# Service difficulty reports: N296PQ

A list on [N296PQ](https://openairdocs.org/aircraft/N296PQ.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 3 · 115 reports

- [SDR REXA2026101601934](https://openairdocs.org/sdr/REXA2026101601934.md): Frame · corroded · Oct 3, 2026 · N296PQ · Cndair CL6002D24 · Fuselage Main, Frame
  > AFTER CORROSION REMOVAL ON FRAME BS 794 FOUND OUT OF LIMITS. REPLACED THE FRAME IAW SRM 51-42-21-001-001-A01.
- [SDR REXA2026101601942](https://openairdocs.org/sdr/REXA2026101601942.md): Shim · cracked · Sep 29, 2026 · N296PQ · Cndair CL6002D24 · Nacelle/Pylon Miscellaneous Structure
  > CRACKED SHIM ON THE SETTLEMENT AREA OF ACCESS PANEL 413AT. THE SHIM WAS REPAIRED IAW EA CRJ 954-23158, REV B.
- [SDR REXA2026101601941](https://openairdocs.org/sdr/REXA2026101601941.md): Doubler · cracked · Sep 29, 2026 · N296PQ · Cndair CL6002D24 · Cargo/Baggage Doors
  > CRACKED DOUBLER ON THE HANDLE OF AFT BAGGAGE DOOR. THE DOUBLER WAS REPLACED IAW SRM 51-42-21-001-001-A01.
- [SDR REXA2026101601939](https://openairdocs.org/sdr/REXA2026101601939.md): Rib · cracked · Sep 23, 2026 · N296PQ · Cndair CL6002D24 · Wing, Rib/Bulkhead
  > CRACKED 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.
- [SDR REXA2026101601933](https://openairdocs.org/sdr/REXA2026101601933.md): Stringer Splice · corroded · Sep 23, 2026 · N296PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > AFTER 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.
- [SDR REXA2026101601937](https://openairdocs.org/sdr/REXA2026101601937.md): Access Panel · chafed · Sep 22, 2026 · N296PQ · Cndair CL6002D24 · Wing, Plate/Skin
  > WORN 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,
- [SDR REXA2026101601936](https://openairdocs.org/sdr/REXA2026101601936.md): Access Panel · worn · Sep 22, 2026 · N296PQ · Cndair CL6002D24 · Wing, Plate/Skin
  > WORN 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 EVA
- [SDR REXA2026101601935](https://openairdocs.org/sdr/REXA2026101601935.md): Access Panel · chafed · Sep 22, 2026 · N296PQ · Cndair CL6002D24 · Wing, Plate/Skin
  > WORN 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 IAW
- [SDR REXA2026101601901](https://openairdocs.org/sdr/REXA2026101601901.md): Frame · cracked · Sep 22, 2026 · N296PQ · Cndair CL6002D24 · Fuselage Main, Frame
  > CRACKED 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.
- [SDR REXA2026101601945](https://openairdocs.org/sdr/REXA2026101601945.md): Drag Angle · cracked · Sep 18, 2026 · N296PQ · Cndair CL6002D24 · Fuselage, Stabilizer Attach Fittings
  > DURING (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.
- [SDR REXA2026101601944](https://openairdocs.org/sdr/REXA2026101601944.md): Drag Angle · cracked · Sep 18, 2026 · N296PQ · Cndair CL6002D24 · Fuselage, Stabilizer Attach Fittings
  > CRACKED 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.
- [SDR REXA2026101601943](https://openairdocs.org/sdr/REXA2026101601943.md): Drag Angle · cracked · Sep 18, 2026 · N296PQ · Cndair CL6002D24 · Fuselage, Stabilizer Attach Fittings
  > CRACKED 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.
- [SDR REXA2026101601946](https://openairdocs.org/sdr/REXA2026101601946.md): Stringer Splice · corroded · Sep 15, 2026 · N296PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > AFTER 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.
- [SDR REXA2026101601940](https://openairdocs.org/sdr/REXA2026101601940.md): Intercostal · corroded · Sep 9, 2026 · N296PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORRODED 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.
