# Service difficulty reports: N902XJ

A list on [N902XJ](https://openairdocs.org/aircraft/N902XJ.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 · 185 reports

- [SDR REXA2025021900205](https://openairdocs.org/sdr/REXA2025021900205.md): Lug · corroded · Feb 7, 2025 · N902XJ · Cndair CL6002D24 · Wing, Control Surface Attach Fittings
  > "FOUND BUSHING LUG BORE LABELED ""F"" TO HAVE PITTING REQUIRES TO GO TO FIRST OVER REPAIRED LH AILERON BUSHING LUG BORE LABELED ""F"" IAW REO 670-57-61-237 REV -- DATED 2017-07-25."
- [SDR REXA2025020500129](https://openairdocs.org/sdr/REXA2025020500129.md): Seat Track · corroded · Feb 4, 2025 · N902XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > RBL9 FLOOR SEAT TRACK IS CORRODED BETWEEN F.S. 349 TO F.S. 379. REMOVED UNSERVICEABLE RBL9 SEAT TRACK BETWEEN FS349-FS483 IAW CRJ 900 AMM 53-00-49-000-801-A19.INSTALLED NEW SERVICEABLE SEAT TRACK P/N SH670-32159-1 IAW CRJ900 AMM 53-00-49-400-801-A19
- [SDR REXA2025020500128](https://openairdocs.org/sdr/REXA2025020500128.md): Angle · corroded · Feb 4, 2025 · N902XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > PAX DOOR UPPER MID SILL ANGLE IS CORRODED REMOVED UNSERVICEABLE PAX DOOR UPPER MID SILL ANGLE IAW CRJ 900 SRM 51-42-06-001-001-A01 & 51-41-02-001-001-A01.INSTALLED NEW PAX DOOR UPPER MID SILL ANGLEP/N SH670-31825-9S IAW CRJ 900 SRM 51-42-06-001-001-A01 & 51-41
- [SDR REXA2025020500127](https://openairdocs.org/sdr/REXA2025020500127.md): Angle · corroded · Feb 4, 2025 · N902XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > PAX DOOR UPPER FWD SILL ANGLE IS CORRODED. REMOVED UNSERVICEABLE PAX DOOR UPPER FWD SILL ANGLE IAW CRJ 900 SRM 51-42-06-001-001-A01. INSTALLED NEW SERVICEABLE PAX DOOR UPPER FWD SILL ANGLE P/N SH670-31821-5S IAW CRJ900 SRM 51-42-06-001-001-A01.
- [SDR REXA2025021900204](https://openairdocs.org/sdr/REXA2025021900204.md): Angle · corroded · Feb 1, 2025 · N902XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FOUND PAX DOOR KICKPLATE ANGLE (P/N: SH670-31875-1) TO BE CORRODED. INSTALLED NEW SERVICEABLE PAX DOOR KICKPLATE ANGLE (P/N: SH670-31875-1) IAW CRJ 900 SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01.
- [SDR REXA2025020500126](https://openairdocs.org/sdr/REXA2025020500126.md): Angle · corroded · Jan 26, 2025 · N902XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > PAX DOOR UPPER AFT SILL ANGLE IS CORRODED. INSTALLED AND SEALED NEW SERVICEABLE ANGLE SUPPORT P/N SH670-33332-5, AND RESTORED SURFACE FINISH ON RIVETS IAW CRJ900 SRM 51-42-13-001-001-A01, SRM 51-23-00-001-001-A01, AND SRM 51-25-16-001-001-A01.
