# Service difficulty reports: N919XJ

A list on [N919XJ](https://openairdocs.org/aircraft/N919XJ.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 3 · 148 reports

- [SDR REXA2026071401074](https://openairdocs.org/sdr/REXA2026071401074.md): Charger · inoperative · Jul 10, 2026 · N919XJ · Cndair CL6002D24 · Emergency Lighting
  > DURING LINE CHECK, FOUND AFT FACING SEAT DIVIDER EMERGENCY LIGHT INOP. R & R PS36 CHARGER IAW 33-51-17. OP CHECK IS GOOD IAW 33-51-17-710-801.
- [SDR REXA2026062900988](https://openairdocs.org/sdr/REXA2026062900988.md): Battery Pack · inoperative · Jun 23, 2026 · N919XJ · Cndair CL6002D24 · Emergency Lighting
  > EMERGENCY LIGHT AT GALLEY SERVICE DOOR IS INOP. R & R NR 2 EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-17. OPS TEST GOOD.
- [SDR REXA2026060100896](https://openairdocs.org/sdr/REXA2026060100896.md): Angle · corroded · May 31, 2026 · N919XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > UPON REMOVAL OF PAX DOOR MID CAP FOUND ANGLE KICKPLATE PN SH670-31875-3 TO BE CORRODED. REMOVED THE PAX DOOR KICKPLATE ANGLE IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.INSTALLED NEW PAX DOOR KICKPLATE ANGLE (P/N SH670-31875-3S) IAW CRJ 90
- [SDR REXA2026052600612](https://openairdocs.org/sdr/REXA2026052600612.md): Drag Angle · cracked · May 23, 2026 · N919XJ · Cndair CL6002D24 · Fuselage, Stabilizer Attach Fittings
  > LH FWD DRAG ANGLE IS CRACKED. COMPLIED WITH CRJ900 SRM REPAIR 55-31-00-201-001-A01 ON L/H FWD DRAG ANGLE.
- [SDR REXA2026052000603](https://openairdocs.org/sdr/REXA2026052000603.md): Lug · cracked · May 19, 2026 · N919XJ · Cndair CL6002D24 · Emergency Exits
  > L/H AFT OVERWING EXIT FWD LUG APPEARS TO BE CRACKED. DOOR S/N IS SB0671 REPAIRED IAW MHIRJ REO 670-52-21-103 DATED 2024-11-06 REV --.
- [SDR REXA2026051200581](https://openairdocs.org/sdr/REXA2026051200581.md): Lug · cracked · May 10, 2026 · N919XJ · Cndair CL6002D24 · Fuselage, Door Hinge
  > R/H FWD OVER WING EXIT DOOR FWD LUG APPEARS TO BE CRACKED. REPAIRED CRACK TO R/H FWD OVERWING EMERGENCY EXIT DOOR TOP SECTION (AROUND BASE OF DOOR PROXIMITY SENSOR STRIKERS) IAW MHIRJ REO 670-52-21-103 REV -- DATED 2024-11-06. DDOR S/N SB0669.
- [SDR REXA2026050400450](https://openairdocs.org/sdr/REXA2026050400450.md): Lug · cracked · May 3, 2026 · N919XJ · Cndair CL6002D24 · Emergency Exits
  > LEFT FWD OVERWING EXIT AFT LUG APPEARS TO BE CRACKED DOOR S/N IS SB0668. REPAIRED LUG IAW REO 670-52-21-103 DATED 2024-11-06 REV --.
- [SDR REXA2026052100604](https://openairdocs.org/sdr/REXA2026052100604.md): Angle · cracked · Apr 30, 2026 · N919XJ · Cndair CL6002D24 · Vertical Stabilizer Miscellaneous Structure
  > L/H DRAG ANGLE ON VERT. STAB HAS A CRACK (MARKED W/ TAPE) REMOVED UNSERVICEABLE LH AFT DRAG ANGLE IAW CRJ900 SRM 51-42-21-001-001-A01 AND 51-42-13-001-001-A01. LOCATED AND DRILLED NEW SERVICEABLE LH AFT DRAG ANGLE PN: AV670-21186-003 IAW CRJ900 SRM 51-40-11-0
- [SDR REXA2026050400445](https://openairdocs.org/sdr/REXA2026050400445.md): Angle · corroded · Apr 27, 2026 · N919XJ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > FS 280 FWD J ANGLE IS HEAVILY CORRODED AND REQUIRES REPLACEMENT REMOVED J ANGLE IAW CRJ-900 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01 LOCATED AND DRILL NEW PART PN# CC670-34095-1SB IAW CRJ-900 SRM 51-40-11-001-001-A01 INSTALLED J-ANGEL IAW CRJ-900 SRM 5
- [SDR REXA2026061100965](https://openairdocs.org/sdr/REXA2026061100965.md): Angle · corroded · Apr 26, 2026 · N919XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR MID CAP ANGLE IS CORRODED. PARTIALLY INSTALLED PAX DOOR PROX SENSOR (PX25) THROUGH MID CAP ANGLE & KICKPLATE ANGLE IAW AMM 52-70-04-400-802-A02 STEP 4.B(1). COMPLIED WITH REMAINING STEPS OF AMM 52-70-04-400-802-A02. OPS TEST GOOD. INSTALLED PAX DOOR G
- [SDR REXA2026011500004](https://openairdocs.org/sdr/REXA2026011500004.md): Beam · cracked · Jan 15, 2026 · N919XJ · Cndair CL6002D24 · Fluid Service Doors
  > DURING MAINTENANCE TO LT HYDRAULIC BAY SKIN, CRACKED LT NLG DOOR BEAM AT LBL 13.40. REPLACED BEAM PER APPLICABLE SRM STANDARD PRACTICES AND DRAWINGS, BEAM IS FCBS & WAS DOCUMENTED AS A MAJOR REPAIR.
