# Service difficulty reports: N918XJ

A list on [N918XJ](https://openairdocs.org/aircraft/N918XJ.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 · 210 reports

- [SDR REXA2026032700248](https://openairdocs.org/sdr/REXA2026032700248.md): Hinge · corroded · Feb 11, 2026 · N918XJ · Cndair CL6002D24 · Accessory Compartment Doors
  > CORROSION WAS FOUND ON FITTINGS LH AND RH SIDE AT AFT NOSE LANDING GEAR DOOR AND ALSO ON FUSELAGE STRUCTURE (4EAS). DUE TO EXCESSIVE CORROSION PER CRJ 900 SRM 51-10-06-001-001-A01 ON FITTINGS (4EAS) LH AND RH SIDE AT AFT NOSE LANDING GEAR DOOR AND ALSO ON FUSE
- [SDR REXA2026032700247](https://openairdocs.org/sdr/REXA2026032700247.md): Fitting · corroded · Feb 11, 2026 · N918XJ · Cndair CL6002D24 · Landing Gear Doors
  > CORROSION WAS FOUND ON FITTINGS LH AND RH SIDE AT AFT NOSE LANDING GEAR DOOR AND ALSO ON FUSELAGE STRUCTURE (4EAS). DUE TO EXCESSIVE CORROSION PER CRJ 900 SRM 51-10-06-001-001-A01 ON FITTINGS (4EAS) LH AND RH SIDE AT AFT NOSE LANDING GEAR DOOR AND ALSO ON FUSE
- [SDR REXA2026032700246](https://openairdocs.org/sdr/REXA2026032700246.md): Fitting · corroded · Feb 11, 2026 · N918XJ · Cndair CL6002D24 · Landing Gear Doors
  > CORROSION WAS FOUND ON FITTINGS LH AND RH SIDE AT AFT NOSE LANDING GEAR DOOR AND ALSO ON FUSELAGE STRUCTURE (4EAS). DUE TO EXCESSIVE CORROSION PER CRJ 900 SRM 51-10-06-001-001-A01 ON FITTINGS (4EAS) LH AND RH SIDE AT AFT NOSE LANDING GEAR DOOR AND ALSO ON FUSE
- [SDR REXA2026032700273](https://openairdocs.org/sdr/REXA2026032700273.md): Hinge Bracket · corroded · Feb 10, 2026 · N918XJ · Cndair CL6002D24 · Trailing Edge Flaps
  > CORROSION ON FWD HINGE AT FLAP STEP PLATE WAS FOUND. CORROSION ON FWD HINGE AT FLAP STEP PLATE WAS FOUND WAS EVALUATED OUT OFF LIMITS PER CRJ 900 SRM 51-10-06-001-001-A01 AND FWD HINGE AT FLAP STEP WAS REPAIRED PER EA NO:CRJ953-21661 REV.IR
- [SDR REXA2026032700264](https://openairdocs.org/sdr/REXA2026032700264.md): Web · cracked · Feb 10, 2026 · N918XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK ON BIN SUPPORT MEMBRANE ON RBL34 AT FWD FACE OF MLG WHEEL WELL. BIN SUPPORT MEMBRANE ON RBL34 AT FWD FACE OF MLG WHEEL WELL WAS REPLACED PER CRJ900 SRM 51-41-02-001-001-A01
- [SDR REXA2026032700259](https://openairdocs.org/sdr/REXA2026032700259.md): Floor Support · cracked · Feb 10, 2026 · N918XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACKED ANGLES AT FLOOR SUPPORT STRUCTURE BTW FS 260.00 TO 280.00 AND RBL 12.00 AND LBL12.00. ANGLES AT FLOOR SUPPORT STRUCTURE BTW FS 260.00 TO 280.00 AND RBL 12.00 AND LBL12.00 WERE REPLACED PER CRJ 900 SRM 51-42-06-001-001-A01,SRM 51-42-10-001-001-A01 AND
- [SDR REXA2026032700258](https://openairdocs.org/sdr/REXA2026032700258.md): Floor Support · cracked · Feb 10, 2026 · N918XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACKED ANGLES AT FLOOR SUPPORT STRUCTURE BTW FS 260.00 TO 280.00 AND RBL 12.00 AND LBL12.00. ANGLES AT FLOOR SUPPORT STRUCTURE BTW FS 260.00 TO 280.00 AND RBL 12.00 AND LBL12.00 WERE REPLACED PER CRJ 900 SRM 51-42-06-001-001-A01,SRM 51-42-10-001-001-A01 AND
