# Service difficulty reports: N934XJ

A list on [N934XJ](https://openairdocs.org/aircraft/N934XJ.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 · 221 reports

- [SDR REXA2026062400975](https://openairdocs.org/sdr/REXA2026062400975.md): Engine · bird ingestion · Jun 18, 2026 · N934XJ · Cndair CL6002D24 · Turbine Engine Air Inlet Section
  > BIRD INGESTED ON CLIMB OUT R ENG DEGRADED FAN VIB 9.9 FOLLOWED QRH VIB CONTINUED EVENTUALLY R ENG FLAME OUT RAN EMER CHECK FOR SEVERE ENGINE DAMAGE. REMOVED AND REPLACED RT ENG ASSY IAW JOBCARD 900-72-430-902 OPS CHECK GOOD
- [SDR REXA2024032900314](https://openairdocs.org/sdr/REXA2024032900314.md): Sign · inoperative · Mar 27, 2024 · N934XJ · Cndair CL6002D24 · Emergency Lighting
  > SVC DOOR EXIT SIGN INOP REMOVE AND REPLACE EXIT SIGN IAW AMM 33-51-05. OPS CHK GOOD
- [SDR REXA2024102901137](https://openairdocs.org/sdr/REXA2024102901137.md): Seat Track · corroded · Nov 30, 2023 · N934XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT RAIL AT STGR 15R IS CORRODED BETWEEN FS 572 AND FS 661+16. FOUND TO BE BEYOND REPAIRABLE LIMITS OF CRJ 900 SRM 53-21-49-101-001-A01 REPLACEMENT REQUIRED REPLACE SEAT TRACK PN SH690-36282-1 INSTALLED NEW SEAT TRACK P/N SH690-36282-1 IAW CRJ900 AMM 53-00-49
- [SDR REXA2024102801089](https://openairdocs.org/sdr/REXA2024102801089.md): Seat Track · corroded · Nov 30, 2023 · N934XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > SEAT RAIL AT LBL 9 IS CORRODED BETWEEN FS 661+32 AND FS 693. FOUND TO BE BEYOND REPAIRABLE LIMITS OF CRJ 900 SRM 53-21-49-101-001-A01 REPLACEMENT REQUIRED REMOVED SEAT RAIL PN BA690-30000-5980 AT LBL 9 BETWEEN FS 661+32 AND FS 693 IAW CRJ900 AMM TASK 53-00-49-
- [SDR REXA2024022700231](https://openairdocs.org/sdr/REXA2024022700231.md): Landing · corroded · Nov 15, 2023 · N934XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "PANEL 196DR HAS A CORRODED LANDING STRIP. REMOVED STRAP ASSEMBLY FROM FAIRING PANEL 196DR PER CRJ 900 SRM 51-41-02-001-001-A01. INSTALLED A FABRICATED NEW WING TO FUSELAGE FAIRING JOINT STRAP P/N CC670-39171-3 IAW CRJ 900 SRM 51-24-36-001-001-A01 AND 51-40-1
- [SDR REXA2024020500155](https://openairdocs.org/sdr/REXA2024020500155.md): Stringer Splice · corroded · Nov 15, 2023 · N934XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > STRINGER 19R IS CORRODED IN MULTIPLE LOCATIONS BETWEEN FS 469.00 AND 661+46 AND ALSO FOUND STRINGER 19R SPLICE AT F.S.477 TO BE CORRODED. REPLACED STGR SPLICE P/N SH670-33264-1 IAW CRJ900 SRM 51-42-06-001-001-A01
- [SDR REXA2024020500154](https://openairdocs.org/sdr/REXA2024020500154.md): Stringer · corroded · Nov 15, 2023 · N934XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER 19R IS CORRODED IN MULTIPLE LOCATIONS BETWEEN FS 469.00 AND 661+46. COMPLIED WITH EA CRJ953-15675 REV IR, AND REPAIRED IAW CRJ900 SRM 53-00-03-201-001-A02 SOLUTION 2
- [SDR REXA2022111400978](https://openairdocs.org/sdr/REXA2022111400978.md): Stringer Splice · corroded · Nov 13, 2023 · N934XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > FOUND STGR 22R SPLICE AT FS 333 TO BE CORRODED. INSTALLED NEW SERVICEABLE STRG 22R (P/N SH670-32429-4S) SPLICE AT FS 333 IAW CRJ 51-42-06-001-001-A01.
