# Service difficulty reports: N295PQ A list on [N295PQ](https://openairdocs.org/aircraft/N295PQ.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 · 99 reports - [SDR REXA2026073101352](https://openairdocs.org/sdr/REXA2026073101352.md): Acoustic Panel · cracked · Jan 31, 2026 · N295PQ · Cndair CL6002D24 · Engine Thrust Reverser > AFTER Z STIFFENER REMOVAL, CRACK WAS FOUND AT ACOUSTIC PANEL SKIN OF THE RH UPPER TRANSCOWL ACOUSTIC PANEL SKIN OF THE RH UPPER TRANSCOWL WAS REPAIRED PER EA CRJ954-21346 REV IR - [SDR REXA2026030900196](https://openairdocs.org/sdr/REXA2026030900196.md): Frame · corroded · Jan 27, 2026 · N295PQ · Cndair CL6002D24 · Fuselage Main, Frame > CORROSION ON FRAME FS 379.00 BTW STGR 20RH TO 21 RH CORROSION ON FRAME FS 379.00 BTW STGR 20RH TO 21 RH WAS EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-21-06-101-006-A02 AND REPLACED PER CRJ-900 SRM 51-42-21-001-001-A01 AND SRM 51-42-06-001-001-A01, SNIEO S18 - [SDR REXA2026073101379](https://openairdocs.org/sdr/REXA2026073101379.md): Stringer · corroded · Jan 23, 2026 · N295PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer > CORROSION ON STRINGER 21R BTWN BS 333 - 349, THE CORROSION ON THE STRINGER WAS EVALUATED OUT LIMITS IAW SRM 53-21-03-101-006-A01, AND REPLACED IAW SRM 51-42-06-001-001-A01. - [SDR REXA2026030900186](https://openairdocs.org/sdr/REXA2026030900186.md): Angle · cracked · Jan 23, 2026 · N295PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CRACK ON FLOOR SUPPORT BTW FS278.00 TO FS280.00 AT RBL12 FLOOR SUPPORT BTW FS278.00 TO FS280.00 AT RBL12 WAS FABRICATED PER EA NO: CRJ953-20566 REV. AND REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND CRJ-900 SRM 51-42-21-001-001-A01 - [SDR REXA2026073101361](https://openairdocs.org/sdr/REXA2026073101361.md): Stringer Splice · corroded · Jan 22, 2026 · N295PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer > CORROSION ON JOINT PIECE STRG23 RH (1EA) REMOVE AND INSTALL OF NEW JOINT PIECE STRG 23 (1EA) WAS ATTENDED ON NRC292, EVALUATED OUT LIMITS PER CRJ-900 SRM 53-00-00-101-001-A01, DRILLED PER CRJ 900 SRM 51-40-11-001-001-A01 AND PAINTED PER CRJ 900 SRM 51-21-11- - [SDR REXA2026073101380](https://openairdocs.org/sdr/REXA2026073101380.md): Stringer · corroded · Jan 20, 2026 · N295PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer > AFTER REMOVAL OF THE INTERCOSTAL, CORROSION WAS FOUND IN STRINGER 20RT, BS 310. DUE TO EXCESSIVE DAMAGE, STRINGER 20R, BS 280 - 319 WILL BE REPLACED IAW SRM 53-21-03-101-002-A01, WAS REMOVED AND INSTALLED IAW SRM 51-42-06-001-001-A01. - [SDR REXA2026073101382](https://openairdocs.org/sdr/REXA2026073101382.md): Support Fitting · corroded · Dec 30, 2025 · N295PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CORROSION ON CARGO NET SUPPORT FITTINGS BS 515, 565, 629, & 661+16, LBL 2 IN THE FWD BAGGAGE BAY. DUE TO EXCESSIVE DAMAGE ON CARGO NET SUPPORT FITTINGS BS 