N926XJ

Service difficulty reports · 253

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 = 'N926XJ' 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 REXA2026082601664Strap · corrodedCORROSION ON STRIPS OF FAIRINGS 192BB, 193AB & 196DR ALSO LOOSE FASTENERS ON STRIP OF FAIRINGS ACCESS 196DR. STRIPS (2EAS) OF FAIRING 193AB WERE REPLACED PER CRJ-900 SRM 51-42-10-001-001-A01, STRAP OF ACCESS PANEL 196DR WERE REPLACED AND FASTENERS WERE INSTALLJun 17, 2026 · N926XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026082601644Seat Track · corrodedCORROSION & WEAR ON SIDE SEAT TRACKS, BTW FS379.00 TO FS669.40 AND STGR 15R. SIDE SEAT TRACKS, BTW FS379.00 TO FS669.40 AND STGR 15R WERE REPLACED PER AMM 53-00-49-400-801-A19.Jun 17, 2026 · N926XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2026082601643Seat Track · corrodedCORROSION & WEAR ON SIDE SEAT TRACKS, BTW FS379.00 TO FS669.40 AND STGR 15L. SIDE SEAT TRACKS, BTW FS379.00 TO FS669.40 AND STGR 15L WERE REPLACED PER CRJ 900 AMM 53-00-49-400-801-A19.Jun 17, 2026 · N926XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2026082601642Seat Track · corroded"CORROSION & WEAR ON FLOOR SEAT TRACKS, BTW FS477.40 TO FS693.00 AND RBL 9''. FLOOR SEAT TRACKS, BTW FS477.40 TO FS693.00 AND RBL 9"" WERE REPLACED PER AMM 53-00-49-400-801-A19."Jun 17, 2026 · N926XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2026082601641Seat Track · corrodedCORROSION & WEAR ON FLOOR SEAT TRACKS, BTW FS477.40 TO FS693.00 AND LBL 9''. FLOOR SEAT RAILS, BTW FS477.40 TO FS693.00 AND LBL 9 WERE REPLACED PER CRJ-900 AMM 53-00-49-400-801-A19.Jun 17, 2026 · N926XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026082601751Angle · corrodedAFTER MID CAP REMOVAL, CORROSION ON KICKPLATE ANGLE WAS FOUND. KICKPLATE ANGLE WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 51-10-06-001-001-A01 AND WAS REPLACED PER CRJ900 SRM 51-42-21-001-001-A01 AND CRJ900 SRM 51-42-06-001-001-A01Jun 16, 2026 · N926XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026082601750Floor Support · corrodedCORROSION ON FLOOR SUPPORTS LOCATED BTW FS280 TO FS295 & LBL 17'', FS379 TO FS364 & LBL17'' AT CPAX FLOOR STRUCTURE (W1) FLOOR SUPPORTS LOCATED BTW FS280 TO FS295 & LBL 17'', FS379 TO FS364 & LBL17'' AT CPAX FLOOR STRUCTURE (W1) WERE EVALUATED OUT OF LIMITS PEJun 16, 2026 · N926XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026082601740Floor Support · corrodedCORROSION ON FLOOR SUPPORTS LOCATED BTW FS280 TO FS295 & LBL 17'', FS379 TO FS364 & LBL17'' AT CPAX FLOOR STRUCTURE (W1) FLOOR SUPPORTS LOCATED BTW FS280 TO FS295 & LBL 17'', FS379 TO FS364 & LBL17'' AT CPAX FLOOR STRUCTURE (W1) WERE EVALUATED OUT OF LIMITS PEJun 16, 2026 · N926XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026082601739Floor Support · corrodedCORROSION ON RH FLOOR SILL BTW FS280 TO FS379 AT CPAX FLOOR STRUCTURE (W1) CORROSION ON RH FLOOR SILL BTW FS280 TO FS379 AT CPAX FLOOR STRUCTURE (W1) WAS REMOVED AND EVALUATED PER CRJ900 SRM 51-21-06-001-001-A01 SILL RH BTW FS349 TO FS379 WAS REPAIRED PER CJun 16, 2026 · N926XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026082601723Rib · crackedCRACK ON LEADING EDGE RIB SS57.16 AT RH WING LEADING EDGE RIB SS57.16 AT RH WING WAS REPAIRED