# Service difficulty reports: N926XJ

A list on [N926XJ](https://openairdocs.org/aircraft/N926XJ.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 · 253 reports

- [SDR REXA2026082601650](https://openairdocs.org/sdr/REXA2026082601650.md): Skin · cracked · Jul 28, 2026 · N926XJ · Cndair CL6002D24 · Wing, Plate/Skin
  > CRACK AND WEAR ON UPPER SKIN OF LEADING EDGE PANEL 522BL. DAMAGED LEADING EDGE PANEL (522BL) P/N: CC670-12301-5 S/N: 15184 WAS REPAIRED PER EA CRJ957-22538 REV. A BUTH DISTORTION AFTER COOLING WAS FOUND THEREFORE WAS REPLACED BY SERVICEABLE LEADING EDGE PANE
- [SDR REXA2026082601698](https://openairdocs.org/sdr/REXA2026082601698.md): Bracket · damaged · Jul 20, 2026 · N926XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > AFTER COAMING LOWER REMOVAL, ELONGATED HOLES ON BRACKETS (4EAS), AT AFT BAGGAGE BAY DOOR SURROUND STRUCTURE FS1047.00 WERE FOUND. ANGLES BRACKETS (4EAS) AT AFT BAGGAGE BAY DOOR SURROUND STRUCTURE FS1047.00 WERE REPLACED PER EA: CRJ953-22823 REV. IR, EA: CRJ95
- [SDR REXA2026082601697](https://openairdocs.org/sdr/REXA2026082601697.md): Bracket · damaged · Jul 20, 2026 · N926XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > AFTER COAMING LOWER REMOVAL, ELONGATED HOLES ON BRACKETS (4EAS), AT AFT BAGGAGE BAY DOOR SURROUND STRUCTURE FS1047.00 WERE FOUND. ANGLES BRACKETS (4EAS) AT AFT BAGGAGE BAY DOOR SURROUND STRUCTURE FS1047.00 WERE REPLACED PER EA: CRJ953-22823 REV. IR, EA: CRJ95
- [SDR REXA2026082601696](https://openairdocs.org/sdr/REXA2026082601696.md): Bracket · damaged · Jul 20, 2026 · N926XJ · Cndair CL6002D24 · Fuselage Main, Attach Fittings
  > AFTER COAMING LOWER REMOVAL, ELONGATED HOLES ON BRACKETS (4EAS), AT AFT BAGGAGE BAY DOOR SURROUND STRUCTURE FS1047.00 WERE FOUND. ANGLES BRACKETS (4EAS) AT AFT BAGGAGE BAY DOOR SURROUND STRUCTURE FS1047.00 WERE REPLACED PER EA: CRJ953-22823 REV. IR, EA: CRJ95
- [SDR REXA2026082601652](https://openairdocs.org/sdr/REXA2026082601652.md): Hinge · corroded · Jul 20, 2026 · N926XJ · Cndair CL6002D24 · Ailerons
  > CORROSION & WEAR ON LUG BORE AIL STA 338.424, AIL STA 342.123, AIL STA 336.4015 (L1), AIL STA 337.657 (L2), AIL STA 342.911 (L5), AIL STA 344.1665 (L6), ALSO WEAR ON LUGS EXTERNAL SURFACE AIL STA 336.4015 (L1), AIL 337.657 (L2), AIL 342.911 (L5), AIL STA 344
- [SDR REXA2026082601718](https://openairdocs.org/sdr/REXA2026082601718.md): Hinge · cracked · Jul 16, 2026 · N926XJ · Cndair CL6002D24 · Fuselage, Door Hinge
