# Service difficulty reports: N406QX, cancelled Apr 18, 2023

A list on [N406QX, cancelled Apr 18, 2023](https://openairdocs.org/deregistered/N406QX-2023-04-18.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 11 · 532 reports

- [SDR QXEA2017122700709](https://openairdocs.org/sdr/QXEA2017122700709.md): Handle · lack of lube · Dec 23, 2017 · N406QX · Bombdr DHC8402 · Service Doors
  > AFT GALLEY SERVICE DOOR WILL NOT OPEN FROM EXTERIOR, DIFFICULT TO UNLOCK FROM INSIDE. LUBED AFT SERVICE DOOR EXTERNAL HANDLE SHAFT IAW AMM TASK 12-20-01-640-811. OPS TEST OF DOOR REF AMM TASK 52-41-00-710-801. RETURNED TO SERVICE. NO PARTS REPLACED.
- [SDR QXEA2017092900585](https://openairdocs.org/sdr/QXEA2017092900585.md): Handle · unsecure · Sep 28, 2017 · N406QX · Bombdr DHC8402 · Passenger/Crew Doors
  > MAIN CABIN DOOR WILL NOT OPEN FROM INSIDE OR OUTSIDE. FERRIED FOR REPAIRS. REMOVED FWD GALLEY INSERT AND CLOSET SIDEWALL, INSPECTED MCD OPEN - CLOSE MECHANISIM, NO DEFECTS NOTED DURRING SEVERAL DOOR OPERATIONS. DOOR OPERATES SMOOTHLY, NO DEFECTS NOTED. REINST
- [SDR QXEA2017081500518](https://openairdocs.org/sdr/QXEA2017081500518.md): Generator · malfunctioned · Aug 14, 2017 · N406QX · Bombdr DHC8402 · DC Generator-Alternator
  > AFTER TAKEOFF, INTERMITTENT CAUTION LIGHT FLICKERED ON AND OFF. WOULDN'T STAY ON LONG ENOUGH TO IDENTIFY. FINALLY IDENTIFIED AS NR 2 DC GENERATOR. AND WOULD BRIEFLY ILLUMINATE EVERY MINUTE THEN IMMEDIATELY GO OUT. THEN BECAME EVERY SECOND. RAN NR 2 DC GEN
- [SDR QXEA2017061300415](https://openairdocs.org/sdr/QXEA2017061300415.md): Lamp · inoperative · Jun 11, 2017 · N406QX · Bombdr DHC8402 · Emergency Lighting
  > FWD F/A'S EMERGENCY LIGHT SWITCH INOPERATIVE. REPLACED THE LAMP.
- [SDR QXEA2017061400420](https://openairdocs.org/sdr/QXEA2017061400420.md): Skin · damaged · Jun 10, 2017 · N406QX · Bombdr DHC8402 · Trailing Edge Flaps
  > LEFT WING OTBD FLAP TRAILING EDGE METAL PEELING BACK AND SECTION MISSING. REMOVED DAMAGED SKIN, COMPLIED WITH RD/8-4-51-475, NO OTHER DAMAGE NOTED.
- [SDR QXEA2017042100316](https://openairdocs.org/sdr/QXEA2017042100316.md): Bracket · corroded · Apr 4, 2017 · N406QX · Bombdr DHC8402 · Passenger/Crew Doors
  > AFT ENTRY DOOR NR 2 BEAM FOUND CRACKED BETWEEN CENTER SUPPORT. LOCATED, & DRILLED NEW BEAM IAW SRM 51-40-07. APPLIED CORROSION INHIBITING COMPOUND TO INNER STRUCTURE IAW DRW 85217301NOTE 10 REV-J & AMM 51-25-01-390-801.
- [SDR QXEA2017042100318](https://openairdocs.org/sdr/QXEA2017042100318.md): Seat Track · corroded · Apr 2, 2017 · N406QX · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK DAMAGED. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-40-15, SRM 51-40-07, SRM 51-40-07, SRM 51-40-07-02-01, SRM 51-42-05-02-01, 51-41-00-00-01 & DWG 853382101 REV A.
