# Service difficulty reports: N908XJ

A list on [N908XJ](https://openairdocs.org/aircraft/N908XJ.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 · 178 reports

- [SDR REXA2026051200573](https://openairdocs.org/sdr/REXA2026051200573.md): Angle · corroded · Nov 9, 2025 · N908XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > AFTER KICKPLATE ANGLE REMOVAL, CORROSION ON AFT CAP AND MID CAP ANGLE WAS FOUND MID CAP ANGLE WAS REPLACED PER CRJ-900 SRM 51-41-02-001-001-A01, CRJ-900 SRM 51-41-04-001-001-A01 AND AFT CAP WAS INSTALLED UNDER NRC 178 IN REFERENCE TO WIP 14.
- [SDR REXA2026072701113](https://openairdocs.org/sdr/REXA2026072701113.md): Hinge Fitting · corroded · Nov 2, 2025 · N908XJ · Cndair CL6002D24 · Ailerons
  > AFTER RT AILERON BUSHINGS REMOVAL: WEAR AND CORROSION ON ALL HINGE FITTINGS OF RT WING TRAILING EDGE WAS FOUND HINGE FITTINGS OF RT WING TRAILING EDGE WERE CLEANED PER SRM 51-26-00-001-001-A01 PAR 5 B CLEANING AND REPAIRED PER REO 690-57-51-491 REV. --
- [SDR REXA2026072701094](https://openairdocs.org/sdr/REXA2026072701094.md): Hinge · corroded · Nov 2, 2025 · N908XJ · Cndair CL6002D24 · Ailerons
  > AFTER LH AILERON BUSHINGS REMOVAL: WEAR AND CORROSION IN ALL BORE LUGS (L1,L2,L3,L4,L5,L6) AT CENTER HINGE FITTING AND HINGE 4 LUG LOWER OF AILERON WAS FOUND BORE LUGS L1 & L6 WERE CLEANED PER CRJ 900 SRM 51-26-00-001-001-A01 CLEANING, BORE LUGS L2, L3, L4 &
- [SDR REXA2026072701135](https://openairdocs.org/sdr/REXA2026072701135.md): Support · corroded · Oct 31, 2025 · N908XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON SETTLEMENT AREA OF BODY FAIRING SUPPORTS BTW FS881.00 AND FS 847.00. CORROSION ON SEATTLEMENT AREA OF BODY FAIRING SUPPORTS BTW FS881.00 TO FS 847.00 +16.00 WAS REMOVED PER CRJ/900 SRM 51-21-06-001-001-A01 AND WERE EVALUATED WITHIN LIMITS PER CRJ-
- [SDR REXA2026051200570](https://openairdocs.org/sdr/REXA2026051200570.md): Web · cracked · Oct 31, 2025 · N908XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK ON LT ELECTRICAL BAY WEB FLOOR FS 193.00 (BELOW ACCUMULATOR GAUGE INDICATOR) AT FWD EQUIPMENT COMPARTMENT LH ELECTRICAL BAY WEB FLOOR FS 193.00 (BELOW ACCUMULATOR GAUGE INDICATOR) AT FWD EQUIPMENT COMPARTMENT WAS REPAIRED PER EA NO: CRJ953-20697 REV. B A
- [SDR REXA2026051200568](https://openairdocs.org/sdr/REXA2026051200568.md): Channel · corroded · Oct 31, 2025 · N908XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON SUPPORTS OF SETTLEMENT AREA RT AND LT SIDE OF BINS WHEEL CORROSION ON SUPPORTS OF SEATTLEMENT AREA RT AND LT SIDE OF BINS WHEEL WAS REMOVED IAW SRM 51-21-06-001-001-A01 AND EVALUATED WITHIN OF LIMITS IAW SRM 53-00-00-101-001-A01.
