# Service difficulty reports: N913XJ A list on [N913XJ](https://openairdocs.org/aircraft/N913XJ.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 6 · 290 reports - [SDR REXA2026042300310](https://openairdocs.org/sdr/REXA2026042300310.md): Drag Angle · cracked · Apr 16, 2026 · N913XJ · Cndair CL6002D24 · Fuselage, Stabilizer Attach Fittings > CRACK ON RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD/AFT DRAG ANGLE BTW 61.56% STGR DATUM TO 67.5% REAR SPAR DATUM CRACK ON RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 61.56% STGR DATUM TO 67.5% REAR SPAR DATUM WAS REPAIRED PER CRJ-9 - [SDR REXA2026042300298](https://openairdocs.org/sdr/REXA2026042300298.md): Bracket · corroded · Apr 15, 2026 · N913XJ · Cndair CL6002D24 · Fuselage Main, Attach Fittings > CORROSION ON LH MLG HYDRAULIC LINES SUPPORT PLATE (UPPER AND LOWER) (IN BK, LG EXT, LG RET) ALSO ON RH MLG HYDRAULIC LINES SUPPORT PLATE (LOWER) ON MAIN WHEEL WELL AREA DUE TO EXCESSIVE CORROSION ON RH MLG HYDRAULIC LINES SUPPORT PLATE (LOWER) ON MAIN WHEEL WE - [SDR REXA2026051500591](https://openairdocs.org/sdr/REXA2026051500591.md): Drag Angle · cracked · Apr 14, 2026 · N913XJ · Cndair CL6002D24 · Fuselage, Stabilizer Attach Fittings > INITIAL INSPECTION: CRACKED AFT DRAG ANGLE AT RH STABILIZER TO FUSELAGE ATTACHMENT BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). AFT DRAG ANGLE AT RH STABILIZER TO FUSELAGE ATTACHMENT BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE - [SDR REXA2026051500590](https://openairdocs.org/sdr/REXA2026051500590.md): Drag Angle · cracked · Apr 14, 2026 · N913XJ · Cndair CL6002D24 · Fuselage, Stabilizer Attach Fittings > INITIAL INSPECTION: CRACKED AFT DRAG ANGLE AT LH STABILIZER TO FUSELAGE ATTACHMENT BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). AFT DRAG ANGLE AT LH STABILIZER TO FUSELAGE ATTACHMENT BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRAC - [SDR REXA2026042300301](https://openairdocs.org/sdr/REXA2026042300301.md): Bracket · cracked · Apr 1, 2026 · N913XJ · Cndair CL6002D24 · Engine Thrust Reverser > CRACKED ANGLE THAT SUPPORT HINGE LINE FAIRING 443BT AT RH ENGINE. ANGLE THAT SUPPORT HINGE LINE FAIRING 44EBT AT RH ENGINE WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 - [SDR REXA2026080601529](https://openairdocs.org/sdr/REXA2026080601529.md): Support · cracked · Mar 31, 2026 · N913XJ · Cndair CL6002D24 · Engine Thrust Reverser > CRACKED ANGLE THAT SUPPORT HINGE LINE FAIRING 443BT WAS FOUND AT RT ENGINE. ANGLE THAT SUPPORT HINGE LINE FAIRING 443BT AT RT ENGINE WAS REPLACED PER SRM 51-42-06-001-001-A01 - [SDR REXA2026080601528](https://openairdocs.org/sdr/REXA2026080601528.md): Fitting · corroded · Mar 31, 2026 · N913XJ · Cndair CL6002D24 · Fuselage, Equipment Attach Fittings > CORROSION ON FITTING THE FRONT RIGHT CORNER (1 EA) AT GALLEY 2 SUMMARY OF NRC 00221:FITTING THE FRONT RIGHT CORNER (1 EA) AT GALLEY 2 WAS REPLACED PER SAFRAN CMM 25-32-84 - [SDR REXA2026080601527](https://openairdocs.org/sdr/REXA2026080601527.md): Fitting · corroded · Mar 31, 2026 · N913XJ · Cndair CL6002D24 · Fuselage, Equipment Attach Fittings > CORROSION FLOOR FITTING ACCESS 109 (1EA), BEHIND ACCESS 