# Service difficulty reports: N925XJ

A list on [N925XJ](https://openairdocs.org/aircraft/N925XJ.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 REXA2026082501640](https://openairdocs.org/sdr/REXA2026082501640.md): Bulb · burned out · Aug 23, 2026 · N925XJ · Cndair CL6002D24 · Emergency Lighting
  > FLOOR LEVEL EMERGENCY FLOOD LIGHTS AT PAX & SERVICE DOOR HAVE BURNED OUT BULBS R & R BULBS OPC GOOD IAW AMM 33-51-00.
- [SDR REXA2026073001348](https://openairdocs.org/sdr/REXA2026073001348.md): Lug · damaged · Jul 28, 2026 · N925XJ · Cndair CL6002D24 · Wing, Control Surface Attach Fittings
  > FABRICATE OVERSIZE BUSHINGS FOR LUGS R1, R2, R5 & R6. LUG R1 WAS REWORKED AND BUSHINGS OVERSIZE FOR LUGS R2, R5 & R6 WERE FABRICATED PER REO 670-57-61-237 REV.--
- [SDR REXA2026073001347](https://openairdocs.org/sdr/REXA2026073001347.md): Lug · corroded · Jul 18, 2026 · N925XJ · Cndair CL6002D24 · Wing, Control Surface Attach Fittings
  > CORROSION AND WEAR WAS FOUND ON LUG BORE ON AIL STA 336.4015 (LUG L1), 337.657 (LUG L2), 342.911 (LUG L5), 344.1665 (LUG L6) AT LH AILERON. CORROSION AND WEAR ON LUG BORE ON AIL STA 336.4015 (LUG L1), 337.657 (LUG L2), 342.911 (LUG L5), 344.1665 (LUG L6) AT LH
- [SDR REXA2026073001334](https://openairdocs.org/sdr/REXA2026073001334.md): Web · corroded · Jun 18, 2026 · N925XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON WEB FLOOR PROTECTOR (4EAS) AT SERVICE DOOR SURROUND STRUCTURE CORROSION ON WEB FLOOR PROTECTOR (4EAS) AT SERVICE DOOR SURROUND STRUCTURE WAS REMOVED AND EVALUATED OUT OF LIMITS PER CRJ900 SRM 51-21-06-001-001-A01 AND CRJ-900 SRM 53-00-00-101-001-
- [SDR REXA2026073001333](https://openairdocs.org/sdr/REXA2026073001333.md): Bracket · corroded · Jun 18, 2026 · N925XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON WEB FLOOR PROTECTOR (4EAS) AT SERVICE DOOR SURROUND STRUCTURE CORROSION ON WEB FLOOR PROTECTOR (4EAS) AT SERVICE DOOR SURROUND STRUCTURE WAS REMOVED AND EVALUATED OUT OF LIMITS PER CRJ900 SRM 51-21-06-001-001-A01 AND CRJ-900 SRM 53-00-00-101-001-
- [SDR REXA2026073001332](https://openairdocs.org/sdr/REXA2026073001332.md): Protector · corroded · Jun 18, 2026 · N925XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON WEB FLOOR PROTECTOR (4EAS) AT SERVICE DOOR SURROUND STRUCTURE CORROSION ON WEB FLOOR PROTECTOR (4EAS) AT SERVICE DOOR SURROUND STRUCTURE WAS REMOVED AND EVALUATED OUT OF LIMITS PER CRJ900 SRM 51-21-06-001-001-A01 AND CRJ-900 SRM 53-00-00-101-001-
- [SDR REXA2026073001331](https://openairdocs.org/sdr/REXA2026073001331.md): Bracket · corroded · Jun 18, 2026 · N925XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON WEB FLOOR PROTECTOR (4EAS) AT SERVICE DOOR SURROUND STRUCTURE CORROSION ON WEB FLOOR PROTECTOR (4EAS) AT SERVICE DOOR SURROUND STRUCTURE WAS REMOVED AND EVALUATED OUT OF LIMITS PER CRJ900 SRM 51-21-06-001-001-A01 AND CRJ-900 SRM 53-00-00-101-001-
