEA2014031000213](https://openairdocs.org/sdr/QXEA2014031000213.md): Seat · corroded · Mar 2, 2014 · N429QX · Bombdr DHC8402 · Passenger Compartment Equipment
  > FWD OTBD SEAT POST 9 A/B IS CORRODED AT MOUNT. R & R INBD AND OTBD PAX SEAT LEG SPREADERS IAW B/E CMM 25-21-21.
- [SDR QXEA2014031000212](https://openairdocs.org/sdr/QXEA2014031000212.md): Seat · corroded · Mar 2, 2014 · N429QX · Bombdr DHC8402 · Passenger Compartment Equipment
  > FWD OTBD SEAT POST 4 A/B IS CORRODED AT MOUNT. R & R INBD AND OTBD PAX SEAT LEG SPREADERS IAW B/E CMM 25-21-21.
- [SDR QXEA2014031000211](https://openairdocs.org/sdr/QXEA2014031000211.md): Seat · corroded · Mar 2, 2014 · N429QX · Bombdr DHC8402 · Passenger Compartment Equipment
  > FWD OTBD SEAT POST 8 A/B IS CORRODED AT MOUNT. R & R INBD AND OTBD PAX SEAT LEG SPREADER IAW B/E CMM 25-21-21.
- [SDR QXEA2014022600160](https://openairdocs.org/sdr/QXEA2014022600160.md): Seat Track · damaged · Feb 24, 2014 · N429QX · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach Fittings
  > NR 12 SEAT TRACK FOUND TO BE OUT OF LIMITS. REMOVED SEAT TRACK IAW SRM 51-40-15, REPAIR-01 AND SRM 51-41-00. INSTALLED NEW SEAT TRACK IAW SRM 51-42-05 REPAIR 1 AND SRM 51-40-15, REPAIR 1.
- [SDR QXEA2014022600159](https://openairdocs.org/sdr/QXEA2014022600159.md): Rivet · corroded · Feb 24, 2014 · N429QX · Bombdr DHC8402 · Fuselage Main, Structure
  > CORRODED RIVETS AT BS 604.5 - 627.5, STRINGER 31R. REPLACED RIVETS IAW SRM 51-42-05 STEP 4E.
- [SDR QXEA2014022600158](https://openairdocs.org/sdr/QXEA2014022600158.md): Rivet · corroded · Feb 24, 2014 · N429QX · Bombdr DHC8402 · Fuselage Main, Structure
  > CORRODED RIVETS AT BS 584.5 - 604.5, STRINGER 31L. REPLACED RIVETS IAW SRM 51-42-05, STEP 4E.
- [SDR QXEA2014022600157](https://openairdocs.org/sdr/QXEA2014022600157.md): Rivet · corroded · Feb 24, 2014 · N429QX · Bombdr DHC8402 · Fuselage Main, Structure
  > CORRODED RIVETS AT BS 584.5 - 604.5 STRINGER 31R. REPLACED RIVETS IAW SRM 51-42-05 STEP 4E.
- [SDR QXEA2014022600155](https://openairdocs.org/sdr/QXEA2014022600155.md): Seat Track · corroded · Feb 24, 2014 · N429QX · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach Fittings
  > NR 7 SEAT TRACK CORRODED BEYOND LIMITS. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-42-05 STEP 4E, 2-8 AND SRM 51-41-00.
- [SDR QXEA2014022600153](https://openairdocs.org/sdr/QXEA2014022600153.md): Seat Track · corroded · Feb 24, 2014 · N429QX · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach Fittings
  > NR 5 SEAT TRACK CORRODED BEYOND LIMITS. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-42-05, 51-41-00, 51-40-15.

Next page: https://openairdocs.org/aircraft/N429QX/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 = 'N429QX' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N429QX/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.