- [SDR REXA2026011500003](https://openairdocs.org/sdr/REXA2026011500003.md): Skin · cracked · Jan 15, 2026 · N919XJ · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > A CRACK WAS FOUND ON LEFT HYDRAULIC BAY SKIN AT TRU DOOR CORNER IAW EA CRJ953-19108. REPLACED SKIN PER APPLICABLE SRM AND DRAWINGS. SKIN WAS DEEMED FCBS AND WAS DOCUMENTED AS A MAJOR REPAIR.
- [SDR REXA2025082600839](https://openairdocs.org/sdr/REXA2025082600839.md): Window · cracked · Aug 20, 2025 · N919XJ · Cndair CL6002D24 · Passenger Compartment Windows
  > OUTER PANE OF CABIN WINDOW AT SEAT 9C/D MOSTLY MISSING REPLACED WINDOW ASSEMBLY
- [SDR REXA2025012100060](https://openairdocs.org/sdr/REXA2025012100060.md): Sensor · inoperative · Jan 15, 2025 · N919XJ · Cndair CL6002D24 · Landing Gear Brake System
  > ON CLIMBOUT @ LGA BRAKE OVERHEAT WARNING POSTED @ APPROX 600 AGL. COMPLIED WITH EMER NON NORMAL CHECK LISTS. DEFERRED IAW MEL 32-46-1D. MX PROCEDURES COMPLIED WITH. MOC NOTIFIED 102658. MMO2 UPDATED AND PLACARD INSTALLED. R&R RHIB THERMOCOUPLE SNSOR IAW CRJ90
- [SDR REXA2025010700009](https://openairdocs.org/sdr/REXA2025010700009.md): Battery Pack · inoperative · Jan 3, 2025 · N919XJ · Cndair CL6002D24 · Emergency Lighting
  > DURING LINE CHECK FOUND EMERGENCY LIGHTS OUT FWD OVERWING AND INTERIOR FWD EMERGENCY EXIT R/R EMERGENCY BATTERY IN POSTION PS37 IAW AMM 33-51-17. R/R EMERGENCY OVERWING LIGHT IAW AMM 33-51-15. OPS CHECK GOOD
- [SDR REXA2022110302382](https://openairdocs.org/sdr/REXA2022110302382.md): Drag Angle · cracked · Oct 30, 2022 · N919XJ · Cndair CL6002D24 · Vertical Stabilizer
  > VERTICAL STAB. RH FWD DRAG ANGLE HAS POSSIBLE CRACK (FLAGGED) PERFORMED CUT OUT OF RH FWD DRAG ANGLE, BUCKET SKIN, AND COMPLIED WITH ALL STEPS OF REO 690-55-31-071 REV. – DATED: 2022-09-26
- [SDR REXA2022102602301](https://openairdocs.org/sdr/REXA2022102602301.md): Drag Angle · cracked · Oct 26, 2022 · N919XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR AFT STAIR WEB DRAG ANGLE HAS CRACK. REMOVED AND REPLACED CRACKED AFT DRAG ANGLE WITH NEW REPLACEMENT DRAG ANGLE USING ALL NEW FASTENERS. REF CRJ900 SRM 51-42-06-001-001 A01
- [SDR REXA2022102602310](https://openairdocs.org/sdr/REXA2022102602310.md): Floorbeam · corroded · Oct 22, 2022 · N919XJ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > FS280 CROSS BEAM CORRODED ON THE UPPER FLANGE UPPER SURFACE BETWEEN LBL 14 & RBL 9. REMOVED AND REPLACED NEW UPPER SPLICE STRAP P/N CC670-34097-1. REF: CRJ-900 SRM 51-42-06-001-001-A01 AND REFERENCED SB 670BA-53-041 REV D FEB 28/2014 PG 162 AND 163
- [SDR REXA2022102602309](https://openairdocs.org/sdr/REXA2022102602309.md): Floor Support · corroded · Oct 20, 2022 · N919XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > LH FLOOR SILL FROM FS 985 TO FS 1047 HAS MULTIPLE SPOTS OF CORROSION REMOVED AND REPLACED LH LOWER SILL MM670-35655-003 FS 1000 - 1047 WITH NEW P/N MM670-35655-003 REF CRJ 900 SRM 51-42-06-001-001-A01, SRM 51-42-10-001-001-A01 AND SRM 51-42-21-001-001-A01. CO
- [SDR REXA2022102602308](https://openairdocs.org/sdr/REXA2022102602308.md): Stringer · corroded · Oct 20, 2022 · N919XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER 20R INTERCOSTAL AFT OF FS349 HAS CORROSION BELOW CANNON PLUG BRACKET REMOVED AND REPLACED INTERCOSTAL AT STGR 20R FS349-FS364 REV. CRJ 900 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, AND DWG SH670-31950 REV. Y
