# Service difficulty reports: N293PQ

A list on [N293PQ](https://openairdocs.org/aircraft/N293PQ.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 2 · 60 reports

- [SDR REXA2026032600265](https://openairdocs.org/sdr/REXA2026032600265.md): Engine · odor · Mar 11, 2026 · N293PQ · Cndair CL6002D24 · Engine (Turbine/Turboprop)
  > FA REPORTED ODOR IN CABIN FORWARD TO AFT WHICH LED TO AIR RETURN. R & R RIGHT ENG PER JC 900-72-430-902. OPS/LEAK CHECKS GOOD.
- [SDR REXA2026052600652](https://openairdocs.org/sdr/REXA2026052600652.md): Hinge · corroded · Dec 3, 2025 · N293PQ · Cndair CL6002D24 · Ailerons
  > CORROSION IN FOR RT AILERON ON CENTER HINGE FITTING AT LUGS: R2 AND R5 CENTER HINGE FITTING LUGS R2 AND R5 AT RH AILERON WERE REPAIRED PER REO 670-57-61-107 REV -B.
- [SDR REXA2026052600651](https://openairdocs.org/sdr/REXA2026052600651.md): Hinge · damaged · Dec 2, 2025 · N293PQ · Cndair CL6002D24 · Ailerons
  > FABRICATE BUSHINGS OVERSIZE FOR RH AILERON ON CENTER HINGE FITTING AT LUGS: R1 AND R6 BUSHINGS OVERSIZE FOR RH AILERON ON CENTER HINGE FITTING AT LUGS R1 AND R6 WERE FABRICATED PER REO 670-57-61-107 REV.-B
- [SDR REXA2026052600644](https://openairdocs.org/sdr/REXA2026052600644.md): Striker · not reported · Dec 2, 2025 · N293PQ · Cndair CL6002D24 · Doors
  > FABRICATE SEAL STRIKER PER DWG SH670-31412 REV.C. AND PER EA CRJ953-20947 REV.IR. NEW SEAL STRIKER P/N: SH670-31412-7 WAS FABRICATED PER EA CRJ953-20947 REV: IR IN REFERENCE TO DWG SH670-31412 REV: C.
- [SDR REXA2026052600655](https://openairdocs.org/sdr/REXA2026052600655.md): Rib · cracked · Nov 25, 2025 · N293PQ · Cndair CL6002D24 · Wing, Rib/Bulkhead
  > CRACK ON WING RIB LEADING EDGE SS27.16 AT RIGHT WING. CRACK ON WING RIB LEADING EDGE SS27.16 AT RIGHT WING. WAS REPAIRED PER CRJ957-20951 REV IR
- [SDR REXA2026052600656](https://openairdocs.org/sdr/REXA2026052600656.md): Web · cracked · Nov 21, 2025 · N293PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK ON ELECTRICAL BAY FLOOR WEB LEFT SIDE (BELOW BRAKES GAUGES) FS193.00. CRACK ON ELECTRICAL BAY FLOOR WEB LEFT SIDE (BELOW BRAKES GAUGES) FS193.00 WAS REPAIRED PER CRJ-900 SRM 53-11-43-201-001-A01
- [SDR REXA2026052600654](https://openairdocs.org/sdr/REXA2026052600654.md): Striker · cracked · Nov 21, 2025 · N293PQ · Cndair CL6002D24 · Emergency Exits
  > CRACK AT RH FWD & LH AFT OVERWING EMERGENCY DOOR TOP SECTION (AROUND BASE OF DOOR PROXIMITY SENSOR STRIKER). RH FWD & LH AFT OVERWING EMERGENCY DOOR TOP SECTION (AROUND BASE OF DOOR PROXIMITY SENSOR STRIKER) WERE REPAIRED PER REO 670-52-21-103 REV.--.