- [SDR REXA2026101601912](https://openairdocs.org/sdr/REXA2026101601912.md): Bracket · corroded · Sep 9, 2026 · N296PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORRODED 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 51-42-21-001-00
- [SDR REXA2026101601932](https://openairdocs.org/sdr/REXA2026101601932.md): Floorbeam · corroded · Aug 27, 2026 · N296PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > AFTER 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.
- [SDR REXA2026101601888](https://openairdocs.org/sdr/REXA2026101601888.md): Hinge · corroded · Aug 27, 2026 · N296PQ · Cndair CL6002D24 · Ailerons
  > SECONDARY 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 RE
- [SDR REXA2026101601947](https://openairdocs.org/sdr/REXA2026101601947.md): Support · corroded · Aug 24, 2026 · N296PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION 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 CRJ953-2326
- [SDR REXA2026101601938](https://openairdocs.org/sdr/REXA2026101601938.md): Support Plate · corroded · Aug 24, 2026 · N296PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORRODED 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
- [SDR REXA2026101601930](https://openairdocs.org/sdr/REXA2026101601930.md): Floorbeam · cracked · Aug 24, 2026 · N296PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > CRACKED 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.
- [SDR REXA2026101601929](https://openairdocs.org/sdr/REXA2026101601929.md): Floorbeam · cracked · Aug 24, 2026 · N296PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > CRACKED 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.
- [SDR REXA2026101601928](https://openairdocs.org/sdr/REXA2026101601928.md): Stringer · corroded · Aug 24, 2026 · N296PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > CORRODED 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.
- [SDR REXA2026101601927](https://openairdocs.org/sdr/REXA2026101601927.md): Beam · corroded · Aug 24, 2026 · N296PQ · Cndair CL6002D24 · Fuselage Main, Structure
  > CORROSION 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.
- [SDR REXA2026101601926](https://openairdocs.org/sdr/REXA2026101601926.md): Fitting · cracked · Aug 24, 2026 · N296PQ · Cndair CL6002D24 · Fuselage Main, Structure
  > CRACKED 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.
- [SDR REXA2026101601925](https://openairdocs.org/sdr/REXA2026101601925.md): Fitting · cracked · Aug 24, 2026 · N296PQ · Cndair CL6002D24 · Fuselage Main, Structure
  > CRACKED 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.
- [SDR REXA2026101601924](https://openairdocs.org/sdr/REXA2026101601924.md): Support Angle · cracked · Aug 24, 2026 · N296PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACKED SUPPORT ANGLE ON EXTRENAL SERVICE PANEL. THE SUPPORT ANGLE WAS REPAIRED IAW EA CRJ953-23097, REV IR, & SRM 51-41-02-001-001-A01.
- [SDR REXA2026101601923](https://openairdocs.org/sdr/REXA2026101601923.md): Web · cracked · Aug 24, 2026 · N296PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACKED 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.
- [SDR REXA2026101601922](https://openairdocs.org/sdr/REXA2026101601922.md): Floor Support · cracked · Aug 24, 2026 · N296PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACKED FLOOR SUPPORT RBL 12, BTW BS 221.73 - 229 IN THE COCKPIT. THE FLOOR SUPPORT WAS REPAIRED & REO 690-53-11-2249, REV --.
- [SDR REXA2026101601921](https://openairdocs.org/sdr/REXA2026101601921.md): Angle · corroded · Aug 24, 2026 · N296PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORRODED 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.