- [SDR REXA2026032700257](https://openairdocs.org/sdr/REXA2026032700257.md): Striker · corroded · Feb 10, 2026 · N918XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON STRIKER SILL AND ANGLE MOUNTING AT GALLEY SERVICE DOOR SURROUND STRUCTURE CORROSION ON STRIKER SILL AND ANGLE MOUNTING AT GALLEY SERVICE DOOR SURROUND STRUCTURE WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01, ANGLE MOUNTING WAS EVALUATED WHITIN
- [SDR REXA2026032700255](https://openairdocs.org/sdr/REXA2026032700255.md): Support · corroded · Feb 10, 2026 · N918XJ · Cndair CL6002D24 · Aerodynamic Fairings
  > CORROSION ON SETTLEMENT AREA OF BODY FAIRING ACCESS PANELS 195AB, 195BB, 196AR AND 195AL AT AFT BODY FAIRING SUPPORT STRUCTURE. CORROSION ON SETTLEMENT AREA OF BODY FAIRING ACCESS PANELS 195AB, 195BB, AND 195AL WAS REMOVED AND EVALUATED WITHIN LIMITS CRJ900 S
- [SDR REXA2026032700271](https://openairdocs.org/sdr/REXA2026032700271.md): Angle · cracked · Feb 9, 2026 · N918XJ · Cndair CL6002D24 · Vertical Stabilizer Miscellaneous Structure
  > CRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). CRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM
- [SDR REXA2026032700270](https://openairdocs.org/sdr/REXA2026032700270.md): Angle · cracked · Feb 9, 2026 · N918XJ · Cndair CL6002D24 · Vertical Stabilizer Miscellaneous Structure
  > CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD AND AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). CRACKS ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD AND AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5%
- [SDR REXA2026032700256](https://openairdocs.org/sdr/REXA2026032700256.md): Angle · corroded · Feb 9, 2026 · N918XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON FWD, AFT AND MID CAP ANGLE AT PASSENGER DOOR SURROUND STRUCTURE. CORROSION ON FWD, AFT WAS REMOVED AND EVALUATED WITHIN LIMITS CRJ 900 SRM 51-21-06-001-001-A01 AND CRJ-900 SRM 53-00-00-101-001-A01, AND MID CAP ANGLE AT PASSENGER DOOR SURROUND STR
- [SDR REXA2026032700254](https://openairdocs.org/sdr/REXA2026032700254.md): Cover · cracked · Feb 9, 2026 · N918XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > CRACKED HANDLE COVER AT PASSENGER DOOR. HANDLE COVER AT PASSENGER DOOR WAS REPLACED PER CRJ 900 SRM 51-42-06-001-001-A01
- [SDR REXA2026032700269](https://openairdocs.org/sdr/REXA2026032700269.md): Web · cracked · Feb 8, 2026 · N918XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACKED FLOOR WEB RIGHT SIDE AT_ ELECTRICAL BAY (BELOW ADG SUPPORT DOUBLER) FS193.00 CRACKED DOUBLER AT FLOOR WEB RIGHT SIDE AT_ ELECTRICAL BAY (BELOW ADG SUPPORT DOUBLER) FS193.00 WAS REPLACED PER CRJ-900 SRM 53-11-43-201-001-A01, SRM 51-42-06-001-001-A01
- [SDR REXA2026032700268](https://openairdocs.org/sdr/REXA2026032700268.md): Web · cracked · Feb 8, 2026 · N918XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACKED FLOOR WEB LEFT SIDE AT_ ELECTRICAL BAY (BELOW BRAKE ACCUMULATOR INDICATION SUPPORT DOUBLER) FS193.00. FLOOR WEB LEFT SIDE AT_ ELECTRICAL BAY (BELOW BRAKE ACCUMULATOR INDICATION SUPPORT DOUBLER) FS193.00 WAS REPAIRED PER CRJ 900 SRM 53-11-43-201-001-A0