- [SDR REXA2026052600653](https://openairdocs.org/sdr/REXA2026052600653.md): Channel · cracked · Nov 21, 2025 · N293PQ · Cndair CL6002D24 · Cargo/Baggage Doors
  > CRACK AT AFT BAGGGAGE-BAY CARGO DOOR TRACK CHANNEL, AFT LOWER SECTION. CHANNEL WAS REMOVED AND NEW CHANNEL WAS DRILLED AND INSTALLED ON AFT BAGGGAGE-BAY CARGO DOOR TRACK CHANNEL, AFT LOWER SECTION PER SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01 AND SR
- [SDR REXA2026052600645](https://openairdocs.org/sdr/REXA2026052600645.md): Door Sill · cracked · Nov 21, 2025 · N293PQ · Cndair CL6002D24 · Fuselage Main, Structure
  > CRACK ON AFT RH DOOR LANDING AT FS 188.00 (LATCH CUT OUT OF ACCESS DOOR 212AR) CRACK ON AFT RT DOOR LANDING AT FS 188.00 (LATCH CUT OUT OF ACCESS DOOR 212AR) WAS REPAIRED PER EA CRJ953-20971 REV. IR AND REPLACED PER SRM 51-42-06-001-001-A01 AND PER SRM 51-42-
- [SDR REXA2026052600642](https://openairdocs.org/sdr/REXA2026052600642.md): Retainer · cracked · Nov 21, 2025 · N293PQ · Cndair CL6002D24 · Passenger/Crew Doors
  > CRACK ON LOWER SEAL RETAINER AT PASSENGER DOOR AND BEND CONDUIT SUPPORT. LOWER SEAL RETAINER WAS REPLACED PER SRM 51-42-10-001-001-A01 AND PASSENGER DOOR HARNESS ASSEMBLY MUST BE REPLACED UNDER NRC 00227
- [SDR REXA2025062300676](https://openairdocs.org/sdr/REXA2025062300676.md): Charger · inoperative · Jun 16, 2025 · N293PQ · Cndair CL6002D24 · Emergency Lighting
  > AFT 3 EMERGENCY FLOOD CEILING LIGHTS NOT WORKING. REMOVED AND REPLACED EMERGENCY BATTERY CHARGER AND BATTERY AT LOCATION PS38 IAW AMM 33-51-17. OPS CHECK GOOD.
- [SDR REXA2025022700237](https://openairdocs.org/sdr/REXA2025022700237.md): Charger · inoperative · Feb 24, 2025 · N293PQ · Cndair CL6002D24 · Emergency Lighting
  > DURING WALK AROUND FOUND MULTIPLE EMERGENCY LIGHTS INOP. (DS93, DS 102, DS 99, DS 100) REMOVED AND REPLACED PS37 EPSU BATTERY CHARGER IAW AMM 33-51-17. OPS CHECK GOOD. A/C OK FOR SVC
- [SDR REXA2024091600710](https://openairdocs.org/sdr/REXA2024091600710.md): Sensor · inoperative · Sep 8, 2024 · N293PQ · Cndair CL6002D24 · Overheat Detection
  > MLG BAY OVHT WARNING MESSAGE IN FLIGHT AT 33000 DEF MLG BAY OVERHEAT DETECTION SYSTEM MEL 26-14-1B CAT B. MAINTENANCE PROCEDURE COMPLETED. MOC NOTIFIED 7821. PLACARD INSTALLED. REMOVED AND REPLACED L/H GEAR BAY TEMPERATURE SENSOR IAW CRJ AMM TASK 26-14
- [SDR REXA2024010500001](https://openairdocs.org/sdr/REXA2024010500001.md): Light · inoperative · Dec 26, 2023 · N293PQ · Cndair CL6002D24 · Emergency Lighting
  > EMERGENCY LIGHT INOP LH MIDDLE OVERWING R/R BULB HOUSING IAW AMM 33-51-15. REPAIRED BROKEN WIRE IAW ESPM 20-16-06. OPS CHECK GOOD. P/N ON/OFF 2LA006954-00
- [SDR REXA2020111200743](https://openairdocs.org/sdr/REXA2020111200743.md): Battery Pack · failed · Nov 6, 2020 · N293PQ · Cndair CL6002D24 · Emergency Lighting
  > EMERGENCY LIGHTS TURN ON AND THEN IMMEDIATELY FADE OUT THROUGHOUT THE AIRCRAFT. EMERGENCY LIGHT SWITCH IN COCKPIT FOUND IN OFF POSITION. F/A EMERGENCY LIGHT SWITCH FOUND IN OFF POSITION. R & R ALL THE EPSU BATTERY PACK, IAW CRJ 900 AMM 35-51-17 AND OPE
