# Service difficulty reports: N907XJ

A list on [N907XJ](https://openairdocs.org/aircraft/N907XJ.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 · 161 reports

- [SDR REXA2026021000052](https://openairdocs.org/sdr/REXA2026021000052.md): Striker · corroded · Feb 9, 2026 · N907XJ · Cndair CL6002D24 · Service Doors
  > FOUND GALLY SERVICE DOOR LWR SEAL STRIKER TO BE CORRODED AROUND FASTENER HOLES. REPLACED SERVICE DOOR SEAL STRIKER WITH PN SH67031412-S0701 IAW MHIRJ SNIEOS SH670-31412-S07 AND SH670-31950-S21. INSTALLED NEW SERVICEABLE FABRICATED SERVICE DOOR LWR SEAL STRIK
- [SDR REXA2026020900050](https://openairdocs.org/sdr/REXA2026020900050.md): Skin · chafed · Feb 8, 2026 · N907XJ · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > FOUND MULTIPLE CHAFED ON BELLY OF AIRCRAFT AT FS 933. REPAIRED FUSELAGE SKIN IAW EA CRJ953-19682 REV IR DATED 1/22/26.
- [SDR REXA2025080600796](https://openairdocs.org/sdr/REXA2025080600796.md): Lamp · inoperative · Aug 5, 2025 · N907XJ · Cndair CL6002D24 · Emergency Lighting
  > OVERWING DOOR RH AFT EXTERNAL EMER LIGHT INOP. REPLACED BULB AT RH AFT OVERWING DOOR EXT EMER LIGHT, OPS TEST GOOD PER AMM 33-51-15. PN: 8GH005123-06.
- [SDR REXA2025021900206](https://openairdocs.org/sdr/REXA2025021900206.md): Charger · inoperative · Feb 19, 2025 · N907XJ · Cndair CL6002D24 · Emergency Lighting
  > PAX DOOR EMER LIGHT HAS NO VOLTAGE GOING TO IT. LIGHT IS INOP. REPLACED PS35 CHARGER (ESPU 1) P/N 11-0049 S/N OFF 27241 S/N ON 10974 IAW AMM 35-51-17. OPS CHECK GOOD, SEE BELOW FOR WORK DETAILS CONTINUATION CARDS: 162942, 162943, 162944
- [SDR REXA2024082200658](https://openairdocs.org/sdr/REXA2024082200658.md): Windshield · cracked · Aug 10, 2024 · N907XJ · Cndair CL6002D24 · Flight Compartment Windows
  > CLIMBING THROUGH FL 240 CAPTAIN SIDE WINDOW CRACKED AND ARCED. DEPLOYED PASSENGER O2 MASKS AND DIVERTED TO JFK. R & R CAPTAIN SIDE WINDSHIELD IAW JC 900-56-900-901. CLEANED AND RESTOWED PASSENGER MASKS IAW AMM 35-21-09. OPS CHECK GOOD.