- [SDR QXEA2017042100320](https://openairdocs.org/sdr/QXEA2017042100320.md): Seat Track · corroded · Apr 1, 2017 · N406QX · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK CORRODED. REMOVED THE DAMAGED SEAT TRACK IAW SRM 51-42-05 & 51-40-15. LOCATED & DRILLED A NEW SEAT TRACK IAW SRM 51-40-07-02-01, AND INSTALLED IAW SRM 51-42-05, 51-40-15, & DWG 85328201.
- [SDR QXEA2017042100319](https://openairdocs.org/sdr/QXEA2017042100319.md): Seat Track · corroded · Mar 31, 2017 · N406QX · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK CORRODED. REMOVED AND REPLACED THE SEAT TRACK ANGLE IAW SRM 51-42-05, LOCATED A NEW SEAT TRACK IAW SRM 51-40-07 AND INSTALLED THE SEAT TRACK IAW SRM 51-42-05-02-01, 51-41-00-00-01, & DWG 85361501, REV E.
- [SDR QXEA2017042100317](https://openairdocs.org/sdr/QXEA2017042100317.md): Seat Track · corroded · Mar 31, 2017 · N406QX · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK 16 CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-42-005 REPAIR -01 & 51-40-15. DRILLING NEW SEAT TRACK IAW SRM 51-40-07-02-01 & DWG 85338201 REV.F.
- [SDR QXEA2017042100321](https://openairdocs.org/sdr/QXEA2017042100321.md): Threshold · corroded · Mar 29, 2017 · N406QX · Bombdr DHC8402 · Fuselage Miscellaneous Structure
  > FWD PAX DOOR THRESHOLD MEMBER CORRODED. THE THRESHOLD WAS REMOVED IAW SRM 51-42-05. A NEW FWD THRESHOLD LOCATED AND DRILLED IAW SRM 51-40-09. A NEW DOOR THRESHOLD INSTALLED IAW SRM 51-42-05.
- [SDR QXEA2017030800109](https://openairdocs.org/sdr/QXEA2017030800109.md): Boot · malfunctioned · Mar 7, 2017 · N406QX · Bombdr DHC8402 · Airfoil Anti/De-ice System
  > DE-ICE PRESSURE CAUTION LIGHT SEGMENT ON RT OUTBOARD TAIL DID NOT ILLUMINATE 21 PSI, 70% TORQUE, BOOT AIR NORM. REMOVED AND REPLACED VERTICAL LEADING EDGE IAW AMM 55-33-00-000-801, 55-33-00-400-801-1-3, 4 C, J, 5-A-E OPS CHECKS GOOD. CAUTION LIGHT EXTINGUISHE
- [SDR QXEA2017012300020](https://openairdocs.org/sdr/QXEA2017012300020.md): Repair · unsecure · Jan 20, 2017 · N406QX · Bombdr DHC8402 · Airfoil Anti/De-ice System
  > ON FINAL, FO NOTICED THE RIGHT WING PATCH ON THE BOOT WAS FLAPPING IN THE WIND AND SHOWING RED LINING UNDERNEATH. REMOVED AND REPLACED OUTER WING LEADING EDGE 613CR AND 613DR IAW AMM TASK 57-23-01-000-801 AND 57-23-01-400-801. OPERATIONAL CHECKS GOOD.
- [SDR QXEA2017012300019](https://openairdocs.org/sdr/QXEA2017012300019.md): Governor · malfunctioned · Jan 18, 2017 · N406QX · Bombdr DHC8402 · Propeller Governor
  > NR 2 PROPELLER NOT COMPLETELY FEATHERING ON SHUTDOWN. CHECKED CDS. NO FAULT CODES PRESENT. REMOVED AND REPLACED NR 2 PROP OSG IAW AMM TASK 61-20-26-000-801 AND 400-801. OSG TEST GOOD. LEAK CHECK C/W. NO LEAKS FOUND. RETURNED TO SERVICE.
- [SDR QXEA2016112100733](https://openairdocs.org/sdr/QXEA2016112100733.md): Wire · chafed · Nov 19, 2016 · N406QX · Bombdr DHC8402 · Fire Protection System Wiring
  > FIRE DETECTION WARNING WITHOUT BELL OR EVIDENCE OF FIRE ON THE T HANDLES. NR 2 ENGINE FIRE DETECT FAULT LIGHT A&B ILLUMINATED AND CIRCUIT BREAKER J7 POPPED. FOUND CHAFED WIRE IN THE NR 2 NACELLE. REPAIRED THE WIRE. OPERATIONAL TEST OF FIRE DETECTION SYSTEM GOO
- [SDR QXEA2016102400675](https://openairdocs.org/sdr/QXEA2016102400675.md): Seal · loose · Oct 24, 2016 · N406QX · Bombdr DHC8402 · Emergency Equipment
  > DITCHING DAM SEAL ON MAIN CABIN DOOR IS LOOSE. SECURED THE SEAL. NO DEFECTS NOTED. RETURNED TO SERVICE.
