# Service difficulty reports: N232PQ A list on [N232PQ](https://openairdocs.org/aircraft/N232PQ.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 4 · 181 reports - [SDR REXA2026052700711](https://openairdocs.org/sdr/REXA2026052700711.md): Angle · cracked · Aug 23, 2025 · N232PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > INITIAL INSPECTION:CRACK ON DIAPHRAGM BTW FS= 797 TO FS= 807 RBL 35 ON FWD AREA W/W AT MLG DIAPHRAGM BTW FS= 797 TO FS= 807 RBL 35 ON FWD AREA W/W AT MLG WAS REPLACED PER CRJ900 SRM 51-41-02-001-001-A01 - [SDR REXA2026052700724](https://openairdocs.org/sdr/REXA2026052700724.md): Fitting · corroded · Aug 14, 2025 · N232PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CORROSION ON SETTLEMENT FITTING OF ENTRANCE COMPARTMENT (1EA)AND GALLEY 1 (1EA) (FLOOR STRUCTURE AREA). DUE TO EXCESIVE CORROSION ON SETTLEMENT FITTING OF ENTRANCE COMPARTMENT (1EA) AND GALLEY 1 (1EA) (FLOOR STRUCTURE AREA) WERE REPLACED PER CRJ900 SRM 53-21- - [SDR REXA2026052700723](https://openairdocs.org/sdr/REXA2026052700723.md): Fitting · corroded · Aug 14, 2025 · N232PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CORROSION ON SETTLEMENT FITTING OF ENTRANCE COMPARTMENT (1EA)AND GALLEY 1 (1EA) (FLOOR STRUCTURE AREA). DUE TO EXCESIVE CORROSION ON SETTLEMENT FITTING OF ENTRANCE COMPARTMENT (1EA) AND GALLEY 1 (1EA) (FLOOR STRUCTURE AREA) WERE REPLACED PER CRJ900 SRM 53-21- - [SDR REXA2026052700712](https://openairdocs.org/sdr/REXA2026052700712.md): Hinge · broken · Aug 14, 2025 · N232PQ · Cndair CL6002D24 · Fuselage, Door Hinge > BROKEN HINGE ON UPPER STAIR PANEL OF THE PASSENGER DOOR HINGE ON ACCESS PANEL 832 ET WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 - [SDR REXA2026052700729](https://openairdocs.org/sdr/REXA2026052700729.md): Floorbeam · corroded · Aug 12, 2025 · N232PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam > AFTER FLOOR PANEL SUPPORT ANGLE, CORROSION AT RH CROSSBEAM FS 280.00 RH CROSSBEAM FS280.00 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-00-00-101-001-A01 AND WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 AND PER CRJ900 SRM 51-42-21-001-001-A01 - [SDR REXA2026052700728](https://openairdocs.org/sdr/REXA2026052700728.md): Floorbeam · corroded · Aug 12, 2025 · N232PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam > AFTER FLOOR PANEL SUPPORT ANGLE, CORROSION AT LH CROSSBEAM FS 280.00. CORROSION AT LH CROSSBEAM FS280.00 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-00-00-101-001-A01 AND WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 AND PER CRJ900 SRM 51-42-21-001-001-A0 - [SDR REXA2026052700725](https://openairdocs.org/sdr/REXA2026052700725.md): Floorbeam · corroded · Aug 12, 2025 · N232PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam > AFTER FLOOR PANEL SUPPORT ANGLE, CORROSION AT RH CROSSBEAM FS 280.00 FLOOR PANEL SUPPORT ANGLE (251ALF FLOOR PANEL AREA) WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-00-00-101-001-A01 AND WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 AND PER CRJ900 SRM 51- - [SDR REXA2026052700720](https://openairdocs.org/sdr/REXA2026052700720.md): Floorbeam · corroded · Aug 12, 2025 · N232PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam > AFTER FLOOR PANEL SUPPORT ANGLE, CORROSION AT LH CROSSBEAM FS 280.00. CORROSION AT LH CROSSBEAM FS280.00 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-00-00-101-001-A01 AND WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 AND PER CRJ900 SRM 51-42-21-001-001-A0 - [SDR REXA2026052700727](https://openairdocs.org/sdr/REXA2026052700727.md): Angle · corroded · Aug 6, 2025 · N232PQ · Cndair CL6002D24 · Passenger/Crew Doors > AFTER TO REMOVAL MID CAP ANGLE WAS FOUND CORROSION ON KICKPLATE ANGLE OF THE PASSENGER DOOR SURROUND KICKPLATE WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-23-101-001-A02 WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 - [SDR REXA2026052700726](https://openairdocs.org/sdr/REXA2026052700726.md): Support Fitting · corroded · Aug 5, 2025 · N232PQ · Cndair CL6002D24 · Passenger/Crew Doors > WEAR AT FWD/AFT HANDRAIL SUPPORT FITTING AT FWD AND AFT SIDE PANEL OF PASSENGER DOOR, ALSO MISSING BUMPERS FWD/AFT HANDRAIL SUPPORT FITTING AT FWD AND AFT SIDE PANEL OF PASSENGER DOOR WERE EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-00-00-101-001-A01 AND MUST B - [SDR REXA2026052700713](https://openairdocs.org/sdr/REXA2026052700713.md): Bushing · corroded · Aug 5, 2025 · N232PQ · Cndair CL6002D24 · Wing, Control Surface Attach Fittings > CORROSION ON BUSHING BORE LUG L1, L2. L5 AND L6 AT LH AILERON CENTER FITTING WERE FOUND BUSHING BORE LUGS L1, L2. L5 AND L6 AT LH AILERON CENTER FITTING WERE REPAIRED PER REO 670-57-61-237 REV. - - - [SDR REXA2026052700710](https://openairdocs.org/sdr/REXA2026052700710.md): Panel · cracked · Aug 5, 2025 · N232PQ · Cndair CL6002D24 · Passenger/Crew Doors > CRACK ON FWD SIDE PANEL OF THE PASSENGER DOOR FWD SIDE PANEL OF THE PASSENGER DOOR WAS REPAIRED PER CRJ-900 SRM 52-11-04-201-004-A01 AND EA CRJ952-19920 REV.A. - [SDR REXA2026052700722](https://openairdocs.org/sdr/REXA2026052700722.md): Beam · chafed · Aug 4, 2025 · N232PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > WEAR ON BEAM ON FWD AND AFT AREA ON AFT BAGGAGE BAY STRUCTURE BTW FS 1000.00 TO 10047.00. BEAM ON FWD AT AFT BAGGAGE BAY STRUCTURE BTW FS 1000.00 TO 1047.00 WAS REPAIRED PER EA CRJ953-19979 REV IR - [SDR REXA2026052700721](https://openairdocs.org/sdr/REXA2026052700721.md): Web · cracked · Aug 4, 2025 · N232PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CRACK ON WEB BELOW OF ADG RESTOW PUMP AT FWD EQUIPMENT COMPARTMENT WEB BELOW OF ADG RESTOW PUMP AT FWD EQUIPMENT COMPARTMENT WAS REPAIRED PER CRJ900 SRM 53-11-43-201-001-A01 AND EA CRJ953-20015 REV B - [SDR REXA2024103101249](https://openairdocs.org/sdr/REXA2024103101249.md): Support · corroded · Jul 16, 2024 · N232PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > FOUND CORROSION ON O/B MOST HOLE F.S. 801.25 L/H SILL DECK. REPAIRED O/B MOST HOLE AT F.S. 801.25 L/H SIDE SILL DECK IAW MHIRJ REO 690-53-41-488 REV-- 7/17/2024. - [SDR REXA2024080600623](https://openairdocs.org/sdr/REXA2024080600623.md): Cap · detached · Jul 16, 2024 · N232PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > BEAM SPLICE CAPS AT F.S. 847.00 FOR BOTH R.B.L. 9.00 AND L.B.L. 9.00 BEAMS HAVE A CONFIGURATION DEVIATION FROM SERVICE BULLETIN INSTALLATION CALL OUT. COMPLIED WITH MHIRJ REO 690-53-41-489 REV.