515, 565, 629, & 661+16, LBL 2, THE PARTS WILL BE REPLACED IAW SRM 51-10-06-001-001-A01, REMOVED & IN - [SDR REXA2026073101381](https://openairdocs.org/sdr/REXA2026073101381.md): Support Fitting · corroded · Dec 30, 2025 · N295PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CORROSION ON CARGO NET SUPPORT FITTINGS BS 515, 565.00, 629, & 661+16, LBL 2 IN THE FWD BAGGAGE BAY. DUE TO EXCESSIVE DAMAGE ON CARGO NET SUPPORT FITTINGS BS 515, 565, 629, & 661+16, LBL 2 AT FWD BAGGAGE-BAY, THE PARTS WILL BE REPLACED IAW SRM 51-10-06-001-00 - [SDR REXA2026030900171](https://openairdocs.org/sdr/REXA2026030900171.md): Fitting · cracked · Dec 30, 2025 · N295PQ · Cndair CL6002D24 · Fuselage Main, Structure > CRACK ON BOTTOM ANGLE POST (2 EAS) LT & RT ON INTERNAL STRUCTURE BTWN WINDSHIELD AND SIDE WINDOWS. BOTTOM ANGLE POST (2 EAS) LH/RH ON INTERNAL STRUCTURE BTWN WINDSHIELD AND SIDE WINDOWS. WERE REPLACED PER CRJ900 SRM 51-42-21-001-001-A01. - [SDR REXA2026030900170](https://openairdocs.org/sdr/REXA2026030900170.md): Fitting · cracked · Dec 30, 2025 · N295PQ · Cndair CL6002D24 · Fuselage Main, Structure > CRACK ON BOTTOM ANGLE POST (2 EAS) LH/RH ON INTERNAL STRUCTURE BTWN WINDSHIELD AND SIDE WINDOWS. BOTTOM ANGLE POST (2 EAS) LH/RH ON INTERNAL STRUCTURE BTWN WINDSHIELD AND SIDE WINDOWS. WERE REPLACED PER SRM 51-42-21-001-001-A01 - [SDR REXA2026073101378](https://openairdocs.org/sdr/REXA2026073101378.md): Seat Track · corroded · Dec 29, 2025 · N295PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings > CORROSION ON RT SIDE SEAT TRACK (11 EAS) FROM BS 379 - 977 AT STR 15R IN PAX CABIN. CORROSION ON RT SIDE SEAT TRACK WAS EVALUATED OUT LIMITS IAW SRM 53-41-49-101-001-A02, SRM 53-51-49-101-001-A02, SRM 53-21-49-101-001-A01, AND SRM 53-31-49-101-001-A02, WAS R - [SDR REXA2026073101377](https://openairdocs.org/sdr/REXA2026073101377.md): Seat Track · corroded · Dec 29, 2025 · N295PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings > CORROSION ON LT SIDE SEAT TRACK (12 EAS) FROM BS 379 - 977, STGR 15L IN PAX CABIN. THE LT SIDE SEAT TRACK (12 EAS) FROM BS 379 TO 977 AT STR 15L AT PAX CAB. WERE EVALUATED OUT LIMITS IAW SRM 53-21-49-101-001-A01, SRM 53-41-49-101-001-A02, AND SRM 53-51-49-1 - [SDR REXA2026073101369](https://openairdocs.org/sdr/REXA2026073101369.md): Fitting · corroded · Dec 29, 2025 · N295PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CORROSION ON FITTINGS OF ACCESS 306 (2 EA) AT GALLEY 3. NEW FITTINGS OF ACCESS 306 (2 EA) AT GALLEY 3 WERE FABRICATED IAW EA CRJ953-21295 REV: IR. AND INSTALLED IAW CMM 25-33-18 - [SDR REXA2026073101353](https://openairdocs.org/sdr/REXA2026073101353.md): Seat Track · corroded · Dec 29, 2025 · N295PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings > CORROSION ON FLOOR SEAT RAILS RBL9 BTW FS850.00 TO FS977.00 AT CPAX. DUE TO EXCESIVE DAMAGE FLOOR SEAT RAILS RBL9 BTW FS850.00 TO FS977.00 AT CPAX