- [SDR QXEA2016090300566](https://openairdocs.org/sdr/QXEA2016090300566.md): Lamp · inoperative · Sep 3, 2016 · N406QX · Bombdr DHC8402 · Emergency Lighting
  > F/A FORWARD EMERGENCY LIGHT SWITCH, GREEN LIGHT INOPERATIVE. REPLACED THE LAMP. CHECKED GOOD. RETURNED TO SERVICE.
- [SDR QXEA2016072200461](https://openairdocs.org/sdr/QXEA2016072200461.md): Escape Rope · unsecure · Jul 22, 2016 · N406QX · Bombdr DHC8402 · Emergency Equipment
  > EMERGENCY ROPE PROTRUDING FROM THE DITCHING DAM ON THE RIGHT FORWARD EMERGENCY EXIT DOOR. SECURED THE ROPE. NO DEFECTS NOTED. RETURNED TO SERVICE.
- [SDR QXEA2016071300451](https://openairdocs.org/sdr/QXEA2016071300451.md): Proximity Sensor · faulted · Jul 13, 2016 · N406QX · Bombdr DHC8402 · Landing Gear Position and Warning
  > RIGHT MAIN GEAR LIGHT ILLUMINATED, RIGHT GEAR DOOR REMAINS OPEN. FOUND FAULT PROXIMITY SENSOR. REPLACED THE PROXIMITY SENSOR. RETURNED TO SERVICE.
- [SDR QXEA2016061900405](https://openairdocs.org/sdr/QXEA2016061900405.md): Actuator · failed · Jun 19, 2016 · N406QX · Bombdr DHC8402 · Engine Oil Cooler
  > AFTER TAKEOFF THE NR 1 ENGINE OIL TEMP CLIMBED TO 114 DEGREES FOR 2 MINUTES. ALL OTHER PARAMETERS NORMAL. OPS CHECK OF OIL COOLER DOOR ACTUATOR FAILED TO OPEN. REPLACED THE ACTUATOR IAW AMM 79-21-31-000-801. OPS TEST GOOD, RETURNED TO SERVICE.
- [SDR QXEA2016061700404](https://openairdocs.org/sdr/QXEA2016061700404.md): Wire Harness · unsecure · Jun 17, 2016 · N406QX · Bombdr DHC8402 · Electrical Power System Wiring
  > WIRE BUNDLE HANGING DOWN ABOVE CAPTAIN'S RT RUDDER PEDAL, AFFECTS USE OF PEDALS. ADJUSTED THE HARNESS, OPERATED THE RUDDER PEDALS THROUGH FULL MOVEMENT, NO DEFECTS NOTED. RETURNED TO SERVICE.
- [SDR QXEA2016042000273](https://openairdocs.org/sdr/QXEA2016042000273.md): Gcu · malfunctioned · Apr 20, 2016 · N406QX · Bombdr DHC8402 · AC Generator-Alternator
  > 2 AC GENERATOR CAUTION LIGHT ILLUMINATED AFTER TAKEOFF. CHECKLIST DONE + NR 2 AC GENERATOR CYCLED. NR 2 AC GENERATOR WOULD NOT RESET. RETURNED TO FIELD. LANDING UNEVENTFUL. INTERROGATED EPCU FOUND FAULT 28 NR 2 AC GCU. REMOVED 2 AC GCU AMM 24-21-00-000-80
- [SDR QXEA2016022000148](https://openairdocs.org/sdr/QXEA2016022000148.md): Light · loose · Feb 20, 2016 · N406QX · Bombdr DHC8402 · Emergency Lighting
  > EMERGENCY LIGHTING STRIP AT MAIN CABIN DOOR CAME OFF. SECURED FLOOR PATH LIGHTING STRIP. RETURNED TO SERVICE.
