# Service difficulty reports: N904XJ

A list on [N904XJ](https://openairdocs.org/aircraft/N904XJ.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 · 192 reports

- [SDR REXA2025032400358](https://openairdocs.org/sdr/REXA2025032400358.md): Bearing · not reported · Mar 20, 2025 · N904XJ · Cndair CL6002D24 · Ailerons
  > RH AILERON O/B HINGE REQUIRES ENGINEERING TO OVERSIZE TO ACCOMMODATE OVERSIZED BEARINGS. REPAIRED IAW REO 690-57-61-373 REV -- DATED 2025-03-18.
- [SDR REXA2025032100343](https://openairdocs.org/sdr/REXA2025032100343.md): Angle · corroded · Mar 20, 2025 · N904XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > GALLEY SERVICE DOOR LOWER SILL ANGLE IS CORRODED. INSTALLED NEW SERVICEABLE SERVICE DOOR LOWER SILL ANGLE PN SH670-31996-3S IAW CRJ-900 SRM 51-42-06-001-001-A01
- [SDR REXA2025032100342](https://openairdocs.org/sdr/REXA2025032100342.md): Drag Angle · cracked · Mar 20, 2025 · N904XJ · Cndair CL6002D24 · Rudder, Plate/Skin
  > "VERTICAL STAB LH FWD DRAG-ANGLE IS CRACKED. FABRICATED, LOCATED AND DRILLED REPAIR PARTS ITEM 1 FWD ANGLE DOUBLER FROM 2024T3 0.090"" P.O.# W72936, ITEM 2 FWD ANGLE FILLER FROM 2024T3 0.090"" P.O# W72936 IAW CRJ900 SRM 55-31-00-201-001-A01 STEP 5.B. (4) THRU
- [SDR REXA2025033100373](https://openairdocs.org/sdr/REXA2025033100373.md): Fitting · damaged · Mar 19, 2025 · N904XJ · Cndair CL6002D24 · Ailerons
  > "R/H WING SIDE AILERON CENTER HINGE LUGS LABELED ""C"", ""D"", ""E"", & ""F"" ARE PREVIOUSLY OVERSIZED & REQUIRE ENGINEERING. FABRICATION OF O/S AILERON BUSHINGS IS REQUIRED. REPAIRED IAW REO 690-57-51-413 REV -- DATED 2025-03-24."
- [SDR REXA2025033100371](https://openairdocs.org/sdr/REXA2025033100371.md): Fitting · damaged · Mar 19, 2025 · N904XJ · Cndair CL6002D24 · Ailerons
  > "L/H WING SIDE AILERON I/B CENTER HINGE LUGS LABELED ""C"" & ""D"" ARE PREVIOUSLY OVERSIZED & REQUIRE ENGINEERING. FABRICATION OF O/S AILERON BUSHINGS IS REQUIRED. REPAIRED IAW REO 670-57-51-412 REV -- DATED 2025-03-24."
- [SDR REXA2025033100370](https://openairdocs.org/sdr/REXA2025033100370.md): Lug · damaged · Mar 18, 2025 · N904XJ · Cndair CL6002D24 · Ailerons
  > RH AILERON BUSHING LUGS MARKED C,F AND G FOUND AT 1ST OVERSIZE WHEN BUSHINGS WERE REMOVED. REPAIRED IAW REO 670-57-61-273 REV -- DATED 2017-07-25.
- [SDR REXA2025033100368](https://openairdocs.org/sdr/REXA2025033100368.md): Bushing · damaged · Mar 18, 2025 · N904XJ · Cndair CL6002D24 · Ailerons
  > LH AILERON BUSHING LUG MARKED F FOUND AT 1ST OVERSIZE WHEN BUSHING WAS REMOVED. NEW BUSHING REQUIRES FAB AND INSTALL. REPAIRED IAW REO 690-57-61-273 REV -- DATED 2025-07-25.