  > SECONDARY NRC FROM NRC. 00318: AFTER REMOVAL PAINT CRACK ON FWD HINGE OF THE FLAP STEP PLATE AT AFT BAGGAGE BAY DOOR CUTOUT WAS FOUND. FWD HINGE OF THE FLAP STEP PLATE AT AFT BAGGAGE BAY DOOR CUTOUT (MM670-35624-003) WAS REPLACED PER CRJ-900 SRM 51-42-06-001-
- [SDR REXA2026082601701](https://openairdocs.org/sdr/REXA2026082601701.md): Bracket · corroded · Jul 7, 2026 · N926XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON BRACKET'S MACHINED (10EAS) BTW FS515 TO FS661+8.40 STGR 22L TO STGR 24R AT CENTER AND FWD BAGGAGE COMPARTMENT. BRACKET'S MACHINED (3EAS) BTW FS515 TO FS661+8.40 STGR 22L TO STGR 24R AT CENTER AND FWD BAGGAGE COMPARTMENT WERE CLEANED AND NOT CORROS
- [SDR REXA2026082601709](https://openairdocs.org/sdr/REXA2026082601709.md): Retainer · corroded · Jul 3, 2026 · N926XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > CORROSION AND WEAR ON SEAL RETAINER OF PASSENGER DOOR LWR STEP PANEL 832FT. SEAL RETAINER ON PASSENGER DOOR LWR STEP PANEL 832FT WAS REPLACED PER CRJ-900 SRM 51-41-02-001-001-A01.
- [SDR REXA2026082601742](https://openairdocs.org/sdr/REXA2026082601742.md): Floor Support · cracked · Jul 1, 2026 · N926XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK ON FLOOR SUPPOR ANGLE (2EAS) LOCATED BTW FS280 TO FS265 AND LBL 12'' & RBL 12'' AT CPIL FLOOR STRUCTURE. FLOOR SUPPOR ANGLE (2EAS) LOCATED BTW FS280 TO FS265 AND LBL 12'' & RBL 12'' AT CPIL FLOOR STRUCTURE WERE REPLACED PER CRJ900 SRM 51-42-06-001-001-A
- [SDR REXA2026082601741](https://openairdocs.org/sdr/REXA2026082601741.md): Floor Support · cracked · Jul 1, 2026 · N926XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK ON FLOOR SUPPORT ANGLE (2EAS) LOCATED BTW FS280 TO FS265 AND LBL 12'' & RBL 12'' AT CPIL FLOOR STRUCTURE. FLOOR SUPPOR ANGLE (2EAS) LOCATED BTW FS280 TO FS265 AND LBL 12'' & RBL 12'' AT CPIL FLOOR STRUCTURE WERE REPLACED PER CRJ900 SRM 51-42-06-001-001-
- [SDR REXA2026082601717](https://openairdocs.org/sdr/REXA2026082601717.md): Rib · cracked · Jul 1, 2026 · N926XJ · Cndair CL6002D24 · Wing, Rib/Bulkhead
  > CRACK ON RIB OF ACCESS PANEL NBR:521AT STIFFENER (RIB) ON ACCESS PANEL 521AT WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01
- [SDR REXA2026082601733](https://openairdocs.org/sdr/REXA2026082601733.md): Fitting · corroded · Jun 29, 2026 · N926XJ · Cndair CL6002D24 · Fuselage Main, Attach Fittings
  > CORROSION FLOOR FITTING IN FWD ACCESS 205 (1EA) ON GALLEY 2 FLOOR FITTING IN FWD ACCESS 205 (1EA) ON GALLEY 2 WAS REPLACED IAW CMM 25-32-84 REV. 9 DATE JUN 06/24.
