# Service difficulty reports: N303PQ

A list on [N303PQ](https://openairdocs.org/aircraft/N303PQ.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 · 80 reports

- [SDR REXA2026060400901](https://openairdocs.org/sdr/REXA2026060400901.md): Light · inoperative · Jun 3, 2026 · N303PQ · Cndair CL6002D24 · Flight Compartment Lighting
  > FO SIDE MAP LIGHT SPARKED AND EMITTED SMOKE WHEN MOVED. REMOVED AND REPLACED FO SIDE MAP READING LIGHT IAW AMM 33-13-03. OPS CHECKS GOOD. NO SMOKE ODOR NOTED.
- [SDR REXA2026041300284](https://openairdocs.org/sdr/REXA2026041300284.md): Overheat Sensor · inoperative · Apr 2, 2026 · N303PQ · Cndair CL6002D24 · Overheat Detection
  > AT FL250 MLG BAY OVHT WARN RAN QRH WARN MSG DID NOT EXTINGUISH BTMS ALL 0000 LANDED W/O ISSUE WARN MSG PERSISTS AT GATE. R/R FIRE DETECTION CONTROL IAW AMM 26-14-01. MESSAGE DID NOT CLEAR. R/R L & R MLG BAY TEMPATURE SENSING ELEMENT IAW AMM 26-14-04. OPS TE
- [SDR REXA2025010300004](https://openairdocs.org/sdr/REXA2025010300004.md): Lamp · inoperative · Dec 30, 2024 · N303PQ · Cndair CL6002D24 · Emergency Lighting
  > RH REAR EXTERIOR EMERGENCY LIGHT IS INOP. REMOVED AND REPLACED EXTERIOR EMEREGENCY LIGHT AT THE RIGHT AFT OVER WING SECTION OF THE FUSELAGE IAW AMM 33-51-15 OPS CHECK GOOD P/N ON/OFF:8GH002473-08
- [SDR REXA2024092400722](https://openairdocs.org/sdr/REXA2024092400722.md): Battery Pack · inoperative · Sep 18, 2024 · N303PQ · Cndair CL6002D24 · Emergency Lighting
  > DURING INSP. FOUND ALL FOUR OVERWING EMER EXITS/ FORWARD FLOOR EMER EXITS AND MID CABIN FORWARD EMERGENCY LIGHTS INOP. TROUBLESHOT AND FOUND EMERGENCY BATTERY PS37 INCORRECTLY INSTALLED. R/R PS37 BATTERY AND WAS ABLE TO GET ONE O/W EXIT LIGHT WORKING AND BO
- [SDR REXA2024040100319](https://openairdocs.org/sdr/REXA2024040100319.md): Door Frame · cracked · Mar 2, 2024 · N303PQ · Cndair CL6002D24 · Fuselage Main, Structure
  > LEFT FORWARD OVER-WING EMERGENCY EXIT 833 APPEARS TO BE CRACKED AT THE BASE OF THE AFT UPPER LUG. REQUIRES EVALUATION. REPAIRED AFT LH EMERGENCY EXIT DOOR IAW ENDEAVOR AIR EA NO: CRJ952-15922 REV IR DATED 3/6/2024
- [SDR REXA2024032000289](https://openairdocs.org/sdr/REXA2024032000289.md): Door Frame · cracked · Mar 2, 2024 · N303PQ · Cndair CL6002D24 · Emergency Exits
  > AFT LH EMERGENCY EXIT DOOR POSSIBLE CRACK NEAR BASE OF UPPER LUG. REPAIRED AFT LH EMERGENCY EXIT DOOR IAW ENDEAVOR AIR EA NO: CRJ952-16063 REV IR DATED 3/4/2024
- [SDR REXA2024103001120](https://openairdocs.org/sdr/REXA2024103001120.md): Panel · corroded · Feb 21, 2024 · N303PQ · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR FWD STAIR SIDE PANEL CORRODED AT APPROX DD7 AROUND HAND RAIL UPPER FWD POST ASSY. REPAIRED SIDE PANEL, FORWARD, PASSENGER DOOR STAIRS, P/N 601R317071-12 IAW ENDEAVOR AIR EA. CRJ952-16088 REV -- DATED 2-19-2024.