- [SDR REXA2026051200558](https://openairdocs.org/sdr/REXA2026051200558.md): Angle · cracked · Oct 31, 2025 · N908XJ · Cndair CL6002D24 · Aerodynamic Fairings
  > CRACK ON WING TO FUSELAGE AFT FAIRING SUPPORT STRUCTURE AT FS849, LBL17'' WING TO FUSELAGE AFT FAIRING SUPPORT STRUCTURE AT FS849, LBL17' WAS REPAIRED PER EA CRJ953-20683 REV. IR
- [SDR REXA2026051200557](https://openairdocs.org/sdr/REXA2026051200557.md): Doubler · cracked · Oct 31, 2025 · N908XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > INITIAL INSPECTION: CRACK ON RH ELECTRICAL BAY FLOOR WEB FS 193.00 (BELOW ADG SUPPORT DOUBLER) AT FWD ACCESORY COMPARTMENT RH ELECTRICAL BAY FLOOR WEB FS 193.00 (BELOW ADG SUPPORT DOUBLER) AT FWD ACCESORY COMPARTMENT WAS FABRICATED PER CRJ-900 SRM-53-11-43-20
- [SDR REXA2026051200556](https://openairdocs.org/sdr/REXA2026051200556.md): Web · corroded · Oct 31, 2025 · N908XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > OUT OF SCOPE': CORROSION AT SERVICE DOOR LOWER SILL, FLOOR PROTECTOR WEBS (4 EAS), LOWER SILL ANGLE, PROTECTOR PLATES & STRIKER SEAL. PROTECTOR PLATES, FLOOR PROTECTOR WEB (2EAS) AND LOWER SILL ANGLE WERE CLEANED AND NOT DAMAGE WAS FOUND PER CRJ900 SRM 51-26-0
- [SDR REXA2026051200555](https://openairdocs.org/sdr/REXA2026051200555.md): Angle · corroded · Oct 31, 2025 · N908XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > OUT OF SCOPE: CORROSION AT SERVICE DOOR LOWER SILL, FLOOR PROTECTOR WEBS (4 EAS), LOWER SILL ANGLE, PROTECTOR PLATES & STRIKER SEAL. PROTECTOR PLATES, FLOOR PROTECTOR WEB (2EAS) AND LOWER SILL ANGLE WERE CLEANED AND NOT DAMAGE WAS FOUND PER CRJ900 SRM 51-26-00
- [SDR REXA2026051200553](https://openairdocs.org/sdr/REXA2026051200553.md): Seat Track · corroded · Oct 31, 2025 · N908XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION AT PASSENGER SEAT TRACK, LBL 9, RBL 9 & LBL 27, BTW 349 TO FS 469.00. (INCLUDED SEAT TRACK FITTING). CORROSION AT PASSENGER SEAT TRACK, LBL 9, RBL 9 & LBL 27, BTW 349 TO FS 469.00. WAS EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-21-49-101-001-A01 THE
- [SDR REXA2026051200551](https://openairdocs.org/sdr/REXA2026051200551.md): Bracket · corroded · Oct 31, 2025 · N908XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON RT & LT MLG HYDRAULIC LINES SUPPORT PLATE (IN BK, LG EXT, LG RET) ON WHEEL WELL AREA, RBL 45/LBL 45. CORROSION ON LH MLG HYDRAULIC LINES SUPPORT PLATE WAS REMOVED AND EVALUATED WITHIN OF LIMITS PER CRJ-900 SRM 51-21-06-001-001-A01, CRJ-900 SRM 53-
- [SDR REXA2026072701133](https://openairdocs.org/sdr/REXA2026072701133.md): Skin · cracked · Oct 30, 2025 · N908XJ · Cndair CL6002D24 · Fuselage Main, Structure
