# Service difficulty reports: N909XJ

A list on [N909XJ](https://openairdocs.org/aircraft/N909XJ.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 5 · 231 reports

- [SDR REXA2026102001948](https://openairdocs.org/sdr/REXA2026102001948.md): Window Post · cracked · Oct 19, 2026 · N909XJ · Cndair CL6002D24 · Fuselage Main, Structure
  > RT WINDOW SUPPORT STRAP OF THE WINDOW POST FOUND CRACKED. REPLACED RT WINDOW STRAP SUPPORT POST.
- [SDR REXA2026060800943](https://openairdocs.org/sdr/REXA2026060800943.md): Channel · cracked · Jun 4, 2026 · N909XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK 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 51-42
- [SDR REXA2026060400922](https://openairdocs.org/sdr/REXA2026060400922.md): Floor Support · corroded · May 18, 2026 · N909XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION 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-
- [SDR REXA2026060400921](https://openairdocs.org/sdr/REXA2026060400921.md): Support · corroded · May 18, 2026 · N909XJ · 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 CRJ-900 SRM 51-21-06-001-001-A01, EVALUATED SUPPORT P
- [SDR REXA2026060400920](https://openairdocs.org/sdr/REXA2026060400920.md): Support · corroded · May 18, 2026 · N909XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION 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) RB
- [SDR REXA2026060400919](https://openairdocs.org/sdr/REXA2026060400919.md): Landing · cracked · May 18, 2026 · N909XJ · Cndair CL6002D24 · Fuselage Main, Structure
  > CRACKS 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-A01
- [SDR REXA2026060400918](https://openairdocs.org/sdr/REXA2026060400918.md): Hinge · cracked · May 18, 2026 · N909XJ · Cndair CL6002D24 · Wing Main, Frame Structure
  > CRACK 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 IR
- [SDR REXA2026060400912](https://openairdocs.org/sdr/REXA2026060400912.md): Hinge · cracked · May 18, 2026 · N909XJ · Cndair CL6002D24 · Wing Main, Frame Structure
  > CRACK 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 IR
- [SDR REXA2026060400910](https://openairdocs.org/sdr/REXA2026060400910.md): Access Panel · cracked · May 18, 2026 · N909XJ · Cndair CL6002D24 · Engine Thrust Reverser
  > CRACK 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-A01
- [SDR REXA2026060400909](https://openairdocs.org/sdr/REXA2026060400909.md): Access Panel · cracked · May 18, 2026 · N909XJ · Cndair CL6002D24 · Engine Thrust Reverser
  > CRACK 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-A01
- [SDR REXA2026060800942](https://openairdocs.org/sdr/REXA2026060800942.md): Seat Track · corroded · May 10, 2026 · N909XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION 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 53-00-49-400-8
- [SDR REXA2026060400904](https://openairdocs.org/sdr/REXA2026060400904.md): Lug · corroded · May 9, 2026 · N909XJ · Cndair CL6002D24 · Wing, Control Surface Attach Fittings
  > CORROSION 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 - -
- [SDR REXA2026060400903](https://openairdocs.org/sdr/REXA2026060400903.md): Hinge · corroded · May 8, 2026 · N909XJ · Cndair CL6002D24 · Ailerons
  > AFTER 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
- [SDR REXA2026060400933](https://openairdocs.org/sdr/REXA2026060400933.md): Fitting · corroded · May 7, 2026 · N909XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION 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/
- [SDR REXA2026060400908](https://openairdocs.org/sdr/REXA2026060400908.md): Fitting · corroded · May 7, 2026 · N909XJ · Cndair CL6002D24 · Fuselage, Equipment Attach Fittings
  > CORROSION 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. 10
- [SDR REXA2026060400906](https://openairdocs.org/sdr/REXA2026060400906.md): Fitting · corroded · May 7, 2026 · N909XJ · Cndair CL6002D24 · Fuselage, Equipment Attach Fittings
  > CORROSION 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. 10
- [SDR REXA2026060400905](https://openairdocs.org/sdr/REXA2026060400905.md): Fitting · corroded · May 7, 2026 · N909XJ · Cndair CL6002D24 · Fuselage, Equipment Attach Fittings
  > CORROSION 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
- [SDR REXA2026060400917](https://openairdocs.org/sdr/REXA2026060400917.md): Floorbeam · corroded · May 6, 2026 · N909XJ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > CORROSION 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.--
- [SDR REXA2026060400925](https://openairdocs.org/sdr/REXA2026060400925.md): Support Angle · corroded · May 5, 2026 · N909XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION 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.
- [SDR REXA2026060400907](https://openairdocs.org/sdr/REXA2026060400907.md): Support Angle · corroded · May 5, 2026 · N909XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION 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.
- [SDR REXA2026060400931](https://openairdocs.org/sdr/REXA2026060400931.md): Support Bracket · cracked · May 4, 2026 · N909XJ · Cndair CL6002D24 · Engine Thrust Reverser
  > CRACK 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 51-42-06-0
- [SDR REXA2026060400930](https://openairdocs.org/sdr/REXA2026060400930.md): Support Bracket · cracked · May 4, 2026 · N909XJ · Cndair CL6002D24 · Engine Thrust Reverser
  > CRACK 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 51-42-06-0
- [SDR REXA2026060400928](https://openairdocs.org/sdr/REXA2026060400928.md): Angle · cracked · May 4, 2026 · N909XJ · Cndair CL6002D24 · Cargo/Baggage Doors
  > BROKEN 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-A01
- [SDR REXA2026060400916](https://openairdocs.org/sdr/REXA2026060400916.md): Channel · cracked · May 4, 2026 · N909XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK 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. CR
- [SDR REXA2026060400915](https://openairdocs.org/sdr/REXA2026060400915.md): Channel · cracked · May 4, 2026 · N909XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK 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. CR