- [SDR REXA2019121181721](https://openairdocs.org/sdr/REXA2019121181721.md): Connector · loose · Dec 8, 2019 · N293PQ · Cndair CL6002D24 · Light System Wiring
  > SERVICE DOOR EMERGENCY LIGHT EXTERIOR INOP "MOVE TO DEFER EXTERIOR SERVICE DOOR EMERGENCY LIGHT REF MEL 33-51-2A. CAT C. NO NIGHT OPS. MM02 UPDATED, PLACARD INSTALLED. MOC NOTIFIED #96184 *** R+R'D RH EMER EXIT LIGHT BULB( AFT OF SVC DOOR) IAW AMM 33-51-15 AN
- [SDR REXA201904260505](https://openairdocs.org/sdr/REXA201904260505.md): Frame · corroded · Apr 22, 2019 · N293PQ · Cndair CL6002D24 · Fuselage Main, Frame
  > CORROSION ON FRAME FS:310 BTW STGR 24LH AND 24RH AT MAIN AVIONICS COMPARTMENT. CORROSION LEVEL 2: FRAME STA. FS=310 BTW STGR 24LH AND 24RH AT MAIN AVIONICS COMPARTMENT WAS REPAIRED PER CRJ-900 EA NO. CRJ953-08650 REV. IR
- [SDR REXA2019042620504](https://openairdocs.org/sdr/REXA2019042620504.md): Stringer · corroded · Apr 22, 2019 · N293PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STGR 26RH FROM STA FS:280 TO FS:295 AT MAIN AVIONICS COMPARTMENT (E/E) (TCI 100-09). A NEW STRINGER 26RH FROM STA FS:280 TO FS:295 AT MAIN AVIONICS COMPARTMENT WAS INSTALLED PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01.
- [SDR REXA2019042620503](https://openairdocs.org/sdr/REXA2019042620503.md): Stringer · corroded · Apr 22, 2019 · N293PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STGR 27 FROM STA FS:280 TO FS:295 AT MAIN AVIONICS COMPARTMENT (E/E) (TCI 100-09) SUMMARY OF NRC 00132: LEVEL 2 OF CORROSION, ON STGR 27 FROM STA FS:280 TO FS:295 AT MAIN AVIONICS COMPARTMENT WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND
- [SDR REXA2019042610507](https://openairdocs.org/sdr/REXA2019042610507.md): Intercostal · corroded · Apr 21, 2019 · N293PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON INTERCOSTAL BTW STA FS:349 TO FS:364 AND BTW STGR 27 AND 26RH AT MAIN AVIONICS COMPARTMENT. INTERCOSTAL BTW STA FS:364 AND BTW STGR 27 AND 26 RH AT MAIN AVIONICS COMPARTMENT (E/E) WAS REPLACED PER CRJ 900 SRM 53-21-23-101-001-A02, 51-42-06-001-0
- [SDR REXA201904260506](https://openairdocs.org/sdr/REXA201904260506.md): Frame · corroded · Apr 20, 2019 · N293PQ · Cndair CL6002D24 · Fuselage Main, Frame
  > CORROSION ON FRAME STA FS:295 BTW STGR 24LH AND 24RH AT MAIN AVIONICS COMPARTMENT (E/E) (TCI 100-09) SUMMARY OF NRC 00135: CORROSION LEVEL 2 ON FRAME STA FS:295 BTW STGR 24LH AND 24RH AT MAIN AVIONICS COMPARTMENT (E/E) WAS REPAIRED PER EA NO: CRJ953-08649 REV
- [SDR REXA2019042680509](https://openairdocs.org/sdr/REXA2019042680509.md): Angle · corroded · Apr 18, 2019 · N293PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON ANGLE FS= 310 / FS=349 LOWER SURROUND STRUCTURE PASSENGER DOOR. CORROSION ON ANGLE FS= 310 / FS=349 AT LOWER SURROUND STRUCTURE OF PASSENGER DOOR WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01. BLENDED AREA ON ANGLE FS= 310 / FS=349 AT LOWER SUR
