# Service difficulty reports: N418QX, cancelled Oct 7, 2019

A list on [N418QX, cancelled Oct 7, 2019](https://openairdocs.org/deregistered/N418QX-2019-10-07.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 3 · 142 reports

- [SDR QXEA2017082500535](https://openairdocs.org/sdr/QXEA2017082500535.md): Warning Light · false activation · Aug 25, 2017 · N418QX · Bombdr DHC8402 · Landing Gear Position and Warning
  > AT GEAR RETRACTION, THE LEFT GEAR DOWNLOCK INDICATION STAYED ILLUMINATED AFTER ALL THREE GEAR WERE UP & LOCKED. REMOVED FROM SERVICE. PERFORMED AN OPS CHECK OF LANDING GEAR PRIMARY EXTENSION & RETRACTION SYS IAW AMM 32-31-00-710-801. GEAR INDICATES NORMAL. I
- [SDR QXEA2017062700431](https://openairdocs.org/sdr/QXEA2017062700431.md): Control Valve · sticking · Jun 26, 2017 · N418QX · Bombdr DHC8402 · Landing Gear Brake System
  > ON T/O ROLL IT FEELS LIKE BRAKES ARE STICKING UNTIL 80-90 KIAS AT WHICH POINT INCREASED ACCELERATION IS EXPERIENCED. REMOVED FROM SERVICE. R&R MAIN BRAKE CONTROL VALVE. RETURNED TO SERVICE.
- [SDR QXEA2017041700270](https://openairdocs.org/sdr/QXEA2017041700270.md): Governor · malfunctioned · Apr 12, 2017 · N418QX · Bombdr DHC8402 · Propeller Controlling System
  > AFTER START, THE NR 1 PROPELLER TAKES APPROXIMATELY 45 SECONDS TO UNFEATHER AFTER CONDITION LEVER IS MOVED TO MAX. NO ASSOCIATED FAULTS IN CDS. REPLACED THE NR 1 OVERSPEED GOVERNOR IAW AMM TASKS 61-20-26-000-801, AND 61-20-26-400-801, LEAK & OPS CHECKED GOO
- [SDR QXEA2017040700221](https://openairdocs.org/sdr/QXEA2017040700221.md): Propeller · malfunctioned · Apr 5, 2017 · N418QX · Bombdr DHC8402 · Propeller System
  > ON PUSHBACK, AFTER NORMAL START, THE NR 1 ENGINE REMAINED IN FEATHER FOR 3-5 MINUTES WITH CODITION LEVER AT MAX. NO HISTORY. INTERROGATED CDS WITH NO FAULTS FOUND. COMPLIED WITH FIM 61-20-00-810-804. PERFORMED FUNCTIONAL TEST OF THE NR 1 PROPELLER TO UNFEA
- [SDR QXEA2017022700076](https://openairdocs.org/sdr/QXEA2017022700076.md): Rudder · binding · Feb 26, 2017 · N418QX · Bombdr DHC8402 · Rudder Control System
  > AFTER ENGINE START, ATTEMPTED RUDDER CONTROL CHECK, AND FOUND RUDDER PEDALS/CONTROL JAMMED ON BOTH SIDES. NO MESSAGES OR CAUTIONS NOTED. RUDDER DEFLECTION ON PFD SHOWS 3/4 DEFLECTION. HYD QUANTITIES INDICATE NORMAL. PERFORMED OPS TEST OF RUD CONT SYSTEM PER AM
- [SDR QXEA2016120900793](https://openairdocs.org/sdr/QXEA2016120900793.md): Controller · failed · Dec 7, 2016 · N418QX · Bombdr DHC8402 · Windshield/Door Rain/Ice Removal
  > LEVEL AT FL 250 "WSHLD CTRL" CAUTION ILLUMINATED. COMPLIED WITH EMERGENCY CHECKLIST.RETURNED TO FIELD. LANDING UNEVENTFUL. FOUND FAULTS R&L WSHLD CTRL FAIL IN CDS. CLEARED FAULTS AND PERFORMED OPS TEST OF THE WINDSHIELD AND PILOT SIDE WINDOW IAW AMM 30-41-00-7
- [SDR QXEA2016120200770](https://openairdocs.org/sdr/QXEA2016120200770.md): Transducer · malfunctioned · Nov 30, 2016 · N418QX · Bombdr DHC8402 · Landing Gear Brake System