WILL BE REPLACED PER CRJ-900 SRM 53-51-49-101-001-A02 AND WERE REPLACED PER CRJ-900 AMM 53-00-49 AND INSTALLED P - [SDR REXA2026030900185](https://openairdocs.org/sdr/REXA2026030900185.md): Floor Support · corroded · Dec 29, 2025 · N295PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CORROSION ON UPPER FACE OF FLOOR BEAM LBL 27 BTW FS 1000.00 TO FS 1047.00 ON AFT CARGO COMPARTMENT FLOOR STRUCTURE. CORROSION ON UPPER FACE OF FLOOR BEAM LBL 27 BTW FS 1000.00 TO FS 1047.00 ON AFT CARGO COMPARTMENT FLOOR STRUCTURE WAS EVALUATED OUT OF LIMITS P - [SDR REXA2026073101376](https://openairdocs.org/sdr/REXA2026073101376.md): Stringer Splice · corroded · Dec 28, 2025 · N295PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer > CORROSION ON STRINGER SPLICE 21R, BTWN BS 330 TO 336 AT MAIN AVIONICS BAY. THE STRINGER SPLICE 21R BTW BS 330 TO 336 AT MAIN AVIONICS BAY WAS EVALUATED OUT LIMITS IAW SRM 53-21-03-101-006-A04 AND REPLACED IAW SRM 51-42-21-001-001-A01, SRM 51-42-06-001-001-A - [SDR REXA2026073101375](https://openairdocs.org/sdr/REXA2026073101375.md): Stringer · corroded · Dec 28, 2025 · N295PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer > CORROSION ON STRINGER 24R, BTWN BS 295 TO 330 AT MAIN AVIONICS COMPARTMENT. CORROSION ON STR 24R BTW BS 295 TO 330 AT MAIN AVIONICS BAY WAS EVALUATED OUT LIMITS IAW SRM 53-21-03-101-002-A04, AND REPLACED IAW SRM 51-42-06-001-001-A01. - [SDR REXA2026073101368](https://openairdocs.org/sdr/REXA2026073101368.md): Door Sill · corroded · Dec 28, 2025 · N295PQ · Cndair CL6002D24 · Fuselage Main, Structure > SILL WITH CORROSION, LOWER PART OF CARGO COMPARTMENT DOOR FRAME AFT DUE TO EXCESS OF DAMAGE LOWER SILL OF CARGO COMPARTMENT DOOR FRAME AFT, WAS REPLACED PER CRJ-900 SRM 53-61-23-201-001-A01, CRJ-900 SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01 AND SRM 5 - [SDR REXA2026073101367](https://openairdocs.org/sdr/REXA2026073101367.md): Intercostal · corroded · Dec 28, 2025 · N295PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CORROSION ON INTERCOSTAL, STR 20RT, BS 310 - 364 IN FWD E/E BAY. THE INTERCOSTAL, WAS EVALUATED OUT OF LIMITS IAW SRM 53-21-23-101-002-A02, & REPLACED IAW SRM 51-42-21-001-001-A01. - [SDR REXA2026073101366](https://openairdocs.org/sdr/REXA2026073101366.md): Intercostal · corroded · Dec 28, 2025 · N295PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CORROSION ON INTERCOSTAL STR 20RT, BS 310 - 364, IN THE FWD E/E BAY. CORROSION ON INTERCOSTAL (3EAS), WERE EVALUATED OUT OF LIMITS IAW SRM 53-21-23-101-002-A02, AND REPLACED IAW SRM 51-42-21-001-001-A01. - [SDR REXA2026073101365](https://openairdocs.org/sdr/REXA2026073101365.md): Intercostal · corroded · Dec 28, 2025 · N295PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CORROSION ON INTERCOSTAL, STR 20 RT, BS 310 - 364 AT FWD E/E BAY. CORROSION ON INTERCOSTAL, STR 20RT, BS 310 - 364 AT FWD E/E BAY (3EAS), WERE