PER REO 690-57-41-240 REV --Jun 16, 2026 · N926XJ · Cndair CL6002D24 · Wing, Rib/BulkheadSDR REXA2026082601722Plate · chafed" WEAR ON FLAP FITTING AND PLATE SUPPORT OF ""FLAP STUB FAIRING"" 171DL AND 172DR AT LH/RH WING TRAILING EDGE. FLAP FITTING AND PLATE SUPPORT OF ""FLAP STUB FAIRING"" 171DL AND 172DR AT LH/RH WING TRAILING EDGE WERE REPLACED PER CRJ 900 SRM 51-42-21-001-001-AJun 16, 2026 · N926XJ · Cndair CL6002D24 · Trailing Edge FlapsSDR REXA2026082601721Fitting · chafed" WEAR ON FLAP FITTING AND PLATE SUPPORT OF ""FLAP STUB FAIRING"" 171DL AND 172DR AT LH/RH WING TRAILING EDGE. FLAP FITTING AND PLATE SUPPORT OF ""FLAP STUB FAIRING"" 171DL AND 172DR AT LH/RH WING TRAILING EDGE WERE REPLACED PER CRJ 900 SRM 51-42-21-001-001-AJun 16, 2026 · N926XJ · Cndair CL6002D24 · Trailing Edge FlapsSDR REXA2026082601720Fitting · chafed" WEAR ON FLAP FITTING AND PLATE SUPPORT OF ""FLAP STUB FAIRING"" 171DL AND 172DR AT LH/RH WING TRAILING EDGE. FLAP FITTING AND PLATE SUPPORT OF ""FLAP STUB FAIRING"" 171DL AND 172DR AT LH/RH WING TRAILING EDGE WERE REPLACED PER CRJ 900 SRM 51-42-21-001-001-AJun 16, 2026 · N926XJ · Cndair CL6002D24 · Trailing Edge FlapsSDR REXA2026082601719Plate · chafed" WEAR ON FLAP FITTING AND PLATE SUPPORT OF ""FLAP STUB FAIRING"" 171DL AND 172DR AT LH/RH WING TRAILING EDGE. FLAP FITTING AND PLATE SUPPORT OF ""FLAP STUB FAIRING"" 171DL AND 172DR AT LH/RH WING TRAILING EDGE WERE REPLACED PER CRJ 900 SRM 51-42-21-001-001-AJun 16, 2026 · N926XJ · Cndair CL6002D24 · Wing Miscellaneous StructureSDR REXA2026082601682Angle · corrodedCORROSION ON MID CAP ANGLE LOCATED BTW FS310 TO FS349 & LBL 40'' AT CPAX FLOOR STRUCTURE (W1) MID CAP ANGLE LOCATED BTW FS310 TO FS349 & LBL 40'' AT CPAX FLOOR STRUCTURE (W1) WAS EVALUATED OUT OF LIMITS AND WAS REPLACED PER CRJ-900 SRM 51-10-06-001-001-A01 AJun 16, 2026 · N926XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026082601680Door Sill · corrodedCORROSION ON INTERCOSTAL BTW FS=310 / FS=349 AND STGR 21LH AT INTERNAL SURROUND STRUCTURE OF THE PASSENGER DOOR, BELOW THE FLOOR. INTERCOSTAL ON FS 310.00 TO FS 333.00 STGR 21LH, STGR 21LH WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001Jun 16, 2026 · N926XJ · Cndair CL6002D24 · Fuselage Main, StructureSDR REXA2026082601714Access Panel · corrodedCORROSION ON ACCESS 542BZ 532DZ, 542AZ AND 642AZ. CORROSION WAS REMOVED ON ACCESS 532DZ PER CRJ-900 SRM 51-21-06-001-001-A01 AND WAS FOUND WITHIN OF LIMITS PER CRJ-900 SRM 57-41-01-101-002-A01, DUE TO EXCESIVE DAMAGE ON ACCESS 542BZ, 542AZ AND 642AZ WAS REPLACJun 15, 2026 · N926XJ · Cndair CL6002D24 · Wing, Plate/SkinSDR REXA2026082601713Access Panel · corrodedCORROSION ON ACCESS 542BZ 532DZ, 542AZ AND 642AZ. CORROSION WAS REMOVED ON ACCESS 532DZ PER CRJ-900 SRM 51-21-06-001-001-A01 AND WAS FOUND WITHIN OF LIMITS PER CRJ-900 SRM 57-41-01-101-002-A01, DUE TO EXCESIVE DAMAGE ON ACCESS 542BZ, 542AZ AND 642AZ WAS REPLACJun 15, 2026 · N926XJ · Cndair CL6002D24 · Wing, Plate/SkinSDR REXA2026082601712Access Panel · corrodedCORROSION ON ACCESS 542BZ 532DZ, 542AZ AND 642AZ. CORROSION WAS REMOVED ON ACCESS 532DZ PER CRJ-900 SRM 51-21-06-001-001-A01 AND WAS FOUND WITHIN OF LIMITS PER CRJ-900 SRM 57-41-01-101-002-A01, DUE TO EXCESIVE DAMAGE ON ACCESS 