  > DURING LANDING ROLLOUT AND BRAKE APPLICATION LEFT BRAKE FELT UNRESPONSIVE AS MORE PRESSURE WAS APPLIED THE ANTI-SKID ENGAGED RELAXED BRAKE PRESSURE TO DISENGAGE ANTI-SKID AND MISSED NORMAL RUNWAY EXIT. FOUND #1 AND #2 WHEEL SPEED TRANSDUCERS WORN, REPLACED #1
- [SDR QXEA2016113000767](https://openairdocs.org/sdr/QXEA2016113000767.md): Generator · malfunctioned · Nov 29, 2016 · N418QX · Bombdr DHC8402 · Landing Gear Brake System
  > BRAKING ACTION IS POOR AFTER LANDING. INNER WHEEL ASSEMBLY ON BOTH SIDES ARE COLD, WHILE THE OUTER WHEELS ARE HOT. FOUND NO FAULT CODES IN CDS. FAOUND FAULT CODE RH INBD WST IN HISTORY. REPLACED THE RH INBOARD WHEEL SPEED GENERATOR IAW AMM 32-46-11-00-801 AND
- [SDR QXEA2016111100708](https://openairdocs.org/sdr/QXEA2016111100708.md): Ecu · malfunctioned · Nov 4, 2016 · N418QX · Bombdr DHC8402 · Stabilizer Control System
  > ON DEPARTURE OUT OF SEA WE GOT A PITCH TRIM CAUTION LIGHT. 2X-INTERROGATED CDS FOUND FAULT CODES 6E,6D,EE,ED,E7,E3,67,74,75,76,77,78 AND 79. PER MOM REQUEST REPLACEMENT OF THE FCECU REQUIRED. R&R FCECU IAW AMM 27-00-01-000-802,400-802. OPS TEST REF TSK 27-00-0
- [SDR QXEA2016102400674](https://openairdocs.org/sdr/QXEA2016102400674.md): Lamp · inoperative · Oct 22, 2016 · N418QX · Bombdr DHC8402 · Emergency Lighting
  > AFT LEFT EMERGENCY EGRESS LIGHT INOPERATIVE. REPLACED THE LAMPS IAW AMM 33-51-11-000-801 AND 33-51-11-400-801. CHECKED GOOD.
- [SDR QXEA2016091600582](https://openairdocs.org/sdr/QXEA2016091600582.md): Seal · failed · Sep 16, 2016 · N418QX · Bombdr DHC8402 · Propeller Controlling System
  > NR 1 ENGINE TOOK 1.5 MINUTES TO COME OUT OF FEATHER AFTER ENGINE START. REPLACED THE NR 1 ENGINE PROPELLER DOME SEALS. RETURNED TO SERVICE.
- [SDR QXEA2016062700410](https://openairdocs.org/sdr/QXEA2016062700410.md): Coupling · loose · Jun 27, 2016 · N418QX · Bombdr DHC8402 · Aircraft Fuel Distribution System
  > AT CRUISE FLIGHT OF 23,000, THE NR 1 ENGINE FUEL PRESSURE CAUTION FLASHED ON AND OFF ABOUT 12 TIMES. DID NOT SELECT THE NR 1 AUXILIARY PUMP ON, DUE TO THE CAUTION FLASHING ON FOR LESS THAN 1-2 SECONDS EACH TIME. DIVERTED AND ACCOMPLISHED UNEVENTFUL LANDING.
- [SDR QXEA2016041200258](https://openairdocs.org/sdr/QXEA2016041200258.md): Brake · overheated · Apr 12, 2016 · N418QX · Bombdr DHC8402 · Landing Gear Brake System
  > AFTER LANDING DURING POST FLIGHT INSPECTION FOUND THE LT OTBD MAIN WHEEL SMOKING. EXCESSIVE BRAKING WAS NOT USED. PERFORMED INSPECTION AND FOUND SIGNS OF OVERHEATING ON THE BRAKE. REPLACED THE TIRE AND THE BRAKE AND PERFORMED EXCESSIVE BRAKING INSPECTION IAW
- [SDR QXEA2016010900018](https://openairdocs.org/sdr/QXEA2016010900018.md): Autofeather Sys · malfunctioned · Jan 9, 2016 · N418QX · Bombdr DHC8402 · Propeller Feathering/Reversing
  > NR 1 ENGINE FAILS DAILY AUTOFEATHER CHECK. CYCLED ACFT POWER OFF/ON. PERFORMED A/F TEST. NR 1, AND 2 A/F TEST SHOWED PASSED. NO FURTHER DEFECTS NOTED.
