# Service difficulty reports: N901XJ

A list on [N901XJ](https://openairdocs.org/aircraft/N901XJ.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 · 190 reports

- [SDR REXA2025041800463](https://openairdocs.org/sdr/REXA2025041800463.md): Floor Support · corroded · Apr 13, 2025 · N901XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON ANGLES FLOOR SUPPORTS BTW FS 310.00 TO 349.00 AND LBL40 AT PASSENGER CABIN FLOOR STRUCTURE CORROSION ON ANGLES FLOOR SUPPORTS BTW FS 310.00 TO 349.00 AND LBL40 AT PASSENGER CABIN FLOOR STRUCTURE WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01 AND
- [SDR REXA2025041800460](https://openairdocs.org/sdr/REXA2025041800460.md): Bracket · corroded · Apr 4, 2025 · N901XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON BRACKET SUPPORT OF ELECTRICAL HARNESS AT RH AND LH MLG ON INBOARD SIDE OF SIDE STAY ASSY BRACKET SUPPORT OF ELECTRICAL HARNESS AT RH MLG ON INBOARD SIDE OF SIDE STAY ASSY WAS REPLACED PER EA CRJ957-18838 REV.IR AND CRJ900 SRM 51-42-06-001-001-A01
- [SDR REXA2025041800459](https://openairdocs.org/sdr/REXA2025041800459.md): Fitting · corroded · Mar 27, 2025 · N901XJ · Cndair CL6002D24 · Fuselage Main, Structure
  > CORROSION ON FITTINGS OVER FS 310 AND RBL43 AND OVER FS 349.00 AND LBL43 AT PASSENGER CABIN FLOOR STRUCTURE. CORROSION ON FITTINGS OVER FS 310 AND RBL43 AND OVER FS 349.00 AND LBL43 AT PASSENGER CABIN FLOOR STRUCTURE WERE EVALUATED OUT LIMITS PER CRJ 900 SRM
- [SDR REXA2025041800458](https://openairdocs.org/sdr/REXA2025041800458.md): Beam · cracked · Mar 27, 2025 · N901XJ · Cndair CL6002D24 · Fuselage Main, Structure
  > WEAR BEAM OF AFT BAGGAGE-BAY CARGO DOOR STRUCTURE (INTERFERENCE WITH AFT BALANCE SPRING CABLE) BEAM OF AFT BAGGAGE-BAY CARGO DOOR STRUCTURE (INTERFERENCE WITH AFT BALANCE SPRING CABLE) WAS REPAIRED PER REO 690-53-61-1548 REV - -
- [SDR REXA2025041800453](https://openairdocs.org/sdr/REXA2025041800453.md): Seat Track · corroded · Mar 15, 2025 · N901XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > INITIAL INSPECTION, CORROSION ON SEVERAL AREAS OF PASSENGER SEAT RAIL WAS FOUND BTW FS 364.00 TO 394.00 AND LBL 9. FLOOR SEAT RAIL BTW FS364.00 TO FS485.00 AND LBL9 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-49-101-001-A01 AND WAS REPLACED PER CRJ900 AMM
- [SDR REXA2025041800452](https://openairdocs.org/sdr/REXA2025041800452.md): Seat Track · corroded · Mar 15, 2025 · N901XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > INITIAL INSPECTION: CORROSION ON SUPPORTS OF MONUMENTS BTW FS 295.00/LBL37 AND BTW FS 377.00/LBL 37 AT PASSENGER CABIN FLOOR STRUCTURE. CORROSION ON SUPPORT OF MONUMENTS BTW FS377.00 LBL37 AT PASSENGER CABIN FLOOR STRUCTURE WAS EVALUATED OUT OF LIMITS PER CRJ9
- [SDR REXA2025041800451](https://openairdocs.org/sdr/REXA2025041800451.md): Floorbeam · corroded · Mar 15, 2025 · N901XJ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > IN REF TO NRC 0283: AFTER FLOOR SUPPORT ANGLE REMOVAL, CORROSION ON RH CROSSBEAM FS280 BTW RBL0 AND RBL12 WAS FOUND. CORROSION ON RH CROSSBEAM FS280.00 BTW BL0 AND RBL 12 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-00-00-101-001-A01 AND WAS REPLACED PER CRJ-
- [SDR REXA2025041800454](https://openairdocs.org/sdr/REXA2025041800454.md): Retainer · cracked · Mar 11, 2025 · N901XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > CRACK ON BOTTOM RETAINER SEAL AT PASSENGER DOOR STRUCTURE. BOTTOM RETAINER SEAL AT PASSENGER DOOR STRUCTURE WAS REPLACED PERV CRJ-900 SRM 51-42-10-001-001-A01
- [SDR REXA2024022200204](https://openairdocs.org/sdr/REXA2024022200204.md): Connector · failed · Feb 11, 2024 · N901XJ · Cndair CL6002D24 · Light System Wiring
  > GALLEY CEILING EMERGENCY LIGHTS INOP. REPLACED CONNECTORS FOR WIRES DS289J1, DS289P2, DS285J1, AND DS285P2 IAW ESPM 20-16-00, OPS CHECK GOOD.