- [SDR REXA2026082601684](https://openairdocs.org/sdr/REXA2026082601684.md): Latch · cracked · Jun 26, 2026 · N926XJ · Cndair CL6002D24 · Engine Thrust Reverser
  > AFTER COAMING LATCH REMOVAL, CRACK ON SKIN AT LH UPPER TRANSCOWL WAS FOUND. SKIN AT LH UPPER TRANSCOWL WAS REPAIRED PER EA NO: CRJ954-22469 REV A
- [SDR REXA2026082601675](https://openairdocs.org/sdr/REXA2026082601675.md): Lug · corroded · Jun 21, 2026 · N926XJ · Cndair CL6002D24 · Ailerons
  > CORROSION & WEAR ON LUG BORE AIL STA 364.016 (UPPER/LOWER), AIL STA 338.424, AILSTA 342.123, AIL STA 311.539, AIL STA 336.4015 (R1), AIL STA 337.657 (R2), AIL 342.911 (R5), AIL STA 344.1665 (R6), ALSO WEAR ON LUGS EXTERNAL SURFACE AIL STA 337.657 (R2), AIL STA
- [SDR REXA2026082601695](https://openairdocs.org/sdr/REXA2026082601695.md): Floor Support · corroded · Jun 20, 2026 · N926XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > AFTER FLOOR ANGLE REMOVAL, CORROSION ON RH FLOOR CROSSBEAM FS280 & RBL 9'' WAS FOUND. RH FLOOR CROSSBEAM FS280 & RBL 9'' WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 51-10-06-001-001-A01 AND WAS REPLACED PER CRJ900 SRM TS #: 008501-R1,SRM 51-42-06-001-001-A01,
- [SDR REXA2026082601716](https://openairdocs.org/sdr/REXA2026082601716.md): Access Panel · cracked · Jun 19, 2026 · N926XJ · Cndair CL6002D24 · Vertical Stabilizer, Plate/Skin
  > CRACK ON FASTENER HOLE OF ACCESS PANEL NBR:326DL. ACCESS PANEL NBR:326DL WAS REPAIRED PER EA NO. CRJ955-22596 REV IR
- [SDR REXA2026082601694](https://openairdocs.org/sdr/REXA2026082601694.md): Floor Support · corroded · Jun 19, 2026 · N926XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON LOWER SILL OF AFT BAGGAGE COMPARTMENT DOOR. CORROSION ON LOWER SILL OF AFT BAGGAGE COMPARTMENT DOOR.WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 51-10-06-001-001-A01 AND WAS REPLACE PER CRJ900 SRM 51-42-06-001-001-A01, CRJ900 SRM 51-42-21-001-001-A
- [SDR REXA2026082601651](https://openairdocs.org/sdr/REXA2026082601651.md): Transcowl · cracked · Jun 19, 2026 · N926XJ · Cndair CL6002D24 · Engine Thrust Reverser
  > CRACK ON SCOOP AT RH UPPER TRANSCOWL. SCOOP AT RH UPPER TRANSCOWL WAS REPAIRED PER EA NO. CRJ954-22542 REV IR.
- [SDR REXA2026082601646](https://openairdocs.org/sdr/REXA2026082601646.md): Latch · cracked · Jun 19, 2026 · N926XJ · Cndair CL6002D24 · Engine Thrust Reverser
  > WEAR AND CRACK ON COAMING LATCH AT RH UPPER AND LOWER TRANSCOWL. WAS REPAER PER REO 670-54-21-1028 REV. NC. AND CRJ 900 SRM 51-42-10-001-001-A01
- [SDR REXA2026082601747](https://openairdocs.org/sdr/REXA2026082601747.md): Support Angle · cracked · Jun 18, 2026 · N926XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK AT FWD SUPPORT ANGLES (2EA) OF UPPER ACUMULATOR AT NOSE HYDRAULICS COMPARTMENT INTERNAL STRUCTURE (INSIDE ACCESS PANEL 121AL). FWD SUPPORT ANGLES (2EA) OF UPPER ACUMULATOR AT NOSE HYDRAULICS COMPARTMENT INTERNAL STRUCTURE (INSIDE ACCESS PANEL 121AL) WERE
- [SDR REXA2026082601746](https://openairdocs.org/sdr/REXA2026082601746.md): Support Angle · cracked · Jun 18, 2026 · N926XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK AT FWD SUPPORT ANGLES (2EA) OF UPPER ACUMULATOR AT NOSE HYDRAULICS COMPARTMENT INTERNAL STRUCTURE (INSIDE ACCESS PANEL 121AL). FWD SUPPORT ANGLES (2EA) OF UPPER ACUMULATOR AT NOSE HYDRAULICS COMPARTMENT INTERNAL STRUCTURE (INSIDE ACCESS PANEL 121AL) WERE