- [SDR REXA2022111300971](https://openairdocs.org/sdr/REXA2022111300971.md): Stringer · corroded · Nov 13, 2023 · N934XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER 21R CORRODED BETWEEN FS 319 AND FS 333. INSTALLED NEW SERVICEABLE STG 21R (P/N SH670-31636-1U) FROM FS 280 TO 333 IAW CRJ900 SRM 51-42-06-001-001-A01 AND CRJ 900 SRM 51-42-21-001-001-A01.
- [SDR REXA2022111300966](https://openairdocs.org/sdr/REXA2022111300966.md): Seat Track · corroded · Nov 13, 2023 · N934XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT RAIL AT STGR 15R IS CORRODED BETWEEN FS 785.15 AND FS 847+16. INSTALLED NEW SERVICEABLE SEAT TRACK AT STGR 15R BETWEEN FS 785.15 AND 847+16 IAW MHIRJ900 AMM TASK 53-00-49-400-801 (CONFIG A19). PART NO SH670-36260-5.
- [SDR REXA2022111300969](https://openairdocs.org/sdr/REXA2022111300969.md): Frame · corroded · Nov 12, 2023 · N934XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FS295 FRAME IS CORRODED AT STGR 24R. CUT AND TRIMMED NEW F.S. 295 FRAME P/N SH670-31353-1 AT STGR 25R TO MATCH PREVIOUS REPAIR IAW CRJ-900 SRM 53-00-06-201-006-A01 REPAIR INSTALLATION -102, REPAIR STEPS 2 AND 3. INSTALLED NEW SERVICABLE FUSELAGE FRAME F.S.295
- [SDR REXA2024012200111](https://openairdocs.org/sdr/REXA2024012200111.md): Seat Track · corroded · Oct 31, 2023 · N934XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > "LBL 9 SEAT RAIL IS CORRODED BETWEEN FS 693 AND FS 835. FABRICATED NEW SERVICEABLE SEAT TRACK P/N BA690-30000-5979 IAW MHIRJ REO 670-53-00-589 REV-C DATE 2023-02-08 REPAIR ""B"" 1A AS PER PARAGRAPH 3.A. INSTALLED NEW SEAT TRACK P/N BA690-30000-5979 IAW CRJ900
- [SDR REXA2024012200110](https://openairdocs.org/sdr/REXA2024012200110.md): Seat Track · corroded · Oct 31, 2023 · N934XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > "RBL 9 SEAT RAIL IS CORRODED BETWEEN FS 847+55 AND FS 977. FABRICATED NEW SERVICEABLE SEAT TRACK P/N BA690-30000-6963 IAW MHIRJ REO 670-53-00-589 REV-C DATE 2023-02-08 REPAIR ""B"" 1A AS PER PARAGRAPH 3.A. INSTALLED NEW SEAT TRACK P/N BA690-30000-6963 IAW CRJ9
- [SDR REXA2024102901136](https://openairdocs.org/sdr/REXA2024102901136.md): Angle · corroded · Oct 24, 2023 · N934XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > RH FLOOR SILL ANGLE IS CORRODED BETWEEN FS 720.85 AND FS 785.15. REPAIRED IAW ENDEAVOR AIR EA CRJ953-15607 REV B DATED 10/21/2023 AND CRJ953-15608 REV B DATED 10/21/2023 AND ENDEAVOR AIR EA CRJ953-15608 DATED 10/3/2023.
- [SDR REXA2024021200186](https://openairdocs.org/sdr/REXA2024021200186.md): Stringer · corroded · Oct 24, 2023 · N934XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER 20R HAS CORROSION FROM FS319 TO FS349. REMOVED, LOCATED AND DRILLED NEW STRINGER 20R FROM 319 TO 349 P/N SH670-32428-3 IAW CRJ-900 SRM 51-40-11-001-001-A01 INSTALLED NEW SERVICEABLE STRINGER 20R P/N SH670-32428-3 AT F.S. 319 TO F.S. 349 IAW CRJ 90
- [SDR REXA2022120701024](https://openairdocs.org/sdr/REXA2022120701024.md): Angle · cracked · Oct 23, 2023 · N934XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > RH FS 280 BULKHEAD LOWER WEB VERTICAL STIFFENER #2 IS CRACKED LOCATED, DRILLED, AND INSTALLED NEW STIFFENER P/N: CC670-34117-6 IAW CRJ900 SRM 51-42-06-001-001-A01 AND 51-42-13-001-001-A01
- [SDR REXA2022110700958](https://openairdocs.org/sdr/REXA2022110700958.md): Web · corroded · Oct 18, 2023 · N934XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > L/H F.S. 280 WEB IS CORRODED. REMOVED L/H F.S 280 LOWER WEB IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01 FABRICATED LOCATED AND DRILLED NEW F.S 280 LOWER WEB IAW CRJ 900 SRM 53-11-10-201-004-A01 REV 38 INSTALLED LH FS 280 IAW CRJ900 SRM 53
- [SDR REXA2024103001239](https://openairdocs.org/sdr/REXA2024103001239.md): Stringer · corroded · Oct 17, 2023 · N934XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STGR 20L IS CORRODED BETWEEN F.S. 280 TO F.S. 295. REPAIRED IAW ENDEAVOR AIR EA CRJ953-15661 REV IR DATED 10/15/2023.