- [SDR REXA2024102901121](https://openairdocs.org/sdr/REXA2024102901121.md): Floorbeam · cracked · Feb 21, 2024 · N303PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > STIFFENING ANGLE AT FS 280 RBL26 PN:CC670-34117-6 IS CRACKED AND REQUIRES REPLACEMENT. REMOVED STIFFENING ANGLE AT FS 280 RBL 26 PN: CC670-34117-6 IAW CRJ 900 SRM 51-42-06-001-001-A01. INSTALLED NEW STIFFENING ANGLE PN CC670-31147-6 IAW CRJ900 SRM 51-42-06-001
- [SDR REXA2024102901116](https://openairdocs.org/sdr/REXA2024102901116.md): Web · cracked · Feb 19, 2024 · N303PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "L/H FWD EQUIPMENT BAY FLOOR WEB APPEARS TO BE CRACKED AT F.S.193. REMOVED DAMAGED AREA IN BAY FLOOR WEB LH SIDE AT FS193 IAW CRJ900 SRM 53-11-43-201-001-A01. FABRICATED, LOCATED DRILLED, DEBURRED AND INSTALLED REPAIR PARTS, DOUBLER AND SHIM 2024T3 0.040"" P
- [SDR REXA2024102901115](https://openairdocs.org/sdr/REXA2024102901115.md): Electrical Box · cracked · Feb 19, 2024 · N303PQ · Cndair CL6002D24 · Fuselage Main, Structure
  > EXTERNAL A/C POWER RECEPTICAL MOUNTING CHANNEL IS CRACKED. DISCONNECTED THE MAIN BATTERY IAW CRJ900 AMM 24-32-00-040-801-A01, CONNECTED MAIN BATTERY IAW CRJ 900 AMM 24-32-00-440-801-A01. REMOVED AND REINSTALLED EXTERNAL AC POWER RECEPTACLE USING PN NAS1149DD
- [SDR REXA2024102901114](https://openairdocs.org/sdr/REXA2024102901114.md): Access Panel · chafed · Feb 19, 2024 · N303PQ · Cndair CL6002D24 · Trailing Edge Flaps
  > RH FLAP L/E ACCESS PANEL 684GB IS CHAFED. FOUND DAMAGE ON PANEL BEYOND REPAIR. LOCATED AND DRILLED NEW SERVICABLE PANEL 684GB IAW CRJ-900 SRM 51-40-11-001-001-A01.
- [SDR REXA2024022600217](https://openairdocs.org/sdr/REXA2024022600217.md): Floorbeam · cracked · Feb 16, 2024 · N303PQ · Cndair CL6002D24 · Fuselage Main, Structure
  > RH COCKPIT FLOOR BEAM (RBL12) IS CRACKED ON O/B AFT RADIUS. COMPLIED WITH MHIRJ REO# 690-53-11-1689 REV. -- DATED 2024-02-22 FOR RBL12 COCKPIT FLOOR BEAM.
- [SDR REXA2024022600216](https://openairdocs.org/sdr/REXA2024022600216.md): Floorbeam · cracked · Feb 16, 2024 · N303PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > LH COCKPIT FLOORBEAM IS CRACKED ON O/B AFT RADIUS. COMPLIED WITH MHIRJ REO# 690-53-11-1689 REV. -- DATED 2024-02-22 FOR RBL12 COCKPIT FLOOR BEAM.