- [SDR REXA2025021900203](https://openairdocs.org/sdr/REXA2025021900203.md): Door Frame · cracked · Jan 23, 2025 · N902XJ · Cndair CL6002D24 · Fuselage Main, Structure
  > L/H FWD. OVERWING EMERGENCY EXIT DOOR UPPER ALIGNMENT SPADE FITTING SURROUNDING STRUCTURE IS CRACKED REPAIRED LH FWD EMERGENCY EXIT DOOR IAW REO 690-52-21-182 REV -- DATED 2025-02-02 AND REO 670-52-21-103 REV -- DATED 2024-11-06
- [SDR REXA2025021300194](https://openairdocs.org/sdr/REXA2025021300194.md): Door Frame · cracked · Jan 23, 2025 · N902XJ · Cndair CL6002D24 · Fuselage Main, Structure
  > "L/H AFT OVERWING EMERGENCY EXIT DOOR UPPER ALIGNMENT SPADE FITTING SURROUNDING STRUCTURE IS CRACKED COMPLIED WITH REO 690-52-21-181 REV -- DATED 2025-02-02 FOR DEVIATION TO STEP 1 OF REO 670-52-21-103 REV -- DATED 2024-11-06. RESTORED TO FINISH IAW CRJ-900
- [SDR REXA2025021300193](https://openairdocs.org/sdr/REXA2025021300193.md): Fitting · cracked · Jan 23, 2025 · N902XJ · Cndair CL6002D24 · Fuselage Main, Structure
  > "RIGHT AFT OVERWING EMERGENCY EXIT DOOR UPPER ALIGNMENT SPADE FITTING SURROUNDING STRUCTURE IS CRACKED COMPLIED WITH REO 690-52-21-180 REV -- DATED 2025-02-02 FOR DEVIATION TO STEP 1 OF REO 670-52-21-103 REV -- DATED 2024-11-06. INSTALLED THE R/H AFT OVER W
- [SDR REXA2024050300367](https://openairdocs.org/sdr/REXA2024050300367.md): Fan · inoperative · May 1, 2024 · N902XJ · Cndair CL6002D24 · Air Distribution Fan
  > FUMES/SMOKE CAME OUT OF ECS VENTS IN THE COCKPIT AND CABIN AFTER TAKE OFF. FUMES/SMOKE MOSTLY DISSIPATED DURING LANDING. REMOVED AND REPLACED THE #1 AND #2 RECIRCULATION FAN FILTERS PER CRJ 900 AMM 21-22-12. PERFORMED OPERATIONAL CHECK PER AMM 21-22-10 AND PER
- [SDR REXA2022040400560](https://openairdocs.org/sdr/REXA2022040400560.md): Light · inoperative · Apr 2, 2022 · N902XJ · Cndair CL6002D24 · Emergency Lighting
  > LIGHT DS101 PINS BROKEN OFF IN CONNECTER REPLACED LIGHT DS101 IAW AMM 33-51-15 AND ESPM 20-16-05 P/N ON/OFF:2LA006954-00
- [SDR REXA2021090200650](https://openairdocs.org/sdr/REXA2021090200650.md): Stringer · corroded · Sep 2, 2021 · N902XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STR 22R IS CORRODED ON AFT SIDE OF F.S. 333.00. REQUIRES EVALUATION. R/R UNSERVICEABLE STGR 22R, STGR 22R SPLICE, AND STGR 22R CLEAT FS 333 TO 349 WITH SERVICEABLE STGR, SPLICE, AND CLEAT IAW SRM 51-42-06-001-001(A01), 51-40-11-001-001(A01).
