# Service difficulty reports: N923XJ

A list on [N923XJ](https://openairdocs.org/aircraft/N923XJ.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 · 203 reports

- [SDR REXA2026080701533](https://openairdocs.org/sdr/REXA2026080701533.md): Floorbeam · cracked · Aug 5, 2026 · N923XJ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > THE RH FS 280 FLOOR BEAM IS CORRODED AND PITTED AND WILL REQUIRE REPLACEMENT. REMOVED DAMAGED RH FS 280.00 CROSSBEAM IAW CRJ900 SRM 51-42-06-001-001-A01. CRJ900 SRM 51-42-13-001-001-A01. AND CRJ900 SRM 51-42-22-001-001-A01. INSTALLED NEW RH FS 280.00 CROSSBEA
- [SDR REXA2026080701532](https://openairdocs.org/sdr/REXA2026080701532.md): Floorbeam · cracked · Aug 5, 2026 · N923XJ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > THE LH FS 280 FLOORBEAM IS CORRODED AND PITTING AND WILL REQUIRE REPLACEMENT. REMOVED DAMAGED LH FS 280.00 CROSSBEAM IAW CRJ900 SRM 51-42-06-001-001-A01. CRJ900 SRM 51-42-13-001-001-A01. AND CRJ900 SRM 51-42-22-001-001-A01. INSTALLED NEW LH FS 280.00 CROSSBEA
- [SDR REXA2026072201085](https://openairdocs.org/sdr/REXA2026072201085.md): Lug · damaged · Jul 20, 2026 · N923XJ · Cndair CL6002D24 · Wing, Control Surface Attach Fittings
  > WHILE RPLACING BUSHINGS IN LT AILERON FOUND LUGS MARKED AS B, C, F, AND G TO BE OVERSIZED. COMPLIED WITH BOMBARDIER REO 670-57-61-237 REV --.
- [SDR REXA2026072201082](https://openairdocs.org/sdr/REXA2026072201082.md): Lug · damaged · Jul 20, 2026 · N923XJ · Cndair CL6002D24 · Wing, Control Surface Attach Fittings
  > WHILE RPLACING BUSHINGS IN RT AILERON, FOUND LUGS B, C, F, AND G TO BE OVERSIZED. COMPLIED WITH BOMBARDIER REO 670-57-61-237 REV -- DATED 2017-07-25.
- [SDR REXA2026072001080](https://openairdocs.org/sdr/REXA2026072001080.md): Door · cracked · Jul 13, 2026 · N923XJ · Cndair CL6002D24 · Emergency Exits
  > THE RT FWD OVERWING EMERGENCY EXIT IS CRACKED AROUND THE PROX SENSOR TARGET LUG. COMPLIED WITH ALL STEPS OF REO 670-52-21-103 REV -. FOR THE REPAIR TO THE RH FWD OVERWING EMERGENCY EXIT LUG.