108 (1EA), IN FRONT ACCESS 107 (1EA) AT GALLEY 1 SUMMARY OF NRC 00220: FLOOR FITTING ACCESS 109 (1EA), BEHIND ACCESS 108 (1EA), IN FRONT ACCESS 107 (1EA) AND DOUBLER (1EA) IN FRONT ACCESS (107) AT GAL - [SDR REXA2026042300309](https://openairdocs.org/sdr/REXA2026042300309.md): Hinge Fitting · corroded · Mar 30, 2026 · N913XJ · Cndair CL6002D24 · Fuselage, Door Hinge > CORROSION WAS FOUND ON LH/RH NLG AFT DOOR HINGE FITTING (2 EAS) AND CORROSION ON RH/LH AIRFRAME HINGE FITTING (2 EAS) AT NLG DUE EXCESSIVE CORROSION RH NLG AFT DOOR HINGE FITTING WAS REPLACED AND MODIFIED PER EA NO. CR952-22005 REV IR AND CRJ 900 SRM 51-10-0 - [SDR REXA2026042300308](https://openairdocs.org/sdr/REXA2026042300308.md): Hinge Fitting · corroded · Mar 30, 2026 · N913XJ · Cndair CL6002D24 · Fuselage, Door Hinge > CORROSION WAS FOUND ON LH/RH NLG AFT DOOR HINGE FITTING (2 EAS) AND CORROSION ON RH/LH AIRFRAME HINGE FITTING (2 EAS) AT NLG DUE EXCESSIVE CORROSION RH/LH AIRFRAME HINGE FITTING WERE REPLACED PER CRJ 900 SRM 51-10-06-001-001-A01, SRM 51-42-21-001-001-A01 - [SDR REXA2026042300307](https://openairdocs.org/sdr/REXA2026042300307.md): Hinge Fitting · corroded · Mar 30, 2026 · N913XJ · Cndair CL6002D24 · Fuselage, Door Hinge > CORROSION WAS FOUND ON LH/RH NLG AFT DOOR HINGE FITTING (2 EAS) AND CORROSION ON RH/LH AIRFRAME HINGE FITTING (2 EAS) AT NLG DUE EXCESSIVE CORROSION RH NLG AFT DOOR HINGE FITTING WAS REPLACED AND MODIFIED PER EA NO. CR952-22005 REV IR AND CRJ 900 SRM 51-10-0 - [SDR REXA2026042300319](https://openairdocs.org/sdr/REXA2026042300319.md): Lug · corroded · Mar 29, 2026 · N913XJ · Cndair CL6002D24 · Ailerons > CORROSION ON CENTER FITTING LUG L1, L2, L3, L4, L5, L6 AT AILERON WAS FOUND. LUGS BORE L3 & L4 AT CENTER FITTING OF LH AILERON WERE CLEANED PER CRJ 900 SRM 51-26-00-001-001-A01 AND LUGS BORE L1, L2, L5 & L6 WAS REPAIRED PER REO 670-57-61-107 REV:-B - [SDR REXA2026042300318](https://openairdocs.org/sdr/REXA2026042300318.md): Lug · corroded · Mar 29, 2026 · N913XJ · Cndair CL6002D24 · Ailerons > CORROSION WAS FOUND ON LUG BORE R2, R5 AND SCRATCHES ON BORE LUG R4(CENTER FITTING) AT RH AILERON. LUG BORE R4 AT CENTTER FITTING WAS CLEANED PER CRJ 900 SRM 51-26-00-001-001-A01 AND LUG BORE R2 AND R5 WERE REPAIRED PER REO 690-57-61-237 REV:-- & REO 690-57-61 - [SDR REXA2026042300302](https://openairdocs.org/sdr/REXA2026042300302.md): Door Sill · cracked · Mar 29, 2026 · N913XJ · Cndair CL6002D24 · Fuselage Main, Structure > CRACK ON AFT RH DOOR LANDING AT FS 188.00 (LATCH CUT OUT OF ACCESS DOOR 212AR). AFT RH DOOR LANDING AT FS 188.00 (LATCH CUT OUT OF ACCESS DOOR 212AR) WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01, CRJ/900 SRM 51-42-10-001-001-A01 AND SRM 51-42-13-001-001- - [SDR REXA2026042400314](https://openairdocs.org/sdr/REXA2026042400314.md): Transcowl · cracked · Mar 27, 2026 · N913XJ · Cndair CL6002D24 · Engine Thrust Reverser > CRACKS IN HOLES ON TRANSCOWL INNER SKIN AND ALSO MISSING IDENTIFICATION PLACARD AT RH LOWER TRANSCOWL. TRANSCOWL INNER SKIN WAS REPAIRED PER EA CRJ954-21989 REV.IR AND IDENTIFICATION PLACARD WAS INSTALLED PER CRJ-900 SRM 51-42-10-001-001-A01 - [SDR