- [SDR REXA2026082601745](https://openairdocs.org/sdr/REXA2026082601745.md): Floor Support · cracked · Jun 18, 2026 · N926XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK ON FLOOR BEAM RBL 12.0 BTW FS 221.73 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE (FLIGHT COMPARTMENT FLOOR STRUCTURE BELOW WL79.50). FLOOR BEAM RBL 12.0 BTW FS 221.73 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE (FLIGHT COMPARTMENT FLOOR STRUCTUR
- [SDR REXA2026082601732](https://openairdocs.org/sdr/REXA2026082601732.md): Receptacle · cracked · Jun 18, 2026 · N926XJ · Cndair CL6002D24 · Fuselage Main, Structure
  > CRACK IN BOX AT A/C EXTERNAL POWER RECEPTACLE SURROUND STRUCTURE BOX AT A/C EXTERNAL POWER RECEPTACLE WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01,CRJ900 SRM 51-42-21-001-001-A01 AND CRJ900 SRM 51-42-10-001-001-A01
- [SDR REXA2026082601731](https://openairdocs.org/sdr/REXA2026082601731.md): Protector · cracked · Jun 18, 2026 · N926XJ · Cndair CL6002D24 · Cargo/Baggage Doors
  > IN REF NRC 0083 CRACK OF 0.500 IN LENGTH WAS FOUND ON COVER HARNESS ON FWD COUNTERBALANCE INNER ARM AT FWD BAGGAGE BAY DOOR TRAY COVER HARNESS ON FWD COUNTERBALANCE INNER ARM AT FWD BAGGAGE BAY DOOR TRAY WAS REPLACED PER CRJ900 SRM 51-41-02-001-001-A01
- [SDR REXA2026082601728](https://openairdocs.org/sdr/REXA2026082601728.md): Stringer · corroded · Jun 18, 2026 · N926XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STGR=21R BTW FS=364 TO FS=379 AT FWD E/E COMPARTMENT. CORROSION ON STGR=21R BTW FS=364 TO FS=379 AT FWD E/E COMPARTMENT WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-00-00-101-001-A01 AND WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 AND CRJ90
- [SDR REXA2026082601727](https://openairdocs.org/sdr/REXA2026082601727.md): Bracket · corroded · Jun 18, 2026 · N926XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON BLOCK CLAMP SUPPORT BTW FS=295 TO 310, STGR=25R AT E/E COMPARTMENT. CORROSION ON BLOCK CLAMP SUPPORT BTW FS=295 TO 310, STGR=25R AT E/E COMPARTMENT WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 51-10-06-001-001-A01 AND WAS REPLACED PER CRJ900 SRM 51-
- [SDR REXA2026082601726](https://openairdocs.org/sdr/REXA2026082601726.md): Stringer · corroded · Jun 18, 2026 · N926XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STGR=26R FS=295 TO FS=310, STGRV25R FS=319 TO FS=333, AT FWD E/E COMPARTMENT. STGR=26R FS=295 TO FS=310, STGR=25R FS=319 TO FS=333, AT FWD E/E COMPARTMENT WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 51-10-06-001-001-A01 AND WERE REPLACE PER CRJ90
- [SDR REXA2026082601725](https://openairdocs.org/sdr/REXA2026082601725.md): Stringer · corroded · Jun 18, 2026 · N926XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STGR=26R FS=295 TO FS=310, STGRV25R FS=319 TO FS=333, AT FWD E/E COMPARTMENT. STGR=26R FS=295 TO FS=310, STGR=25R FS=319 TO FS=333, AT FWD E/E COMPARTMENT WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 51-10-06-001-001-A01 AND WERE REPLACE PER CRJ90