  > CRACK ON AFT UPPER BRACKET AT LH FWD AND AFT OVER WING EMERGENCY-EXIT STRUCTURE. AFT UPPER BRACKET AT LH FWD AND AFT OVERWING EMERGENCY-EXIT STRUCTURE WERE REPAIRED REO 670-52-21-103 REV: --
- [SDR REXA2026072701132](https://openairdocs.org/sdr/REXA2026072701132.md): Bracket · cracked · Oct 30, 2025 · N908XJ · Cndair CL6002D24 · Emergency Exits
  > CRACK ON AFT UPPER BRACKET AT LH FWD AND AFT OVER WING EMERGENCY-EXIT STRUCTURE. AFT UPPER BRACKET AT LH FWD AND AFT OVERWING EMERGENCY-EXIT STRUCTURE WERE REPAIRED REO 670-52-21-103 REV: --
- [SDR REXA202601134](https://openairdocs.org/sdr/REXA202601134.md): Bracket · cracked · Oct 30, 2025 · N908XJ · Cndair CL6002D24 · Emergency Exits
  > CRACK ON AFT UPPER BRACKET AT RH AFT OVERWING EMERGENCY-EXIT STRUCTURE AFT UPPER BRACKET AT RH AFT OVERWING EMERGENCY-EXIT STRUCTURE WERE REPAIRED PER REO 670-52-21-103 REV: REV: --
- [SDR REXA2026051200567](https://openairdocs.org/sdr/REXA2026051200567.md): Angle · cracked · Oct 30, 2025 · N908XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON SILL AND ANGLE KICKPLATE AT PASSENGER DOOR SURROUND. ANGLE KICKPLATE AT PASSENGER DOOR SURROUND WAS REPLACED PER SRM 51-21-06-001-001-A01, SRM 53-21-23-101-001-A02 AND SILL WAS CLEANED PER SRM 51-26-00-001-001-A01 AND NOT DAMAGE WAS FOUND.
- [SDR REXA2026051200541](https://openairdocs.org/sdr/REXA2026051200541.md): Beam · corroded · Oct 30, 2025 · N908XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > SECONDARY NRC FROM NRC 00244 - AFTER PAINT REMOVAL, CORROSION AT TRANSVERSAL BEAM, FS 333.00, BTW BL 0.0 & RBL 27 TRANSVERSAL BEAM, FS 333.00, BTW BL 0.0 & RBL 27 WAS REPAIRED PER EA NO: CRJ953-20738 REV. A
- [SDR REXA2026051200540](https://openairdocs.org/sdr/REXA2026051200540.md): Skin · worn · Oct 30, 2025 · N908XJ · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > WEAR ON EXTERNAL FUSELAGE SKIN FS913.00 TP FS 927.00 BTW STGR 26LH TO STGR 26RH DISTRIBUTION DUCT FS913.00 TP FS 927.00 WAS REMOVED AND INSTALLED PER CRJ-900 AMM 21-23-38, LEAK TEST WAS PERFORMED PER CRJ-900 AMM 21-23-00. WEAR ON EXTERNAL FUSELAGE SKIN FS913.0
- [SDR REXA2026051200564](https://openairdocs.org/sdr/REXA2026051200564.md): Fitting · cracked · Oct 29, 2025 · N908XJ · Cndair CL6002D24 · Fuselage Main, Structure
  > INITIAL INSPECTION: CRACK ON AFT CAM FITTING AT FS. 349.00 FRAME ON PASSENGER DOOR SURROUND STRUCTURE. CAM FITTING AT FS. 349.00 FRAME ON PASSENGER DOOR SURROUND STRUCTURE WAS REPLACED PER CRJ-900 SRM 51-42-21-001-001-A01
- [SDR REXA2026051200539](https://openairdocs.org/sdr/REXA2026051200539.md): Drag Angle · cracked · Oct 29, 2025 · N908XJ · Cndair CL6002D24 · Fuselage, Stabilizer Attach Fittings