REXA2026042300306](https://openairdocs.org/sdr/REXA2026042300306.md): Support · cracked · Mar 27, 2026 · N913XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CRACKS ON SUPPORT BASE MAIN BATTERY DIRECT BUS (JB6) AT FWD EQUIPMENT COMPARTMENT SUPPORT BASE MAIN BATTERY DIRECT BUS (JB6) AT FWD EQUIPMENT COMPARTMENT WAS REPLACED PER CRJ 900 SRM 51-42-06-001-001-A01 - [SDR REXA2026042300305](https://openairdocs.org/sdr/REXA2026042300305.md): Seat Track · corroded · Mar 27, 2026 · N913XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings > CORROSION ON SEAT TRACKS LBL9 AND RBL 9 BTW FS 349.00 TO 394.00 AT PASSENGER CABIN. CORROSION ON SEAT TRACKS LBL9 AND RBL 9 BTW FS 349.00 TO 394.00 AT PASSENGER CABIN WAS EVALUATED OUT OFF LIMITS PER CRJ 900 SRM 53-21-49-101-001-A01 AND SEAT RAILS WERE REPLACE - [SDR REXA2026042300304](https://openairdocs.org/sdr/REXA2026042300304.md): Floor Support · cracked · Mar 27, 2026 · N913XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CRACKED FLOOR ANGLES SUPPORTS BTW FS 259.00 AND 280.00 AND RBL12/ LBL12 AT FLOOR STURCTURE. FLOOR ANGLE SUPPORT BTW FS 259.00 AND 280.00 AND RBL12 WAS FABRICATED PER EA NO. CRJ953-21975 REV. IR AND RBL 12 AT FLOOR ANGLES SUPPORT STURCTURE WAS REPLACED PER CRJ- - [SDR REXA2026042300303](https://openairdocs.org/sdr/REXA2026042300303.md): Floor Support · cracked · Mar 27, 2026 · N913XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CRACKED FLOOR ANGLES SUPPORTS BTW FS 259.00 AND 280.00 AND RBL12/ LBL12 AT FLOOR STURCTURE. FLOOR ANGLE SUPPORT BTW FS 259.00 AND 280.00 AND LBL12 WAS REPLACED PER CRJ-900 SRM 51-42-13-001-001-A01 AND SRM 51-42-06-001-001-A01 - [SDR REXA2026042300317](https://openairdocs.org/sdr/REXA2026042300317.md): Bracket · corroded · Mar 26, 2026 · N913XJ · Cndair CL6002D24 · Aerodynamic Fairings > CORROSION ON ANGLES SUPPORTS OF REFUEL/DEFUEL CONTROL PANEL AT FAIRING 192BB. ANGLES SUPPORTS OF REFUEL/DEFUEL CONTROL PANEL AT FAIRING 192BB WAS REPLACED PER CRJ/900 SRM 51-42-10-001-001-A01 - [SDR REXA2026042300316](https://openairdocs.org/sdr/REXA2026042300316.md): Bracket · corroded · Mar 26, 2026 · N913XJ · Cndair CL6002D24 · Aerodynamic Fairings > CORROSION ON ANGLES SUPPORTS OF REFUEL/DEFUEL CONTROL PANEL AT FAIRING 192BB. ANGLES SUPPORTS OF REFUEL/DEFUEL CONTROL PANEL AT FAIRING 192BB WAS REPLACED PER CRJ/900 SRM 51-42-10-001-001-A01 - [SDR REXA2026042300300](https://openairdocs.org/sdr/REXA2026042300300.md): Fairing · corroded · Mar 26, 2026 · N913XJ · Cndair CL6002D24 · Aerodynamic Fairings > CORROSION ON SETTLEMENT AREA OF FUSELAJE FAIRINGS 196DR, 195DL, 195BB AND 195AB. CORROSION ON SETTLEMENT AREA OF FUSELAGE FAIRINGS 196DR, 195DL, 195BB AND 195AB WERE REMOVED PER CRJ 900 SRM 51-21-06-001-001-A01. SETTLEMENT AREA SUPPORT OF FAIRINGS 196DR, 195DL - [SDR REXA2026042300315](https://openairdocs.org/sdr/REXA2026042300315.md): Drag Angle · cracked · Mar 25, 2026 · N913XJ · Cndair CL6002D24 · Fuselage, Stabilizer Attach Fittings > INITIAL INSPECTION: CRACK ON LH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD AND AFT DRAG ANGLE BTW 61.56% STGR DATUM TO 67.5% REAR SPAR DATUM. LH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD AND AFT DRAG ANGLE BTW 