N296PQ

Service difficulty reports · 115

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 = 'N296PQ' 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 REXA2026101601934Frame · corrodedAFTER CORROSION REMOVAL ON FRAME BS 794 FOUND OUT OF LIMITS. REPLACED THE FRAME IAW SRM 51-42-21-001-001-A01.Oct 3, 2026 · N296PQ · Cndair CL6002D24 · Fuselage Main, FrameSDR REXA2026101601942Shim · crackedCRACKED SHIM ON THE SETTLEMENT AREA OF ACCESS PANEL 413AT. THE SHIM WAS REPAIRED IAW EA CRJ 954-23158, REV B.Sep 29, 2026 · N296PQ · Cndair CL6002D24 · Nacelle/Pylon Miscellaneous StructureSDR REXA2026101601941Doubler · crackedCRACKED DOUBLER ON THE HANDLE OF AFT BAGGAGE DOOR. THE DOUBLER WAS REPLACED IAW SRM 51-42-21-001-001-A01.Sep 29, 2026 · N296PQ · Cndair CL6002D24 · Cargo/Baggage DoorsSDR REXA2026101601939Rib · crackedCRACKED RIB SS 58.41, RT WING LE, THE RIB WAS REPLACED IAW SRM 51-42-06-001-001-A01, SRM 51-42-10-001-001-A01, AND SRM 51-42-21-001-001-A01.Sep 23, 2026 · N296PQ · Cndair CL6002D24 · Wing, Rib/BulkheadSDR REXA2026101601933Stringer Splice · corrodedAFTER REMOVAL OF STRINGER 21R, CORROSION WAS FOUND ON THE STRINGER SPLICE, BETWEEN BS 469 - 485. THE STRINGER SPLICE WAS REPLACED IAW SRM 51-42-06-001-001-A01, & SRM 51-42-21-001-001-A01.Sep 23, 2026 · N296PQ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2026101601937Access Panel · chafedWORN WING ACCESS PANELS, 584FT, 599CB, 584BB, 599BB, 584GB, 584JB, 584EB, 584LB, 584AB, 584ET, 699BB, 699AB, 684ET, 684HT, 684BB, 684EB, 684GB, 684JB, & 684LB. ACCESS PANELS NBR 584FT, 599CB, 584BB, 599BB, 584GB, 584JB.584EB,584LB, 584AB,584ET, 699BB, 699AB, Sep 22, 2026 · N296PQ · Cndair CL6002D24 · Wing, Plate/SkinSDR REXA2026101601936Access Panel · wornWORN WING ACCESS PANELS, 584FT, 599CB, 584BB, 599BB, 584GB, 584JB.584EB, 584LB, 584AB, 584ET, 699BB, 699AB, 684ET, 684HT, 684BB, 684EB, 684GB, 684JB, & 684LB. THE ACCESS PANELS WERE BLENDED OUT IAW SRM 51-12-00-001-001-A01. NR 584EB, 684ET, & 684EB WERE EVASep 22, 2026 · N296PQ · Cndair CL6002D24 · Wing, Plate/SkinSDR REXA2026101601935Access Panel · chafedWORN WING ACCESS PANELS, 584FT, 599CB, 584BB, 599BB, 584GB, 584JB.584EB, 584LB, 584AB,584ET, 699BB, 699AB, 684ET, 684HT, 684BB, 684EB, 684GB, 684JB, & 684LB. THE ACCESS PANELS WERE BLENDED OUT IAW SRM 51-12-00-001-001-A01, AND WERE EVALUATED WITHIN LIMITS IAWSep 22, 2026 · N296PQ · Cndair CL6002D24 · Wing, Plate/SkinSDR REXA2026101601901Frame · crackedCRACKED FRAME, INTERNAL FUSELAGE STRUCTURE BS 333 AND BTWN STR 2L TO 2R. FRAME AT INTERNAL FUSELAGE STRUCTURE OVER BS 333 AND BTWN STRINGERS 2L TO 2R WAS REPLACED IAW SRM 51-42-06-001-001-A01.Sep 22, 2026 · N296PQ · Cndair CL6002D24 · Fuselage Main, FrameSDR REXA2026101601945Drag Angle · crackedDURING (ET) HFEC INSPECTION ON DRAG ANGLE IAW NRC 252, A CRACK WAS FOUND ON THE AFT DRAG ANGLE BTW 55.62% STR DATUM TO 61.56% STGR DATUM (LT SIDE) AT VERTICAL STABILIZER TO FUSELAGE. THE AFT DRAG ANGLE WAS REPAIRED IAW SRM 55-31-00-201-001-A01.Sep 18, 2026 · N296PQ · Cndair CL6002D24 · Fuselage, Stabilizer Attach FittingsSDR REXA2026101601944Drag Angle · crackedCRACKED FWD DRAG ANGLE BTW 55.62% STR DATUM TO 61.56% STGR DATUM (LT SIDE) ON THE VERTICAL STABILIZER TO FUSELAGE. THE FWD DRAG ANGLE WAS REPAIRED IAW SRM 55-31-00-201-001-A01.Sep 18, 2026 · N296PQ · Cndair CL6002D24 · Fuselage, Stabilizer Attach FittingsSDR REXA2026101601943Drag Angle · crackedCRACKED AFT DRAG ANGLE BTWN 55.62% STR DATUM TO 61.56% STR DATUM ON THE VERTICAL STABILIZER TO FUSELAGE. THE AFT DRAG ANGLE WAS REPAIRED IAW SRM 55-31-00-201-001-A01.Sep 18, 2026 · N296PQ · Cndair CL6002D24 · Fuselage, Stabilizer Attach FittingsSDR REXA2026101601946Stringer Splice · corrodedAFTER REMOVAL STRINGER SPLICE, CORROSION WAS FOUND ON STRINGER 21R BTWN BS 469 - 485, REPAIRED THE STRINGER SPLICE IAW SRM 53-00-03-201-001-A02.Sep 15, 2026 · N296PQ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2026101601940Intercostal · corrodedCORRODED INTERCOSTAL, BTWN BS 310 - 319, STR 20R. THE INTERCOSTAL WAS REPLACED IAW SRM 53-00-00-101-001-A01, SRM 51-42-06-001-001-A01, AND SRM 51-42-21-001-001-A01.Sep 9, 2026 · N296PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026101601912Bracket · corrodedCORRODED BRACKETS (6EA) IN THE FWD CARGO BAY, PAINT ON BRACKETS (5EAS) WERE REMOVED & NO DAMAGE FOUND IAW SRM 51-26-01-001-001-A01, DUE TO EXCESSIVE DAMAGE ON BRACKET WAS REPLACED IAW SRM 51-10-06-001-001-A01, SRM 51-42-13-001-001-A01, AND SRM 51-42-21-001-00Sep 9, 2026 · N296PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026101601932Floorbeam · corrodedAFTER FLOORBEAM REMOVAL IAW NRC 200, THE LT FLOORBEAM AT FS280 WAS FOUND CORROSION. THE FLOORBEAM WAS REPLACED IAW SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, & SRM 51-42-22-001-001-A01.Aug 27, 2026 · N296PQ · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR REXA2026101601888Hinge · corrodedSECONDARY NRC FROM RC 900-27-900-910: AFTER LT AILERON BUSHINGS REMOVAL, WEAR ON L1, L2, L3, L4, L5, & L6 LUG BORE AT LH AILERON. LUG BORES L1, L2, L5 AND L6 AT LH AILERON WERE REPAIRED PER REO 670-57-61-237 REV - - & LUG BORES L3 AND L4 AT LH AILERON WERE REAug 27, 2026 · N296PQ · Cndair CL6002D24 · AileronsSDR REXA2026101601947Support · corrodedCORROSION ON LOWER SUPPORT BTWN BS 761.85 - 797 RT & LT SIDES AT INTERNAL OVERWING. LOWER SUPPORTS WERE REPAIRED IAW EA CRJ953-23259, REV IR, EA CRJ953-23260, REV IR, EA CRJ953-23261, REV IR , EA CRJ953-23262, REV IR, & EA CRJ953-23263, REV IR, EA CRJ953-2326Aug 24, 2026 · N296PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026101601938Support Plate · corrodedCORRODED CONNECTOR SUPPORT PLATES LT / RT (PX33, PX17, PX34, PX19) ON LT & RT MAIN WHEEL WELL SUPPORT PLATE RH (PX33, PX17, PX34, PX19) ON RT MAIN WHEEL WELL WAS REPLACED IAW SRM 51-42-21-001-001-A01. CORROSION ON SUPPORT PLATE LH (PX33, PX17, PX34, PX19) ON Aug 24, 2026 · N296PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026101601930Floorbeam · crackedCRACKED FLOORBEAMS (2 EA) BTWN LBL 12 - RBL 12, BS 280 & 265. THE FLOORBEAMS MANUFACTURED IAW DWG CC670-33199, REV B, & DLA 5039 & WERE REPLACED IAW SRM 51-42-21-001-001-A01, & SRM 51-42-06-001-001-A01.Aug 24, 2026 · N296PQ · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR REXA2026101601929Floorbeam · crackedCRACKED FLOORBEAMS (2 EA) BTWN LBL12 - RBL12, BS 280 & 265. THE FLOORBEAM REMOVED IAW DWG CC670-33199 REV -B & DLA 5039. THE FLOORBEAMS WERE REPLACED IAW SRM 51-42-21-001-001-A01, AND SRM 51-42-06-001-001-A01.Aug 24, 2026 · N296PQ · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR REXA2026101601928Stringer · corrodedCORRODED STRINGER 25R, BTWN BS280 & 295 IN THE E/E COMPARTMENT. THE STRINGER WAS REMOVED IAW SRM SRM 51-21-06-001-001-A01, EVALUATED OUT LIMITS IAW SRM 51-10-06-001-001-A01, AND WAS REPLACED IAW SRM 51-42-06-001-001-A01.Aug 24, 2026 · N296PQ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2026101601927Beam · corrodedCORROSION ON LONGITUDINAL BEAM LBL 9, BS 1000 - 1088 IN THE AFT BAGGAGE BAY. THE BEAM WAS REPAIRED IAW SRM 53-00-41-201-001-A03.Aug 24, 2026 · N296PQ · Cndair CL6002D24 · Fuselage Main, StructureSDR REXA2026101601926Fitting · crackedCRACKED LOWER SIDE POST FITTING OF THE LT & RT WINDSHIELD FRAME IN THE COCKPIT. THE SIDE POST FITTINGS WERE REPLACED IAW SRM 51-42-20-001-001-A01.Aug 24, 2026 · N296PQ · Cndair CL6002D24 · Fuselage Main, StructureSDR REXA2026101601925Fitting · crackedCRACKED LOWER SIDE POST FITTING OF THE LT & RT WINDSHIELD FRAME IN THE COCKPIT. THE SIDE POST FITTINGS WERE REPLACED IAW SRM 51-42-20-001-001-A01.Aug 24, 2026 · N296PQ · Cndair CL6002D24 · Fuselage Main, StructureSDR REXA2026101601924Support Angle · crackedCRACKED SUPPORT ANGLE ON EXTRENAL SERVICE PANEL. THE SUPPORT ANGLE WAS REPAIRED IAW EA CRJ953-23097, REV IR, & SRM 51-41-02-001-001-A01.Aug 24, 2026 · N296PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026101601923Web · crackedCRACKED WEB BTWN BS 195 - 205, WL79.5, LT SIDE IN THE FWD HYDRAULIC BAY. THE WEB WAS REPLACED IAW SRM 51-42-06-001-001-A01.Aug 24, 2026 · N296PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026101601922Floor Support · crackedCRACKED FLOOR SUPPORT RBL 12, BTW BS 221.73 - 229 IN THE COCKPIT. THE FLOOR SUPPORT WAS REPAIRED & REO 690-53-11-2249, REV --.Aug 24, 2026 · N296PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026101601921Angle · corrodedCORRODED ANGLE CAP OF LOWER SILL AREA IN THE PASSENGER DOOR CUTOUT. THE ANGLE CAP WAS REMOVED IAW SRM 51-21-06-001-001-A01, & WAS EVALUATED OUT LIMITS IAW SRM 51-10-06-001-001-A01, REPLACED IAW SRM 51-41-02-001-001-A01.Aug 24, 2026 · N296PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026101601920Angle · corrodedCORROSION ON LOWER SILL BTWN BS 761.85 - 797, RT & LT SIDES AT INTERNAL OVERWING LONGERON ASSEMBLIES. THE SILLS WERE REPAIRED IAW EA CRJ953-23259, REV IR, EA CRJ953-23260, REV IR, EA CRJ953-23261, REV IR, EA CRJ953-23262, REV IR, EA CRJ953-23263, REV IR, EA CAug 24, 2026 · N296PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026101601919Angle · corrodedCORROSION ON LOWER SILL BTWN BS 761.85 - 797, RT & LT SIDES AT INTERNAL OVERWING LONGERON ASSEMBLIES. THE SILLS WERE REPAIRED IAW EA CRJ953-23259, REV IR, EA CRJ953-23260, REV IR, EA CRJ953-23261, REV IR, EA CRJ953-23262, REV IR, EA CRJ953-23263, REV IR, EA CAug 24, 2026 · N296PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026101601918Angle · corrodedCORROSION ON LOWER SILL BTWN BS 761.85 - 797, RT & LT SIDES AT INTERNAL OVERWING LONGERON ASSEMBLIES. THE SILLS WERE REPAIRED IAW EA CRJ953-23259, REV IR, EA CRJ953-23260, REV IR, EA CRJ953-23261, REV IR, EA CRJ953-23262, REV IR, EA CRJ953-23263, REV IR, EA CAug 24, 2026 · N296PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026101601917Angle · corrodedCORROSION ON LOWER SILL BTWN BS 761.85 - 797, RT & LT SIDES AT INTERNAL OVERWING LONGERON ASSEMBLIES. THE SILLS WERE REPAIRED IAW EA CRJ953-23259, REV IR, EA CRJ953-23260, REV IR, EA CRJ953-23261, REV IR, EA CRJ953-23262, REV IR, EA CRJ953-23263, REV IR, EA CAug 24, 2026 · N296PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026101601916Angle · corrodedCORROSION ON LOWER SILL BTWN BS 761.85 - 797, RT & LT SIDES AT INTERNAL OVERWING LONGERON ASSEMBLIES. THE SILLS WERE REPAIRED IAW EA CRJ953-23259, REV IR, EA CRJ953-23260, REV IR, EA CRJ953-23261, REV IR, EA CRJ953-23262, REV IR, EA CRJ953-23263, REV IR, EA Aug 24, 2026 · N296PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026101601915Angle · corrodedCORROSION ON LOWER SILL BTWN BS 761.85 - 797 RT & LT SIDES AT INTERNAL OVERWING LONGERON ASSEMBLIES. THE SILL WERE REPAIRED IAW EA CRJ953-23259, REV IR, EA CRJ953-23260, REV IR, EA CRJ953-23261, REV IR, EA CRJ953-23262, REV IR, EA CRJ953-23263, REV IR, EA CRJAug 24, 2026 · N296PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026101601914Angle · corrodedCORROSION ON LOWER SILL BTWN BS 761.85 - 797 RT & LT SIDES. THE SILL WAS REPAIRED IAW EA CRJ953-23259, REV IR , EA CRJ953-23260, REV IR, EA CRJ953-23261, REV IR, EA CRJ953-23262, REV IR, EA CRJ953-23263, REV IR, EA CRJ953-23264, REV IR , EA CRJ953-23265, REVAug 24, 2026 · N296PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026101601913Splice · corrodedCORROSION ON SPLICE ABOVE STRINGER 22R, BS 333. THE SPLICE WAS REPAIRED IAW SRM 51-42-06-001-001-A01.Aug 23, 2026 · N296PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026101601910Access Panel · corrodedCORROSION ON THE ACCESS PANELS 642AZ, 642BZ, 542AZ, & 542BZ. THE ACCESS PANELS WERE REMOVED IAW SRM 51-21-06-001-001-A01, & WERE EVALUATED OUT LIMITS IAW SRM 53-00-00-101-001-A01, & REPLACED.Aug 23, 2026 · N296PQ · Cndair CL6002D24 · Wing, Plate/SkinSDR REXA2026101601909Access Panel · corrodedCORROSION ON THE ACCESS PANELS 642AZ, 642BZ, 542AZ, & 542BZ. THE ACCESS PANELS WERE REMOVED IAW SRM 51-21-06-001-001-A01, & WERE EVALUATED OUT LIMITS IAW SRM 53-00-00-101-001-A01, & REPLACED.Aug 23, 2026 · N296PQ · Cndair CL6002D24 · Wing, Plate/SkinSDR REXA2026101601908Access Panel · corrodedCORRODED