# Service difficulty reports: N300PQ

A list on [N300PQ](https://openairdocs.org/aircraft/N300PQ.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 · 67 reports

- [SDR REXA2025102900969](https://openairdocs.org/sdr/REXA2025102900969.md): Lamp · inoperative · Oct 13, 2025 · N300PQ · Cndair CL6002D24 · Emergency Lighting
  > #8 EXTERIOR EMERGENCY LIGHT INOP R/R #8 EXTERIOR EMERGENCY LIGHT LAMP IAW AMM 33-51-15. OPS CHECK GOOD
- [SDR REXA2025011300039](https://openairdocs.org/sdr/REXA2025011300039.md): Hydraulic System · low · Jan 7, 2025 · N300PQ · Cndair CL6002D24 · Hydraulic System, Main
  > HYD 3 LO PRESS CAUTION AND IB GND SPLRS CAUTION DURING CRUISE. OTY INDICATING 0%. PROCEDURES FOLLOWED IAW QRH REMOVED AND REPLACED HYDRAULIC SYSTEM 3A ACMP IAW 900 JOBCARD 900-29- 900-914. PERFORMED FUNCTIONAL CHECK OF SYSTEM 3 HYDRAULIC F
- [SDR REXA2024100700851](https://openairdocs.org/sdr/REXA2024100700851.md): Drag Angle · cracked · Apr 18, 2024 · N300PQ · Cndair CL6002D24 · Vertical Stabilizer
  > R/H AFT DRAG ANGLE IS CRACKED. REMOVED CRACKED RH AFT DRAG ANGLE AND INSTALLED NEW AFT DRAG ANGLE P/N: AV670-21186-004 IAW CRJ 900 SRM 51-42-13-001-001-A01, 51-42-21-001-001-A01, AND 51-42-22-001-001-A01
- [SDR REXA2024051700390](https://openairdocs.org/sdr/REXA2024051700390.md): Handle · cracked · Apr 9, 2024 · N300PQ · Cndair CL6002D24 · Electrical/Electronic Compartment Doors
  > WHILE PERFORMING SPECIAL DETAILED INSPECTION (EDDY CURRENT) OF THE MAIN AVIONICS COMPARTMENT DOOR HANDLE FOUND CRACK INDICATIONS TRAVERSAL AROUND THE BASE OF THE SHAFT HANDLE HOUSE ON LEFT AND RIGHT SIDES. FAILED NDT. REMOVED MAIN AVIONICS-COMPARTMENT DOOR-HA
- [SDR REXA2024102901098](https://openairdocs.org/sdr/REXA2024102901098.md): Angle · corroded · Apr 5, 2024 · N300PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORRODED MID CAP ANGLE P/N: SH670-31825-9 AT PAX ENTRY DOOR FLOOR LEVEL. INSTALLED NEW MID CAP ANGLE P/N: SH670-31825-9 IAW CRJ900 SRM 51-42-21-001-001-A01 AND CRJ900 AMM 20-21-00-910-801-A01.