- [SDR REXA2026072001079](https://openairdocs.org/sdr/REXA2026072001079.md): Floorbeam · cracked · Jul 13, 2026 · N923XJ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > THE RT COCKPIT FLOORBEAM IS CRACKED ON THE AFT FLANGE IN A PREVIOUSLY REPAIRED AREA. COMPLIED WITH JOB SET-UP & FUSELAGE SHORING AT FS250.00 IAW STEPS 1 THRU 6F OF SRM 53-11-43-201-003-A01. LOCATED, DRILLED & TRIMMED TO FIT NEW RT COCKPIT FLOORBEAM. SEGMENT BE
- [SDR REXA2026080401482](https://openairdocs.org/sdr/REXA2026080401482.md): Window Frame · damaged · Jul 12, 2026 · N923XJ · Cndair CL6002D24 · Fuselage Main, Structure
  > DURING INSPECTION OF LT WINDSHIELD STRUCTURE FOR INSTALL OF LT WINDSHIELD, FOUND 3 ELONGATED HOLES. NO LIMITS NOTED IN SRM HOLE MEASUREMENTS ARE.372.353.323. COMPLIED WITH STEP 1 AND 3 IAW REO 690-53-11-2232, REV. --(P2). COMPLIED WITH ALL STEPS OF REO 690
- [SDR REXA2026071001073](https://openairdocs.org/sdr/REXA2026071001073.md): Floorbeam · corroded · Jun 21, 2026 · N923XJ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > BS 280 FORWARD J ANGLE IS HEAVILY CORRODED AND REQUIRES REPLACEMENT. BS 280 FORWARD J ANGLE IS HEAVILY CORRODED & REQUIRES REPLACEMENT. REMOVED UNSERVICEABLE FWD J ANGLE IAW SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01. LOCATED & DRILLED NEW BS 28
- [SDR REXA2022071200490](https://openairdocs.org/sdr/REXA2022071200490.md): Fitting · damaged · Jul 11, 2023 · N923XJ · Cndair CL6002D24 · Fuselage Structure (General)
  > WHILE PERFORMING SB 670BA-53-044 REVISION G DATED JUL 05/2022 PART B FOUND LH STR12 FITTING PN CC670-33563-001SB CANNOT BE INSTALLED IN ACCORDANCE WITH SERVICE BULLETIN INSTRUCTIONS DUE TO LOW EDGE DISTANCE AT FASTENER GOING THROUGH FITTING AND BULKHEAD AND TH
- [SDR REXA2022082800702](https://openairdocs.org/sdr/REXA2022082800702.md): Fitting · deformed · Jun 29, 2023 · N923XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > WHILE PERFORMING SB 670BA-53-044 REVISION G DATED JUL 05/2022 PART B FOUND RH STR12 FITTING PN CC670-33562-001SB CANNOT BE INSTALLED IN ACCORDANCE WITH SERVICE BULLETIN INSTRUCTIONS DUE TO LOW EDGE DISTANCE AT 2 FASTENERS GOING THROUGH FITTING AND CANNOT PICK
- [SDR REXA2022122802726](https://openairdocs.org/sdr/REXA2022122802726.md): Support · corroded · Dec 28, 2022 · N923XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FWD JACK FITTING RT SUPPORT IS CORRODED. REPAIRED RT SUPPORT AT FWD JACK FITTING IAW MHIRJ REO 690-53-11-1505 REV-.
- [SDR REXA2022010600014](https://openairdocs.org/sdr/REXA2022010600014.md): Seat Track · corroded · Dec 23, 2022 · N923XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > R/H #2 SIDE SEAT TRACK FROM FS 485 TO FS 570 HAS CORROSION BEYOND LIMITS REMOVED AND REPLACED R/H #2 SIDE SEAT TRACK FROM FS 485 TO FS 570 IAW MHIRJ REO 670-53-00-587 REV -B DATE 08/16/2022 HAS BEEN ATTACHED.
- [SDR REXA2022010600012](https://openairdocs.org/sdr/REXA2022010600012.md): Seat Track · corroded · Dec 23, 2022 · N923XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK IS CORRODED BEYOND LIMITS AT FS 839 TO 847+48 RBL 9 ROMVED AND REPLACED SEAT TRACK AT FS 839 TO 847+48 RBL 9 IAW MHIRJ REO 670-53-00-589 REV -B DATED 2022-08-18.