- [SDR REXA2022082800701](https://openairdocs.org/sdr/REXA2022082800701.md): Fitting · deformed · Jun 27, 2023 · N901XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > WHILE INCORPORATING SB 670BA-53-044 REV G, WE HAVE DISCOVERED @ FS202 BULKHEAD RHS STR12A LOCATION CAN ONLY PICK UP 2 FASTENERS IN LIEU OF THE CALLED OUT 3 COMMON TO THE BULKHEAD, CAP ANGLE DOUBLER AND STR 12A FITTINGS. ALSO ON RHS ONE FASTENER ABOVE STR12A FI
- [SDR REXA2022071000454](https://openairdocs.org/sdr/REXA2022071000454.md): Doubler · deformed · Jun 25, 2023 · N901XJ · Cndair CL6002D24 · Fuselage Main, Structure
  > DURING INCORPORATION OF SB 670-53-044 REV G, OVERSIZE FASTENERS FOUND @ STR 14L ON FS 202 BULKHEAD. (6 TOTAL FASTENERS) REPAIRED IAW MHIRJ REO # 690-53-11-1570 REV A DATED 2023-06-30.
- [SDR REXA2022072001608](https://openairdocs.org/sdr/REXA2022072001608.md): Battery · discharged · Jul 13, 2022 · N901XJ · Cndair CL6002D24 · Emergency Lighting
  > EMERG LIGHT BATTERY PACK #4 IS LOW/INOP. REMOVED AND REPLACED #4 BATT PACK OLD S/N 130287, OLD P/N AD-2013-1A AND NEW S/N 14528, NEW P/N 2013-1ASMI IAW MHI AMM 33-51-17. OPS CHK GOOD.
- [SDR REXA2021092300749](https://openairdocs.org/sdr/REXA2021092300749.md): Yoke · chafed · Sep 19, 2021 · N901XJ · Cndair CL6002D24 · Engine Mount Section
  > " LH ENG FWD ENG MOUNT YOKE CHAFED FROM UPPER AND LOWER HINGE LINE FAIRINGS. " "REPAIRED DAMAGE ON LH ENG FWD ENG MOUNT YOKE IAW REO 690-71-21-027 REV-- DATE 2021-08-27.
- [SDR REXA2021092300762](https://openairdocs.org/sdr/REXA2021092300762.md): Lug · elongated · Sep 17, 2021 · N901XJ · Cndair CL6002D24 · Aileron Control System
  > "WHILE REMOVING RH AILERON WING SIDE BUSHINGS FOUND 4EA CENTER LAG BORES TO BE OVERSIZED MEASURING 0.8900"". " " REPAIRED DAMAGE IAW MHIRJ REO 690-57-51-232 REV -- DATED 2021-09-09 WVAC EMP STAMP # 780 MTC.
