# Service difficulty reports: N297PQ A list on [N297PQ](https://openairdocs.org/aircraft/N297PQ.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 · 119 reports - [SDR REXA2026081701544](https://openairdocs.org/sdr/REXA2026081701544.md): Battery Pack · inoperative · Aug 9, 2026 · N297PQ · Cndair CL6002D24 · Emergency Lighting > FWD EXTERIOR EMERGENCY LIGHT DS52 INOPERATIVE. DEFERRING FWD EXTERIOR EMERGENCY LIGHT DS52 IAW MEL 33-51-2A PLACARD INSTALLED MM02. MX PROCEDURES COMPLIED WITH. LIGHT DS52 POPS BATTERY CHARGER FUSE AFTER A FEW SECONDS, NO SHORT FOUND ON LIGHT ASSY. SCHEMAT - [SDR REXA2026081701543](https://openairdocs.org/sdr/REXA2026081701543.md): Charger · inoperative · Aug 8, 2026 · N297PQ · Cndair CL6002D24 · Emergency Lighting > EMERGENCY CEILING LIGHTS LT#1 DS429 LT#2 DS431. FOUND FAULTY BATTERY CHARGER ASSEMBLY. R & R NR 2 BATTERY CHARGER PS36 IAW AMM 33-51-17. FWD EMERGENCY LIGHTS DS429 + DS431 FUNCTIONING PROPERLY. - [SDR REXA2026081001538](https://openairdocs.org/sdr/REXA2026081001538.md): Charger · inoperative · Aug 5, 2026 · N297PQ · Cndair CL6002D24 · Emergency Lighting > RIGHT FWD EMERGENCY LIGHT INOPERATIVE. R & R BATTERY CHARGER 2 IAW AMM 33-51-17. OPS TESTED GOOD. - [SDR REXA2026081001537](https://openairdocs.org/sdr/REXA2026081001537.md): Battery Pack · inoperative · Aug 3, 2026 · N297PQ · Cndair CL6002D24 · Emergency Lighting > FOUND FWD RT EXTERIOR EMERGENCY LIGHT INOPERATIVE. R & R LIGHT BULB. OPS TEST FAILED. SUSPECT INOPERATIVE HOUSING. NO FIX. DEFERRING RT FWD EMERGENCY LIGHT IAW MEL 33-51-2A. PLACARD INSTALLED. R & R EMERGENCY LIGHT IAW AMM 33-51-15. R & R BATTERY PACK 1 & - [SDR REXA2026080401480](https://openairdocs.org/sdr/REXA2026080401480.md): Charger · inoperative · Aug 1, 2026 · N297PQ · Cndair CL6002D24 · Emergency Lighting > CEILING EMERGENCY LIGHTS IN 1ST CLASS & EXTERIOR SERVICE DOOR EMERGENCY LIGHT ARE INOP. R/R BATTERY CHARGER 2 IAW CRJ900 AMM 33-51-17 OPC GOOD P/N 11-0049 S/N OFF 26590 ON 23019 - [SDR REXA2026080601503](https://openairdocs.org/sdr/REXA2026080601503.md): Door Frame · cracked · Mar 26, 2026 · N297PQ · Cndair CL6002D24 · Fuselage Main, Structure > CRACK ON DOOR POST WAS FOUND. DOOR POST WAS REPAIRED PER CRJ900 SRM 51-71-59-001-001-A01 - [SDR REXA2026080601500](https://openairdocs.org/sdr/REXA2026080601500.md): Panel · cracked · Mar 11, 2026 · N297PQ · Cndair CL6002D24 · Passenger/Crew Doors > CRACKS (4 LOCATIONS) ON AFT SIDE PANEL AT PASSENGER DOOR. AFT SIDE PANEL AT PASSENGER DOOR WAS REPAIRED PER CRJ-900 SRM 52-11-04-201-004-A01 - [SDR REXA2026080601520](https://openairdocs.org/sdr/REXA2026080601520.md): Handle · cracked · Mar 3, 2026 · N297PQ · Cndair CL6002D24 · Passenger/Crew Doors > CRACK ON EXTERNAL HANDLE FLAPPER AT PASSENGER DOOR. EXTERNAL HANDLE FLAPPER AT PASSENGER DOOR WAS REPLACED IAW SRM 51-42-06-001-001-A01, SRM 