- [SDR REXA2021090200657](https://openairdocs.org/sdr/REXA2021090200657.md): Angle · corroded · Aug 20, 2021 · N902XJ · Cndair CL6002D24 · Trailing Edge Flaps
  > "RH IB FLAP LOWER SKIN CHAFED FROM CONTACT WITH IB CANOE FAIRING (683BB). FOUND CHAFE TO BE OUT OF LIMITS PER SRM 37-52-01-001-001-A01. REMOVED UNSERVICEABLE SKIN AND INSTALLED SERVICEABLE SKIN IAW SRM 57-52-01-201-005-A01. R & R SAME SERVICEABLE R/H I/B F
- [SDR REXA2021090200655](https://openairdocs.org/sdr/REXA2021090200655.md): Stringer · corroded · Aug 17, 2021 · N902XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > "STR 21R HAS MULTIPLE AREAS OF CORROSION FROM F.S. 333.00 TO 453.00. REMOVED STR 21R FROM FS 394 - FS 477 AND FROM FS 333 - FS 379. LOCATED, DRILLED, AND INSTALLED NEW STR 21R FROM FS 333-379 AND 394-477 AND INCLUDING NEW STR SPLICES AND JOINT PIECES IAW CRJ
- [SDR REXA2021090200654](https://openairdocs.org/sdr/REXA2021090200654.md): Stringer · corroded · Aug 17, 2021 · N902XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STR 21R HAS MULTIPLE AREAS OF CORROSION FROM F.S. 333.00 TO 453.00. REMOVED STR 21R FROM FS 394 - FS 477 AND FROM FS 333 - FS 379. LOCATED, DRILLED, AND INSTALLED NEW STR 21R FROM FS 333-379 AND 394-477 AND INCLUDING NEW STR SPLICES AND JOINT PIECES IAW CRJ 9
- [SDR REXA2021090200653](https://openairdocs.org/sdr/REXA2021090200653.md): Cleat · corroded · Aug 17, 2021 · N902XJ · Cndair CL6002D24 · Fuselage Main, Attach Fittings
  > "STR 21R HAS MULTIPLE AREAS OF CORROSION FROM F.S. 333.00 TO 453.00. REMOVED STR 21R FROM FS 394 - FS 477 AND FROM FS 333 - FS 379. LOCATED, DRILLED, AND INSTALLED NEW STR 21R FROM FS 333-379 AND 394-477 AND INCLUDING NEW STR SPLICES AND JOINT PIECES IAW SR
- [SDR REXA2021090200652](https://openairdocs.org/sdr/REXA2021090200652.md): Stringer · corroded · Aug 17, 2021 · N902XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > "STR 21R HAS MULTIPLE AREAS OF CORROSION FROM F.S. 333.00 TO 453.00. REMOVED STR 21R FROM FS 394 - FS 477 AND FROM FS 333 - FS 379. LOCATED, DRILLED, AND INSTALLED NEW STR 21R FROM FS 333-379 AND 394-477 AND INCLUDING NEW STR SPLICES AND JOINT PIECES IAW CRJ 9
- [SDR REXA2021090200651](https://openairdocs.org/sdr/REXA2021090200651.md): Stringer · corroded · Aug 17, 2021 · N902XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > "STR 21R HAS MULTIPLE AREAS OF CORROSION FROM F.S. 333.00 TO 453.00. REMOVED STR 21R FROM FS 394 - FS 477 AND FROM FS 333 - FS 379. LOCATED, DRILLED AND INSTALLED NEW STR 21R FROM FS 333-379 AND 394-477 AND INCLUDING NEW STR SPLICES AND JOINT PIECES IAW CRJ
- [SDR REXA2021090200678](https://openairdocs.org/sdr/REXA2021090200678.md): Stringer · corroded · Aug 16, 2021 · N902XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER 22R HAS CORROSION BTW BS 437 TO 453. CUT & REMOVED FROM SECTION FS 469 FOR ACCESS. REMOVED AND REPLACED STRINGER 22R FROM 394-477 IAW CRJ900 SRM 51-42-06-001-001-A01 AND 51-40-11-001-001-A01. REINSTALLED FROM SECTION FS 469 AND REPAIR SPLICE IAW C