EVALUATED OUT OF LIMITS IAW SRM 53-21-23-101-002-A02, AND WERE REPLACED IAW SRM 51-42-21-001-001-A01. - [SDR REXA2026030900184](https://openairdocs.org/sdr/REXA2026030900184.md): Stringer · corroded · Dec 28, 2025 · N295PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer > CORROSION ON STGR 24RH BTW FS333.00 TO FS349.00 AT MAIN AVIONICS COMPARTMENT STGR 24RH BTW FS333.00 TO FS349.00 AT MAIN AVIONICS COMPARTMENT WAS REPAIRED Ï¿½PER CRJ900 SRM 53-00-03-201-001-A02 - [SDR REXA2026030900174](https://openairdocs.org/sdr/REXA2026030900174.md): Stringer Splice · corroded · Dec 28, 2025 · N295PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer > CORROSION ON STRINGER SPLICE 24RH BTW FS330.00 TO FS336.00 AT MAIN AVIONICS COMPARTMENT STRINGER SPLICE 24RH BTW FS330.00 TO FS336.00 AT MAIN AVIONICS COMPARTMENT WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 & SRM 51-42-21-001-001-A01 - [SDR REXA2026030900159](https://openairdocs.org/sdr/REXA2026030900159.md): Stringer · corroded · Dec 28, 2025 · N295PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer > CORROSION ON STGR 20RH BTW FS349.00 TO FS379.00 AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT CORROSION ON STGR 20RH BTW FS349.00 TO FS379.00 AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT WAS REPAIRED PER EA NO: CRJ953-20473 REV IR - [SDR REXA2026030900183](https://openairdocs.org/sdr/REXA2026030900183.md): Rib · cracked · Dec 27, 2025 · N295PQ · Cndair CL6002D24 · Wing, Rib/Bulkhead > CRACK ON MACHINED RIB OF LEADING EDGE ON SS57.16 SIDE LEFT WING CRACK ON MACHINED RIB OF LEADING EDGE ON SS57.16 SIDE LEFT WING WAS REPAIRED REO 690-57-41-240 REV.- - [SDR REXA2026030900168](https://openairdocs.org/sdr/REXA2026030900168.md): Rib · cracked · Dec 27, 2025 · N295PQ · Cndair CL6002D24 · Wing, Rib/Bulkhead > CRACK ON MACHINED RIB LEADING EDGE SS57.16 AT RIGHT WING. CRACK ON MACHINED RIB LEADING EDGE SS57.16 AT RIGHT WING WERE REPAIRED PER GREO 690-57-41-240 REV-- - [SDR REXA2026073101364](https://openairdocs.org/sdr/REXA2026073101364.md): Seat Track · corroded · Dec 26, 2025 · N295PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings > CORROSION ON SEAT TRACKS RBL 9, LBL 9 AND LBL 27, BTW BS 349 - 485 AT PASSENGER CABIN DUE TO EXCESIVE DAMAGE SEAT TRACKS RBL 9, LBL 9 AND LBL 27, BTW BS 349 - 485 AT PASSENGER CABIN WILL BE REPLACED IAW SRM 53-21-49-101-001-A01 AND WERE REPLACED IAW AMM 53-00 - [SDR REXA2026073101363](https://openairdocs.org/sdr/REXA2026073101363.md): Striker · corroded · Dec 26, 2025 · N295PQ · Cndair CL6002D24 · Fuselage Main, Structure > CORROSION AT LOWER SILL, SEAL STRIKER & MOUNTING ANGLES OF WEB FLOOR PROTECTOR BTW FS 320.00 TO FS 349.00 OF SERVICE DOOR SURROUND STRUCTURE. CORROSION AT LOWER SILL, SEAL STRIKER & MOUNTING ANGLES OF WEB FLOOR PROTECTOR BTW FS 320.00 TO FS 349.00 OF SERVICE - [SDR REXA2026030900190](https://openairdocs.org/sdr/REXA2026030900190.md): Joint · corroded · Dec 26, 2025 · N295PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CORROSION ON CIRCUMFERENTIAL JOINT FS 280.0 TO FS 282.86 BTW STRGR 21RH TO STGR 24 RH AND BTW 25 RH TO 26 RH RH AT MAIN AVIONICS COMPARTMENT. AREA WAS CLEANED ON CIRCUMFERENTIAL JOINT FS 280.0 TO FS 282.86 BTW STRGR 20 RH TO STGR 20.5 RH AND 24.5 RH TO 26 RH - [SDR REXA2026030900189](https://openairdocs.org/sdr/REXA2026030900189.md): Floorbeam · cracked · Dec 26, 2025 · N295PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam > CRACKED CENTER COCKPIT FLOOR BEAM RBL12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT. CRACKED CENTER COCKPIT FLOOR BEAM RBL12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT WAS REPAIRED PER REO 690-53-11-2121 - [SDR REXA2026030900182](https://openairdocs.org/sdr/REXA2026030900182.md): Floorbeam · cracked · Dec 26, 2025 · N295PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam > CRACKED CENTER COCKPIT FLOOR BEAM RBL12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT. CRACKED CENTER COCKPIT FLOOR BEAM RBL12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT WAS REPAIRED PER REO 690-53-11-2121 - [SDR REXA2026030900167](https://openairdocs.org/sdr/REXA2026030900167.md): Support Angle · cracked · Dec 26, 2025 · N295PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CRACKED SUPPORT ANGLE (2 EAS) OF SHEAR BOX FS 280 LBL 12.0 AND RBL 12.0 MAIN AVIONICS COMPARTMENT. SUPPORT ANGLE (2 EAS) OF SHEAR BOX FS 280 LBL 12.0 AND RBL 12.0 MAIN AVIONICS COMPARTMENT WAS REPLACED ANGLES PER CRJ900 SRM 51-42-21-001-001-A01 - [SDR REXA2026030900166](https://openairdocs.org/sdr/REXA2026030900166.md): Support Angle · cracked · Dec 26, 2025 · N295PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CRACKED SUPPORT ANGLE (2 EAS) OF SHEAR BOX FS 280 LBL 12.0 AND RBL 12.0 MAIN AVIONICS COMPARTMENT. SUPPORT ANGLE (2 EAS) OF SHEAR BOX FS 280 LBL 12.0 AND RBL 12.0 MAIN AVIONICS COMPARTMENT WAS REPLACED ANGLES PER CRJ900 SRM 51-42-21-001-001-A01 - [SDR REXA2026030900181](https://openairdocs.org/sdr/REXA2026030900181.md): Canister · cracked · Dec 23, 2025 · N295PQ · Cndair CL6002D24 · Wing Miscellaneous Structure > CRACK IN WELDED CANISTER NO.3 IN STA. WS148 OF INTERNAL RH MAIN FUEL TANK. WELDED CANISTER NO.3 IN STA. WS148 OF INTERNAL RH MAIN FUEL TANK WAS REPAIRED PER REO 670-57-42-577.REV. - - [SDR REXA2026030900180](https://openairdocs.org/sdr/REXA2026030900180.md): Canister · cracked · Dec 23, 2025 · N295PQ · Cndair CL6002D24 · Wing Miscellaneous Structure > CRACK IN WELDED CANISTER NO.3 IN STA. WS148 OF INTERNAL LH MAIN FUEL TANK. WELDED CANISTER NO.3 IN STA. WS148 OF INTERNAL LH MAIN FUEL TANK WAS REPAIRED PER REO 670-57-42-577.REV. - - [SDR REXA2026073101372](https://openairdocs.org/sdr/REXA2026073101372.md): Stringer · corroded · Dec 22, 2025 · N295PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > INTERCOSTAL