# Service difficulty reports: N146PQ A list on [N146PQ](https://openairdocs.org/aircraft/N146PQ.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 · 191 reports - [SDR REXA2026080401435](https://openairdocs.org/sdr/REXA2026080401435.md): Landing · cracked · Jun 10, 2026 · N146PQ · Cndair CL6002D24 · Wing Structure > SECONDARY NRC FROM TC 900-57-580-503: AFTER REMOVING THE 584FB ACCESS PANEL, ELONGATED HOLE WAS FOUND IN THE SETTLEMENT AREA. SETTLEMENT AREA OF 584FB ACCESS PANEL WAS REPAIRED PER REO 690-57-52-595 REV: - - - [SDR REXA2026080401439](https://openairdocs.org/sdr/REXA2026080401439.md): Handle · cracked · Jun 7, 2026 · N146PQ · Cndair CL6002D24 · Passenger/Crew Doors > CRACK OUTER HANDLE OF PASSENGER DOOR. OUTER HANDLE OF PASSENGER DOOR WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 - [SDR REXA2026080401471](https://openairdocs.org/sdr/REXA2026080401471.md): Fitting · cracked · Jun 4, 2026 · N146PQ · Cndair CL6002D24 · Fuselage Main, Structure > CRACK ON AFT LOWER FITTING SIDE POST LH/RH SIDE BTW WINDSHIELD AND SIDE WINDOWS. AFT LOWER FITTING SIDE POST LH/RH SIDE BTW WINDSHIELD AND SIDE WINDOWS WERE REPLACED PER CRJ900 SRM 51-42-21-001-001-A01 - [SDR REXA2026080401470](https://openairdocs.org/sdr/REXA2026080401470.md): Fitting · cracked · Jun 4, 2026 · N146PQ · Cndair CL6002D24 · Fuselage Main, Structure > CRACK ON AFT LOWER FITTING SIDE POST LT/RT SIDE BTW WINDSHIELD AND SIDE WINDOWS. AFT LOWER FITTING SIDE POST LH/RH SIDE BTW WINDSHIELD AND SIDE WINDOWS WERE REPLACED PER CRJ900 SRM 51-42-21-001-001-A01 - [SDR REXA2026080401443](https://openairdocs.org/sdr/REXA2026080401443.md): Door Frame · corroded · Jun 3, 2026 · N146PQ · Cndair CL6002D24 · Fuselage Main, Structure > SECONDARY NRC FROM NRC 290: CORROSION ON INNER CHORD (3EAS) BTW FS1000 TO FS1047 AT AFT BAGGAGE DOOR SURROUND STRUCTURE LOWER SIDE. CORROSION ON INNER CHORD (2EAS) BTW FS1000 TO FS1047 AT AFT BAGGAGE DOOR SURROUND STRUCTURE LOWER SIDE WAS REMOVED PER CRJ/900 S - [SDR REXA2026080401442](https://openairdocs.org/sdr/REXA2026080401442.md): Angle · corroded · Jun 3, 2026 · N146PQ · Cndair CL6002D24 · Wing Miscellaneous Structure > SECONDARY NRC FROM NRC 00099 AND 00100: AFTER REMOVAL, CORROSION ON ANGLE SUPPORTS (2EA) OF ACCESS PANELS 542AZ AND 642AZ. CORROSION ON ANGLE SUPPORTS (2EA) OF ACCESS PANELS 542AZ AND 642AZ WAS REMOVED PER SRM 51-21-06-001-001-A01 AND ANGLE SUPPORT (1EA) OF AC - [SDR REXA2026080401458](https://openairdocs.org/sdr/REXA2026080401458.md): Rib · cracked · Jun 2, 2026 · N146PQ · Cndair CL6002D24 · Wing, Rib/Bulkhead > CRACK ON MACHINED RIB OF LEADING EDGE SS27.16 AT LEFT WING MACHINED RIB OF LEADING EDGE SS27.16 AT LEFT WING WAS REPLACED PER CRJ-900 SRM 51-42-21-001-001-A01, CRJ-900 SRM 51-42-06-001-001-A01 AND CRJ-900 SRM 51-42-10-001-001-A01 - [SDR REXA2026080401457](https://openairdocs.org/sdr/REXA2026080401457.md): Attach Angle · cracked · Jun 2, 2026 · N146PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CRACK ON CLIP THAT ATTACH AFT FACE OF PRESSURE BULKHEAD TO INTERCOSTAL, FS=1098.20 AND SGTR 24LH AT AFT EQUIPMENT COMPARMENT. CLIP THAT ATTACH AFT FACE OF PRESSURE BULKHEAD TO INTERCOSTAL, FS=1098.20 AND SGTR 24LH AT AFT EQUIPMENT COMPARMENT WAS REPLACED PER C - [SDR REXA2026080401479](https://openairdocs.org/sdr/REXA2026080401479.md): Fitting · corroded · May 28, 2026 · N146PQ · Cndair CL6002D24 · Fuselage, Equipment Attach Fittings > CORROSION FLOOR FITTING IN AFT AND FWD ACCESS 205 (2EAS) ON GALLEY 2. SUMMARY OF NRC 00336:NEW FLOOR FITTING IN FWD ACCESS 205 (1EA) ON GALLEY 2 WAS REPLACED PER SAFRAN CMM 25-32-84 AND NEW FLOOR FITTING IN AFT (1EA) ON GALLEY 2 WAS FABRICATED PER EA NO: CRJ95 - [SDR REXA2026080401478](https://openairdocs.org/sdr/REXA2026080401478.md): Fitting · corroded · May 28, 2026 · N146PQ · Cndair CL6002D24 · Fuselage, Equipment Attach Fittings > CORROSION FLOOR FITTING IN AFT AND FWD ACCESS 205 (2EAS) ON GALLEY 2. SUMMARY OF NRC 00336:NEW FLOOR FITTING IN FWD ACCESS 205 (1EA) ON GALLEY 2 WAS REPLACED PER SAFRAN CMM 25-32-84 AND NEW FLOOR FITTING IN AFT (1EA) ON GALLEY 2 WAS FABRICATED PER EA NO: CRJ95 - [SDR REXA2026080401477](https://openairdocs.org/sdr/REXA2026080401477.md): Fitting · corroded · May 28, 2026 · N146PQ · Cndair CL6002D24 · Fuselage, Equipment Attach Fittings > CORROSION FLOOR FITTING IN FWD ACCESS 109 (1EA) ON GALLEY 1. SUMMARY OF NRC 00333:NEW FLOOR FITTING IN FWD ACCESS 109 (1EA) ON GALLEY 1 WAS FABRICATED PER EA NO: CRJ953-22394 REV IR AND INSTALLED PER SAFRAN CMM 25-33-67 - [SDR REXA2026080401467](https://openairdocs.org/sdr/REXA2026080401467.md): Fitting · corroded · May 28, 2026 · N146PQ · Cndair CL6002D24 · Fuselage, Equipment Attach Fittings > CORROSION FLOOR FITTING IN FRONT PAPER CONTAINER ON FWD LAV (1EA). SUMMARY OF NRC 00338: FLOOR FITTING IN FRONT PAPER CONTAINER ON FWD LAV (1EA) WAS FABRICATED PER EA NO: CRJ953-22392 REV IR AND INSTALLED PER SAFRAN CMM 25-40-76 - [SDR REXA2026080401466](https://openairdocs.org/sdr/REXA2026080401466.md): Fitting · corroded · May 28, 2026 · N146PQ · Cndair CL6002D24 · Fuselage, Equipment Attach Fittings > CORROSION FLOOR FITTING IN FWD AND AFT ACCESS 306 (2EAS) ON GALLEY 3. SUMMARY OF NRC 00337: FLOOR FITTING IN FWD AND AFT ACCESS 306 (2EAS) ON GALLEY 3 WERE REPLACED PER ZODIAC AEROSPACE CMM 25-33-18 REV. NO 5 DATED MAY 15/15 - [SDR REXA2026080401465](https://openairdocs.org/sdr/REXA2026080401465.md): Fitting · corroded · May 28, 2026 · N146PQ · Cndair CL6002D24 · Fuselage, Equipment Attach Fittings > CORROSION FLOOR FITTING IN FWD ACCESS 107 (1EA) ON GALLEY 1. SUMMARY OF NRC 00335: FLOOR FITTING IN FWD ACCESS 107 (1EA) ON GALLEY 1 WAS REPLACED PER SAFRAN CMM 25-33-67 REV NO 10 DATED JUN 20/22 - [SDR REXA2026080401464](https://openairdocs.org/sdr/REXA2026080401464.md): Fitting · corroded · May 28, 2026 · N146PQ · Cndair CL6002D24 · Fuselage, Equipment Attach Fittings > CORROSION FLOOR FITTING IN AFT ACCESS 108 (1EA) ON GALLEY 1. SUMMARY OF NRC 00334: FLOOR FITTING IN AFT ACCESS 108 (1EA) ON GALLEY 1 WAS REPLACED PER SAFRAN CMM 25-33-67 REV. 10 DATED JUN 20/22 - [SDR REXA2026080401456](https://openairdocs.org/sdr/REXA2026080401456.md): Angle · corroded · May 28, 2026 · N146PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CORROSION ON KICKPLATE ANGLE (PASSENGER FLOOR SILL AREA) AT PAX CABIN FLOOR STRUCTURE. DUE TO EXCESSIVE CORROSION ON KICKPLATE ANGLE (PASSENGER FLOOR SILL AREA) AT PAX CABIN FLOOR STRUCTURE WAS REPLACED PER CRJ 900 SRM 53-00-00-101-001-A01, SRM 51-42-06-001-0 - [SDR REXA2026080401451](https://openairdocs.org/sdr/REXA2026080401451.md): Support Fitting · corroded · May 28, 2026 · N146PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CORROSION ON SUPPORT FITTINGS OF GALLEY/LAVATORY AS FOLLOW; (6/A) BTW FS280 AND FS310 BTW LBL45 AND RBL45 AND (2E/A) BTW FS364 AND FS394 BTW RBL9 AND RBL45 AT PAX CABIN FLOOR STRUCTURE. DUE TO EXCESSIVE CORROSION ON SUPPORT FITTINGS (2 EA) BTW FS280 BTW RBL45 - [SDR REXA2026080401450](https://openairdocs.org/sdr/REXA2026080401450.md): Support Fitting · corroded · May 28, 2026 · N146PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CORROSION ON SUPPORT FITTINGS OF GALLEY/LAVATORY AS FOLLOW; (6/A) BTW FS280 AND FS310 BTW LBL45 AND RBL45 AND (2E/A) BTW FS364 AND FS394 BTW RBL9 AND RBL45 AT PAX CABIN FLOOR STRUCTURE. DUE TO EXCESSIVE CORROSION ON SUPPORT FITTINGS (2 EA) BTW FS280 BTW RBL45 - [SDR REXA2026080401446](https://openairdocs.org/sdr/REXA2026080401446.md): Fairing · cracked · May 28, 2026 · N146PQ · Cndair CL6002D24 · Engine Thrust Reverser > CRACKED HINGE FAIRING 443BT HINGE FAIRING 443BT WAS REPAIRED PER EA CRJ954-22614 REV. A - [SDR REXA2026080401421](https://openairdocs.org/sdr/REXA2026080401421.md): Angle · corroded · May 28, 2026 · N146PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CORROSION ON FWD, MID AND AFT CAP ANGLES (PASSENGER FLOOR SILL AREA) AT PAX CABIN FLOOR STRUCTURE DUE TO EXCESSIVE CORROSION ON FWD, MID AND AFT CAP ANGLES (PASSENGER FLOOR SILL AREA) AT PAX CABIN FLOOR STRUCTURE WERE REPLACED PER CRJ-900 SRM 51-10-06-001-001- - [SDR REXA2026080401420](https://openairdocs.org/sdr/REXA2026080401420.md): Angle · corroded · May 28, 2026 · N146PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CORROSION ON FWD, MID AND AFT CAP ANGLES (PASSENGER FLOOR SILL AREA) AT PAX CABIN FLOOR STRUCTURE DUE TO EXCESSIVE CORROSION ON FWD, MID AND AFT CAP ANGLES (PASSENGER FLOOR SILL AREA) AT PAX CABIN FLOOR STRUCTURE WERE REPLACED PER CRJ-900 SRM 51-10-06-001-001- - [SDR REXA2026080401419](https://openairdocs.org/sdr/REXA2026080401419.md): Angle · corroded · May 28, 2026 · N146PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CORROSION ON FWD, MID AND