- [SDR REXA2026073001335](https://openairdocs.org/sdr/REXA2026073001335.md): Seal · worn · Jun 17, 2026 · N925XJ · Cndair CL6002D24 · Wing Main, Frame Structure
  > LT WING TRAILING EDGE P-SEAL WORN BELOW MFS LOWER TRAILIND EDGE. LT WING TRAILING EDGE P-SEAL ON MFS LOWER TRAILIND EDGE WAS REPLACED PER CRJ-900 AMM 57-50-07 (CONFIG A01)
- [SDR REXA2026073001351](https://openairdocs.org/sdr/REXA2026073001351.md): Fitting · corroded · Jun 14, 2026 · N925XJ · Cndair CL6002D24 · Fuselage, Equipment Attach Fittings
  > CORROSION FLOOR FITTING IN AFT ACCESS 108 (1EA) ON GALLEY 1. SUMMARY OF NRC 00306: NEW FLOOR FITTING P/N: CDSP2019-7C-760 IN AFT ACCESS 108 (1EA) ON GALLEY 1. WAS REPLACED PER SAFRAN CMM 25-33-67 REV. NO 10 DATED JUN 20/22
- [SDR REXA2026073001350](https://openairdocs.org/sdr/REXA2026073001350.md): Fitting · corroded · Jun 14, 2026 · N925XJ · Cndair CL6002D24 · Fuselage, Equipment Attach Fittings
  > CORROSION FLOOR FITTING IN FWD ACCESS 306 (1EA) ON GALLEY 3. SUMMARY OF NRC 00304: NEW FLOOR FITTING P/N: CDSP2019-7C-650 IN FWD ACCESS 306 (1EA) ON GALLEY 3. WAS REPLACED PER ZODIAC AEROSPACE CMM 25-33-18 REV NO 5 DATED MAY 15/15
- [SDR REXA2026073001349](https://openairdocs.org/sdr/REXA2026073001349.md): Fitting · corroded · Jun 14, 2026 · N925XJ · Cndair CL6002D24 · Fuselage, Equipment Attach Fittings
  > CORROSION FLOOR FITTING IN FWD ACCESS 107 (1EA) ON GALLEY 1. SUMMARY OF NRC 00303: NEW FLOOR FITTING P/N: CDSP2019-7C-620 IN FWD ACCESS 107 (1EA) ON GALLEY 1. WAS REPLACED PER SAFRAN CMM 25-33-67 REV. NO 10 DATED JUN 20/22
- [SDR REXA2026073001346](https://openairdocs.org/sdr/REXA2026073001346.md): Hinge · corroded · Jun 14, 2026 · N925XJ · Cndair CL6002D24 · Fuselage, Door Hinge
  > CORROSION ON STEP DOOR HINGE FWD, CENTER, AFT AT AFT BAGGAGE BAY DOOR AREA STEP DOOR HINGE CENTER, AFT AT AFT BAGGAGE BAY DOOR AREA WERE REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01, AND STEP DOOR HINGE FWD AT AFT BAGGAGE BAY DOOR AREA WAS FABRICATED PER EA
- [SDR REXA2026073001345](https://openairdocs.org/sdr/REXA2026073001345.md): Hinge · corroded · Jun 14, 2026 · N925XJ · Cndair CL6002D24 · Fuselage, Door Hinge
  > CORROSION ON STEP DOOR HINGE FWD, CENTER, AFT AT AFT BAGGAGE BAY DOOR AREA STEP DOOR HINGE CENTER, AFT AT AFT BAGGAGE BAY DOOR AREA WERE REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01, AND STEP DOOR HINGE FWD AT AFT BAGGAGE BAY DOOR AREA WAS FABRICATED PER EA