ACCESS PANELS 642AZ, 642BZ, 542AZ, & 542BZ. THE ON ACCESS PANELS WERE REMOVED IAW SRM 51-21-06-001-001-A01 AND WERE EVALUATED OUT LIMITS IAW SRM 53-00-00-101-001-A01, & REPLACED.Aug 23, 2026 · N296PQ · Cndair CL6002D24 · Wing, Plate/SkinSDR REXA2026101601907Access Panel · corrodedCORROSION ON THE ACCESS PANELS 642AZ, 642BZ, 542AZ, & 542BZ. THE ACCESS PANELS WERE REMOVED IAW SRM 51-21-06-001-001-A01, AND WERE EVALUATED OUT LIMITS IAW SRM 53-00-00-101-001-A01 & REPLACED.Aug 23, 2026 · N296PQ · Cndair CL6002D24 · Wing, Plate/SkinSDR REXA2026101601906Seat Track · corrodedCORROSION ON THE RT SIDE SEAT TRACK BTWN BS 661 - 977. THE SEAT TRACK WAS REPLACED IAW AMM 53-00-49.Aug 22, 2026 · N296PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2026101601905Seat Track · corrodedCORROSION ON THE SEAT TRACK BTWN BS 661+74 - 693, LBL 9 IN THE PAX CABIN. THE SEAT TRACK WAS REPLACED IAW AMM 53-00-49.Aug 22, 2026 · N296PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2026101601904Seat Track · corrodedCORROSION ON SEAT TRACK BTWN BS 477 - 581, RBL 9 IN THE PAX CABIN. THE SEAT TRACK WAS REPLACED IAW AMM 53-00-49.Aug 22, 2026 · N296PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026101601903Seat Track · corrodedCORROSION ON SEAT TRACK BTWN BS 661+32 - 661+74, RBL 9 IN THE PAX CABIN. THE SEAT TRACK WAS REPLACED IAW AMM 53-00-49.Aug 22, 2026 · N296PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2026101601902Seat Track · corrodedCORROSION ON SEAT TRACK BTWN BS 349 - 409, RBL 9 IN THE PAX CABIN. THE SEAT TRACK WAS REPLACED IAW AMM 53-00-49.Aug 22, 2026 · N296PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2026101601900Stringer · corrodedCORROSION ON STRINGER 24R, BS 280 - 295 AT MAIN AVIONICS COMPARTMENT. THE STRINGER 24R, BS 280 - 295, WAS EVALUATED OUT LIMITS IAW SRM 53-21-03-101-002-A04. REPLACED IAW SRM 51-42-06-001-001-A01.Aug 22, 2026 · N296PQ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2026101601899Floorbeam · corrodedCORROSION ON FLOOR SUPPORT ANGLE AND ANGLES ON FS 280 BTW RBL12 TO LBL 12 AT PASSENGER FLOOR. CORROSION ON FLOOR SUPPORT ANGLE AND ANGLES ON BS 280 BTWN RBL12 TO LBL 12 AT PASSENGER FLOOR WAS REMOVED IAW SRM 51-21-06-001-001-A01 AND FLOOR SUPPORT BS 280 BTW Aug 22, 2026 · N296PQ · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR REXA2026101601896Support Fitting · corrodedCORROSION ON SUPPORT FITTING OF SENSOR PX36 AT GALLEY SERVICE DOOR. SUPPORT FITTING OF SENSOR PX36 AT GALLEY SERVICE DOOR WAS REPLACED IAW SRM 51-41-02-001-001-A01.Aug 20, 2026 · N296PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026101601895Seal Depressor · corrodedCORROSION ON LOWER DEPRESOR SEAL ON GALLEY SURROUND AREA AT PAX CABIN. CORROSION ON LOWER DEPRESOR SEAL ON GALLEY SURROUND AREA AT PAX CABIN WAS REMOVED IAW SRM 51-21-06-001-001-A01 AND WAS EVALUATED OUT LIMITS IAW SRM 51-10-06-001-001-A01 THEREFORE WAS REPLAAug 20, 2026 · N296PQ · Cndair CL6002D24 · Fuselage Main, Structure
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