- [SDR REXA2019042670517](https://openairdocs.org/sdr/REXA2019042670517.md): Stringer Splice · corroded · Apr 17, 2019 · N293PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > CORROSION ON SPLICE STRINGER 21 RH BTW FS=333 E/E BAY. SPLICE ON STRINGER 21 RH BTW FS=333 WAS REPLACED PER CRJ-900, SRM 51-42-06-001-001-A01,P.6.D AND 51-41-02-001-001-A01.
- [SDR REXA2019042670514](https://openairdocs.org/sdr/REXA2019042670514.md): Seat Track · corroded · Apr 17, 2019 · N293PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SIDE SEAT RAIL BTW 672-722, 743-763, 780-847+14, 847+14-907, 907-986. CORROSION SEAT RAIL REPLACED PER CRJ-900 SRM 51-41-02-001-001-A01 AND AMM 53-00-49-400-801
- [SDR REXA2019042670495](https://openairdocs.org/sdr/REXA2019042670495.md): Stringer Splice · corroded · Apr 17, 2019 · N293PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > INITIAL INSPECTION: CORROSION ON STGR SPLICE 26 RH BTW STA FS:330 AND FS:337 AT MAIN AVIONICS COMPARTMENT (E/E) (TCI 100-09). THE STGR SPLICE 26RH BTW STA FS:330 AND FS:337 WAS REPLACED PER CRJ900 SRM 51-42-20-001-001-A01 AND 51-42-06-001-001-A01
- [SDR REXA2019042610516](https://openairdocs.org/sdr/REXA2019042610516.md): Stringer · corroded · Apr 16, 2019 · N293PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STRINGER 21 RH BTW FS=310/364 E/E BAY. STRINGER 21 RH BTW FS=310/364 E/E BAY WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 PAR.C AND SRM 51-42-20-001-001-A01 PAR.C
- [SDR REXA2019042610497](https://openairdocs.org/sdr/REXA2019042610497.md): Angle · corroded · Apr 16, 2019 · N293PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON MID CAP ANGLE LOWER SURROUND STRUCTURE PASSENGER DOOR (SM)[FUS]. CORROSION ON ANGLE MID CAP WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01 BLENDED AREA WAS MEASURED. ORIGINAL THICKNESS IS 0.060'' AND MINIMUN REMAINING THICKNESS IS 0.038'' THEREF
- [SDR REXA2019042660496](https://openairdocs.org/sdr/REXA2019042660496.md): Stringer Splice · corroded · Apr 16, 2019 · N293PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STGR SPLICE 25 RH BTW STA FS:330 AND FS:337 AT MAIN AVIONICS COMPARTMENT (E/E) (TCI 100-09). DUE EXCESIVE CORROSION ON STGR SPLICE 25 RH BTW STA FS:330 AND FS:337 WILL BE REPLACED PER CRJ/900 SRM 53-00-00-101-001-A01 PAR 4. NEW STGR SPLICE 25 RH
- [SDR REXA2019042640500](https://openairdocs.org/sdr/REXA2019042640500.md): Floor Support · corroded · Apr 14, 2019 · N293PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > AWR: CORROSION ON FLOOR FITTING SUPPORT BTW FS=280/295 AND RBL 38 IN REF R53520 STEP 7 (SM)[W1]. SUMMARY OF NRC 231 CORROSION LEVEL 2: FLOOR FITTING SUPPORT BTW FS=280/295 AND RBL 38 WAS REPLACED PER CRJ-900 SRM 51-42-20-001-001-A01
- [SDR REXA2019042640499](https://openairdocs.org/sdr/REXA2019042640499.md): Floor Support · corroded · Apr 14, 2019 · N293PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > AWR: CORROSION ON FLOOR SILL STRUCTURE FS= 280+2 AND FS= 319 RBL 42 IN REF R53520 STEP 7 (SM)[W1]. SUMMARY OF NRC 00230 CORROSION LEVEL 2:FLOOR SILL WAS REPLACED PER CRJ-900 SRM 51-42-10-001-001-A01 PAR. 8.C. AND 51-42-06-001-001-A01 PAR. 6.C.
