# Service difficulty reports: N417QX, cancelled Jan 23, 2020

A list on [N417QX, cancelled Jan 23, 2020](https://openairdocs.org/deregistered/N417QX-2020-01-23.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 · 351 reports

- [SDR QXEA2019121600461](https://openairdocs.org/sdr/QXEA2019121600461.md): Light · loose · Dec 14, 2019 · N417QX · Bombdr DHC8402 · Emergency Lighting
  > LUMINESCENT STRIP BETWEEN SEATS 10 & 11 A,B IS COMING UP. REMOVED FROM SERVICE. REMOVED AND REPLACED LUMINESCENT STRIP IAW AMM 33-51-16-000/400-801. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA2019102200391](https://openairdocs.org/sdr/QXEA2019102200391.md): Ground Stud · dirty · Oct 21, 2019 · N417QX · Bombdr DHC8402 · Communications System Wiring
  > #2 ARCDU FAIL MESSAGE. DIVERTED. REMOVED FROM SERVICE. FOUND HIGH RESISTANCE GREATER THAN 25 OHMS AT GROUND STUD 238-GS2 CLEANED GRD STUD RESISTANCE IS NOW LESS THAN.1 OHMS REF TC 6238101 FOR OPS CK A/C REMAINS CAT 3 PLACARD REMAINS CAT 3. AIRCRAFT RETURNED T
- [SDR QXEA2019073100293](https://openairdocs.org/sdr/QXEA2019073100293.md): Transceiver · malfunctioned · Jul 30, 2019 · N417QX · Bombdr DHC8402 · Weather Radar System
  > DURING CLIMBOUT FROM SEA RECIEVED WX FAIL MESSAGE ON MFD AFTER ATTEMPTING TO MAKE WX RADAR WORK. TRIED ADJUSTING GAIN AND TILT AND NEVER GOT AN ECHO. CYCLED POWER AND STILL NO RETURNS. RETURNED TO FIELD. LANDING UNEVENTFUL. REMOVED FROM SERVICE. R+R WX TRANSCE
- [SDR QXEA2019061700250](https://openairdocs.org/sdr/QXEA2019061700250.md): Propeller · malfunctioned · Jun 14, 2019 · N417QX · Bombdr DHC8402 · Propeller Controlling System
  > #2 PROP WOULD NOT COME OUT OF FEATHER WITH CONDITION LEVERS AT MAX. AFTER SETTING PARKING BRAKE BACK AT GATE THE NUMBER 2 PROP DID UNFEATHER. CONDITION LEVERS HAD BEEN AT MAX FOR APPROX 7 MIN WHEN THE PROP UNFEATHERED. REMOVED FROM SERVICE. INTERROGATED CDS FO
- [SDR QXEA2019031800123](https://openairdocs.org/sdr/QXEA2019031800123.md): Link · malfunctioned · Mar 15, 2019 · N417QX · Bombdr DHC8402 · Drag Control System
  > ON TAXI OUT @ SEA, AIRCRAFT WAS CONFIGURED FOR TAKEOFF AND NO TAKEOFF WARNING DURING T/O WARN TEST. UPON POWER APPLICATION, STILL DID NOT GET T/O WARNING HORN. DURING ROTATION @ 117 KTS, AS NOSE GEAR CAME OFF RUNWAY, TAKE OFF WARNING HORN SOUNDED FOR APPROX. 2
- [SDR QXEA2019031100110](https://openairdocs.org/sdr/QXEA2019031100110.md): Pcu · malfunctioned · Mar 9, 2019 · N417QX · Bombdr DHC8402 · Propeller Controlling System
  > NR 1 PROP DOES NOT UNFEATHER USING CDS UNFEATHER SWITCH. PLACED ON MEL 61-20-1. CLEARED 3/10. REMOVED NR 1 PCU REFERING TO AMM TASK 61-20-11-000-801. INSTALLED SERVICABLE PCU REFERING TO AMM TASK 61-20-11-400-801 STEPS 1-4(A16). OPERATIONAL CHECKS GOOD AND NO
- [SDR QXEA2019011100010](https://openairdocs.org/sdr/QXEA2019011100010.md): Motor · seized · Jan 9, 2019 · N417QX · Bombdr DHC8402 · Steering Unit
