# Service difficulty reports: N905XJ

A list on [N905XJ](https://openairdocs.org/aircraft/N905XJ.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 · 235 reports

- [SDR REXA2026060800899](https://openairdocs.org/sdr/REXA2026060800899.md): Bulb · burned out · Jun 2, 2026 · N905XJ · Cndair CL6002D24 · Emergency Lighting
  > DURING WAKE UP EXTERIOR VISUAL INSPECTION FOUND LH FWD EMERGENCY LIGHT OUT. R & R EMERGENCY LIGHT BULB IAW AMM 33-51-15. OPS CHECK GOOD. NO MORE DEFECTS FOUND AT THIS TIME. ACFT OK FOR SERVICE.
- [SDR REXA2025082200828](https://openairdocs.org/sdr/REXA2025082200828.md): Door · inoperative · Aug 12, 2025 · N905XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > PASSENGER DOOR WILL NOT OPEN AFTER HANDLE LIFTED PLACING PAX DOOR ON MEL #52-21-1 CAT A, INSTALLED BALLAST IAW AMM 52-00-00867-801. PERFORMED FUNCTIONAL TEST OF PAX DOOR IAW AMM 52-11-00-720-802. ADJUSTED UPPER FWD PAX DOOR LATCH PIN IAW AMM 52-11-02. LOCKIN
- [SDR REXA2025080600795](https://openairdocs.org/sdr/REXA2025080600795.md): Housing · cracked · Jul 29, 2025 · N905XJ · Cndair CL6002D24 · Fuselage Main, Structure
  > CRACK ON AFT LATCH HOUSING CUTOUT FS188.00 OF ACCESS DOOR 212AR AFT LATCH HOUSING CUTOUT FS188.00 OF ACCESS DOOR 212AR WAS FABRICATED PER EA CRJ953-19660 REV. IR AND WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 AND CRJ900 SRM 51-42-10-001-001-A01
- [SDR REXA2026072901289](https://openairdocs.org/sdr/REXA2026072901289.md): Membrane · cracked · Jul 23, 2025 · N905XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK ON FWD MEMBRANE OF INBD DOOR AT LH MLG FWD MEMBRANE OF INBD DOOR AT LH MLG WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01
- [SDR REXA2025080600794](https://openairdocs.org/sdr/REXA2025080600794.md): Skin · damaged · Jul 23, 2025 · N905XJ · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > PERFORM PERMANENT REPAIR OF LIGHTNING DMG AT FS 720 ST5L-6L LIGHTNING DMG AT FS 720 ST5L-6L WAS REPAIRED PER EA CRJ953-19773 REV. IR
- [SDR REXA2025080600793](https://openairdocs.org/sdr/REXA2025080600793.md): Access Panel · corroded · Jul 23, 2025 · N905XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > ITIAL INSPECTION: CORROSION ON SETTLEMENT AREA OF ACCESS PANEL 195AB CORROSION ON SETTLEMENT AREA OF ACCESS PANEL 195AB (DOOR LANDING) WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-00-00-101-001-A01 AND WAS REPLACED PER CRJ900 SRM 51-42-10-001-001-A01 AND CRJ9
- [SDR REXA2025080600792](https://openairdocs.org/sdr/REXA2025080600792.md): Bracket · corroded · Jul 23, 2025 · N905XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON HYDRAULIC LINES SUPPORT PLATES (IN BK, LG EXT, LG RET) RBL 45 AND LBL45 AT RH/LH MLG WHEEL WELL. CORROSION ON HYDRAULIC LINES SUPPORT PLATES (IN BK, LG EXT, LG RET) RBL 45 AND LBL45 AT RH/LH MLG WHEEL WELL WAS REMOVED PER CRJ900 SRM 51-21-06-001-0
- [SDR REXA2025080600791](https://openairdocs.org/sdr/REXA2025080600791.md): Hinge · corroded · Jul 23, 2025 · N905XJ · Cndair CL6002D24 · Fuselage, Door Hinge
  > OUT OF SCOPE: CORROSION ON AFT HINGE OF AFT CARGO STEP PLATE AFT HINGE OF AFT CARGO STEP PLATE WAS EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-00-00-101-001-A01, WAS FABRICATED PER EA CRJ953-19720 REV. IR AND WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01