51-25-06-001-001-A01, SRM 51-25-16-001-001-A01 AND AMM 20-60-04-400-801-A01. - [SDR REXA2026080601512](https://openairdocs.org/sdr/REXA2026080601512.md): Fitting · corroded · Feb 26, 2026 · N297PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CORROSION ON FITTING (2EA) ON CORNER ACCESS 205 AND UNDER THE FLASHLIGHT AT GALLEY 2. FITTING (2EA) ON CORNER ACCESS 205 AND UNDER THE FLASHLIGHT AT GALLEY 2 WERE REPLACED PER SAFRAN CMM 25-32-84 - [SDR REXA2026080601510](https://openairdocs.org/sdr/REXA2026080601510.md): Support Fitting · damaged · Feb 26, 2026 · N297PQ · Cndair CL6002D24 · Aerodynamic Fairings > ELONGATED HOLE ON FWD LEFT SUPPORT FITTING AT FAIRING 193AB FWD LEFT SUPPORT FITTING AT FAIRING 193AB WAS REPLACED PER CRJ-900 SRM 51-41-02-001-001-A01. - [SDR REXA2026080601506](https://openairdocs.org/sdr/REXA2026080601506.md): Fitting · corroded · Feb 26, 2026 · N297PQ · Cndair CL6002D24 · Fuselage, Equipment Attach Fittings > CORROSION AFT RH FLOOR FITTING ON ACCESS 306 (1EA) ON GALLEY 3. AFT RH FLOOR FITTING ON ACCESS 306 (1EA) (PN: CDSP2019-7C-650) ON GALLEY 3 WAS REPLACED PER ZODIAC AEROSPACE CMM 25-33-18 - [SDR REXA2026080601505](https://openairdocs.org/sdr/REXA2026080601505.md): Fitting · corroded · Feb 26, 2026 · N297PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CORROSION ON FITTING (2EA) ON CORNER ACCESS 205 AND UNDER THE FLASHLIGHT AT GALLEY 2 SUMMARY OF NRC 00502: FITTING (2EA) ON CORNER ACCESS 205 AND UNDER THE FLASHLIGHT AT GALLEY 2 WERE REPLACED PER SAFRAN CMM 25-32-84 - [SDR REXA2026080601501](https://openairdocs.org/sdr/REXA2026080601501.md): Skin · cracked · Feb 26, 2026 · N297PQ · Cndair CL6002D24 · Fuselage Main, Plate/Skin > SECONDARY NRC FROM NRC 00115: AFTER STIFFENETR REMOVAL, CRACK WAS FOUND ON SKIN OF ACCESS PANEL 171CL. SKIN OF ACCESS PANEL 171CL WAS REPAIRED PER REO 670-53-82-430 REV:-- - [SDR REXA2026042800407](https://openairdocs.org/sdr/REXA2026042800407.md): Angle · cracked · Feb 26, 2026 · N297PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CRACK ON REINFORCEMENT ANGLE LOCATED BTW FRAME FS310 AND 25R TO 26R WAS FOUND CRACK ON REINFORCEMENT ANGLE LOCATED BTW FRAME FS310 AND 25R TO 26R WAS REPAIRED PER CRJ900 SRM 53-00-06-201-001-A03 - [SDR REXA2026042800405](https://openairdocs.org/sdr/REXA2026042800405.md): Stringer Splice · corroded · Feb 26, 2026 · N297PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer > CORROSION ON STRINGER SPLICE 25RH IN FS= 327 TO FS= 337 AT MAIN AVIONICS COMPARTMENT. CORROSION ON STRINGER SPLICE 25RH IN FS= 327 TO FS= 337 AT MAIN AVIONICS COMPARTMENT WAS EVALUATED OUT OF LIMITS AND STRINGER SPLICE WAS REPLACED PER CRJ900 SRM 51-42-21-001- - [SDR REXA2026042800392](https://openairdocs.org/sdr/REXA2026042800392.md): Drag Angle · cracked · Feb 26, 2026 · N297PQ · Cndair CL6002D24 · Fuselage, Stabilizer Attach Fittings > CRACKED FWD AND AFT DRAG ANGLE AT RIGHT STABILIZER TO FUSELAGE ATTACHMENT BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). CRACKED FWD AND AFT DRAG ANGLE AT RIGHT STABILIZER TO FUSELAGE ATTACHMENT BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DAT - [SDR REXA2026080601523](https://openairdocs.org/sdr/REXA2026080601523.md): Skin · corroded · Feb 25, 2026 · N297PQ · Cndair CL6002D24 · Fuselage Main, Plate/Skin > AFTER REMOVAL INTERNAL PRODUCTION DOUBLER, CORROSION ON FUSELAGE INNER SKIN, BETWEEN FS= 295 TO FS= 310 AND STGR 26LH TO 26RH AT MAIN AVIONICS COMPARTMENT WAS FOUND CORROSION ON FUSELAGE INNER SKIN, BETWEEN FS= 295 TO FS= 310 AND STGR 26LH TO 26RH AT MAIN AVIO - [SDR REXA2026042800412](https://openairdocs.org/sdr/REXA2026042800412.md): Stringer · corroded · Feb 25, 2026 · N297PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CORROSION ON STRG 23RH BTW FS349 TO FS364 AT MAIN AVIONICS COMPARTMENT CORROSION ON STRG 23RH BTW FS349 TO FS364 AT MAIN AVIONICS COMPARTMENT WAS EVALAUTED OUT OF LIMITS, THEREFORE WAS REPLACED PER CRJ 900 SRM 53-00-00-101-001-A01, SRM 51-42-06-001-001-A01 - [SDR REXA2026042800411](https://openairdocs.org/sdr/REXA2026042800411.md): Stringer · corroded · Feb 25, 2026 · N297PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CORROSION ON STRG 21RH BTW FS364 TO FS379 AT MAIN AVIONICS COMPARTMENT CORROSION ON STRG 21RH BTW FS364 TO FS379 AT MAIN AVIONICS COMPARTMENT WAS EVALUATED OUT OF LIMITS, THEREFORE WAS REPLACED PER CRJ-900 SRM 53-00-00-101-001-A01 AND SRM 51-42-06-001-001-A0 - [SDR REXA2026042800409](https://openairdocs.org/sdr/REXA2026042800409.md): Stringer · corroded · Feb 25, 2026 · N297PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CORROSION ON STRG 25RH BTW FS 295 TO FS 326 AT MAIN AVIONICS COMPARTMENTT. STRG 25RH BTW FS 280 TO FS 326 AT MAIN AVIONICS COMPARTMENT WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01. - [SDR REXA2026042800408](https://openairdocs.org/sdr/REXA2026042800408.md): Channel · corroded · Feb 25, 2026 · N297PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CORROSION ON INTERNAL PRODUCTION DOUBLER OF ANTENNA IN FS= 295 TO FS= 310 BETWEEN STGR 26LH TO 26RH AT MAIN AVIONICS COMPARTMENT. PRODUCTION DOUBLER LOCATED ON FS= 295 TO FS= 310 BETWEEN STGR 26LH TO 26RH AT MAIN AVIONICS COMPARTMENT WAS EVALUATED OUT OF LIMI - [SDR REXA2026042800406](https://openairdocs.org/sdr/REXA2026042800406.md): Channel · corroded · Feb 25, 2026 · N297PQ · Cndair CL6002D24 · Wing Miscellaneous Structure > CORROSION ON SEVERAL CHANNEL NUT BTW WS 148.01 TO WS 48.00 LEFT WING FRONT SPART FORWARD, LOWER SECTION. DUE TO EXCESSIVE CORROSION ON SEVERAL CHANNEL NUT BTW WS 148.01 TO WS 48.00 LEFT WING FRONT SPART FORWARD, LOWER SECTION WERE REPLACED PER CRJ900 SRM 51-10 - [SDR REXA2026042800404](https://openairdocs.org/sdr/REXA2026042800404.md): Floorbeam · cracked · Feb 25, 2026 · N297PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam > CRACK ON ANGLE FS 280 RBL 25 AT E/E COMPARTMENT. ANGLE ON FS 280 RBL 25 AT E/E COMPARTMENT WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 AND SRM 51-42-10-001-001-A01. - [SDR REXA2026042800403](https://openairdocs.org/sdr/REXA2026042800403.md): Support Angle · cracked · Feb 25, 2026 · N297PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CRACK ON ANGLE SUPPORTS (2EAS) BTW FS=1000, STGR 8LH AND FS= 1051.30, STGR 7LH ANGLE SUPPORTS (2EAS) BTW FS=1000, STGR 8LH AND FS= 1051.30, STGR 7LH WERE FABRICATED AND REPLACED PER EA CRJ953-21721 REV IR, EA CRJ953-21787 REV IR, CRJ 900 SRM 51-42-06-001-00 - [SDR REXA2026042800402](https://openairdocs.org/sdr/REXA2026042800402.md): Angle · cracked · Feb 25, 2026 · N297PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CRACK ON ANGLE SUPPORTS (2EAS) BTW FS=1000, STGR 8LH AND FS= 1051.30, STGR 7LH ANGLE SUPPORTS (2EAS) BTW FS=1000, STGR 8LH AND FS= 1051.30, STGR 7LH WERE FABRICATED AND REPLACED PER EA CRJ953-21721 REV IR, EA CRJ953-21787 REV IR, CRJ 900 SRM 51-42-06-001-00 - [SDR REXA2026042800385](https://openairdocs.org/sdr/REXA2026042800385.md): Channel · corroded · Feb 25, 2026 · N297PQ · Cndair CL6002D24 · Wing Miscellaneous Structure > CORROSION ON SEVERAL CHANNEL NUT BTW WS 178.00 TO WS 88.00 RIGHT WING FRONT SPART FORWARD, LOWER SECTION. DUE TO EXCESSIVE CORROSION ON SEVERAL CHANNEL NUTS BTW WS 178.00 TO WS 88.00 RIGHT WING FRONT SPART FORWARD, LOWER SECTION WERE REPLACED PER CRJ 900 SRM - [SDR REXA2026042800384](https://openairdocs.org/sdr/REXA2026042800384.md): Stringer · corroded · Feb 25, 2026 · N297PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CORROSION ON STRINGER 27 IN FS= 349 TO FS= 364 AT MAIN AVIONICS COMPARTMENT DUE TO EXCESSIVE CORROSION ON STRINGER 27 IN FS= 349 TO FS= 364 AT MAIN AVIONICS COMPARTMENT WAS REPLACED PER CRJ/900 SRM 51-10-06-001-001-A01, SRM 51-42-06-001-001-A01 AND SRM 51-42-2 - [SDR REXA2026042800376](https://openairdocs.org/sdr/REXA2026042800376.md): Stringer · corroded · Feb 25, 2026 · N297PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer > CORROSION ON STRG 20RH BTW FS364 TO FS379 AT MAIN AVIONICS COMPARTMENT STRG 20RH BTW FS364 TO FS379 AT MAIN AVIONICS COMPARTMENT WAS REPAIRED PER EA CRJ953-20530 REV. IR - [SDR REXA2026042800375](https://openairdocs.org/sdr/REXA2026042800375.md): Stringer · corroded · Feb 25, 2026 · N297PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer > CORROSION ON STRG 24RH BTW FS280 TO FS295 AT MAIN AVIONICS COMPARTMENT. STRG 24RH BTW FS280 TO FS333 AT MAIN AVIONICS COMPARTMENT WAS REPLACED PER CRJ/900 SRM 51-42-06-001-001-A01 & CRJ/900 SRM 51-42-21-001-001-A01 - [SDR REXA2026042800374](https://openairdocs.org/sdr/REXA2026042800374.md): Angle · cracked · Feb 25, 2026 · N297PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CRACK ON PREVIOUS ANGLE REPAIR FS 280 RBL 12 AT E/E COMPARTMENT. ANGLE REPAIR FS 280 RBL 12 AT E/E COMPARTMENT WAS REPAIRED PER REO 690-53-11-1141 REV -- - [SDR REXA2026042800383](https://openairdocs.org/sdr/REXA2026042800383.md): Bracket · corroded · Feb 24, 2026 · N297PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CORROSION ON MACHINED FITTINGS BTW FS519.64 TO FS631.34, & STGR 24RH AND &22 LH (10EAS) AT INTERNAL STRUCTURE OF FWD BAGGAGE BAY. DUE TO EXCESSIVE CORROSION ON MACHINED FITTINGS BTW FS FS519.64 TO FS631.34, & STGR 24RH AND &22 LH (9EAS) AT INTERNAL STRUCTURE O - [SDR REXA2026080601522](https://openairdocs.org/sdr/REXA2026080601522.md): Strap · corroded · Feb 23, 2026 · N297PQ · Cndair CL6002D24 · Aerodynamic Fairings > CORROSION AT SUPPORT STRUCTURE STRAP BTW FAIRING ACCESS PANEL 193AL & 193AR TO FAIRING ACCESS PANEL 193AB STRAP P/N: CC670-39052-4S AND STRAP P/N: CC670-39052-3S ON FAIRING ACCESS PANEL 193AB WAS REPLACED PER CRJ-900 SRM 51-42-13-001-001-A01 AND CRJ-900 SRM 51 - [SDR REXA2026080601521](https://openairdocs.org/sdr/REXA2026080601521.md): Strap · corroded · Feb 23, 2026 · N297PQ · Cndair CL6002D24 · Aerodynamic Fairings > CORROSION AT SUPPORT STRUCTURE STRAP BTW FAIRING ACCESS PANEL 193AL & 193AR TO FAIRING ACCESS PANEL 193AB STRAP P/N: CC670-39052-4S AND STRAP P/N: CC670-39052-3S ON FAIRING ACCESS PANEL 193AB WAS REPLACED PER CRJ-900 SRM 51-42-13-001-001-A01 AND CRJ-900 SRM 51 - [SDR REXA2026042800401](https://openairdocs.org/sdr/REXA2026042800401.md): Angle · cracked · Feb 23, 2026 · N297PQ · Cndair CL6002D24 · Wing Miscellaneous Structure > CRACK ON ATTACHMENT ANGLE OF ACCESS PANEL 542AZ AT MLG SHOCK STRUT BAY ANGLE ON ACCESS PANEL 542AZ AT MLG SHOCK STRUT BAY WAS REPLACED PER CRJ900 SRM 51-42-21-001-001-A01 - [SDR REXA2026042800400](https://openairdocs.org/sdr/REXA2026042800400.md): Floor Support · cracked · Feb 23, 2026 · N297PQ · 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). FLOOR BEAM RBL 12.0 BTW FS 221.73 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE (FLIGHT COMPARTMENT FLOOR STRUCTURE - [SDR REXA2026042800386](https://openairdocs.org/sdr/REXA2026042800386.md): Rib · cracked · Feb 23, 2026 · N297PQ · Cndair CL6002D24 · Wing, Rib/Bulkhead > CRACK ON MACHINED RIB OF LEADING EDGE SS58.41 AT RIGHT WING. CRACK ON MACHINED RIB OF LEADING EDGE SS58.41 AT RIGHT WING WAS REPAIRED PER 690-57-41-240 REV - - - [SDR REXA2026042800373](https://openairdocs.org/sdr/REXA2026042800373.md): Rib · corroded · Feb 23, 2026 · N297PQ · Cndair CL6002D24 · Wing, Rib/Bulkhead > CRACK ON MACHINED RIB OF LEADING EDGE SS58.41 AT LEFT WING. MACHINED RIB OF LEADING EDGE SS58.41 AT LEFT WING WAS REPAIRED PER REO 690-57-41-240 REV. - -. - [SDR