- [SDR REXA2021090200677](https://openairdocs.org/sdr/REXA2021090200677.md): Stringer · corroded · Aug 16, 2021 · N902XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER 22R HAS CORROSION BTW BS 437 TO 453. CUT & REMOVED FROM SECTION FS 469 FOR ACCESS- REMOVED AND REPLACED STRINGER 22R FROM 394-477 IAW CRJ900 SRM 51-42-06-001-001-A01 AND 51-40-11-001-001-A01. REINSTALLED FROM SECTION FS 469 AND REPAIR SPLICE IAW CRJ
- [SDR REXA2021090200674](https://openairdocs.org/sdr/REXA2021090200674.md): Frame · corroded · Aug 16, 2021 · N902XJ · Cndair CL6002D24 · Fuselage Main, Frame
  > FRAME BS 379 HAS CORROSION BTW STR 20R TO STR 21R. REMOVED STR 22R AND 3 CLEATS AT ST 21, 22, AND 24R, REMOVED SPLICE FRAME AND ANGLE AT FS 379. REMOVED AND REPLACED RH REINFORCING ANGLE AND FRAME SECTION AT FS 379 BTW ST 20R-21R IAW CRJ 900 SRM 51-42-06-001
- [SDR REXA2021090200673](https://openairdocs.org/sdr/REXA2021090200673.md): Frame · corroded · Aug 16, 2021 · N902XJ · Cndair CL6002D24 · Fuselage Main, Frame
  > FRAME BS 379 HAS CORROSION BTW STR 20R TO STR 21R. REMOVED STR 22R AND 3 CLEATS AT ST 21, 22, AND 24R, REMOVED SPLICE FRAME AND ANGLE AT BS 379. REMOVED AND REPLACED RH REINFORCING ANGLE AND FRAME SECTION AT FS 379 BTW ST 20R-21R IAW CRJ 900 SRM 51-42-06-00
- [SDR REXA2021090200672](https://openairdocs.org/sdr/REXA2021090200672.md): Stringer · corroded · Aug 15, 2021 · N902XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER 20R HAS MULTIPLE AREAS OF CORROSION FROM BS 364 TO 409. REMOVED, LOCATED, DRILLED AND REPLACED STR 20R AT FS 364-469 IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01 AND 51-40-11-001-001-A01.
- [SDR REXA2021090200679](https://openairdocs.org/sdr/REXA2021090200679.md): Frame · corroded · Aug 13, 2021 · N902XJ · Cndair CL6002D24 · Fuselage Main, Frame
  > FOUND CORROSION AT BS 942, STRINGER 22R ON FRAME. REPAIRED THE BS 942 FRAME IAW CRJ 900 SRM 53-00-06-201-001-A03, 51-42-06-001-001-A01, 51-40-11-001-001-A01 & 53-51-06-101-003-A04.
- [SDR REXA2021090200675](https://openairdocs.org/sdr/REXA2021090200675.md): Joint · corroded · Aug 13, 2021 · N902XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > ANGLE JOINT PIECE LOCATED BTW FS 379 TO FS 394 AT LEVEL STR 21R HAS CORROSION. REMOVED, LOCATED, DRILLED, DEBURRED, AND REPLACED ANGLE JOINT/STRINGER BETWEEN FS 379-394 STGR 21R IAW CRJ 900 SRM 51-47-06-001-001-A01 AND 51-40-11-001-001-A01.
- [SDR REXA2021090200681](https://openairdocs.org/sdr/REXA2021090200681.md): Floor Support · corroded · Aug 11, 2021 · N902XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FLOOR BEAM AT LBL27 HAS MULTIPLE SPOTS OF CORROSION FROM FS 1000.00 TO FS 1098.00. REMOVED AND REPLACED FLOORBEAM AT LBL 27 FS 1000-1098 IAW CRJ 900 SRM 53-00-41-201-001-A03. RESTORED FINISH IAW SRM 51-25-00-001-001-A01.
- [SDR REXA2021090200671](https://openairdocs.org/sdr/REXA2021090200671.md): Intercostal · corroded · Aug 10, 2021 · N902XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > INTERCOSTAL AT STRINGER 20R IS CORRODED BETWEEN FS. 349 TO 364. R & R UNSERVICEABLE INTERCOSTAL WITH A SERVICEABLE INTERCOSTAL IAW SRM 51-42-06-001-001(A01), 51-40-11-001-001-(A01) & 51-42-21-001-001-A01.
