N909XJ

Service difficulty reports · 231

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 = 'N909XJ' 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 REXA2026102001948Window Post · crackedRT WINDOW SUPPORT STRAP OF THE WINDOW POST FOUND CRACKED. REPLACED RT WINDOW STRAP SUPPORT POST.Oct 19, 2026 · N909XJ · Cndair CL6002D24 · Fuselage Main, StructureSDR REXA2026060800943Channel · crackedCRACK ON AFT LOW CHANNEL FS 1047.00 ATTACHED TO DOOR SURROUND STRUCTURE OF AFT BAGGAGE BAY COMPARTMENT AFT LOW CHANNEL FS 1047.00 ATTACHED TO DOOR SURROUND STRUCTURE OF AFT BAGGAGE BAY COMPARTMENT WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42Jun 4, 2026 · N909XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026060400922Floor Support · corrodedCORROSION ON FLOOR SILL RH BTW FS280 TO FS319.70 AT FLOOR STRUCTURE OF PASSENGER CABIN. CORROSION WAS EVALUATED OUT LIMITS DUE TO EXCESIVE DAMAGE THEREFORE WAS REPLACED PER CRJ-900 SRM 53-00-45-201-001-A01 AND CRJ-900 SRM 51-42-06-001-001-A01 SRM 51-42-13-001-May 18, 2026 · N909XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026060400921Support · 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 CRJ-900 SRM 51-21-06-001-001-A01, EVALUATED SUPPORT PMay 18, 2026 · N909XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026060400920Support · corrodedCORROSION ON RH/LH MLG HYDRAULIC LINES SUPPORT PLATE (UPPER AND LOWER) (IN BK, LG EXT, LG RET) (4 EAS) RBL 45/LBL 45 ON WHEEL WELL. SUMMMARY OF NRC 00034: CORROSION ON RH/LH MLG HYDRAULIC LINES SUPPORT PLATE (UPPER AND LOWER) (IN BK, LG EXT, LG RET) (4 EAS) RBMay 18, 2026 · N909XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026060400919Landing · crackedCRACKS ON AFT RT DOOR LANDING AT FS 188.00 (LATCH CUT OUT OF ACCESS DOOR 212AR REPLACE PER CRJ900 SRM 51-42-06-001-001-A01 AND SRM 51-42-13-001-001-A01May 18, 2026 · N909XJ · Cndair CL6002D24 · Fuselage Main, StructureSDR REXA2026060400918Hinge · crackedCRACK HINGES OTBD EDGES OF ACCESS PANELS NBR 591LB & 691LB AT LH/RH WINGS PERFORM THE REPLACEMENT OF THE HINGE PER SRM 51-42-06-001-001-A01 AND EA CRJ957-22208 REV IRMay 18, 2026 · N909XJ · Cndair CL6002D24 · Wing Main, Frame StructureSDR REXA2026060400912Hinge · crackedCRACK HINGES OTBD EDGES OF ACCESS PANELS NBR 591LB & 691LB AT LH/RH WINGS PERFORM THE REPLACEMENT OF THE HINGE PER SRM 51-42-06-001-001-A01 AND EA CRJ957-22208 REV IRMay 18, 2026 · N909XJ · Cndair CL6002D24 · Wing Main, Frame StructureSDR REXA2026060400910Access Panel · crackedCRACK ON ACCESS PANEL 433BT AND 433BB ACCESS PANEL 433BT AND 433BB WERE REPLACE PER SRM 51-42-10-001-001-A01 AND 51-42-06-001-001-A01May 18, 2026 · N909XJ · Cndair CL6002D24 · Engine Thrust ReverserSDR REXA2026060400909Access Panel · crackedCRACK ON ACCESS PANEL 433BT AND 433BB ACCESS PANEL 433BT AND 433BB WERE REPLACE PER SRM 51-42-10-001-001-A01 AND 51-42-06-001-001-A01May 18, 2026 · N909XJ · Cndair CL6002D24 · Engine Thrust ReverserSDR REXA2026060800942Seat Track · corrodedCORROSION ON SEAT RAIL BTW FS 349 TO FS 409 9RBL AND FS 370 TO FS 409 LBL9 AT FLOOR PASSENGER CABIN SEAT RAIL BTW FS 349 TO FS 409 9RBL AND FS 370 TO FS 409 LBL9 AT FLOOR