- [SDR REXA2025080600790](https://openairdocs.org/sdr/REXA2025080600790.md): Hinge · cracked · Jul 23, 2025 · N905XJ · Cndair CL6002D24 · Fuselage, Door Hinge
  > OUT OF SCOPE: CRACK ON FWD HINGE OF AFT CARGO STEP PLATE FWD HINGE OF AFT CARGO STEP PLATE WAS EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-00-00-101-001-A01, WAS FABRICATED PER EA CRJ953-19672 REV. IR AND WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01
- [SDR REXA2025080600789](https://openairdocs.org/sdr/REXA2025080600789.md): Skin · cracked · Jul 22, 2025 · N905XJ · Cndair CL6002D24 · Trailing Edge Flaps
  > "SECONDARY NRC IN REF. TO NRC 00013: AFTER PAINT STRIPPING ON LOWER SKIN AT LH INBOARD FLAP, CRACK WAS FOUND ON LOWER SKIN BTW FS30.00 / FS36.00 FROM 0.750Ï¿½ TO TRAILING EDGE. LOWER SKIN AT LH INBOARD FLAP BTW FLS 30.00 / FLS 36.00 0.750"" ABOVE OF TRAILING
- [SDR REXA2025080600788](https://openairdocs.org/sdr/REXA2025080600788.md): Access Panel · corroded · Jul 21, 2025 · N905XJ · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > INITIAL INSPECTION: CORROSION ON SETTLEMENT AREA OF ACCESS PANELS 196DR CORROSION ON SETTLEMENT AREA OF ACCESS PANELS 196DR WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01, FS927 TO FS942 BTW STGR 21R TO STGR 23R WAS EVALUATED WITHIN LIMITS PER CRJ900 SRM 53-5
- [SDR REXA2025080600787](https://openairdocs.org/sdr/REXA2025080600787.md): Channel · corroded · Jul 21, 2025 · N905XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > SECUNDARY NRC IN REFERENCE WITH NRC 00160: AFTER SUPPORT DIAPHRAGM REMOVAL, CORROSION AND ELONGATED HOLES WAS FOUND ON ATTACHMENT AREA. SUPPORT OF DIAPHRAGM WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-00-00-101-001-A01 AND WAS REPLACED PER CRJ900 SRM 51-42-2
- [SDR REXA2025080600786](https://openairdocs.org/sdr/REXA2025080600786.md): Floorbeam · corroded · Jul 21, 2025 · N905XJ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > INITIAL INSPECTION: CORROSION ON CROSSBEAM FS280.00 BTW LBL 9 TO RBL 9 AT CPAX. CORROSION ON CROSSBEAM (STRIP, UPPER SPLICE) FS280.00 BTW LBL 9 TO RBL 9 AT CPAX WAS EVALUATED OUT OF LIMITS AND WAS REPLACED PER CRJ900 SRM 53-00-00-101-001-A01 AND PER CRJ900 SRM
- [SDR REXA2025080600785](https://openairdocs.org/sdr/REXA2025080600785.md): Skin · damaged · Jul 18, 2025 · N905XJ · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > IN REFERENCE TO CARD 900-53-900-105': PREVIOUS BLEND OUT FOUND AT REPAIR DOUBLER LOCATED AT FUSELAGE SKIN AT FS 581 BTW STGR 16 LH AND 17 LH. PREVIOUS REPAIR DOUBLER LOCATED AT FUSELAGE SKIN AT FS 581 BTW STGR 16 LH AND 17 LH WAS REPLACED PER CRJ-900 SRM 51-42
- [SDR REXA2024102500972](https://openairdocs.org/sdr/REXA2024102500972.md): Door · cracked · Mar 2, 2024 · N905XJ · Cndair CL6002D24 · Emergency Exits
  > LH AFT OVERWING EMERGENCY EXIT DOOR (835) HAS A CRACK AT THE BASE OF THE TOP AFT LUG REPAIRED IAW MHIRJ REO 690-52-21-157 REV-- DATED 2024-02-29.
- [SDR REXA2024102500971](https://openairdocs.org/sdr/REXA2024102500971.md): Door · cracked · Mar 2, 2024 · N905XJ · Cndair CL6002D24 · Emergency Exits
  > RH AFT OVERWING EMERGENCY EXIT DOOR (845) HAS A CRACK AT THE BASE OF THE TOP AFT LUG REPAIRED IAW MHIRJ REO# 690-52-21-158 REV -- DATED 2024-02-25.
