# Service difficulty reports: N917XJ A list on [N917XJ](https://openairdocs.org/aircraft/N917XJ.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 · 245 reports - [SDR REXA2026031300239](https://openairdocs.org/sdr/REXA2026031300239.md): Panel · damaged · Mar 10, 2026 · N917XJ · Cndair CL6002D24 · Wing Main, Frame Structure > LEADING EDGE PANEL 622CB HAS ELONGATED HOLE. MARKED WITH RED TAPE. REPAIRED IAW ENDEAVOR AIR EA CRJ957-21685 REV IR DATED 3/11/2026. - [SDR REXA2026031000236](https://openairdocs.org/sdr/REXA2026031000236.md): Lug · damaged · Mar 9, 2026 · N917XJ · Cndair CL6002D24 · Wing Main, Frame Structure > LH AILERON CENTER HINGE FITTING BEARING LUGS MARKED D & E FOUND TO BE OVERSIZED UPON REMOVAL OF BEARINGS BOTH LUGS MEASURE.9825"" DIA. COMPLIED WITH MHIRJ REO 690-57-61-500 REV -- DATED 2026-03-03. - [SDR REXA2026031000235](https://openairdocs.org/sdr/REXA2026031000235.md): Skin · chafed · Mar 9, 2026 · N917XJ · Cndair CL6002D24 · Fuselage Main, Plate/Skin > RIVETS ON FUSELAGE OUTER SKIN ARE CHAFED AND SHEARD OFF AT FS 913.00 STGR 27. RECEIVED AND COMPLIED WITH ENDEAVOR AIR EA: CRJ-953-21545 REV IR DATED 2/15/2026. - [SDR REXA2026030900233](https://openairdocs.org/sdr/REXA2026030900233.md): Bushing · abnormal · Feb 27, 2026 · N917XJ · Cndair CL6002D24 · Ailerons > RH AILERON BUSHING LUGS MARKED C AND F FOUND TO BE OVERSIZED UPON BUSHING REMOVAL COMPLIED WITH STEPS F7- F13 AND G IAW REO 670-57-61-237 REV -- 2017-07-25 - [SDR REXA2026030900232](https://openairdocs.org/sdr/REXA2026030900232.md): Bushing · abnormal · Feb 27, 2026 · N917XJ · Cndair CL6002D24 · Ailerons > LH AILERON BUSHING LUGS MARKED C AND F FOUND TO BE OVERSIZED UPON BUSHING REMOVAL. FABRICATED 2EA O/S BUSHINGS AS REQUIRED USING AMS5659 15-5PH H1000 PO# CP00009965/9662 IAW STEP F.7 OF BOMBARDIER REO 670-57-61-237 REV -- DATED 2017-07-25. C/W LPI ON LH AILERO - [SDR REXA2026022300063](https://openairdocs.org/sdr/REXA2026022300063.md): Crossbeam · corroded · Feb 7, 2026 · N917XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > LEFT BS 280 CROSSBEAM CORRODED FROM BL0 - LBL9. REMOVED DAMAGE IAW SRM 51-21-06-001-001-A01, NO ALLOWABLE LIMITS GIVEN. 50% MATERIAL LOSS REQUIRES REPLACEMENT INSTALLED CROSSBEAM, IAW SRM 51-42-06-001-001-A01, SRM 51-42-13-001-001-A01, SRM 51-42-21-001-00 - [SDR REXA2026022300062](https://openairdocs.org/sdr/REXA2026022300062.md): Crossbeam · corroded · Feb 7, 2026 · N917XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > RIGHT BS 280 CROSSBEAM CORRODED FROM BL0 - RBL9. CROSSBEAM CORRODED FROM BL0 - RBL9, REMOVED DAMAGE & STOPPED AT 50% MATERIAL LOSS. NO ALLOWABLE DAMAGE GIVEN. REQUIRES REPLACEMENT REMOVED DAMAGE IAW SRM 51-21-06-001-001-A01. REMOVED SPLICE FROM LBL9 - RBL9 - [SDR REXA20240701488](https://openairdocs.org/sdr/REXA20240701488.md): Outflow Valve · inoperative · Jun 25, 2024 · N917XJ · Cndair CL6002D24 · Pressure Regulator/Outflow Valve > DURING CLIMBOUT AT ABOUT 19,000 CABIN PRESSURE CAUTION POSTED, LEVELED AIRCRAFT CABIN PRESSURE WAS LOW SHORTLY FOLLOWED BY CABIN