- [SDR REXA2024071600546](https://openairdocs.org/sdr/REXA2024071600546.md): Web · cracked · Apr 5, 2024 · N300PQ · Cndair CL6002D24 · Passenger/Crew Doors
  > WHILE PERFORMING SRM TASK 52-11-04-201-002-A01 PASSENGER DOOR (PHASE IV) STAIR AFT DRAG ANGLE REPAIR, FOUND PAX DOOR AFT WEB CRACKED COMMON TO DRAG ANGLE AND LOWER POWER ASSIST MOTOR BRACKET. COMPLIED WITH ALL STEPS OF ENDEAVOR AIR EA CRJ952-16348 REV IR DATE
- [SDR REXA2024102901099](https://openairdocs.org/sdr/REXA2024102901099.md): Floorbeam · cracked · Apr 1, 2024 · N300PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > RH FS280, RBL 12 COCKPIT FLOOR BEAM HAS A PREVIOUS REPAIR THAT IS CRACKED. REMOVED PREVIOUS CRACKED REPAIR IAW CRJ900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. COMPLIED WITH BOMBARDIER REO 690-53-11-1238, REV.--, DATED 2020-03-09 AND BOMBARDIER REO 69
- [SDR REXA2024102801018](https://openairdocs.org/sdr/REXA2024102801018.md): Angle · corroded · Mar 29, 2024 · N300PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > PAX DOOR SILL LOWER SILL ANGLE IS CORRODED. INSTALLED NEW SERVICEABLE KICK PLATE ANGLE PN: SH670-31875-7S IAW CRJ 900 SRM 51-42-06-001-001-A01. INSTALLED NEW MID CAP ANGLE P/N: SH670-31825-9 IAW CRJ900 SRM 51-42-21-001-001-A01 AND CRJ900 AMM 20-21-00-910-801-A
- [SDR REXA2024071600544](https://openairdocs.org/sdr/REXA2024071600544.md): Drag Angle · cracked · Mar 29, 2024 · N300PQ · Cndair CL6002D24 · Vertical Stabilizer
  > L/H AFT VERTICAL STAB DRAG ANGLE IS CRACKED. REMOVED CRACKED LH AFT DRAG ANGLE IAW CRJ 900 SRM 51-42-13-001-001-A01, 51-42-21-001-001-A01, AND 51-42-22-001-001-A01. INSTALLED NEW AFT DRAG ANGLE P/N: AV670-21186-003, ATTACHED WITH FASTENERS TO VERTICAL FLANGE
- [SDR REXA2024071600543](https://openairdocs.org/sdr/REXA2024071600543.md): Drag Angle · cracked · Mar 29, 2024 · N300PQ · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR AFT DRAG ANGLE CRACKED ABOVE DOOR ASSIST CABLE PULLEY BRACKET. PERFORMED CRJ900 SRM TASK 52-11-04-201-002-A01 TYPE 1 REPAIR.
- [SDR REXA2020121800832](https://openairdocs.org/sdr/REXA2020121800832.md): Smoke Warning · activated · Dec 10, 2020 · N300PQ · Cndair CL6002D24 · Smoke Detection
  > SMOKE AFT LAV AND SMOKE ALARM IN FLIGHT. PAX IN LAV AT THE TIME. QUESTIONED AFTER FLIGHT AND DENIED SMOKING. WARNING STOPPED AFTER 5 SECONDS. FLIGHT COMPLETED. INSPECT AFT LAV NO SIGN OF SMOKE. PERFORM OPERATIONS OF SMOKE DECT, IAW AMM 26-16-00. OPS GOOD
- [SDR REXA2020041300452](https://openairdocs.org/sdr/REXA2020041300452.md): Seat Track · corroded · Apr 4, 2020 · N300PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > INITIAL INSPECTION. CORROSION ON FLOOR SEAT RAIL FROM FS 364 TO 485, LBL 27 AT PAX CABIN. (SM)(CPAX)(TCI 53-20-243). SUMMARY: ON NRC. 00266 CORROSION LEVEL 2. ON FLOOR SEAT RAIL FROM FS 364 TO 485, LBL 27 AT PAX CABIN CORROSION OUT OF LIMITS PER CRJ-900 SRM 5