- [SDR REXA2026073001344](https://openairdocs.org/sdr/REXA2026073001344.md): Hinge · corroded · Jun 14, 2026 · N925XJ · Cndair CL6002D24 · Fuselage, Door Hinge
  > CORROSION ON STEP DOOR HINGE FWD, CENTER, AFT AT AFT BAGGAGE BAY DOOR AREA STEP DOOR HINGE CENTER, AFT AT AFT BAGGAGE BAY DOOR AREA WERE REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01, AND STEP DOOR HINGE FWD AT AFT BAGGAGE BAY DOOR AREA WAS FABRICATED PER EA
- [SDR REXA2026073001330](https://openairdocs.org/sdr/REXA2026073001330.md): Seat Track · corroded · Jun 13, 2026 · N925XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON STGR 24R AND FS333.00/FS349.00. CORROSION ON STGR 24R AND FS333.00/FS349.00. WAS EVALUATED OUT LIMITS THEREFORE WAS REPAIRED PER CRJ-900 SRM 53-21-03-101-002-A04 AND SRM 53-00-03-201-001-A0
- [SDR REXA2026073001329](https://openairdocs.org/sdr/REXA2026073001329.md): Floorbeam · cracked · Jun 13, 2026 · N925XJ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > CRACK ON FLOOR BEAM ANGLE RBL 12 AT FS 280.00 WAS FOUND. NEW FLOOR BEAM ANGLE RBL 12 AT FS 280.00 WAS VERIFIED PER CRJ900 SRM 53-11-43-001-001-A01 ///REPLACE WAS PERFORMED UNDER NRC 0057
- [SDR REXA2026073001328](https://openairdocs.org/sdr/REXA2026073001328.md): Stub Frame · corroded · Jun 13, 2026 · N925XJ · Cndair CL6002D24 · Fuselage Main, Structure
  > CORROSION ON STUB FRAME AT FS 533.00 AND FS 549.00 APROX STGR 18 LH AT SURROUND STRUCTURE OF FWD BAGGAGE BAY DOOR STUB FRAME AT FS 533.00 AND FS 549.00 APROX STGR 18 LH AT SURROUND STRUCTURE OF FWD BAGGAGE BAY DOOR WERE EVALUATED OUT LIMITS PER CRJ 900 SRM 51-
- [SDR REXA2026073001327](https://openairdocs.org/sdr/REXA2026073001327.md): Stub Frame · corroded · Jun 13, 2026 · N925XJ · Cndair CL6002D24 · Fuselage Main, Structure
  > CORROSION ON STUB FRAME AT FS 533.00 AND FS 549.00 APROX STGR 18 LH AT SURROUND STRUCTURE OF FWD BAGGAGE BAY DOOR STUB FRAME AT FS 533.00 AND FS 549.00 APROX STGR 18 LH AT SURROUND STRUCTURE OF FWD BAGGAGE BAY DOOR WERE EVALUATED OUT LIMITS PER CRJ 900 SRM 51-
- [SDR REXA2026073001326](https://openairdocs.org/sdr/REXA2026073001326.md): Floor Support · corroded · Jun 13, 2026 · N925XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR SILL AT FLOOOR STRUCTURE PASSENGER CABIN BTW FS 280.00 TO 319.70 FLOOR SILL AT FLOOOR STRUCTURE PASSENGER CABIN BTW FS 280.00 TO 319.70 WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01, SRM 51-42-10-001-001-A01 AND CRJ900 SRM 51-42-13-001-00
- [SDR REXA2026073001325](https://openairdocs.org/sdr/REXA2026073001325.md): Fitting · corroded · Jun 13, 2026 · N925XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON FITTING APROX ON RBL12 FITTING ON RBL12 FS:290 APROX WAS REMPLACED PER. CRJ900 SRM 51-42-21-001-001-A01 6. C.