REMOVAL, CORROSION ON STRINGER 20R BTW BS 330 - 349 WAS FOUND CORRODED ON STRINGER 20R BTW BS330 TO 349 WAS EVALUATED OUT OF LIMITS IAW SRM 53-21-03-101-006-A02 AND REPLACED IAW SRM 51-42-21-001-001-A01 AND SRM 51-42-06-001-001-A01. - [SDR REXA2026030900199](https://openairdocs.org/sdr/REXA2026030900199.md): Bracket · cracked · Dec 22, 2025 · N295PQ · Cndair CL6002D24 · Fuselage Main, Attach Fittings > CRACK AT UPPER AND FWD LOWER SUPPORT ANGLES OF EXTERNAL POWER RECEPTACLE. UPPER AND FWD LOWER SUPPORT ANGLES OF EXTERNAL POWER RECEPTACLE WERE REPLACED PER CRJ900 SRM 51-42-21-001-001-A01 AND PER CRJ-900 SRM 51-42-10-001-001-A01 - [SDR REXA2026030900195](https://openairdocs.org/sdr/REXA2026030900195.md): Hinge · corroded · Dec 22, 2025 · N295PQ · Cndair CL6002D24 · Fuselage, Door Hinge > CORRODED HINGE AND HINGE FITTINGS OF AFT LAVATORY WASTE SERVICE ACCESS PANEL 196ER (4 EAS) CORRODED HINGE AND HINGE FITTINGS OF AFT LAVATORY WASTE SERVICE ACCESS PANEL 196ER (4 EAS) WERE EVALUATED OUT OF LIMITS PER PER CRJ 900 SRM 53-00-00-101-001-A01 AND RE - [SDR REXA2026030900194](https://openairdocs.org/sdr/REXA2026030900194.md): Hinge · corroded · Dec 22, 2025 · N295PQ · Cndair CL6002D24 · Fuselage, Door Hinge > CORRODED HINGE AND HINGE FITTINGS OF AFT LAVATORY WASTE SERVICE ACCESS PANEL 196ER (4 EAS) CORRODED HINGE AND HINGE FITTINGS OF AFT LAVATORY WASTE SERVICE ACCESS PANEL 196ER (4 EAS) WERE EVALUATED OUT OF LIMITS PER PER CRJ 900 SRM 53-00-00-101-001-A01 AND RE - [SDR REXA2026030900193](https://openairdocs.org/sdr/REXA2026030900193.md): Hinge · corroded · Dec 22, 2025 · N295PQ · Cndair CL6002D24 · Fuselage, Door Hinge > CORRODED HINGE AND HINGE FITTINGS OF AFT LAVATORY WASTE SERVICE ACCESS PANEL 196ER (4 EAS) CORRODED HINGE AND HINGE FITTINGS OF AFT LAVATORY WASTE SERVICE ACCESS PANEL 196ER (4 EAS) WERE EVALUATED OUT OF LIMITS PER PER CRJ 900 SRM 53-00-00-101-001-A01 AND RE - [SDR REXA2026030900192](https://openairdocs.org/sdr/REXA2026030900192.md): Hinge · corroded · Dec 22, 2025 · N295PQ · Cndair CL6002D24 · Fuselage, Door Hinge > CORRODED HINGE AND HINGE FITTINGS OF AFT LAVATORY WASTE SERVICE ACCESS PANEL 196ER (4 EAS) CORRODED HINGE AND HINGE FITTINGS OF AFT LAVATORY WASTE SERVICE ACCESS PANEL 196ER (4 EAS) WERE EVALUATED OUT OF LIMITS PER PER CRJ 900 SRM 53-00-00-101-001-A01 AND RE - [SDR REXA2026030900179](https://openairdocs.org/sdr/REXA2026030900179.md): Support · cracked · Dec 22, 2025 · N295PQ · Cndair CL6002D24 · Aerodynamic Fairings > CRACK ON WING TO FUSELAGE AFT FAIRING SUPPORT STRUCTURE AT FS849, LBL17. CRACK ON WING TO FUSELAGE AFT FAIRING SUPPORT STRUCTURE AT FS849, LBL17. WAS REPAIRED PER EA NO:CRJ953-21165 REV IR - [SDR REXA2026030900178](https://openairdocs.org/sdr/REXA2026030900178.md): Floor Support · corroded · Dec 22, 2025 · N295PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CRACK ON FLOOR BEAM 