61.56% STGR DATUM TO 67.5% REAR SPAR DAT - [SDR REXA2026042300299](https://openairdocs.org/sdr/REXA2026042300299.md): Handle · cracked · Mar 25, 2026 · N913XJ · Cndair CL6002D24 · Cargo/Baggage Doors > CRACK AT AFT CARGO DOOR HANDLE HOUSING (AFT END) AFT CARGO DOOR HANDLE HOUSING WAS REPLACED PER. CRJ-900 AMM 52-31-03 AND SRM 51-42-21-001-001-A01 - [SDR REXA2025101700955](https://openairdocs.org/sdr/REXA2025101700955.md): Bulb · inoperative · Oct 15, 2025 · N913XJ · Cndair CL6002D24 · Emergency Lighting > FOUND EXTERIOR RT FWD EMER LIGHT OUT. R & R RH EXTERIOR FWD EMER LIGHT BULB IAW AMM 33-51-15. PN OFF/ON: 8GA411060-06 - [SDR REXA2022033000268](https://openairdocs.org/sdr/REXA2022033000268.md): Unknown · inoperative · Mar 29, 2023 · N913XJ · Cndair CL6002D24 · Passenger/Crew Doors > MAIN CABIN DOOR WONT FULLY SHUT, THEN BINDS, AND WONT OPEN ADJUSTED FWD UPPER TENSION BUTTON TIE PER AMM 52-11-19. FOUND FWD HANDRAIL ACTUATOR ROD OUT OF LIMITS. ADJUSTED ROD PER AMM 52-11-05. PERFORMED OPS TEST AND FUNCTIONAL TEST PER AMM 52-11-00 OPS, FUN - [SDR REXA2022110102324](https://openairdocs.org/sdr/REXA2022110102324.md): Bulb · inoperative · Oct 23, 2022 · N913XJ · Cndair CL6002D24 · Emergency Lighting > LEFT AFT OUTSIDE EMERGENCY LIGHT INOP EMERGENCY LIGHT INOP. CORRECTIVE ACTION: REMOVED 4 SCREWS AND COVER. REMOVED AND REPLACED L/H AFT OUTSIDE EMERGENCY BULB WITH P/N 8GH0024-73-08. INSTALLED COVER AND 4 SCREWS IAW CRJ900 AMM 20-21-00-910-801- A01. OP TEST GO - [SDR REXA2022102502283](https://openairdocs.org/sdr/REXA2022102502283.md): Angle · corroded · Oct 17, 2022 · N913XJ · Cndair CL6002D24 · Passenger/Crew Doors > PAX DOOR UPPER SEAL ANGLE IS CORRODED. REMOVED CAP ANGLE IAW CRJ 900 SRM 51-41-02-001-001-A01. LOCATED AND DRILLED NEW MID CAP ANGLE IAW CRJ 900 SRM 51-40-11-001-001-A01. INSTALLED CAP ANGLE IAW CRJ 900 SRM 51-41-02-001-001-A01. - [SDR REXA2022102502287](https://openairdocs.org/sdr/REXA2022102502287.md): Intercostal · corroded · Oct 15, 2022 · N913XJ · Cndair CL6002D24 · Passenger/Crew Doors > PAX DOOR, INTERCOSTAL FWD DD4 IS CORRODED. INSTALLED NEW INTERCOSTAL IAW CRJ 900 SRM 51-42-06-001-001-A01 - [SDR REXA2022102502286](https://openairdocs.org/sdr/REXA2022102502286.md): Intercostal · corroded · Oct 15, 2022 · N913XJ · Cndair CL6002D24 · Passenger/Crew Doors > PAX DOOR, INTERCOSTAL FWD DD5 IS CORRODED. INSTALLED NEW INTERCOSTAL IAW CRJ 900 SRM 51-42-06-001-001-A01 - [SDR REXA2022102502285](https://openairdocs.org/sdr/REXA2022102502285.md): Stringer · corroded · Oct 15, 2022 · N913XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer > CORROSION FOUND ON STR22 L LOCATED BETWEEN F.S 333 TO F.S 349 REMOVED AND INSTALLED NEW SECTION STRINGER BETWEEN FS 333 TO FS 364+7.5 AND STRINGER 22L IAW CRJ 900 SRM 53-00-03-201-001-A01. REMOVED AND INSTALLED 3 CLEATS AT STRINGER 22L FS 333 AND FS 364 IAW CR - [SDR REXA2022102502284](https://openairdocs.org/sdr/REXA2022102502284.md): Bracket · corroded · Oct 15, 2022 · N913XJ · Cndair CL6002D24 · Cargo/Baggage Doors > CENTER CARGO DOOR AFT H BRACKET IS CORRODED AT F.S. 661+8.40. REPAIR WAS DONE IAW ENDEAVOR EA CRJ953-14611 REV. IR DATED 09/24/2022 - [SDR