- [SDR REXA2026073001322](https://openairdocs.org/sdr/REXA2026073001322.md): Skin Splice · corroded · Jun 12, 2026 · N925XJ · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > CORROSION ON INTERNAL SKIN SPLICE AT FS 280.00 TO FS 282.00 FROM STGR 24RH TO 26LH CORROSION ON INTERNAL SKIN SPLICE AT FS 280.00 TO FS 282.00 FROM STGR 24RH TO 26LH WAS REMOVED PER CRJ-900 SRM SRM 51-21-06-001-001-A01 EVALUATED BTW FS 280.00 TO FS 282.00 FROM
- [SDR REXA2026073001339](https://openairdocs.org/sdr/REXA2026073001339.md): Collector · corroded · Jun 11, 2026 · N925XJ · Cndair CL6002D24 · Cabin Equipment/Furnishings
  > CORROSION ON COLLECTOR TRAY CORROSION OF THE COLLECTOR TRAY WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01 AND WAS EVALUATED PER CRJ-900 SRM 53 -00-00-101-001-A01 AND WAS DETERMINING WITH EXCESSIVE DAMAGE. NEW COLLECTOR TRAY WAS VERIFIED PER CRJ900 AIPC 24-2
- [SDR REXA2026073001343](https://openairdocs.org/sdr/REXA2026073001343.md): Strap · corroded · Jun 9, 2026 · N925XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON STRAP AT FAIRING 193AB. STRAP(2EAS) AT FAIRING 193AB WERE REPLACED PER SRM 51-42-10-001-001-A01 AND SRM 51-42-06-001-001-A01
- [SDR REXA2026073001342](https://openairdocs.org/sdr/REXA2026073001342.md): Strap · corroded · Jun 9, 2026 · N925XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON STRAP AT FAIRING 193AB. STRAP(2EAS) AT FAIRING 193AB WERE REPLACED PER CRJ-900 SRM 51-42-10-001-001-A01 AND SRM 51-42-06-001-001-A01
- [SDR REXA2026073001341](https://openairdocs.org/sdr/REXA2026073001341.md): Bracket · corroded · Jun 9, 2026 · N925XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON INTERNAL ANGLES IN REFUEL/DEFUEL PANEL AT INTERNAL AREA OF FAIRING 192AR. CORROSION ANGLE (1 EA) IN REFUEL/DEFUEL PANEL AT INTERNAL AREA OF FAIRING 192AR WERE REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01 AND WAS FOUND WITHIN OF LIMITS PER CRJ-900
- [SDR REXA2026073001324](https://openairdocs.org/sdr/REXA2026073001324.md): Stringer · corroded · Jun 9, 2026 · N925XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STGR 21 RH BTWN FS 364.00 TO FS 379.00 CORROSION ON STGR 21 RH BTWN FS 364.00 TO FS 379.00 WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01 EVALUATED OUT LIMITS PER CRJ-900 SRM 53-21-03-101-006-A04 THEREFORES WAS REPLACED PER CRJ 900 SRM 51-42-21-
- [SDR REXA2026073001323](https://openairdocs.org/sdr/REXA2026073001323.md): Angle · corroded · Jun 9, 2026 · N925XJ · Cndair CL6002D24 · Service Doors
  > CORROSION ON MOUNITNG ANGLE OF SERVICE DOOR BTW FS 319 TO 349 AT CPAX MOUNITNG ANGLE OF SERVICE DOOR BTW FS 319 TO 349 AT CPAX WAS EVALUATED OUT OF LIMITS DUE TO EXCESIVE CORROSION PER CRJ-900 SRM 53-00-00-101-001-A01, THEREFORE WAS REPLACED PER CRJ-900 SRM 51
- [SDR REXA2026073001340](https://openairdocs.org/sdr/REXA2026073001340.md): Access Panel · corroded · Jun 8, 2026 · N925XJ · Cndair CL6002D24 · Fuselage Main, Structure