- [SDR REXA2026060400914](https://openairdocs.org/sdr/REXA2026060400914.md): Retainer · chafed · May 4, 2026 · N909XJ · Cndair CL6002D24 · Cargo/Baggage Doors
  > BENT 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 CR
- [SDR REXA2026060400913](https://openairdocs.org/sdr/REXA2026060400913.md): Retainer · chafed · May 4, 2026 · N909XJ · Cndair CL6002D24 · Cargo/Baggage Doors
  > BENT 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 CR
- [SDR REXA2026060400902](https://openairdocs.org/sdr/REXA2026060400902.md): Skin · chafed · May 4, 2026 · N909XJ · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > WEAR 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.
- [SDR REXA2026060400927](https://openairdocs.org/sdr/REXA2026060400927.md): Drag Angle · cracked · May 3, 2026 · N909XJ · Cndair CL6002D24 · Fuselage, Stabilizer Attach Fittings
  > CRACK 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 AT
- [SDR REXA2026060400926](https://openairdocs.org/sdr/REXA2026060400926.md): Drag Angle · cracked · May 3, 2026 · N909XJ · Cndair CL6002D24 · Fuselage, Stabilizer Attach Fittings
  > CRACK 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
- [SDR REXA2026060400923](https://openairdocs.org/sdr/REXA2026060400923.md): Hinge · corroded · May 3, 2026 · N909XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > "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
- [SDR REXA2025022600226](https://openairdocs.org/sdr/REXA2025022600226.md): Valve · inoperative · Feb 21, 2025 · N909XJ · Cndair CL6002D24 · Landing Gear Retraction/Extension System
  > "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 LAND
- [SDR REXA2025021000178](https://openairdocs.org/sdr/REXA2025021000178.md): Controller · inoperative · Feb 4, 2025 · N909XJ · Cndair CL6002D24 · Windshield/Door Rain/Ice Removal
  > RIGHT 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 POPPED
- [SDR REXA2025012300072](https://openairdocs.org/sdr/REXA2025012300072.md): Selector Valve · inoperative · Jan 21, 2025 · N909XJ · Cndair CL6002D24 · Landing Gear Retraction/Extension System
  > GEAR 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 PERFORM
- [SDR REXA2025011300045](https://openairdocs.org/sdr/REXA2025011300045.md): Engine · damaged · Jan 4, 2025 · N909XJ · Cndair CL6002D24 · Engine (Turbine/Turboprop)
  > ON 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 CONNECTED
- [SDR REXA2022031500260](https://openairdocs.org/sdr/REXA2022031500260.md): Lamp · inoperative · Mar 13, 2023 · N909XJ · Cndair CL6002D24 · Emergency Lighting
  > FWD EMERGENCY FLOOR LIGHT HAS BURNT OUT BULBS R/R BULBS IAW CRJ900 AMM 33-51-11 OPC GOOD P/N OFF/ON 3071BPEGPL
- [SDR REXA2022031000251](https://openairdocs.org/sdr/REXA2022031000251.md): Battery Pack · inoperative · Mar 10, 2023 · N909XJ · Cndair CL6002D24 · Emergency Lighting
  > NOTED 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 16248
- [SDR REXA2022071401591](https://openairdocs.org/sdr/REXA2022071401591.md): Tie Clip · corroded · Jul 8, 2022 · N909XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > CORROSION 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.
- [SDR REXA2022071401590](https://openairdocs.org/sdr/REXA2022071401590.md): Frame · corroded · Jul 8, 2022 · N909XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FRAME 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 IR
- [SDR REXA2022071401589](https://openairdocs.org/sdr/REXA2022071401589.md): Fitting · cracked · Jul 8, 2022 · N909XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX 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-A01
- [SDR REXA2022071401588](https://openairdocs.org/sdr/REXA2022071401588.md): Angle · corroded · Jul 8, 2022 · N909XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX 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.CRJ90
- [SDR REXA2022071401587](https://openairdocs.org/sdr/REXA2022071401587.md): Frame · corroded · Jul 8, 2022 · N909XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > CORROSION 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.
- [SDR REXA2022071401586](https://openairdocs.org/sdr/REXA2022071401586.md): Former · corroded · Jul 8, 2022 · N909XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > CORROSION 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.
- [SDR REXA2022071401585](https://openairdocs.org/sdr/REXA2022071401585.md): Tie Clip · corroded · Jul 8, 2022 · N909XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > CORROSION 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-A01
- [SDR REXA2022071401584](https://openairdocs.org/sdr/REXA2022071401584.md): Angle · corroded · Jul 8, 2022 · N909XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > CORROSION 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-A01
- [SDR REXA2022071401583](https://openairdocs.org/sdr/REXA2022071401583.md): Web · corroded · Jul 8, 2022 · N909XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > CORROSION 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-A01
- [SDR REXA2022071401582](https://openairdocs.org/sdr/REXA2022071401582.md): Web · corroded · Jul 8, 2022 · N909XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > CORROSION 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-A01
- [SDR REXA2022071401581](https://openairdocs.org/sdr/REXA2022071401581.md): Skin · corroded · Jul 8, 2022 · N909XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > CORROSION 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-A01
- [SDR REXA2022071401580](https://openairdocs.org/sdr/REXA2022071401580.md): Frame · cracked · Jul 8, 2022 · N909XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > R/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 REP
- [SDR REXA2022071401579](https://openairdocs.org/sdr/REXA2022071401579.md): Frame · cracked · Jul 8, 2022 · N909XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > L/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 5/11/2022

Next page: https://openairdocs.org/aircraft/N909XJ/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 = 'N909XJ' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N909XJ/reports

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