- [SDR REXA2024102500970](https://openairdocs.org/sdr/REXA2024102500970.md): Door · cracked · Mar 2, 2024 · N905XJ · Cndair CL6002D24 · Emergency Exits
  > RH FWD OVERWING EMERGENCY EXIT (843) HAS A CRACK AT THE BASE OF THE TOP AFT LUG REPAIRED IAW MHIRJ REO 690-52-21-157 REV-- DATED 2024-02-29
- [SDR REXA2024062400480](https://openairdocs.org/sdr/REXA2024062400480.md): Seat Track · corroded · Feb 21, 2024 · N905XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > FLOOR SEAT TRACK LOCATED AT RBL9 BETWEEN FS693 AND FS847 IS CORRODED. REMOVED AND REPLACED IAW MHIRJ REO 670-53-00-589 REV -C DATED 2023-02-08.
- [SDR REXA2024062400479](https://openairdocs.org/sdr/REXA2024062400479.md): Seat Track · corroded · Feb 21, 2024 · N905XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > FLOOR SEAT TRACK LOCATED AT LBL9 BETWEEN FS693 AND FS847 IS CORRODED. REMOVED AND REPLACED IAW MHIRJ REO 670-53-00-589 REV -C DATED 2023-02-08.
- [SDR REXA2022041200283](https://openairdocs.org/sdr/REXA2022041200283.md): Lamp · inoperative · Apr 10, 2023 · N905XJ · Cndair CL6002D24 · Emergency Lighting
  > DURING LINE CHECK FOUND FLOOR LEVEL EMERGENCY FLOOD LIGHT OUT REMOVED AND REPLACED FLOOR LEVEL EMERGENCY LIGHT IAW 33-51-11. OPS CHECK GOOD P/N ON/OFF- OL371 NSN
- [SDR REXA2022021000204](https://openairdocs.org/sdr/REXA2022021000204.md): Bracket · corroded · Jan 28, 2022 · N905XJ · Cndair CL6002D24 · Wing Main, Frame Structure
  > "RH SIDE BELOW OUT PNL ATTACH BRACKET ATTACHED TO WING TRAILING EDGE IS CORRODED " "REMOVED, LOCATED, DRILLED & INSTALLED NEW ANGLE BRACKET IAW CRJ900 SRM 51-40-11-001-001-A01, 51-42-21-001-001-A01, 51-23-00-0
- [SDR REXA2022021000192](https://openairdocs.org/sdr/REXA2022021000192.md): Angle · corroded · Jan 28, 2022 · N905XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > PAX DOOR SILL MID CAP ANGLE IS CORRODED. H-CHECK TCI: 53-20-319 "LOCATED & DRILLED NEW SERVICEABLE CAP ANGLE IAW CRJ-900 SRM 51-40-11- 001-001-A01. REMOVED & REPLACED CAP ANGLE WITH NEW SERVICABLE PART IAW CRJ-900 SRM 51-41-02-001-001-A01 & APPLIED CIC IAW
- [SDR REXA2022020900188](https://openairdocs.org/sdr/REXA2022020900188.md): Floorbeam · corroded · Jan 28, 2022 · N905XJ · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > "FLOORBEAM AT RBL 27 HAS MULTIPLE SPOTS OF CORROSION FROM FS 1000 TO FS 1098. " "REPAIRED FLOORBEAM AT RBL27 F.S. 1000-1088 IAW ENDEAVOR EA#CRJ 953- 12538 REV A DATED 12/22/2021 AND MHIRJ REO 690-
- [SDR REXA2022021000208](https://openairdocs.org/sdr/REXA2022021000208.md): Retainer · corroded · Jan 27, 2022 · N905XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > AVI DOOR FWD L/H & R/H SEAL RETAINER IS CORRODED "REMOVED AND INSTALLED AVI DOOR IAW CRJ 900 AMM 52-42-00-000/400-801- A01, INSULATION IAW AMM 25-84-00-000/400-802-A01 REMOVED AND INSTALLED BOTH FWD AND AFT (LH & RH) SEAL RETAINERS IAW CRJ 900 SRM
- [SDR REXA2022021000207](https://openairdocs.org/sdr/REXA2022021000207.md): Retainer · corroded · Jan 27, 2022 · N905XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > AVI DOOR FWD L/H & R/H SEAL RETAINER IS CORRODED "REMOVED AND INSTALLED AVI DOOR IAW CRJ 900 AMM 52-42-00-000/400-801- A01, INSULATION IAW AMM 25-84-00-000/400-802-A01 REMOVED AND INSTALLED BOTH FWD AND AFT (LH & RH) SEAL RETAINERS IAW CRJ 900 SRM