PRESSURE WARNING, DESCENDED TO 10K PERFORMED QRH 7,7 WAS ABLE TO CONTROL CABIN SLT IN MAN MODE, REMOVED AND REPLACED OUTFLOW VALVE - [SDR REXA2022020700224](https://openairdocs.org/sdr/REXA2022020700224.md): Acm · not reported · Feb 1, 2023 · N917XJ · Cndair CL6002D24 · Cabin Cooling System > DURING CLIMB CREW NOTED VISIBLE SMOKE/SMELL IN CABIN AND UNCONTROLLABLE LEFT PACK TEMP. SMOKE SMELL SUBSIDED. NORMAL LANDING. ON TAXI CREW RECEIVED L PACK AUTO FAIL CAUTION. LEFT HAND PACK OVERTEMPING AND UNCONTROLLABLE IAW AMM2736-R1 AND FIM 21-22-00. FOUND # - [SDR REXA2022070501466](https://openairdocs.org/sdr/REXA2022070501466.md): Bracket · cracked · Jun 20, 2022 · N917XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > MAIN CABIN FLOOR BEAM ATTACHMENT CLIP AT FS 364, LBL 30 BROKEN REPLACED FLOOR BEAM BRACKET AT FS 364, LBL 30 - [SDR REXA2022070501465](https://openairdocs.org/sdr/REXA2022070501465.md): Bracket · cracked · Jun 20, 2022 · N917XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > BRACKET ON STR 7R AT FS 1162 BROKE IN HALF. REPLACED BRACKET ON STR 7R AT FS 1162 - [SDR REXA2022070501464](https://openairdocs.org/sdr/REXA2022070501464.md): Cowl Door · damaged · Jun 9, 2022 · N917XJ · Cndair CL6002D24 · Engine Thrust Reverser > "RH LOWER TRANSCOWL LATCH DOOR GOUGED..40"" X.20"" X.040"" DEEP" REPLACED RH LOWER TRANSCOWL LATCH DOOR. - [SDR REXA2022070501463](https://openairdocs.org/sdr/REXA2022070501463.md): Latch · chafed · Jun 9, 2022 · N917XJ · Cndair CL6002D24 · Engine Cowling System > RH UPPER TRANSCOWL LATCH COAMING HAS CHAFING WITH 100% MATERIAL LOSS. REMOVED AND REPLACED RH UPPER TRANSCOWL LATCH COAMING - [SDR REXA2022070701471](https://openairdocs.org/sdr/REXA2022070701471.md): Panel · chafed · Jun 8, 2022 · N917XJ · Cndair CL6002D24 · Trailing Edge Flaps > RHIB FLAP ACCESS PANEL 684EB CHAFED.023" DEEP, THIS IS BEYOND SRM LIMITS REPLACED ACCESS PANEL 684EB - [SDR REXA2022070501462](https://openairdocs.org/sdr/REXA2022070501462.md): Latch · chafed · Jun 8, 2022 · N917XJ · Cndair CL6002D24 · Engine Cowling System > RH LOWER TRANSCOWL LATCH COAMING HAS CHAFED AREA WITH 100% MATERIAL LOSS REPLACED RH LOWER TRANSCOWL LATCH COAMING. - [SDR REXA2022070501461](https://openairdocs.org/sdr/REXA2022070501461.md): Latch · chafed · Jun 8, 2022 · N917XJ · Cndair CL6002D24 · Engine Cowling System > LH UPPER TRANSCOWL LATCH COAMING HAS CHAFED AREA WITH 100% MATERIAL LOSS REPLACED LH UPPER TRANSCOWL LATCH COAMING. - [SDR REXA2022070501460](https://openairdocs.org/sdr/REXA2022070501460.md): Lug · worn · Jun 7, 2022 · N917XJ · Cndair CL6002D24 · Ailerons > LH AILERON IB PCU ATTACHMENT LUG SCORED. AFTER BLENDING INSIDE DIAMETER IS.9392" REMOVED AND REPLACE LH AILERON - [SDR REXA2022070501459](https://openairdocs.org/sdr/REXA2022070501459.md): Lug · cracked · Jun 7, 2022 · N917XJ · Cndair CL6002D24 · Ailerons > RH AILERON IB PCU ATTACHMENT LUG CRACKED REMOVED AND REPLACED RH AILERON - [SDR REXA2022070501458](https://openairdocs.org/sdr/REXA2022070501458.md): Stringer · corroded · May 29, 2022 · N917XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer > STRINGER 21R HAS MULTIPLE AREAS OF CORROSION BETWEEN FS310-333 WITH 100% MATERIAL LOSS REPLACED STRINGER 21R. - [SDR REXA2022070501457](https://openairdocs.org/sdr/REXA2022070501457.md): Door Latch · corroded · May 22, 2022 · N917XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > PAX DOOR LOWER FRAME FWD CORNER ATTACH CLIP CORRODED, CORROSION.028" DEEP REPLACE CLIP - [SDR REXA2022070501456](https://openairdocs.org/sdr/REXA2022070501456.md): Stringer · corroded · May 21, 2022 · N917XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > STRINGER 18R HAS MULTIPLE AREAS OF CORROSION BETWEEN FS280-295 WITH 100% MATERIAL LOSS REPLACED STRINGER 18R. - [SDR REXA2022071801597](https://openairdocs.org/sdr/REXA2022071801597.md): Cover · cracked · May 18, 2022 · N917XJ · Cndair CL6002D24 · Passenger/Crew Doors > PAX DOOR AFT HINGE COVER CORNER BROKEN OUT. REPLACED PAX DOOR AFT HINGE COVER - [SDR REXA2022070501455](https://openairdocs.org/sdr/REXA2022070501455.md): Frame · corroded · May 16, 2022 · N917XJ · Cndair CL6002D24 · Fuselage Main, Frame > FS310.00 FRAME CORRODED BETWEEN STR 26R-26L. CORROSION MEASURES 5.0" X.7" X.015" DEEP. PERFORM FLANGE REPAIR PER CRJ 900 SRM 53-00-06.. - [SDR REXA2022070501454](https://openairdocs.org/sdr/REXA2022070501454.md): Splice · corroded · May 15, 2022 · N917XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > STRINGER 24R SPLICE AT FS 333.00 HAS CORROSION WITH 100% MATERIAL LOSS. REPLACED STRINGER 24R SPLICE AT FS 333.00 - [SDR REXA2022070501451](https://openairdocs.org/sdr/REXA2022070501451.md): Splice · corroded · May 15, 2022 · N917XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer > STR 22R SPLICE HAS MULTIPLE AREAS OF CORROSION WITH 100% MATERIAL LOSS REPLACE STR 22R SPLICE AT FS333.00 - [SDR REXA2022070501443](https://openairdocs.org/sdr/REXA2022070501443.md): Stringer · corroded · May 14, 2022 · N917XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer > STRINGER 21R SPLICE AT FS 333.00 HAS MULTIPLE AREAS OF CORROSION WITH 100% MATERIAL LOSS REPLACE STRINGER 21R SPLICE AT FS 333.00 - [SDR REXA2022070501442](https://openairdocs.org/sdr/REXA2022070501442.md): Stiffener · cracked · May 13, 2022 · N917XJ · Cndair CL6002D24 · Passenger/Crew Doors > PAX DOOR AFT RISER VERTICAL STIFFENER CRACKED. REPLACED STIFFENER - [SDR REXA2022070501441](https://openairdocs.org/sdr/REXA2022070501441.md): Stringer · corroded · May 12, 2022 · N917XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer > STRINGER 21R HAS MULTIPLE AREAS OF CORROSION BETWEEN FS333-349 WITH 100% MATERIAL LOSS. REPLACED STRINGER 21R. - [SDR REXA2022070501440](https://openairdocs.org/sdr/REXA2022070501440.md): Stringer · corroded · May 10, 2022 · N917XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer > STR 22L HAS AREAS OF CORROSION WITH 100% MATERIAL LOSS BETWEEN FS295-310 REMOVE AND REPLACE STR 22L FROM FS280-333. - [SDR REXA2022070501439](https://openairdocs.org/sdr/REXA2022070501439.md): Stringer · corroded · May 10, 2022 · N917XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer > STR 22R HAS MULTIPLE SPOTS OF CORROSION WITH 100% MATERIAL LOSS BETWEEN FS310-319 REMOVE AND REPLACE STR 24R. - [SDR REXA2022070501436](https://openairdocs.org/sdr/REXA2022070501436.md): Stringer · corroded · May 9, 2022 · N917XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer > STRINGER 21L HAS AREA OF CORROSION BETWEEN FS394-409, BLENDED CORROSION DIMENSIONS AS FOLLOWS, 1.0" X.50" X.010" DEEP. REPLACED STRINGER 21L. - [SDR REXA2022070501435](https://openairdocs.org/sdr/REXA2022070501435.md): Intercostal · corroded · May 9, 2022 · N917XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > INTERCOSTAL AT STR20R BETWEEN FS319-349 WEB IS CORRODED WITH 100% MATERIAL LOSS. REMOVE AND REPLACE INTERCOSTAL.. - [SDR REXA2022070501434](https://openairdocs.org/sdr/REXA2022070501434.md): Door Sill · corroded · May 8, 2022 · N917XJ · Cndair CL6002D24 · Cargo/Baggage Doors > AFT CARGO DOOR LOWER SILL HAS MULTIPLE AREAS OF CORROSION WITH A MAX DEPTH OF.011" REPLACED AFT CARGO DOOR LOWER SILL - [SDR REXA2022070501453](https://openairdocs.org/sdr/REXA2022070501453.md): Stringer · corroded · May 6, 2022 · N917XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer > STRINGER 20R HAS MULTIPLE SPOTS OF CORROSION WITH 100% MATERIAL LOSS BETWEEN FS 364-379 REPLACED STRINGER 20R - [SDR REXA2022070501433](https://openairdocs.org/sdr/REXA2022070501433.md): Intercostal · corroded · May 6, 2022 · N917XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer > INTERCOSTAL AT STR 20R BETWEEN FS349-364 HAS AREA OF CORROSION ON THE WEB WITH 100% MATERIAL LOSS. REPLACE INTERCOSTAL - [SDR REXA2022070501432](https://openairdocs.org/sdr/REXA2022070501432.md): Stringer · corroded · May 6, 2022 · N917XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer > STRINGER 20R CLIP AT FS 310.00 HAS EXFOLIATED CORROSION REPLACE STRINGER 20R CLIP AT FS 310.00 - [SDR REXA2022070501431](https://openairdocs.org/sdr/REXA2022070501431.md): Stringer · corroded · May 6, 2022 · N917XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer > STRINGER 19R HAS AREAS OF CORROSION BETWEEN FS295-310 WITH 100% MATERIAL LOSS REMOVE AND REPLACE STRINGER 19R FROM FS280-319. - [SDR REXA2022070501430](https://openairdocs.org/sdr/REXA2022070501430.md): Transcowl · cracked · May 5, 2022 · N917XJ · Cndair CL6002D24 · Engine Cowling System > RH ENGINE LOWER TRANSCOWL HAS 2 EA. CRACKS ON THE INNER SKIN, WITH A MAX LENGTH OF.75". REPAIRED RH LOWER TRANSCOWL PER EA CRJ954-13806. - [SDR REXA2022070501429](https://openairdocs.org/sdr/REXA2022070501429.md): Latch · cracked · May 5, 2022 · N917XJ · Cndair CL6002D24 · Engine Cowling System > LH LOWER TRANSCOWL LATCH COAMING CHAFED. 