- [SDR REXA2025032400357](https://openairdocs.org/sdr/REXA2025032400357.md): Hinge · not reported · Mar 18, 2025 · N904XJ · Cndair CL6002D24 · Ailerons
  > LH AILERON O/B HINGE REQUIRES ENGINEERING TO OVERSIZE TO ACCOMMODATE OVERSIZED BEARINGS. REPAIRED LH AILERON O/B HINGE IAW MHIRJ REO 690-57-61-372 REV -- DATED 2025-03-18
- [SDR REXA2025031700330](https://openairdocs.org/sdr/REXA2025031700330.md): Seat Track · corroded · Mar 15, 2025 · N904XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > LBL9 FLOOR SEAT TRACK IS CORRODED AT F.S. 379 INSTALLED NEW SERVICEABLE FLOOR SEAT TRACK (P/N SH670-32249-3) AT LBL9 FROM FS 379 TO FS 469 IAW CRJ-900 AMM 53-00-49-400-801-A19.
- [SDR REXA2025033100367](https://openairdocs.org/sdr/REXA2025033100367.md): Lug · cracked · Mar 10, 2025 · N904XJ · Cndair CL6002D24 · Emergency Exits
  > L/H FWD OVERWING EXIT DOOR P/N SH670-36600, S/N SB0565 UPPER AFT LUG IS CRACKED. REPAIRED IAW REO 670-52-21-103 REV -- DATED 2024-11-06.
- [SDR REXA2025032400356](https://openairdocs.org/sdr/REXA2025032400356.md): Frame · cracked · Mar 10, 2025 · N904XJ · Cndair CL6002D24 · Fuselage Main, Structure
  > R/H AFT OVERWING EXIT DOOR UPPER AFT LUG IS CRACKED. REPAIRED PER MHIRJ GREO 670-52-21-103.
- [SDR REXA2025032400355](https://openairdocs.org/sdr/REXA2025032400355.md): Door Frame · cracked · Mar 10, 2025 · N904XJ · Cndair CL6002D24 · Fuselage Main, Structure
  > LH AFT OVERWING EXIT DOOR UPPER AFT LUG IS CRACKED. REPAIRED PER MHIRJ GREO 670-52-21-103.
- [SDR REXA2025032400354](https://openairdocs.org/sdr/REXA2025032400354.md): Door Frame · cracked · Mar 10, 2025 · N904XJ · Cndair CL6002D24 · Fuselage Main, Structure
  > R/H FWD OVERWING EXIT DOOR P/N SH670-36600, S/N SB0566 UPPER AFT LUG IS CRACKED. REPAIRED PER MHIRJ GREO 670-52-21-103.
- [SDR REXA2024111101465](https://openairdocs.org/sdr/REXA2024111101465.md): Lamp · inoperative · Nov 2, 2024 · N904XJ · Cndair CL6002D24 · Emergency Lighting
  > EXTERIOR RIGHT HAND AFT EMERGENCY LIGHT INOP. R/R EMERGENCY LIGHT IAW AMM 31-51-15. OPS CHECK GOOD. NO DEFECTS NOTED. P/N ON/OFF: 8GH002473-08 S/N ON: NSN
- [SDR REXA2022041300289](https://openairdocs.org/sdr/REXA2022041300289.md): Lamp · inoperative · Apr 10, 2023 · N904XJ · Cndair CL6002D24 · Emergency Lighting
  > FOUND FWD RH SIDE EXTERIOR EMERGENCY EXIT LIGHT TO BE OUT INSTALLED SERVICEABLE LH FWD EMERGENCY LIGHT LAMP ASSY PN: 8GH- 409570-28 IAW CRJ 900 AMM 33-51-15-400-A08 OPS CHECK GOOD WVAC EMP # 53745