- [SDR REXA2021092300761](https://openairdocs.org/sdr/REXA2021092300761.md): Fitting · gouged · Sep 17, 2021 · N901XJ · Cndair CL6002D24 · Aileron Control System
  > "LH AILERON CENTER FITTIN HAS DAMAGE HOLES. " "REQUIRED AILERON IAW CRJ 900 REO 690-57-61-215 REV -- DATED 2021-09-12 WVAC EMP STAMP # 711 MTC. "
- [SDR REXA2021092300759](https://openairdocs.org/sdr/REXA2021092300759.md): Fitting · gouged · Sep 17, 2021 · N901XJ · Cndair CL6002D24 · Aileron Control System
  > "LH AILERON CENTER OB HINGE NODE GOUGED IB OF PCU ATTACH NODE. " "REQUIRED AILERON IAW REO 690-57-61215 REV--DATED 9/12/2021 WVAC EMP STAMP # 711 MTC. "
- [SDR REXA2021092300746](https://openairdocs.org/sdr/REXA2021092300746.md): Striker · corroded · Sep 17, 2021 · N901XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "GALLEY SVC DOOR LOWER SEAL STRIKER HAS LIGHT CORROSION AROUND FASTENER HOLES. " "REMOVED CORROSION AROUND FASTENER HOLES FOUND TO BE OUT LIMITS. REMOVED, DRILLED, LOCATED SEAL STRIKER INSTALLED SERVICEABL
- [SDR REXA2021092300744](https://openairdocs.org/sdr/REXA2021092300744.md): Panel · chafed · Sep 17, 2021 · N901XJ · Cndair CL6002D24 · Wing Structure
  > "RH AILERON LOWER L/E ON O/B END HAS HEAVY CHAFING. " "REPARIED & CW EO DRAWING # 681R13400 OF EO 601R13444 FOR RH LOWER AILERON L/E ON OB END CHAFE. WVAC EMP STAMP # 796 MTC. "
- [SDR REXA2021092300760](https://openairdocs.org/sdr/REXA2021092300760.md): Fitting · gouged · Sep 14, 2021 · N901XJ · Cndair CL6002D24 · Aileron Control System
  > "RH AILERON CENTER IB HINGE NODE GOUGED BOTTOM EDGE APROX.5"" X VARIOUS DEPTHS. " "BLENDED DAMAGE AND REPAIR DAMAGE CRJ 900 SRM 51-12-00-001-001-A01. MHIRJ REO 690-57-61-214 APP END F
- [SDR REXA2021092300754](https://openairdocs.org/sdr/REXA2021092300754.md): Rail · corroded · Sep 13, 2021 · N901XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "R/H SIDE SEAT RAIL FS 677-669 CORRODED. " "REMOVED AND INSTALLED FABRICATED SERVICEABLE RH SIDE SEAT RAIL AT FS 677-649 IAW CRJ 900 REO 670-53-00-343 REV N DATED 2019-07-16 AND CRJ 900 AMM 53-00-49-201-002-A01 AND 53-00-49-400-801(A07) WVAC
- [SDR REXA2021092300757](https://openairdocs.org/sdr/REXA2021092300757.md): Seat Track · corroded · Sep 8, 2021 · N901XJ · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > "RH FLOOR SEAT TRACK FS 847-1000 CORRODED. " " REMOVED & REPLACED RH FLOOR SEAT TRACK FROM FS 847-1000 FOUND NO CORROSION NOTED ON RBL9 SEAT TRACK FS 847.00-FS 901.00 WVAC EMP STAMP # 796 MTC. "
- [SDR REXA2021092300756](https://openairdocs.org/sdr/REXA2021092300756.md): Rail · corroded · Sep 4, 2021 · N901XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "R/H SIDE SEAT RAIL FS 565 TO 661 CORRODED. " "REMOVED FABRICATED, PAINTED AND REINSTALLED SEAT TRACK ON RH SIDE AT FS 565 TO 661. R/R SEVERAL SCREWS AS REQUIRE PER CRJ 700 AMM 53-00-49-000/400-801-A07. WVAC EMP ST
- [SDR REXA2021092300755](https://openairdocs.org/sdr/REXA2021092300755.md): Rail · corroded · Sep 4, 2021 · N901XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "R.H SIDE SEAT RAIL FS 661.00+16 TO 669 CORRODED. " "REMOVED, FABRICATED & INSTALLED RH SIDE SEAT RAIL AT FS 661.00 TO 669. WVAC EMP STAMP # 796 MTC. "
