# Service difficulty reports: N294PQ

A list on [N294PQ](https://openairdocs.org/aircraft/N294PQ.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 · 74 reports

- [SDR REXA2026070201001](https://openairdocs.org/sdr/REXA2026070201001.md): Stringer · chafed · Jun 30, 2026 · N294PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > MAINTENANCE FOUND CHAFE DAMAGE ON STR 7L BETWEEN FS 1144.00 AND 1162.00 CAUSED BY LOOSE AND DAMAGED HEAT EXCHANGER DIFFUSER AND WATER SPRAYER LINE. REPAIRED CHAFE DAMAGE TO STR 7L IAW GREO 670-53-61-292 REV E
- [SDR REXA2025122401056](https://openairdocs.org/sdr/REXA2025122401056.md): Switch · out of position · Dec 21, 2025 · N294PQ · Cndair CL6002D24 · Indicating/Recording System
  > BURNING WIRE ODOR COMING FROM FO SIDE PFD OR MFD MAINLY IN FLIGHT. PERFORMED OPS TEST OF THE DISPLAY COOLING SYSTEM IAW AMM 21-24-00. OPS CHECK GOOD SWITCH WAS FOUND IN STBY.
- [SDR REXA2026052800831](https://openairdocs.org/sdr/REXA2026052800831.md): Bracket · corroded · Nov 2, 2025 · N294PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON BRACKETS, MACHINED (6EAS) OF INTERNAL STRUCTURE AT FWD CARGO COMPARTMENT. CORROSION ON BRACKETS, MACHINED (6EAS) OF INTERNAL STRUCTURE AT FWD CARGO COMPARTMENT WAS EVALUATED OUT PER CRJ-900 SRM 51-21-06-001-001-A01 AND REPLACED PER CRJ 900 SRM 51-
- [SDR REXA2026052800827](https://openairdocs.org/sdr/REXA2026052800827.md): Stiffener · cracked · Nov 2, 2025 · N294PQ · Cndair CL6002D24 · Passenger/Crew Doors
  > CRACK ON UPPPER STIFFENER ATTACHED TO POWER-ASSIST MOTOR BTW DATUM 4 AND DATUM 5 (AFT SIDE PANEL) OF PASSENGER DOOR INTERNAL STRUCTURE CRACK ON UPPPER STIFFENER ATTACHED TO POWER-ASSIST MOTOR BTW DATUM 4 AND DATUM 5 (AFT SIDE PANEL) OF PASSENGER DOOR INTERNAL
- [SDR REXA2026052800838](https://openairdocs.org/sdr/REXA2026052800838.md): Floorbeam · cracked · Oct 14, 2025 · N294PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > AFTER CUT DOOR POST RBL12 AT FS 280.00 LOWER SECTION OF THE BULKHEAD POST, CRACK ON FLOORBEAM WAS FOUND. FLOORBEAM WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01
- [SDR REXA2026052800818](https://openairdocs.org/sdr/REXA2026052800818.md): Lug · corroded · Oct 8, 2025 · N294PQ · Cndair CL6002D24 · Ailerons
  > CORROSION WAS FOUND ON LUGS BORES R1, R2, R3, R4, R5 AND R6 AT RH AILERON CENTER FITTING. BORE LUGS R3 AND R4 OF AILERON CENTER FITTING WAS CLEANED PER CRJ 900 SRM 51-26-00-001-001-A01 AND NOT DAMAGE FOUND & CENTER FITTING LUG BORES R1, R2, R5 AND R6 AILERON