--, DATED 2024-07-23. - [SDR REXA2022050300810](https://openairdocs.org/sdr/REXA2022050300810.md): None · corroded · Apr 26, 2022 · N232PQ · Cndair CL6002D24 · Passenger/Crew Doors > PAX DOOR FORMER ATTACHING CLIP CORRODED AT FS 329.41 BETWEEN DD5 AND DD6. CA: REMOVED AND REPLACED CLIPIAW CRJ 900 SRM 51-40-11-001-001-A01 & 51-42-06-001-001-A01. - [SDR REXA2022050300759](https://openairdocs.org/sdr/REXA2022050300759.md): Frame · corroded · Apr 26, 2022 · N232PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > FS 280 FRAME CORRODED ON UPPER FLANGE BETWEEN STR 25L AND 25R. REPAIRED IAW CRJ953-13274 REV IR DATED 4/7/2022. - [SDR REXA2022050300813](https://openairdocs.org/sdr/REXA2022050300813.md): Angle · corroded · Apr 24, 2022 · N232PQ · Cndair CL6002D24 · Passenger/Crew Doors > PAX DOOR AFT WEB HAS MULTIPLE SPOTS OF CORROSION. REMOVED PAX DOOR AFT WEB. REPLACED AFT WEB LOCATED AND DRILLED NEW WEB. REMOVED AND INSTALLED 9 STIFFNERS. REMOVED AND INSTALLED GAS TUBE MOUNT AND HANDRAIL STOP. REMOVAED AND REPLACED DRAG ANGLE STEP, SUPPORT - [SDR REXA2022050300806](https://openairdocs.org/sdr/REXA2022050300806.md): Former · corroded · Apr 24, 2022 · N232PQ · Cndair CL6002D24 · Passenger/Crew Doors > PAX DOOR FWD FORMER HAS MULTIPLE SPOTS OF CORROSION. CA: REMOVED AND REPLACED FWD MIDDLE, FWD UPPER, AND FWD LOWER SEAL RETAINERS. REMOVED AND INSTALLED FWD UPPER CORNER COVERS. REMOVED AND INSTALLED FWE UPPER DOOR CENTERING PLATE IAW CRJ-900 SRM 51-42-06-001- - [SDR REXA2022050300805](https://openairdocs.org/sdr/REXA2022050300805.md): Web · corroded · Apr 24, 2022 · N232PQ · Cndair CL6002D24 · Passenger/Crew Doors > PAX DOOR FWD WEB HAS MULTIPLE SPOTS OF CORROSION. CA: REMOVED PAX DOOR FWD WEB IAW CRJ-900 SRM 51-42-06-001-001-A01 AND 51-42-13-001-001-A01. RECEIVED NEW SERVICABLE WEB PN: 601R317071-R5. LAYOUT AND DRILLUP IAW SRM 51-40-11-001-001-A01. INSTALLED 9 STIFFNERS - [SDR REXA2022050300804](https://openairdocs.org/sdr/REXA2022050300804.md): Angle · corroded · Apr 24, 2022 · N232PQ · Cndair CL6002D24 · Passenger/Crew Doors > PAX DOOR AFT WEB HAS MULTIPLE SPOTS OF CORROSION. CA: REMOVED PAX DOOR AFT WEB. REPLACED AFT WEB LOCATED AND DRILLED NEW WEB. REMOVED AND INSTALLED 9 STIFFNERS. REMOVED AND INSTALLED GAS TUBE MOUNT AND HANDRAIL STOP. REMOVAED AND REPLACED DRAG ANGLE STEP, SUPP - [SDR REXA2022050300803](https://openairdocs.org/sdr/REXA2022050300803.md): Former · corroded · Apr 24, 2022 · N232PQ · Cndair CL6002D24 · Passenger/Crew Doors > PAX DOOR AFT FORMER HAS MULTIPLE SPOTS OF CORROSION. CA: REMOVED AND REPLACED FWD MIDDLE, FWD UPPER, AND FWD LOWER SEAL RETAINERS. REMOVED AND INSTALLED FWD UPPER CORNER COVERS. REMOVED AND INSTALLED FWE UPPER DOOR CENTERING PLATE IAW CRJ-900 SRM 51-42-06-001- - [SDR REXA2022050300802](https://openairdocs.org/sdr/REXA2022050300802.md): Skin · corroded · Apr 24, 2022 · N232PQ · Cndair CL6002D24 · Passenger/Crew Doors > PAX DOOR INNER SKIN CORRODED IN MULTIPLE PLACES CA: REMOVED ANGLE FROM PAX DOOR UPPER CENTER SKIN, REMOVED CORROSION, INSTALLED ANGLE IAW CRJ-900 SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01, 51-21-06-001-001-A01 REV. 38, (7/25/20). REMOVED INNER DOOR SKIN, - [SDR REXA2022050300801](https://openairdocs.org/sdr/REXA2022050300801.md): Spar · damaged · Apr 24, 2022 · N232PQ · Cndair CL6002D24 · Vertical Stabilizer > DURING REPLACEMENT OF RUDDER LOWER CENTER HINGE FOUND A HOLE THROUGH VERTICAL STAB STRUCTURE TO BE OVERSIZED. CA: REPAIRED VERTICAL STAB DAMAGE IAW MHIRJ REO 690-55-31-067 REV. A DATED 2022-04-16. - [SDR REXA2022050300772](https://openairdocs.org/sdr/REXA2022050300772.md): Frame · corroded · Apr 24, 2022 · N232PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > F.S. 265.00 FRAME IS CORRODED BETWEEN STGR 27 TO STGR 26R. CA: COMPLIED WITH ENDEAVOR EA CRJ953-12983, REV. B DATED 4/23/22. - [SDR REXA2022050300765](https://openairdocs.org/sdr/REXA2022050300765.md): Panel · corroded · Apr 24, 2022 · N232PQ · Cndair CL6002D24 · Passenger/Crew Doors > PASSENGER DOOR STEPS TOP PANEL IS CORRODED AROUND SCREW HOLES. CA: PAX DOOR TOP STEP PANEL BLENDED, FOUND TO BE OUT OF LIMITS, LOCATED DRILLED NEW PANEL PN: 601R317075-3 AND INSTALLED IAW CRJ900 SRM 51-42-06-001-001-A01, 51-42-13-01-001-A01 REV. 38 (7-25-21), - [SDR REXA2022050300771](https://openairdocs.org/sdr/REXA2022050300771.md): Frame · corroded · Apr 22, 2022 · N232PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > FS250 FRAME IS CORRODED BETWEEN STGR 26R TO STGR 26L. REPAIRED FS250 FRAME IAW ENDEAVOR AIR EA CRJ953-13199 REV-IR DATED 3/26/2022 - [SDR REXA2022050300800](https://openairdocs.org/sdr/REXA2022050300800.md): Angle · corroded · Apr 17, 2022 · N232PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CRAWLWAY FLOOR ANGLE SUPPORT AT FS 280 CORRODED. CA: REMOVED AND REPLACED SUPPORT ANGLE IAW CRJ 900 SRM 51-42-06-001-001-A01AND 51-40-11-001-001-A01. - [SDR REXA2022050300795](https://openairdocs.org/sdr/REXA2022050300795.md): Angle · corroded · Apr 17, 2022 · N232PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > LH AND RH FWD JACK PAD FITTING ANGLE CORRODED. CA: REMOVED AND REPLACED FITTING ANGLE IAW CRJ 900 SRM 51-40-11-001-001-A01 AND 51-42-21-00-001-001-A01. - [SDR REXA2022050300794](https://openairdocs.org/sdr/REXA2022050300794.md): Angle · corroded · Apr 17, 2022 · N232PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > FS265/STR27 STIFFENING ANGLE PN: CC670-34104-1 CORRODED. CA: REMOVED AND REPLACED ANGLE IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01 AND 51-40-11-001-001-A01. - [SDR REXA2022050300764](https://openairdocs.org/sdr/REXA2022050300764.md): Fitting · corroded · Apr 17, 2022 · N232PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > LH AND RH FWD JACK FITTING SUPPORTS ARE CORRODED. CC670-32179-3 & CC670-32179-4 CA: REMOVED AND REPLACED LH AND RH SUPPORTS IAW ENDEAVOR EA CRJ953-13164 AND CRJ953-13165, REV IR, DATED 3/25/2022. - [SDR REXA2022050300776](https://openairdocs.org/sdr/REXA2022050300776.md): Intercostal · corroded · Apr 14, 2022 · N232PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > 3EACH FWD INTERCOSTALS ARE CORRODED AT AVIONICS DOOR SURROUNDING STRUCTURE FS 349.00-364.00, STR26L-26R. CA: REMOVED AND REPLACED INTERCOSTALS IAW CRJ 900SRM 51-40-11-001-001-A01, 51-42-21-001-001-A01, 53-21-23-001-003-A01 AND 51-42-06-001-001-A01. (2EA) SH670 - [SDR REXA2022050300799](https://openairdocs.org/sdr/REXA2022050300799.md): Intercostal · cracked · Apr 12, 2022 · N232PQ · Cndair CL6002D24 · Passenger/Crew Doors > PAX DOOR INTERCOSTAL DD1 IS CRACKED. CA: REMOVED AND REPLACED INTERCOSTAL IAW CRJ 900SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01. - [SDR REXA2022050300796](https://openairdocs.org/sdr/REXA2022050300796.md): Lug · damaged · Apr 12, 2022 · N232PQ · Cndair CL6002D24 · Wing Structure > RH AILERON LUG MARKED "C" HAS DAMAGE TO BORE. CA: REPAIRED BORE AND REPLACED BUSHING IAW BOMBARDIER REO 670-57-61-237 REV -- DATED 2017-07-25. - [SDR REXA2022050300793](https://openairdocs.org/sdr/REXA2022050300793.md): Lug · damaged · Apr 12, 2022 · N232PQ · Cndair CL6002D24 · Wing Structure > LH AILERON LUG MARKED "F" HAS DAMAGE TO BORE. CA: REPAIRED BORE AND REPLACED BUSHING IAW BOMBARDIER REO 670-57-61-237 REV -- DATED 2017-07-25. - [SDR REXA2022050300812](https://openairdocs.org/sdr/REXA2022050300812.md): Yoke · chafed · Apr 10, 2022 · N232PQ · Cndair CL6002D24 · Engine Mount Section > RH FORWARD ENGINE MOUNT HAS CHAFFING. CA: REPAIRED IAW BOMBARDIER REO 670-71-21-057 REV-- DATED 2013-09-13 AND MHIRJ REO 690-71-21-039 REV A DATED 2022-04-01. - [SDR REXA2022050300811](https://openairdocs.org/sdr/REXA2022050300811.md): Yoke · chafed · Apr 10, 2022 · N232PQ · Cndair CL6002D24 · Engine Mount Section > LH FORWARD ENGINE MOUNT HAS CHAFING. CA: REPAIRED IAW BOMBARDIER REO 670-71-21-057 REV-- DATED 2013-09-13 AND MHIRJ REO 690-71-21-038 REV -- DATED 2022-03-27. - [SDR REXA2022050300808](https://openairdocs.org/sdr/REXA2022050300808.md): Cleat · corroded · Apr 8, 2022 · N232PQ · Cndair CL6002D24 · Passenger/Crew Doors > PAX DOOR INTERCOSTAL DD6 & CLEAT CORRODED. CA: REMOVED AND REPLACED INTERCOSTAL & CLEAT IAW CRJ 900 SRM 51-40-11-001-001-A01 & 51-42-06-001-001-A01. - [SDR REXA2022050300807](https://openairdocs.org/sdr/REXA2022050300807.md): Intercostal · corroded · Apr 8, 2022 · N232PQ · Cndair CL6002D24 · Passenger/Crew Doors > PAX DOOR INTERCOSTAL DD6 & CLEAT CORRODED. CA: REMOVED AND REPLACED INTERCOSTAL & CLEAT IAW CRJ 900 SRM 51-40-11-001-001-A01 & 51-42-06-001-001-A01. - [SDR REXA2022050300798](https://openairdocs.org/sdr/REXA2022050300798.md): Angle · corroded · Apr 5, 2022 · N232PQ · Cndair CL6002D24 · Passenger/Crew Doors > PAX DOOR OUTER HANDLE ASSY ANGLE CORRODED P/N 61R317052-1 CA: REMOVED & REPLACED ANGLE IAW CRJ 900 SRM 51-40-11-001-001-A01 & 51-42-21-001-001-A01 - [SDR REXA2022050300797](https://openairdocs.org/sdr/REXA2022050300797.md): Former · corroded · Apr 5, 2022 · N232PQ · Cndair CL6002D24 · Passenger/Crew Doors > PAX DOOR FORMER @ FS 329.41 CORRODED. CA: REMOVED & REPLACED FORMER IAW CRJ 900 SRM 