- [SDR REXA2024103001219](https://openairdocs.org/sdr/REXA2024103001219.md): Floorbeam · corroded · Oct 17, 2023 · N934XJ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > R/H FITTING FOR THIRD CREW FOOT REST ON COCKPIT FLOOR BEAM CRACKED REPAIRED PER REO 690-53-11-1626
- [SDR REXA2022101800898](https://openairdocs.org/sdr/REXA2022101800898.md): Floor Support · corroded · Oct 17, 2023 · N934XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > LBL 9 FLOOR SUPPORT UPPER FLANGE IS CORRODED BETWEEN FS 693 AND FS 847. REPAIRED IAW ENDEAVOR EA CRJ953-15620 REV. IR DATED 10/7/2023
- [SDR REXA2022101800897](https://openairdocs.org/sdr/REXA2022101800897.md): Seat Track · corroded · Oct 17, 2023 · N934XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT RAIL AT STGR 15L IS CORRODED BETWEEN FS 744.15 AND FS 761.85. REMOVED AND REPLACED SIDE SEAT RAIL AT STGR.15L BETWEEN FS 744.15 AND 761.85 IAW CRJ 900 AMM 53-00-49-400-801 (A07)
- [SDR REXA2022101700895](https://openairdocs.org/sdr/REXA2022101700895.md): Floor Support · corroded · Oct 15, 2023 · N934XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > R/H FLOOR SILL IS CORRODED BETWEEN F.S. 280 TO F.S. 310. REMOVED AND REPLACED RH FLOOR SILL IAW CRJ900 SRM 51-42-06-001-001-A01, 51-40-11-001-001-A01, 51-42-13-001-001-A01, AND 51-42-21-001-001-A01.
- [SDR REXA2022101600892](https://openairdocs.org/sdr/REXA2022101600892.md): Intercostal · corroded · Oct 10, 2023 · N934XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > SERVICE DOOR INTERCOSTAL IS CORRODED BETWEEN F.S. 310 TO F.S. 319 STGR 20R. INSTALLED NEW INTERCOSTAL 20R P/N SH670-32047-1 BETWEEN FS 310 - FS 319.70 IAW CRJ-900 SRM 51-42-06-001-001-A01.
- [SDR REXA2024100100764](https://openairdocs.org/sdr/REXA2024100100764.md): Bulkhead · corroded · Oct 6, 2023 · N934XJ · Cndair CL6002D24 · Fuselage Main, Bulkhead
  > "RH F.S. 280 WEB IS CORRODED. LOCATED AND DRILLED NEW LOWER RH FS280 BULKHEAD WEB AND BUTTSTRAP FROM 7075-T6.040"" PO 5-4871 IAW CRJ900 SRM 53-11-10-201-004-A01.INSTALLED RH FS 280 WEB AND BUTT STRAP IAW CRJ900 SRM 53-11-10-201-004-A01"
- [SDR REXA2024100100763](https://openairdocs.org/sdr/REXA2024100100763.md): Stringer Splice · corroded · Oct 2, 2023 · N934XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STGR 20R SPLICE IS CORRODED AT FS 477 REMOVED CORRODED STRG 20R SPLICE AT FS 477.00 IAW CRJ-900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. FABRICATED NEW STRINGER SPLICE PN. SH670-332S2-1 PER SAMPLE WITH EXTRUSION PN. N126-3999 LOT# A751431 PO# 5000008
- [SDR REXA2024110601436](https://openairdocs.org/sdr/REXA2024110601436.md): Stringer · corroded · Sep 28, 2023 · N934XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER 26R CORRODED AROUND 4 FASTENERS BETWEEN FS 265.00 TO FS 280.00 REPAIRED STGR 26R P/N CC670-33150-2 IAW MHIRJ EO CL-600-2D24-53-L07599 REV. IR DATED 10-17-2023.