- [SDR REXA2021090200680](https://openairdocs.org/sdr/REXA2021090200680.md): Frame · corroded · Aug 8, 2021 · N902XJ · Cndair CL6002D24 · Fuselage Main, Frame
  > FRAME AT BS 954 CORRODED BETWEEN STRINGERS 25R AND 26R. PERFORMED CUT OUT OF FRAME AT STGR 27 AND REMOVED FRAME SECTION FROM STGR 20 TO 27 @ 954 IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01 AND 53-00-06-201-001-A03. PERFORMED EDDY CURRENT OF
- [SDR REXA2021090200667](https://openairdocs.org/sdr/REXA2021090200667.md): Fitting · corroded · Aug 6, 2021 · N902XJ · Cndair CL6002D24 · Elevator Structure
  > RIGHT AILERON CENTER FITTING, INBD BUSHING LUGS FOUND TO BE CORRODED UPON REMOVAL OF BUSHINGS. REPAIRED RH AILERON CENTER FITTING INBD BUSHING LUGS IAW REO 670-57-61-237 REV-.
- [SDR REXA2021090200664](https://openairdocs.org/sdr/REXA2021090200664.md): Angle · corroded · Aug 6, 2021 · N902XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR ACCESS HOLES 832 AL, 832 BL, 83 DL, 832 EL, AND 832 FL HAVE INTERNAL SKIN CORROSION. LOCATED, DRILLED, AND INSTALLED NEW PAX DOOR FWD DRAG ANGLE IAW SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01 REV 38.
- [SDR REXA2021090200662](https://openairdocs.org/sdr/REXA2021090200662.md): Skin · corroded · Aug 6, 2021 · N902XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR ACCESS HOLE 832 JR HAS A CORRODED FASTNER HOLE. AFTER FURTHER INVESTIGATION FOUND PAX DOOR INNER SKIN TO REQUIRE REPLACEMENT R/R PAX DOOR INNER SKIN IAW CRJ 900 SRM 51-40-11-001-001(A01) & 51-42-06/13/21/22-001-001(A01).
- [SDR REXA2021090200658](https://openairdocs.org/sdr/REXA2021090200658.md): Web · cracked · Aug 6, 2021 · N902XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR FWD WEB BOTTOM FASTNER FLANGE FOR PNL 832 CT IS CRACKED. LOCATED AND DRILLED NEW PAX DOOR FWD STAIR WEB P/N 601R317071-12 AND INSTALLED SUPPORT ANGLES ONTO NEW WEB IAW CRJ 900 SRM 51-40-11-001- 001-A01 AND 51-42-06-001-001-A01 REV 38.
- [SDR REXA2021090200666](https://openairdocs.org/sdr/REXA2021090200666.md): Fitting · chafed · Aug 5, 2021 · N902XJ · Cndair CL6002D24 · Trailing Edge Flaps
  > FLAP STUB FAIRING 172 DR FWD MOUNTING BRACKET CHAFED. R & R UNSERVICABLE FLAP STAB FAIRING BRACKET WITH SERVICABLE BRACKET IAW CRJ 900 SRM 51-42-21-001-001(A01) & 51-25-06/16-001-001(A01).
- [SDR REXA2021090200663](https://openairdocs.org/sdr/REXA2021090200663.md): Angle · corroded · Aug 4, 2021 · N902XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR ACCESS HOLE 832DR HAS INTERNAL SKIN CORROSION. LOCATED, DRILLED AND INSTALLED NEW PAX DOOR AFT DRAG ANGLE IAW SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01 REV 38.
- [SDR REXA2021090200661](https://openairdocs.org/sdr/REXA2021090200661.md): Panel · corroded · Aug 4, 2021 · N902XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR AFT WEB BOTTOM FASTNER FLANGE FOR STEP PNL 832 BT IS CORRODED. LOCATED AND DRILLED NEW PAX DOOR AFT STAIR WEB AND INSTALLED SUPPORT ANGLES ONTO NEW WEB IAW SRM 51-40-11-001- 001-A01 AND 51-42-06-001-001-A01 REV 38.