  > NOSE WHEEL STEERING HYD MOTOR IS SEIZED AND WILL NOT TURN. FOUND METAL CHIPS AND PARTICLES IN THE STEERING HYDRAULIC CASE DRAIN LINE. MOROT REPLACED. AIRCRAFT OUT OF SERVICE FOR STRUCTURAL REPAIRS FOR DAMAGE TO THE LEFT SIDE OF THE AIRCRAFT BELOW THE PILOTS SI
- [SDR QXEA2019010300004](https://openairdocs.org/sdr/QXEA2019010300004.md): Battery Pack · discharged · Jan 2, 2019 · N417QX · Bombdr DHC8402 · Emergency Lighting
  > EMERGENCY LIGHTS BY RT FWD EMERGENCY EXIT AND FWD CABIN CEILING FAIL TO ILLUMINATE WITH EMERGENCY LIGHT SWITCH SELECTED ON. REPLACED BOTH EPSU BATTERY PACKS IN NR 2 EMERGENCY LIGHTS POWER SUPPLY PER AMM TASK 33-51-00-820-801. OPS CHECK IS GOOD.
- [SDR QXEA2018121700456](https://openairdocs.org/sdr/QXEA2018121700456.md): Pump · leaking · Dec 15, 2018 · N417QX · Bombdr DHC8402 · Fuel Boost Pump
  > LEFT HAND WING BOOST PUMP FOUND TO BE LEAKING AND IS CLASSIFIED AS A HEAVY SEEP IAW Q400 AMM 28-10-11-790-802, STEP 2.B, TABLE 201 NOTE 2. PLACED ON DMI. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA2018100800361](https://openairdocs.org/sdr/QXEA2018100800361.md): Light · inoperative · Oct 8, 2018 · N417QX · Bombdr DHC8402 · Emergency Lighting
  > F/A EMERGENCY LIGHT SWITCH DOES NOT ILLUMINATE. REMOVED FROM SERVICE. RELAMPED LIGHT SWITCH. CHECKS GOOD. RETURNED TO SERVICE.
- [SDR QXEA2018091700333](https://openairdocs.org/sdr/QXEA2018091700333.md): Spoiler · deployed · Sep 17, 2018 · N417QX · Bombdr DHC8402 · Drag Control System
  > TAKE OFF WARNING HORN SOUNDED AT APPROX 70 KTS. TAKE OFF WAS ABORTED, NORMAL BRAKING WAS USED. UPON EXITING THE RUNWAY, NOTICED SPOILERS WERE STILL DEPLOYED. UPON RUNNING CHECKLIST, WE WERE UNABLE TO GET THE SPOILERS TO RETRACT WHEN POWER LEVERS WERE PUT ABOVE
- [SDR QXEA2018072700265](https://openairdocs.org/sdr/QXEA2018072700265.md): Unknown · malfunctioned · Jul 27, 2018 · N417QX · Bombdr DHC8402 · Propeller Controlling System
  > AFTER START FLOW COMPLETED. NR 2 PROP 1020 DID NOT UNFEATHER PROP NR 2 AC GEN CAUTION REMAINED ON. CONTACTED MAINTENANCE CONTROL. MOVED CONDITION LEVER FROM 1020 TO FEATHER WITH NO CHANGE. MOVED CONDITION LEVER TO 1020 AND AGAIN NO CHANGE. AFTER SEVERAL MINUTE
- [SDR QXEA2018061800225](https://openairdocs.org/sdr/QXEA2018061800225.md): Proximity Sensor · malfunctioned · Jun 16, 2018 · N417QX · Bombdr DHC8402 · Landing Gear Position and Warning
  > UNCOMMANDED RIGHT MAIN GEAR DOOR OPENED FOR ABOUT ONE SECOND DURING CRUISE. REMOVED FROM SERVICE. INTERROGATED THE PSEU, SHOWED A FAULT RGDRCL. INDUCTANCE VALUE FOR RT GEAR DOOR CLOSED PROXIMITY SENSOR WAS OBSERVED TO BE SPORATIC. REMOVED AND REPLACED T
- [SDR QXEA2018060100206](https://openairdocs.org/sdr/QXEA2018060100206.md): Switch · malfunctioned · May 30, 2018 · N417QX · Bombdr DHC8402 · Elevator Control System