- [SDR REXA2022050200281](https://openairdocs.org/sdr/REXA2022050200281.md): Unknown · corroded · Apr 9, 2023 · N904XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > WHILE INCORPORATING SB 670BA-53-061/ ENDEAVOR EO R53595^ WE HAVE FOUND MULTIPLE FASTENERS WITH CORROSION AROUND COUNTERSINKS @ FS 792 AND FS 801 ON BOTH L/H SIDES. REPAIRED IAW MHIRJ REO 690-53-41-384 REV-- DATED 2023-04-07
- [SDR REXA2021110400936](https://openairdocs.org/sdr/REXA2021110400936.md): Fitting · damaged · Oct 30, 2021 · N904XJ · Cndair CL6002D24 · Wing Structure
  > "WHILE PERFORMING AILERON WING SIDE BUSHING REPLACEMENT, DAMAGE WAS CAUSED TO MOST I/B FITTING OUTER LUG " "R/R UNSERVICEABLE L/H AILERON WING SIDE FITTING WITH SERVICEABLE FITTING. REFERENCE LINE ITEMS #1-19 FOR WORK PERFORMED WVAC EM
- [SDR REXA2021110400934](https://openairdocs.org/sdr/REXA2021110400934.md): Plate · damaged · Oct 30, 2021 · N904XJ · Cndair CL6002D24 · Wing Structure
  > "WHILE PERFORMING AILERON WING SIDE BUSHING REPLACEMENT, DAMAGE WAS CAUSED TO MOST I/B FITTING OUTER LUG " "R/R UNSERVICEABLE L/H AILERON WING SIDE FITTING WITH SERVICEABLE FITTING. REFERENCE LINE ITEMS #1-19 FOR WORK PERFORMED WVAC EM
- [SDR REXA2021110400932](https://openairdocs.org/sdr/REXA2021110400932.md): Fitting · elongated · Oct 29, 2021 · N904XJ · Cndair CL6002D24 · Aileron Control System
  > "LH AILERON MIDDLE LUG I/B FITTING FOUND TO HAVE 2EA OVERSIZED BUSHING BORES. (MEASURED AT.800"" AND.885"") " "FABBED AND INSTALLED OVERSIZED BUSHINGS ON L/H AILERON MID LUG IAW MHIRJ REO 690-57-51-234 REV-- DATED 2021-10-18 & AMM
- [SDR REXA2021110400893](https://openairdocs.org/sdr/REXA2021110400893.md): Angle · corroded · Oct 28, 2021 · N904XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "RH MLG TIRE BURST PANEL FWD SUPPORT ANGLE HAS MULTIPLE SPOTS OF CORROSION. " "REPLACED RH FWD SUPPORT ANGLE IAW SRM 57-42-21-001-001-A01 & 51-40-11-001-001-A01. LK CK GOOD. WVAC E
- [SDR REXA2021110400892](https://openairdocs.org/sdr/REXA2021110400892.md): Angle · corroded · Oct 28, 2021 · N904XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "LH MLG TIRE BURST PNL FWD SUPPORT ANGLE HAS MULTIPLE SPOTS OF CORROSION. " "REPLACED UNSERVICEABLE L/H FWD SUPPORT ANGLE WITH A SERVICEABLE ANGLE IAW CRJ900 SRM 51-42-21-001-001(A01 & 51-40-11-001-001(A01)
- [SDR REXA2021110400933](https://openairdocs.org/sdr/REXA2021110400933.md): Fitting · elongated · Oct 25, 2021 · N904XJ · Cndair CL6002D24 · Aileron Control System
  > "RH AILERON BEARING LUG A WAS FOUND TO BE OVERSIZE, BEYOND LIMITS, NOMINAL SIZE 0.9057"" - 0.9067"" BORE MEASURES 0.9092"". " "COMPLIED WITH MHIRJ REO #690-57-61-232 REV-- DATED 2021-10-20 FOR REPAIR.