- [SDR REXA2022092902152](https://openairdocs.org/sdr/REXA2022092902152.md): Harness · damaged · Sep 23, 2022 · N907XJ · Cndair CL6002D24 · Emergency Lighting
  > CB PANEL 1: E3 AND M10 POPPING; CB PANEL 2: U3 POPPING. LOST CABIN READING LTS AND PASS SIGNS, EMERGENCY LIGHTS ON AND OFF UNCOMMANDED THROUGHOUT FLIGHT. T/S & FOUND WIRING HARNESS P5402/P340 DAMAGED. REMOVED L FWD WARDROBE UNIT IAW 25-24-01. R&R P5402/P340 WI
- [SDR REXA2022062201286](https://openairdocs.org/sdr/REXA2022062201286.md): Frame · cracked · Jun 14, 2022 · N907XJ · Cndair CL6002D24 · Emergency Exits
  > LH AFT EMERGENCY EXIT DOOR AFT MICROSWITCH BRACKET HAS SUSPECTED CRACK ON LOWER SECTION. PERFORMED CUT-OUT AND APPLIED DOUBLER. REF EA CRJ952-13352 REV IR 4/8/2022
- [SDR REXA2022060801054](https://openairdocs.org/sdr/REXA2022060801054.md): Bracket · cracked · May 22, 2022 · N907XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > THE RH FWD EMERGENCY EXIT DOOR AFT MICROSWITCH BRACKET HAS SUSPECTED CRACK ON LOWER SECTION. PERFORMED REPAIR DOUBLER REF EA NO: CRJ952-13270, DATED 4/20/2022, EA REV A
- [SDR REXA2022060801053](https://openairdocs.org/sdr/REXA2022060801053.md): Coaming · chafed · May 17, 2022 · N907XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > THE AFT BAG BAY DOOR SURROUND UPPER COAMING IS CHAFFED REMOVED AND REPLACED AFT BAGGAGE BAY DOOR SURROUND UPPER COAMING REF CRJ 900 SRM 51-41-02-001-001-A01
- [SDR REXA2022062001238](https://openairdocs.org/sdr/REXA2022062001238.md): Intercostal · corroded · May 9, 2022 · N907XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > INTERCOSTAL ON STGR 21R IS CORRODED. FS 897.00-FS 913.00 INSTALLED NEW INTERCOSTAL ON STGR 21R FS 897.00-913.00
- [SDR REXA2022060801052](https://openairdocs.org/sdr/REXA2022060801052.md): None · corroded · May 4, 2022 · N907XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FLOOR BEAM RBL 9 UPPER SURFACE IS CORRODED BETWEEN F.S. 1031.00-1069.00 REPAIRED CORROSION ON FLOOR BEAM AT RBL9 BETWEEN F.S. 977.00-1088.00 (BEAM SPLICE REPAIR) REF CRJ 900 SRM 53-00-41-201-001-A03
- [SDR REXA2020082610639](https://openairdocs.org/sdr/REXA2020082610639.md): Battery Pack · inoperative · Aug 21, 2020 · N907XJ · Cndair CL6002D24 · Emergency Lighting
  > DURNG OPS TEST OF EMERGENCY LIGHT, NOTED LTS FOR BATTERY PACK #1 PS35 DID NOT ILLUMINATE. REF NRWC 691188 CONT CARD DISC #18. R & R EPSU BATTERY PACK #1 (PS35) AND EPSU CHARGER ASSY (PS35) IAW AMM 35-17-400-801 & AMM 33-51-17-400-802. OPS TEST OK P/N:2013-1
- [SDR REXA2020070600582](https://openairdocs.org/sdr/REXA2020070600582.md): Connector · defective · Jun 15, 2020 · N907XJ · Cndair CL6002D24 · Light System Wiring
  > RT FWD EXT EMER LIGHT INOP. REPLACED PS36 & RECONNECTED CONNECTOR P341. CHECKS GOOD IAW MM 33-51-00.
- [SDR REXA2019090401320](https://openairdocs.org/sdr/REXA2019090401320.md): Plate · worn · Sep 4, 2019 · N907XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > AWR IN REF EO R53582. WEAR ON LOW PRESSURE GROUND CONNECTION PLATE. (SM)(FUS). LOW PRESSURE GROUND CONNECTION PLATE WAS REPLACED PER EA CRJ953-09559 REV IR.
- [SDR REXA2019090301318](https://openairdocs.org/sdr/REXA2019090301318.md): Strap · cracked · Sep 3, 2019 · N907XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > HIDDEN DAMAGE: AFTER CLEAN UP OF STRAP, RT STRAP WAS FOUND CRACKED. IN REF NRC S/N 00084. STRAP WAS REPLACED FOR A NEW STRAP P/N: CC670-39052-4 AND INSTALLED PER SRM 51-42-13.