  > FO'S ELEVATOR TRIM SWITCH FAILED IN FLIGHT. RETURNED TO FIELD. LANDING UNEVENTFUL. REMOVED FROM SERVICE. CDS SHOWS CPILTRIM SW FAILURE. REMOVED AND REPLACED THE CO-PILOTS TRIM SWITCH IAW TASK CARD 273000Q01-1, WO 242829. OPS CHECK GOOD. WHILE CHANGING CO-PILOT
- [SDR QXEA2018031900096](https://openairdocs.org/sdr/QXEA2018031900096.md): Controller · malfunctioned · Mar 16, 2018 · N417QX · Bombdr DHC8402 · Propeller Controlling System
  > POWERPLANT MESSAGE DISPLAYED ON ED. OCCURRED DURING CLIMB OUT. SLIGHT SURGE WAS FELT RIGHT BEFORE MESSAGE BEING DISPLAYED. REMOVED FROM SERVICE. INTERROGATED CDS & FOUND CODE 260. R & R THE PEC IAW 61-20-36-000/400-801. OPS CHECKED GOOD. NO POWERPLANT ME
- [SDR QXEA2018031600088](https://openairdocs.org/sdr/QXEA2018031600088.md): Warning Light · false activation · Mar 13, 2018 · N417QX · Bombdr DHC8402 · Trailing Edge Flap Control System
  > ON APPROACH, WHEN SELECTING FLAPS FROM 15 TO 35, FLAP POWER CAUTION LIGHT ILLUMINATED CAUSING FLAPS TO REMAIN IN FLAP 15 POSITION. A GO AROUND WAS EXECUTED IN THE PROCESS THE FLAP 15 VFE WAS EXCEEDED MAX SPEED NOTED AT FLAPS 15 SETTING WAS APPROX 190 KTS FLAP
- [SDR QXEA2018012400026](https://openairdocs.org/sdr/QXEA2018012400026.md): Lens · broken · Jan 24, 2018 · N417QX · Bombdr DHC8402 · Emergency Lighting
  > FA NOTE EMERGENCY EXIT SIGN PLASTIC LENS ON RIGHT SIDE WAS BROKEN. REMOVED FROM SERVICE. REPLACED THE EMERGENCY LIGHT ASSY. OPS TESTED IAW AMM 33-51-00-710-801. TESTED GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA2017111400667](https://openairdocs.org/sdr/QXEA2017111400667.md): Connector · stuck · Nov 13, 2017 · N417QX · Bombdr DHC8402 · Light System Wiring
  > SOCKET NR 5 STUCK IN CONNECTOR 3351-P6, NR 4 POSITION EMERGENCY POWER SUPPLY. REMOVED AND REPLACED CONNECTOR PLUG 3351-P6 WITH SERVICEABLE CONNECTOR PLUG IAW Q400 WM 20-17-11. C/W OPS CHECK OF EMERGENCY LIGHT SYS IAW Q400 AMM 33-51-00-710-803 OPS CHECKS GOOD.
- [SDR QXEA2017110100655](https://openairdocs.org/sdr/QXEA2017110100655.md): Liner · out of position · Oct 31, 2017 · N417QX · Bombdr DHC8402 · Passenger/Crew Doors
  > RAMP REPORTED AFT PAX DOOR WILL NOT OPEN. REMOVED FROM SERVICE. INSPECTED AND FOUND AFT PAX DOOR LOWER LINER HINGE COVER OBSTRUCTING DOOR HINGE. REMOVED LOWER DOOR LINER IAW AMM 25-26-21-000-801. REPAIRED THE HINGE COVER IAW CMM 25-23-31. INSTALLED THE LIN
- [SDR QXEA2017082100526](https://openairdocs.org/sdr/QXEA2017082100526.md): Bulkhead · cracked · Aug 18, 2017 · N417QX · Bombdr DHC8402 · Fuselage Main, Bulkhead
  > FOUND CHAFE ON THE FORWARD LOWER PRESSURE BULKHEAD IN THE NLG WHEEL WELL AFT OF THE NLG STEERING HARNESS. BLENDED AREA IAW SRM 53-10-19-02-01. DURING INSPECTION, FOUND A CRACK 5/8 INCH. CUT OUT DAMAGED AREA AND FABRICATED DOUBLER AND INSTALLED.