- [SDR QXEA2016010600006](https://openairdocs.org/sdr/QXEA2016010600006.md): Battery Pack · malfunctioned · Jan 6, 2016 · N418QX · Bombdr DHC8402 · Emergency Lighting
  > EMERGENCY LIGHTS COME ON WHEN SWITCH IN ARM POSITION. REPLACED BATTERIES IN POSITIONS 1-4. RETURNED TO SERVICE.
- [SDR QXEA2015092500503](https://openairdocs.org/sdr/QXEA2015092500503.md): Seat Track · corroded · Sep 24, 2015 · N418QX · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach Fittings
  > REPLACE SEAT TRACK FROM BS 697.6 - 728.102 AT Y-29.320. REMOVED SEAT TRACK, NR 4, PN:85337843-103, REF SRM 51-42-05 AND 51-42-45. INSTALLED NEW SEAT TRACK NR 4, PN:85337843-103, REF SRM 51-42-05 AND 51-42-45, PO:TX-3661. LOCATED, DRILLED AND COUNTERSUNK SEAT
- [SDR QXEA2015092300494](https://openairdocs.org/sdr/QXEA2015092300494.md): Channel · corroded · Sep 18, 2015 · N418QX · Bombdr DHC8402 · Fuselage Miscellaneous Structure
  > FORWARD PAX DOOR LWR CHANNEL ASSY HAS CORROSION. REMOVED CHANNEL ASSY PN 85329540-001, REF SRM 51-42-05-02-01. J. INSTALLED THRESHOLD CHANNEL ASSY, PN:85329540-001, REF SRM 51-42-05, NEW THRESHOLD CHANNEL. RECEIVED NEW FWD PAX DOOR LWR CHANNEL ASSY PN:853295
- [SDR QXEA2015092300493](https://openairdocs.org/sdr/QXEA2015092300493.md): Seat Track · corroded · Sep 18, 2015 · N418QX · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK NR 16 CORRODED. REMOVED SEAT TRACK NR 16 S/W 85338210-119 IAW SRM 51-40-07. RECEIVED NEW SEAT TRACK NR 16, PN:85328710-119, PO:T-21571 LOCATED AND DRILL HOLES COMMON TO VERTICAL WEB FROM FS X670.0 TO FS X728.102 IAW SRM 51-40-07, REPAIR 01 PARA 5B
- [SDR QXEA2015092300481](https://openairdocs.org/sdr/QXEA2015092300481.md): Seat Track · corroded · Sep 15, 2015 · N418QX · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach Fittings
  > REPLACE SEAT TRACK NR 14, PN: 85338210-113. REMOVED SPLICE COMMON TO SEAT TRACK, NR 13 & 14, PN 85338215-101 AND 85338216-101. INSTALLED SPLICE COMMON TO SEAT TRACK NR 13 AND NR 14, REF SRM 51-42-05, SRM 51-40-15, AND DWG NR 85338201, REV-C. REMOVED SPLICE
- [SDR QXEA2015092300502](https://openairdocs.org/sdr/QXEA2015092300502.md): Seat Track · corroded · Sep 13, 2015 · N418QX · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach Fittings
  > REPLACE SEAT TRACK NR 7, CORRODED. REMOVED DRIP TRAY FROM LT SIDE FROM FS X 71.00 TO FS X 388.000, REF SRM 51-41-00-00-01. INSTALLED DRIP TRAY FROM FS X 71.200 TP FS X 388.000 REF SRM 51-41-00-00-01. REMOVED 2 EA DRIP ANGLES FROM LT SIDE FROM FS X 116.000 TO F
- [SDR QXEA2015092300499](https://openairdocs.org/sdr/QXEA2015092300499.md): Seat Track · corroded · Sep 13, 2015 · N418QX · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach Fittings
  > NR 11 SEAT TRACK CORRODED. INSTALLED SEAT TRACK IAW SRM 51-42-05-02-01 AND SRM 51-40-15-02-01.