- [SDR REXA2026052800816](https://openairdocs.org/sdr/REXA2026052800816.md): Floor Support · corroded · Oct 8, 2025 · N294PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSIN ON FLOOR SUPPORT LOCATED BTW FS1010.00AND LBL38. CORROSION ON FLOOR SUPPORT LOCATED BTW FS1010.00AND LBL38 WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01 AND EVALUATED OUT OFF LIMITS PER CRJ-900 SRM 53-00-00-101-001-A01 AND SUPPORT WAS REPLACED PER
- [SDR REXA2026052800837](https://openairdocs.org/sdr/REXA2026052800837.md): Seat Track · corroded · Oct 7, 2025 · N294PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON FLOOR SEAT RAILS IN SECTIONS [ BTW FS= 474 TO FS= 394, FS=437 AND BTW FS=597 TO 613 LBL 9.00 ] AT PAX CABIN. CORROSION ON FLOOR SEAT RAILS IN SECTIONS [ BTW FS= 474 TO FS= 394, FS=437 AND BTW FS=597 TO 613 LBL 9.00 ] AT PAX CABIN WAS EVALUATED OU
- [SDR REXA2026052800836](https://openairdocs.org/sdr/REXA2026052800836.md): Bearing · excess play · Oct 7, 2025 · N294PQ · Cndair CL6002D24 · Vertical Stabilizer Miscellaneous Structure
  > FREE PLAY ON SELF-ALIGN SELF-LUB BEARING PLAIN ON HINGE FITTING NR 2 AND NR 3 AT VERTICAL STABILIZER REAR SPAR MIDDLE SECTION. FITTING BEARINGS ON HINGE NO. 2 AND NO. 3 AT VERTICAL STABILIZER REAR SPAR MIDDLE SECTION WERE REPLACED AND FREE PLAY WAS CORRECTED
- [SDR REXA2026052800817](https://openairdocs.org/sdr/REXA2026052800817.md): Seat Track · corroded · Oct 7, 2025 · N294PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SIDE SEAT RAILS IN SECTIONS [ FS= 744, BTW FS=785 TO FS=793, FS=847+16 AND BTW FS=897 TO FS=913 STGR 15LH ] AND [ BTW FS= 744 TO FS=764, FS=785, BTW FS=846 TO FS=847+16 AND BTW FS=897 TO FS=927 STGR 15RH ] AT PAX CABIN. CORROSION ON SIDE TRACK IN
- [SDR REXA2026052800835](https://openairdocs.org/sdr/REXA2026052800835.md): Seat Track · corroded · Oct 6, 2025 · N294PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAIL 9RBL FS693 TO FS 847+16 (1E/A) FS847+16 TO FS977 (1E/A) AND SEAT RAIL 9LBL FS693 TO FS 847+16 (1E/A) FS847+16 TO FS977 (1E/A). CORROSION ON SEAT RAIL 9RBL FS693 TO FS 847+16 (1E/A) FS847+16 TO FS977 (1E/A) AND SEAT RAIL 9LBL FS693 TO FS
- [SDR REXA2026052800834](https://openairdocs.org/sdr/REXA2026052800834.md): Strap · corroded · Oct 6, 2025 · N294PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON INTERNAL STRAP, SETTLEMENT AREA OF FAIRING ACCESS PANEL 194AB & 193AB CORROSION ON INTERNAL STRAP, SETTLEMENT AREA OF FAIRING ACCESS PANEL 194AB & 193AB WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01 AND EVALUATED OUT LIMITS PER CRJ900 SRM 51-1
- [SDR REXA2026052800821](https://openairdocs.org/sdr/REXA2026052800821.md): Bonding Plate · corroded · Oct 6, 2025 · N294PQ · Cndair CL6002D24 · Nacelle/Pylon, Plate/Skin