- [SDR REXA2026082601693](https://openairdocs.org/sdr/REXA2026082601693.md): Floor Support · corroded · Jun 18, 2026 · N926XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON LONGITUDINAL BEAMS (3E/A) FROM FS1000 TO FS1069 ON LBL27, LBL09 AND RBL09 AT AFT BAGGAGE COMPARTMENT CORROSION ON LONGITUDINAL BEAMS (3E/A) FROM FS1000 TO FS1069 ON LBL27, LBL09 AND RBL09 AT AFT BAGGAGE COMPARTMENT WERE EVALUATED OUT OF LIMITS PER
- [SDR REXA2026082601692](https://openairdocs.org/sdr/REXA2026082601692.md): Floor Support · corroded · Jun 18, 2026 · N926XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON LONGITUDINAL BEAMS (3E/A) FROM FS1000 TO FS1069 ON LBL27, LBL09 AND RBL09 AT AFT BAGGAGE COMPARTMENT CORROSION ON LONGITUDINAL BEAMS (3E/A) FROM FS1000 TO FS1069 ON LBL27, LBL09 AND RBL09 AT AFT BAGGAGE COMPARTMENT WERE EVALUATED OUT OF LIMITS PER
- [SDR REXA2026082601691](https://openairdocs.org/sdr/REXA2026082601691.md): Floor Support · corroded · Jun 18, 2026 · N926XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON LONGITUDINAL BEAMS (3E/A) FROM FS1000 TO FS1069 ON LBL27, LBL09 AND RBL09 AT AFT BAGGAGE COMPARTMENT CORROSION ON LONGITUDINAL BEAMS (3E/A) FROM FS1000 TO FS1069 ON LBL27, LBL09 AND RBL09 AT AFT BAGGAGE COMPARTMENT WERE EVALUATED OUT OF LIMITS PER
- [SDR REXA2026082601690](https://openairdocs.org/sdr/REXA2026082601690.md): Stringer · corroded · Jun 18, 2026 · N926XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STGR=20R, FS=295 TO FS=319, FS=349 TO FS=370 AND FS=445 AT FWD E/E CORROSION ON STGR=20R, FS=295 TO FS=319, FS=349 TO FS=370 AND FS=445 AT FWD E/E WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 51-10-06-001-001-A01, THEREFORE STRINGER 20R BTW FS280 T
- [SDR REXA2026082601689](https://openairdocs.org/sdr/REXA2026082601689.md): Stringer · corroded · Jun 18, 2026 · N926XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STGR=20R, FS=295 TO FS=319, FS=349 TO FS=370 AND FS=445 AT FWD E/E CORROSION ON STGR=20R, FS=295 TO FS=319, FS=349 TO FS=370 AND FS=445 AT FWD E/E WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 51-10-06-001-001-A01, THEREFORE STRINGER 20R BTW FS280 T
- [SDR REXA2026082601688](https://openairdocs.org/sdr/REXA2026082601688.md): Stringer · corroded · Jun 18, 2026 · N926XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STRINGER 19R BWT FS597 TO FS613 AT FWD BAGGAGE COMPARTMENT. CORROSION ON STRINGER 19R BWT FS597 TO FS613 AT FWD BAGGAGE COMPARTMENT WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 51-10-06-001-001-A01 AND WAS REPAIRED PER CRJ900 SRM 53-00-03-201-001-A
- [SDR REXA2026082601683](https://openairdocs.org/sdr/REXA2026082601683.md): Fitting · corroded · Jun 18, 2026 · N926XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION FLOOR FITTING IN AFT ACCESS 205 OUT SIDE (1EA) ON GALLEY 2. SUMMARY OF NRC 00244: FLOOR FITTING IN AFT ACCESS 205 OUT SIDE (1EA) ON GALLEY 2 WAS REPLACED PER SAFRAN CMM 25-32-84 REV 9 DATE JUN 06/24
- [SDR REXA2026082601674](https://openairdocs.org/sdr/REXA2026082601674.md): Seat Track · corroded · Jun 18, 2026 · N926XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > "CORROSION & WEAR ON FLOOR SEAT TRACK BTW FS927.00 TO BS 977 AND LBL 27 FLOOR SEAT TRACK BTW FS927.00 TO FS977.00 AND LBL 27' WAS REPLACED PER CRJ-900 AMM 53-00-49."