- [SDR REXA2024102901135](https://openairdocs.org/sdr/REXA2024102901135.md): Seat Track · corroded · Sep 28, 2023 · N934XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT RAIL AT LBL 9 IS CORRODED BETWEEN FS 370 AND FS 485 INSTALLED NEW SEAT TRACK P/N SH670-32249-3 IAW CRJ-900 AMM 53-00-49-400-801-A07.
- [SDR REXA2024103001240](https://openairdocs.org/sdr/REXA2024103001240.md): Former · corroded · Sep 26, 2023 · N934XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR AFT FORMER CORRODED LOCATED MATCH DRILLED AND INSTALLED NEW SERVICEABLE AFT FORMER PN 601R318034-5 CRJ900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01
- [SDR REXA2024021600197](https://openairdocs.org/sdr/REXA2024021600197.md): Skin · cracked · Sep 26, 2023 · N934XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > UPON REMOVAL OF PAX DOOR INNER SKIN FOUND CRACK RUNNING FROM EDGE TO NUTPLATE. SKIN REQUIRES REPLACEMENT. LOCATED AND DRILLED NEW SERVICEABLE INNER SKIN PN 601R318024-15 IAW CRJ900 SRM 51-40-11-001-001-A01. REFERENCE HN00113531 FOR INSTALLATION.
- [SDR REXA2022110800961](https://openairdocs.org/sdr/REXA2022110800961.md): Stringer · corroded · Sep 26, 2023 · N934XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STGR 26R IS CORRODED BETWEEN FS 349 AND FS 364 REMOVED AND REPLACED STRG 26R BETWEEN FS 349.00 AND FS 364.00 IAW CRJ900 IAW 51-42-06-001-001-A01,51-40-11-001-001-A01. AND SRM 51-42-21-001-001-A01. P/N INSTALLED IS SH670-31372-4S
- [SDR REXA2024021200185](https://openairdocs.org/sdr/REXA2024021200185.md): Floorbeam · corroded · Sep 24, 2023 · N934XJ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > FOUND CORROSION ON L/H 280 CROSSBEAM REMOVED AND REPLACED LH FS 280 CROSSBEAM IAW CRJ900 SRM 51-42-21-001-001-A01, 51-42-06-001-001-A01, AND SB 670BA-53-041 REV M DATED 9/20/22
- [SDR REXA2022120101003](https://openairdocs.org/sdr/REXA2022120101003.md): Floorbeam · corroded · Sep 20, 2023 · N934XJ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > "FOUND CORROSION ON R/H 280 CROSSBEAM OUT OF LIMITS NO ALLOWABLE LIMITS GIVEN. REQUIRES REPLACEMENT REMOVED RH FS280 CROSSBEAM IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, AND 51-42-22-001-001-A01. INSTALLED RT FS280 CROSSBEAM PN CC670-34094JP-2S IAW SR
- [SDR REXA2024103001188](https://openairdocs.org/sdr/REXA2024103001188.md): Doubler · corroded · Sep 19, 2023 · N934XJ · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > TCAS ANTENNA DOUBLER IS CORRODED AROUND CUTOUT BETWEEN FS 295 AND FS 310. REMOVED LOWER TCAS ANTENNA DOUBLER IAW CRJ 900 SRM 51-42-06-001-001-A01. INSTALLED NEW TCAS LOWER ANTENNA'S DOUBLER P/N SH670-32364-7S IAW CRJ 900 SRM 51-42-06-001-001-A01.