  > CORROSION ON UPPER/LOWER BONDING PLATES AT AFT SKIN, LH/RH PYLONS. CORROSION ON UPPER/LOWER BONDING PLATES AT AFT SKIN, LH/RH PYLONS WAS EVALUATED WITH EXCESSIVE DAMAGE PER CRJ-900 SRM 53-00-00-101-001-A01 AND UPPER/LOWER BONDING PLATES AT AFT SKIN WERE REPLAC
- [SDR REXA2026052800832](https://openairdocs.org/sdr/REXA2026052800832.md): Stringer Splice · corroded · Oct 5, 2025 · N294PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STGR 21RH BTW FS394.00 TO FS 409.00 AT MAIN AVIONICS COMPARTMENT STGR 21RH BTW FS394.00 TO FS 409.00 AT MAIN AVIONICS COMPARTMENT WAS REPAIRED AND SFECU 2, COVER, RACK AND GS (GS484, GS454, GS464) WERE REMOVED/INSTALLED OPS CHECK GOOD PER EA CRJ95
- [SDR REXA2026052800820](https://openairdocs.org/sdr/REXA2026052800820.md): Retainer · cracked · Oct 5, 2025 · N294PQ · Cndair CL6002D24 · Cargo/Baggage Doors
  > WEAR ON LOWER SEAL RETAINER OF CENTER BAGGAGE-BAY DOOR; CRACKS ON LOWER SEAL RETAINER OF FWD BAGGAGE-BAY DOOR; AND BENTS ON LOWER PLATE OF CENTER AND FWD BAGGAGE-BAY DOOR. LOWER SEAL RETAINER OF CENTER BAGGAGE-BAY DOOR AND LOWER PLATE OF CENTER AND FWD BAGGAGE
- [SDR REXA2026052800815](https://openairdocs.org/sdr/REXA2026052800815.md): Intercostal · corroded · Oct 5, 2025 · N294PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "CORROSION ON INTERCOSTAL (3E/A) BTW FS 364 TO FS 369 STGR 26L TO STGR 25R CORROSION ON INTERCOSTAL (3E/A) BTW FS 364 TO FS 369 STGR 26L TO STGR 25R WAS REMOVED PER CRJ 900 SRM 51-21-06-001-001-A01 AND EVALUATED INTERCOSTALS (2EA'S) BTW FS 364 TO FS 369 ST
- [SDR REXA2026052800814](https://openairdocs.org/sdr/REXA2026052800814.md): Bolt · stuck · Oct 3, 2025 · N294PQ · Cndair CL6002D24 · Ailerons
  > A STUCK BOLT WAS DETECTED IN THE AILERON LUG T/E ALSO DAMAGE TO BOTH LUG 2 AND 3. A STUCK BOLT WAS REMOVED PER CRJ 900 SRM 51-40-11-001-001-A01 AND DAMAGE TO BOTH LUG 2 AND 3 WERE REPAIRED PER REO 690-57-51-482 REV. -A
- [SDR REXA2026052800839](https://openairdocs.org/sdr/REXA2026052800839.md): Web · cracked · Oct 2, 2025 · N294PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK ON ELECTRICAL BAY FLOOR WEB RIGHT SIDE (BELOW ADG SUPPORT DOUBLER) FS193.00 REPAIR ON ELECTRICAL BAY FLOOR WEB RIGHT SIDE (BELOW ADG SUPPORT DOUBLER) FS193.00 WAS PERFORMED PER CRJ900 SRM 53-11-43-201-001-A01
- [SDR REXA2026052800828](https://openairdocs.org/sdr/REXA2026052800828.md): Floor Support · cracked · Oct 2, 2025 · N294PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK ON FLOOR SUPPORT RBL 12.0 BTW FS 221.73 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE (FLIGHT COMPARTMENT FLOOR STRUCTURE BELOW WL79.50). CRACK ON FLOOR SUPPORT RBL 12.0 BTW FS 221.73 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE (FLIGHT COMPARTMENT