PASSENGER CABIN WERE REPLACED PER CRJ 900 SRM 53-00-49-000-801-A07 AND SRM 53-00-49-400-8May 10, 2026 · N909XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2026060400904Lug · corrodedCORROSION AND WEAR WAS FOUND ON LUG BORE ON AIL STA 337.657 (LUG L2) AND 342.911 (LUG L5) LUG BORE ON AIL STA 337.657 (LUG L2) AND 342.911 (LUG L5) WERE REPAIRED PER REO 690-57-61-521 REV. - - AND REO 670-57-61-237 REV - -May 9, 2026 · N909XJ · Cndair CL6002D24 · Wing, Control Surface Attach FittingsSDR REXA2026060400903Hinge · corrodedAFTER RH AILERON BUSHINGS REMOVAL, CORROSION AND WEAR WAS FOUND ON LUG BORE ON AIL STA 336.4015 ( LUG R1), 337.657 (LUG R2), 338.424 (LUG R3), 342.911 (LUG R5) AND 344.1665 (LUG R6) LUG BORE ON AIL STA 336.4015 ( LUG R1), AND 338.424 (LUG R3) WERE CLEANED PER May 8, 2026 · N909XJ · Cndair CL6002D24 · AileronsSDR REXA2026060400933Fitting · corrodedCORROSION FLOOR FITTING IN AFT ACCESS 107 OUT SIDE (1EA) ON GALLEY 1 NEW FLOOR FITTING P/N: A661091-1 IN AFT ACCESS 107 OUT SIDE (1EA) ON GALLEY 1. WAS MANUFACTURED PER EA NO: CRJ953-22230 REV IR. AND REPLACED PER SAFRAN CMM 25-33-67 REV NO. 10 DATED JUN 20/May 7, 2026 · N909XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026060400908Fitting · corrodedCORROSION FLOOR FITTING IN AFT ACCESS 108 (1EA) ON GALLEY 1. FLOOR FITTING IN AFT ACCESS 108 (1EA) ON GALLEY 1 WAS REPLACED PER SAFRAN CMM 25-33-67 REV. 10May 7, 2026 · N909XJ · Cndair CL6002D24 · Fuselage, Equipment Attach FittingsSDR REXA2026060400906Fitting · corrodedCORROSION FLOOR FITTING IN AFT ACCESS 108 (1EA) ON GALLEY 1. FLOOR FITTING IN AFT ACCESS 108 (1EA) ON GALLEY 1 WAS REPLACED PER SAFRAN CMM 25-33-67 REV. 10May 7, 2026 · N909XJ · Cndair CL6002D24 · Fuselage, Equipment Attach FittingsSDR REXA2026060400905Fitting · corrodedCORROSION FLOOR FITTING IN AFT AND FWD ACCESS 205 (2EAS) ON GALLEY 2. FLOOR FITTING (PN: A391251-3) IN AFT ACCESS 205 (1 EA) ON GALLEY 2 WAS MANUFACTURED PER EA CRJ953-22214 REV IR AND INSTALLED PER CMM 25-32-84 REV NO. 9 AND FLOOR FITTING ( PN: 9861251-3 IN May 7, 2026 · N909XJ · Cndair CL6002D24 · Fuselage, Equipment Attach FittingsSDR REXA2026060400917Floorbeam · corrodedCORROSION ON CROSSBEAMS ON FS349 BTW LBL9 TO RBL9 AT FLOOR STRUCTURE PASSENGER. CROSSBEAMS ON FS349 BTW LBL9 TO RBL9 AT FLOOR STRUCTURE PASSENGER WAS REPAIRED PER REO 690-53-21-2136 REV.--May 6, 2026 · N909XJ · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR REXA2026060400925Support Angle · corrodedCORROSION ON SUPPORT ANGLES (2EA) ON FUEL PANEL ON ACCESS PANEL 192AR. SUPPORT ANGLES (2EA) ON FUEL PANEL ON ACCESS PANEL 192AR WERE REPLACED PER CRJ-900 SRM 51-42-10-001-001-A01.May 5, 2026 · N909XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026060400907Support Angle · corrodedCORROSION ON SUPPORT ANGLES (2EA) ON FUEL PANEL ON ACCESS PANEL 192AR. SUPPORT ANGLES (2EA) ON FUEL PANEL ON ACCESS PANEL 192AR WERE REPLACED PER SRM 51-42-10-001-001-A01.May 5, 2026 · N909XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026060400931Support Bracket · crackedCRACK ON UPPER / LOWER SUPPORT BRACKET OF PYLON TIE-BAR, THROUGH PYLON ACCESS PANELS 433BT AND 433BB AT LH ENGINE.. UPPER / LOWER SUPPORT BRACKET OF PYLON TIE-BAR, THROUGH PYLON ACCESS PANELS 433BT AND 433BB AT LH ENGINE WERE REPLACED PER CRJ900 SRM 51-42-06-0May 4, 2026 · N909XJ · Cndair CL6002D24 · Engine Thrust ReverserSDR REXA2026060400930Support Bracket · crackedCRACK ON UPPER / LOWER SUPPORT BRACKET OF PYLON TIE-BAR, THROUGH PYLON ACCESS PANELS 433BT AND 433BB AT LH ENGINE.. UPPER / LOWER SUPPORT BRACKET OF PYLON TIE-BAR, THROUGH PYLON ACCESS PANELS 433BT AND 433BB AT LH ENGINE WERE REPLACED PER CRJ900 SRM 51-42-06-0May 4, 2026 · N909XJ · Cndair CL6002D24 · Engine Thrust ReverserSDR REXA2026060400928Angle · crackedBROKEN OUTBOARD CORNER SETTLEMENT AREA OF EQUIPPED LINER AT CTR BAGGAGE BAY DOOR ANGLE (2EAS) UPPER AFT AND UPPER FWD WERE REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01, SRM 51-41-02-001-001-A01May 4, 2026 · N909XJ · Cndair CL6002D24 · Cargo/Baggage DoorsSDR REXA2026060400916Channel · crackedCRACK ON LH & RH CHANNEL LOCATED BTW FS 799.00 AT LBL42.00 AND RBL42.00 ON MLG WHEEL WELL AREA (WHEEL BIN SUPPORT CHANNEL). CHANNEL LH & RH LOCATED BTW FS 799.00 AT LBL42.00 AND RBL42.00 ON MLG WHEEL WELL AREA (WHEEL BIN SUPPORT CHANNEL) WERE REMPLACED PER. CRMay 4, 2026 · N909XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026060400915Channel · crackedCRACK ON LH & RH CHANNEL LOCATED BTW FS 799.00 AT LBL42.00 AND RBL42.00 ON MLG WHEEL WELL AREA (WHEEL BIN SUPPORT CHANNEL). CHANNEL LH & RH LOCATED BTW FS 799.00 AT LBL42.00 AND RBL42.00 ON MLG WHEEL WELL AREA (WHEEL BIN SUPPORT CHANNEL) WERE REMPLACED PER. CRMay 4, 2026 · N909XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026060400914Retainer · chafedBENT AND WEAR ON INNER AND OUTBOARD (4 EAS) RETAINER SEAL AT FWD AND CTR BAGGAGE BAY DOORS COMPARTMENT SEAL RETAINER (2AE) AT FWD AND CTR BAGGAGE BAY DOORS COMPARTMENT WERE EVALUATED PER CRJ-900 SRM 52-35-07-201-001-A01 OUT LIMITS THEREFORE WERE REPLACED ER CRMay 4, 2026 · N909XJ · Cndair CL6002D24 · Cargo/Baggage DoorsSDR REXA2026060400913Retainer · chafedBENT AND WEAR ON INNER AND OUTBOARD (4 EAS) RETAINER SEAL AT FWD AND CTR BAGGAGE BAY DOORS COMPARTMENT SEAL RETAINER (2AE) AT FWD AND CTR BAGGAGE BAY DOORS COMPARTMENT WERE EVALUATED PER CRJ-900 SRM 52-35-07-201-001-A01 OUT LIMITS THEREFORE WERE REPLACED ER CRMay 4, 2026 · N909XJ · Cndair CL6002D24 · Cargo/Baggage DoorsSDR REXA2026060400902Skin · chafedWEAR ON EXTERNAL FUSELAGE SKIN LOCATED BTW BS 897 - 913 AND STGR 27. EXTERNAL FUSELAGE SKIN LOCATED BTW FS 897.00 TO FS 913.00 AND STGR 27 WAS REPAIRED PER REO 670-53-00-290 REV. -F, PL 670-53-00-29 0 SHEET #5, REV.-E FIGURE 3.May 4, 2026 · N909XJ · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR REXA2026060400927Drag Angle · crackedCRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE ATMay 3, 2026 · N909XJ · Cndair CL6002D24 · Fuselage, Stabilizer Attach FittingsSDR REXA2026060400926Drag Angle · crackedCRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE May 3, 2026 · N909XJ · Cndair CL6002D24 · Fuselage, Stabilizer Attach FittingsSDR REXA2026060400923Hinge · corroded"CORROSION ON ACCESS PANEL 832EL AND CORROSION ON HINGE AT ACCESS DOOR 832ET CORROSION WAS REMOVED