- [SDR REXA2019090301316](https://openairdocs.org/sdr/REXA2019090301316.md): Door Frame · cracked · Sep 3, 2019 · N907XJ · Cndair CL6002D24 · Fuselage Main, Structure
  > PART RACK: CRACKED SCUFF PLATES ACCESS 151MLW FWD DOOR JAMB. (SM)(CCD). NEW DOOR JAMB (P/N: 9846301-1) WAS VERIFIED PER IPC 53-32-31 FIGURE 5, ITEM 290 AND IS INSTALLED UNDER JOB CARD 900-52-810-103 STEP 4.
- [SDR REXA2019090201315](https://openairdocs.org/sdr/REXA2019090201315.md): Angle · corroded · Sep 2, 2019 · N907XJ · Cndair CL6002D24 · Wing Miscellaneous Structure
  > INITIAL INSPECTION. CORROSION ON SETTLEMENT AREA OF TIRE BURN COVER 542AZ AND 542BZ AT LT MLG BAY. (TCI 500-12). CORROSION WAS REMOVED ON SETTLEMENT AREA OF TIRE BURN COVER 542AZ AND 542BZ AT LT MLG BAY PER SRM 51-21-06. AND IS WITHIN LIMITS PER SRM 57-00-01-1
- [SDR REXA2019083001308](https://openairdocs.org/sdr/REXA2019083001308.md): Floor Support · corroded · Aug 30, 2019 · N907XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > AWR CORROSION ON FLOOR SUPPORT FS 280 BTW 26L-26R. (TCI 100-09). FLOOR SUPPORT FS 280 BTW 26L-26R WAS REPLACED PER SRM 51-42-06-001-001-A01 PAR 6C AND SRM 51-42-20-001-001-A01 PAR 6C (CORROSION LEVEL 2).
- [SDR REXA2019083001307](https://openairdocs.org/sdr/REXA2019083001307.md): Stringer · corroded · Aug 30, 2019 · N907XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > AWR CORROSION ON STRINGERS 26(L/R), FS 280-325. (TCI 100-09). STRINGER 26 (R/L) FS 280/325 WERE REPLACED FOR NEW ONES PER SRM 51-42-06-001-001-A01 PAR. 6C. LEVEL CORROSION 2.
- [SDR REXA2019083001306](https://openairdocs.org/sdr/REXA2019083001306.md): Stringer · corroded · Aug 30, 2019 · N907XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > AWR CORROSION ON STRINGER 27 FS 280-297. (TCI 100-09). STRINGER 27 FS 280-297 WAS REMOVED AND WAS REPLACED A NEW ONE PER SRM 51-42-06-001-001-A01 PAR 6C LEVEL CORROSION 2.
- [SDR REXA2019082901305](https://openairdocs.org/sdr/REXA2019082901305.md): Intercostal · corroded · Aug 29, 2019 · N907XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > AWR CORROSION ON INTERCOSTALS 21L (3EAS), FROM FS 310-349. (TCI 100-09). INTERCOSTALS 21L (2EAS), FROM FS310/349 WERE REPLACED PER SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01. LEVEL CORROSION 2.
- [SDR REXA2019082901304](https://openairdocs.org/sdr/REXA2019082901304.md): Seat Track · corroded · Aug 29, 2019 · N907XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > AWR CORROSION ON SEAT RAIL LBL9 BTW FS 364-379. FLOOR SEAT RAIL LBL 9 BTW FS 364-379 WAS REPLACED PER AMM 53-00-49-400-801 (CONFIG A07) (LEVEL CORROSION 2).