REXA2022102502281](https://openairdocs.org/sdr/REXA2022102502281.md): Housing · gouged · Oct 15, 2022 · N913XJ · Cndair CL6002D24 · Cargo/Baggage Doors > AFT CARGO DOOR HANDLE CUT OUT IS GOUGED INSTALLED NEW HANDLE HOUSING ON AFT CARGO DOOR IAW CRJ-900SRM51-42-21-001-001-A01 - [SDR REXA2022102502280](https://openairdocs.org/sdr/REXA2022102502280.md): Floor Support · corroded · Oct 14, 2022 · N913XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > L/H FLOOR SILL IS CORRODED BETWEEN F.S. 785.15 TO F.S. 797. REPAIRED IAW ENDEAVOR EA CRJ953-14491 DATE 09/17/2022 EA REV IR. - [SDR REXA2022101902279](https://openairdocs.org/sdr/REXA2022101902279.md): Pressure Deck · corroded · Oct 14, 2022 · N913XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > R/H PRESSURE FLOOR SILL IS CORRODED BETWEEN F.S. 797 TO F.S. 813. REPAIRED IAW ENDEAVOR EA CRJ953-14601 DATED 09/23/2022 REV IR. - [SDR REXA2022101702277](https://openairdocs.org/sdr/REXA2022101702277.md): None · corroded · Oct 13, 2022 · N913XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > R/H FLOOR SILL IS CORRODED BETWEEN F.S. 310 TO F.S. 319. REPLACED SILL AND ATTACH ANGLE IAW CRJ-900-SRM-51-42-06-001-001-A01, CRJ-900-SRM-51-42-13-001-001-A01, AND CRJ-900-SRM-51-42-15-001-001-A01 (P/N OF SILL SH670-32172-11, ANGLE SH670-32177-1) - [SDR REXA2022101702276](https://openairdocs.org/sdr/REXA2022101702276.md): None · corroded · Oct 13, 2022 · N913XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CORROSION FOUND ON RH SIDE SEAT RAIL BETWEEN FS661+90 AND FS672. REMOVED AND REPLACED IAW CRJ 900 SRMS 51-40-11-001-001-A01, 53-00-49-201-002-A01, AND CRJ 900 AMM 53-00-49-400-801-A07. - [SDR REXA2022101702275](https://openairdocs.org/sdr/REXA2022101702275.md): None · corroded · Oct 13, 2022 · N913XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CORROSION FOUND RH SIDE SEAT RAIL BETWEEN FS 483.00-571.00 REMOVED AND REPLACED IAW CRJ 900 SRMS 51-40-11-001-001-A01, 53-00-49-201-002-A01, AND CRJ 900 AMM 53-00-49-400-801-A07. - [SDR REXA2022101702274](https://openairdocs.org/sdr/REXA2022101702274.md): Intercostal · corroded · Oct 13, 2022 · N913XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > INTERCOSTAL IS CORRODED BETWEEN F.S. 849 TO F.S. 881 AT STGR 21R. REPAIRED IAW ENDEAVOR EA CRJ953-14608 REV IR DATED 09/30/2022 - [SDR REXA2022101402264](https://openairdocs.org/sdr/REXA2022101402264.md): Bracket · corroded · Oct 12, 2022 · N913XJ · Cndair CL6002D24 · Passenger/Crew Doors > FOUND BRACKET ON AFT DD5 TO BE CORRODED ON PAX DOOR. REMOVED AND REPLACED IAW CRJ 900 SRMS 51-40-11-001-001-A01, AND 51-42-06-001-001-A01. - [SDR REXA2022101402263](https://openairdocs.org/sdr/REXA2022101402263.md): Stringer · corroded · Oct 12, 2022 · N913XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > STGR 19R FS 280 - 319 IS CORRODED. REMOVED AND REPLACED IAW CRJ900 SRMS 51-40-11-001-001-A01, 51-42-06-001-001-A01 AND 51-42-21-001-001-A01 - [SDR REXA2022101402262](https://openairdocs.org/sdr/REXA2022101402262.md): Angle · corroded · Oct 12, 2022 · N913XJ · Cndair CL6002D24 · Passenger/Crew Doors > PAX DOOR AFT DRAG ANGLE IS CRACKED REMOVED AND REPLACED IAW CRJ900 SRMS 51-40-11-001-001-A01, AND 