OF ACCESS PANEL 832EL PER CRJ900 SRM 51-21-06-001-001-A01 AND WAS FOUND WITHIN LIMITS PER CRJ-900 SRM 52-11-32-101-001-A01, HINGE (P/N: CC670-31981-3) AT ACCESS May 3, 2026 · N909XJ · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA2025022600226Valve · inoperative"ON FINAL APPROACH, ""GEAR DISAGREE"" WARNING MESSAGE. GEAR DID NOT COME DOWN. RECYCLED LANDING GEAR LEVER 2 TIMES. GEAR STILL DID NOT COME DOWN RAN QRH. PER QRH RELEASED GEAR VIA MANUAL GEAR RELEASE. THEN WE RECEIVED GREEN INDICATIONS ON ALL THREE. AFTER LANDFeb 21, 2025 · N909XJ · Cndair CL6002D24 · Landing Gear Retraction/Extension SystemSDR REXA2025021000178Controller · inoperativeRIGHT SIDE WINDSHIELD HEAT CONTROLLER POPPED DURING CRUISE. SPARKS SMOKE AND FUMES PRESENT, SIMULTANEOUSLY DISPLAYING RIGHT WINDSHIELD HEAT CAUTION MSG. RAN RIGHT WINDSHIELD HEAT QRH PROCEDURE AND SHUT OFF RIGHT WINDSHIELD HEAT CONTROLLER. THERE WERE NO POPPEDFeb 4, 2025 · N909XJ · Cndair CL6002D24 · Windshield/Door Rain/Ice RemovalSDR REXA2025012300072Selector Valve · inoperativeGEAR DISAGREE WARNING AFTER GEAR RETRACTION HANDLE SELECTED UP. ALL GEAR REMAINED DOWN AFTER CYCLNG HANDLE. GEAR WAS ABLE TO RETRACT ON THIRD ATTEMPT. R/R LANDING GEAR SELECTOR VALVE IAW AMM 32-32-10 REFER TO NRWC #869574, 869575, AND 869803 FOR WORK PERFORMJan 21, 2025 · N909XJ · Cndair CL6002D24 · Landing Gear Retraction/Extension SystemSDR REXA2025011300045Engine · damagedON INITIAL CLIMB OUT HEARD VIBRATION FOLLOWED BY A LOUD BANG, SAW OBJECT FLY BY FO WINDOW EMERGENCY DECLARED WITH ATC, RETURNED TO LAND IN ATL, NO ABNORMAL INDICATIONS ON EICAS ON POST FLIGHT WALK AROUND, A PIECE OF HEAD SET JACK WAS DISCOVERED STILL CONNECTEDJan 4, 2025 · N909XJ · Cndair CL6002D24 · Engine (Turbine/Turboprop)SDR REXA2022031500260Lamp · inoperativeFWD EMERGENCY FLOOR LIGHT HAS BURNT OUT BULBS R/R BULBS IAW CRJ900 AMM 33-51-11 OPC GOOD P/N OFF/ON 3071BPEGPLMar 13, 2023 · N909XJ · Cndair CL6002D24 · Emergency LightingSDR REXA2022031000251Battery Pack · inoperativeNOTED AFT EMERGENCY LIGHTS OVER WING WENT DIM/OUT R+R BATTERY PACK PS43 PER AMM REF. 33-15-17 PERFORMED OPS TEST PER AMM REF. 33-51-17 OPS TEST GOOD AT THIS TIME P/N OFF/ON 2013-1ASMI S/N OFF 14058 S/N ON 16248Mar 10, 2023 · N909XJ · Cndair CL6002D24 · Emergency LightingSDR REXA2022071401591Tie Clip · corrodedCORROSION FOUND ON PAX DOOR CLIP AT FS 313.56 BETWEEN DD4 AND DD5 INTERCOSTALS REMOVED CLEAT, AND REPLACED WITH NEW CLIP, PART NUMBER: 600-31902-269 WITH NEW FASTENERS. REF. CRJ900 SRM 51-42-06-001-001-A01.Jul 8, 2022 · N909XJ · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA2022071401590Frame · corrodedFRAME CORRODED AT FS1031.00 BETWEEN STRG. 26R AND STGR. 25R REPAIRED FRAME SECTION AT FS.1031 STRG 25R AND 26L PER EA NO: CRJ953-13596 DATE 5-16-22 REV IRJul 8, 2022 · N909XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2022071401589Fitting · crackedPAX DOOR STAIR STEP LOWER CUP FEED THROUGH CASTING IS CRACKED REMOVED AND REPLACED PAX DOOR STAIR STEP LOWER CUP FEED THROUGH CASTING P/N 601R317077-3 WITH NEW FASTENERS. REF CRJ 900 SRM 51-42-06-001-001-A01Jul 8, 2022 · N909XJ · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA2022071401588Angle · corrodedPAX DOOR FWD FORMER SUPPORT ANGLE AT FS311.75 HAS EXFOLIATED CORROSION. EVALUATED, CORRODED, PAX DOOR, FORWARD FORMER SUPPORT ANGLE AT FS311.75, AS OUT-OF-LIMITS. REMOVED CORRODED FORMER SUPPORT ANGLE AND INSTALLED NEW SUPPORT ANGLE PN: 601R318731-3. REF.CRJ90Jul 8, 2022 · N909XJ · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA2022071401587Frame · corrodedCORROSION FOUND ON PAX DOOR FRAME AT FS 313.56 BETWEEN DD4 AND DD5 INTERCOSTALS REMOVED FRAME SECTION AND REPLACED WITH NEW FRAME SECTION PART NUMBER: 601R318086-1 WITH NEW FASTENERS. REF. CRJ900 SRM 51-42-06-001-001-A01.Jul 8, 2022 · N909XJ · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA2022071401586Former · corrodedCORROSION FOUND ON PAX DOOR FORMER AT FS 329.41 BETWEEN DD5 AND DD6 INTERCOSTALS REMOVED AND INSTALLED A NEW PAX DOOR FORMER AT FS329.41 BETWEEN DD5-DD6 WITH NEW FASTENERS. REF CRJ 900 SRM 51-42-06-001-001-A01.Jul 8, 2022 · N909XJ · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA2022071401585Tie Clip · corrodedCORROSION FOUND ON CLEAT AT JUNCTION OF FS 320 FRAME AND DD4 INTERCOSTAL INSTALLED A NEW CLEAT AT FS320.00 FRAME AND DD4 INTERCOSTAL, P/N 600-31902-269 WITH NEW FASTENERS. REF CRJ 900 SRM 51-42-06-001-001-A01Jul 8, 2022 · N909XJ · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA2022071401584Angle · corrodedCORROSION FOUND ON PAX DOOR STAIR LOWER ANGLE AT MULTIPLE LOCATIONS INSTALLED NEW REPLACEMENT PAX DOOR STAIR LOWER ANGLE. REF CRJ900 SRM 51-42-13-001-001-A01, SRM 51-45-00-001-001-A01Jul 8, 2022 · N909XJ · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA2022071401583Web · corrodedCORROSION FOUND ON PAX DOOR FWD STAIR WEB AT MULTIPLE LOCATIONS REPLACED PAX DOOR FWD STAIR WEB REF CRJ 900 SRM 51--42-06-001-001-A01Jul 8, 2022 · N909XJ · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA2022071401582Web · corrodedCORROSION FOUND ON PAX DOOR AFT STAIR WEB AT MULTIPLE LOCATIONS REPLACED PAX DOOR AFT STAIR WEB WEB REF CRJ900 SRM 51-40-11-001-001-A01Jul 8, 2022 · N909XJ · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA2022071401581Skin · corrodedCORROSION FOUND ON PAX DOOR INNER SKIN AT MULTIPLE LOCATIONS INSTALLED NEW INNER SKIN TO PAX DOOR REF CRJ900 SRM 51-42-06-001-001-A01, SRM 51-42-13-001-001-A01Jul 8, 2022 · N909XJ · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA2022071401580Frame · crackedR/H FORWARD OVER WING EMERGENCY EXIT DOOR HAS A SUSPECTED CRACK IN THE CAST BODY AT THE BASE OF ONE HOOK FITTING, MARKED. COMPLIED WITH FINAL REVISION OF ENDEAVOR EA NO: CRJ952-13562, ISSUE DATE: 5/12/2022,REV -IR. FOR RH FWD OVER WING EMER EXIT DOOR CRACK REPJul 8, 2022 · N909XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2022071401579Frame · crackedL/H FORWARD OVER WING EMERGENCY EXIT DOOR HAS A SUSPECTED CRACK IN THE CAST BODY AT THE BASE OF ONE HOOK FITTING, MARKED. PERFORMED REPAIR AT THE LH OVER WING EMER EXIT DOOR CAST BODY AT HOOK FITTING REF. ENDEAVOR AIR EA NO. CRJ952-13584 REV.IR DATED 5/11/2022Jul 8, 2022 · N909XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
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