- [SDR REXA2019082601309](https://openairdocs.org/sdr/REXA2019082601309.md): Seat Track · corroded · Aug 26, 2019 · N907XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > AWR IN REF NRC S/N 00008 DURING PASSENGER SEAT REMOVAL, CORROSION WAS FOUND ON SIDE RAIL STRG 15 (L/R) FROM FS 434-545. SUMMARY: SIDE RAIL STR 15R FS477 TO FS545 WAS REPLACED FOR A NEW ONE DUE CORROSION LEVEL 2 PER AMM 53-00-49-400-801-A07. THE SIDE RAIL STR 1
- [SDR REXA2019082601303](https://openairdocs.org/sdr/REXA2019082601303.md): Crossbeam · cracked · Aug 26, 2019 · N907XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > AWR: PER MTC REQUEST: DURING REMOTION CORROSION:CRACK WAS FOUND ON CROSSBEAM FS280 BTW LBL14 UPPER SIDE (W1)(SM). CROSSBEAM FS280 BTW LBL14 UPPER SIDE WAS REPLACED PER SRM 51-42-06-001-001-A01 PAR 6C AND SRM 51-42-21-001-001-A01 PAR 6C.
- [SDR REXA2019082601302](https://openairdocs.org/sdr/REXA2019082601302.md): Intercostal · corroded · Aug 26, 2019 · N907XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > AWR. CORROSION ON INTERCOSTALS 20R (2EAS), FROM FS 310-349. (TCI 100-09). INTERCOSTALS 20R (2EAS), FROM FS 310-349. WERE REPLACED PER SRM 51-42-21-001-001-A01. LEVEL CORROSION 2.
- [SDR REXA2019082601299](https://openairdocs.org/sdr/REXA2019082601299.md): Angle · corroded · Aug 26, 2019 · N907XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > INITIAL INSPECTION: CORROSION ON SILL ANGLE AT SERVICE DOOR SURROUND STRUCTURE. (R1)(TCI 53-20-219). SILL ANGLE AT SERVICE DOOR SURROUND STRUCTURE WAS REPLACED FOR A NEW ONE PER SRM 51-42-21-001-001-A01, AND 51-42-06-001-001-A01. (LEVEL CORROSION 2)
- [SDR REXA2019082601298](https://openairdocs.org/sdr/REXA2019082601298.md): Stringer · corroded · Aug 26, 2019 · N907XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > AWR:HIDEN DAMAGE: IN REFERENCE WITH THE NRC S/N 00214. CORROSION ON STRGINGER 20R FROM FS 319-349. (TCI 100-09). STRINGER 20R FROM FS 319-349 WAS REPLACED FOR A NEW ONE PER SRM 51-42-06-001-001-A01 PAR. 6 C (LEVEL CORROSION 2)
- [SDR REXA2019082601297](https://openairdocs.org/sdr/REXA2019082601297.md): Seat Track · corroded · Aug 26, 2019 · N907XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > AWR IN REF NRC S/N 00008 DURING PASSENGER SEAT REMOVAL, CORROSION WAS FOUND ON FLOOR RAIL 9RBL AND 27LBL FROM FS 434-545. FLOOR SEAT RAIL 9RBL AND 27LBL FROM FS434 TO FS545 WERE REPLACED PER AMM 53-00-49-400-801-A07. (LEVEL CORROSION 2).