- [SDR REXA2024100100761](https://openairdocs.org/sdr/REXA2024100100761.md): Fitting · cracked · Sep 19, 2023 · N934XJ · Cndair CL6002D24 · Fuselage Main, Structure
  > L/H FIGHT COMPARTMENT SIDE WINDSHIELD SUPPORT POST AFT LOWER FITTING IS CRACKED. LOCATED AND DRILLED NEW AFT LOWER FITTING PART #GC212-0045-3 FOR L/H FLIGHT COMPARTMENT SIDE WINDOW SUPPORT POST IAW CRJ 900 SRM 51-40-11-001-001-A01.INSTALLED LH FLIGHT COMPARTME
- [SDR REXA2022120101007](https://openairdocs.org/sdr/REXA2022120101007.md): Frame · corroded · Sep 19, 2023 · N934XJ · Cndair CL6002D24 · Fuselage Main, Frame
  > FS 364 FRAME IS CORRODED BETWEEN STGR 26R AND 25R FRAME FABRICATED REPAIR PARTS IAW SRM 53-21-23-201-008-A01 STEP 5E NO INDICATIONS NOTED AT THIS TIME REMAINING STEPS OF CRJ 900 SRM 53-21-23-201-008-A01 COMPLIED WITH STEPS 5 H-J OF CRJ 900 SRM 53-21-23-201
- [SDR REXA2022101200860](https://openairdocs.org/sdr/REXA2022101200860.md): Fitting · cracked · Sep 19, 2023 · N934XJ · Cndair CL6002D24 · Fuselage Main, Structure
  > R/H FIGHT COMPARTMENT SIDE WINDSHIELD SUPPORT POST AFT LOWER FITTING IS CRACKED. REMOVED FITTING P/N:GC212-0045-4 IAW CRJ900 SRM 51-42-21-001-001-A01. REQUIRES REPLACE. INSTALLED NEW FITTING P/N:GC212-0045-4 IAW CRJ900 SRM 51-42-21-001-001-A01. AND COMPLETED F
- [SDR REXA2022101100851](https://openairdocs.org/sdr/REXA2022101100851.md): Stringer · corroded · Sep 19, 2023 · N934XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STGR 25R IS CORRODED BETWEEN FS 310 AND FS 333 REMOVED AND REPLACED STRINGER 25R P/N SH670-31212-2U IAW CRJ-900-SRM-51-42-06-001-001-A01 AND 51-42-21-001-001-A01
- [SDR REXA2024103001237](https://openairdocs.org/sdr/REXA2024103001237.md): Stringer · corroded · Sep 18, 2023 · N934XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STGR 22L IS CORRODED BETWEEN F.S. 349 TO F.S. 364. REPAIRED STGR 22L BETWEEN F.S. 349 TO F.S. 364 IAW ENDEAVOR AIR EA CRJ953-15538 REV IR DATED 10/05/2023,
- [SDR REXA2024103001236](https://openairdocs.org/sdr/REXA2024103001236.md): Expansion Joint · corroded · Sep 18, 2023 · N934XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > H SPLICE AT FS 629.00 STGR 26L IS CORRODED. LOCATED, DRILLED, COUNTERSINK, AND INSTALLED NEW EXTERNAL JOINT PLATE P/N SH670-33793-4 AT FS 629 STGR 26L IAW CRJ900 SRM 51-40-11-001-001-A01, 51-42-27-001-001-A01, AND 51-42-21-001-001-A01
- [SDR REXA2024103001187](https://openairdocs.org/sdr/REXA2024103001187.md): Anchor Fitting · corroded · Sep 18, 2023 · N934XJ · Cndair CL6002D24 · Fuselage Main, Attach Fittings
  > MACHINED ANCHOR FITTING AT FS 629.00 LEFT OF STGR 27 IS CORRODED. REPAIRED MACHINED ANCHOR FITTING AT F.S. 629 LEFT OF STGR 27 IAW ENDEAVOR AIR EA CRJ953-15573, REV IR, DATED 9/26/2023.
- [SDR REXA2024103001186](https://openairdocs.org/sdr/REXA2024103001186.md): Splice · corroded · Sep 18, 2023 · N934XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > H SPLICE AT FS 535 STGR 26L IS CORRODED. REMOVED CORROSION IAW CRJ900 SRM 51-21-06-001-001-A01. FOUND TO BE OUT OF ALLOWABLE DAMAGE LIMITS IAW CRJ900 SRM 53-31-23-101-001-A02.INSTALLED NEW H SPLICE PART # SH670-33793-3 IAW CRJ-900 SRM 51-42-21-001-001-A01, AN
- [SDR REXA2024103001185](https://openairdocs.org/sdr/REXA2024103001185.md): Skin · corroded · Sep 18, 2023 · N934XJ · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > FUSELAGE INNER SKIN IS CORRODED IN FRONT OF FRAME AT FS 661+62 BETWEEN STGR 26L AND 26R. REPAIRED FUSELAGE INNER SKIN CORROSION IN FRONT OF FRAME AT F.S. 661+62 AND BETWEEN STGR 26L TO STGR 26R IAW EMDEAVOR AIR EA CRJ953-1554, REV IR, DATED 9/29/2023.