- [SDR REXA2019042640494](https://openairdocs.org/sdr/REXA2019042640494.md): Angle · corroded · Apr 14, 2019 · N293PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION IN INTERNAL STRUCTURE OF FWD WASTE LAVATORY SERVICE PANEL INCLUDING ANGLE IMPACT AT LOWER FUSELAGE (FUS) (SM) (TCI 100-16). CORROSION LEVEL:1 IN INTERNAL STRUCTURE OF FWD WASTE LAVATORY SERVICE PANEL INCLUDING ANGLE IMPACT AT LOWER FUSELAGE WAS REM
- [SDR REXA2019042630498](https://openairdocs.org/sdr/REXA2019042630498.md): Floorbeam · corroded · Apr 13, 2019 · N293PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > INITIAL INSPECTION: CORROSION ON FLOOR SUPPORT FS 280 AND BTW LBL12-RBL12. FLOOR SUPPORT FS 280, RBL12-LBL12 AT COCKPIT AREA WAS REPLACED FOR NEW ONE PER CRJ900 SRM 51-42-20-001-001-A01AND 51-42-06-001-001-A01
- [SDR REXA2019042600515](https://openairdocs.org/sdr/REXA2019042600515.md): Angle · corroded · Apr 12, 2019 · N293PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION AND MISSING SCREWS ON LOWER SURROUND STRUCTURE AT GALLEY SERVICE DOOR. AREAS OUT OF LIMITS, DUE TO EXCESSIVE CORROSION ON ANGLE MOUNTING LOWER SURROUND STRUCTURE AT GALLEY SERVICE DOOR, MUST BE REPLACED PER CRJ-900 SRM 53-00-00-101-001-A01, ANGLE M
- [SDR REXA201904260510](https://openairdocs.org/sdr/REXA201904260510.md): Seat Track · corroded · Apr 11, 2019 · N293PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > INITIAL INSPECTION. CORROSION ON FLOOR SEAT RAILS LBL9, LBL27, RBL9 BTW FS 364-485. (SM)(CPAX)(TCI 53-20-243). SUMMARY: OF NRC: 00163, NEW SECTION OF SEAT RAILS LBL9, LBL27, RBL9 BTW FS 364-485 WERE REPLACED PER CRJ-900 SRM 51-41-02-001-001-A01 AND AMM 53-00-
- [SDR REXA2019042610513](https://openairdocs.org/sdr/REXA2019042610513.md): Seat Track · corroded · Apr 10, 2019 · N293PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SIDE SEAT RAILS STRG 15R & 15L BTW 379-483, 483-573, 573-661+14, 661+14-672. SIDE SEAT RAILS STRG 15R & 15L BTW 379-483, 483-573, 573-661+14, 661+14-672 WERE REPLACED PER CRJ 900 SRM 51-41-02-001-001-A01 AND 51-41-04-001-001-A01,AMM 53-00-49-400
- [SDR REXA2019042610512](https://openairdocs.org/sdr/REXA2019042610512.md): Seat Track · corroded · Apr 10, 2019 · N293PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON FLOOR SEAT RAILS LBL9 & RBL9 BTW FS 691-836, 836-847+51, 847+51-977. (SM)(CPAX)(TCI 100-20). SUMMARY: ON NRC: 00165, FLOOR SEAT RAILS LBL9 & RBL9 BTW FS 691-836, 836-847+51, 847+51-977. WERE REPLACED PER CRJ/900 AMM 53-00-49-400-801 (CONFIG. A-1