- [SDR REXA2022121502709](https://openairdocs.org/sdr/REXA2022121502709.md): Stringer · corroded · Dec 14, 2022 · N923XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER 24R IS CORRODED BETWEEN FS 421.00 AND 453.00 REMOVED CORRODED STRINGER, INSTALLED NEW SERVICABLE STRINGER 24R BETWEEN FS 333 AND FS 477 IAW CRJ900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01
- [SDR REXA2022121502708](https://openairdocs.org/sdr/REXA2022121502708.md): Intercostal · corroded · Dec 14, 2022 · N923XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > INTERCOSTAL AT STGR 20R, BETWEEN F.S.349 TO F.S.364, IS CORRODED. REPLACED INTERCOSTAL ON FS 20R BETWEEN FS 349-364 IAW CRJ 900 SRM 51-42-06-001-001-A01
- [SDR REXA2022121502707](https://openairdocs.org/sdr/REXA2022121502707.md): Stringer Clip · corroded · Dec 14, 2022 · N923XJ · Cndair CL6002D24 · Fuselage Main, Attach Fittings
  > STGR 22R, F.S.319.70 STRINGER CLIP IS CORRODED. REMOVED CORRODED CLEAT AND INSTALLED NEW CLEAT IAW CRJ900 SRM 51-42-06-001-001-A01. P/N SH670-35625-1
- [SDR REXA2022121502706](https://openairdocs.org/sdr/REXA2022121502706.md): Frame · corroded · Dec 14, 2022 · N923XJ · Cndair CL6002D24 · Fuselage Main, Frame
  > FRAME 927 BETWEEN STGR 26L - STGR 25R HAS CORROSION. REPAIRED FRAME F.S.927 BETWEEN STGR 26L TO 25R IAW CRJ 900 SRM 53-00-06-201-001-A03.
- [SDR REXA2022121302698](https://openairdocs.org/sdr/REXA2022121302698.md): Stringer Splice · corroded · Dec 11, 2022 · N923XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER 19R SPLICE CORRODED AT BS 487. LOCATED AND DRILLED A NEW STRINGER SPLICE IAW SRM 51-40-11-001-001-A01.
- [SDR REXA2022120702688](https://openairdocs.org/sdr/REXA2022120702688.md): Stringer · corroded · Dec 6, 2022 · N923XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER 21L IS CORRODED BETWEEN FS 364.00 AND 394.00 REPAIRED STRINGER 21L. REPLACED STRINGER SPLICE IAW SRM 53-00-03-201-001-A02.
- [SDR REXA2022120702687](https://openairdocs.org/sdr/REXA2022120702687.md): Seat Track · corroded · Dec 6, 2022 · N923XJ · Cndair CL6002D24 · Fuselage Main, Frame
  > FS 942.00 FRAME IS CORRODED BETWEEN STRINGER 25R AND 26R. REPAIRED LOWER FUSLEGE FRAME IAW SRM SRM 53-00-06-201-001-A03.
- [SDR REXA2022120702685](https://openairdocs.org/sdr/REXA2022120702685.md): Fitting · cracked · Dec 6, 2022 · N923XJ · Cndair CL6002D24 · Emergency Exits
  > L/H FWD OVER WING EMERGENCY EXIT DOOR TOP AFT FITTING IS CRACKED. REPAIRED L/H FWD OVER WING EMERGENCY EXIT DOOR(SB0726) TOP UPPER MEMBER IAW REO 690-52-21-123 REV -.
- [SDR REXA2022120602681](https://openairdocs.org/sdr/REXA2022120602681.md): Stringer · corroded · Dec 6, 2022 · N923XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER 26R IS CORRODED BETWEEN FS 333.00 AND 349.00 REPLACED THE AFT STRINGER IAW SRM 51-42-06-001-001-A01.
- [SDR REXA2022121902718](https://openairdocs.org/sdr/REXA2022121902718.md): Stringer · corroded · Dec 3, 2022 · N923XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER 24R IS CORRODED BEYOND LIMITS BETWEEN FS 280 AND FS 310 REMOVED AND REPLACED STRINGER 24R BETWEEN FS 280 AND FS 310
- [SDR REXA2022121202697](https://openairdocs.org/sdr/REXA2022121202697.md): Stringer · corroded · Dec 3, 2022 · N923XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER 22R BETWEEN FS 333 AND FS 349 IS CORRODED. REMOVED STGR 22R BETWEEN FS 333 AND FS 349 IAW CRJ900 SRM 51-42-06-001-001-A01, AND INSTALLED NEW STGR 22R P/N: SH670-31379-1S IAW CRJ900 SRM 51-42-06-001-001-A01.
- [SDR REXA2022120702691](https://openairdocs.org/sdr/REXA2022120702691.md): Diaphragm · corroded · Dec 1, 2022 · N923XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > WATER WASTE DOOR SURROUND LOWER DIAPHRAGM P/N SH670-32284-3 CORRODED ON OUTER SURFACE BETWEEN BS 379 & 394; S23R. INSTALLED A NEW LOWER DIAPHRAGM IAW SRM 51-42-06-001-001-A01.