- [SDR REXA2024102901113](https://openairdocs.org/sdr/REXA2024102901113.md): Floor Support · corroded · Feb 15, 2024 · N303PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > RH FLOOR SILL BETWEEN FS 280 TO 319 IS CORRODED ON UPPER AND LOWER SURFACE. REMOVED AND REPLACED RH FLOOR SILL IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01
- [SDR REXA2024102901112](https://openairdocs.org/sdr/REXA2024102901112.md): Attach Angle · cracked · Feb 15, 2024 · N303PQ · Cndair CL6002D24 · Fuselage Main, Attach Fittings
  > RBL 9 FWD OB ATTACH ANGLE FOUND TO BE CRACKED. LOCATED AND DRILLED SERVICEABLE RBL 9 FWD OB ATTACH ANGLE P/N CC670-34269-8 INSTALLED SERVICEABLE RBL 9 FWD OB ATTACH ANGLE P/N CC670-34269-8 IAW CRJ 900 SRM 51-42-21-001-001-A01.
- [SDR REXA2024102901111](https://openairdocs.org/sdr/REXA2024102901111.md): Attach Angle · cracked · Feb 15, 2024 · N303PQ · Cndair CL6002D24 · Fuselage Main, Attach Fittings
  > RBL 12 FWD ATTACH ANGLE FOUND TO BE CRACKED. LOCATED AND DRILLED SERVICEABLE RBL 12 FWD ATTACH ANGLE P/N CC670-34099-2.INSTALLED SERVICEABLE RBL 12 FWD ATTACH ANGLE P/N CC670-34099-2 IAW CRJ 900 SRM 51-42-21-001-001-A01.
- [SDR REXA2024102901110](https://openairdocs.org/sdr/REXA2024102901110.md): Attach Angle · cracked · Feb 15, 2024 · N303PQ · Cndair CL6002D24 · Fuselage Main, Attach Fittings
  > LBL 12 FWD ATTACH ANGLE FOUND TO BE CRACKED. LOCATED AND DRILLED SERVICEABLE LBL 12 FWD ATTACH ANGLE P/N CC670-34099-1SB. INSTALLED SERVICEABLE LBL 12 FWD ATTACH ANGLE P/N CC670-34099-1SB IAW CRJ 900 SRM 51-42-21-001-001-A01.
- [SDR REXA2024102901109](https://openairdocs.org/sdr/REXA2024102901109.md): Floorbeam · corroded · Feb 15, 2024 · N303PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > "FS 280 ""J"" ANGLE IS CORRODED BETWEEN LBL 9 AND RBL 9 REMOVED FS 280 ""J"" ANGLE IAW CRJ900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. LOCATED AND DRILLED NEW ""J"" ANGLE PN: CC670-34095-1 IAW CRJ900 SRM 51-40-11-001-001-A01. INSTALLED NEW FS 280 ""
- [SDR REXA2024102901108](https://openairdocs.org/sdr/REXA2024102901108.md): Bulkhead Web · corroded · Feb 15, 2024 · N303PQ · Cndair CL6002D24 · Fuselage Main, Bulkhead
  > LH FS 280 BULKHEAD LOWER WEB IS CORRODED. REPAIRED LH FS 280 BULKHEAD LOWER WEB IAW CRJ 900 SRM 53-11-10-201-004-A01.
- [SDR REXA2024102901107](https://openairdocs.org/sdr/REXA2024102901107.md): Bulkhead Web · corroded · Feb 15, 2024 · N303PQ · Cndair CL6002D24 · Fuselage Main, Bulkhead
  > RH FS 280 BULKHEAD LOWER WEB IS CORRODED. REPAIRED RH FS 280 BULKHEAD LOWER WEB IAW CRJ 900 SRM 53-11-10-201-004-A01.