- [SDR REXA2020041300451](https://openairdocs.org/sdr/REXA2020041300451.md): Seat Track · corroded · Apr 4, 2020 · N300PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > INITIAL INSPECTION. CORROSION ON FLOOR SEAT RAIL FROM FS 379 TO 485, LBL 9 AT PAX CABIN. (SM)(CPAX)(TCI 53-20-243). SUMMARY OF NRC 00265 CORROSION LEVEL2: CORROSION ON FLOOR SEAT RAIL FROM FS 379 TO 485, LBL 9 AT PAX CABIN. FOUND OUT OF LIMITS PER CRJ-900 SRM
- [SDR REXA2020041300444](https://openairdocs.org/sdr/REXA2020041300444.md): Bracket · corroded · Apr 3, 2020 · N300PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > INITIAL INSPECTION: CORROSION ON BRACKET CONNECTOR DS151 FS 897 BTW STGR 24R / 23R (FUS)(SM)[TCI: 100-19]. SUMMARY: DAMAGED BRACKET CONNECTOR DS151 FS 897 BTW STGR 24R / 23R WAS REPLACED PER CRJ/900 SRM 51-41-02-001-001-A01
- [SDR REXA2020041300443](https://openairdocs.org/sdr/REXA2020041300443.md): Retainer · worn · Apr 3, 2020 · N300PQ · Cndair CL6002D24 · Cargo/Baggage Doors
  > INITIAL INSPECTION: BENT AND WEAR ON FWD/AFT LOWER CORNERS ON SEAL RETAINER AT FWD/CENTRAL BAGGAGE BAY DOOR. (C1). SUMMARY OF NRC 00126: BENT AND WEAR ON FWD/AFT LOWER CORNERS ON SEAL RETAINER AT FWD/CENTRAL BAGGAGE BAY DOOR. SEAL RETAINER AT FWD/CENTRAL BAG
- [SDR REXA2020041300462](https://openairdocs.org/sdr/REXA2020041300462.md): Fitting · corroded · Apr 2, 2020 · N300PQ · Cndair CL6002D24 · Ailerons
  > AWR HIDDEN DISCREPANCY: DURING BUSHING REMOVAL, CORROSION WAS FOUND ON INB/OUTB PCU´S BUSHINGS HOUSING FITTINGS 4EA AT LEFT AILERON [IN REF NRC 00384]. (AI) SUMMARY BUSHINGS WERE FABRICATED AND HOUSING FITTINGS 4EA AT LEFT AILERON ON INB/OUTB PCU´S WERE REWOR
- [SDR REXA2020041300440](https://openairdocs.org/sdr/REXA2020041300440.md): Floor Panel · delaminated · Apr 1, 2020 · N300PQ · Cndair CL6002D24 · Fuselage Floor Panel
  > INITIAL INSPECTION: DELAMINATED FLOOR PANEL 252CRF AT CABIN PASSENGER. (CPAX). - SUMMARY: FLOOR PANEL 252CRF WAS REPLACED PER CRJ/900 AMM 53-00-47
- [SDR REXA2020041300463](https://openairdocs.org/sdr/REXA2020041300463.md): Fitting · corroded · Mar 31, 2020 · N300PQ · Cndair CL6002D24 · Ailerons
  > AWR HIDDEN DISCREPANCY: CORROSION ON HOUSING BUSHING OF RIGHT AILERON SURFACE HINGE PCU´S LUG FITTINGS [IN REF NRC 00383 (AI).] SUMMARY BUSHINGS WERE FABRICATED AND HOUSING FITTINGS 4 EA AT RIGHT AILERON ON INB/OUTB PCU´S WERE REWORKED PER BOMBARDIER REO 670-
- [SDR REXA2020041300467](https://openairdocs.org/sdr/REXA2020041300467.md): Seal · torn · Mar 29, 2020 · N300PQ · Cndair CL6002D24 · APU Exhaust System
  > AWR. HIDDEN DISCREPANCY: TORN SEAL IN APU TAILCONE EXHAUST CONE ASSY [IN REF NRC 00055 ] (APU) (SM). SUMMARY: B-SEAL AFT WAS REPLACED PER CRJ-900 AMM 49-81-00-960-801 (CONFIG A02) PAR.4.A. AND CMMS HONEYWELL 49-81-01 REPAIR 5-1 PAR.1.C.
- [SDR REXA2020041300450](https://openairdocs.org/sdr/REXA2020041300450.md): Diaphragm · cracked · Mar 29, 2020 · N300PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > INITIAL INSPECTION: CRACK IN LH FAIRING SUPPORT DIAPHRAGM IN STA. FS=797 TO FS= 807 AND 35LBL AT LH MLG WHEEL WELL. (FYT) SUMMARY: SUPPORT DIAPHRAGM ASSY WAS REPLACED PER CRJ-900 SRM 51-41-02-001-001-A01.