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 BEAM RBL 12.0 BTW FS 221.73 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE (FLIGHT COMPARTMENT FLOO - [SDR REXA2026030900173](https://openairdocs.org/sdr/REXA2026030900173.md): Drag Angle · cracked · Dec 22, 2025 · N295PQ · Cndair CL6002D24 · Vertical Stabilizer > CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD & AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00 FWD ANGLE NO CRACKS WERE FOUND PER CRJ 700/900/1000 NDT MANUAL PART 06. 53-00-000-250-A01 (EQUIPMENT: NORTEC 600 C/N - [SDR REXA2026030900169](https://openairdocs.org/sdr/REXA2026030900169.md): Support Angle · cracked · Dec 22, 2025 · N295PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CRACK AT UPPER AND FWD LOWER SUPPORT ANGLES OF EXTERNAL POWER RECEPTACLE. UPPER AND FWD LOWER SUPPORT ANGLES OF EXTERNAL POWER RECEPTACLE WERE REPLACED PER CRJ900 SRM 51-42-21-001-001-A01 AND PER CRJ-900 SRM 51-42-10-001-001-A01 - [SDR REXA2026030900163](https://openairdocs.org/sdr/REXA2026030900163.md): Bracket · cracked · Dec 22, 2025 · N295PQ · Cndair CL6002D24 · Wing Miscellaneous Structure > CRACKED RH & LH WING BRACKET SUPPORT ANGLE SS 15.50, LOWER INNER AREA (2 EAS) LH AND RH WING BRACKET SUPPORT ANGLE SS 15.50, LOWER INNER AREA (2 EAS) WERE REPLACED PER CRJ-900 SRM 51-42-13-001-001-A01 AND SRM 51-42-06-001-001-A01 - [SDR REXA2026030900162](https://openairdocs.org/sdr/REXA2026030900162.md): Bracket · cracked · Dec 22, 2025 · N295PQ · Cndair CL6002D24 · Wing Miscellaneous Structure > CRACKED RH & LH WING BRACKET SUPPORT ANGLE SS 15.50, LOWER INNER AREA (2 EAS) LH AND RH WING BRACKET SUPPORT ANGLE SS 15.50, LOWER INNER AREA (2 EAS) WERE REPLACED PER CRJ-900 SRM 51-42-13-001-001-A01 AND SRM 51-42-06-001-001-A01 - [SDR REXA2026030900188](https://openairdocs.org/sdr/REXA2026030900188.md): Landing · cracked · Dec 20, 2025 · N295PQ · Cndair CL6002D24 · Fuselage Main, Structure > CRACK ON AFT LH DOOR LANDING AT FS 188.00 (LATCH CUT OUT OF ACCESS DOOR 211AL) DOOR LANDING LH (LATCH CUT OUT OF ACCESS DOOR 211AL) WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 AND CRJ900 SRM 51-42-10-001-001-A01 - [SDR REXA2026030900176](https://openairdocs.org/sdr/REXA2026030900176.md): Support · cracked · Dec 20, 2025 · N295PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CRACK AT CORNERS SUPPORT OF THE JB 6 MODULE AT FWD EQUIPMENT COMPARTMENT. SUPPORT OF THE JB 6 MODULE AT FWD EQUIPMENT COMPARTMENT. REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 - [SDR REXA2026030900175](https://openairdocs.org/sdr/REXA2026030900175.md): Web · cracked · Dec 20, 2025 · N295PQ · 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 Next page: https://openairdocs.org/aircraft/N295PQ/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 = 'N295PQ' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N295PQ/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.