AFT CAP ANGLES (PASSENGER FLOOR SILL AREA) AT PAX CABIN FLOOR STRUCTURE DUE TO EXCESSIVE CORROSION ON FWD, MID AND AFT CAP ANGLES (PASSENGER FLOOR SILL AREA) AT PAX CABIN FLOOR STRUCTURE WERE REPLACED PER CRJ-900 SRM 51-10-06-001-001- - [SDR REXA2026080401418](https://openairdocs.org/sdr/REXA2026080401418.md): Floorbeam · corroded · May 28, 2026 · N146PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam > CORROSION ON FLOOR CROSSBEAM FS333 BTW RBL7 AND RBL45 AT PAX CABIN FLOOR STRUCTURE. CORROSION ON FLOOR CROSSBEAM FS333 BTW RBL7 AND RBL45 AT PAX CABIN FLOOR STRUCTURE WAS REPAIRED PER EA NO. CR953-22493 REV IR - [SDR REXA2026080401472](https://openairdocs.org/sdr/REXA2026080401472.md): Stringer · corroded · May 27, 2026 · N146PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer > CORROSION ON STGR19R BTW FS 295 AND FS 310 AT MAIN AVIONICS COMPARTMENT. CORROSION ON STGR19R BTW FS 295 AND FS 310 AT MAIN AVIONICS COMPARTMENT WAS REMOVED AND EVALUATED OUT OF LIMITS, THEREFORE WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01, CRJ900 SRM 51- - [SDR REXA2026080401441](https://openairdocs.org/sdr/REXA2026080401441.md): Door Sill · corroded · May 27, 2026 · N146PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CORROSION ON LOWER SILL AT AFT BAGGAGE BAY DOOR CUT OUT. CORROSION ON LOWER SILL AT AFT BAGGAGE BAY DOOR CUT OUT WAS EVALUATED OUT LIMITS PER SRM 51-10-06-001-001-A01 THEREFORE WAS REPLACED PER SRM 51-42-21-001-001-A01, SRM 51-42-06-001-001-A01 AND 51-42-13- - [SDR REXA2026080401434](https://openairdocs.org/sdr/REXA2026080401434.md): Plate · corroded · May 27, 2026 · N146PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CORROSION ON FWD AND AFT GUSSET PLATES ALSO CORROSION ON PLATES (BTW STGR24L AND STGR26L) OF FWD AND CTR DOOR LOWER SURROUND STRUCTURE AT FWD BAGGAGE BAY COMPARTMENT. DUE TO NOT ALLOWABLE CORROSION ON FWD AND AFT GUSSET PLATES ALSO CORROSION ON PLATES (BTW STG - [SDR REXA2026080401433](https://openairdocs.org/sdr/REXA2026080401433.md): Stringer · corroded · May 27, 2026 · N146PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer > INITIAL INSPECTION: CORROSION ON STGR18R FROM FS629 TO FS661 AND FROM FS661+62 TO FS661+90 AT FWD BAGGAGE BAY COMPARTMENT. CORROSION ON STGR18R FROM FS629 TO FS661 AND FROM FS661+62 TO FS661+90 AT FWD BAGGAGE BAY COMPARTMENT WAS REMOVED PER CRJ-900 SRM 51-21- - [SDR REXA2026080401432](https://openairdocs.org/sdr/REXA2026080401432.md): Stringer · corroded · May 27, 2026 · N146PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer > INITIAL INSPECTION: CORROSION ON STGR20R (LONGITUDINAL JOINT AREA); FROM FS485 TO FS533, FROM FS565 TO FS581 AND FROM FS597 TO FS613 AT FWD BAGGAGE BAY COMPARTMENT. CORROSION ON STGR20R (LONGITUDINAL JOINT AREA); FROM FS485 TO FS533, FROM FS565 TO FS581 AND F - [SDR REXA2026080401431](https://openairdocs.org/sdr/REXA2026080401431.md): Bracket · corroded · May 27, 2026 · N146PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CORROSION ON CONNECTORS SUPPORT PLATES LH/RH (PX33, PX17, PX34, PX19) ON LH/RH MAIN WHEEL WELL. CORROSION ON CONNECTORS SUPPORT PLATES LH/RH (PX33, PX17, PX34, PX19) ON LH/RH MAIN WHEEL WELL WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01 AND SUPPORT PLATE L - [SDR REXA2026080401430](https://openairdocs.org/sdr/REXA2026080401430.md): Stringer Splice · corroded · May 27, 2026 · N146PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer > CORROSION ON STGR19R, BTW FS 437 AND FS 453 AND BTW FS 469 AND FS 485 AT MAIN AVIONICS COMPARTMENT. CORROSION ON STGR19R, BTW FS 437 AND FS 453 AND BTW FS 469 AND FS 485 AT MAIN AVIONICS COMPARTMENT WAS EVALUATED OUT LIMITS PER CRJ900 SRM 53-21-03-101-007-A01 - [SDR REXA2026080401462](https://openairdocs.org/sdr/REXA2026080401462.md): Strap · corroded · May 26, 2026 · N146PQ · Cndair CL6002D24 · Aerodynamic Fairings > CORROSION SEVERAL PLACES ON METAL STRIP AT FAIRING PANEL 193AB INNER AND OUTER FACE STRAPS ON FAIRING PANEL 193AB WERE REPLACED IAW SRM 51-42-10-001-001-A01. - [SDR REXA2026080401455](https://openairdocs.org/sdr/REXA2026080401455.md): Support Angle · corroded · May 26, 2026 · N146PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CRACK AT FWD SUPPORT ANGLES (2EA) OF UPPER ACUMULATOR AT NOSE HYDRAULICS COMPARTMENT INTERNAL STRUCTURE (INSIDE ACCESS PANEL 121AL). FWD SUPPORT ANGLES (2EA) OF UPPER ACUMULATOR AT NOSE HYDRAULICS COMPARTMENT INTERNAL STRUCTURE (INSIDE ACCESS PANEL 121AL) WERE - [SDR REXA2026080401454](https://openairdocs.org/sdr/REXA2026080401454.md): Support Angle · corroded · May 26, 2026 · N146PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CRACK AT FWD SUPPORT ANGLES (2EA) OF UPPER ACUMULATOR AT NOSE HYDRAULICS COMPARTMENT INTERNAL STRUCTURE (INSIDE ACCESS PANEL 121AL). FWD SUPPORT ANGLES (2EA) OF UPPER ACUMULATOR AT NOSE HYDRAULICS COMPARTMENT INTERNAL STRUCTURE (INSIDE ACCESS PANEL 121AL) WERE - [SDR REXA2026080401453](https://openairdocs.org/sdr/REXA2026080401453.md): Strap · corroded · May 26, 2026 · N146PQ · Cndair CL6002D24 · Aerodynamic Fairings > CORROSION SEVERAL PLACES ON METAL STRIP AT FAIRING PANEL 193AB INNER AND OUTER FACE STRAPS ON FAIRING PANEL 193AB WERE REPLACED PER CRJ-900 SRM 51-42-10-001-001-A01. - [SDR REXA2026080401449](https://openairdocs.org/sdr/REXA2026080401449.md): Seat Track · corroded · May 26, 2026 · N146PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings > CORROSION ON RH SIDE SEAT RAIL (4 EAS) FROM FS 379.00 TO FS 669.40 ON STGR 15R AT PAX CAB. RH SIDE SEAT RAIL (3 EAS) FROM FS 485.00 TO FS 669.40 ON STGR 15R AT PAX CAB WAS CLEANED PER CRJ900 SRM 51-26-00-001-001-A01 AND NO DAMAGE WAS FOUND, DUE TO EXCESSIVE C - [SDR REXA2026080401448](https://openairdocs.org/sdr/REXA2026080401448.md): Support · cracked · May 26, 2026 · N146PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CRACK ON FWD EDGE LT & RT OF SUPPORT AT JB6. SUPPORT AT JB6 WAS REPLACED PER SRM 51-42-06-001-001-A01. - [SDR REXA2026080401445](https://openairdocs.org/sdr/REXA2026080401445.md): Seat Track · corroded · May 26, 2026 · N146PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings > CORROSION ON LT SIDE SEAT TRACK (4 EAS) FROM BS 379.00 TO BS 669.40 ON STR 15L AT PAX CAB. SEAT TRACK (3 EAS) FROM BS 485.00 TO BS 669.40 ON STR 15L AT PAX CAB WAS CLEANED PER IAW SRM 51-26-00-001-001-A01 & NO DAMAGE WAS FOUND. LT SIDE SEAT TRACK (1 EA) FROM - [SDR REXA2026080401429](https://openairdocs.org/sdr/REXA2026080401429.md): Stringer Splice · corroded · May 26, 2026 · N146PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer > CORROSION ON STGR-19R (2EA) FIRST LOCATED BTW FS469 AND FS485 AND SECOND LOCATED ON FS597 TO FS613. CORROSION ON STGR-19R (2EA) FIRST LOCATED BTW FS469 AND FS485 AND SECOND LOCATED ON FS597 TO FS613 WAS EVALUATED OUT LIMITS PER CRJ-900 SRM 51-10-06-001-001-A01 - [SDR REXA2026080401427](https://openairdocs.org/sdr/REXA2026080401427.md): Thrust Reverser · cracked · May 26, 2026 · N146PQ · Cndair CL6002D24 · Engine Thrust Reverser > DEGRADATED AFT EDGE OF INBD BIFURCATION PANELS ON UPPER AND LOWER CORE COWL AT RH ENGINE SUMMARY: PAINT WAS REMOVED ON LOWER CORE COWL AT RH ENGINE PER CRJ-900 SRM 51-26-01-001-001-A01 AND DAMAGE WAS NOT FOUND AND ON UPPER BIFURCATION PANEL AT RH ENGINE WAS RE - [SDR REXA2026080401444](https://openairdocs.org/sdr/REXA2026080401444.md): Hinge · cracked · May 25, 2026 · N146PQ · Cndair CL6002D24 · Fuselage, Door Hinge > PAX PASSENGER DOOR WAS REPAIRED PER EA CRJ952-22490 REV.IR - [SDR REXA2026080401461](https://openairdocs.org/sdr/REXA2026080401461.md): Hinge · cracked · May 24, 2026 · N146PQ · Cndair CL6002D24 · Fuselage, Door Hinge > SECONDARY NRC: AFTER STEP PANEL 832FT REMOVAL IN REF NRC 046, CRACK ON HINGE WAS FOUND. HINGE ON ACCESS PANEL 832FT WAS REPLACED PER CRJ-900 SRM 51-41-02-001-001-A01 - [SDR REXA2026080401426](https://openairdocs.org/sdr/REXA2026080401426.md): Tee Angle · corroded · May 24, 2026 · N146PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CORROSION ON ANGLE SETTLEMENT AREA OF FAIRING PANEL STA=693 RBL=45 TO LBL=45 /// CORROSION ON ANGLE SETTLEMENT OF FAIRING PANEL FS= 661+90 LBL=40 TO RBL=40 /// CORROSION ON ANGLE SETTLEMENT OF FAIRING FS=661+62 RBL=45 TO LBL=45 ALSO CORROSION ON ANGLE SETTLEME - [SDR REXA2026080401425](https://openairdocs.org/sdr/REXA2026080401425.md): Door Frame · corroded · May 24, 2026 · N146PQ · Cndair CL6002D24 · Fuselage Main, Structure > CORROSION ON ANGLES STA= 847+32 BTW STG 17RH TO 17 LH. CORROSION ON ANGLES BTW STA= 847+32 AND 847+64 AND RBL=18 AND LBL=18. CORROSION ON ANGLE STA= 794 BOTTOM SIDE AND RBL=46 LBL=46 ANGLES STA= 847+32 BTW STG 17RH TO 17 LH, ANGLES, STA= 847+32 AND - [SDR