  > CORROSION ON ACCESS PANEL 542AZ, 542BZ, 642AZ AND 642BZ. CORROSION WERE REMOVED ON ACCESS PANEL 542BZ AND 642BZ PER CRJ-900 SRM 51-21-06-001-001-A01 AND WERE FOUND WITHIN LIMITS PER CRJ-900 SRM 53-00-01-101-001-A01. ACCESS PANELS 542AZ AND 642AZ WERE REPLACED
- [SDR REXA2026073001321](https://openairdocs.org/sdr/REXA2026073001321.md): Seat Track · corroded · Jun 6, 2026 · N925XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SIDE SEAT RAILS BTW STA FS379 TO FS699 STGR15LH AND STGR15RH SIDE SEAT RAILS BTW STA FS379 TO FS699 STGR15LH AND STGR15RH WERE EVALUATED OUT LIMITS PER CRJ/900 SRM 53-21-49-101-001-A01, SRM 53-31-49-101-001-A02 THEREFORE WERE REPLACED PER CRJ 900
- [SDR REXA2026073001319](https://openairdocs.org/sdr/REXA2026073001319.md): Strap · cracked · Jun 6, 2026 · N925XJ · Cndair CL6002D24 · Spoilers
  > CRACK ON STRAP AT GROUND SPOILERS (2EAS INB/OUT) AT LH WING AND (1EA INB) AT RH WING SPS 21.80 PROTECTOR PLATE AT SERVICE DOOR SURROUND STRUCTURE WAS EVALUATED DUE EXCCESSIVE CORROSION AND WILL BE REPLACED PER CRJ900 SRM 51-10-06-001-001-A01, THEREFORE NEW PRO
- [SDR REXA2026073001318](https://openairdocs.org/sdr/REXA2026073001318.md): Strap · cracked · Jun 6, 2026 · N925XJ · Cndair CL6002D24 · Spoilers
  > CRACK ON STRAP AT GROUND SPOILERS (2EAS INB/OUT) AT LH WING AND (1EA INB) AT RH WING SPS 21.80 PROTECTOR PLATE AT SERVICE DOOR SURROUND STRUCTURE WAS EVALUATED DUE EXCCESSIVE CORROSION AND WILL BE REPLACED PER CRJ900 SRM 51-10-06-001-001-A01, THEREFORE NEW PRO
- [SDR REXA2026073001317](https://openairdocs.org/sdr/REXA2026073001317.md): Stringer · corroded · Jun 6, 2026 · N925XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STGR 27 BTW FS1162.00 AND FS 1181.00 AT REAR FUSELAGE INERNAL STRUCURE. NEW STRINGER STGR 27 BTW FS1162.00 AND FS 1181.00 AT REAR FUSELAGE INERNAL STRUCURE WAS FABRICATED PER CRJ-900 DGW: MM670-38134 REV. F AND REPLACED PER CRJ-900 SRM 51-42-06-00
- [SDR REXA2026073001316](https://openairdocs.org/sdr/REXA2026073001316.md): Support Angle · cracked · Jun 6, 2026 · N925XJ · Cndair CL6002D24 · Wing Miscellaneous Structure
  > CRACK ON LH WING BRACKET SUPPORT ANGLE SS 15.50, LOWER INNER AREA. CRACK ON LH WING BRACKET SUPPORT ANGLE SS 15.50, LOWER INNER AREA WAS REPAIRED PER EA NO: CRJ957-22519 EA REV IR
- [SDR REXA2026073001315](https://openairdocs.org/sdr/REXA2026073001315.md): Track · worn · Jun 6, 2026 · N925XJ · Cndair CL6002D24 · Cargo/Baggage Doors
  > WEAR LOWER AFT RAIL OF AFT BAGGAGE DOOR LOWER AFT RAIL OF AFT BAGGAGE DOOR WAS REPAIRED PER EA:CRJ953-22520 REV IR
- [SDR REXA2026073001314](https://openairdocs.org/sdr/REXA2026073001314.md): Roller · worn · Jun 6, 2026 · N925XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > WEAR AFT ROLLER GUIDE UPPER AT AFT BAGGAGE BAY DOOR AFT ROLLER GUIDE UPPER AT AFT BAGGAGE BAY DOOR WAS EVALUATED OUT LIMITS PER CRJ 900 SRM 53-00-00-101-001-A01 THEREFORE WAS REPLACED PER CRJ 900 SRM 51-42-06-001-001-A01