- [SDR REXA2026052800813](https://openairdocs.org/sdr/REXA2026052800813.md): Support · cracked · Oct 2, 2025 · N294PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK ON JB6 SUPPORT AT FWD EQUIPMENT COMPARTMENT. JB6 SUPPORT AT FWD EQUIPMENT COMPARTMENT/JUNCTION BOX 6 (JB-6) WERE REMOVED AND INSTALLED PER CRJ 900 SRM 51-42-06-001-001-A01, AMM 24-04-15-000-801-A01 AND AMM 24-04-15-400-801-A01. JB6 SUPPORT (P/N: CC670-5
- [SDR REXA2026052800826](https://openairdocs.org/sdr/REXA2026052800826.md): Support Plate · corroded · Oct 1, 2025 · N294PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "CORROSION ON HYDRAULIC SUPPORT PLATES(2E/A) ALSO CORROSION ON SEVERAL WASHERS AT 40 RBL/LBL IN THE WHEEL WELL AREA. CORROSION ON HYDRAULIC SUPPORT PLATES(2E/A AT 40 RBL/LBL IN THE WHEEL WELL AREA WAS REMOVED AND EVALUATED IN LH SUPPORT ORIGINAL THICKNESS IS:
- [SDR REXA2026052800825](https://openairdocs.org/sdr/REXA2026052800825.md): Structure · cracked · Sep 30, 2025 · N294PQ · Cndair CL6002D24 · Emergency Exits
  > CRACK AT OVERWING EMERGENCY EXIT DOOR RH AFT TOP SECTION (AROUND BASE OF DOOR PROXIMITY SENSOR STRIKER). EMERGENCY EXIT DOOR RH AFT TOP SECTION (AROUND BASE OF DOOR PROXIMITY SENSOR STRIKER) WAS REPAIRED PER REO 670-52-21-103 REV. --
- [SDR REXA2026052800824](https://openairdocs.org/sdr/REXA2026052800824.md): Structure · cracked · Sep 30, 2025 · N294PQ · Cndair CL6002D24 · Emergency Exits
  > CRACK AT OVERWING EMERGENCY EXIT DOOR RH FWD TOP SECTION (AROUND BASE OF DOOR PROXIMITY SENSOR STRIKER). EMERGENCY EXIT DOOR RH FWD TOP SECTION (AROUND BASE OF DOOR PROXIMITY SENSOR STRIKER) WAS REPAIRED REO 670-52-21-103 REV. --
- [SDR REXA2026052800812](https://openairdocs.org/sdr/REXA2026052800812.md): Drag Angle · cracked · Sep 30, 2025 · N294PQ · Cndair CL6002D24 · Fuselage, Stabilizer Attach Fittings
  > CRACK ON RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 61.56% STRG DATUM TO 67.5% REAR SPAR DATUM REPAIR ON CRACK ON RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 61.56% STRG DATUM TO 67.5% REAR SPAR DATUM WAS PERFORMED PE
- [SDR REXA2026052800811](https://openairdocs.org/sdr/REXA2026052800811.md): Striker · cracked · Sep 30, 2025 · N294PQ · Cndair CL6002D24 · Emergency Exits
  > CRACK AT OVERWING EMERGENCY EXIT DOOR LH FWD TOP SECTION (AROUND BASE OF DOOR PROXIMITY SENSOR STRIKER). EMERGENCY EXIT DOOR LH FWD TOP SECTION (AROUND BASE OF DOOR PROXIMITY SENSOR STRIKER) WAS REPAIRED PER REO 670-52-21-103 REV -.