- [SDR REXA2026082601673](https://openairdocs.org/sdr/REXA2026082601673.md): Seat Track · corroded · Jun 18, 2026 · N926XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION & WEAR ON FLOOR SEAT TRACKS (3 EAS), BTW FS847.00 TO FS977.00AND RBL 9''. FLOOR SEAT TRACKS (3 EAS), BTW FS847.00 TO FS977.00 AND RBL 9'' WERE REPLACED PER CRJ-900 AMM 53-00-49
- [SDR REXA2026082601672](https://openairdocs.org/sdr/REXA2026082601672.md): Seat Track · corroded · Jun 18, 2026 · N926XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION & WEAR ON FLOOR SEAT TRACKS (3 EAS), BTW FS847.00 TO FS977.00AND LBL 9'' FLOOR SEAT TRACKS (3 EAS), BTW FS847.00 TO FS977.00AND LBL 9'' WERE REPLACED PER CRJ-900 AMM 53-00-49.
- [SDR REXA2026082601748](https://openairdocs.org/sdr/REXA2026082601748.md): Stringer · corroded · Jun 17, 2026 · N926XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STGR=19R, FS=295 TO FS=319 A5 FWD E/E CORROSION ON STGR=19R, FS=295 TO FS=319 A5 FWD E/E WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 51-10-06-001-001-A01 AND WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 AND CRJ900 SRM 51-42-21-001-001-A01
- [SDR REXA2026082601738](https://openairdocs.org/sdr/REXA2026082601738.md): Diaphragm · cracked · Jun 17, 2026 · N926XJ · Cndair CL6002D24 · Aerodynamic Fairings
  > CRACK IN LH/RH FAIRING SUPPORT DIAPHRAGM IN STA. FS= 797 TO FS= 807 AND 35LBL & 35RBL AT MLG WHEEL WELL. LH/RH FAIRING SUPPORT DIAPHRAGM IN STA. FS= 797 TO FS= 807 AND 35LBL & 35RBL AT MLG WHEEL WELL WERE REPLACED PER CRJ900 SRM 51-41-02-001-001-A01
- [SDR REXA2026082601737](https://openairdocs.org/sdr/REXA2026082601737.md): Diaphragm · cracked · Jun 17, 2026 · N926XJ · Cndair CL6002D24 · Aerodynamic Fairings
  > CRACK IN LH/RH FAIRING SUPPORT DIAPHRAGM IN STA. FS= 797 TO FS= 807 AND 35LBL & 35RBL AT MLG WHEEL WELL. LH/RH FAIRING SUPPORT DIAPHRAGM IN STA. FS= 797 TO FS= 807 AND 35LBL & 35RBL AT MLG WHEEL WELL WERE REPLACED PER CRJ900 SRM 51-41-02-001-001-A01
- [SDR REXA2026082601715](https://openairdocs.org/sdr/REXA2026082601715.md): Seat Track · corroded · Jun 17, 2026 · N926XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION & WEAR ON FLOOR SEAT RAILS, BTW FS349 TO FS477.40 AND LBL 9''. CORROSION & WEAR ON FLOOR SEAT RAILS, BTW FS349 TO FS477.40 AND LBL 9'' WAS EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-21-49-101-001-A01, TEHEREFORE WAS REPLACED PER CRJ-900 AMM 53-00-4
- [SDR REXA2026082601681](https://openairdocs.org/sdr/REXA2026082601681.md): Seat Track · corroded · Jun 17, 2026 · N926XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION & WEAR ON SIDE SEAT TRACK BTW FS669.40 TO FS977.00 AND STGR 15R SIDE SEAT TRACK BTW FS669.40 TO FS977.00 AND STGR 15R WERE REPLACED PER AMM 53-00-49.