  > CRACK ON LH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD & AFT DRAG ANGLE BTW 61.56% STRG DATUM TO 67.5% REAR SPAR DATUM CRACK ON LH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD & AFT DRAG ANGLE BTW 61.56% STRG DATUM TO 67.5% REAR SPAR DATUM
- [SDR REXA2026051200538](https://openairdocs.org/sdr/REXA2026051200538.md): Attach Angle · cracked · Oct 29, 2025 · N908XJ · Cndair CL6002D24 · Fuselage, Stabilizer Attach Fittings
  > CRACK ON RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD & AFT DRAG ANGLE BTW 61.56% STRG DATUM TO 67.5% REAR SPAR DATUM RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 61.56% STRG DATUM TO 67.5% REAR SPAR DATUM WAS REPAIRED PER CRJ-900 SRM
- [SDR REXA2026072701114](https://openairdocs.org/sdr/REXA2026072701114.md): Lug · corroded · Oct 28, 2025 · N908XJ · Cndair CL6002D24 · Wing, Control Surface Attach Fittings
  > WEAR AND CORROSION IN ALL BORE LUGS (R1,R2,R3,R4,R5,R6) AT CENTER HINGE FITTING AND HINGE 4 LUG UPPER OF AILERON WAS FOUND. BORE LUGS R1, R6 & HINGE 4 LUG UPPER WERE CLEANED PER CRJ 900 SRM 51-26-00-001-001-A01 AND NO DAMAGE FOUND. LUGS R3 Y R4 WERE REPAIRED P
- [SDR REXA2026051200559](https://openairdocs.org/sdr/REXA2026051200559.md): Support · cracked · Oct 28, 2025 · N908XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > INTERNAL LOWER ANGLE OF EXTERNAL POWER RECEPTACLE SUPPORT STRUCTURE IINTERNAL LOWER ANGLE OF EXTERNAL POWER RECEPTACLE SUPPORT STRUCTURE WAS REPLACED PER SRM 51-42-06-001-001-A01 AND SRM 51-42-10-001-001-A01 TO GAIN ACCESS EXTERNAL AC POWER RECEPTACLE P/N: MS9
- [SDR REXA2026051200549](https://openairdocs.org/sdr/REXA2026051200549.md): Web · cracked · Oct 28, 2025 · N908XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > PASSENGER DOOR BELOW TOP STEP WEB IS CRACKED ON AFT SIDE TOP STEP WEB ON AFT SIDE OF PASSENGER DOOR WAS REPAIRED PER SRM 52-11-04-201-006-A01
- [SDR REXA2026051200548](https://openairdocs.org/sdr/REXA2026051200548.md): Support · cracked · Oct 28, 2025 · N908XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK ON MAIN LANDING GEAR BINS SUPPORT STRUCTURE RETAINER ANGLE RH (FS 797.00 AND RBL 34). MAIN LANDING GEAR BINS SUPPORT STRUCTURE RETAINER ANGLE RH (FS 797.00 AND RBL 34) WAS REPLACED PER CRJ-900 SRM 51-41-02-001-001-A01
- [SDR REXA2026051200547](https://openairdocs.org/sdr/REXA2026051200547.md): Hinge · cracked · Oct 28, 2025 · N908XJ · Cndair CL6002D24 · Cargo/Baggage Doors
  > CRACK AT FWD / MIDDLE & AFT HINGES OF FLAP STEP PLATE AT AFT BAGGAGE BAY DOOR CUTOUT FWD / MIDDLE & AFT HINGES OF FLAP STEP PLATE AT AFT BAGGAGE BAY DOOR CUTOUT WERE REMPLACED PER CRJ-900 SRM 51-42-06-001-001-A01.