- [SDR REXA2026052800810](https://openairdocs.org/sdr/REXA2026052800810.md): Door · cracked · Sep 30, 2025 · N294PQ · Cndair CL6002D24 · Emergency Exits
  > CRACK AT OVERWING EMERGENCY EXIT DOOR LH AFT TOP SECTION (AROUND BASE OF DOOR PROXIMITY SENSOR STRIKER). EMERGENCY EXIT DOOR LH AFT TOP SECTION (AROUND BASE OF DOOR PROXIMITY SENSOR STRIKER) WAS REPAIRED PER REO 670-52-21-103 REV. --
- [SDR REXA2026052800822](https://openairdocs.org/sdr/REXA2026052800822.md): Support Angle · cracked · Sep 26, 2025 · N294PQ · Cndair CL6002D24 · Wing Miscellaneous Structure
  > CRACKED SUPPORT ANGLE OF WING RH SIDE, SUPPORT ANGLE OF ACCESS PANEL 642AZ. SUPPORT ANGLE OF WING RH SIDE, SUPPORT ANGLE OF ACCESS PANEL 642AZ WAS REPLACED PER CRJ 900 SRM 51-42-21-001-001-A01
- [SDR REXA2025013100108](https://openairdocs.org/sdr/REXA2025013100108.md): Unknown · odor · Jan 28, 2025 · N294PQ · Cndair CL6002D24 · Air Distribution System
  > DURING FLIGHT AFTER SETTING TO POWER ODD ODOR BEGAN COMING OUT OF AIR VENT. NO VISIBLE SMOKE AND SCENT OF THE SMELL WAS THROUGHOUT AIRPLANE. SCENT DISSAPATED AFTER A FEW MINUTES. CREW REPORTED PLASTIC ODOR IN AIRCRAFT, C/W FIM 21-22-00 AND TS# 002736-R1, NO
- [SDR REXA2022120602680](https://openairdocs.org/sdr/REXA2022120602680.md): Web · cracked · Dec 2, 2022 · N294PQ · Cndair CL6002D24 · Fuselage Main, Structure
  > PAX DOOR AFT WEB IS CRACKED AT (2) STEP LOCATIONS. REPAIRED IAW REO 690-52-11-798 REV-.
- [SDR REXA2022120602679](https://openairdocs.org/sdr/REXA2022120602679.md): Channel · cracked · Dec 2, 2022 · N294PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR OPENING UPPER SUPPORT C CHANNEL IS CRACKED. REPLACED IAW CRJ 900 SRMS 51-42-06-001-001-A01, 51-41-02-001-001-A01, 51-42-13-001-001-A01, AND 51-25-21-001-001-A01.
- [SDR REXA2022120602678](https://openairdocs.org/sdr/REXA2022120602678.md): Striker · corroded · Dec 2, 2022 · N294PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > SERVICE DOOR LOWER SEAL STRIKER CORRODED AT ALL SCREW HOLES. REPLACED IAW CRJ 900 SRMS 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.
- [SDR REXA2022120602677](https://openairdocs.org/sdr/REXA2022120602677.md): Bulkhead Web · corroded · Dec 1, 2022 · N294PQ · Cndair CL6002D24 · Fuselage Main, Bulkhead
  > FS 280.00 LH AFT LOWER WEB IS CORRODED. REPLACED IAW CRJ 900 SRM 53-11-10-201-004-A01.
- [SDR REXA2022120202668](https://openairdocs.org/sdr/REXA2022120202668.md): Web · corroded · Dec 1, 2022 · N294PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FS 280.00 RH AFT LOWER WEB IS CORRODED. REPLACED IAW CRJ 900 SRM 53-11-10-201-004-A01.
- [SDR REXA2022120602676](https://openairdocs.org/sdr/REXA2022120602676.md): Panel · chafed · Nov 21, 2022 · N294PQ · Cndair CL6002D24 · Wing, Control Surfaces
  > PANEL 584LB IS CHAFED. REQUIRES EVAL. BLENDED CHAFE IAW SRM 51-12-00-001-001-A01. FOUND TO BE OUT OF ALLOWABLE LIMITS IAW SRM 57-52-01-101-001-A01. REPAIRED PANEL 584LB IAW EO CL-600-2D24-57-LO7275.
- [SDR REXA2022120102651](https://openairdocs.org/sdr/REXA2022120102651.md): Seat Track · corroded · Nov 18, 2022 · N294PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > THE FWD FLOOR SEAT TRACK AT RBL 9 IS HEAVILY CORRODED AT APPROX. FS 349-364 AND REQUIRES REPLACEMENT. NSTALLED NEW SERVICEABLE SEAT TRACK (PN:SH670-32159-1) IAW CRJ 900 AMM 53-00-49-400-801-A12
- [SDR REXA2022120102629](https://openairdocs.org/sdr/REXA2022120102629.md): Floor Support · corroded · Nov 16, 2022 · N294PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > RH FLOOR SUPPORT CORRODED AT BS 280. REPLACED THE FLOOR SUPPORT BETWEEN BS 280 - 319 IAW SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01 & 51-42-21-001-001-A01.