- [SDR REXA2022102602307](https://openairdocs.org/sdr/REXA2022102602307.md): Stringer · corroded · Oct 20, 2022 · N919XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER 25R BETWEEN FS280 AND 295 HAS CORROSION REMOVED AND REPLACED STR 25R SECTION SH670-31212-2 BETWEEN FS 280- FS 333 REF CRJ900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01.
- [SDR REXA2022102602305](https://openairdocs.org/sdr/REXA2022102602305.md): Angle · corroded · Oct 20, 2022 · N919XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > PAX DOOR SILL KICK ANGLE IS CORRODED AROUND FASTENER HOLES INSTALLED NEW SILL KICK ANGLE AND MID CAP ANGLE P/NS SH670-31825-9 & SH670-31875-3 REF. CRJ 900 SRM 51-42-21-001-001-A01, 51-42-06-001-001-A01 & DWG SH670-31810 REV AE
- [SDR REXA2022102602303](https://openairdocs.org/sdr/REXA2022102602303.md): Intercostal · corroded · Oct 20, 2022 · N919XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL (FWD) DD4 IS CORRODED. INSTALLED NEW INTERCOSTAL P/N 601R318093-1 REF CRJ 900 SRM 51-42-06-001-001-A01 AND DWG. NO. 601R31702 REV. N
- [SDR REXA2022102602302](https://openairdocs.org/sdr/REXA2022102602302.md): Former · corroded · Oct 20, 2022 · N919XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR FWD FORMER IS CORRODED IN MULTIPLE AREAS REMOVED AND REPLACED PAX DOOR FWD FORMER WITH NEW P/N 601R318031-5 REF CRJ 900 SRM 51-42-06-001-001-A01, CRJ SRM 51-42-21-001-001-A01 AND DWG.NO. 601R31702 REV.N
- [SDR REXA2022102602300](https://openairdocs.org/sdr/REXA2022102602300.md): Web · cracked · Oct 20, 2022 · N919XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR AFT STAIR WEB HAS CRACK ON LOWER STEP CORNER REMOVED AND REPLACED CRACKED AFT PAX DOOR WEB WITH NEW WEB PER CRJ900 SRM'S 51-42-06-001-001 A01, 51-42-21-001-001 A01 AND 51-42-13-001-001 A01
- [SDR REXA2022102602299](https://openairdocs.org/sdr/REXA2022102602299.md): Cleat · corroded · Oct 20, 2022 · N919XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > CORROSION ON PAX DOOR CLEAT COMMON TO INTERCOSTAL DD6 & FORMER, FS329.41 REMOVED AND REPLACED CORRODED PAX DOOR CLEAT WITH NEW PAX DOOR CLEAT (P/N 600-31902-269) AT FS329.41 DD6 WITH NEW FASTENERS. REF DWG 601R31702 REV-N AND CRJ 900 SRM 51-42-06-001-001-A01
- [SDR REXA2022102602298](https://openairdocs.org/sdr/REXA2022102602298.md): Intercostal · corroded · Oct 20, 2022 · N919XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > CORROSION ON PAX DOOR INTERCOSTAL DD6 UPPER AND LOWER SIDE REMOVED AND REPLACED INTERCOSTAL AT DD6 FROM FS320-FS338 WITH NEW P/N 601R318057-1 REF DWG 601R31702 REV-N, CRJ 900 SRM 51-42-06-001-001-A01 AND CRJ 900 SRM 51-42-21-001-001-A01
- [SDR REXA2022102602297](https://openairdocs.org/sdr/REXA2022102602297.md): Drag Angle · worn · Oct 20, 2022 · N919XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CENTER BAG BAY DOOR DEFLECTOR WORN THROUGH AT SEVERAL SPOTS CUT AWAY DAMAGED AREA & PERFORMED DRAG ANGLE REPAIR REF CRJ 900 SRM 55-31-00-201-001-A01
