N295PQ

Service difficulty reports · 99

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR REXA2026073101352Acoustic Panel · crackedAFTER 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 IRJan 31, 2026 · N295PQ · Cndair CL6002D24 · Engine Thrust ReverserSDR REXA2026030900196Frame · corrodedCORROSION 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 S18Jan 27, 2026 · N295PQ · Cndair CL6002D24 · Fuselage Main, FrameSDR REXA2026073101379Stringer · corrodedCORROSION 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.Jan 23, 2026 · N295PQ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2026030900186Angle · crackedCRACK 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-A01Jan 23, 2026 · N295PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026073101361Stringer Splice · corrodedCORROSION 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-Jan 22, 2026 · N295PQ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2026073101380Stringer · corrodedAFTER 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.Jan 20, 2026 · N295PQ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2026073101382Support Fitting · corrodedCORROSION 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 & INDec 30, 2025 · N295PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026073101381Support Fitting · corrodedCORROSION 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 51-10-06-001-00Dec 30, 2025 · N295PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026030900171Fitting · crackedCRACK 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.Dec 30, 2025 · N295PQ · Cndair CL6002D24 · Fuselage Main, StructureSDR REXA2026030900170Fitting · crackedCRACK 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-A01Dec 30, 2025 · N295PQ · Cndair CL6002D24 · Fuselage Main, StructureSDR REXA2026073101378Seat Track · corrodedCORROSION 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 RDec 29, 2025 · N295PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2026073101377Seat Track · corrodedCORROSION 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 53-51-49-1Dec 29, 2025 · N295PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2026073101369Fitting · corrodedCORROSION 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 25-33-18Dec 29, 2025 · N295PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026073101353Seat Track · corrodedCORROSION 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 PDec 29, 2025 · N295PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2026030900185Floor Support · corrodedCORROSION 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 PDec 29, 2025 · N295PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026073101376Stringer Splice · corrodedCORROSION 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-ADec 28, 2025 · N295PQ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2026073101375Stringer · corrodedCORROSION 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.Dec 28, 2025 · N295PQ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2026073101368Door Sill · corrodedSILL 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 5Dec 28, 2025 · N295PQ · Cndair CL6002D24 · Fuselage Main, StructureSDR REXA2026073101367Intercostal · corrodedCORROSION 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.Dec 28, 2025 · N295PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026073101366Intercostal · corrodedCORROSION 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.Dec 28, 2025 · N295PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026073101365Intercostal · corrodedCORROSION 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.Dec 28, 2025 · N295PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026030900184Stringer · corrodedCORROSION 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-A02Dec 28, 2025 · N295PQ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2026030900174Stringer Splice · corrodedCORROSION 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-A01Dec 28, 2025 · N295PQ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2026030900159Stringer · corrodedCORROSION 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 IRDec 28, 2025 · N295PQ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2026030900183Rib · crackedCRACK 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.-Dec 27, 2025 · N295PQ · Cndair CL6002D24 · Wing, Rib/BulkheadSDR REXA2026030900168Rib · crackedCRACK 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--Dec 27, 2025 · N295PQ · Cndair CL6002D24 · Wing, Rib/BulkheadSDR REXA2026073101364Seat Track · corrodedCORROSION 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 53-00Dec 26, 2025 · N295PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2026073101363Striker · corrodedCORROSION 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 SERVICEDec 26, 2025 · N295PQ · Cndair CL6002D24 · Fuselage Main, StructureSDR REXA2026030900190Joint · corrodedCORROSION 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 RHDec 26, 2025 · N295PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026030900189Floorbeam · crackedCRACKED 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 690-53-11-2121Dec 26, 2025 · N295PQ · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR REXA2026030900182Floorbeam · crackedCRACKED 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 690-53-11-2121Dec 26, 2025 · N295PQ · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR REXA2026030900167Support Angle · crackedCRACKED 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-A01Dec 26, 2025 · N295PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026030900166Support Angle · crackedCRACKED 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-A01Dec 26, 2025 · N295PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026030900181Canister · crackedCRACK 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. -Dec 23, 2025 · N295PQ · Cndair CL6002D24 · Wing Miscellaneous StructureSDR REXA2026030900180Canister · crackedCRACK 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. -Dec 23, 2025 · N295PQ · Cndair CL6002D24 · Wing Miscellaneous StructureSDR REXA2026073101372Stringer · corrodedINTERCOSTAL 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.Dec 22, 2025 · N295PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026030900199Bracket · crackedCRACK 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-A01Dec 22, 2025 · N295PQ · Cndair CL6002D24 · Fuselage Main, Attach FittingsSDR REXA2026030900195Hinge · corrodedCORRODED 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 REDec 22, 2025 · N295PQ · Cndair CL6002D24 · Fuselage, Door HingeSDR REXA2026030900194Hinge · corrodedCORRODED 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 REDec 22, 2025 · N295PQ · Cndair CL6002D24 · Fuselage, Door HingeSDR REXA2026030900193Hinge · corrodedCORRODED 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 REDec 22, 2025 · N295PQ · Cndair CL6002D24 · Fuselage, Door HingeSDR REXA2026030900192Hinge · corrodedCORRODED 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 REDec 22, 2025 · N295PQ · Cndair CL6002D24 · Fuselage, Door HingeSDR REXA2026030900179Support · crackedCRACK 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 IRDec 22, 2025 · N295PQ · Cndair CL6002D24 · Aerodynamic FairingsSDR REXA2026030900178Floor Support · corrodedCRACK 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 FLOODec 22, 2025 · N295PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026030900173Drag Angle · crackedCRACK 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 Dec 22, 2025 · N295PQ · Cndair CL6002D24 · Vertical StabilizerSDR REXA2026030900169Support Angle · crackedCRACK 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-A01Dec 22, 2025 · N295PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026030900163Bracket · crackedCRACKED 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-A01Dec 22, 2025 · N295PQ · Cndair CL6002D24 · Wing Miscellaneous StructureSDR REXA2026030900162Bracket · crackedCRACKED 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-A01Dec 22, 2025 · N295PQ · Cndair CL6002D24 · Wing Miscellaneous StructureSDR REXA2026030900188Landing · crackedCRACK 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-A01Dec 20, 2025 · N295PQ · Cndair CL6002D24 · Fuselage Main, StructureSDR REXA2026030900176Support · crackedCRACK 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-A01Dec 20, 2025 · N295PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026030900175Web · crackedCRACK 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-A01Dec 20, 2025 · N295PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
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