542BZ, 542AZ AND 642AZ WAS REPLACJun 15, 2026 · N926XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026082601711Hinge · crackedCRACK AND WEAR ON LOWER HINGE AND MID HINGE AT ACCESS PANEL 832ET. LOWER HINGE AND MID HINGE AT ACCESS PANEL 832ET WERE REPLACED PER CRJ-900 SRM 51-41-02-001-001-A01 AND PER CRJ-900 SRM 51-42-06-001-001-A01.Jun 15, 2026 · N926XJ · Cndair CL6002D24 · Fuselage, Door HingeSDR REXA2026082601710Hinge · crackedCRACK AND WEAR ON LOWER HINGE AND MID HINGE AT ACCESS PANEL 832ET. LOWER HINGE AND MID HINGE AT ACCESS PANEL 832ET WERE REPLACED PER CRJ-900 SRM 51-41-02-001-001-A01 AND PER CRJ-900 SRM 51-42-06-001-001-A01.Jun 15, 2026 · N926XJ · Cndair CL6002D24 · Fuselage, Door HingeSDR REXA2026082601687Frame · crackedCRACK ON FRAME AT INTERNAL FUSELAGE STRUCTURE OVER FS333.00 AND BTW STGR 2L TO 2R. FRAME AT INTERNAL FUSELAGE STRUCTURE FS333.00 AND BTW STGR 2L TO 9R. WAS REPLACE PER CRJ900 SRM 51-42-06-001-001-A01 AND CRJ900 SRM 51-42-21-001-001-A01Jun 15, 2026 · N926XJ · Cndair CL6002D24 · Fuselage Main, FrameSDR REXA2026082601663Angle · corrodedCORROSION ON STRIKER SILL, ANGLE AND MOUNTING ANGLE AT SURROUND STRUCTURE OF GALLEY SERVICE DOOR. CORROSION ON STRIKER SILL, ANGLE AND MOUNTING ANGLE AT SURROUND STRUCTURE OF GALLEY SERVICE DOOR. WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01, MOUNTING ANGLE Jun 15, 2026 · N926XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026082601662Striker · corrodedCORROSION ON STRIKER SILL, ANGLE AND MOUNTING ANGLE AT SURROUND STRUCTURE OF GALLEY SERVICE DOOR. CORROSION ON STRIKER SILL, ANGLE AND MOUNTING ANGLE AT SURROUND STRUCTURE OF GALLEY SERVICE DOOR. WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01, MOUNTING ANGLE Jun 15, 2026 · N926XJ · Cndair CL6002D24 · Fuselage Main, StructureSDR REXA2026082601659Support Angle · corrodedCORROSION AT FS 280.00 FLOOR ACCESS PANEL SUPPORT ANGLE, BTW LBL 12'' TO RBL12'' FS 280.00 FLOOR ACCESS PANEL SUPPORT ANGLE, BTW LBL 12'' TO RBL12'' WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 & SRM 51-42-21-001-001-A01Jun 15, 2026 · N926XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026082601658Rib · crackedCRACK 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 --Jun 15, 2026 · N926XJ · Cndair CL6002D24 · Wing, Rib/BulkheadSDR REXA2026082601671Rib · crackedCRACK ON LEADING EDGE RIB SS57.16 AT RH WING LEADING EDGE RIB SS57.16 AT RH WING WAS REPAIRED PER REO 690-57-41-240 REV --Jun 14, 2026 · N926XJ · Cndair CL6002D24 · Wing, Rib/BulkheadSDR REXA2026082601670Angle · crackedCRACK ANGLE (2EA) ON FS1148.00 STGR 10RH AND FS1155.00 STGR 8RH AT AFT ACCESORIES COMPARMENT. ANGLE (2EA) ON FS1148.00 STGR 10RH AND FS1155.00 STGR 8RH AT AFT ACCESORIES COMPARMENT WERE REPLACED PER CRJ-900 SRM 51-42-21-001-001-A01 & SRM 51-42-13-001-001-A01Jun 14, 2026 · N926XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026082601669Angle · crackedCRACK ANGLE (2EA) ON FS1148.00 STGR 10RH AND FS1155.00 STGR 8RH AT AFT ACCESORIES COMPARMENT. ANGLE (2EA) ON FS1148.00 STGR 10RH AND FS1155.00 STGR 8RH AT AFT ACCESORIES COMPARMENT WERE REPLACED PER CRJ-900 SRM 51-42-21-001-001-A01 & SRM 51-42-13-001-001-A01Jun 14, 2026 · N926XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026082601668Panel · crackedCRACK ON TOP PANEL AT MAIN PASSENGER DOOR. TOP PANEL AT MAIN PASSENGER DOOR WAS REPAIRED PER CRJ-900 SRM 52-11-04-201-006-A01.Jun 14, 2026 · N926XJ · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA2026082601657Bracket · corrodedCORROSION ON CONNECTORS SUPPORT PLATES LH/RH (PX33, PX17, PX34, PX19), SUPPORT PLATE LBL 40'' & RBL 40'' & SUPPORT PLATE (IN BK, LG EXT, LG RET) ON WHEEL WELL LH/RH AREA, RBL 45 AND LBL45. CONNECTORS SUPPORT PLATES LH/RH (PX33, PX17, PX34, PX19) & SUPPORT PLATJun 14, 2026 · N926XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026082601656Support Plate · corrodedCORROSION ON CONNECTORS SUPPORT PLATES LH/RH (PX33, PX17, PX34, PX19), SUPPORT PLATE LBL 40'' & RBL 40'' & SUPPORT PLATE (IN BK, LG EXT, LG RET) ON WHEEL WELL LH/RH AREA, RBL 45 AND LBL45. CONNECTORS SUPPORT PLATES LH/RH (PX33, PX17, PX34, PX19) & SUPPORT PLATJun 14, 2026 · N926XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026082601655Support Plate · corrodedCORROSION ON CONNECTORS SUPPORT PLATES LH/RH (PX33, PX17, PX34, PX19), SUPPORT PLATE LBL 40'' & RBL 40'' & SUPPORT PLATE (IN BK, LG EXT, LG RET) ON WHEEL WELL LH/RH AREA, RBL 45 AND LBL45. CONNECTORS SUPPORT PLATES LH/RH (PX33, PX17, PX34, PX19) & SUPPORT PLATJun 14, 2026 · N926XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026082601647Rib · 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 REPLACE PER CRJ900 SRM 51-42-21-001-001-A01,SRM 51-42-22-001-001-A01 AND SRM 51-41-02-001-001-A01.Jun 14, 2026 · N926XJ · Cndair CL6002D24 · Wing, Rib/BulkheadSDR REXA2026082601645Handle · crackedCRACK ON OUTER HANDLE OF PASSENGER DOOR LATCH MECHANISM. OUTER HANDLE OF PASSENGER DOOR LATCH MECHANISM WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01.Jun 14, 2026 · N926XJ · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA2026082601736Skin · crackedINITIAL INSPECTION: CRACK MULTI-FUNCTION SPOILER PANEL UPPER SKIN (2EAS OUTB) AT LH/RH WING MULTI-FUNCTION SPOILER PANEL UPPER SKIN RH WING WAS REPAIRED PER REO 690-57-73-027 REV -- AND MULTI-FUNCTION SPOILER PANEL UPPER SKIN LH WAS INSPECTED AND NOT DAMAGE WJun 13, 2026 · N926XJ · Cndair CL6002D24 · SpoilersSDR REXA2026082601734Fitting · wornWEAR ON LH/RH SIDE STAY FITTING IN MAIN WHEEL WELL AREA. LT - RT SIDE STAY FITTING IN MAIN WHEEL WELL AREA WERE BLEND OUT PER CRJ900 SRM 51-12-00-001-001-A01 AND WERE REPAIRED PER EA CRJ953-22582 REV IR AND EA CRJ953-22583 REV IRJun 13, 2026 · N926XJ · Cndair CL6002D24 · Wing Main, Frame StructureSDR REXA2026082601685Skin · crackedCRACK ON SKIN AROUND HANDLE CUTOUT AT AFT BAGGAGE COMPARTMENT DOOR. HOUSING (P/N ON:H3415-31, S/N ON:2150 // P/N OFF:H3415-31, S/N OFF:2366) AT AFT BAGGAGE COMPARTMENT DOOR WAS REPLACED PER CRJ900 SRM 51-42-21-001-001-01Jun 13, 2026 · N926XJ · Cndair CL6002D24 · Cargo/Baggage DoorsSDR REXA2026082601735Fitting · wornINITIAL INSPECTION: WEAR ON LH/RH SIDE STAY FITTING IN MAIN WHEEL WELL AREA. LH/RH SIDE STAY FITTING IN MAIN WHEEL WELL AREA WERE BLEND OUT PER CRJ900 SRM 51-12-00-001-001-A01 AND WERE REPAIRED PER EA CRJ953-22582 REV IR AND EA CRJ953-22583 REV IRJun 12, 2026 · N926XJ · Cndair CL6002D24 · Wing Main, Frame StructureSDR REXA2026082601699Web · crackedCRACK ON FLOOR WEB RIGHT SIDE AT ELECTRICAL