- [SDR REXA2020041300442](https://openairdocs.org/sdr/REXA2020041300442.md): Hinge · corroded · Mar 28, 2020 · N300PQ · Cndair CL6002D24 · Fluid Service Doors
  > INITIAL INSPECTION: CORROSION ON HINGE FITTINGS AND HINGES OF THE LAVATORY WASTE SERVICE PANEL NBR 196ER (SM) (FUS) SUMMARY OF NRC 00047: HINGE FITTINGS AND HINGES OF THE LAVATORY WASTE SERVICE PANEL NBR 196ER WERE REPLACE PER CRJ/900 AMM 52-45-01-400-801-A01
- [SDR REXA2020041300461](https://openairdocs.org/sdr/REXA2020041300461.md): Canister · cracked · Mar 27, 2020 · N300PQ · Cndair CL6002D24 · Wing Miscellaneous Structure
  > INITIAL INSPECTION: CRACK IN CANISTER, WELDED NO.3 IN STA WS148 AT LH MAIN FUEL TANK. (AI) SUMMARY OF NRC: 00340 CRACK IN CANISTER, WELDED NO.3 IN STA WS148 AT LH MAIN FUEL TANK WAS REPAIRED PER CRJ/900 REO 670-57-42-577 REV.--
- [SDR REXA2020041300453](https://openairdocs.org/sdr/REXA2020041300453.md): Seat Track · corroded · Mar 27, 2020 · N300PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > INITIAL INSPECTION. CORROSION AND SCRATCHES ON FLOOR SEAT RAIL RBL9 FROM 485 TO 581, 581 TO 661+32, 661+32 TO 677, 677 TO 847+16 AT PAX CABIN. (SM)(CPAX)(TCI 53-20-245) SUMMARY: ON NRC. 00267 CORROSION LEVEL 2. ON FLOOR SEAT RAIL FROM 485 TO 581, 581 TO 661
- [SDR REXA2020041300466](https://openairdocs.org/sdr/REXA2020041300466.md): Seat Track · corroded · Mar 26, 2020 · N300PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > MPEDV: FLOOR SEAT RAIL LBL27, FS 485 TO 581, 581 TO 661+32, 661+32 TO 693 (SM)(IN REF NRC 269) FLOOR SEAT RAIL LBL27, FS 485 TO 581, 581 TO 661+32, 661+32 TO 693 (SM)(IN REF NRC 269) WAS MACHINED PER REO 670-53-00-343 REV.N
- [SDR REXA2020041300465](https://openairdocs.org/sdr/REXA2020041300465.md): Seat Track · corroded · Mar 26, 2020 · N300PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > MPEDV: FLOOR SEAT RAIL FROM FS 364 TO 485, LBL 27 AT PAX CABIN. (SM)(CPAX)(IN REF NRC 266) FLOOR SEAT RAIL FROM FS 364 TO 485, LBL 27 AT PAX CABIN. (SM)(CPAX)(IN REF NRC 266) WAS MACHINED PER REO 670-53-00-343 REV.N
- [SDR REXA2020041300464](https://openairdocs.org/sdr/REXA2020041300464.md): Seat Track · corroded · Mar 24, 2020 · N300PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > MPEDV: FLOOR SEAT RAILS IN SECTIONS FS= 349.00 TO FS= 485.00, 9 RBL AT PAX CABIN. (CPAX)(IN REF NRC 264) FLOOR SEAT RAILS IN SECTIONS FS= 349.00 TO FS= 485.00, 9 RBL AT PAX CABIN. (CPAX)(IN REF NRC 264) WAS MACHINED PER REO 670-53-00-343 REV. N
- [SDR REXA2020041300458](https://openairdocs.org/sdr/REXA2020041300458.md): Angle · corroded · Mar 24, 2020 · N300PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > INITIAL INSPECTION: CORROSION ON LOWER STRIKER SEAL OF CUTOUT AT GALLEY SERVICE DOOR (FUS) (SM) (TCI 53-20-219). SUMMARY OF NRC. 00299: ANGLE LOWER STRIKER SEAL WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01.