- [SDR REXA2021090200668](https://openairdocs.org/sdr/REXA2021090200668.md): Former · corroded · Aug 2, 2021 · N902XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > UPON REMOVAL OF PAX DOOR INNER SKIN FOUND FWD FORMER P/N 601R318031-5 TO BE CORRODED BEYOND LIMITS. FORMER REQUIRES REPLACEMENT. REMOVED MID AND LOWER TENSION TIES IAW AMM 52-11-19-000-801-A01 REV 67. REF MWC 81513131/301 FOR TENSION TIE INSTALL. REMOVED F
- [SDR REXA2021090200665](https://openairdocs.org/sdr/REXA2021090200665.md): Seat Track · damaged · Aug 2, 2021 · N902XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT AND RIGHT SIDE SEAT TRACKS BETWEEN BS 744.15 AND 761.85 HAVE SCRATCHES AND GOUGES AT THE FWD ENDS.
- [SDR REXA2021090200660](https://openairdocs.org/sdr/REXA2021090200660.md): Panel · corroded · Aug 2, 2021 · N902XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR AIRSTAIR TOP COVER PLATE FASTNER HOLES ARE CORRODED. FOUND PAX DOOR TO HAVE SEVERAL AREAS OF CORROSION. REMOVED, LOCATED, DRILLED AND INSTALLED STIFFENERS IAW SRM (51-45-00-001-001-A01), (51-42-06-001-001-A01), (51-40-11-001-001-A01 (51-40-11-0
- [SDR REXA2021090200659](https://openairdocs.org/sdr/REXA2021090200659.md): Stiffener · corroded · Aug 2, 2021 · N902XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR AIRSTAIR TOP COVER PLATE FASTNER HOLES ARE CORRODED. FOUND PAX DOOR TO HAVE SEVERAL AREAS OF CORROSION. REMOVED, LOCATED, DRILLED AND INSTALLED STIFFENERS IAW SRM CRJ 900 (51-45-00-001-001-A01), (51-42-06-001-001-A01), (51-40-11-001-001-A01, (5
- [SDR REXA2021090200670](https://openairdocs.org/sdr/REXA2021090200670.md): Angle · cracked · Aug 1, 2021 · N902XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR POWER-ASSIST MOTOR UPPER ATTACH ANGLE P/N 601R317745-7 IS CRACKED. LOCATED AND DRILLED NEW SUPPORT ANGLE IAW CRJ 900 SRM 51-40-4-001-001-A01. REV 38. REF MWC 81513131/200 FOR ANGLE INSTALL.
- [SDR REXA2021090200669](https://openairdocs.org/sdr/REXA2021090200669.md): Cleat · corroded · Aug 1, 2021 · N902XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > UPON REMOVAL OF PAX DOOR INNER SKIN FOUND FWD MID CLEAT P/N 600-31902-269 CORRODED BEYOND LIMITS. REMOVED AND REPLACED WITH NEW P/N 600-31902-269 CLEAT IAW SRM 51-42-06-001-001-A01 REV 38.
- [SDR REXA2021090200656](https://openairdocs.org/sdr/REXA2021090200656.md): Angle · corroded · Aug 1, 2021 · N902XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "FWD WING TO FUSELAGE FAIRING SUPPORT INTERCOSTAL BETWEEN F.S. 661.00+62 AND F.S. 661.00+90 BELOW THE FWD KEEL BEAM HAS CORROSION IN FASTENER HOLES. R & R UNSERVICEABLE INTERCOSTAL WITH A SERVICEABLE INTERCOSTAL BETWEEN FS 661+62 AND 661+90 IAW CRJ900 SRM 51-
- [SDR REXA2020071400595](https://openairdocs.org/sdr/REXA2020071400595.md): Light · inoperative · Jul 7, 2020 · N902XJ · Cndair CL6002D24 · Emergency Lighting
  > EMERGENCY EXIT SIGN ON G1 NEXT TO SVC DOOR HAS BULBS INOP. RELAMPED EMERGENCY EXIT SIGN ON G1 NEXT TO SVC DOOR IAW AMM 33-51-05.