- [SDR REXA2021110400931](https://openairdocs.org/sdr/REXA2021110400931.md): Fitting · elongated · Oct 25, 2021 · N904XJ · Cndair CL6002D24 · Aileron Control System
  > "RH AILERON BUSHING LUGS G&D BORES OUT OF LIMITS MEASURED AT.7495, LUG D MEASURED AT.7490, LUG C AND H GOUGED AND WILL REQ OVERSIZE REO REQ'D. " " COMPLIED WITH MHIRJ REO #690-57-61-233 REV-- DATED
- [SDR REXA2021110400913](https://openairdocs.org/sdr/REXA2021110400913.md): Support · corroded · Oct 25, 2021 · N904XJ · Cndair CL6002D24 · Fuselage Main, Structure
  > "FWD JACK FITTING AT FS278 BL0 BOTH SUPPORT INTERCOSTALS ARE CORRODED. " " COMPLIED WITH ENDEAVOR EA#CRJ953-12286 REV IR DATED 10/19/2021 FOR REPAIR, REMOVED AND REINSTALLED SAME SERVICEABLE NOSE JACK PAD
- [SDR REXA2021110400929](https://openairdocs.org/sdr/REXA2021110400929.md): Intercostal · damaged · Oct 23, 2021 · N904XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "FOUND IN 70R COSTAL DAMAGED @ FWD END BETWEEN STR 23L AND 22L FS 501-THRU 517. " "CLEANED REPAIR AREA AND CIC BAYS BETWEEN STGR 23L TO 22L AND FS 501 THRU 517 IAW CRJ 900 SRM 51-26-00-001-001-A01 AND 51
- [SDR REXA2021110400930](https://openairdocs.org/sdr/REXA2021110400930.md): Fitting · elongated · Oct 21, 2021 · N904XJ · Cndair CL6002D24 · Aileron Control System
  > "LH AILERON BUSHING LUG D BORE OUT OF LIMITS MEASURED @.7494 MAX ALLOWED.7488, REO REQ'D. " "REPAIRED L/H AILERON BUSHING JUG D AND INSTALLED BUSHING IAW MHIRJ REO 690-57-61-231 REV-- 2021-10-19. WVAC EMP #7358
- [SDR REXA2021110400911](https://openairdocs.org/sdr/REXA2021110400911.md): Longeron · corroded · Oct 21, 2021 · N904XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "FWD BAGGAGE BAY DOOR SURROUND STRUCTURE, LOWER LONGERON HAS DRILL HOLES IN SILL PLATE BTW FS517 AND FS533. " "COMPLIED WITH ENDEAVOR EA# CRJ953-12093 REV IR DATED 9/15/2021 FOR REPAIR. REMOVED AND REINSTALLED FWD BAGGAGE BAY DOOR BALANCE SP
- [SDR REXA2021110400908](https://openairdocs.org/sdr/REXA2021110400908.md): Intercostal · corroded · Oct 20, 2021 · N904XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "STRINGER AND INTERCOSTAL CORRODED AT STGR 20R BETWEEN FS 295 AND FS 349. " "LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE INTERCOSTALS AT STG 20R IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-06
- [SDR REXA2021110400907](https://openairdocs.org/sdr/REXA2021110400907.md): Intercostal · corroded · Oct 20, 2021 · N904XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "STRINGER AND INTERCOSTAL CORRODED AT STGR 20R BETWEEN FS 295 AND FS 349. " "LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE INTERCOSTALS AT STG 20R IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-06
- [SDR REXA2021110400906](https://openairdocs.org/sdr/REXA2021110400906.md): Stringer · corroded · Oct 20, 2021 · N904XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "STRINGER AND INTERCOSTAL CORRODED AT STGR 20R BETWEEN FS 295 AND FS 349. " "LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE INTERCOSTALS AT STG 20R IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-06
- [SDR REXA2021110400909](https://openairdocs.org/sdr/REXA2021110400909.md): Frame · corroded · Oct 19, 2021 · N904XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "FRAME AT FS 319 CORRODED BETWEEN STGR 19L AND STGR 25R. " "REPLACED FRAME A FS319 IAW SRM 53-00-00-101-001-A01 51-42-06-001-001-A01, 53-00-06-201-006-A01 & APPLIED CIC IAW SRM 51-21-11-001-001-A01. WVAC EMP # 60