- [SDR REXA2025031000298](https://openairdocs.org/sdr/REXA2025031000298.md): Battery Pack · inoperative · Mar 9, 2025 · N925XJ · Cndair CL6002D24 · Emergency Lighting
  > L AND R AFT EXTERIOR EMERGENCY LIGHTS INOP R/R AFT(PS38) EMERGENCY LIGHT BATTERY ASSY AND CHARGER ASSY IAW CRJ900 AMM 33-51-17 OPC GOOD
- [SDR REXA2025031000297](https://openairdocs.org/sdr/REXA2025031000297.md): Battery Pack · inoperative · Mar 6, 2025 · N925XJ · Cndair CL6002D24 · Emergency Lighting
  > FOUND EMERGENCY LIGHTING IN CABIN REAR AND EXTERNAL REAR NOT WORKING R/R EPSU BATTERY PACK PS38 IAW JOB CARD 33-900-701. OPS CHECK GOOD, NO FURTHER DEFECTS NOTED P/N ON/OFF 2013-1ASMI S/N ON 19356 S/N OFF 19241
- [SDR REXA2024062400483](https://openairdocs.org/sdr/REXA2024062400483.md): Windshield · inoperative · Jun 19, 2024 · N925XJ · Cndair CL6002D24 · Flight Compartment Windows
  > DURING TAKEOFF AT ABOUT 1000 FEET, CAPTAIN'S WINDSHIELD ON LOWER LEFT SIDE STARTED SMOKING. TURNED OFF WINDSHIELD HEAT AND RETURNED TO CVG. ALSO SMELLED SMOKE FOR THE REMAINDER OF THE FLIGHT. REMOVED AND REPLACED LH CAPTAINS WINDSHIELD IAW 700/900 JC 900-56-9
- [SDR REXA2022042100295](https://openairdocs.org/sdr/REXA2022042100295.md): Beam · cracked · Apr 4, 2023 · N925XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > RBL 18 POST AT INBOARD FLANGE CRACKED. REMOVED AND REPLACED IAW CRJ 900 SRMS 51-40-11-001-001-A01, AND 51-42-06-001-001-A01.
- [SDR REXA2022031600261](https://openairdocs.org/sdr/REXA2022031600261.md): Web · cracked · Mar 15, 2023 · N925XJ · Cndair CL6002D24 · Fuselage Main, Structure
  > FWD EQUIPMENT COMPARTMENT, L/H FLOOR IS CRACKED AT F.S.193. REPAIRED L/H FLOOR IN THE FWD EQUIPMENT COMPARTMENT AT F.S. 193.
- [SDR REXA2021080300527](https://openairdocs.org/sdr/REXA2021080300527.md): Bulb · inoperative · Jul 29, 2021 · N925XJ · Cndair CL6002D24 · Emergency Lighting
  > RIGHT SIDE AFT MOST EMER LIGHT EXTERIOR IS INOP. REMOVED AND REPLACED RH AFT MOST OVERWING EMER. EXIT LIGHT BULB IAW AMM 33-51-15. OP/C GOOD.
- [SDR REXA2021042000246](https://openairdocs.org/sdr/REXA2021042000246.md): Battery Pack · discharged · Apr 16, 2021 · N925XJ · Cndair CL6002D24 · Emergency Lighting
  > EPSU BATTERY PACK DEAD (PS38). REMOVED AND REPLACED EPSU BATTERY PACK (PS38). OPERATIONAL TEST OF THE EPSU CHECK GOOD IAW AMM 33-51-17 PN OFF 2013-1A SN OFF 101377 PN ON 2013-1ASMI SN ON 12016
- [SDR REXA2020122100839](https://openairdocs.org/sdr/REXA2020122100839.md): Strap · damaged · Dec 16, 2020 · N925XJ · Cndair CL6002D24 · Wing Miscellaneous Structure
  > LT LOWER BUTT STRAP COMMON TO LOWER WING PLANK HAS 1 EA 2ND OVERSIZE 3/8 HOLE LOCATED IN COLD WORK AREA OF TRUNNION. REPAIRED AREA, IAW REO 690-57-21-380 REV-- DATED 12/15/20.