- [SDR REXA2026051200546](https://openairdocs.org/sdr/REXA2026051200546.md): Hinge · cracked · Oct 28, 2025 · N908XJ · Cndair CL6002D24 · Cargo/Baggage Doors
  > CRACK AT FWD / MIDDLE & AFT HINGES OF FLAP STEP PLATE AT AFT BAGGAGE BAY DOOR CUTOUT FWD / MIDDLE & AFT HINGES OF FLAP STEP PLATE AT AFT BAGGAGE BAY DOOR CUTOUT WERE REMPLACED PER CRJ-900 SRM 51-42-06-001-001-A01
- [SDR REXA2026051200545](https://openairdocs.org/sdr/REXA2026051200545.md): Hinge · cracked · Oct 28, 2025 · N908XJ · Cndair CL6002D24 · Cargo/Baggage Doors
  > CRACK AT FWD / MIDDLE & AFT HINGES OF FLAP STEP PLATE AT AFT BAGGAGE BAY DOOR CUTOUT FWD / MIDDLE & AFT HINGES OF FLAP STEP PLATE AT AFT BAGGAGE BAY DOOR CUTOUT WERE REMPLACED PER CRJ-900 SRM 51-42-06-001-001-A01
- [SDR REXA2026051200544](https://openairdocs.org/sdr/REXA2026051200544.md): Stop · cracked · Oct 28, 2025 · N908XJ · Cndair CL6002D24 · Cargo/Baggage Doors
  > BROKEN STOPPERS 2 EAS OF FLAP STEP PLATE AT AFT BAGGAGE BAY DOOR CUTOUT STOPPERS 2 EAS OF FLAP STEP PLATE AT AFT BAGGAGE BAY DOOR CUTOUT WERE REPAIRED PER EA NO. CRJ953-20779 REV. IR AND EA NO. CRJ953-20769 REV. IR
- [SDR REXA2026051200543](https://openairdocs.org/sdr/REXA2026051200543.md): Stop · cracked · Oct 28, 2025 · N908XJ · Cndair CL6002D24 · Cargo/Baggage Doors
  > BROKEN STOPPERS 2 EAS OF FLAP STEP PLATE AT AFT BAGGAGE BAY DOOR CUTOUT STOPPERS 2 EAS OF FLAP STEP PLATE AT AFT BAGGAGE BAY DOOR CUTOUT WERE REPAIRED PER EA NO. CRJ953-20779 REV. IR AND EA NO. CRJ953-20769 REV. IR
- [SDR REXA2026051200542](https://openairdocs.org/sdr/REXA2026051200542.md): Attach Angle · cracked · Oct 28, 2025 · N908XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > CRACK ON ATTACHMENT ANGLE INNER SKIN-TO-AFT SIDE PANEL AT PASSENGER DOOR EXTERNAL STRUCTURE ANGLE INNER SKIN-TO-AFT SIDE PANEL AT PASSENGER DOOR EXTERNAL STRUCTURE WAS REPAIRED PER CRJ-900 SRM 52-11-04-201-002-A01
- [SDR REXA2024123001621](https://openairdocs.org/sdr/REXA2024123001621.md): Battery Pack · inoperative · Dec 29, 2024 · N908XJ · Cndair CL6002D24 · Emergency Lighting
  > MULTIPLE EMERGENCY LIGHTS INOP NEAR FWD LH AND RH EMERGENCY EXITS R/R EPSU #5 PS43 IAW AMM 33-51-17 OPS CHECK GOOD PN ON/OFF 2013-1ASMI SN OFF 19038 SN ON 19242
- [SDR REXA2024041900358](https://openairdocs.org/sdr/REXA2024041900358.md): Controller · failed · Apr 14, 2024 · N908XJ · Cndair CL6002D24 · Windshield/Door Rain/Ice Removal
  > LEFT WINDSHIELD CONTROLLER PRODUCED ELECTRICAL SMELL AND SMOKE. INSPECTED LEFT HAND WINDSHIELD, NO DAMAGE TO STRUCTURE REF AMM 56-11-01. DEFERRED LEFT WINDSHIELD HEAT MEL 30-41-01A MX PROCEDURE C/W MOC NOTIFIED 7821 PLACARD INSTALLED**REMOVED AND REPLACED LH
- [SDR REXA2022060901086](https://openairdocs.org/sdr/REXA2022060901086.md): Power Supply · discharged · Jun 6, 2022 · N908XJ · Cndair CL6002D24 · Emergency Lighting
  > FOUND EMER LIGHT AT FWD CABIN INOP. REMOVED AND REPLACED EMER LIGHT BATT PS35 IAW AMM 33-51-17. OPS CHECK GOOD.
- [SDR REXA2022051800968](https://openairdocs.org/sdr/REXA2022051800968.md): Frame · corroded · May 16, 2022 · N908XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FRAME FS 954.00 IS CORRODED BETWEEN STGR 26L AND 25R. REMOVED AND INSTALLED FS954.00. FRAME SECTOR FROM STRINGER 25L TO STRINGER 25R REF. CRJ900 SRM 51-42-06-001-001-A01 AND ENDEAVOR AIR EA CRJ953-13485 DATED 4/30/2022 REV IR.