- [SDR REXA2026032700267](https://openairdocs.org/sdr/REXA2026032700267.md): Skin · cracked · Feb 8, 2026 · N918XJ · Cndair CL6002D24 · Engine Thrust Reverser
  > TORN UPPER AND LOWER AFT SEAL AT RT UPPER AND LOWER THRUST REVERSE ALSO CRACK AFT SEAL PLATE AT RT LOWER THRUST REVERSE. CRACK AFT SEAL PLATE AT RT LOWER THRUST REVERSE WAS REPAIRED PER EA CRJ954-21516 REV IR AND UPPER AND LOWER AFT SEAL AT RT UPPER AND LOWER
- [SDR REXA2026032700263](https://openairdocs.org/sdr/REXA2026032700263.md): Support · cracked · Feb 8, 2026 · N918XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK AT CORNERS OF SUPPORT AT THE JB 6 MODULE AT FWD EQUIPMENT COMPARTMENT SUPPORT AT THE JB 6 MODULE AT FWD EQUIPMENT COMPARTMENT WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01
- [SDR REXA2026032700261](https://openairdocs.org/sdr/REXA2026032700261.md): Fitting · corroded · Feb 8, 2026 · N918XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON FITTING (10 EACH) BTW FS280/FS379 AND LBL42/RBL42 AT FLOOR STRUCTURE. CORROSION ON FITTING (10 EAÏ¿½S) BTW FS280/FS379 AND LBL42/RBL42 AT FLOOR STRUCTURE WAS CLEANED, REMOVED, EVALUATED WHITIN LIMITS, EVALUATED DUE TO EXCESSIVE DAMAGE AND REPLAC
- [SDR REXA2026032700253](https://openairdocs.org/sdr/REXA2026032700253.md): Fairing · cracked · Feb 8, 2026 · N918XJ · Cndair CL6002D24 · Engine Thrust Reverser
  > CRACKED THRUST-REVERSER AFT UPPER HINGE LINE FAIRING 443BT ALSO BEND AND WEAR AFT LOWER HINGE LINE FAIRING 443BB AT RH ENGINE. THRUST-REVERSER AFT UPPER HINGE LINE FAIRING 443BT WAS REPLACED PER CRJ900 AMM 54-12-01 AND AFT LOWER HINGE LINE FAIRING 443BB AT RH
- [SDR REXA2026032700262](https://openairdocs.org/sdr/REXA2026032700262.md): Fitting · corroded · Feb 7, 2026 · N918XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON PROXIMITY SENSOR PX36 AT GALLEY SERVICE DOOR CORROSION ON FITTING ASSY, SLIDE AT GALLEY SERVICE DOOR WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01 AND DUE TO EXCESSIVE DAMAGE WILL BE REPLACE PER CRJ 900 SRM 53-21-43-101-001-A03 AND WAS REPLACED
- [SDR REXA2026032700251](https://openairdocs.org/sdr/REXA2026032700251.md): Hinge · corroded · Feb 6, 2026 · N918XJ · Cndair CL6002D24 · Fuselage, Door Hinge
  > CORROSION ON HINGE(2EAS), HINGE ARMS(2EAS) AND HARDWARE ATTACHED TO ACCESS DOOR 196DR HINGE ASSY LWR P/N CC670-39189-1 WAS CLEANED PER CRJ900 SRM 51-26-00-001-001-A01 AND CORROSION WAS NOT FOUND AND DUE TO EXCESSIVE CORROSION ON HINGES OUTBD (NP: CC670-39095-1
- [SDR REXA2026032700250](https://openairdocs.org/sdr/REXA2026032700250.md): Hinge · corroded · Feb 6, 2026 · N918XJ · Cndair CL6002D24 · Fuselage, Door Hinge
  > CORROSION ON HINGE(2EAS), HINGE ARMS(2EAS) AND HARDWARE ATTACHED TO ACCESS DOOR 196DR HINGE ASSY LWR P/N CC670-39189-1 WAS CLEANED PER CRJ900 SRM 51-26-00-001-001-A01 AND CORROSION WAS NOT FOUND AND DUE TO EXCESSIVE CORROSION ON HINGES OUTBD (NP: CC670-39095-1