- [SDR REXA2024102901106](https://openairdocs.org/sdr/REXA2024102901106.md): Floorbeam · corroded · Feb 15, 2024 · N303PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > RH FS 280 CROSSBEAM IS CORRODED REPLACED CROSS BEAM IAW SRM 51-40 AND 51-42
- [SDR REXA2024040200327](https://openairdocs.org/sdr/REXA2024040200327.md): Floorbeam · cracked · Feb 13, 2024 · N303PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > LH FS 280 CROSSBEAM IS CORRODED REMOVED AND REPLACED LH FS 280 CROSSBEAM IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 AND 51-21-11-001-001-A01.
- [SDR REXA2024030500234](https://openairdocs.org/sdr/REXA2024030500234.md): Post · corroded · Feb 13, 2024 · N303PQ · Cndair CL6002D24 · Fuselage Main, Structure
  > FS 280 DOOR CORNER POST IS CORRODED AT LBL9 FLOOR LEVEL REPAIRED FS 280 DOOR CORNER POST AT LBL9 FLOOR LEVEL IAW CRJ 900 SRM 53-11-10-201-006-A01. REMOVED AND REINSTALLED INSTALLED SAME SERVICEABLE GUSSET AND INSTALLED NEW SERVICEABLE ATTACH ANGLE AT LH FS
- [SDR REXA2022110402413](https://openairdocs.org/sdr/REXA2022110402413.md): Control Panel · inoperative · Oct 31, 2022 · N303PQ · Cndair CL6002D24 · Cabin Pressure Control System
  > AT 29000 FT WE RECIEVED A CABIN ALT CAUTION THAT ESCALATED TO A CABIN ALT WARNING. THE CABIN ALT INCREASED TO 12,300 FT. WE RAN THE EMERGENCY CHECKLIST CARD WHICH DIRECTED US TO QRH 7-7. WE PREFORMED THE QRH PROCEDURE AS UNPRESSURIZED AND CONTINUED THE FLIGHT
- [SDR REXA2020070600576](https://openairdocs.org/sdr/REXA2020070600576.md): Battery Pack · discharged · May 10, 2020 · N303PQ · Cndair CL6002D24 · Emergency Lighting
  > FA REPORTS FLOOR LEVEL EMRGENCY LIGHTED EXIT SIGNS ON BOTH SIDES IN ROW 13 ARE INOP. REMOVED AND REPLACED PS38 EPSU BATTERY PACK IAW AMM 33-51-17. OPS CHECK OK.
- [SDR REXA2020040900438](https://openairdocs.org/sdr/REXA2020040900438.md): Piston · worn · Mar 28, 2020 · N303PQ · Cndair CL6002D24 · Nose/Tail Landing Gear Strut/Axle
  > INITIAL INSPECTION: WEAR ON SETTLEMENT AREA OF THE WHEEL AT NLG PISTON/AXLE ASSEMBLY. (SM).IN REFERENCE NRC SN 461. SETTLEMENT AREA OF THE WHEEL AT NLG PISTON/AX
- [SDR REXA2020042300542](https://openairdocs.org/sdr/REXA2020042300542.md): Seal · torn · Mar 10, 2020 · N303PQ · Cndair CL6002D24 · Engine Cowling System
  > EDV AIR: LH ENGINE TR COWL LOWER SEAL TORN.(MOT1)(AYP) SUMMARY: SEAL (P/N: G50483) LOWER TR COWL LH ENGINE WAS REPLACED PER CRJ 900 SRM 51-42-10-001-001-A01.