- [SDR REXA2021090200753](https://openairdocs.org/sdr/REXA2021090200753.md): Rail · corroded · Sep 2, 2021 · N901XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "R/H SIDE SEAT RAIL FS 847 TO 785 CORRODED. " "REPLACED R/H SIDE SEAT RAIL AT FS 785 TO 847 IAW CRJ 900 AMM 53-00-49-400-801-A01. WVAC EMP STAMP # 761 MTC. "
- [SDR REXA2021092300751](https://openairdocs.org/sdr/REXA2021092300751.md): Attach Fitting · corroded · Sep 2, 2021 · N901XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "L/H AND FITTING FOR FLOOR SUPPORT CROSSBEAM AT F.S. 310 IS CORRODED. " "REMOVED AND REPLACED FLOOR BEAM ATTACH FITTING LOCATED AT FS 310 LH SIDE IAW CRJ 900 SRM 51-40-11-001-001-A01 AND 51-42-21-001-001-A01 WVAC EMP # 6449
- [SDR REXA2021092300750](https://openairdocs.org/sdr/REXA2021092300750.md): Intercostal · corroded · Sep 2, 2021 · N901XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "INTERCOSTALS (4EA) FROM F.S. 310.00 TO F.S. 364.00 AT STR 20R ARE CORRODED ALONG LOWER EDGE. " "REPLACED INTERCOSTAL AT FS 310-319, STGR 20R IAW CRJ 900 SRM 51-42-06- 001-001-A01 AND 51-42-21-001-001-A01. REPAIRED INT
- [SDR REXA2021092300745](https://openairdocs.org/sdr/REXA2021092300745.md): Angle · corroded · Sep 2, 2021 · N901XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "FS 280 FWD ""J"" ANGLE IS CORRODED AROUND NUT PLATES. " "FOUND FS 280 J ANGLE TO BE OUT OF LIMITS LOCATED DRILLED, & INSTALLED FS 280 J ANGLE WVAC EMP STAMP # 796 MTC "
- [SDR REXA2021092300736](https://openairdocs.org/sdr/REXA2021092300736.md): Panel · chafed · Sep 2, 2021 · N901XJ · Cndair CL6002D24 · Wing Structure
  > "PANEL 699AB CHAFED " "BLENDED CHAFE ON PANEL 699AB FOUND TO BE OUT OF LIMITS. LOCATED, DRILLED, COUNTERS IN SERVICEABLE PANEL WVAC EMP STAMP # 796 MTC "
- [SDR REXA2021092300758](https://openairdocs.org/sdr/REXA2021092300758.md): Seat Track · corroded · Sep 1, 2021 · N901XJ · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > "L/H FLOOR SEAT TRACK FS 995 TO 1002 CORRODED. " "REPLACED LH FLOOR SEAT TRACK AT FS 995 TO 1002 IAW CRJ 900 AMM 53-00-49-000/400-802-A02. WVAC EMP # 6449. "
- [SDR REXA2021092300752](https://openairdocs.org/sdr/REXA2021092300752.md): Rail · corroded · Sep 1, 2021 · N901XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "L/H SIDE SEAT TRACK CORRODED BETWEEN FWD/AFT EMERG EXITS, FS 744-761 " "REPLACED L/H SIDE TRACK FS 744-761 BETWEEN FWD/AFT EMERG EXITS, IAW CRJ 900 AMM 53-00-49-400-801-A07 NEW RAIL P/N:SH690-36285-1 WVAC EMP STAMP # 781 MTC
- [SDR REXA2021092300748](https://openairdocs.org/sdr/REXA2021092300748.md): Drag Angle · cracked · Sep 1, 2021 · N901XJ · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > "L/H VERT. STAB AFT DRAG ANGLE TO TAIL CONE APPEARS TO BE CRACKED. " "REMOVED AND INSTALLED NEW AFT DRAG ANGLE (LH SIDE) VER. STAB TO TAIL- CONE IAW CRJ-900 SRM 51-42-13-001-001-0A01 AND SRM 51-42-21-001-001- A01 WVAC EMP STAMP # 796 MTC
- [SDR REXA2021092300747](https://openairdocs.org/sdr/REXA2021092300747.md): Drag Angle · cracked · Sep 1, 2021 · N901XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "R/H VERT STAB AFT DRAG ANGLE TO TAILCONE APPEARS TO BE CRACKED. " "REMOVED AND REPLACED RH VERT. STAB. AFT DRAG ANGLE IAW A/C CRJ 900 SRM 51-42-13-001-001-A01 AND 51-42-21-001-001-A01 WVAC EMP STAMP # 796 MTC "