- [SDR REXA2022120102665](https://openairdocs.org/sdr/REXA2022120102665.md): Floorbeam · cracked · Nov 30, 2022 · N923XJ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > CKPT FLOOR PANEL 221ALF, LBL 12 AND RBL 12 SUPPORT ANGLES CRACKED JUST FORWARD OF FS280.00. REMOVED AND REPLACED SUPPORT ANGLES AT FS280 LBL 12 AND RBL 12 IAW CRJ900 SRM TASKS 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.
- [SDR REXA2022120102664](https://openairdocs.org/sdr/REXA2022120102664.md): Floorbeam · corroded · Nov 30, 2022 · N923XJ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > CKPT FLOOR PANEL 221ALF, LBL 12 AND RBL 12 SUPPORT ANGLES CRACKED JUST FORWARD OF FS280.00. REMOVED AND REPLACED SUPPORT ANGLES AT FS280 LBL 12 AND RBL 12 IAW CRJ900 SRM TASKS 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.
- [SDR REXA2022120102656](https://openairdocs.org/sdr/REXA2022120102656.md): Stringer · corroded · Nov 30, 2022 · N923XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER 22L IS CORRODED BETWEEN FS 501.00 AND 517.00 REMOVED AND REPLACED STRINGER 22L BETWEEN FS477 AND FS517 IAW CRJ900 SRM TASKS 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.
- [SDR REXA2022120102644](https://openairdocs.org/sdr/REXA2022120102644.md): Floorbeam · corroded · Nov 30, 2022 · N923XJ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > RH FS 280 FLOORBEAM FOUND TO BE CORRODED. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-42-06-001-001-AO1,51-42-13-001-001-AO1, 51-42-21-001-001-AO1.
- [SDR REXA2022120102643](https://openairdocs.org/sdr/REXA2022120102643.md): Bulkhead Web · corroded · Nov 30, 2022 · N923XJ · Cndair CL6002D24 · Fuselage Main, Bulkhead
  > FS 280 BULKHEAD WEB IS CORRODED BETWEEN LBL9 TO LBL12. REMOVED LH BULKHEAD WEB AT FS 280 IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01, AND 51-42-21-001-001-A01 FABRICATED, LOCATED AND DRILLED NEW LH BULKHEAD LWR WEB AT FS 280 IAW CRJ 900 SRM 51-2
- [SDR REXA2022120102641](https://openairdocs.org/sdr/REXA2022120102641.md): Floor Support · corroded · Nov 30, 2022 · N923XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > R/H FLOOR SILL FROM F.S.280 TO F.S.295 IS CORRODED. COMPLIED WITH CRJ-900 SRM 53-00-45-201-001-A01.