- [SDR REXA2020042300541](https://openairdocs.org/sdr/REXA2020042300541.md): Hinge Fitting · corroded · Mar 6, 2020 · N303PQ · Cndair CL6002D24 · Ailerons
  > AWR IN REF NRC S/N 00523, AFTER BUSHING REMOVAL CORROSION WAS FOUND ON PCU HINGES FITTING LUGS (4EAS) OF LH AILERON. HINGES FITTING LUGS (4EAS) OF LH AILERON WERE REPAIRED PER REO 670-57-61-237 REV.--
- [SDR REXA2020042300540](https://openairdocs.org/sdr/REXA2020042300540.md): Hinge Fitting · corroded · Mar 6, 2020 · N303PQ · Cndair CL6002D24 · Ailerons
  > AWR IN REF NRC S/N 00524, AFTER BUSHING REMOVAL CORROSION WAS FOUND ON PCU HINGES FITTING LUGS (4EAS) OF RH AILERON. HINGES FITTING LUGS (4EAS) OF RH AILERON WERE REPAIRED PER REO 670-57-61-237 REV. --
- [SDR REXA2020042300539](https://openairdocs.org/sdr/REXA2020042300539.md): Seat Track · corroded · Mar 5, 2020 · N303PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > INITIAL INSPECTION: CORROSION ON SIDE SEAT RAIL 15RH BETWEEN FS847+16 TO FS897.70, FS897.70 TO FS913, FS913 TO FS969 AT PASSENGER CABIN.(SM)(CPAX)(TCI 53-20-301) SUMMARY. SIDE SEAT RAILS 15RH BETWEEN FS847+16
- [SDR REXA2020040900437](https://openairdocs.org/sdr/REXA2020040900437.md): Canister · cracked · Mar 5, 2020 · N303PQ · Cndair CL6002D24 · Wing Miscellaneous Structure
  > INITIAL INSPECTION: CRACK IN CANISTER, WELDED NO.3 IN STA WS148 AT LH MAIN FUEL TANK. (AI) CANISTER, WELDED NO. 3 IN WS148 AT LH MAIN FUE
- [SDR REXA2020040900436](https://openairdocs.org/sdr/REXA2020040900436.md): Seal Depressor · worn · Mar 5, 2020 · N303PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > INITIAL INSPECTION. WEAR ON SEAL DEPRESSURE FS 517 AND 565, BTW STRG 23L-24L AT FWD CARGO BAY SURROUND. SEAL DEPRESSURE FS 517 BTW STRG 23L-24L AT FWD
- [SDR REXA2020042300538](https://openairdocs.org/sdr/REXA2020042300538.md): Stringer · corroded · Mar 4, 2020 · N303PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > INTIAL INSPECTION: CORROSION ON STRINGER 26RH BETWEEN FS 349 AND FS364 AT MAIN AVIONICS COMPARTMENT. (SM)(E/E)(CI 100-09E5) SUMMARY: STRINGER 26RH BTW FS=333 TO FS=364 WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01.
- [SDR REXA2020042300537](https://openairdocs.org/sdr/REXA2020042300537.md): Retainer · worn · Mar 3, 2020 · N303PQ · Cndair CL6002D24 · Engine Thrust Reverser
  > INITIAL INSPECTION: WEAR ON RETAINER 8E/A OF LOWER AND UPPER RH ENGINE TRASCOWL (MOT 2) SUMMARY: RETAINER 8E/A OF LOWER AND UPPER RH ENGINE TRASCOWL WERE REPLACED PER CRJ900 SRM 51-42-20-001-001-A01.