- [SDR REXA2022120102632](https://openairdocs.org/sdr/REXA2022120102632.md): Floorbeam · corroded · Nov 14, 2022 · N294PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > FS 280.00 RH CROSS BEAM IS CORRODED. REPLACED RH FS 280 CROSS BEAM PN CC670-34094-2 IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01, 51-42-21-001-001-A01
- [SDR REXA2022120102631](https://openairdocs.org/sdr/REXA2022120102631.md): Angle · corroded · Nov 14, 2022 · N294PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > FS 280.00 CROSSBEAM J-ANGLE IS CORRODED. REPLACED FS280 CROSSBEAM J ANGLE IAW SRM 51-42-06-001-001-A01 51-42-21-001-001-A01
- [SDR REXA2022120102630](https://openairdocs.org/sdr/REXA2022120102630.md): Drag Angle · cracked · Nov 13, 2022 · N294PQ · Cndair CL6002D24 · Vertical Stabilizer
  > VERTICAL STABILIZER, L/H AFT DRAG ANGLE IS CRACKED. REPLACED AFT L/H VERT DRAG ANGLE IAW CRJ-900-SRM-51-42-13-001-001-A01, 51-42-22-001-001-A01 AND 51-42-21-001-001-A01.
- [SDR REXA2019060730812](https://openairdocs.org/sdr/REXA2019060730812.md): Overhead Bin · out of rig · Jun 3, 2019 · N294PQ · Cndair CL6002D24 · Passenger Compartment Equipment
  > FOUND LH FWD EMER DOOR DOES NOT OPEN. RERIGGED OVER HEAD BIN ABOVE LH FWD EMER DOOR IAW 25-23-01 OPS CHECK GOOD
- [SDR REXA2019041250460](https://openairdocs.org/sdr/REXA2019041250460.md): Light · missing · Apr 5, 2019 · N294PQ · Cndair CL6002D24 · Emergency Lighting
  > EMER LIGHT STRIP MISSING 9 A/B. REPLACED EMER LIGHT IAW AMM 33-51-01.
- [SDR REXA2019031300280](https://openairdocs.org/sdr/REXA2019031300280.md): Angle · corroded · Mar 13, 2019 · N294PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > AWR: CORROSION ON ANGLE MOUNTING AND PROTECTOR WED FLOOR AT SERVICE DOOR SILL FS 319 TO FS 349, STR 17R. (TCI: 53-20-315) (CPAX) SUMMARY OF CARD 00127: ANGLE MOUNTING AND PROTECTOR WED FLOOR AT SERVICE DOOR SILL FS 319 TO FS 349, STR 17R WERE REPLACED PER SRM
- [SDR REXA2019031200272](https://openairdocs.org/sdr/REXA2019031200272.md): Door Sill · corroded · Mar 12, 2019 · N294PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > INITIAL INSPECTION: CORROSION ON RH FLOOR SILLS FS 280 TO FS 310. (TCI: 53-20-315) (CPAX) DUE TO SEVERAL CORROSION ON RH FLOOR SILL FS 280 TO FS 310 SILL WAS REPLACED PER SRM 53-00-45-201-001-A01 PAR.6.B, SRM 51-42-10-001-001-A01, SRM 51-42-06-001-001-A01 AND
- [SDR REXA2019031100286](https://openairdocs.org/sdr/REXA2019031100286.md): Seat Track · corroded · Mar 11, 2019 · N294PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > INITIAL INSPECTION. CORROSION AND SCRATCHES ON SIDE SEAT RAIL (RT/LT) FROM 672 TO 722, 743 TO 763, 785 TO 847, 847 TO 907, 907 TO 986 AT PAX CABIN. (SM)(CPAX)(TCI 53-20-318). (CORROSION LEVEL 2) SEAT RAILS (RT/LT) FROM 672 TO 722, 743 TO 763, 785 TO 847, 847 T