- [SDR REXA2021110400896](https://openairdocs.org/sdr/REXA2021110400896.md): Channel · corroded · Oct 19, 2021 · N904XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "TCAS ANTENNA, LOWER CHANNEL CORRODED BETWEEN FS 295 AND FS 310 AT STGR 27. " "LOCATED, DRILLED, AND INSTALLED NEW TCAS CHANNEL IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-
- [SDR REXA2021110400928](https://openairdocs.org/sdr/REXA2021110400928.md): Stringer · corroded · Oct 16, 2021 · N904XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > STR 27 FS 310-333 IS CORRODED AROUND FASTENERS. "REPLACED STR 27 FS 310-333 & APPLIED CIC IAW SRM 51-42-06-011- 001-A01 & 51-21-11-001-001-A01. WVAC EMP #6027 "
- [SDR REXA2021110400937](https://openairdocs.org/sdr/REXA2021110400937.md): Beam · corroded · Oct 13, 2021 · N904XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "4 EACH FASTENER HOLES HAVE LOW EDGE DISTANCE ON LBL9 & RBL9 LONGITUDINAL BEAMS JUST AFT OF FS280 CROSSBEAM COMMON TO ""T"" BRACKETS. " "REPAIRED FASTNERS HOLES LBL9 & RBL9 LONGITUDINAL BEAMS AFT OF
- [SDR REXA2021110400935](https://openairdocs.org/sdr/REXA2021110400935.md): Cleat · damaged · Oct 13, 2021 · N904XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "STRINGER CLIP AT FS 333 STR 26R DAMAGED ON REMOVAL. " "REMOVED AND REPLACED WITH A NEW SERVICEABLE FRAME CLIP AT FS 333 STGR 26R IAW CRJ 900 SRM 51-42-06-001-001-A01. WVAC EMP STAMP #791 MTC "
- [SDR REXA2021110400923](https://openairdocs.org/sdr/REXA2021110400923.md): Longeron · corroded · Oct 13, 2021 · N904XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "LONGERON AT STR 25R FROM FS 333 TO FS 364 IS HEAVILY CORRODED. " "REMOVED/REPLACED LONGERON IAW SRM 51-40-11-001-001-A01, 51-42-21-001-001-A01, 51-42-00-001-001-A01, 51-23-00-001-001-A01. WVAC EMP # 6027
- [SDR REXA2021110400919](https://openairdocs.org/sdr/REXA2021110400919.md): Retainer · corroded · Oct 13, 2021 · N904XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "LH SIDE SEAT TRACK RETAINER CHANNEL FS 785-847+8.4 SEGEMENT IS CORRODED. " "REMOVED AND REPLACED LH SIDE SEAT TRACK RETAINER PT#SH690-37556-953 IAW CRJ 900 SRM 51-23-00-001-001-A01 AT FS 785 TO 847, REMO
- [SDR REXA2021110400910](https://openairdocs.org/sdr/REXA2021110400910.md): Frame · corroded · Oct 13, 2021 · N904XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "FRAME AT FS501 CORRODED BTW STGR 24L AND STGR 25R. " "REMOVED CORROSION 25L TO 25R WITHIN LIMITS SRM 51-31-06-101-003-A04. REPAIRED FRAME AT 24L - 25L IAW EA CRJ 953-12152. INSTALLED ANGLE AND INTERCOSTAL IAW SRM 51-42-21-001-001-A01 AND 51-42-24-001-001-
- [SDR REXA2021110400905](https://openairdocs.org/sdr/REXA2021110400905.md): Bracket · corroded · Oct 13, 2021 · N904XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "STRINGER AND BRACKET CORRODED AT STGR 22R BETWEEN FS 280 AND FS 295. " "FOUND NO CORROSION ON STR 22R 280-295 REPLACED BRACKET IAW SRM 51-42- 06-001-001. WVAC EMP STAMP #714 MTC "
- [SDR REXA2021110400903](https://openairdocs.org/sdr/REXA2021110400903.md): Frame · corroded · Oct 13, 2021 · N904XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "FRAME AT FS 310 CORRODED BETWEEN STGR 25L AND STGR 25R. " "REPAIRED FRAME 310 IAW EA CRJ 953-12226 & SRM 53-00-06-201-006-A01 WVAC EMP #6027 "
- [SDR REXA2021110400927](https://openairdocs.org/sdr/REXA2021110400927.md): Stringer · corroded · Oct 11, 2021 · N904XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "STRINGER 26R CORRODED BTWN FS 280-333. REQUIRES REMOVAL. " "REMOVED AND REPLACED STGR 26R FS 280-333 IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01,51-40-11-001-001-A01, AND 51-25-16-001-001-A01. WVAC EMP # 6027