- [SDR REXA2020042300536](https://openairdocs.org/sdr/REXA2020042300536.md): Baffle · cracked · Mar 3, 2020 · N303PQ · Cndair CL6002D24 · Engine Thrust Reverser
  > INITIAL INSPECTION: CRACK ON BAFFLES 2E/A ON RH ENGINE LOWER THRUST REVERSER CASCADE FITTINGS.(MOT2) BAFFLES 2E/A ON RH ENGINE LOWER THRUST REVERSER CASCADE FITTINGS WERE REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 ADD
- [SDR REXA2020042300534](https://openairdocs.org/sdr/REXA2020042300534.md): Support Angle · corroded · Mar 3, 2020 · N303PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > AWR; [TASK R53520 STEP 7]; INITIAL INSPECTION: CORROSION ON SUPPORT MOUNTING ANGLE IN STA. FS= 319 TO FS= 349 AND 41RBL AT GALLEY SERVICEDOOR LOWER SILL,FWD WET AREA. (W1) (CPAX) SUMMARY: CORROSION ON ANGLE, LOWER SILL REMOVED PER CRJ900 SRM 51-21-0 6-001-00
- [SDR REXA2020042300533](https://openairdocs.org/sdr/REXA2020042300533.md): Support Angle · corroded · Mar 3, 2020 · N303PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > AWR; [TASK R53520 STEP 7]; INITIAL INSPECTION: CORROSION ON PROTECTION PLATE SUPPORT IN STA. FS= 346 BETWEEN 41RBL TO 44RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX) PROTECTION PLATE SUPPORTS ANGLE WAS REPLACED PER CRJ900 SRM 51-42-21-001-
- [SDR REXA2020042300532](https://openairdocs.org/sdr/REXA2020042300532.md): Support Angle · corroded · Mar 3, 2020 · N303PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > AWR; [TASK R53520 STEP 7]; INITIAL INSPECTION: CORROSION ON PROTECTION PLATE SUPPORT IN STA. FS= 322 BETWEEN 41RBL TO 44RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX) SUMMARY: PROTECTION PLATE SUPPORTS ANGLE WAS REPLACED PER CRJ900 SRM 51-4
- [SDR REXA2020042300531](https://openairdocs.org/sdr/REXA2020042300531.md): Support Angle · corroded · Mar 3, 2020 · N303PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > AWR; [TASK R53520 STEP 7]; INITIAL INSPECTION: CORROSION ON PROTECTION PLATE SUPPORTS ANGLE IN STA. FS= 346 BETWEEN 41RBL TO 44RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX) SUMMARY:CORROSION ON ANGLE, LOWER SILL WAS REMOVED PER CRJ900 SRM
- [SDR REXA2020042300529](https://openairdocs.org/sdr/REXA2020042300529.md): Support Angle · corroded · Mar 3, 2020 · N303PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > AWR; [TASK R53520 STEP 7]; INITIAL INSPECTION: CORROSION ON PROTECTION PLATE SUPPORTS ANGLE IN STA. FS= 329 BETWEEN 41RBL TO 44RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX) SUMMARY:PROTECTION PLATE SUPPORTS ANGLE WAS REPLACE
- [SDR REXA2020042300528](https://openairdocs.org/sdr/REXA2020042300528.md): Support Angle · corroded · Mar 3, 2020 · N303PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "AWR; [TASK R53520 STEP 7]; INITIAL INSPECTION: CORROSION ON PROTECTION PLATE SUPPORTS ANGLE IN STA. FS= 322 BETWEEN 41RBL TO 44RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX) " "SUMMARY: PROTECTION PLATE SUPPORTS ANGLE WAS REPLACED PER CRJ90
- [SDR REXA2020042300527](https://openairdocs.org/sdr/REXA2020042300527.md): Seat Track · corroded · Mar 3, 2020 · N303PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > INITIAL INSPECTION: CORROSION ON SEAT SIDE RAIL SECTION FS847+16 TO FS913, FS913 TO FS969 LH SIDE RAIL AT PASSENGER CABIN. (SM) (CPAX) (TCI 53-20-301) SEAT SIDE RAIL SECTION FS847+16 TO FS913, FS913 TO FS969 LH SIDE RAIL AT PASSENGER CABIN WERE REPLACED PER C