- [SDR REXA2024021600196](https://openairdocs.org/sdr/REXA2024021600196.md): Stringer · corroded · Sep 18, 2023 · N934XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STGR 26R IS CORRODED BETWEEN F.S. 295 TO F.S. 310. REPLACED AND INSTALLED NEW SERVICEABLE STGR 26R P/N SH670-31634-2S AT FS 280 TO 333 IAW CRJ900 51-42-06-001-001-A01
- [SDR REXA2024021600194](https://openairdocs.org/sdr/REXA2024021600194.md): Angle · corroded · Sep 18, 2023 · N934XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FRAME AT FS 645.00 IS CORRODED BETWEEN STGR 17L AND 18L. REMOVED UNSERVICEABLE FRAME SEGMENT IAW CRJ 900 SRM 51-42-06-001-001-A01, AND 51-42-21-001-001-A01 LOCATED AND DRILLED NEW, AND INSTALLED FS 645 FRAME SEGMENT, PN SH690-33166-3, BETWEEN STGR 16L - 18L A
- [SDR REXA2022111400976](https://openairdocs.org/sdr/REXA2022111400976.md): Cleat · corroded · Sep 18, 2023 · N934XJ · Cndair CL6002D24 · Fuselage Main, Attach Fittings
  > F.S. 349 FRAME TO INTERCOSTAL CLIP IS CORRODED AT STGR 20R. EVALUATED AND FOUND TO BE OUT OF LIMITS DUE TO EXCEEDS ALLOWABLE DAMAGE LIMITS IAW CRJ-900 SRM 51-21-23-101-002-A02. REPLACED INTERCOSTAL CLIP P/N SH670-32045-1 AT FS 349 STGR 20R IAW CRJ 900 SRM
- [SDR REXA2022111300968](https://openairdocs.org/sdr/REXA2022111300968.md): Stringer · corroded · Sep 18, 2023 · N934XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STGR 22R IS CORRODED BETWEEN F.S. 280 TO F.S. 310. LOCATED AND DRILLED STGR 22R P/N SH670-31210-2U FROM FS 280-333 IAW CRJ 900 SRM 51-40-11-001-001-A01. INSTALLED NEW STRINGER 22R, P/N SH670-31210-2U, AT FS 280 TO FS 333 IAW CRJ900 SRM 51-42-06-001-001-A01
- [SDR REXA2022101600890](https://openairdocs.org/sdr/REXA2022101600890.md): Frame · corroded · Sep 18, 2023 · N934XJ · Cndair CL6002D24 · Fuselage Main, Frame
  > FRAME AT FS 549.00 IS CORRODED BETWEEN STGR 17L AND 18L FABRICATED, LOCATED AND DRILLED, NDT AND INSTALLED FRAME REPAIR AT FS549 IAW CRJ900 SRM 53-00-06-201-001-A03 FIG 53-00-06-991-883.
- [SDR REXA2022101600889](https://openairdocs.org/sdr/REXA2022101600889.md): Frame · corroded · Sep 18, 2023 · N934XJ · Cndair CL6002D24 · Fuselage Main, Frame
  > FRAME AT FS 533.00 IS CORRODED BETWEEN STGR 17L AND 18L FABRICATED, LOCATED AND DRILLED, NDT AND INSTALLED FRAME REPAIR AT FS533 IAW CRJ900 SRM 53-00-06-201-001-A03 FIG 53-00-06-991-883.
- [SDR REXA2022101300861](https://openairdocs.org/sdr/REXA2022101300861.md): Intercostal · corroded · Sep 18, 2023 · N934XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "INTERCOSTAL AT STGR 24R BETWEEN FS 645 AND 661 IS CORRODED. REMOVED FASTENERS IAW CRJ900 SRM 51-42-06-001-001-A01 REMOVED CORROSION IAW CRJ900 SRM 51-21-06-001-001-A01 PERFORMED U.T. THICKNESS ON S24R INTERCOSTAL BETWEEN FS645-FS661 REWORK AREAS IAW CRJ 900
- [SDR REXA2022101200856](https://openairdocs.org/sdr/REXA2022101200856.md): Seat Track · corroded · Sep 18, 2023 · N934XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > AFT CARGO FLOOR SEAT TRACK AT F.S. 1000.00^ LBL 9.00 IS CORRODED. REMOVED OLD TRACK AND INSTALLED NEW SERVICEABLE SEAT/FLOOR TRACK (P/N: BA670-45074-3) @ FS.1000 LBL9.0 & INSTALLED NEW SERVICEABLE LAV MOUNT/TRACK FITTING ASSY (P/N: CDSP1900-509) ONTO SEAT TRA

Next page: https://openairdocs.org/aircraft/N934XJ/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 = 'N934XJ' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N934XJ/reports

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