- [SDR QXEA2015081500431](https://openairdocs.org/sdr/QXEA2015081500431.md): Battery Pack · failed · Aug 15, 2015 · N406QX · Bombdr DHC8402 · Emergency Lighting
  > CEILING LIGHT FOR EMERGENCY LIGHTS AT ROW 2 AND 5 FAILED OPS TEST. REMOVED CEILING PANEL AT ROW 2 AND 5 IAW AMM TASK 25-27-01-000-801. NO DEFECTS NOTED. R & R EMERGENCY LIGHT POWER SUPPLY UNIT IAW AMM TASK 33-51-01-000-801/400-801. NO HELP. R & R EMERGENC
- [SDR QXEA2015062700344](https://openairdocs.org/sdr/QXEA2015062700344.md): Proximity Sensor · out of adjust · Jun 27, 2015 · N406QX · Bombdr DHC8401 · Door Warning System
  > CLIMBING OUT, FORWARD CARGO DOOR MASTER WARNING FUSELAGE DOOR, IT WOULD CONTINUE TO COME ON AND TURN OFF THEN STAYED ON. PRESSURIZATION NORMAL. RETURNED TO FIELD. LANDING UNEVENTFUL. ADJUSTED FORWARD BAGGAGE DOOR CLOSED PROXIMITY SENSOR IAW AMM 52-71-01-830-
- [SDR QXEA2015040600176](https://openairdocs.org/sdr/QXEA2015040600176.md): Skin · scratched · Apr 2, 2015 · N406QX · Bombdr DHC8402 · Trailing Edge Flaps
  > LEFT OTBD FLAP BELOW INBD ACTUATOR HAS 4" SCRATCH. REMOVED SCRATCH MARKS IAW SRM 51-14-00-02-03. C/W ET INSP + UT THICK TEST ON AREA REF NDTM PT1 51-00-06 & 51-00-04. NO DEFECTS NOTED MINIMUM THICKNESS MEASURED =.029". NO DAMAGES ALLOW IAW 57-52-30. RECEI
- [SDR QXEA2015040600181](https://openairdocs.org/sdr/QXEA2015040600181.md): Seat Track · unknown · Apr 1, 2015 · N406QX · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK NR 2 REQUIRES REPLACEMENT. REMOVED SEAT TRACK NR 2, PN:85361561-103, REF SRM 51-42-05, REPAIR -01 AND 51-40-15, REPAIR -01. LOCATED AND DRILLED NEW SEAT TRACK NR 2 IAW SRM 51-40-07-02-01. DEBURRED SEAT TRACK NR 2, REF SRM 51-40-07-02-01. INSTALL
- [SDR QXEA2015040600180](https://openairdocs.org/sdr/QXEA2015040600180.md): Seat Track · unknown · Apr 1, 2015 · N406QX · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK, NR 11 REQUIRES REPLACEMENT. REMOVED SEAT TRACK SPLICE AT FS X102.5 COMMON TO SEAT TRACK 11 AND 12 IAW SRM'S 51-40-15, PAR 6M, 51-42-05, PAR 4E. INSTALLED SEAT TRACK SPLICE AT FS X102.5 COMMON TO SEAT TRACKS 11 AND 12, REF SRM 51-40-15, REF 51-42-
- [SDR QXEA2015040600175](https://openairdocs.org/sdr/QXEA2015040600175.md): Door Sill · corroded · Apr 1, 2015 · N406QX · Bombdr DHC8402 · Fuselage Miscellaneous Structure
  > FORWARD BAGGAGE DOOR LOWER SILL SURFACE CORROSION ON OUTER EDGE BEAM. REMOVED THRESHOLD PLATE, PN:85329610, REF SRM 51-41-00. INSTALLED THRESHOLD PLATE COMMON TO FWD BAGGAGE DOOR SILL REF AMM 20-10-01-430-801. REPLACED OUTER EDGE BEAM, PN:85329604-001 AT FWD
- [SDR QXEA2015040600179](https://openairdocs.org/sdr/QXEA2015040600179.md): Doubler · corroded · Mar 31, 2015 · N406QX · Bombdr DHC8402 · Fuselage Main, Structure