- [SDR REXA2020042300526](https://openairdocs.org/sdr/REXA2020042300526.md): Seat Track · corroded · Mar 3, 2020 · N303PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > INITIAL INSPECTION: CORROSION ON SEAT SIDE RAIL SECTIONS FS677 TO FS720.85, FS744.15 TO FS761.85, FS785.15 TO FS847+FS8.40, FS847+8.40 TO FS847+16 SIDE RAIL LH/RH SECTIONS AT PASSENGER CABIN.(SM)(CPAX)(TCI 53-20-301)
- [SDR REXA2020042300525](https://openairdocs.org/sdr/REXA2020042300525.md): Seat Track · corroded · Mar 3, 2020 · N303PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > INITIAL INSPECTION: CORROSION ON SEAT SIDE RAIL SECTIONS FS485 TO FS565, FS565 TO 661+16, FS 661+16 TO FS661+90 LH SIDE ALSO FS661 TO FS661+16,FS661+16 TO FS661+90 SECTION RH SIDE AT PASSENGER CABIN. (SM) (CPAX) (TCI 53-20-301) SEAT SIDE RAIL SECTIONS FS485 T
- [SDR REXA2020042300523](https://openairdocs.org/sdr/REXA2020042300523.md): Seat Track · corroded · Mar 3, 2020 · N303PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > INITIAL INSPECTION: CORROSION ON FLOOR SEAT RAILS IN SECTIONS [ FS= 349 TO FS= 485, 9RBL/LBL ] [FS485 TO FS581 9RBL][ FS= 661+32 TO FS= 847+8.40, 9LBL/9RBL ] ALSO [27LBL FS954 TO FS 985 AND 9LBL FS977 TO FS 985] AT PAX CABIN. (CPAX) (TCI: 53-20-243)
- [SDR REXA2020042300522](https://openairdocs.org/sdr/REXA2020042300522.md): Hinge · corroded · Mar 3, 2020 · N303PQ · Cndair CL6002D24 · Cargo Compartments
  > "PARTS RACK: CORROSION ON HINGES OF FLAP STEP PLATE AT AFT BAGGAGE BAY DOOR CUTOUT. (CCT). " "HINGES OF FLAP STEP PLATE AT AFT BAGGAGE BAY DOOR CUTOUT WERE REPLACED FOR NEW ONES PER CRJ-900 SRM 51-42-06-001-001-A01 PAR. 6A."
- [SDR REXA2020040900435](https://openairdocs.org/sdr/REXA2020040900435.md): Frame · corroded · Mar 3, 2020 · N303PQ · Cndair CL6002D24 · Fuselage Main, Frame
  > INITIAL INSPECTION. CORROSION ON FRAME FS 549, STRG 18 AT FWD CARGO BAY. (TCI 53-20-333). FRAME FS 549, STRG 18 AT FWD CARGO BAY WAS REP
- [SDR REXA2020040900430](https://openairdocs.org/sdr/REXA2020040900430.md): Retainer · worn · Mar 3, 2020 · N303PQ · Cndair CL6002D24 · Cargo/Baggage Doors
  > INITIAL INSPECTION: BENT SEAL RETAINER LOWER EDGE OF AFT CARGO COMPARTMENT DOOOR (PTAS) SEAL RETAINER LOWER EDGE OF AFT CARGO COMPARTMENT DOOOR WAS REPAIRED PER EA NO: CRJ952-10646 REV. IR
- [SDR REXA2020042300521](https://openairdocs.org/sdr/REXA2020042300521.md): Channel · cracked · Mar 2, 2020 · N303PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > INITIAL INSPECTION: CRACK ON CHANNEL OF AFT CARGO DOOR SURROUND STRUCTURE. (CCT) "CHANNEL OF AFT CARGO DOOR SURROUND STRUCTURE WAS REPLACED PER CRJ-900 SRM 51-41-02-001-001-A01."
- [SDR REXA2020042300519](https://openairdocs.org/sdr/REXA2020042300519.md): Channel · cracked · Mar 2, 2020 · N303PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > PARTS RACK:. CRACK ON CHANNEL 1E/A OF WING TO FUSELAGE FAIRING 196DR. (FUS) DAMAGED CHANNEL WAS REPLACED PER CRJ 900 SRM 51-42-10-001-001-A01

Next page: https://openairdocs.org/aircraft/N303PQ/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 = 'N303PQ' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N303PQ/reports

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