- [SDR REXA2026032700249](https://openairdocs.org/sdr/REXA2026032700249.md): Hinge · corroded · Feb 6, 2026 · N918XJ · Cndair CL6002D24 · Fuselage, Door Hinge
  > CORROSION ON HINGE(2EAS), HINGE ARMS(2EAS) AND HARDWARE ATTACHED TO ACCESS DOOR 196DR HINGE ASSY LWR P/N CC670-39189-1 WAS CLEANED PER CRJ900 SRM 51-26-00-001-001-A01 AND CORROSION WAS NOT FOUND AND DUE TO EXCESSIVE CORROSION ON HINGES OUTBD (NP: CC670-39095-1
- [SDR REXA2026080301384](https://openairdocs.org/sdr/REXA2026080301384.md): Landing · cracked · Feb 5, 2026 · N918XJ · Cndair CL6002D24 · Fuselage Main, Structure
  > "CRACK ON AFT RH DOOR LANDING AT FS 188.00 (LATCH CUT OUT OF ACCESS DOOR 212AR) RH DOOR LANDING AT FS 188.00 (LATCH CUT OUT OF ACCESS DOOR 212AR) WAS MANUFACTURED PER EA NO: CRJ953-21561 REV IR, DWG CC670-33151-6 REV ""D"", AND REPLACED PER CRJ 900 SRM 51-42-0
- [SDR REXA2026032700274](https://openairdocs.org/sdr/REXA2026032700274.md): Landing · cracked · Feb 5, 2026 · N918XJ · Cndair CL6002D24 · Service Doors
  > CRACK ON AFT RH DOOR LANDING AT FS 188.00 (LATCH CUT OUT OF ACCESS DOOR 212AR) RH DOOR LANDING AT FS 188.00 (LATCH CUT OUT OF ACCESS DOOR 212AR) WAS MANUFACTURED PER EA NO: CRJ953-21561 REV IR, DWG CC670-33151-6 REV ""D"", AND REPLACED PER CRJ 900 SRM 51-42-06
- [SDR REXA2026032700260](https://openairdocs.org/sdr/REXA2026032700260.md): Support · cracked · Feb 5, 2026 · N918XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACKED INTERNAL ANGLE OF EXTERNAL POWER RECEPTACLE SUPPORT STRUCTURE INTERNAL ANGLE OF EXTERNAL POWER RECEPTACLE SUPPORT STRUCTURE WAS REPLACED PER CRJ900 SRM 51-41-10-001-001-A01 AND SRM 51-42-06-001-001-A01
- [SDR REXA2022072500532](https://openairdocs.org/sdr/REXA2022072500532.md): Post · cracked · Jul 24, 2023 · N918XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > UPON REMOVAL LBL 27 POST WAS FOUND TO BE CRACKED. INSTALLED SERVICABLE LBL 27 POST IAW SERVICE BULLETIN FIGURE 105, SHEET 4 OF 8.
- [SDR REXA2022080801754](https://openairdocs.org/sdr/REXA2022080801754.md): Fitting · cracked · Aug 4, 2022 · N918XJ · Cndair CL6002D24 · Emergency Exits
  > RH FWD EMERGENCY EXIT DOOR HAS CRACK IN AFT PROX SENSOR FITTING. REPAIRED CRACKED STRUCTURE IN RH FWD EMERGENCY EXIT DOOR PER EA CRJ952-14082 REV IR, DATED 7/7/2022
- [SDR REXA2022080301731](https://openairdocs.org/sdr/REXA2022080301731.md): Channel · chafed · Aug 1, 2022 · N918XJ · Cndair CL6002D24 · Engine Thrust Reverser
  > RH LOWER TRANSCOWL LATCH DOOR COAMING CHANNEL CHAFED. REPLACED CHANNEL.
- [SDR REXA2022080301730](https://openairdocs.org/sdr/REXA2022080301730.md): Skin Panel · corroded · Aug 1, 2022 · N918XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > PASSENGER DOOR INNER SKIN CORRODED. REPLACED PASSENGER DOOR INNER SKIN.
- [SDR REXA2022072601698](https://openairdocs.org/sdr/REXA2022072601698.md): Bracket · cracked · Jul 22, 2022 · N918XJ · Cndair CL6002D24 · Engine Thrust Reverser
  > LH UPPER TRANSCOWL OUTBOARD-FWD STANDOFF ("A" BRACKET) CRACKED/BROKEN. REPLACED LH UPPER TRANSCOWL OUTBOARD-FWD STANDOFF.