  > FOUND CORROSION ON LAV SERVICE PORT INTERNAL DOUBLER, PN 85307789-101 AT AFT LOWER CORNER. BLENDED DAMAGE AREA REF SRM 52-42-10, REPAIR-01. C/W ET INSP & UT THICK TEST ON REWORKED AREA REF NDTM PT1 51-00-06 & 51-00-04. NO DEFECTS NOTED. MIN THICKNESS MEASU
- [SDR QXEA2015040200169](https://openairdocs.org/sdr/QXEA2015040200169.md): Plate · corroded · Mar 29, 2015 · N406QX · Bombdr DHC8402 · Fuselage Miscellaneous Structure
  > FWD LAVATORY SERVICE DOOR ADAPTOR PLATE PN 85307781-105 CORRODED. REMOVED CORROSION ON ADAPTOR PLATE, PN: 85307781-105 OF FWD LAVATORY SERVICE DOOR IAW SRM 51-21-00. ET INSP IAW NDTM 51-00-06. NO DEFECTS NOTED. UT INSP IAW NDTM 51-00-04, MIN THICKNESS IS.084
- [SDR QXEA2015040200165](https://openairdocs.org/sdr/QXEA2015040200165.md): Seat Track · unknown · Mar 29, 2015 · N406QX · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK NR 19 REQUIRES REPLACEMENT. REMOVED FWD SPLICE COMMON TO SEAT TRACK NR 18 AND NR 19 REF SRM 51-40-15 AND SRM 51-42-05. INSTALLED FWD SPLICE COMMON TO SEAT TRACK NR 18 AND NR 19, REF SRM 51-42-05, REPAIR-01, 51-40-15, REPAIR-04 AND 51-42-45, REPAIR-
- [SDR QXEA2015040600174](https://openairdocs.org/sdr/QXEA2015040600174.md): Web · cracked · Mar 27, 2015 · N406QX · Bombdr DHC8402 · Fuselage Miscellaneous Structure
  > WEB CRACKED, LOCATED BETWEEN FS X341.00 AND X361.00 AT STR 23S. REMOVED INTERCOSTAL PN 85361567-102-9 CRACKED WEB, BETWEEN FSX 341.00 AND X 361.00 AT STR 235, REF SRM 51-42-05. INSTALLED NEW INTERCOSTAL PN QX85361567-102 BETWEEN X341.00 AND X361.00 AT STR 23S
- [SDR QXEA2015040200162](https://openairdocs.org/sdr/QXEA2015040200162.md): Seat Track · unknown · Mar 25, 2015 · N406QX · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK NR 7 REQUIRES REPLACEMENT. REMOVED FWD SEAT TRACK SPLICE COMMON TO TRACK NR 6 & NR 7 FOM REF SRM 51-42-05, 51-40-15. INSTALLED FWD SEAT TRACK SPLICE COMMON TO TRACK NR 6 & NR 7 REF SRM 51-42-05, STEP 4.A-D AND 51-40-15. REMOVED AFT SPLICE COMMON T
- [SDR QXEA2015040200161](https://openairdocs.org/sdr/QXEA2015040200161.md): Seat Track · unknown · Mar 24, 2015 · N406QX · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK, NR 10 REQUIRES REPLACEMENT. SEAT TRACK, NR 10 REMOVED IAW SRM 51-42-05 STEP 4E, 51-41-00, 51-40-15. SEAT TRACK, NR 10 INSTALLED IAW SRM 51-40-07, 51-42-05 AND 53-20-49, 51-42-75, DWG 85328201, REV E 13/01/19, 51-41-00. SPLICES REMOVED IAW SRM 51
- [SDR QXEA2015040200164](https://openairdocs.org/sdr/QXEA2015040200164.md): Threshold · corroded · Mar 23, 2015 · N406QX · Bombdr DHC8402 · Fuselage Miscellaneous Structure
  > CORROSION ON FWD PAX DOOR THRESHOLD PLATE. REMOVED CORRODED THRESHOLD PLATE, PN 85329539-105, REF SRM 51-42-05-02-01-4 (E). INSTALLED NEW THRESHOLD PLATE, PN 85329539-105 REF SRM 51-42-05, REPAIR-01. LOCATED AND DRILLED NEW THRESHOLD PLATE, PN 85329539-105
- [SDR QXEA2015040200166](https://openairdocs.org/sdr/QXEA2015040200166.md): Beam · corroded · Mar 21, 2015 · N406QX · Bombdr DHC8402 · Fuselage Main, Structure