- [SDR REXA2022121902716](https://openairdocs.org/sdr/REXA2022121902716.md): Seat Track · corroded · Nov 29, 2022 · N923XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > RH SIDE SEAT RAIL FS 847+16 - FS 865 HAS CORROSION REMOVED UNSERVICEABLE RH SIDE SEAT RAIL LOCATED AT FS 847+16 - FS 865 IAW CRJ900 AMM 53-00-49-000-801-A19. FABRICATED AND INSTALLED NEW SERVICEABLE RH SIDE SEAT RAIL LOCATED AT FS 847+16 IAW REO 670-53-00-587
- [SDR REXA2022121902714](https://openairdocs.org/sdr/REXA2022121902714.md): Seat Track · corroded · Nov 29, 2022 · N923XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > R/H SIDE SEAT TRACK #3 FROM FS 570 TO FS 661+14 HAS CORROSION BEYOND LIMITS REMOVED AND REPLACED SIDE SEAT RAIL FROM FS 570 TO 661+14 IAW CRJ 900 SRM 53-00-49-400-801(A19)
- [SDR REXA2022010600013](https://openairdocs.org/sdr/REXA2022010600013.md): Frame · corroded · Nov 28, 2022 · N923XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FOUND CORROSION BEYOND LIMITS ON AFT SIDE OF FRAME F.S.379 BETWEEN STGR 20R AND 22R. REMOVED AND REPLACED FRAME 379 BETWEEN STRINGER 20R - 25R IAW CRJ-900 SRM 51-42-06-001-001-A01
- [SDR REXA2022120102663](https://openairdocs.org/sdr/REXA2022120102663.md): Channel · corroded · Nov 28, 2022 · N923XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > WHILE WORKING JOB 81517735 OP 6002 FOUND DOUBLER/CHANNEL P/N MM670-43255-001 TO BE CORRODED AT STGR 27 BETWEEN FS 1031.00 AND 1047.00. REQUIRES REPLACEMENT REMOVED/INSTALLED NEW DRAIN MAST CHANNEL IAW CRJ 900 SRM 51-42-06-001-001-A01
- [SDR REXA2022120102657](https://openairdocs.org/sdr/REXA2022120102657.md): Floor Support · corroded · Nov 28, 2022 · N923XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT AT RBL 9 HAS MULTIPLE SPOTS OF CORROSION FROM FS 1000 TO FS 1088. REPAIRED FLOOR SUPPORT AT RBL 9 BETWEEN FS 1000.00 AND FS 1088.00 IAW REO 690-53-61-1151.
- [SDR REXA2022120102655](https://openairdocs.org/sdr/REXA2022120102655.md): Floor Support · corroded · Nov 28, 2022 · N923XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > LH FLOOR SILL HAS MULTIPLE SPOTS OF CORROSION FROM FS 985 TO FS 1000 REPAIRED LH FLOOR SILL FS 985 TO FS 1000 IAW MHIRJ REO 690-53-61-1147 REV-- DATED 2022-11-23
- [SDR REXA2022120102654](https://openairdocs.org/sdr/REXA2022120102654.md): Skin · chafed · Nov 28, 2022 · N923XJ · Cndair CL6002D24 · Trailing Edge Flaps
  > FLAP PANEL 584JB HAS CHAFE ON L/E CHAFED OUT OF LIMITS REPLACED PANEL 584JB P/N CC670-14178-1 LOCATED HOLES, TRIMMED EDGE. ALODINED, PRIMED, AND PAINTED IAW CRJ900 SRM 51-21-11-001-001-A01, 51-25-06-001-001-A01, AND 51-25-06-001-001-A01
- [SDR REXA2022120102653](https://openairdocs.org/sdr/REXA2022120102653.md): Skin · chafed · Nov 28, 2022 · N923XJ · Cndair CL6002D24 · Ailerons
  > L/H WING/AILERON PANEL 599AB IS CHAFED. REMOVED CHAFE DAMAGE IAW CRJ-900 SRM 51-12-00-001-001-A01. UPON FURTHER INVESTIGATION, DAMAGE MEASUREMENTS ARE OUT OF LIMITS IAW CRJ-900 SRM 57-61-01-101-001-A01. ORIGINAL THICKNESS: 0.100" MAX MATERIAL REMOVED: 0.075" M
- [SDR REXA2022120102610](https://openairdocs.org/sdr/REXA2022120102610.md): Stringer · corroded · Nov 28, 2022 · N923XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER 23R IS CORRODED BETWEEN FS 661+74 AND 677.00. REMOVED, FABERCATED, AND INSTALL STRINGER 23R BETWEEN FS 661+74 AND 677.00 IAW CRJ 900 SRM 53-00-03-201-001-A02
- [SDR REXA2022120102608](https://openairdocs.org/sdr/REXA2022120102608.md): Plate · corroded · Nov 28, 2022 · N923XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > PLATE JOINT AT STRINGER 26L FS 629.00 IS CORRODED. INSTALLED NEW PLATE JOINT P/N SH670-33793-4 ON STRINGER 26L FS 629.00 IAW CRJ 900 SRM 51-42-27--001-A01.