3.0" X.40" X 100% REPLACED LH LOWER TRANSCOWL LATCH COAMING. - [SDR REXA2022070501428](https://openairdocs.org/sdr/REXA2022070501428.md): Stringer · corroded · May 3, 2022 · N917XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer > STR 19R CORRODED BETWEEN FS469-485. CORROSION MEASURES 5.0" X 1.0" X.030" DEEP REMOVE AND REPLACE STR 19R. - [SDR REXA2022071801596](https://openairdocs.org/sdr/REXA2022071801596.md): Handle · cracked · May 2, 2022 · N917XJ · Cndair CL6002D24 · Passenger/Crew Doors > PAX DOOR INNER HANDLE HAS.50" CRACK REPLACED PAX DOOR INNER HANDLE - [SDR REXA2022070601470](https://openairdocs.org/sdr/REXA2022070601470.md): Handle · cracked · May 2, 2022 · N917XJ · Cndair CL6002D24 · Passenger/Crew Doors > PAX DOOR OUTER HANDLE FLAP HAS.350" CRACK REPLACED PAX DOOR OUTER HANDLE FLAP - [SDR REXA2022070501427](https://openairdocs.org/sdr/REXA2022070501427.md): Seat Track · corroded · May 2, 2022 · N917XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > LH FLOOR SEAT TRACK HAS MULTIPLE AREAS OF CORROSION BETWEEN FS 849-954 OVER.020" DEEP REPLACED LH FLOOR SEAT TRACK BETWEEN FS 849-954 - [SDR REXA2022070501426](https://openairdocs.org/sdr/REXA2022070501426.md): Seat Track · corroded · May 2, 2022 · N917XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > LH SIDE SEAT TRACK HAS MULTIPLE AREAS OF CORROSION BETWEEN FS 549-666 OVER.020" DEEP REPLACED LH SIDE SEAT TRACK FROM FS 549-666 - [SDR REXA2022070101425](https://openairdocs.org/sdr/REXA2022070101425.md): Seat Track · corroded · May 2, 2022 · N917XJ · Cndair CL6002D24 · Fuselage Floor Panel > RH FLOOR SEAT TRACK HAS MULTIPLE AREAS OF CORROSION BETWEEN FS700-720 OVER.025". REPLACED RH FLOOR SEAT TRACK BETWEEN FS 700-720 - [SDR REXA2022070101424](https://openairdocs.org/sdr/REXA2022070101424.md): Intercostal · corroded · May 2, 2022 · N917XJ · Cndair CL6002D24 · Passenger/Crew Doors > PAX DOOR 7TH INTERCOSTAL DOWN FROM TOP, MIDDLE SECTION, HAS AREAS OF CORROSION WITH 100% MATERIAL LOSS. REPLACED INTERCOSTAL - [SDR REXA2022063001423](https://openairdocs.org/sdr/REXA2022063001423.md): Bracket · cracked · May 2, 2022 · N917XJ · Cndair CL6002D24 · Passenger/Crew Doors > PAX DOOR FWD HANDRAIL CUP HAS.5" CRACK. REPLACED FWD HANDRAIL CUP - [SDR REXA2022063001422](https://openairdocs.org/sdr/REXA2022063001422.md): Riser · corroded · May 2, 2022 · N917XJ · Cndair CL6002D24 · Passenger/Crew Doors > PAX DOOR FWD RISER HAS 25 EA. AREAS OF CORROSION WITH A MAX DEPTH OF.009". REMOVE AND REPLACE PAX DOOR FWD RISER. - [SDR REXA2022063001421](https://openairdocs.org/sdr/REXA2022063001421.md): Riser · corroded · May 2, 2022 · N917XJ · Cndair CL6002D24 · Passenger/Crew Doors > PAX DOOR AFT RISER HAS MULTIPLE AREAS OF CORROSION AND CRACKS WITH 1 EA CRACK IN A NO REPAIR AREA. REMOVE AND REPLACE PAX DOOR AFT RISER. - [SDR REXA2022063001420](https://openairdocs.org/sdr/REXA2022063001420.md): Seat Track · corroded · May 2, 2022 · N917XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > LH SIDE SEAT TRACK HAS AREA OF CORROSION AT FS 370..5" X.5" X.024" DEEP REPLACED LH SIDE SEAT TRACK FOR CORROSION AT FS 370.00 Next page: https://openairdocs.org/aircraft/N917XJ/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 = 'N917XJ' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N917XJ/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.