REXA2026042800365](https://openairdocs.org/sdr/REXA2026042800365.md): Rib · corroded · Feb 23, 2026 · N297PQ · Cndair CL6002D24 · Wing, Rib/Bulkhead > CRACK ON MACHINED RIB OF LEADING EDGE SS58.41 AT LEFT WING. MACHINED RIB OF LEADING EDGE SS58.41 AT LEFT WING WAS REPAIRED PER REO 690-57-41-240 REV. - -. - [SDR REXA2026042800413](https://openairdocs.org/sdr/REXA2026042800413.md): Seat Track · corroded · Feb 22, 2026 · N297PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings > CORROSION ON LH SIDE SEAT RAIL, (3 SECTIONS) FROM FS785 TO FS900 AND (1 SECTION) FROM FS915 TO FS977 CORROSION ON LH SIDE SEAT RAIL, (3 SECTIONS) FROM FS785 TO FS900 AND (1 SECTION) FROM FS915 TO FS977 WERE EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-41-49-101 - [SDR REXA2026042800410](https://openairdocs.org/sdr/REXA2026042800410.md): Frame · corroded · Feb 22, 2026 · N297PQ · Cndair CL6002D24 · Fuselage Main, Frame > CORROSION ON FRAME FS349 BTW STRG 26LH TO 26RH AT MAIN AVIONICS COMPARTMENT. CORROSION ON FRAME FS349 BTW STRG 26LH TO 26RH AT MAIN AVIONICS COMPARTMENT WAS EVALUATED OUT OF LIMITS AND FRAME FS349 WAS REPLACED PER CRJ900 SRM 51-10-06-001-001-A01,CRJ900 SRM 51 - [SDR REXA2026042800399](https://openairdocs.org/sdr/REXA2026042800399.md): Seat Track · corroded · Feb 22, 2026 · N297PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings > CORROSION ON LH SEAT RAILS LBL26 (1 SECTION) FROM FS 927 TO FS977 AT PAX CABIN CORROSION ON LH SEAT RAIL LBL26 (1 SECTION) FROM FS 927 TO FS977 AT PAX CABIN WAS REMOVED AND EVALUATED OUT OF LIMITS PER CRJ900 SRM 51-21-06-001-001-A01 AND SRM 53-51-49-101-001-A - [SDR REXA2026042800398](https://openairdocs.org/sdr/REXA2026042800398.md): Post · corroded · Feb 22, 2026 · N297PQ · Cndair CL6002D24 · Fuselage Main, Structure > CORROSION ON FLOOR POST, LOWER SECTION LOCATED BTW FS 280 AND STGR 25RH. FLOOR POST, LOWER SECTION LOCATED BTW FS 280 AND STGR 25RH WAS REPLACED PER CRJ900 SRM 51-42-21-001-001-A01, SRM 51-42-06-001-001-A01. - [SDR REXA2026042800397](https://openairdocs.org/sdr/REXA2026042800397.md): Post · corroded · Feb 22, 2026 · N297PQ · Cndair CL6002D24 · Fuselage Main, Structure > CORROSION ON FLOOR POST, LOWER SECTION LOCATED BTW FS 280 AND STGR 25LH. FLOOR POST, LOWER SECTION LOCATED BTW FS 280 AND STGR 25LH WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, SRM 51-42-13-001-001-A01 SRM 51-42-10-001-001-A01 - [SDR REXA2026042800395](https://openairdocs.org/sdr/REXA2026042800395.md): Support Plate · corroded · Feb 22, 2026 · N297PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CORROSION ON RH/LH MLG HYDRAULIC LINES SUPPORTS PLATE (4EA) (IN BK, LG EXT, LG RET) ON WHEEL WELL AREA. RH/LH MLG HYDRAULIC LINES SUPPORTS PLATE (4EA) (IN BK, LG EXT, LG RET) ON WHEEL WELL AREA WERE EVALUATED OUT OF LIMITS AND WERE REPLACED PER CRJ900 SRM 51- - [SDR