- [SDR REXA2019031100285](https://openairdocs.org/sdr/REXA2019031100285.md): Seat Track · corroded · Mar 11, 2019 · N294PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > INITIAL INSPECTION. CORROSION AND SCRATCHES ON SIDE SEAT RAIL (LT/RT) FROM 379 TO 483, 483 TO 573, 573 TO 661+14, 661+14 TO 672 AT PAX CABIN. (SM)(CPAX)(TCI 53-20-301). (CORROSION LEVEL 2) SEAT RAIL (LT/RT) FROM 379 TO 483, 483 TO 573, 573 TO 661+14, 661+14 TO
- [SDR REXA2019031100284](https://openairdocs.org/sdr/REXA2019031100284.md): Seat Track · corroded · Mar 11, 2019 · N294PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > INITIAL INSPECTION. CORROSION AND SCRATCHES ON FLOOR SEAT RAIL (LBL9, RBL9) FROM 485 TO 581, 581 TO 661+32, 661+32 TO 683 AT PAX CABIN. (SM)(CPAX)(TCI 53-20-318). (CORROSION LEVEL 2) FLOOR SEAT RAIL (LBL9, RBL9) FROM 485 TO 581, 581 TO 661+32, 661+32 TO 683 A
- [SDR REXA2019031100283](https://openairdocs.org/sdr/REXA2019031100283.md): Seat Track · corroded · Mar 11, 2019 · N294PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > INITIAL INSPECTION. CORROSION AND SCRATCHES ON FLOOR SEAT RAIL FROM 364 TO 485 (LBL27, LBL9, RBL9) AT PAX CABIN. (CORROSION LEVEL 2) SEAT RAIL FROM 364 TO 485 (LBL27, LBL9, RBL9) WAS REPLACED PER AMM 53-00-49-400-801 (CONF. A12)
- [SDR REXA2019031100278](https://openairdocs.org/sdr/REXA2019031100278.md): Stringer · corroded · Mar 11, 2019 · N294PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > INITIAL INSPECTION: CORROSION ON STRINGER 25R AND 26R FROM FS= 280 TO FS= 330 AT MAIN AVIONICS COMPARTMENT. (E/E) (TCI:53-20-304). STRINGER 25R AND 26R FROM FS= 280 TO FS= 330 WERE REPLACED PER SRM 51-42-06-001-001-A01 AND SRM 51-42-20-001-001-A01 AND EA NO:
- [SDR REXA2019031100275](https://openairdocs.org/sdr/REXA2019031100275.md): Frame · corroded · Mar 11, 2019 · N294PQ · Cndair CL6002D24 · Fuselage Main, Frame
  > INITIAL INSPECTION: CORROSION ON FRAME IN STA. FS= 295 BETWEEN STRG 26L TO 25R AT MAIN AVIONIC COMPARTMENT. (E/E)(TCI:53-20-304. FRAME IN STA. FS= 295 WAS REPAIR PER EA NO.: CRJ953-08476 REV IR
- [SDR REXA2019031100274](https://openairdocs.org/sdr/REXA2019031100274.md): Doubler · corroded · Mar 11, 2019 · N294PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > INITIAL INSPECTION: CORROSION ON INTERNAL DOUBLER IN STA. FS= 295 TO FS= 310 BETWEEN STRG 26L TO 26R AT MAIN AVIONICS COMPARTMENT. (E/E)(TCI:53-20-304. COMPLETE: INTERNAL DOUBLER IN STA. FS= 295 TO FS= 310 BETWEEN STRG 26L TO 26R WAS REPAIR PER EA NO.: CRJ95

Next page: https://openairdocs.org/aircraft/N294PQ/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 = 'N294PQ' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N294PQ/reports

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