- [SDR REXA2021092300743](https://openairdocs.org/sdr/REXA2021092300743.md): Bracket · corroded · Sep 1, 2021 · N901XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > "PAX DOOR FWD WEB CORRODED " "REMOVED, DRILLED, LOCATED, & INSTALLED NEW FWD WEB, RETAINING BRACKET, STIFFNER, & STIFFNER TEE ON PAX DOOR FWD WEB WVAC EMP STAMP # 796 MTC INSTALLED PAX DOOR FWD WEB IAW CRJ 900 SRM 51-42-06-001-001-A01 WVAC EMP STAMP # 7
- [SDR REXA2021092300742](https://openairdocs.org/sdr/REXA2021092300742.md): Panel · corroded · Sep 1, 2021 · N901XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > "PAX DOOR FWD WEB CORRODED " "REMOVED, DRILLED, LOCATED, & INSTALLED NEW FWD WEB, RETAINING BRACKET, STIFFNER, & STIFFNER TEE ON PAX DOOR FWD WEB WVAC EMP STAMP # 796 MTC INSTALLED PAX DOOR FWD WEB IAW CRJ 900 SRM 51-42-06-001-001-A01 WVAC EMP STAMP # 7
- [SDR REXA2021092300741](https://openairdocs.org/sdr/REXA2021092300741.md): Stiffener · corroded · Sep 1, 2021 · N901XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > "PAX DOOR FWD WEB CORRODED " "REMOVED, DRILLED, LOCATED, & INSTALLED NEW FWD WEB, RETAINING BRACKET, STIFFNER, & STIFFNER TEE ON PAX DOOR FWD WEB WVAC EMP STAMP # 796 MTC INSTALLED PAX DOOR FWD WEB IAW CRJ 900 SRM 51-42-06-001-001-A01 WVAC EMP STAMP # 7
- [SDR REXA2021092300740](https://openairdocs.org/sdr/REXA2021092300740.md): Stiffener · corroded · Sep 1, 2021 · N901XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > "PAX DOOR FWD WEB CORRODED " "REMOVED, DRILLED, LOCATED, & INSTALLED NEW FWD WEB, RETAINING BRACKET, STIFFNER, & STIFFNER TEE ON PAX DOOR FWD WEB WVAC EMP STAMP # 796 MTC INSTALLED PAX DOOR FWD WEB IAW CRJ 900 SRM 51-42-06-001-001-A01 WVAC EMP STAMP # 7
- [SDR REXA2021092300737](https://openairdocs.org/sdr/REXA2021092300737.md): Former · corroded · Sep 1, 2021 · N901XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > "PAX DOOR FWD FORMER AT FS 311.75 CORRODED " "LOCATED & DRILLED FWD FORMER P/N 601R3108031-5 IAW CRJ 900 SRM 51-40-11-001-001-A01. INSTALLED FWD FORMER IAW CRJ 900 SRM 51- 42-06-001-001-A01 AND 51-42-21-001-001-A01 REV 38 7-25-20 WVAC EMP # 7006
- [SDR REXA2021092300739](https://openairdocs.org/sdr/REXA2021092300739.md): Skin · corroded · Aug 25, 2021 · N901XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > "PAX DOOR INNER SKIN CORRODED ON I/B AND O/B SURFACE IN SEVERAL AREAS " "REPLACED SKIN IAW CRJ 900 SRM 51-40-11-001-001-A01 REV 38 7-25-20. WVAC EMP STAMP # 711 MTC "
- [SDR REXA2021092300738](https://openairdocs.org/sdr/REXA2021092300738.md): Intercostal · corroded · Aug 25, 2021 · N901XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > "PAX DOOR DD6 INTERCOSTAL CORRODED. " "LOCATED & DRILLED DD INTERCOSTEL P/N 601R318057 IAW CRJ 900 SRM 51-40-11-001-001-A01 INSTALLED INTERCOSTEL IAW CRJ 900 SRM 51-42-06- 001-001-A01, 51-42-21-001-001-A01 REV 38 7-25-20 WVAC EMP
- [SDR REXA2020070600577](https://openairdocs.org/sdr/REXA2020070600577.md): Light · inoperative · May 23, 2020 · N901XJ · Cndair CL6002D24 · Emergency Lighting
  > RT EMERGENCY EXTERIOR BULB INOP. REMOVED AND REPLACED RT EMERGENCY EXTERIOR BULB IAW AMM 33-51-15 OPS CHECK GOOD; PN ON/OFF: 8GH002473-08; SN ON/OFF: N/A.