REXA2026080401424](https://openairdocs.org/sdr/REXA2026080401424.md): Door Frame · corroded · May 24, 2026 · N146PQ · Cndair CL6002D24 · Fuselage Main, Structure > CORROSION ON ANGLES BS 847+32 BTW STG 17R TO 17L. CORROSION ON ANGLES BTW BS 847+32 & 847+64 AND RBL 18 LBL 18. CORROSION ON ANGLE BS 794 BOTTOM SIDE AND RBL 46 LBL 46. CORROSION ON ANGLES BS 847+32 BTW S17R TO 17L. CORROSION ON ANGLES BTW BS 847+32 & - [SDR REXA2026080401423](https://openairdocs.org/sdr/REXA2026080401423.md): Rib · cracked · May 24, 2026 · N146PQ · Cndair CL6002D24 · Wing, Rib/Bulkhead > INITIAL INSPECTION': CRACK ON MACHINED RIB LEADING EDGE SS57.16 AT LEFT WING. MACHINED RIB LEADING EDGE SS57.16 AT LEFT WING WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 AND SRM 51-42-10-001-001-A01 - [SDR REXA2026080401440](https://openairdocs.org/sdr/REXA2026080401440.md): Thrust Reverser · cracked · May 23, 2026 · N146PQ · Cndair CL6002D24 · Engine Thrust Reverser > CRACK ON RH LOWER THRUST REVERSER TORQUE BOX FRAME AT LH ENGINE CRACK ON RH LOWER THRUST REVERSER TORQUE BOX FRAME AT LH ENGINE WAS REPAIRED PER REO 690-54-22-130REV. - - - [SDR REXA2026080401447](https://openairdocs.org/sdr/REXA2026080401447.md): Rib · cracked · May 22, 2026 · N146PQ · Cndair CL6002D24 · Fuselage Main, Bulkhead > CRACKED BAT RIB AT WS 14.50 OUTER WING, RT MLG WHEEL WELL TRUNNION AREA. BAT RIB AT WS 14.50 OUTER WING, RT MLG WHEEL WELL TRUNNION AREA WAS REPLACED PER SRM 51-42-21-001-001-A01, SRM 51-41-02-001-001-A01, AND SRM 51-42-10-001-001-A01. - [SDR REXA2026080401416](https://openairdocs.org/sdr/REXA2026080401416.md): Rib · cracked · May 22, 2026 · N146PQ · Cndair CL6002D24 · Wing, Rib/Bulkhead > CRACKED BAT RIB AT WS 14.50 OUTER WING, LH MLG WHEEL WELL TRUNNION AREA. BAT RIB AT WS 14.50 OUTER WING, LH MLG WHEEL WELL TRUNNION AREA WAS REPLACED PER CRJ-900 SRM 51-41-02-001-001-A01, SRM 51-42-10-001-001-A01 AND SRM 51-42-21-001-001-A01 - [SDR REXA2026080401460](https://openairdocs.org/sdr/REXA2026080401460.md): Latch · broken · May 21, 2026 · N146PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > BROKEN SPRING LATCH (2 EAS) OF REFUEL/DEFUEL CONTROL PANEL 192AR SPRING LATCH (2 EAS) OF REFUEL/DEFUEL CONTROL PANEL 192AR WERE REPLACED PER CRJ-900 SRM 51-42-10-001-001-A01 - [SDR REXA2026080401459](https://openairdocs.org/sdr/REXA2026080401459.md): Access Panel · corroded · May 21, 2026 · N146PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CORROSION ON MLG WHEEL WELL ACCESS PANELS NO. 542AZ, 542BZ, 642AZ AND 642BZ CORROSION ON MLG WHEEL WELL ACCESS PANELS NO. 542BZ, 642AZ AND 642BZ WAS REMOVED PER SRM 51-21-06-001-001-A01 AND WERE FOUND WITHIN LIMITS PER SRM 53-00-00-101-001-A01. NEW MLG WHEEL W Next page: https://openairdocs.org/aircraft/N146PQ/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 = 'N146PQ' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N146PQ/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.