- [SDR REXA2022021000206](https://openairdocs.org/sdr/REXA2022021000206.md): Retainer · corroded · Jan 27, 2022 · N905XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > AVI DOOR FWD L/H & R/H SEAL RETAINER IS CORRODED "REMOVED AND INSTALLED AVI DOOR IAW CRJ 900 AMM 52-42-00-000/400-801- A01, INSULATION IAW AMM 25-84-00-000/400-802-A01 REMOVED AND INSTALLED BOTH FWD AND AFT (LH & RH) SEAL RETAINERS IAW CRJ 900 SRM
- [SDR REXA2022021000205](https://openairdocs.org/sdr/REXA2022021000205.md): Retainer · corroded · Jan 27, 2022 · N905XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > AVI DOOR FWD L/H & R/H SEAL RETAINER IS CORRODED "REMOVED AND INSTALLED AVI DOOR IAW CRJ 900 AMM 52-42-00-000/400-801- A01, INSULATION IAW AMM 25-84-00-000/400-802-A01 REMOVED AND INSTALLED BOTH FWD AND AFT (LH & RH) SEAL RETAINERS IAW CRJ 900 SRM
- [SDR REXA2022021000237](https://openairdocs.org/sdr/REXA2022021000237.md): Frame · gouged · Jan 24, 2022 · N905XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "WHILE REPLACING FS 942 LOWER FRAME SEGMENT P/N SH690-37095-3S, FREE FLANGE WAS GOUGED AND BENT BETWEEN STR 26L & STR 27 DURING TEMP. INSTALLATION OF NEW FRAME SEGMENT. " "REPAIRED DAMAGE IAW ENDEAVOR EA #CRJ953-12637 REV
- [SDR REXA2022020900187](https://openairdocs.org/sdr/REXA2022020900187.md): Angle · cracked · Jan 22, 2022 · N905XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > LH AFT DRAG ANGLE IS CRACKED. REMOVED CRACKED L/H AFT DRAG ANGLE AND INSTALLED NEW SERVICABLE DRAG ANGLE IAW CRJ 900 SRM 51-42-13-001-001-A01 AND 51-42-21-001-001-A01.
- [SDR REXA2022020900191](https://openairdocs.org/sdr/REXA2022020900191.md): Stringer · corroded · Jan 21, 2022 · N905XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > STRINGER 25R IS CORRODED FROM FS 280 TO FS 333. "REPAIRED STRINGER 25R FROM FS 280 TO FS 333 IAW ENDEAVOR EA CRJ 953-12643, REV IR DATED 1/5/22. REMOVED AND REINSTALLED INSULATION IAW CRJ900 AMM'S 25-84-00-000/400-801-A05 FROM FS 280 TO FS 333 FR
- [SDR REXA2022020900190](https://openairdocs.org/sdr/REXA2022020900190.md): Floorbeam · corroded · Jan 21, 2022 · N905XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "FLOORBEAM AT LBL 27 HAS MULTIPLE SPOTS OF CORROSION FROM FS 969 TO FS 1098. " "PERFORMED SPLICE REPAIR IAW CRJ900 SRM 53-00-41-201-001-A03 REPAIR FIG 53-00-41-995-829 ON LBL 27 FROM FS 969 - FS 1098.
- [SDR REXA2022020900182](https://openairdocs.org/sdr/REXA2022020900182.md): Stringer · corroded · Jan 21, 2022 · N905XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > STRINGER 25R IS CORRODED FROM FS 280 TO FS 333. "REPAIRED STRINGER 25R FROM FS 280 TO FS 333 IAW ENDEAVOR EA CRJ 953-12643, REV IR DATED 1/5/22. REMOVED AND REINSTALLED INSULATION IAW CRJ900 AMM'S 25-84-00-000/400-801-A05 FROM FS 280 TO FS 333 FR
- [SDR REXA2022021000238](https://openairdocs.org/sdr/REXA2022021000238.md): Fitting · chafed · Jan 20, 2022 · N905XJ · Cndair CL6002D24 · Horizontal Stabilizer Structure
  > LEFT & RIGHT H-STAB ANTI-ROTATION FITTINGS HAVE CHAFING & SCRATCHES "REPAIRED THE LEFT AND RIGHT H-STAB ANTI-ROTATION FITTINGS IAW MHIRJ REO 690-55-11-148, NO DEFECTS NOTED.