- [SDR QXEA2015092300495](https://openairdocs.org/sdr/QXEA2015092300495.md): Splice · corroded · Sep 13, 2015 · N418QX · Bombdr DHC8402 · Fuselage Miscellaneous Structure
  > SPLICE ANGLE CORRODED AT STA X102.5 BETWEEN SEAT TRACK NR 11, AND SEAT TRACK NR 12, PN 85338210-112 TO BE REPLACED WITH SPLICE ANGLE'S, PN 85338216-101 AND PN 85338215-101. LOCATED AND DRILLED SPLICES ANGLES, PN 85338216-101 AND 85338215-101 TO SEAT TRACK NR
- [SDR QXEA2015091300479](https://openairdocs.org/sdr/QXEA2015091300479.md): Seat Track · corroded · Sep 13, 2015 · N418QX · Bombdr DHC8402 · Fuselage Main, Structure
  > SEAT TRACK NR 13 CORRODED. REMOVED SPLICE AND SEAT TRACK NR 13 AND INSTALLED NEW TRACK IAW SRM 51-40-00.
- [SDR QXEA2015092300480](https://openairdocs.org/sdr/QXEA2015092300480.md): Seat Track · corroded · Sep 13, 2015 · N418QX · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach Fittings
  > REPLACE SEAT TRACK NR 15, PN: 85338210-115. REMOVED SPLICE COMMON TO SEAT TRACKS NR 14 AND 15 PN 85338210-113 AND PN 85338210-115, REF SRM 51-40-15, SRM 51-41-00, SRM 51-42-05. INSTALLED SPLICE COMMON TO SEAT TRACKS NR 14 AND NR 15, REF SRM 51-42-05, SRM 51-40
- [SDR QXEA2015092300498](https://openairdocs.org/sdr/QXEA2015092300498.md): Seat Track · corroded · Sep 12, 2015 · N418QX · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK NR 12 CORRODED. DISPLACED ANVC ACCELERMETER AT BS X 223.00 REF AMM 23-35-01-000-801. INSTALLED ANVC ACCELERMETER AT BS X 223.0, REF AMM 23-35-01-400-801. DISPLACED 3EA WIRE BUNDLES BETWEEN BS X 94.8 TPSTAF X 116.0, 2EA BETWEEN BS X 136.0 TO X BS 15
- [SDR QXEA2015092300497](https://openairdocs.org/sdr/QXEA2015092300497.md): Seat Track · corroded · Sep 12, 2015 · N418QX · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK NR 9 CORRODED. REMOVED SEAT TRACK NR 9, PN 85338210.000 IAW SRM 51-40-07. INSTALLED 25 PERCENT OF FASTENERS ON SEAT TRACK NR 9 REF DWG 85338201 REV-1E AND SRM 51-42-05-02-01, STEP 4D (3-10). LOCATED AND DRILLED SEAT TRACK NR 9, PN 85338210-111 IA
- [SDR QXEA2015092300496](https://openairdocs.org/sdr/QXEA2015092300496.md): Seat Track · corroded · Sep 12, 2015 · N418QX · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK NR 8 CORRODED. REMOVED FWD SEAT TRACK SPLICE COMMON TO SEAT TRACK NR 7 AND NR 8 REF SRM 51-42-05-02-01 AND SRM 51-40-15-02-01. SEAT TRACK SPLICE INSTALLED REF DWG 85307071, REV A 98/10/06 COMMON TO SEAT TRACK NR 7 & NR 8. REMOVED SEAT TRACK NR 8
- [SDR QXEA2015092300482](https://openairdocs.org/sdr/QXEA2015092300482.md): Seat Track · not reported · Sep 12, 2015 · N418QX · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach Fittings
  > NR 10 SEAT TRACK. INSTALLED SEAT TRACK IAW SRM 51-42-05 AND SRM 51-40-15.
- [SDR QXEA2015092300500](https://openairdocs.org/sdr/QXEA2015092300500.md): Angle · corroded · Sep 11, 2015 · N418QX · Bombdr DHC8402 · Fuselage Miscellaneous Structure
  > ANGLE AT FS X26.0, STR 25P CORRODED. ANGLE REMOVED AND REPLACED IAW SRM 51-40-07.