- [SDR REXA2019082601296](https://openairdocs.org/sdr/REXA2019082601296.md): Seat Track · corroded · Aug 26, 2019 · N907XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > AWR IN REF NRC S/N 00010 DURING PASSENGER SEAT REMOVAL, CORROSION WAS FOUND ON FLOOR RAIL 9(LBL/RBL) FROM FS 661+67-699. FLOOR RAIL STR 9(LBL/RBL) FROM FS 661+67-699 WERE REPLACED PER AMM 53-00-49-400-801 (CONFIG A07) (LEVEL CORROSION 2)
- [SDR REXA2019082601295](https://openairdocs.org/sdr/REXA2019082601295.md): Seat Track · corroded · Aug 26, 2019 · N907XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > AWR IN REF NRC S/N 00010 DURING PASSENGER SEAT REMOVAL, CORROSION WAS FOUND ON SIDE RAIL STR 15 (L/R) FROM FS 661+67-699. SIDE SEAT RAIL STR 15 (L/R) FROM FS 661+67-699 WERE REPLACED PER PER AMM 53-00-49-400-801 (CONFIG A07). (LEVEL CORROSION 2)
- [SDR REXA2019082601294](https://openairdocs.org/sdr/REXA2019082601294.md): Seat Track · corroded · Aug 26, 2019 · N907XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > AWR IN REF NRC S/N 00009 DURING PASSENGER SEAT REMOVAL, CORROSION WAS FOUND ON FLOOR RAIL 9 (LBL/RBL) FROM FS 830+40 -935. FLOOR RAIL 9(LBL/RBL) FROM FS 830+40 -935 WERE REPLACED PER AMM 53-00-49-400-801 (CONFIG A07). (LEVEL CORROSION 2)
- [SDR REXA2019082601293](https://openairdocs.org/sdr/REXA2019082601293.md): Seat Track · corroded · Aug 26, 2019 · N907XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > AWR IN REF NRC S/N 00009 DURING PASSENGER SEAT REMOVAL, CORROSION WAS FOUND ON SIDE RAIL STR 15 (L/R) FROM FS 830+40 -935. SIDE SEAT RAIL STR 15 (L/R) FROM FS 830+40 -935 WERE REPLACED PER AMM 53-00-49-400-801 CONFIG A07). (LEVEL CORROSION 2)
- [SDR REXA2019082601289](https://openairdocs.org/sdr/REXA2019082601289.md): Intercostal · corroded · Aug 26, 2019 · N907XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > AWR CORROSION ON INTERCOSTALS, FS 349, 364 BTW 26L-26R. (TCI 100-09). SUMMARY OF NRC S/N 00211: INTERCOSTALS (4EAS) FS 349, 364 BTW 26L-26R WERE REPLACED FOR A NEW ONE PER SRM 51-42-21-001-001-A01 AND SRM 51-42-06-001-001-A01 (LEVEL CORROSION 2)
- [SDR REXA2019082501290](https://openairdocs.org/sdr/REXA2019082501290.md): Stringer · corroded · Aug 25, 2019 · N907XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > AWR. CORROSION ON STRINGERS 26(L/R), FS 337-364. (TCI 100-09). STRINGER 26R/26L BTW FS337/364 WERE REPLACED FOR A NEW ONE PER SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01 (LEVEL CORROSION 2).
- [SDR REXA2019082401313](https://openairdocs.org/sdr/REXA2019082401313.md): Striker · corroded · Aug 24, 2019 · N907XJ · Cndair CL6002D24 · Service Doors
  > INITIAL INSPECTION: CORROSION ON LOWER SEAL STRICKER OF GALLEY SERVICE DOOR EXTERNAL SURROUND STRUCTURE. (R1)(TCI:. 53-20-219). LOWER SEAL STRICKER OF GALLEY SERVICE DOOR EXTERNAL SURROUND STRUCTURE WAS REPLACED FOR NEW ONE (P/N: SH670-31412-7) PER SRM 51-42-
- [SDR REXA2019082401301](https://openairdocs.org/sdr/REXA2019082401301.md): Canister · cracked · Aug 24, 2019 · N907XJ · Cndair CL6002D24 · Leading Edge Devices
  > INITIAL INSPECTION. CRACK ON SLAT TRACK CANISTER 1-3 INSIDE LT WING MAIN FUEL TANK WS 148. (SM)(AD). SLAT TRACK CANISTER 1-3 INSIDE LT WING MAIN FUEL TANK WS148 WAS REPAIRED PER REO 670-57-42-577 REV.