REXA2026042800394](https://openairdocs.org/sdr/REXA2026042800394.md): Support Plate · corroded · Feb 22, 2026 · N297PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CORROSION ON RH/LH MLG HYDRAULIC LINES SUPPORTS PLATE (4EA) (IN BK, LG EXT, LG RET) ON WHEEL WELL AREA. RH/LH MLG HYDRAULIC LINES SUPPORTS PLATE (4EA) (IN BK, LG EXT, LG RET) ON WHEEL WELL AREA WERE EVALUATED OUT OF LIMITS AND WERE REPLACED PER CRJ900 SRM 51- - [SDR REXA2026042800391](https://openairdocs.org/sdr/REXA2026042800391.md): Seat Track · corroded · Feb 22, 2026 · N297PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings > CORROSION ON RH SEAT RAIL RBL9 (1 SECTION) 847+16 TO FS977 AT PAX CABIN. CORROSION ON RH SEAT RAIL RBL9 (1 SECTION) 847+16 TO FS977 AT PAX CABIN WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01 EVALUATED OUT LIMITS PER CRJ-900 SRM 53-51-49-101-001-A02 THEREFORE - [SDR REXA2026042800389](https://openairdocs.org/sdr/REXA2026042800389.md): Seat Track · corroded · Feb 22, 2026 · N297PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings > CORROSION ON RH SIDE SEAT RAILS, (1 SECTION) FROM FS379 TO FS483 AND (1 SECTION) FROM FS661+16 TO FS661+90 AT PAX CABIN CORROSION ON RH SIDE SEAT RAILS, (1 SECTION) FROM FS379 TO FS483 AND (1 SECTION) FROM FS661+16 TO FS661+90 AT PAX CABIN WAS REMOVED PER CRJ9 - [SDR REXA2026042800387](https://openairdocs.org/sdr/REXA2026042800387.md): Seat Track · corroded · Feb 22, 2026 · N297PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings > CORROSION ON LH SIDE SEAT RAILS, (2 SECTIONS) FROM FS379 TO FS 573 AND (4 SECTIONS) FROM FS573 TO FS669 AT PAX CABIN. CORROSION ON LH SIDE SEAT RAILS, (2 SECTIONS) FROM FS379 TO FS 573 AND (4 SECTIONS) FROM FS573 TO FS669 AT PAX CABIN WAS REMOVED PER CRJ900 SR - [SDR REXA2026042800382](https://openairdocs.org/sdr/REXA2026042800382.md): Seat Track · corroded · Feb 22, 2026 · N297PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings > CORROSION ON LH SEAT RAILS LBL9, (1 SECTION) FROM FS847+16 TO FS988 AND (1 SECTION) FROM FS988 TO FS1000 AT PAX CABIN. CORROSION ON LH SEAT RAILS LBL9, (1 SECTION) FROM FS847+16 TO FS988 AND (1 SECTION) FROM FS988 TO FS1000 AT PAX CABIN WAS REMOVED CRJ900 SRM - [SDR REXA2026042800381](https://openairdocs.org/sdr/REXA2026042800381.md): Seat Track · corroded · Feb 22, 2026 · N297PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings > CORROSION ON RH SEAT RAILS RBL9, (1 SECTION) FROM FS581 TO FS661+32, (1 SECTION) FROM FS661+32 TO FS677 AND (1 SECTION) FROM FS677 TO FS847+16 AT PAX CABIN. CORROSION ON RH SEAT RAILS RBL9, (1 SECTION) FROM FS581 TO FS661+32, (1 SECTION) FROM FS661+32 TO FS677 Next page: https://openairdocs.org/aircraft/N297PQ/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 = 'N297PQ' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N297PQ/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.