- [SDR REXA2022072601697](https://openairdocs.org/sdr/REXA2022072601697.md): Bracket · cracked · Jul 22, 2022 · N918XJ · Cndair CL6002D24 · Engine Thrust Reverser
  > LH UPPER TRANSCOWL INBOARD-FWD STANDOFF ("A" BRACKET) CRACKED/BROKEN. REPLACED LH UPPER TRANSCOWL INBOARD-FWD STANDOFF..
- [SDR REXA2022072601694](https://openairdocs.org/sdr/REXA2022072601694.md): Panel · corroded · Jul 22, 2022 · N918XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > PASSENGER DOOR TOP PANEL AT UPPER STAIR WEB CORRODED. REPLACE PAX DOOR TOP PANEL AT UPPER STAIR WEB.
- [SDR REXA2022072201657](https://openairdocs.org/sdr/REXA2022072201657.md): Transcowl · cracked · Jul 18, 2022 · N918XJ · Cndair CL6002D24 · Engine Thrust Reverser
  > AFTER REMOVAL OF Z-ANGLE ON UPPER RH TRANSCOWL (FOR REPAIR OF DAMAGED FASTENERS) FOUND 1.159" CRACK IN INNER PERFORATED SKIN. REPAIRED RH UPPER TRANSCOWL SKIN PER EA CRJ954-13905 REV B.
- [SDR REXA2022072601696](https://openairdocs.org/sdr/REXA2022072601696.md): Sill Drain · corroded · Jul 16, 2022 · N918XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FLOOR SILL CORRODED AT FS 565.00 LH SIDE INSTALLED NEW LH LOWER FLOOR SILL FROM FS517 TO FS565 REF CRJ900 SRM 51-42-06-001-001-A01
- [SDR REXA2022072001612](https://openairdocs.org/sdr/REXA2022072001612.md): Frame · corroded · Jul 16, 2022 · N918XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > FRAME INTERNAL TO PAX DOOR AT FS313.56 BETWEEN DD4-DD5 HAS INTERGRANULAR CORROSION AROUND RIVET HOLES. REMOVED AND REPLACED CORRODED FRAME WITH NEW REPLACEMENT FRAME (P/N 601R318086-1) AND CLEAT (P/N 600-31902-269) USING ALL NEW HARDWARE. REF BOMBARDIER DWG 60
- [SDR REXA2022072001613](https://openairdocs.org/sdr/REXA2022072001613.md): Latch · chafed · Jul 15, 2022 · N918XJ · Cndair CL6002D24 · Engine Thrust Reverser
  > RH UPPER TRANSCOWL LATCH DOOR CHAFED IN MULTIPLE AREAS REPLACED RH UPPER TRANSCOWL LATCH DOOR
- [SDR REXA2022072001611](https://openairdocs.org/sdr/REXA2022072001611.md): Floor Panel · corroded · Jul 15, 2022 · N918XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > BACKUP SILL, STRINGER 21L, FS310-333 CORRODED BER. REPLACED BACKUP SILL, STRINGER 21L, FS310-333.
- [SDR REXA2022080301729](https://openairdocs.org/sdr/REXA2022080301729.md): Panel · corroded · Jun 30, 2022 · N918XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > PASSENGER DOOR, TOP PANEL ON STAIR WEB, AROUND SCREW HOLES HAS EVIDENCE OF CORROSION. REPLACED PASSENGER DOOR TOP PANEL ON STAIR WEB
- [SDR REXA2022072001614](https://openairdocs.org/sdr/REXA2022072001614.md): Channel · chafed · Jun 30, 2022 · N918XJ · Cndair CL6002D24 · Engine Thrust Reverser
  > RH LOWER TRANSCOWL CHANNEL C, FORWARD, IS CHAFED REPLACED CHANNEL C, FORWARD
- [SDR REXA2022071801600](https://openairdocs.org/sdr/REXA2022071801600.md): Latch · chafed · Jun 30, 2022 · N918XJ · Cndair CL6002D24 · Engine Thrust Reverser
  > LATCH DOOR COAMING CHAFED ON RH LOWER TRANSCOWL. " REPLACED LATCH DOOR COAMING ON RH LOWER TRANSCOWL."