- [SDR REXA2022120802693](https://openairdocs.org/sdr/REXA2022120802693.md): Stringer · corroded · Nov 23, 2022 · N923XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER 22R IS CORRODED BEYOND LIMITS BETWEEN FS280 AND 295 REMOVED AND REPLACED STRINGER 22R BETWEEN FS280 AND 295
- [SDR REXA2022120702690](https://openairdocs.org/sdr/REXA2022120702690.md): Stringer · corroded · Nov 23, 2022 · N923XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER 21R HEAVILY CORRODED JUST AFT OF FS319.70 INSTALLED NEW STRINGER BETWEEN BS 280 - 333 IAW SRM 51-42-06-001-001-A01, & 51-42-21-001-001-A01.
- [SDR REXA2022120102618](https://openairdocs.org/sdr/REXA2022120102618.md): Floorbeam · corroded · Nov 23, 2022 · N923XJ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > FLOORBEAM AT F.S.280 ON LEFT SIDE IS CORRODED. REMOVED AND REPLACED LEFT F.S.280 FLOORBEAM.
- [SDR REXA2022120102616](https://openairdocs.org/sdr/REXA2022120102616.md): Stringer · corroded · Nov 23, 2022 · N923XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > STRINGER 22L FROM F.S.333 TO F.S.349 IS CORRODED. REPAIRED STRINGER 22L
- [SDR REXA2022120102607](https://openairdocs.org/sdr/REXA2022120102607.md): Floorbeam · corroded · Nov 23, 2022 · N923XJ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > FLOOR BEAM AT RBL 27 HAS MULTIPLE SPOTS OF CORROSION FROM F.S.1000 TO F.S.1088. REPAIRED RBL 27 FLOOR BEAM IAW MHIRJ REO 690-53-61-1150
- [SDR REXA2022120702689](https://openairdocs.org/sdr/REXA2022120702689.md): Angle · corroded · Nov 20, 2022 · N923XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR C ANGLE AT INTERCOSTAL DD7 A FOUNT TO BE CORRODED LOCATED AND DRILLED NEW C ANGLE IAW CRJ 900 SRM 51-40-11-001-001-A01. INSTALLED NEW C ANGLE IAW SRM 51-42-21-001-001-A01.
- [SDR REXA2022112102592](https://openairdocs.org/sdr/REXA2022112102592.md): Bracket · corroded · Nov 20, 2022 · N923XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR BRACKET ON FWD INTERCOSTAL DD4 FOUND TO BE CORRODED. REMOVED PAX DOOR BRACKET ON FWD INTERCOSTAL DD4 IAW CRJ900 SRM 51-42-06-001-001-A01. LOCATED AND DRILLED NEW BRACKET P/N 601R31902-461 IAW CRJ900 SRM 51-40-11-001-001-A01, INSTALLED NEW BRACKET IAW
- [SDR REXA2022112102591](https://openairdocs.org/sdr/REXA2022112102591.md): Intercostal · corroded · Nov 20, 2022 · N923XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL DD4 AT FWD SIDE FOUND TO BE CORRODED. REMOVED PAX DOOR FWD INTERCOSTAL DD4 IAW CRJ 900 SRM 51-42-06-001-001-A01. LOCATED AND DRILLED NEW INTERCOSTAL P/N 601R318093-1 IAW CRJ 900 SRM 51-40-11-001-001-A01, INSTALLED NEW INTERCOSTAL IAW CRJ90
- [SDR REXA2022112102590](https://openairdocs.org/sdr/REXA2022112102590.md): Cleat · corroded · Nov 20, 2022 · N923XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR CLEAT ON FWD INTERCOSTAL DD6 FOUND TO BE CORRODED REMOVED PAX DOOR CLEAT ON FWD INTERCOSTAL DD6 IAW CRJ 900 SRM 51-42-06-001-001-A01. LOCATED AND DRILLED NEW CLEAT P/N 600-31902-269 IAW CRJ 900 SRM 51-40-11-001-001-A01, INSTALLED NEW CLEAT IAW CRJ 90

Next page: https://openairdocs.org/aircraft/N923XJ/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 = 'N923XJ' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N923XJ/reports

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