- [SDR REXA2026101601920](https://openairdocs.org/sdr/REXA2026101601920.md): Angle · corroded · Aug 24, 2026 · N296PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION 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 C
- [SDR REXA2026101601919](https://openairdocs.org/sdr/REXA2026101601919.md): Angle · corroded · Aug 24, 2026 · N296PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION 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 C
- [SDR REXA2026101601918](https://openairdocs.org/sdr/REXA2026101601918.md): Angle · corroded · Aug 24, 2026 · N296PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION 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 C
- [SDR REXA2026101601917](https://openairdocs.org/sdr/REXA2026101601917.md): Angle · corroded · Aug 24, 2026 · N296PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION 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 C
- [SDR REXA2026101601916](https://openairdocs.org/sdr/REXA2026101601916.md): Angle · corroded · Aug 24, 2026 · N296PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION 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
- [SDR REXA2026101601915](https://openairdocs.org/sdr/REXA2026101601915.md): Angle · corroded · Aug 24, 2026 · N296PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION 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 CRJ
- [SDR REXA2026101601914](https://openairdocs.org/sdr/REXA2026101601914.md): Angle · corroded · Aug 24, 2026 · N296PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION 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, REV
- [SDR REXA2026101601913](https://openairdocs.org/sdr/REXA2026101601913.md): Splice · corroded · Aug 23, 2026 · N296PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON SPLICE ABOVE STRINGER 22R, BS 333. THE SPLICE WAS REPAIRED IAW SRM 51-42-06-001-001-A01.
- [SDR REXA2026101601910](https://openairdocs.org/sdr/REXA2026101601910.md): Access Panel · corroded · Aug 23, 2026 · N296PQ · Cndair CL6002D24 · Wing, Plate/Skin
  > CORROSION 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.
- [SDR REXA2026101601909](https://openairdocs.org/sdr/REXA2026101601909.md): Access Panel · corroded · Aug 23, 2026 · N296PQ · Cndair CL6002D24 · Wing, Plate/Skin
  > CORROSION 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.
- [SDR REXA2026101601908](https://openairdocs.org/sdr/REXA2026101601908.md): Access Panel · corroded · Aug 23, 2026 · N296PQ · Cndair CL6002D24 · Wing, Plate/Skin
  > CORRODED 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.
- [SDR REXA2026101601907](https://openairdocs.org/sdr/REXA2026101601907.md): Access Panel · corroded · Aug 23, 2026 · N296PQ · Cndair CL6002D24 · Wing, Plate/Skin
  > CORROSION 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.
- [SDR REXA2026101601906](https://openairdocs.org/sdr/REXA2026101601906.md): Seat Track · corroded · Aug 22, 2026 · N296PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON THE RT SIDE SEAT TRACK BTWN BS 661 - 977. THE SEAT TRACK WAS REPLACED IAW AMM 53-00-49.
- [SDR REXA2026101601905](https://openairdocs.org/sdr/REXA2026101601905.md): Seat Track · corroded · Aug 22, 2026 · N296PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION 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.
- [SDR REXA2026101601904](https://openairdocs.org/sdr/REXA2026101601904.md): Seat Track · corroded · Aug 22, 2026 · N296PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON SEAT TRACK BTWN BS 477 - 581, RBL 9 IN THE PAX CABIN. THE SEAT TRACK WAS REPLACED IAW AMM 53-00-49.
- [SDR REXA2026101601903](https://openairdocs.org/sdr/REXA2026101601903.md): Seat Track · corroded · Aug 22, 2026 · N296PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION 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.
- [SDR REXA2026101601902](https://openairdocs.org/sdr/REXA2026101601902.md): Seat Track · corroded · Aug 22, 2026 · N296PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK BTWN BS 349 - 409, RBL 9 IN THE PAX CABIN. THE SEAT TRACK WAS REPLACED IAW AMM 53-00-49.
- [SDR REXA2026101601900](https://openairdocs.org/sdr/REXA2026101601900.md): Stringer · corroded · Aug 22, 2026 · N296PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > CORROSION 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.
- [SDR REXA2026101601899](https://openairdocs.org/sdr/REXA2026101601899.md): Floorbeam · corroded · Aug 22, 2026 · N296PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > CORROSION 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
- [SDR REXA2026101601896](https://openairdocs.org/sdr/REXA2026101601896.md): Support Fitting · corroded · Aug 20, 2026 · N296PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION 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.
- [SDR REXA2026101601895](https://openairdocs.org/sdr/REXA2026101601895.md): Seal Depressor · corroded · Aug 20, 2026 · N296PQ · Cndair CL6002D24 · Fuselage Main, Structure
  > CORROSION 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 REPLA

Next page: https://openairdocs.org/aircraft/N296PQ/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 = 'N296PQ' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N296PQ/reports

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