- [SDR QXEA2017061200413](https://openairdocs.org/sdr/QXEA2017061200413.md): Pitot Tube · malfunctioned · Jun 10, 2017 · N417QX · Bombdr DHC8402 · Pitot/Static Anti-Ice System
  > PITOT HEAT 2 CAUTION ILLUMINATED AS WE WERE ABOUT TO ENTER THE RUNWAY FOR TAKEOFF. RIGHT DURING BELOW THE LINE CHECKLIST FLOW. COMPLIED WITH FIM TASK CARD 33-30-00-810-807 PARA 1-3. CDS SHOWS PITOT 2 FAIL. PITOT MAST IS COLD TO THE TOUCH. REMOVED AND REPLACED
- [SDR QXEA2017053000373](https://openairdocs.org/sdr/QXEA2017053000373.md): Proximity Sensor · out of adjust · May 25, 2017 · N417QX · Bombdr DHC8402 · Landing Gear Position and Warning
  > AT 270 KIAS AND APPROXIMATELY 15K FEET MSL THE FIRST OFFICER AND I FELT A SLIGHT SHUDDER, LASTING ONE SECOND. LOOKED AT THE PANELS AND SAW THE RIGHT MAIN GEAR DOOR LIGHT (AMBER) ILLUMINATED. THE LIGHT ALMOST IMMEDIATELY EXTINGUISHED. THE REMAINDER OF THE FLIG
- [SDR QXEA2017052200367](https://openairdocs.org/sdr/QXEA2017052200367.md): Light · loose · May 18, 2017 · N417QX · Bombdr DHC8402 · Emergency Lighting
  > EMERGENCY LIGHT STRIP AT ROW 2, SEAT B IS LOOSE. REPLACED THE LIGHT STRIP BETWEEN ROWS 2 - 4. CHECKED GOOD, RETURNED TO SERVICE.
- [SDR QXEA2017050800346](https://openairdocs.org/sdr/QXEA2017050800346.md): Light · loose · May 8, 2017 · N417QX · Bombdr DHC8402 · Emergency Lighting
  > EMERGENCY LIGHT STRIP LOOSE. SECURED THE EMERGENCY LIGHT STRIP.
- [SDR QXEA2017042100312](https://openairdocs.org/sdr/QXEA2017042100312.md): Stringer · corroded · Apr 20, 2017 · N417QX · Bombdr DHC8402 · Fuselage Main, Longeron/Stringer
  > CORROSION FOUND ON STRINGER 25S, BETWEEN BS 176 AND 196. CORROSION BLENDED ON STRINGER 25S BETWEEN BS 176 AND 196.
- [SDR QXEA2017042100311](https://openairdocs.org/sdr/QXEA2017042100311.md): Stringer · corroded · Apr 20, 2017 · N417QX · Bombdr DHC8402 · Fuselage Main, Longeron/Stringer
  > CORRROSION FOUND ON STRINGER 24S AT BS 168. PERFORMED A PERMANENT SPLICE REPAIR TO STRINGER 24S BETWEEN BS 156 AND 176 IAW RD 84-53-8177.
- [SDR QXEA2017042100310](https://openairdocs.org/sdr/QXEA2017042100310.md): Stringer Clip · corroded · Apr 20, 2017 · N417QX · Bombdr DHC8402 · Fuselage Main, Attach Fittings
  > CORROSION FOUND ON STRINGER CLIP AT STRINGER 24P, BS 116. REPLACED THE STRINGER CLIP IAW SRM 51-42-05-02-01, REV 16.