51-42-06-001-001-A01. - [SDR REXA2022101402261](https://openairdocs.org/sdr/REXA2022101402261.md): Intercostal · corroded · Oct 12, 2022 · N913XJ · Cndair CL6002D24 · Passenger/Crew Doors > PAX DOOR DD6 MID INTERCOSTAL IS CORRODED. REMOVED AND REPLACED IAW CRJ900 SRMS 51-40-11-001-001-A01, 51-42-06-001-001-A01 AND 51-42-21-001-001-A01 - [SDR REXA2022101402260](https://openairdocs.org/sdr/REXA2022101402260.md): Former · corroded · Oct 12, 2022 · N913XJ · Cndair CL6002D24 · Passenger/Crew Doors > PAX DOOR FWD FORMER IS CORRODED IN MULTIPLE AREAS. REMOVED AND REPLACED IAW CRJ900 SRM 51-42-06-001-001-A01 AND 51-42-13-001-001-A01 - [SDR REXA2022101302249](https://openairdocs.org/sdr/REXA2022101302249.md): Support Angle · corroded · Oct 11, 2022 · N913XJ · Cndair CL6002D24 · Passenger/Crew Doors > PAX DOOR FWD SUPPORT ANGLE FOUND CORRODED REMOVED AND REPLACED PAX DOOR FWD SUPPORT ANGLE P/N 601R318731-3 IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 AND 51-42-21-001–001-A0 - [SDR REXA2022101302248](https://openairdocs.org/sdr/REXA2022101302248.md): Angle · corroded · Oct 11, 2022 · N913XJ · Cndair CL6002D24 · Passenger/Crew Doors > PAX DOOR UPPER SILL ANGLE IS CORRODED REMOVED KICKPLATE ANGLE IAW CRJ 900 SRM 51-42-06-001-001-A01 AND INSTALLED NEW SERVICABLE KICKPLATE ANGLE IAW CRJ 900 SRM 51-42-06-001-001-A01 - [SDR REXA2022101302247](https://openairdocs.org/sdr/REXA2022101302247.md): Seat Track · corroded · Oct 11, 2022 · N913XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings > RBL9 FLOOR SEAT TRACK IS CORRODED BETWEEN F.S. 693 TO F.S. 847. FABRICATED AND REPLACED SEAT TRACK AT RBL9 BETWEEN F.S.693-F.S.847 IAW AMM 53-00-49-400-801-A07 AND CRJ900 SRM 53-00-49-201-002-A01 - [SDR REXA2022101102243](https://openairdocs.org/sdr/REXA2022101102243.md): Frame · corroded · Oct 9, 2022 · N913XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CORROSION FOUND ON FRAME AT F.S 319 AND STR 21L REMOVED FRAME AT F.S 319 BETWEEN STR 21L-18L IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. INSTALLED NEW SERVICEABLE FRAME AT F.S 319 BETWEEN STR 21L-18L IAW CRJ 900 SRM 51-42-06-001-001-A01 AND - [SDR REXA2022101102237](https://openairdocs.org/sdr/REXA2022101102237.md): Intercostal · corroded · Oct 9, 2022 · N913XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > SUPPORT INTERCOSTAL LEFT OF STGR 27 IS CORRODED BETWEEN FS 349.00 AND 364.00 LOCATED AND DRILLED NEW INTERCOSTAL PN SH670-32075-3S I.A.W. CRJ900 SRM 51-40-11-001-001-A01. INSTALLED NEW SERVICEABLE INTERCOSTAL P/N SH670-32075-3S JUST LEFT OF STIR 27 BETWEEN FS - [SDR REXA2022101102236](https://openairdocs.org/sdr/REXA2022101102236.md): None · corroded · Oct 7, 2022 · N913XJ · Cndair CL6002D24 · Passenger/Crew Doors > PAX DOOR CLIPS ON FS 320 HINGE SIDE ARE CORRODED. REMOVED DAMAGED CLIPS, LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE CLIPS PN601R319034-1/2 IAW CRJ 900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01 Next page: https://openairdocs.org/aircraft/N913XJ/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 = 'N913XJ' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N913XJ/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.