  > FWD BAGGAGE DOOR SURROUND HAS SURFACE CORROSION ON INNER EDGE BEAM. REMOVED FWD SPLICE COMMON TO SEAT TRACK NR 18 AND NR 19 REF SRM 51-40-15 AND SRM 51-42-05. INSTALLED FWD SPLICE COMMON TO SEAT TRACK NR 18 AND NR 19 REF SRM 51-42-05, REPAIR-01, 51-40-15, REP
- [SDR QXEA2015040200167](https://openairdocs.org/sdr/QXEA2015040200167.md): Beam · corroded · Mar 18, 2015 · N406QX · Bombdr DHC8402 · Fuselage Main, Structure
  > AFT PAX DOOR SURROUND STRUCTURE HAS OUTER EDGE BEAM CORRODED, PN 85339542-101. REMOVED OUTER EDGE BEAM, PN 85339542-101, REF SRM 51-42-05-02-01 STEP 4E. LOCATED & DRILLED NEW OUTER EDGE BEAM & INSTALLED ANCHOR NUTS REF DWG 85339511, REV -B DATED 96/09/27 & SRM
- [SDR QXEA2015040200163](https://openairdocs.org/sdr/QXEA2015040200163.md): Beam · corroded · Mar 18, 2015 · N406QX · Bombdr DHC8402 · Passenger/Crew Doors
  > EDGE BEAM, PN 85339512-101, CORRODED TO LIMITS. REMOVE DAMAGED EDGE BEAM, INNER, PN:85339512-11, REF SRM 51-42-05, PARA E, 1-8 AND 51-42-45, PARA H, 1 AND 2. REMOVED INNER EDGE BEAM, PN 85339512-101, REF SRM 51-42-05-02-01, STEP 4E/SRM 51-42-45, STEP 6H/ SR
- [SDR QXEA2015040600177](https://openairdocs.org/sdr/QXEA2015040600177.md): Skin · corroded · Mar 15, 2015 · N406QX · Bombdr DHC8402 · Fuselage Main, Plate/Skin
  > LT FUSELAGE INNER SKIN HAS CORROSION AT AFT PAX DOOR CUTOUT BETWEEN STA X669.3 TO STA 697.6. REMOVED 4 NUTPLATES FOR ACCESS REF SRM 51-42-05 STEP 4E. INSTALLED 4 EA NUTPLATES TO INNER SKIN AT AFT PAX DOOR REF SRM 51-42-05, REPAIR-01. REMOVED CORROSION AT LT F
- [SDR QXEA2015031700143](https://openairdocs.org/sdr/QXEA2015031700143.md): Rib · corroded · Mar 15, 2015 · N406QX · Bombdr DHC8402 · Fuselage Main, Structure
  > AFT PAX DOOR SURROUND STRUCTURE HAS RIB CORRODED AT BS X669.3 AND Z100.032, PN 85339516-101. REMOVED RIB, PN:85339516-101 AT BS X669.3, REF SRM 51-42-05 STEP 4E. INSTALLED NEW RIB, PN 85339516-101 AT BS X669.3, REF SRM 51-42-05, REPAIR-01. LOCATED AND DRILLED
- [SDR QXEA2015031700142](https://openairdocs.org/sdr/QXEA2015031700142.md): Rib · corroded · Mar 15, 2015 · N406QX · Bombdr DHC8402 · Fuselage Main, Structure
  > AFT PASSENGER DOOR SURROUND STRUCTURE HAS CORRODED RIB AT BS X676.45 AND Z100.032, PN 85339514-101. REMOVED RIB, PN:85339514-101 AT BS X676.45, REF SRM 51-42-05, STEP 4.E INSTALLED NEW RIB, PN 85339514-101 AT BS X676.45 AT AFT PAX DOOR SILL REF SRM 51-42-05,
- [SDR QXEA2015031700141](https://openairdocs.org/sdr/QXEA2015031700141.md): Rib · corroded · Mar 15, 2015 · N406QX · Bombdr DHC8402 · Fuselage Main, Structure
  > AFT PASSENGER DOOR SURROUND STRUCTURE HAS RIB CORRODED AT BS X683.45 AND Z100.032, PN 85339514-101. REMOVED RIB, PN:85339514-101, REF BS X683.45, REF SRM 51-42-05, STEP 4E. M. INSTALLED NEW RIB, PN 85339514-101 AT BS X683.45 AT AFT PAX DOOR SILL REF SRM 51-4