- [SDR QXEA2017042500324](https://openairdocs.org/sdr/QXEA2017042500324.md): Stringer · corroded · Apr 19, 2017 · N417QX · Bombdr DHC8402 · Fuselage Main, Longeron/Stringer
  > CORROSION FOUND ON STRINGER 25S AT X168. BLENDED THE STRINGER.
- [SDR QXEA2017042100314](https://openairdocs.org/sdr/QXEA2017042100314.md): Frame · corroded · Apr 19, 2017 · N417QX · Bombdr DHC8402 · Fuselage Main, Frame
  > CORROSION FOUND ON AFT CARGO FRAME WEB FLANGE AT BS 697.60, LBL 23. PERFORMED A PERMANENT REPAIR TO THE AFT FRAME WEB IAW RD 84-53-8168 ISS 1.
- [SDR QXEA2017042100313](https://openairdocs.org/sdr/QXEA2017042100313.md): Stringer · corroded · Apr 19, 2017 · N417QX · Bombdr DHC8402 · Fuselage Main, Longeron/Stringer
  > CORROSION FOUND ON STRINGER 24P, BETWEEN BS 281 AND 301. PERFORMED A PERMANENT REPAIR TO THE STRINGER IAW RD 84-53-8178 ISSUE.1.
- [SDR QXEA2017042000307](https://openairdocs.org/sdr/QXEA2017042000307.md): Shear Web · corroded · Apr 14, 2017 · N417QX · Bombdr DHC8402 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON AFT BAGGAGE SHEAR WEB BETWEEN X698.0 AND X714.0. REPLACED AFT BAGGAGE WEB BETWEEN X698.0 AND X714.0 WITH NEW PN 85339527-108 IAW SRM 51-42-05-02-01 REV 16.
- [SDR QXEA2017041900279](https://openairdocs.org/sdr/QXEA2017041900279.md): Seat Track · corroded · Apr 14, 2017 · N417QX · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION FOUND ON LT INBD EQUIPMENT SEAT RAIL AT Y-12.63, BETWEEN X697.60 AND X728.102. REPLACED LT INBD EQUIPMENT SEAT RAIL AT Y-12.63 BETWEEN X697.60 AND X728.102 WITH NEW PN 85337843-107SP IAW SRM 51-42-05-02-01 REV 16.
- [SDR QXEA2017042000305](https://openairdocs.org/sdr/QXEA2017042000305.md): Seat Track · corroded · Apr 13, 2017 · N417QX · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION FOUND ON LT CABIN SEAT TRACK NR 5 AT Y-9.25, BETWEEN X-39.00 AND X102.50. REPLACED LT INBD CABIN SEAT TRACK NR 5 AT Y.25 BETWEEN X39.00 AND X102.50 PN 85328210-119 WITH NEW IAW SRM 51-42-05-02-01 AND SRM 51-40-15-02-01 REV 16.
- [SDR QXEA2017042000303](https://openairdocs.org/sdr/QXEA2017042000303.md): Seat Track · corroded · Apr 13, 2017 · N417QX · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION FOUND ON RT CABIN SEAT TRACK NR 12 AT Y9.25, BETWEEN X 102.50 AND X228.50. RT INBD CABIN SEAT TRACK NR 12 AT Y9.25 BETWEEN X102.50 AND X228.50 WAS REPLACED WITH NEW IAW SRM 51-42-05-02-01 REV 16 AND SRM 51-40-15-02-01 REV 16.
- [SDR QXEA2017042000302](https://openairdocs.org/sdr/QXEA2017042000302.md): Seat Track · corroded · Apr 13, 2017 · N417QX · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION FOUND ON RT CABIN SEAT TRACK NR 10 AT Y9.25, BETWEEN X-39 AND X10.50. REPLACED RT INBD CABIN SEAT TRACK NR 10 AT Y9.25 BETWEEN X-39.00 AND X10.50 WITH NEW IAW SRM 51-42-05-02-01 AND SRM 51-40-15-02-01 REV 16.