- [SDR REXA201910141426](https://openairdocs.org/sdr/REXA201910141426.md): Stop Fitting · corroded · Oct 10, 2019 · N925XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > CORROSION ON LOWER STOP FITTING AT PASSENGER DOOR. BRACKET ASSY WAS REPLACED FOR NEW ONE (P/N: 601R38921-9) PER CRJ-900 SRM 51-42-06-001-001-A01. PAR 6C.
- [SDR REXA2019101491474](https://openairdocs.org/sdr/REXA2019101491474.md): Shield · perforated · Oct 9, 2019 · N925XJ · Cndair CL6002D24 · Engine (Turbine/Turboprop)
  > WEAR ON PRODUCTION DOUBLER OF PANEL BLOW OFF DOOR AT FORWARD CORE COWL ASSEMBLY UPPER RIGHT SIDE.(INNER FACE) ENGINE NR 2. A NEW BLOW OFF DOOR FIRESHIELD WAS INSTALLED PER SRM 51-22-00-001-001-A01, PAR.5, SRM 51-42-06-001-001-A01, SRM 51-42-10-001-001-A01, A
- [SDR REXA2019101491461](https://openairdocs.org/sdr/REXA2019101491461.md): Insert · missing · Oct 9, 2019 · N925XJ · Cndair CL6002D24 · Fuselage Floor Panel
  > MISSING INSERT ON FLOOR PANEL 282JRF AT AFT CARGO COMPARTMENT. THE FLOOR PANEL WAS REPLACED FOR NEW ONE IAW AMM 53-00-47.
- [SDR REXA2019101491423](https://openairdocs.org/sdr/REXA2019101491423.md): Intercostal · corroded · Oct 9, 2019 · N925XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > CORROSION ON INTERCOSTAL DD6 BTW FORMER FS320.163 TO 338.963 AT PASSENGER DOOR. INTERCOSTAL DD6 BTW FORMER FS320.163 TO 338.963 AT PASSENGER DOOR WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 PAR. 6. C. AND SRM 51-42-21-001-001-A01 PAR. 6. C
- [SDR REXA2019101491420](https://openairdocs.org/sdr/REXA2019101491420.md): Retainer · dented · Oct 9, 2019 · N925XJ · Cndair CL6002D24 · Cargo/Baggage Doors
  > SEVERAL DENTS ON LOWER RETAINER SEAL ALSO LOWER EDGE AT FWD AND MID CARGO COMPARTMENT DOOR. LOWER RETAINER SEAL FWD AND MID WERE REPLACED PER CRJ/900 AMM 52-35-07-400-802-A02, TOOL USED; TORQUEMETER P/N:QDRIVER4 S/N:0515405073 D/D:06/MAR/20.
- [SDR REXA2019101481465](https://openairdocs.org/sdr/REXA2019101481465.md): Angle · corroded · Oct 8, 2019 · N925XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON SUPPORT MOUNTING ANGLE BTW BS 319 TO 349 AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX). SUPPORT MOUNTING ANGLE BTW FS= 319 TO 349 AT GALLEY SERVICE DOOR LOWER WAS REPLACED PER SRM 51-42-06-001-001-A01.
- [SDR REXA2019101401458](https://openairdocs.org/sdr/REXA2019101401458.md): Floor Support · corroded · Oct 7, 2019 · N925XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR BEAM 9LBL BTW STA. FS= 1015 AND FS= 1047 AT AFT BAGGAGE BAY. FLOOR BEAM 9LBL BTW FS:1015 AND FS:1047 AT AFT BAGGAGE BAY WAS REPAIRED PER CRJ-900 SRM. 53-00-41-201-001-A03 AND CRJ-900 SRM 51-21-06-001-001-A01. CORROSION LEVEL 2.

Next page: https://openairdocs.org/aircraft/N925XJ/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 = 'N925XJ' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N925XJ/reports

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