- [SDR REXA2019072901142](https://openairdocs.org/sdr/REXA2019072901142.md): Light · inoperative · Jul 29, 2019 · N902XJ · Cndair CL6002D24 · Emergency Lighting
  > EMERGENCY LIGHT NEAR SERVICE DOOR INOP. (CREW NOTED) RELAMPED EXIT LAMP SIGN BULB # 'S OL3071BPE/GPL.
- [SDR REXA2019070901112](https://openairdocs.org/sdr/REXA2019070901112.md): Frame · corroded · Jul 9, 2019 · N902XJ · Cndair CL6002D24 · Fuselage Main, Frame
  > INITIAL INSPECTION: CORROSION ON FRAME IN STA. FS= 333 BETWEEN STR 25L TO 25R AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT (E/E) (SM). IN REFERENCE NRC 00084 TASK 900-53-140-300 APPENDIX A ]. FRAME IN STA. FS= 333 BETWEEN STR 25L TO 25R AT INTERNAL STRUC
- [SDR REXA2019070801116](https://openairdocs.org/sdr/REXA2019070801116.md): Stringer · corroded · Jul 8, 2019 · N902XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > INITIAL INSPECTION: CORROSION STR 25R BTW FS=280.00 / FS=333.00 AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT (E/E) (SM). IN REFERENCE NRC 00084 TASK 900-53-140-300 APPENDIX A ]. NEW STR 25R BTW FS=280.00 / FS=333.00 AT INTERNAL STRUCTURE OF MAIN AVIONICS
- [SDR REXA2019070801115](https://openairdocs.org/sdr/REXA2019070801115.md): Stringer · corroded · Jul 8, 2019 · N902XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > INITIAL INSPECTION: CORROSION STR 26L BTW FS=280.00 / FS=333.00 AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT (E/E) (SM). IN REFERENCE NRC 00084 TASK 900-53-140-300 APPENDIX A ]. NEW STRINGER 26L BTW FS=280 AND FS=333 ATINTERNAL STRUCTURE OF MAIN AVIONICS
- [SDR REXA2019070801114](https://openairdocs.org/sdr/REXA2019070801114.md): Frame · corroded · Jul 8, 2019 · N902XJ · Cndair CL6002D24 · Fuselage Main, Frame
  > INITIAL INSPECTION: CORROSION ON FRAME IN STA. FS= 319 BETWEEN STR 25L TO 25R AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT (E/E) (SM). IN REFERENCE NRC 00084 TASK 900-53-140-300 APPENDIX A ]. FRAME IN STA. FS= 319 BETWEEN STR 25L TO 25R AT INTERNAL STRUC
- [SDR REXA2019070801113](https://openairdocs.org/sdr/REXA2019070801113.md): Stringer · corroded · Jul 8, 2019 · N902XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > INITIAL INSPECTION: CORROSION STR 27 BTW FS=295.00 / FS=333.00 AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT (E/E) (SM). IN REFERENCE NRC 00084 TASK 900-53-140-300 APPENDIX A ]. NEW STRINGERS 27 BTW FS=280.00 / FS=333.00 AT INTERNAL STRUCTURE OF MAIN AVIO
- [SDR REXA2019070801111](https://openairdocs.org/sdr/REXA2019070801111.md): Stringer · corroded · Jul 8, 2019 · N902XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > INITIAL INSPECTION: CORROSION STR 26R BTW FS=280.00 / FS=333.00 AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT (E/E) (SM). IN REFERENCE NRC 00084 TASK 900-53-140-300 APPENDIX A ]. NEW STRINGER 26R BTW FS=280 AND FS=333 AT INTERNAL STRUCTURE OF MAIN AVIONIC

Next page: https://openairdocs.org/aircraft/N902XJ/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 = 'N902XJ' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N902XJ/reports

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