- [SDR REXA2022020900189](https://openairdocs.org/sdr/REXA2022020900189.md): Floorbeam · corroded · Jan 19, 2022 · N905XJ · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > "FLOORBEAM AT LBL 9 HAS MULTIPLE SPOTS OF CORROSION FROM FS 1000 TO FS 1098 TCI-53-30-306 " "LOCATED AND DRILLED NEW FLOORBEAM P/N S6283 NAD INSTALLED @ F.S. 1000 TO F.S. 1088 LBL 9 IAW CRJ-900 SRM 53-00-41-201-0
- [SDR REXA2022021000233](https://openairdocs.org/sdr/REXA2022021000233.md): Seat Track · corroded · Jan 10, 2022 · N905XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > SEAT TRACK AT 15R BETWEEN FS 581.00 TO FS 661.00+16 IS CORRODED. "REMOVED, FABRICATED AND INSTALLED SEAT TRACK IAW CRJ 900 AMM 53-00-49- 000/400-801-A19 AND SRM 53-00-49-200-002-A01.
- [SDR REXA2022021000236](https://openairdocs.org/sdr/REXA2022021000236.md): Frame · corroded · Jan 9, 2022 · N905XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FRAME AT FS 942 CORRODED BETWEEN STR 25L AND 23R. "REMOVED/LOCATED/DRILLED/DEBURRED/ INSTALLED LOWER SECTION FRAME AT FS 942, 14EA CLEATS,POST SUPPORT,CLAMPS, 2EA DOME NUTPLATES, 2 HYDRO CLAMPS IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-42-21-00
- [SDR REXA2022021000232](https://openairdocs.org/sdr/REXA2022021000232.md): Frame · cracked · Jan 9, 2022 · N905XJ · Cndair CL6002D24 · Fuselage Main, Structure
  > LH FRAME AT FS 235 CRACKED BETWEEN STGR 11L AND STGR 13L. "REPAIRED LH F.S. 235 FRAME IAW MHIRJ REO 690-53-11-1391 REV+- DATED 2022-01-05.
- [SDR REXA2022021000193](https://openairdocs.org/sdr/REXA2022021000193.md): Retainer · corroded · Jan 9, 2022 · N905XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "RH SIDEWALL SEAT TRACK RETAINER HAS MULTIPLE SPOTS OF CORROSION FROM FS 785 - FS 847+16 " "REMOVED & REPLACED RH SIDEWALL SEAT TRACK RETAINER AT F.S. 785-847 +16 IAW CRJ-AMM 53-00-49-000/400-801-A19. WAS OUT OF LIMITS
- [SDR REXA2022020900183](https://openairdocs.org/sdr/REXA2022020900183.md): Plate · corroded · Jan 8, 2022 · N905XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > PAX DOOR LWR KICKPLATE ANGLE IS CORRODED "REMOVED PAX DOOR LWR KICKPLATE LOCATED DRILLED AND INSTALLED NEW SERVICABLE KICKPLATE P/M SH670-31895 IAW CRJ900 SRM 51-42-06-001- 001-A01 51-40-11-001-001-A01 WVAC EMP STAMP
- [SDR REXA2022021000223](https://openairdocs.org/sdr/REXA2022021000223.md): Fitting · elongated · Jan 7, 2022 · N905XJ · Cndair CL6002D24 · Wing Structure
  > L AILERON LUG "E" OVERSIZED TO BETWEEN 0.9755" AND 0.9765". "REPAIRED L/H AILERON LUG ""E"" IAW MHIRJ REO 690-57-61-242 REV-- DATED 2021-12-16.