- [SDR REXA2022071801598](https://openairdocs.org/sdr/REXA2022071801598.md): Track · corroded · Jun 15, 2022 · N918XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > SEAT TRACK AT RBL9, FS349-379 IS CORRODED IN SEVERAL AREAS, ON SEVERAL ELEMENTS. REPLACED SEAT TRACK PN SH670-32159-1 WITH NEW PART.
- [SDR REXA2022072001610](https://openairdocs.org/sdr/REXA2022072001610.md): Intercostal · corroded · Jun 13, 2022 · N918XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > PASSENGER DOOR INTERNAL STRUCTURE AT MID INTERCOSTAL DD6 HAS EVIDENCE OF CORROSION. REPLACED MID INTERCOSTAL DD6 PER CRJ900 SRM 51-42-06-001-001-A01, CRJ900 SRM 51-42-01-001-001-A01, DWG 601R31702 REV N.
- [SDR REXA2022080301728](https://openairdocs.org/sdr/REXA2022080301728.md): Frame · corroded · Jun 10, 2022 · N918XJ · Cndair CL6002D24 · Fuselage Main, Frame
  > FS1031.00 FRAME HAS CORROSION ON ITS ATTACHED FLANGE BETWEEN STGR23L AND 24L
- [SDR REXA2022071801599](https://openairdocs.org/sdr/REXA2022071801599.md): Panel · chafed · Jun 10, 2022 · N918XJ · Cndair CL6002D24 · Leading Edge Devices
  > LH INBOARD FLAP LEADING EDGE SKIN PANEL 584GB IS CHAFED FROM CONTACT WITH MOVABLE FLAP VANE. REPLACED PANEL 584GB WITH NEW SKIN PANEL PN CC670-14178-1.
- [SDR REXA2020020520149](https://openairdocs.org/sdr/REXA2020020520149.md): Floor Panel · delaminated · Jan 12, 2020 · N918XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > AWR: DELAMINATED FLOOR PANELS NBR, NRB 281DLF AND 282JRF AT AFT CARGO COMPARTMENT (COMPOSITE). SUMMARY: FLOOR PANELS NBR, NRB 281DLF AND 282JRF AT AFT CARGO COMPARTMENT WERE REPLACED PER CRJ-900 AMM 53-00-47-400
- [SDR REXA2019111421591](https://openairdocs.org/sdr/REXA2019111421591.md): Unknown · none · Nov 12, 2019 · N918XJ · Cndair CL6002D24 · Standard Practices/Structures
  > WHILE INCORPORATING SB607BA-57-020, CLEARANCE ISSUES WITH 1 FASTENER EACH SIDE UNDER FITTING. COMPLIED WITH BOMBARDIER REO 690-57-21-322 REV. DATED 2019-11-08. WVAC EMP STAMP 771.
- [SDR REXA2019090501288](https://openairdocs.org/sdr/REXA2019090501288.md): Light · inoperative · Sep 5, 2019 · N918XJ · Cndair CL6002D24 · Emergency Lighting
  > ESCAPE PATH LIGHTS IN GALLEY (R & L) BULBS INOP PN OL3071BPEGPL. REPLACED INOP BULBS IAW AMM 33-51-11. OP CK GOOD PN OL3071BPEGPL.
- [SDR REXA2019020300121](https://openairdocs.org/sdr/REXA2019020300121.md): Stringer Splice · corroded · Feb 3, 2019 · N918XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > OUT OF LIMITS CORROSION ON STRINGER SPLICE 25R IN STA FS= 329 TO FS= 339 AT MAIN AVIONICS COMPARTMENT. STRINGER SPLICE 25R BTW FS329/339 WAS REPLACED PER SRM 51-42-06-001-001-A01 PAR 6D AND SRM 51-42-20-001-001-A0 1 PAR 6E.
- [SDR REXA2019020300120](https://openairdocs.org/sdr/REXA2019020300120.md): Stringer · corroded · Feb 3, 2019 · N918XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STRINGER 25R IN STA FS= 280 TO FS= 329 AT MAIN AVIONICS COMPARTMENT. CORROSION LEVEL 2; STRINGER 25R IN STA FS= 280 TO FS= 329 AT MAIN AVIONICS COMPARTMENT WAS REPLACED PER SRM 51-42-06-001-001-A01.

Next page: https://openairdocs.org/aircraft/N918XJ/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 = 'N918XJ' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N918XJ/reports

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