- [SDR REXA2019082401300](https://openairdocs.org/sdr/REXA2019082401300.md): Canister · cracked · Aug 24, 2019 · N907XJ · Cndair CL6002D24 · Leading Edge Devices
  > INITIAL INSPECTION. CRACK ON SLAT TRACK CANISTER 1-3 INSIDE RH WING MAIN FUEL TANK WS 148. (SM)(AD). SLAT TRACK CANISTER 1-3 INSIDE RT WING MAIN FUEL TANK WS148 WAS REPAIRED PER REO 670-57-42-577 REV.
- [SDR REXA2019082201292](https://openairdocs.org/sdr/REXA2019082201292.md): Doubler · corroded · Aug 22, 2019 · N907XJ · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > AWR. CORROSION ON INTERNAL DOUBLER (ANTENNA CUTOUT) FS 297-307, STR 27. (TCI 100-09). INTERNAL DOUBLER (ANTENNA CUTOUT) FS 297-307, STR 27 WAS REPLACED FOR A NEW ONE PER SRM 51-42-06-001-001-A01. (LEVEL CORROSION 2)
- [SDR REXA2019081501312](https://openairdocs.org/sdr/REXA2019081501312.md): Skin · corroded · Aug 15, 2019 · N907XJ · Cndair CL6002D24 · Wing, Plate/Skin
  > INITIAL INSPECTION: CORROSION ON EXTERNAL UPPER SKIN AT LT WING BTW WS 398-370 NEAR TO TRAILING EDGE PANEL 561AT. (TCI 57-20-203). AREA WAS REPAIRED PER EA NO:CRJ957-09614 REV IR.
- [SDR REXA2019081501311](https://openairdocs.org/sdr/REXA2019081501311.md): Skin · corroded · Aug 15, 2019 · N907XJ · Cndair CL6002D24 · Wing, Plate/Skin
  > INITIAL INSPECTION: CORRSION ON SETTLEMENT AREA OF ACCESS PANEL [561AT] AT LT WING REAR SPAR BTWN WS398.93 AND WS353.00.(SM)(AI). (TCI: 57-20-203). AREA WAS REPAIRED PER EA CRJ957-09577 REV IR LEVEL CORROSION #1.
- [SDR REXA2019081501310](https://openairdocs.org/sdr/REXA2019081501310.md): Fitting · cracked · Aug 15, 2019 · N907XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > INITIAL INSPECTION: CRACK ON LINTEL NR 3L AT CIRCUMFERENTIAL JOINT FS=280. (FUS) LINTEL NR 3L AT CIRCUMFERENTIAL JOINT FS:280 WAS REPAIRED PER ENGINEERING ORDER R53568 REVISION: FOUR, TASK CARD NUMBER: ADD-27:R53568.
- [SDR REXA2019081301317](https://openairdocs.org/sdr/REXA2019081301317.md): Intercostal · corroded · Aug 13, 2019 · N907XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > AWR CORROSION ON INTERCOSTAL DD6 AT PASSENGER DOOR. (L1). INTERCOSTAL DD6 (P/N 601R318057-1) AT PASSENGER DOOR WAS REPLACED PER SRM 51-42-06-001-001-A01 PAR 6 AND SRM 51-42-21-001-001-A01. PAR 6C (CORROSION LEVEL 2)
- [SDR REXA2019081301291](https://openairdocs.org/sdr/REXA2019081301291.md): Stringer Splice · corroded · Aug 13, 2019 · N907XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > AWR. CORROSION ON STRINGER SPLICES 25(L/R) 26(L/R), FS 329-337. (TCI 100-09). SUMMARY OF NRC S/N 00208: STRINGER SPLICES 25(L/R) 26(L/R), FS 329-337 WERE REPLACED FOR A NEW ONE PER SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01 (LEVEL CORROSION 2)
- [SDR REXA2019080401319](https://openairdocs.org/sdr/REXA2019080401319.md): Strap · corroded · Aug 4, 2019 · N907XJ · Cndair CL6002D24 · Aerodynamic Fairings
  > PART RACKS: CORROSION ON FAIRING 193AB. (FUS) STRAP (P/N:CC670-39052-3) WAS FOUND OUT OF LIMITS PER SRM 53-00-06-201-005-A01 PAR 6 (A). THEREFORE STRAP (P/N:CC670-39052-3) WAS REPLACED PER SRM 51-42-13-001-001-A01 PAR 6C. STRAP (P/N: CC670-39052-4) WAS REPLACE
- [SDR REXA2018041500298](https://openairdocs.org/sdr/REXA2018041500298.md): Brake · overheated · Apr 15, 2018 · N907XJ · Cndair CL6002D24 · Landing Gear Brake System
  > WHILE FLYING AT APROX 17000 FT, A BRAKE OVHT WARNING ILLUMINATED. EXTENDED THE GEAR IAW QRH, MESSAGE WENT AWAY, THEN WE RETRACTED GEAR WARNING MESSAGE CAME BACK. REMOVED AND REPLACED THE RT OTBD BRAKE THERMOCOUPLE SENSOR IAW AMM 32-46-01, OPS CHECKED NORMAL.