- [SDR REXA2019042680508](https://openairdocs.org/sdr/REXA2019042680508.md): Intercostal · corroded · Apr 8, 2019 · N293PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON INTERCOSTAL BTW STA FS:349 TO FS:364 AND BTW STGR 27 AND 26LH AT MAIN AVIONICS COMPARTMENT.: INTERCOSTAL BTW STA FS:364 AND BTW STGR 27 AND 26 LH AT MAIN AVIONICS COMPARTMENT (E/E) WAS REPLACED PER CRJ 900 SRM 53-21-23-101-001-A02, 51-42-06-001-
- [SDR REXA201904267511](https://openairdocs.org/sdr/REXA201904267511.md): Seat Track · corroded · Apr 7, 2019 · N293PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > INITIAL INSPECTION. CORROSION ON FLOOR SEAT RAILS LBL9 & RBL9 BTW FS 485-581, 581-661+32, 661+32-691. (SM)(CPAX)(TCI 53-20-245). SUMMARY NRC 164 CORROSION LEVEL 2: FLOOR SEAT RAILS LBL9 & RBL9 BTW FS 485-581, 581-661+32, 661+32-691.WAS REPLACED PER CRJ-900 SR
- [SDR REXA2019042670502](https://openairdocs.org/sdr/REXA2019042670502.md): Canister · cracked · Apr 7, 2019 · N293PQ · Cndair CL6002D24 · Fuel Storage
  > CRACK IN CANISTER, WELDED NO.3 IN STA WS148 AT LH MAIN FUEL TANK. SUMMARY OF NRC 299:CANISTER, WELDED NO.3 IN STA WS148 AT LH MAIN FUEL TANK.WAS REPAIRED PER REO 670-57-42-577 REV.--
- [SDR REXA2019042670501](https://openairdocs.org/sdr/REXA2019042670501.md): Canister · cracked · Apr 7, 2019 · N293PQ · Cndair CL6002D24 · Fuel Storage
  > INITIAL INSPECTION: CRACK IN CANISTER, WELDED NO.3 IN STA WS148 AT RH MAIN FUEL TANK. (AD) SUMMARY OF NRC 298:CANISTER, WELDED NO.3 IN STA WS148 AT RH MAIN FUEL TANK WAS REPAIRED PER REO 670-57-42-577 REV.--
- [SDR REXA2018100200925](https://openairdocs.org/sdr/REXA2018100200925.md): Heater · shorted · Sep 30, 2018 · N293PQ · Cndair CL6002D24 · Heating System
  > DURING CLIMBOUT THROUGH 10,000'THE FWD FA BRIEFLY SMELLED ELECTRICAL SMOKE IN THE GALLEY. THEN SHE NOTICED THAT HEAT WAS COMING OUT OF THE VENTS AS IF THE GALLEY HEATER SWITCH WAS ON. THEIR GALLEY HEATER SWITCH WAS FOUND TO BE NON-RESPONSIVE. I OPENED CIRCUIT
- [SDR REXA2018070200593](https://openairdocs.org/sdr/REXA2018070200593.md): Flashlight · inoperative · Jul 2, 2018 · N293PQ · Cndair CL6002D24 · Emergency Equipment
  > FWD EMERGENCY FLASHLIGHT DOES NOT BLINK TEST, AND STRAP IS BROKEN. REMOVED & REPLACED FWD FLASHLIGHT IAW CMM 25-60-11. NO DEFECTS NOTED. A/C OK FOR SVC.