- [SDR REXA2022021000197](https://openairdocs.org/sdr/REXA2022021000197.md): Rail · corroded · Jan 7, 2022 · N905XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "RH SIDEWALL SEAT TRACK HAS MULTIPLE SPOTS OF CORROSION FROM FS 847+16 - FS 865. " "REPLACED R/H SIDEWALL SEAT RAIL @ FS 847+16-FS 865 IAW CRJ 900 AMM 53- 00-49-400-801-A19 53-00-49-000-801(A19) WVAC EMP # "
- [SDR REXA2022021000196](https://openairdocs.org/sdr/REXA2022021000196.md): Seat Track · corroded · Jan 6, 2022 · N905XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > RH SIDEWALL SEAT TRACK HAS MULTIPLE SPOTS OF CORROSION FROM FS 865 -FS 969. REMOVED, FABRICATED AND INSTALLED NEW RH SEAT TRACK SIDEWALL FOR FS 865-FS 969 REMOVED EXCESS SEALANT & REPLACED STRIPPED SCREW IAW CRJ 900 SRM /AMM 53-00-49-000-801-A19, 53-00-49-20
- [SDR REXA2022021000216](https://openairdocs.org/sdr/REXA2022021000216.md): Rail · corroded · Jan 5, 2022 · N905XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "SIDE SEAT TRACK AT STGR 15L BETWEEN FS 485.00 AND FS 565.00 IS CORRODED " "INSTALLED NEW SEAT RAIL SIDETRACK PN#SH690-36281-1 AT STGR 15L BTW FS 485.00 & FS 565.00 IAW CRJ 900 AMM 53-00-49-400-801-A19 IA
- [SDR REXA2022021000199](https://openairdocs.org/sdr/REXA2022021000199.md): Rail · corroded · Jan 5, 2022 · N905XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "RH SIDEWALL SEAT TRACK HAS MULTIPLE SPOTS OF CORROSION FROM FS 677 - FS 720. " "REMOVED FABRICATED AND INSTALLED RH SIDEWALL SEAT TRACK AT FS 677 TO FS 720 IAW CRJ900 SRM 53-00-49-201-002-A01 CRJ9
- [SDR REXA2022021000194](https://openairdocs.org/sdr/REXA2022021000194.md): Retainer · corroded · Jan 5, 2022 · N905XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "RH SIDEWALL SEAT TRACK RETAINER HAS MULTIPLE SPOTS OF CORROSION FROM FS 677 - FS 720. " "REMOVED DAMAGE RH SIDEWALL SEAT TRACK RETAINER INSTALLED NEW SERVICEABLE RH SEAT TRACK RETAINER AT FS 677 TO FS 720
- [SDR REXA2022021000221](https://openairdocs.org/sdr/REXA2022021000221.md): Panel · chafed · Jan 4, 2022 · N905XJ · Cndair CL6002D24 · Wing, Control Surfaces
  > PANEL 684ET IS CHAFED "BLENDING REMOVED AREA FOUND OT BE OUT OF LIMITS REMOVE AND REPLACED PRE PAD FASTENER HOLES AND INSTALLED 4EA FASTENERS AND PAINTED PANEL 684ET IAW CRJ 900 SRM 57-52-01-001-001-A01, 51-77-00-001-001-A01, 51-40-11-001-001-A01, 51-4
- [SDR REXA2022021000211](https://openairdocs.org/sdr/REXA2022021000211.md): Seat Track · corroded · Jan 4, 2022 · N905XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "FLOOR SEAT TRACK AT LBL 9 BETWEEN FS 581.00 AND FS 661.00+32 IS CORRODED. " "REMOVED & REPLACED SEAT RAIL LBL9 FS 581-661+32 IAW CRJ 900 AMM 53-00-49-000/400-801(A10) & SRM'S 53-00-09-201-002-A01
- [SDR REXA2022021000202](https://openairdocs.org/sdr/REXA2022021000202.md): Rail · corroded · Jan 4, 2022 · N905XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "LH SIDEWALL SEAT TRACK MULTIPLE SPOTS OF CORROSION FROM FS 744 - FS 752. " "INSTALLED NEW SEAT RAIL P/N SH690-36285-1 IAW CRJ 900 AMM 53-00-49- 400-801-A19 DUE TO OLD SEAT RAIL CORRODED OUT OF
- [SDR REXA2022021000220](https://openairdocs.org/sdr/REXA2022021000220.md): Floorboard · cracked · Jan 2, 2022 · N905XJ · Cndair CL6002D24 · Fuselage Main, Structure
  > FWD EQUIPMENT COMPARTMENT LH SIDE AT FS 193 THE FLOOR IS CRACKED. " REPAIRED FWD EQUIPMENT LH SIDE FS 193 FLOOR CRACK IAW CRJ 900 SRM 53-11-43-201-001-A01. REMOVED AND REINSTALLED BRAKE ACCUMULATOR LINES AND GAUGE BRKT AND PERFORMED OPS/LEAKS/BLEED
- [SDR REXA2022021000203](https://openairdocs.org/sdr/REXA2022021000203.md): Seat Track · corroded · Jan 2, 2022 · N905XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "LH SIDEWALL SEAT TRACK MULTIPLE SPOTS OF CORROSION FROM FS 693 - FS 720. " "INSTALLED NEW SEAT RAIL SH690-36284-1 FROM L/H SIDE WALL FS 693- FS 720 IAW CRJ 900 AMM 53-00-49-400-801-A19 WVAC EMP STAM

Next page: https://openairdocs.org/aircraft/N905XJ/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 = 'N905XJ' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N905XJ/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.