- [SDR REXA2017081000870](https://openairdocs.org/sdr/REXA2017081000870.md): Smoke Detector · inoperative · Aug 10, 2017 · N907XJ · Cndair CL6002D24 · Smoke Detection
  > GREEN LIGHT ON AFT LAV SMOKE DETECTOR IS INOPERATIVE. REMOVED AND REPLACED AFT LAV SMOKE DETECTOR IAW AMM 26-16-01. OPS CHECKED GOOD.
- [SDR REXA2017072600810](https://openairdocs.org/sdr/REXA2017072600810.md): Fire Bottle · discharged · Jul 26, 2017 · N907XJ · Cndair CL6002D24 · Fire Bottle, Portable
  > FOUND FLT DECK PORTABLE FIRE BOTTLE SAFETY PIN MISSING AND DISCHARGED. REMOVED AND REPLACED FLT DECK PORTABLE FIRE EXTINGUISHER IAW AMM 26-23-01
- [SDR REXA2017062000720](https://openairdocs.org/sdr/REXA2017062000720.md): Line · leaking · Jun 20, 2017 · N907XJ · Cndair CL6002D24 · Crew Oxygen System
  > DURING PREFLIGHT, OXYGEN PRESSURE WAS NOTED TO BE APROXIMATELY 1420 PSI. OXYGEN LOW PRESSURE CAUTION MESSAGE POSTED AND NOTED THE OXYGEN TO BE 1390 PSI WITHIN A HALF HOUR OXYGEN WAS NOTED TO BE 1240LBS. DEPRESSURIZED CREW OXYGEN IAW AMM 35-10-00-862-801-A01
- [SDR REXA2017032300397](https://openairdocs.org/sdr/REXA2017032300397.md): Engine · damaged · Mar 23, 2017 · N907XJ · Cndair CL6002D24 · Engine (Turbine/Turboprop)
  > DURING TAKEOFF ROLL, AIRCRAFT PULLED TO THE RIGHT TWICE PRIOR TO ROTATION, NR 2 ENGINE WENT OUT OF FLEX THRUST, ACCOMPLANIED BY NOISE, AND VIBRATION. REMOVED AND REPLACED THE RT ENGINE. OPS CHECKED GOOD.
- [SDR REXA2017021100192](https://openairdocs.org/sdr/REXA2017021100192.md): Oxygen Mask · unserviceable · Feb 11, 2017 · N907XJ · Cndair CL6002D24 · Passenger Oxygen System
  > FOUND O2 MASK A 5DC UNSERVICEABLE. R&R O2 MASK A 5DC IAW AMM 35-21-09. P/N OFF/ON 289-601-066-1.

Next page: https://openairdocs.org/aircraft/N907XJ/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 = 'N907XJ' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N907XJ/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.