- [SDR REXA2022051800967](https://openairdocs.org/sdr/REXA2022051800967.md): Frame · corroded · May 16, 2022 · N908XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FRAME AT FS 942.00 BETWEEN STGR 22R AND 26L IS CORRODED. COMPLIED WITH EA CRJ953-13484 DATED 4/30/2022 REV IR REPAIRED/REPLACED FS942 FRAME STR 20R-STR 25L
- [SDR REXA2022051800966](https://openairdocs.org/sdr/REXA2022051800966.md): Frame · corroded · May 16, 2022 · N908XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR FORWARD FORMER HAS CORROSION ON ITS INTERIOR SIDE AT THE LOWER LATCH CAM AREA REPLACED CORRODED PAX DOOR FWD FORMER WITH NEW REPLACEMENT FORMER (PN 601R318031-5S) USING ALL NEW FASTENERS. REF BOMBARDIER DWG#601R31702 REV N AND CRJ900 SRM 51-42-06-001-
- [SDR REXA2022051800948](https://openairdocs.org/sdr/REXA2022051800948.md): Frame · corroded · May 11, 2022 · N908XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FRAME FS501.00 LOWER FLANGE AND WEB ARE CORRODED STGR24L-26L REPLACED WITH NEW FRAME SECTOR AT FS-501 BETWEEN STGR 25L AND STGR 19L REF CRJ900 SRM 51-42-06-001-001-A01, CRJ900 SRM 51-42-20-001-001-A01 AND DWG. NO. SH690-33750 REV Y.
- [SDR REXA2022051800947](https://openairdocs.org/sdr/REXA2022051800947.md): Angle · corroded · May 11, 2022 · N908XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > LEFT MAIN LANDING GEAR WHEEL WELL FORWARD ATTACH ANGLE FOR 542AZ IS CORRODED. REMOVED UNSERVICEABLE AND INSTALLED NEW RIGHT MAIN LANDING GEAR WHEEL WELL FORWARD. ATTACH ANGLE FOR 542AZ. REF CRJ900 SRM 51-42-21-001-001-A01, LEAK CHECK GOOD.
- [SDR REXA2022051800946](https://openairdocs.org/sdr/REXA2022051800946.md): Angle · corroded · May 11, 2022 · N908XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > RIGHT MAIN LANDING GEAR WHEEL WELL FORWARD ATTACH ANGLE FOR 642AZ IS CORRODED. REMOVED UNSERVICEABLE AND INSTALLED NEW RIGHT MAIN LANDING GEAR WHEEL WELL FORWARD. ATTACH ANGLE FOR 642AZ. REF CRJ900 SRM 51-42-21-001-001-A01, LEAK CHECK GOOD.
- [SDR REXA2022051800951](https://openairdocs.org/sdr/REXA2022051800951.md): Stringer · corroded · Apr 29, 2022 · N908XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > STRINGER 25R REPLACMENT FS280-FS333 DUE TO HEAVY CORROSION DAMAGE. COMPLIED WITH REPLACEMENT OF THE STRINGER 25R FROM FS280 TO FS333 REF ENGINEERING AUTHORIZATION CRJ953-13383, DATED 4/16/2022
- [SDR REXA2022051800952](https://openairdocs.org/sdr/REXA2022051800952.md): Piston · corroded · Apr 14, 2022 · N908XJ · Cndair CL6002D24 · Main Landing Gear
  > LH MAIN LANDING GEAR HAS MINOR CORROSION AND MISSING FINISH AT #2 AXLE ROOT RADIUS. ATTACHED GENERIC REO 670-32-11-361 REV-DATED 2014-07-30 ROUTINELY USED TO REPAIR THIS DAMAGE. COMPLIED WITH THE REPAIR ON LH MLG PISTON AXLE #2 REF REO 670-32-11-361 REV A, DA
- [SDR REXA2022051800950](https://openairdocs.org/sdr/REXA2022051800950.md): Intercostal · corroded · Apr 14, 2022 · N908XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > INTERCOSTAL 20R HAS CORROSION. AFT OF FS 379.00. REPLACED INTERCOSTAL 20R LOCATED AT FS319 TO FS349 REF CRJ900 SRM 51-42-06-01-001-001-A01, CRJ900 SRM 51-42-21-001-001-A01, DWG #SH670-31950 REV Y
- [SDR REXA2022051800949](https://openairdocs.org/sdr/REXA2022051800949.md): Intercostal · corroded · Apr 14, 2022 · N908XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > INTERCOSTAL 20R HAS CORROSION. FORWARD OF FS 379.00. REPLACED INTERCOSTAL 20R LOCATED AT FS310 TO FS319 REF CRJ900 SRM 51-42-06-001-001-A01, CRJ900 SRM 51-42-21-001-001-A01 DWG #SH670-31950 REV Y.