- [SDR QXEA2017042000301](https://openairdocs.org/sdr/QXEA2017042000301.md): Seat Track · corroded · Apr 13, 2017 · N417QX · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION FOUND ON RT INBD CABIN SEAT TRACK AT Y9.25, BETWEEN X570.00 AND X612.00. REPLACED CABIN SEAT TRACK AT Y.925 BETWEEN X570.00 AND X612.00 WITH NEW IAW SRM 51-42-02-01 AND SRM 51-40-15-02-01 REV 16.
- [SDR QXEA2017042000300](https://openairdocs.org/sdr/QXEA2017042000300.md): Seat Track · corroded · Apr 13, 2017 · N417QX · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION FOUND ON LT INBD CABIN SEAT TRACK AT Y-9.25, BETWEEN X102.50 AND X228.50. REPLACED LT INBD CABIN SEAT TRACK NR 6 AT Y.9.25 BETWEEN X102.50 AND X228.50 WITH NEW IAW SRM 51-42-05-02-01 AND SRM 51-40-15-02-01 REV 16.
- [SDR QXEA2017042000299](https://openairdocs.org/sdr/QXEA2017042000299.md): Seat Track · corroded · Apr 13, 2017 · N417QX · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION FOUND ON CABIN SEAT TRACK NR 7, AT Y 9.25 LT, BETWEEN X 228.50 AND X570.00. REPLACED CABIN SEAT TRACK NR 7 AT Y9.25 LT BETWEEN X228.50 AND X570.00 WITH NEW PN 85361510-103 IAW SRM 51-42-05-02-01 REV 16 AND SRM 51-40-15-02-01 REV 16.
- [SDR QXEA2017042000298](https://openairdocs.org/sdr/QXEA2017042000298.md): Seat Track · corroded · Apr 13, 2017 · N417QX · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION FOUND ON CABIN SEAT TRACK NR 13, AT Y 9.25 RT, BETWEEN X 228.50 AND X570.00. REPLACED RT INBD CABIN SEAT TRACK NR 13 AT Y 9.25 BETWEEN X228.50 AND X570.00 WITH NEW IAW SRM 51-42-05-02-01 REV 16 AND SRM 51-40-15-02-01 REV 16.
- [SDR QXEA2017041900295](https://openairdocs.org/sdr/QXEA2017041900295.md): Frame · corroded · Apr 11, 2017 · N417QX · Bombdr DHC8402 · Fuselage Main, Frame
  > CORROSION FOUND ON FUSELAGE FRAME LOWER FLANGE AT X547.0, BETWEEN STR 31S AND STR 32S. CORROSION ON FUSELAGE FRAME LOWER FLANGE AT X54.70 BETWEEN STR 31S AND STR 32S WAS FOUND TO BE BEYOND LIMITS AS PER SRM 53-00-00 REPAIR 9 REV 16. PERFORMED A PERMANENT REPAI
- [SDR QXEA2017042000308](https://openairdocs.org/sdr/QXEA2017042000308.md): Angle · corroded · Apr 10, 2017 · N417QX · Bombdr DHC8402 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON BAGGAGE FLOOR SUPPORT ANGLE PN 85339286, AT X783.102. REPLACED AFT BAGGAGE FLOOR SUPPORT ANGLE PN 85339286-115 AT X783.102 WITH NEW IAW SRM 51-42-05-02-01 REV 16.
- [SDR QXEA2017042000306](https://openairdocs.org/sdr/QXEA2017042000306.md): Stringer Clip · corroded · Apr 10, 2017 · N417QX · Bombdr DHC8402 · Fuselage Main, Attach Fittings
  > CORROSION FOUND ON STRINGER CLIP AT STR 32S, X236.0. REPLACED STRINGER CLIP AT STR 32S AND X236.0 WITH NEW IAW SRM 51-42-05-02-01 REV 16.