- [SDR QXEA2015031700140](https://openairdocs.org/sdr/QXEA2015031700140.md): Rib · corroded · Mar 15, 2015 · N406QX · Bombdr DHC8402 · Fuselage Main, Structure
  > AFT PAX DOOR SURROUND STRUCTURE HAS RIB CORRODED AT BS X690.45 AND Z100.032, PN 85339515-101. REMOVED RIBS AT BS X690.45, PN:85339515-101 REF SRM 51-42-05, STEP 4C. INSTALLED NEW RIB PN 85339515-101 TO AFT PAX DOOR SILL AT BS X690.45, REF SRM 51-42-05, REPAIR
- [SDR QXEA2015031700139](https://openairdocs.org/sdr/QXEA2015031700139.md): Rib · corroded · Mar 15, 2015 · N406QX · Bombdr DHC8402 · Passenger/Crew Doors
  > AFT PAX DOOR SURROUND STRUCTURE HAS RIB CORRODED AT STA X 697.600 AND Z100.032, PN 85339517-101. REMOVED RIB, PN:85339517-101 REF SRM 51-42-05, STEP 4E AT STA X697.600. INSTALLED NEW RIB, PN 85339516-101 AT STA 697.6 AT AFT PAX DOOR REF SRM 51-42-05, REPAIR-0
- [SDR QXEA2014102500854](https://openairdocs.org/sdr/QXEA2014102500854.md): Sleeve · loose · Oct 25, 2014 · N406QX · Bombdr DHC8402 · Door Warning System
  > FORWARD CARGO DOOR INDCATED OPEN DURING CLIMBOUT, MASTER CAUTION FOR FUSELAGE DOORS. RETURNED TO FIELD. LANDING UNEVENTFUL. IAW FIM TASK 52-70-00-810-801 FOUND PRESENT FAULT FBDCL UNREASONABLE FAR. GAP WAS 8.30 MH. FOUND PROXIMITY SENSOR SLEEVE LOOSE. ADJ
- [SDR QXEA2014090400768](https://openairdocs.org/sdr/QXEA2014090400768.md): Autofeather Sys · no test · Sep 4, 2014 · N406QX · Bombdr DHC8402 · Propeller Feathering/Reversing
  > AUTOFEATHER WILL NOT TEST. PERFORMED OPS TEST OF THE PROPELLER AUTOFEATHER AND UPTRIM REF AMM TASK 61-20-00-710-801. OPS TEST GOOD. RETURNED TO SERVICE.
- [SDR QXEA2014090400740](https://openairdocs.org/sdr/QXEA2014090400740.md): Autofeather Sys · no test · Sep 4, 2014 · N406QX · Bombdr DHC8402 · Propeller Feathering/Reversing
  > AUTOFEATHER WILL NOT TEST. PERFORMED OPS TEST IAW AMM 61-20-00-710-801. CHECKS GOOD, NO DEFECTS. RETURNED TO SERVICE.
- [SDR QXEA2014080100644](https://openairdocs.org/sdr/QXEA2014080100644.md): Lamp · inoperative · Aug 1, 2014 · N406QX · Bombdr DHC8402 · Emergency Lighting
  > EMERGENCY LIGHT SWITCH FOR CABIN "NORMAL" MODE IS NOT ILLUMINATED. REPLACED THE LAMP FOR THE BACKLIGHTING. OPS CHECKED GOOD. RETURNED TO SERVICE.
- [SDR QXEA2014070700557](https://openairdocs.org/sdr/QXEA2014070700557.md): Lamp · failed · Jul 7, 2014 · N406QX · Bombdr DHC8402 · Emergency Lighting
  > FORWARD EMERGENCY EXIT DOOR BETA LAMP FAILED FUNCTIONAL CHECK. REPLACED THE BETA LAMP IAW AMM 33-51-00-960-801.

Next page: https://openairdocs.org/deregistered/N406QX-2023-04-18/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 = 'N406QX' AND deregistration_id = 'N406QX-2023-04-18'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N406QX-2023-04-18/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, except the copies of manufacturers’ service documents, which belong to their rights holders.