- [SDR REXA2020041300457](https://openairdocs.org/sdr/REXA2020041300457.md): Angle · corroded · Mar 24, 2020 · N300PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > INITIAL INSPECTION: CORROSION ON ANGLE MOUNTING LOWER SURROUND STRUCTURE AT GALLEY SERVICE DOOR (SM) (TCI 53-20-219) ANGLE MOUNTING LOWER SURROUND STRUCTURE AT GALLEY SERVICE DOOR WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01.
- [SDR REXA2020041300456](https://openairdocs.org/sdr/REXA2020041300456.md): Angle · corroded · Mar 24, 2020 · N300PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > AWR: CORROSION ON MID CAP ANGLE [ JUMPER/PROX-SENSOR/CONNECTOR-WIRING ANGLE ] IN STA. FS= 310 TO FS= 349 AT MAIN ENTRANCE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX) SUMMARY:CORROSION IN THE MID CAP ANGLE EXCEEDS MORE THAN 10 PERCENT DEPTH, ACCORDING TO THE LI
- [SDR REXA2020041300454](https://openairdocs.org/sdr/REXA2020041300454.md): Structure · cracked · Mar 24, 2020 · N300PQ · Cndair CL6002D24 · Emergency Exits
  > INITIAL INSPECTION: CRACKED TOP EDGE STRUCTURE OF LEFT FORWARD OVERWING EMERGENCY EXIT DOOR ( PTAS) TOP EDGE STRUCTURE OF LEFT FORWARD OVERWING EMERGENCY EXIT DOOR WAS REPAIRED PER CRJ-900 REO690-52-21-091 REV --
- [SDR REXA2020041300449](https://openairdocs.org/sdr/REXA2020041300449.md): Seat Track · corroded · Mar 24, 2020 · N300PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > INITIAL INSPECTION. CORROSION ON SIDE SEAT RAILS STRG 15RH BTW (FS379-FS485), ( FS485-FS573),(FS 573 -FS661+16), (FS661+16-FS669.40) (SM)(CPAX)(TCI 53-20-301). ON NRC. 00232 CORROSION LEVEL 2. CORROSION ON SIDE SEAT RAILS STRG 15RH BTW (FS379-FS485), ( FS
- [SDR REXA2020041600468](https://openairdocs.org/sdr/REXA2020041600468.md): Seat Track · corroded · Mar 23, 2020 · N300PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > MPEDV: FLOOR SEAT RAIL FROM FS 379 TO 485, LBL 9 AT PAX CABIN. (SM)(CPAX)(IN REF NRC 265) FLOOR SEAT RAIL FROM FS 379 TO 485, LBL 9 AT PAX CABIN. (SM)(CPAX)(IN REF NRC 265) WAS MACHINED PER REO 670-53-00-343 REV.M
- [SDR REXA2020041300448](https://openairdocs.org/sdr/REXA2020041300448.md): Seat Track · corroded · Mar 22, 2020 · N300PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > INITIAL INSPECTION: CORROSION ON SIDE SEAT RAILS STRG 15RH BTW STA ( FS669.40-FS720.85) (FS744.15-FS761.85) ( FS785.15- FS847.00+8.40) ( FS847.00 +8.40 - FS847.00+16) ( FS847.00+16-FS847.70) ( FS847.70-FS913.00)( FS913.00-FS969.00) PAX CABIN ( TCI: 53-
- [SDR REXA2020041300447](https://openairdocs.org/sdr/REXA2020041300447.md): Seat Track · corroded · Mar 22, 2020 · N300PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > INITIAL INSPECTION: CORROSION ON SIDE SEAT RAILS STRG 15LH BTW STA ( FS669.40-FS720.85) (FS744.15-FS761.85) ( FS785.15- FS847.00+8.40) ( FS847.00 +8.40 - FS847.00+16) ( FS847.00+16-FS847.70) ( FS847.70-FS913.00)( FS913.00-FS969.00) PAX CABIN ( TCI: 53-