- [SDR QXEAA201509140045](https://openairdocs.org/sdr/QXEAA201509140045.md): Angle · corroded · Sep 11, 2015 · N418QX · Bombdr DHC8402 · Fuselage Miscellaneous Structure
  > ANGLE AT FS X6.70, STR 25P REQUIRES REPLACEMENT DUE TO EXFOILIATION CORROSION ANGLE COMMON TO MACHINED INTERCOSTAL. RECEIVED NEW ANGLE, PN 85329576-103. REMOVED CORRODED ANGLE PN 85329576-103 FROM MACHINED INTERCOSTAL COMMON TO MACHINED WEB AT X6.70, STR 25P
- [SDR QXEA2015091400461](https://openairdocs.org/sdr/QXEA2015091400461.md): Angle · corroded · Sep 10, 2015 · N418QX · Bombdr DHC8402 · Fuselage Miscellaneous Structure
  > ANGLE, COMMON TO MACHINED WEB, RIB AT FS X 26.70 BETWEEN STR 25P AND LOWER PAX DOOR THRESHOLD HAS CORROSION AND REQUIRES REPLACEMENT IAW T/C 6-53-1160-FWD PAX DOOR. RECEIVED NEW ANGLE, PN 85329542-116. REMOVED CORRODED ANGLE FROM PARTIAL WEB AT X19.50 COMMO
- [SDR QXEA2015091400460](https://openairdocs.org/sdr/QXEA2015091400460.md): Angle · corroded · Sep 10, 2015 · N418QX · Bombdr DHC8402 · Fuselage Miscellaneous Structure
  > ANGLE, COMMON TO PARTIAL WEB, RIB, AT FS X19.50 BETWEEN STR 25P AND LWR PAX DOOR THRESHOLD HAS CORROSION AND REQUIRES REPLACMENT TC:6-53-1160-FWD PAX DOOR. RECEIVED NEW ANGLE, PN 85329573-101. REMOVED CORRODED ANGLE FROM PARTIAL WEB AT X19.50 COMMON TO FUSE
- [SDR QXEA2015091400459](https://openairdocs.org/sdr/QXEA2015091400459.md): Angle · corroded · Sep 10, 2015 · N418QX · Bombdr DHC8402 · Fuselage Miscellaneous Structure
  > ANGLE COMMON TO MACHINED WEB, RIB AT FS X6.70 BETWEEN STR 25P AND LWR PAX DOOR THRESHOLD HAS CORROSION AND REQUIRES REPLACMENT TC:6-53-1160-FWD PAX DOOR. RECEIVED NEW ANGLE, PN 85329542-115. REMOVED CORRODED ANGLE FROM MACHINED WEB AT X6.70 COMMON TO FUSELAG
- [SDR QXEA2015092300501](https://openairdocs.org/sdr/QXEA2015092300501.md): Stringer · corroded · Sep 6, 2015 · N418QX · Bombdr DHC8402 · Fuselage Main, Longeron/Stringer
  > STRINGER 25P CORRODED, FWD PAX DOOR UNDERFLOOR. PERFORMED CUTOUT OF LOWER MAIN SILL, STR 25P FROM FS X1.00 TO FS X32.40, REF TC 6-53-1160-FWD PAX DR ITEM 17. C/W ET INSP ON STR 25P CUT LINES REF NDTM PT1 51-00-06. NO DEFECTS NOTED. FABRICATED NEW LOWER MAIN
- [SDR QXEA2015042100217](https://openairdocs.org/sdr/QXEA2015042100217.md): Circuit Breaker · tripped · Apr 21, 2015 · N418QX · Bombdr DHC8402 · AC Power Distribution System
  > WRB BAGGAGE CB POPPED, LESS K-2. DIVERTED AND ACCOMPLISHED A UNEVENTFUL LANDING. CHECKED FWD AND AFT CARGO LT OPS ALL CHECKS GOOD C/W CB RESET PROCEDURE IAW GPM REF 9.2.2.1 CB REMAINED CLOSED ALL LAMPS REMAINED ILLUMINATED. NO HISTORY RECORDED LAST 60 DAYS.