BAY (BELOW ADG SUPPORT DOUBLER) FS 193.00. FLOOR WEB RIGHT SIDE (REPAIR DOUBLER) AT ELECTRICAL BAY (BELOW ADG SUPPORT DOUBLER) FS 193.00 WAS REPLACED PER CRJ900 SRM 53-11-43-201-001-A01.Jun 12, 2026 · N926XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026082601661Support Bracket · crackedCRACK ON BRACKET SUPPORT OF JB6 AT FWD EQUIPMENT COMPARTMENT BRACKET SUPPORT OF JB6 AT FWD EQUIPMENT COMPARTMENT WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01Jun 12, 2026 · N926XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026082601660Hinge · crackedFWD LAV SERVICE DOOR UPPER HINGE WONT LOCK AND CRACKED FWD LAV SERVICE DOOR UPPER HINGE WAS REPLACED PER CRJ 900 AMM 52-45-17 & SRM 51-42-21-001-001-A01Jun 12, 2026 · N926XJ · Cndair CL6002D24 · Fuselage, Door HingeSDR REXA2026082601654Drag Angle · crackedCRACKED AFT DRAG ANGLE AT LH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM. AFT DRAG ANGLE AT LH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM WAS REPAIRED PER CRJ900 SRMJun 12, 2026 · N926XJ · Cndair CL6002D24 · Fuselage, Stabilizer Attach FittingsSDR REXA2026082601653Drag Angle · crackedCRACKED AFT DRAG ANGLE AT RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM. AFT DRAG ANGLE AT RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM WAS REPAIRED PER CRJ900 SRMJun 12, 2026 · N926XJ · Cndair CL6002D24 · Fuselage, Stabilizer Attach FittingsSDR REXA2026061700966Fan · inoperativeDURING FINAL APPROACH FLIGHT ATTENDANT REPORTED SMELL OF SMOKE AS WELL AS HAZE { LIGHT SMOKE} IN FWD CABIN EMERGENCY DECLEARED- CABIN QRH CHECK LIST COMPLETED HAZE CONDITION DISSIPATED ODOR REMAINED SAFE ENOUGH TO CONTINUE TO GATE NO SMELL IN COCKPIT OR AFT CAJun 10, 2026 · N926XJ · Cndair CL6002D24 · Air Distribution FanSDR REXA2024091600711Lamp · inoperativeSERVICE DOOR EXTERIOR EMERGENCY LIGHT INOP RELAMPED SERVICE DOOR EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-15. OPS TEST PASS.P/N OFF/ON: 8GA411060-06Sep 7, 2024 · N926XJ · Cndair CL6002D24 · Emergency LightingSDR REXA2022050400310Angle · crackedPAX DOOR AFT WEB ANGLE IS CRACKED. COMPLETED REPAIR OF PAX DOOR AFT DRAG ANGLE IAW CRJ 900 SRM 52-11-04-201-002-A01May 3, 2023 · N926XJ · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA2022050200304Retainer · corrodedPAX DOOR CLIP ON FWD SIDE OF SUPPORT ANGLE AT DD7A IS CORRODED LOCATED ,DRILLED AND INSTALLED NEW PAX DOOR CLIP P/N 601R318058-1 IAW CRJ 900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01Apr 27, 2023 · N926XJ · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA2022050200303Angle · corrodedPAX DOOR SUPPORT ANGLE AT DD7A FOUND TO BE CORRODED LOCATED DRILLED AND INSTALLED NEW SERVICEABLE PAX DOOR ANGLE AT DD7A IAW CRJ900 SRM 51-40-11-001-001-A01 AND 51-42-21-001-001-A01Apr 27, 2023 · N926XJ · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA2022050800317Doubler · crackedPAX DOOR FORWARD LATCH FITTING BACK-UP STRUCTURE IS CRACKED. ACCESSED THRU PANEL 832AL LOCATED DRILLED AND INSTALLED NEW SERVICEABLE FWD LATCH FITTING BACK UP STRUCTURE IAW CRJ900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01 AND 51-42-21-001-001-A01Apr 24, 2023 · N926XJ · Cndair CL6002D24 · Passenger/Crew Doors
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