- [SDR REXA2020041300455](https://openairdocs.org/sdr/REXA2020041300455.md): Door Sill · corroded · Mar 17, 2020 · N300PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > AWR: CORROSION ON RH FLOOR SILL BTW FS280 TO FS319.70 AT CABIN PASSENGER. (CPAX). SUMMARY: FLOOR SILL BTW FS280 TO FS319.70 AT CABIN PASSENGER WAS REPLACED PER CRJ/900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01
- [SDR REXA2020031400459](https://openairdocs.org/sdr/REXA2020031400459.md): Angle · corroded · Mar 14, 2020 · N300PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > INITIAL INSPECTION: CORROSION ON SILL ANGLES BTW STGR 15LH TO 16LH, FS720.85 TO 744.15 ALSO 15RH TO 16RH, FS720.85 TO FS744.15 BELOW LOWER SURROUND STRUCTURE EMERGENCY EXIT DOORS PAX CABIN ( CPAX) ( TCI 53-20-334) SUMMARY: ON NRC. 00326 CORROSION LEVEL 1 O
- [SDR REXA2020031400460](https://openairdocs.org/sdr/REXA2020031400460.md): Angle · corroded · Mar 14, 2020 · N300PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > INITIAL INSPECTION: CORROSION ON CLIPS 2EA ABOVE SILL ANGLES BTW STGR 15RH TO 16RH AT FS720.85 AND FS744.15 CAVITY BELOW LOWER SURROUND STRUCTURE EMERGENCY EXIT DOORS PAX CABIN ( CPAX) ( TCI 53-20-334) SUMMARY: CORROSION ON CLIPS 2EA ABOVE SILL ANGLES BTW S
- [SDR REXA2020041300445](https://openairdocs.org/sdr/REXA2020041300445.md): Stringer · corroded · Mar 13, 2020 · N300PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > INITIAL INSPECTION: CORROSION ON STRINGER 25LH BTW FS280 AND FS295 AT MAIN AVIONICS COMPARMENT.(SM)(E/E)(TCI 53-20-304) SUMMARY OF NRC:00198 CORROSION LEVEL:2 ON STRINGER 25LH BTW FS280 AND FS295 AT MAIN AVIONICS COMPARMENT. STRINGER 25LH WAS REPLACED PER CRJ
- [SDR REXA2020031300441](https://openairdocs.org/sdr/REXA2020031300441.md): Angle · corroded · Mar 13, 2020 · N300PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > INITIAL INSPECTION: CORROSION ON INTERCOSTAL BETWEEN FS310 TO FS319 STGR 20R ALSO ANGLE ON FS319 AT MAIN AVIONICS COMPARTMENT.(SM)(E/E)(TCI 53-20-304) SUMMARY OF NRC:00189 CORROSION LEVEL: 1 ON INTERCOSTAL BETWEEN FS310 TO FS319 STGR 20R WAS REMOVED PER CRJ-9
- [SDR REXA2018080300669](https://openairdocs.org/sdr/REXA2018080300669.md): Charger · inoperative · Aug 2, 2018 · N300PQ · Cndair CL6002D24 · Emergency Lighting
  > FORWARD EXIT SIGN NOT ILLUMINATED. REMOVE AND REPLACED CHARGER ASSY 1 AND BATTERY PACK ASSY 1 IAW AMM 33-51-17 AND AMM 33-51-17. OPS CHECK GOOD A/C OK FOR SERVICE AT THIS TIME.
- [SDR REXA2018013100076](https://openairdocs.org/sdr/REXA2018013100076.md): Pbe · damaged · Jan 31, 2018 · N300PQ · Cndair CL6002D24 · Emergency Equipment
  > DURING INSPECTION, NOTED THE FLIGHT DECK PBE TO BE SOFT, VACUUM SEAL WAS LOST. REMOVED & REPLACED THE PBE IAW AMM 35-31-06.