- [SDR QXEA2015013000034](https://openairdocs.org/sdr/QXEA2015013000034.md): Strut · failed · Jan 30, 2015 · N418QX · Bombdr DHC8402 · Passenger/Crew Doors
  > MAIN CABIN DOOR DIFFICULT TO OPEN AND CLOSE. REPLACED GAS SPRING STRUTS IAW AMM 52-11-16-400-802. CHECKS GOOD RETURNED TO SERVICE.
- [SDR QXEA2014120301002](https://openairdocs.org/sdr/QXEA2014120301002.md): Switch · missing · Dec 3, 2014 · N418QX · Bombdr DHC8402 · Emergency Lighting
  > F/A EMERGENCY LIGHT SWITCH MISSING. REPLACED SWITCH. RETURNED TO SERVICE.
- [SDR QXEA2014102400857](https://openairdocs.org/sdr/QXEA2014102400857.md): Door · lack of lube · Oct 24, 2014 · N418QX · Bombdr DHC8402 · Passenger/Crew Doors
  > MAIN CABIN DOOR DIFFICULT FOR THE F/A TO OPEN. LUBED THE DOOR IAW AMM 52-11-00-640-801. OPS TESTS GOOD IAW AMM 52-11-00-710-801. RETURNED TO SERVICE.
- [SDR QXEA2014092300801](https://openairdocs.org/sdr/QXEA2014092300801.md): Light · odor · Sep 23, 2014 · N418QX · Bombdr DHC8402 · Cargo Compartment Lighting
  > GROUND CREW REPORTED STRONG SULPHUR ODOR IN AFT CARGO BAY. FOUND TO BE COMING FROM AFT CARGO LIGHT. R & R LIGHT IAW AMM TASK 33-31-01-000-801, & 33-31-01-400-801. OPS CHECKED GOOD.
- [SDR QXEA2014040800295](https://openairdocs.org/sdr/QXEA2014040800295.md): Switch · failed · Apr 8, 2014 · N418QX · Bombdr DHC8402 · Emergency Lighting
  > EMERGENCY LIGHT SWITCH INOPERATIVE. REPLACED SWITCH IAW AMM 33-51-05-00-800/400-801, OPS CHECKED GOOD. RETURNED TO SERVICE.
- [SDR QXEA2014021100116](https://openairdocs.org/sdr/QXEA2014021100116.md): Latch · broken · Feb 11, 2014 · N418QX · Bombdr DHC8402 · Doors
  > COMPARTMENT DOOR UNDER LT F/A JUMPSEAT DOES NOT SPRING CLOSED. R & R LT AFT FA'S JUMPSEAT COMPARTMENT DOOR HINGE SPRINGS AS REQUIRED, COMPARTMENT DOOR OP CK'S GOOD. RETURNED TO SERVICE.
- [SDR QXEA2013122401560](https://openairdocs.org/sdr/QXEA2013122401560.md): Antenna · malfunctioned · Dec 24, 2013 · N418QX · Bombdr DHC8402 · Dependent Position Determining System
  > ERRATIC INDICATIONS ON BOTH PFDS DURING APPROACH. FLIGHT GUIDANCE INDICATED A RT TURN WHEN LOC NEEDLE WAS MOVING LT. LOC NEEDLE WAS SELDOM STEADY AND CONSTANTLY MIGRATING AROUND. HGS DISPLAY WAS VERY ERRATIC. 2 APPROACHES WERE CONDUCTED. GOOD IDENTS ON BO
- [SDR QXEA2013122201555](https://openairdocs.org/sdr/QXEA2013122201555.md): Latch · broken · Dec 22, 2013 · N418QX · Bombdr DHC8402 · Passenger Compartment Equipment
  > STORAGE COMPARTMENT UNDER FORWARD F/A SEAT DOES NOT LATCH FULLY. REPLACED LATCH. RETURNED TO SERVICE.