- [SDR REXA2018070300591](https://openairdocs.org/sdr/REXA2018070300591.md): Light · inoperative · Jun 30, 2018 · N293PQ · Cndair CL6002D24 · Emergency Lighting
  > LT AFT OVERWING EXTERIOR EMERGENCY LIGHT. R&R LT EXTERIOR AFT OVERWING EMERGENCY LIGHT HOUSING ASSY IAW AMM 33-51-15.
- [SDR REXA2017092101018](https://openairdocs.org/sdr/REXA2017092101018.md): Smoke Detector · inoperative · Sep 21, 2017 · N293PQ · Cndair CL6002D24 · Smoke Detection
  > FWD LAVATORY SMOKE DETECTOR GREEN POWER LIGHT NOT VISIBLE. REMOVED AND REPLACED THE SMOKE DETECTOR IAW AMM 26-16-01-400-802. OPS CHECKED GOOD.
- [SDR REXA2017090500973](https://openairdocs.org/sdr/REXA2017090500973.md): Oxygen Mask · separated · Sep 5, 2017 · N293PQ · Cndair CL6002D24 · Crew Oxygen System
  > DURING PREFLIGHT, CREW FOUND THE CAPTAIN`S SIDE OXYGEN MASK HARDNESS SEPARATED. SWAPPED THE CAPTAIN`S OXYGEN MASK WITH OBSERVER`S IAW AMM 35-11-12.
- [SDR REXA2017013000130](https://openairdocs.org/sdr/REXA2017013000130.md): Seal · broken · Jan 30, 2017 · N293PQ · Cndair CL6002D24 · Emergency Equipment
  > CA FLASH LIGHT SEAL BROKE. REPLACED CAPTAINS FLASH LIGHT SEAL AS NECESSARY. OK FOR SERVICE.
- [SDR REXA2016122702550](https://openairdocs.org/sdr/REXA2016122702550.md): Strut · flat · Dec 27, 2016 · N293PQ · Cndair CL6002D24 · Nose/Tail Landing Gear Strut/Axle
  > UPON GEAR RETRACTION AFTER TAKEOFF WE GOT A GEAR DISAGREEMENT WARNING MESSAGE AND A STEERING INOP CAUTION MESSAGE. THE GEAR DISAGREEMENT WENT AWAY BUT THE STEERING INOP PERSISTED. RAN THE QRH. LANDED SAFELY PERFORMED THE FAULT RESET PROCEDURE ON THE RUNWAY IN
- [SDR REXA2016110802175](https://openairdocs.org/sdr/REXA2016110802175.md): Seal · missing · Nov 8, 2016 · N293PQ · Cndair CL6002D24 · Emergency Equipment
  > FLIGHT DECK PBE IS MISSING BOTH SEALS. REPLACED BOTH SEALS ON FLIGHT DECK PBE IAW AMM 25-61-00.
- [SDR REXA2016100601849](https://openairdocs.org/sdr/REXA2016100601849.md): Light · missing · Oct 6, 2016 · N293PQ · Cndair CL6002D24 · Emergency Lighting
  > EMERGENCY LIGHT STRIP MISSING AT SEATS 12 A/B. REPLACED THE LIGHT IAW AMM 33-51-00 TS003648
- [SDR REXA2016092601810](https://openairdocs.org/sdr/REXA2016092601810.md): Oxygen Mask · unsecure · Sep 26, 2016 · N293PQ · Cndair CL6002D24 · Passenger Oxygen System
  > O2 MASK COVER ABOVE SEATS 20C+D CAME OUT DURING FLIGHT. RESTOWED PASSENGER O2 MASK AT SEAT 20CD IAW AMM 35-21-09.

Next page: https://openairdocs.org/aircraft/N293PQ/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 = 'N293PQ' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N293PQ/reports

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