- [SDR REXA2021110400926](https://openairdocs.org/sdr/REXA2021110400926.md): Intercostal · corroded · Oct 11, 2021 · N904XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "PAX DOOR INTERCOSTAL DD7 1ST FROM HINGE FWD SIDE IS CORRODED P/N: 601R318826-1 " "REMOVED AND REPLACED INTERCOTAL DD7 P/N 601R318826-1 IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, REV 38 7
- [SDR REXA2021110400925](https://openairdocs.org/sdr/REXA2021110400925.md): Intercostal · cracked · Oct 11, 2021 · N904XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "PAX DOOR INTERCOSTAL DD7 1ST FROM HINGE AFT SIDE IS CRACK P/N: 601R318825-1. " "REMOVED AND REPLACED INTERCOTAL DD7 P/N 601R318825-1 IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, REV 38 7-25-2
- [SDR REXA2021110400924](https://openairdocs.org/sdr/REXA2021110400924.md): Stiffener · cracked · Oct 11, 2021 · N904XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "STIFFENER ON PAX DOOR AFT WEB FOR POWER ASSIST MOTOR IS CRACK P/N: 601R317745-7. " "REMOVED AND REPLACED PAX DOOR AFT WEB STIFFENER P/N 601R317745-7 IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-06-001-00
- [SDR REXA2021110400922](https://openairdocs.org/sdr/REXA2021110400922.md): Seat Track · corroded · Oct 11, 2021 · N904XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "RH SIDE SEAT TRACK FS 744- FS 761 SEGMENT IS CORRODED. " "REMOVED/REINSTALLED FASTENERS ON INSTECOSTALS FOR ACCESS REMOVED/REPLACED SEAT TRACK IAW SRM 51-42-06-001-001-A01, 51-42-13- 001-001-A01, 51-42-21-001-001-A01 AND AMM 53-00-49-000/400-801
- [SDR REXA2021110400904](https://openairdocs.org/sdr/REXA2021110400904.md): Frame · corroded · Oct 11, 2021 · N904XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "FRAME AT FS 295 CORRODED BETWEEN STGR 25L AND STGR 25R " "COMPLIED WITH CRJ900 SRM 53-00-06-201-006-A01 FOR REPAIR TO FRAME AT F.S. 295 BETWEEN STGR 25L AND STGR 25R WVAC EMP STAMP # 738 MTC "
- [SDR REXA2021110400902](https://openairdocs.org/sdr/REXA2021110400902.md): Frame · corroded · Oct 11, 2021 · N904XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "FRAME AT FS 349 CORRODED BETWEEN STGR 25L AND 25R " "REMOVED AND REPLACED FRAME FS 349 24L-24R IAW CRJ SRM 57-42-06-001- 001-A01, 51-42-21-001-001-A01, 51-40-11-001-001-A01 WVAC EMP # 6027 "
- [SDR REXA2021110400899](https://openairdocs.org/sdr/REXA2021110400899.md): Intercostal · corroded · Oct 11, 2021 · N904XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "MAIN AVIONICS BAY DOOR STRUCTURE (SURROUND) FWD INTERCOSTAL CORRODED AT STGR 27L BETWEEN FS 349 AND FS 364 " "REMOVED & REPLACED INTERCOSTAL IAW SRM 51-40-11-001-001-A01, 51-42- 06-001-001-A01, 51-42-21-001-001-A01 AND 51-25-01-001 WVAC EMP
- [SDR REXA2021110400895](https://openairdocs.org/sdr/REXA2021110400895.md): Intercostal · corroded · Oct 11, 2021 · N904XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "PAX DOOR INTERCOSTAL AT BASE OF LATCH LOCK BOX MECHANISM IS CORRODED. " "INSTALLED NEW CLEAT P/N: 600-31902-269 AND REMOVED AND REPLACED INTERCOSTAL P/N: 601R318057-1 IAW CRJ900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
- [SDR REXA2021110400894](https://openairdocs.org/sdr/REXA2021110400894.md): Cleat · corroded · Oct 11, 2021 · N904XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "PAX DOOR INTERCOSTAL AT BASE OF LATCH LOCK BOX MECHANISM IS CORRODED. " "INSTALLED NEW CLEAT P/N: 600-31902-269 AND REMOVED AND REPLACED INTERCOSTAL P/N: 601R318057-1 IAW CRJ900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.

Next page: https://openairdocs.org/aircraft/N904XJ/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 = 'N904XJ' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N904XJ/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.