- [SDR QXEA2013082701312](https://openairdocs.org/sdr/QXEA2013082701312.md): Lens · broken · Aug 27, 2013 · N418QX · Bombdr DHC8402 · Emergency Lighting
  > EMEMERGENCY LIGHT COVER BROKEN AT FWD RT EMERGENCY EXIT. REMOVED FWD EMERGENCY EXIT REF AMM TASK 52-22-00-000-801. R & R SIGN ASSY REINSTALLED FWD EMERGENCY EXIT REF AMM TASK 52-22-000-400-801 AND MCN 65257701. OPS CHECKED GOOD. NO FURTHER DEFECTS NOTED. R
- [SDR QXEA2013072501200](https://openairdocs.org/sdr/QXEA2013072501200.md): Insert · failed · Jul 25, 2013 · N418QX · Bombdr DHC8402 · Passenger/Crew Doors
  > UNABLE TO OPEN MAIN CABIN DOOR, WHEN THE DAMPER OPERATED THE DOOR FROM OUTSIDE, A SCREW AT THE DOOR HANDLE CAME OFF. REPLACED INSERT ON FWD MCD RAIL AT 'BREAK-OVER' POINT. NO FURTHER DEFECTS. DOOR OPERATES NORMALLY. RETURNED TO SERVICE.
- [SDR QXEA2013070101149](https://openairdocs.org/sdr/QXEA2013070101149.md): Warning Horn · activated · Jul 1, 2013 · N418QX · Bombdr DHC8402 · Drag Control System
  > ADVANCED POWER LEVER FOR TAKE OFF RECEIVED A WARNING HORN AND OBSERVED INBD AND OTBD SPOILERS DID NOT RETRACT. ABORTED TAKEOFF AND RETURNED TO GATE. INTERROGATED CDS, FOUND NO FAULT CODES. PERFORMED OPS TEST OF THE ROLL SPOILER SYS IAW AMM TASK 27-61-00-710
- [SDR QXEA2013052001022](https://openairdocs.org/sdr/QXEA2013052001022.md): Guard · broken · May 20, 2013 · N418QX · Bombdr DHC8402 · Emergency Lighting
  > SWITCH COVER ON F/A EMERGENCY LIGHT FELL OFF FOWARD F/A POSITION. REPLACED SWITCH COVER FOR FORWARD F/A EMERGENCY LIGHT SWITCH. OPS CHECK GOOD. RETURNED TO SERVICE.
- [SDR QXEA2013042100813](https://openairdocs.org/sdr/QXEA2013042100813.md): Panel · corroded · Apr 21, 2013 · N418QX · Bombdr DHC8402 · Fuselage Structure (General)
  > PANEL 144JZ HAS MULTIPLE SPOTS OF CORROSION. REMOVED PAINT IAW SRM 51-26-10-02-01. FOUND CORROSION OUT OF LIMITS. STEPPED UP AND COUNTER SUNK SCREW HOLES IAW SRM 51-40-07-02-01. TREATED IAW AMM 51-25-16-390-801.
- [SDR QXEA2013042100799](https://openairdocs.org/sdr/QXEA2013042100799.md): Panel · corroded · Apr 21, 2013 · N418QX · Bombdr DHC8402 · Fuselage Structure (General)
  > PANEL 144HZ HAS CORROSION AROUND SCREW HOLES. CHEMICALLY REMOVED PAINT FROM AFFECTED AREA IAW SRM 51-26-10-02-01. FOUND CORROSION TO BE OUT OF LIMITS. RECEIVED NEW PANEL 144HZ, STEPPED UP AND COUNTER SUNK SCREW HOLES IAW SRM 51-40-07-02-01. TREATED SCREW HOL
- [SDR QXEA2013041900801](https://openairdocs.org/sdr/QXEA2013041900801.md): Angle · corroded · Apr 19, 2013 · N418QX · Bombdr DHC8402 · Fuselage Miscellaneous Structure
  > FOUND CORROSION IN AFT CARGO ON LT SIDE AT STA 783.102. REMOVED CORRODED ANGLE IAW SRM 51-42-05-02-01 AND 51-42-45-02-01. LOCATED AND DRILLED NEW ANGLE IAW SRM 51-40-07-02-01. COUNTERSUNK HOLES ON SHEAR WEB AS REQUIRED. INSTALLED SHEAR WEB ANGLE IAW RD 8/4-

Next page: https://openairdocs.org/deregistered/N418QX-2019-10-07/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 = 'N418QX' AND deregistration_id = 'N418QX-2019-10-07'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N418QX-2019-10-07/reports

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