- [SDR QXEA2017042000304](https://openairdocs.org/sdr/QXEA2017042000304.md): Stringer Splice · corroded · Apr 7, 2017 · N417QX · Bombdr DHC8402 · Fuselage Main, Longeron/Stringer
  > CORROSION FOUND ON STRINGER SPLICE AT STR 32R, X-18.25. REPLACED STRINGER SPLICE AT STR 32R, X-18.25, WITH NEW PN 85300611-104 IAW SRM 51-42-05-02-01 REV 16.
- [SDR QXEA2017041900283](https://openairdocs.org/sdr/QXEA2017041900283.md): Stringer Splice · corroded · Apr 7, 2017 · N417QX · Bombdr DHC8402 · Fuselage Main, Longeron/Stringer
  > CORROSION FOUND ON STRINGER SPLICE AT STR 33, X-18.25. REPLACED STRINGER SPLICE AT STR 33, X-18.25, WITH NEW PN 85300693-103 IAW SRM 51-42-05-02-01 REV 16.
- [SDR QXEA2017041900282](https://openairdocs.org/sdr/QXEA2017041900282.md): Stringer Clip · corroded · Apr 5, 2017 · N417QX · Bombdr DHC8402 · Fuselage Main, Attach Fittings
  > CORROSION FOUND ON STRINGER CLIP AT STA X115 AND STRINGER 26S. REPLACED STRINGER SLIP AT STA X115 AND STR 26S WITH NEW PN 85328131-163 IAW SRM 51-42-05-02-01 REV. 16.
- [SDR QXEA2017041900280](https://openairdocs.org/sdr/QXEA2017041900280.md): Threshold · corroded · Apr 3, 2017 · N417QX · Bombdr DHC8402 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON EMERGENCY EXIT DOOR CUTOUT LOWER THRESHOLD, BETWEEN X65.20 AND X100.80. REPLACED EMERGENCY EXIT DOOR CUTOUT LOWER THRESHOLD EDGE BEAM PN 85329514-101 WITH NEW IAW SRM 51-42-05-02-01 REV 16.
- [SDR QXEA2017041900291](https://openairdocs.org/sdr/QXEA2017041900291.md): Threshold · corroded · Apr 3, 2017 · N417QX · Bombdr DHC8402 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON FWD PAX DOOR LOWER THRESHOLD MEMBER. FWD PAX DOOR LOWER THRESHOLD MEMBER PN 85329539-105 WAS REPLACED WITH NEW IAW SRM 51-42-05-02-01 REV 16.
- [SDR QXEA2017041900285](https://openairdocs.org/sdr/QXEA2017041900285.md): Stringer Clip · corroded · Apr 1, 2017 · N417QX · Bombdr DHC8402 · Fuselage Main, Attach Fittings
  > CORROSION FOUND ON STRINGER CLIP AT X136 AND STRINGER 24S. REPLACED CORRODED STRINGER CLIP AT X136 AND STRINGER 24S WITH NEW IAW SRM 51-42-05-02-01 REV 16.
- [SDR QXEA2017041900284](https://openairdocs.org/sdr/QXEA2017041900284.md): Stringer Splice · corroded · Apr 1, 2017 · N417QX · Bombdr DHC8402 · Fuselage Main, Longeron/Stringer
  > CORROSION FOUND ON STRINGER SPLICE AT STA X118 AND STRINGER 24S. REPLACED CORRODED STRINGER AT STA X118 AND STRINGER 24S WITH NEW IAW SRM 51-42-05-02-01 REV 16.
- [SDR QXEA2017041900289](https://openairdocs.org/sdr/QXEA2017041900289.md): Stringer Clip · corroded · Apr 1, 2017 · N417QX · Bombdr DHC8402 · Fuselage Main, Attach Fittings
  > STRINGER CLIP FOUND CORRODED ON STRINGER 24S, AT X361. REPLACED CORRODED STRINGER CLIP AT X361 STR 24S WITH NEW IAW SRM 51-42-05-02-01 REV 16.

Next page: https://openairdocs.org/deregistered/N417QX-2020-01-23/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 = 'N417QX' AND deregistration_id = 'N417QX-2020-01-23'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N417QX-2020-01-23/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.