- [SDR REXA2018122181311](https://openairdocs.org/sdr/REXA2018122181311.md): Light · inoperative · Dec 18, 2018 · N901XJ · Cndair CL6002D24 · Emergency Lighting
  > L/H AFT OVERWING WXIT LIGHT INOP REPAIRED L/H AFT OVERWING EXIT LIGHT GOOD IAW CRJ 900 AMM 33.51.15.710.801
- [SDR REXA2018122181310](https://openairdocs.org/sdr/REXA2018122181310.md): Stringer · corroded · Dec 18, 2018 · N901XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > AFTER REMOVAL OF STR22L SPLICE FOUND STR 22L CORRODED REPAIRED STR 22L FS 333-349 PER IAW CRJ 900 SRM 53.00.03/51.42.06 AND REMOVED AND REPLACED STR 22L SPLICE FS 333 PER IAW CRJ 900 SRM 51.42.21
- [SDR REXA2018122171303](https://openairdocs.org/sdr/REXA2018122171303.md): Frame · corroded · Dec 17, 2018 · N901XJ · Cndair CL6002D24 · Fuselage Main, Frame
  > FS847.00+32.00, STGR26L TO STGR26R FRAME IS CORRODED. REPAIRED FRAME 847+32 IAW EA CRJ 953-08011 REV IR AAR SM-107
- [SDR REXA2018122161302](https://openairdocs.org/sdr/REXA2018122161302.md): Frame · corroded · Dec 16, 2018 · N901XJ · Cndair CL6002D24 · Fuselage Main, Frame
  > FRAME AT FS847+16 IS CORRODED FROM S26L TO S26R. REMOVED/REPLACED FRAME SECTION AND REINFORCEMENT ANGLE AT FS 847+16 IAW CRJ 900 SRM 51-42-06,51-42-21 LEAK CK OF DISTRIBUTION DUCTS GOOD IAW CRJ 900 AMM 21-23-00-79-801
- [SDR REXA2018122161301](https://openairdocs.org/sdr/REXA2018122161301.md): Skin · damaged · Dec 16, 2018 · N901XJ · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > ANTENNA DOUBLER FS629-FS646 STGR1L THRU STGR 1R HAS ELONGATED HOLES REPAIRED FUSELAGE SKIN WITH FREEZE PLUGS AND SKIN DOUBLE IAW EA CRJ953-07928
- [SDR REXA2018122111299](https://openairdocs.org/sdr/REXA2018122111299.md): Stringer Splice · corroded · Dec 11, 2018 · N901XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > SPLICE ON STGR 23R HAS CORROSION AT FS 333, IN THE FWD E & E BAY. REMOVED AND REPLACED STR 23R SPLICE FS 333 PER CRJ-900 SRM 51-42-06/51-42-21 OPS CHECK GOOD CRJ-900 AMM 34-53-00-710-801
- [SDR REXA201812211298](https://openairdocs.org/sdr/REXA201812211298.md): Stringer · corroded · Dec 11, 2018 · N901XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > LONGERON ON STGR 25R HAS CORROSION BETWEEN FRAMES 349 AND 333, IN THE FWD E & E BAY REMOVED CORRODED LONGERON AND REPLACED WITH NEW LONGERON IAW CRJ-900 SRM 51-42-06.
- [SDR REXA2018122101300](https://openairdocs.org/sdr/REXA2018122101300.md): Intercostal · corroded · Dec 10, 2018 · N901XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > INTERCOSTAL THAT SITS ON STGR 21L HAS CORROSION BETWEEN FRAMES 310 AND 333, IN THE FWD E & E BAY. REMOVED AND REPLACED INTERCOSTAL STGR 21L FS 310-333 PER CRJ-900 SRM 51-42-21
- [SDR REXA2018122191297](https://openairdocs.org/sdr/REXA2018122191297.md): Channel · corroded · Dec 9, 2018 · N901XJ · Cndair CL6002D24 · Fluid Service Doors
  > FWD LAV SERVICE DOOR 142BR ACCESS LOWER CHANNEL PAINT BUBBLED REMOVED/REPLACED IMPACT ANGLE IAW CRJ 900 SRM 51-42-06. REMOVED CORROSION IAW CRJ 900 SRM 51-21-06. APPLIED FINISH IAW CRJ 900 SRM 51-25-16
- [SDR REXA2018122181287](https://openairdocs.org/sdr/REXA2018122181287.md): Stringer · corroded · Dec 8, 2018 · N901XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STGR 26R HAS CORROSION BETWEEN FRAMES 349 AND 333, IN THE FWD E & E BAY REMOVED/REPLACED AFT SECTION OF STRINGER 26R IN FWD E AND E BAY IAW CRJ 900 SRM 51-42-06 AND SRM 51-42-21

Next page: https://openairdocs.org/aircraft/N901XJ/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 = 'N901XJ' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N901XJ/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.