- [SDR REXA2026082601679](https://openairdocs.org/sdr/REXA2026082601679.md): Seat Track · corroded · Jun 17, 2026 · N926XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION & WEAR ON SIDE SEAT TRACK BTW FS669.40 TO FS977.00 AND STGR 15R SIDE SEAT TRACK BTW FS669.40 TO FS977.00 AND STGR 15R WERE REPLACED PER AMM 53-00-49.
- [SDR REXA2026082601678](https://openairdocs.org/sdr/REXA2026082601678.md): Seat Track · corroded · Jun 17, 2026 · N926XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION & WEAR ON SIDE SEAT TRACK BTW FS669.40 TO FS977.00 AND STGR 15R SIDE SEAT TRACK BTW FS669.40 TO FS977.00 AND STGR 15R WERE REPLACED PER AMM 53-00-49.
- [SDR REXA2026082601677](https://openairdocs.org/sdr/REXA2026082601677.md): Seat Track · corroded · Jun 17, 2026 · N926XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION & WEAR ON SIDE SEAT TRACK BTW FS669.40 TO FS977.00 AND STGR 15R SIDE SEAT TRACK BTW FS669.40 TO FS977.00 AND STGR 15R WERE REPLACED PER AMM 53-00-49.
- [SDR REXA2026082601676](https://openairdocs.org/sdr/REXA2026082601676.md): Seat Track · corroded · Jun 17, 2026 · N926XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION & WEAR ON SIDE SEAT TRACK BTW FS669.40 TO FS977.00 AND STGR 15R SIDE SEAT TRACK BTW FS669.40 TO FS977.00 AND STGR 15R WERE REPLACED PER AMM 53-00-49.
- [SDR REXA2026082601667](https://openairdocs.org/sdr/REXA2026082601667.md): Strap · corroded · Jun 17, 2026 · N926XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON STRIPS OF FAIRINGS 192BB, 193AB & 196DR ALSO LOOSE FASTENERS ON STRIP OF FAIRINGS ACCESS 196DR. STRIPS (2EAS) OF FAIRING 193AB WERE REPLACED PER CRJ-900 SRM 51-42-10-001-001-A01, STRAP OF ACCESS PANEL 196DR WERE REPLACED AND FASTENERS WERE INSTALL
- [SDR REXA2026082601666](https://openairdocs.org/sdr/REXA2026082601666.md): Strap · corroded · Jun 17, 2026 · N926XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON STRIPS OF FAIRINGS 192BB, 193AB & 196DR ALSO LOOSE FASTENERS ON STRIP OF FAIRINGS ACCESS 196DR. STRIPS (2EAS) OF FAIRING 193AB WERE REPLACED PER CRJ-900 SRM 51-42-10-001-001-A01, STRAP OF ACCESS PANEL 196DR WERE REPLACED AND FASTENERS WERE INSTALL
- [SDR REXA2026082601665](https://openairdocs.org/sdr/REXA2026082601665.md): Strap · corroded · Jun 17, 2026 · N926XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON STRIPS OF FAIRINGS 192BB, 193AB & 196DR ALSO LOOSE FASTENERS ON STRIP OF FAIRINGS ACCESS 196DR. STRIPS (2EAS) OF FAIRING 193AB WERE REPLACED PER CRJ-900 SRM 51-42-10-001-001-A01, STRAP OF ACCESS PANEL 196DR WERE REPLACED AND FASTENERS WERE INSTALL

Next page: https://openairdocs.org/aircraft/N926XJ/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 = 'N926XJ' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N926XJ/reports

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