51-40-11-001-001-A01 & 51-42-06-001-001-A01 - [SDR REXA2022050300792](https://openairdocs.org/sdr/REXA2022050300792.md): None · corroded · Apr 5, 2022 · N232PQ · Cndair CL6002D24 · Passenger/Crew Doors > PAX DOOR DD7 INTERCOSTAL CLIP IS CORRODED. CA: REMOVED, FABRICATED & REPLACED CLIP IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 & 51-24-16-001-001-A01. - [SDR REXA2022050300763](https://openairdocs.org/sdr/REXA2022050300763.md): Angle · cracked · Apr 5, 2022 · N232PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > RH FWD EQUIPMENT COMPARTMENT FLOOR SILL (DOOR LANDING) ABOVE AFT LATCH & ATTACH ANGLE ARE CRACKED. CA: REMOVED & REPLACED LANDING IAW CRJ 900 SRM 51-42-06-001-001-A01 & 51-42-10-001-001-A01. REMOVED, FABICATED & REPLACED ANGLE IAW CRJ 900 SRM 51-24-21-001-001- - [SDR REXA2022050300762](https://openairdocs.org/sdr/REXA2022050300762.md): None · cracked · Apr 5, 2022 · N232PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > RH FWD EQUIPMENT COMPARTMENT FLOOR SILL (DOOR LANDING) ABOVE AFT LATCH & ATTACH CLIP ARE CRACKED. CA: REMOVED & REPLACED LANDING IAW CRJ 900 SRM 51-42-06-001-001-A01 & 51-42-10-001-001-A01. REMOVED, FABICATED & REPLACED CLIP IAW CRJ 900 SRM 51-24-21-001-001-A0 - [SDR REXA2022050300761](https://openairdocs.org/sdr/REXA2022050300761.md): Angle · cracked · Apr 3, 2022 · N232PQ · Cndair CL6002D24 · Vertical Stabilizer > RH AFT VERTICAL STAB DRAG ANGLE IS CRACKED. CA: REMOVED & REPLACED DRAG ANGLE IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-22-001-001-A01, 51-42-21-001-001-A01, 51-22-00-001-001-A01 & 51-42-13-001-001-A01. - [SDR REXA2022050300760](https://openairdocs.org/sdr/REXA2022050300760.md): Angle · cracked · Apr 3, 2022 · N232PQ · Cndair CL6002D24 · Vertical Stabilizer > LH AFT VERTICAL STAB DRAG ANGLE IS CRACKED. CA: REMOVED & REPLACED DRAG ANGLE IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-22-001-001-A01, 51-42-21-001-001-A01, 51-22-00-001-001-A01 & 51-42-13-001-001-A01. - [SDR REXA2022050300777](https://openairdocs.org/sdr/REXA2022050300777.md): Plate · corroded · Apr 1, 2022 · N232PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > GALLEY 1 FORWARD INBOARD AND OUTBOARD MOUNTS CORRODED. CA: REMOVED AND REPLACED GALLEY 1 INBOARD AND OUTBOARD MOUNT PLATES IAW CRJ 900 SRM 51-40-11-001-001-A01 & 51-42-21-001-001-A04 - [SDR REXA2022050300782](https://openairdocs.org/sdr/REXA2022050300782.md): Seat Track · corroded · Mar 31, 2022 · N232PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > RH CABIN SIDE SEAT TRACK CORRODED FS847+31 CA: REMOVED AND REPLACED IAW CRJ 900 AMM 53-00-49-400-801-A11 - [SDR REXA2022050300779](https://openairdocs.org/sdr/REXA2022050300779.md): None · cracked · Mar 31, 2022 · N232PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > FS. 280 RBL 9 OB CLIP CRACKED CA: REPLACED RBL. 9 FS.280. CLIP IAW CRJ 900 SRM 51-40-11-001-001-A01. Next page: https://openairdocs.org/aircraft/N232PQ/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 = 'N232PQ' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N232PQ/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.