- [SDR REXA2017092201028](https://openairdocs.org/sdr/REXA2017092201028.md): Seal · missing · Sep 22, 2017 · N300PQ · Cndair CL6002D24 · Emergency Equipment
  > FWD FA PBE SEAL MISSING. RESECURED SEAL AS REQUIRED IAW AMM 20-00 STANDARD PRACTICES.
- [SDR REXA2017062800756](https://openairdocs.org/sdr/REXA2017062800756.md): Battery · misinstalled · Jun 28, 2017 · N300PQ · Cndair CL6002D24 · Emergency Equipment
  > FWD FA JUMPSEAT FLASHLIGHT IS INSTALLED WRONG. UNABLE TO CHECK IF FUNCTIONING. R & R FWD FA FLASHLIGHT BATTERY IAW AMM 25-61-00, OPS CHECKED GOOD.
- [SDR REXA2017020700169](https://openairdocs.org/sdr/REXA2017020700169.md): Glowstrip · missing · Feb 7, 2017 · N300PQ · Cndair CL6002D24 · Emergency Equipment
  > ON PREFLIGHT FLIGHT ATTENDANT AND CLEANER FOUND AND REPORTED A MISSING EXIT ROW FLOOR GUIDE GLOW STRIP. INSTALLED THE GLOWSTRIP IAW AMM 33-51-01.
- [SDR REXA2017012000081](https://openairdocs.org/sdr/REXA2017012000081.md): Riser · cracked · Jan 20, 2017 · N300PQ · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR AFT RISER IS CRACKED AT HANDRAIL RECEPTACLE. REPAIRED PAX DOOR AFT RISER IAW SRM 52-11-04.
- [SDR REXA2017012000080](https://openairdocs.org/sdr/REXA2017012000080.md): Riser · cracked · Jan 20, 2017 · N300PQ · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR FWD RISER IS CRACKED AT HANDRAIL RECEPTACLE. REPAIRED PAX DOOR FWD RISER IAW SRM 52-11-04.
- [SDR REXA2017012000079](https://openairdocs.org/sdr/REXA2017012000079.md): Door Sill · corroded · Jan 20, 2017 · N300PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > RT FLOOR SILL CORRODED AT FS280.00 CROSSBEAM ATTACHMENT. REPAIRED RT FLOOR SILL AT FS 280 IAW REO 670-53-21-139 REV A.
- [SDR REXA2017012000078](https://openairdocs.org/sdr/REXA2017012000078.md): Support Angle · corroded · Jan 20, 2017 · N300PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FS280.00 CROSSBEAM FLOOR PANEL SUPPORT ANGLE CORRODED, LBL11 TO RBL11. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 51-21-06 AND 53-00-00. REMOVED AND REPLACED CROSSBEAM PANEL SUPPORT IAW SRM 51-42-21 AND 51-42-06.
- [SDR REXA2017012000077](https://openairdocs.org/sdr/REXA2017012000077.md): Floorbeam · corroded · Jan 20, 2017 · N300PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > 280 BEAM CORRODED RBL 11. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 51-21-06 AND 53-00-00. REMOVED AND REPLACED RT FLOORBEAM AT FS 280 IAW CRJ900 SRM 51-42-06, 51-42-21 AND 51-42-10.
- [SDR REXA2017012000076](https://openairdocs.org/sdr/REXA2017012000076.md): Beam · corroded · Jan 20, 2017 · N300PQ · Cndair CL6002D24 · Fuselage Main, Structure
  > 280 BEAM CORRODED LBL 11. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 51-21-06 AND 53-00-00. REMOVED AND REPLACED CROSS BEAM IAW SRM 53-11-10, 51-42-06, 51-42-21 AND 51-42-10.

Next page: https://openairdocs.org/aircraft/N300PQ/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 = 'N300PQ' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N300PQ/reports

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