- [SDR REXA2019021100140](https://openairdocs.org/sdr/REXA2019021100140.md): Wire · burned · Feb 11, 2019 · N908XJ · Cndair CL6002D24 · Window System Wiring
  > ONCE IN FLIGHT GOT A STRONG SMELL OF FUMES IN FLIGHT DECK. WAS AN ELECTRIC BURNING SMELL. DECIDED IT WAS TO STRONG AND DIVERTED BACK TO JFK. T/S AND FOUND LT WINDOW WIRES P1/P2 BURNED, R&R P1&P2 TERMINALS IAW ESPM 20-16-00. R&R LT WINDOW IAW JC 900-56-900-902,
- [SDR REXA2018080870677](https://openairdocs.org/sdr/REXA2018080870677.md): Oxygen Mask · broken · Aug 7, 2018 · N908XJ · Cndair CL6002D24 · Crew Oxygen System
  > CAPTAIN`S SIDE OXYGEN MASK, RED TAB WAS BROKEN. R & R THE OXYGEN MASK IAW AMM 33-25-03, OPS CHECKED GOOD.
- [SDR REXA2018072400641](https://openairdocs.org/sdr/REXA2018072400641.md): Light · worn · Jul 19, 2018 · N908XJ · Cndair CL6002D24 · Emergency Lighting
  > EMERGENCY PATH LIGHTING STRIPS IN FRONT OF WARDROBE AND FWD LAV ARE WORN. REMOVED AND REPLACED EPL WARDROBE AND FWD LAV IAW AMM 33-51-01-000-801 A021 AND 33-51-01-400-801-A021.
- [SDR REXA2018072400639](https://openairdocs.org/sdr/REXA2018072400639.md): Angle · cracked · Jul 12, 2018 · N908XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > MAIN ENTRY DOOR HAS A CRACKED ANGLE AFT SIDE FWD OF DOOR ASSIST SWIVEL PULLEY. REMOVED AND REPLACED AFT ANGLE ON MAIN ENTRY DOOR ASSIST SWIVEL PULLEY IAW SRM 52-11-04.
- [SDR REXA2018072400640](https://openairdocs.org/sdr/REXA2018072400640.md): Lens · cracked · Jul 10, 2018 · N908XJ · Cndair CL6002D24 · Emergency Lighting
  > PANEL ABOVR SERVICE DOOR EMERGENGY LIGHT LENS CRACKED. REMOVED AND REPLACED NEW LIGHT LENS AT PANEL ABOVE SERVICES DOOR AS REQUIRED WITH LIGHT HAND PRESSURE.
- [SDR REXA2018072400638](https://openairdocs.org/sdr/REXA2018072400638.md): Floorbeam · corroded · Jul 8, 2018 · N908XJ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > WHILE REMOVING FWD FLIGHT DECK FLOOR SUPPORT FOUND RT 280 FLOORBEAM CORRODED. REMOVED DAMAGED FS280 RT FLOOR SUPPORT BEAM & INSTALLED NEW BEAM IAW SRM 51-42-06, 51-42-13, 51-42-21.

Next page: https://openairdocs.org/aircraft/N908XJ/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 = 'N908XJ' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N908XJ/reports

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