N146PQ

Service difficulty reports · 191

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 = 'N146PQ' 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 REXA2026080401435Landing · crackedSECONDARY 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: - -Jun 10, 2026 · N146PQ · Cndair CL6002D24 · Wing StructureSDR REXA2026080401439Handle · crackedCRACK OUTER HANDLE OF PASSENGER DOOR. OUTER HANDLE OF PASSENGER DOOR WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01Jun 7, 2026 · N146PQ · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA2026080401471Fitting · crackedCRACK 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-A01Jun 4, 2026 · N146PQ · Cndair CL6002D24 · Fuselage Main, StructureSDR REXA2026080401470Fitting · crackedCRACK 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-A01Jun 4, 2026 · N146PQ · Cndair CL6002D24 · Fuselage Main, StructureSDR REXA2026080401443Door Frame · corrodedSECONDARY 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 SJun 3, 2026 · N146PQ · Cndair CL6002D24 · Fuselage Main, StructureSDR REXA2026080401442Angle · corrodedSECONDARY 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 ACJun 3, 2026 · N146PQ · Cndair CL6002D24 · Wing Miscellaneous StructureSDR REXA2026080401458Rib · crackedCRACK 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-A01Jun 2, 2026 · N146PQ · Cndair CL6002D24 · Wing, Rib/BulkheadSDR REXA2026080401457Attach Angle · crackedCRACK 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 CJun 2, 2026 · N146PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026080401479Fitting · corrodedCORROSION 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: CRJ95May 28, 2026 · N146PQ · Cndair CL6002D24 · Fuselage, Equipment Attach FittingsSDR REXA2026080401478Fitting · corrodedCORROSION 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: CRJ95May 28, 2026 · N146PQ · Cndair CL6002D24 · Fuselage, Equipment Attach FittingsSDR REXA2026080401477Fitting · corrodedCORROSION 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 25-33-67May 28, 2026 · N146PQ · Cndair CL6002D24 · Fuselage, Equipment Attach FittingsSDR REXA2026080401467Fitting · corrodedCORROSION 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 25-40-76May 28, 2026 · N146PQ · Cndair CL6002D24 · Fuselage, Equipment Attach FittingsSDR REXA2026080401466Fitting · corrodedCORROSION 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 15/15May 28, 2026 · N146PQ · Cndair CL6002D24 · Fuselage, Equipment Attach FittingsSDR REXA2026080401465Fitting · corrodedCORROSION 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 20/22May 28, 2026 · N146PQ · Cndair CL6002D24 · Fuselage, Equipment Attach FittingsSDR REXA2026080401464Fitting · corrodedCORROSION 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 20/22May 28, 2026 · N146PQ · Cndair CL6002D24 · Fuselage, Equipment Attach FittingsSDR REXA2026080401456Angle · corrodedCORROSION 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 51-42-06-001-0May 28, 2026 · N146PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026080401451Support Fitting · corrodedCORROSION 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 RBL45May 28, 2026 · N146PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026080401450Support Fitting · corrodedCORROSION 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 RBL45May 28, 2026 · N146PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026080401446Fairing · crackedCRACKED HINGE FAIRING 443BT HINGE FAIRING 443BT WAS REPAIRED PER EA CRJ954-22614 REV. AMay 28, 2026 · N146PQ · Cndair CL6002D24 · Engine Thrust ReverserSDR REXA2026080401421Angle · corrodedCORROSION 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-May 28, 2026 · N146PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026080401420Angle · corrodedCORROSION 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-May 28, 2026 · N146PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026080401419Angle · corrodedCORROSION 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-May 28, 2026 · N146PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026080401418Floorbeam · corrodedCORROSION 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 IRMay 28, 2026 · N146PQ · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR REXA2026080401472Stringer · corrodedCORROSION 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-May 27, 2026 · N146PQ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2026080401441Door Sill · corrodedCORROSION 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-May 27, 2026 · N146PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026080401434Plate · corrodedCORROSION 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 STGMay 27, 2026 · N146PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026080401433Stringer · corrodedINITIAL 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-May 27, 2026 · N146PQ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2026080401432Stringer · corrodedINITIAL 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 FMay 27, 2026 · N146PQ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2026080401431Bracket · corrodedCORROSION 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 LMay 27, 2026 · N146PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026080401430Stringer Splice · corrodedCORROSION 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-A01May 27, 2026 · N146PQ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2026080401462Strap · corrodedCORROSION 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.May 26, 2026 · N146PQ · Cndair CL6002D24 · Aerodynamic FairingsSDR REXA2026080401455Support Angle · corrodedCRACK 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) WEREMay 26, 2026 · N146PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026080401454Support Angle · corrodedCRACK 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) WEREMay 26, 2026 · N146PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026080401453Strap · corrodedCORROSION 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.May 26, 2026 · N146PQ · Cndair CL6002D24 · Aerodynamic FairingsSDR REXA2026080401449Seat Track · corrodedCORROSION 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 CMay 26, 2026 · N146PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2026080401448Support · crackedCRACK ON FWD EDGE LT & RT OF SUPPORT AT JB6. SUPPORT AT JB6 WAS REPLACED PER SRM 51-42-06-001-001-A01.May 26, 2026 · N146PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026080401445Seat Track · corrodedCORROSION 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 May 26, 2026 · N146PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2026080401429Stringer Splice · corrodedCORROSION 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-A01May 26, 2026 · N146PQ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2026080401427Thrust Reverser · crackedDEGRADATED 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 REMay 26, 2026 · N146PQ · Cndair CL6002D24 · Engine Thrust ReverserSDR REXA2026080401444Hinge · crackedPAX PASSENGER DOOR WAS REPAIRED PER EA CRJ952-22490 REV.IRMay 25, 2026 · N146PQ · Cndair CL6002D24 · Fuselage, Door HingeSDR REXA2026080401461Hinge · crackedSECONDARY 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-A01May 24, 2026 · N146PQ · Cndair CL6002D24 · Fuselage, Door HingeSDR REXA2026080401426Tee Angle · corrodedCORROSION 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 SETTLEMEMay 24, 2026 · N146PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026080401425Door Frame · corrodedCORROSION 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 ANDMay 24, 2026 · N146PQ · Cndair CL6002D24 · Fuselage Main, StructureSDR REXA2026080401424Door Frame · corrodedCORROSION 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 & May 24, 2026 · N146PQ · Cndair CL6002D24 · Fuselage Main, StructureSDR REXA2026080401423Rib · crackedINITIAL 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-A01May 24, 2026 · N146PQ · Cndair CL6002D24 · Wing, Rib/BulkheadSDR REXA2026080401440Thrust Reverser · crackedCRACK 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. - -May 23, 2026 · N146PQ · Cndair CL6002D24 · Engine Thrust ReverserSDR REXA2026080401447Rib · crackedCRACKED 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.May 22, 2026 · N146PQ · Cndair CL6002D24 · Fuselage Main, BulkheadSDR REXA2026080401416Rib · crackedCRACKED 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-A01May 22, 2026 · N146PQ · Cndair CL6002D24 · Wing, Rib/BulkheadSDR REXA2026080401460Latch · brokenBROKEN 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-A01May 21, 2026 · N146PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026080401459Access Panel · corrodedCORROSION 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 WMay 21, 2026 · N146PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
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