- [SDR REXA2022102602296](https://openairdocs.org/sdr/REXA2022102602296.md): Drag Angle · cracked · Oct 20, 2022 · N919XJ · Cndair CL6002D24 · Vertical Stabilizer
  > VERTICAL STAB RH AFT DRAG ANGLE HAS POSSIBLE CRACK CUT AWAY DAMAGED AREA & PERFORMED DRAG ANGLE REPAIR REF CRJ 900 SRM 55-31-00-201-001-A01
- [SDR REXA2022102602295](https://openairdocs.org/sdr/REXA2022102602295.md): Angle · corroded · Oct 14, 2022 · N919XJ · Cndair CL6002D24 · Fuselage Main, Bulkhead
  > RH FS280.00 BULKHEAD WEB CAP ANGLE CORRODED. REMOVED AND INSTALLED NEW CAP ANGLE COMMON TO RH FLOOR BEAM AT FS280 AND RH LOWER WEB RBL9.0-RBL39 REF CRJ900 SRM 51-42-006-001-A01, 51-42-13-001-001-A01 AND SRM 51-42-15-001-001-A01
- [SDR REXA2022102602294](https://openairdocs.org/sdr/REXA2022102602294.md): Floorbeam · corroded · Oct 14, 2022 · N919XJ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > CORROSION FOUND ON CAP AT FS 280.00 RH CROSS BEAM AT RBL 9 TO RBL 24. REMOVED AND REPLACED FS 280.00 RH CROSS BEAM AT BL0-RBL42.00 WITH NEW P/N CC670-34094-2 REF CRJ-900 SRM 51-42-06-001-001-A01, CRJ-900 SRM 51-42-22-001-001-A01, CRJ900 SRM 51-42-13-001-001-A0
- [SDR REXA2022102602293](https://openairdocs.org/sdr/REXA2022102602293.md): Floor Support · corroded · Oct 14, 2022 · N919XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > RIGHT FLOOR SILL FS280.00 - FS319.00 IS CORRODED IN MULTIPLE AREAS. REMOVED AND REPLACED RH FLOOR SILL BETWEEN FS280.00 AND FS319.00 WITH NEW P/N SH670-32172-9 REF CRJ 900 SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01 AND 51-42-21-001-001-A01
- [SDR REXA2022102602312](https://openairdocs.org/sdr/REXA2022102602312.md): Bulkhead Web · corroded · Oct 7, 2022 · N919XJ · Cndair CL6002D24 · Fuselage Main, Bulkhead
  > LH FS280.00 BULKHEAD LOWER WEB (PN CC670-34170-7) AFT SIDE FROM LBL39 TO LBL9 HAS CORROSION IN MULTIPLE AREAS REMOVED AND REPLACED LH BULKHEAD LOWER WEB COMMON TO LH FS280.00 FLOOR BEAM AND BUTTSTRAP AT LBL 12.00-LBL45.00 WITH NEW PARTS REF CRJ900 SRM 53-11-10
- [SDR REXA2022102602311](https://openairdocs.org/sdr/REXA2022102602311.md): Angle · corroded · Oct 7, 2022 · N919XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CAP ANGLE (PN CC670-34096-1) COMMON TO FS280.00 FLOOR BEAM AND FS280.00 BULKHEAD LOWER WEB FROM LBL39 TO LBL9 HAS CORROSION IN MULTIPLE AREAS ON FAYING SURFACES REMOVED AND REPLACED CAP ANGLE COMMON TO LH FLOOR BEAM AT FS280 AND LH LOWER WEB LBL9.0-LBL39 WITH
- [SDR REXA2022092202135](https://openairdocs.org/sdr/REXA2022092202135.md): None · corroded · Sep 19, 2022 · N919XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON LH SIDE SEAT RAIL CHANNEL BETWEEN FS 903.00-961.00 INSTALLED NEW SEAT RAIL IAW CRJ900 AMM 53-00-49-400-801-A07.
- [SDR REXA2022092202134](https://openairdocs.org/sdr/REXA2022092202134.md): None · corroded · Sep 19, 2022 · N919XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION FOUND LH SIDE SEAT RAIL BETWEEN FS 379-483 INSTALLED NEW SEAT RAIL IAW CRJ900 AMM 53-00-49-400-801-A07.
- [SDR REXA2022092202123](https://openairdocs.org/sdr/REXA2022092202123.md): Seat Track · corroded · Sep 19, 2022 · N919XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > LBL 9 FLOOR SEAT TRACK IS CORRODED BETWEEN F.S. 847+48 TO F.S. 985. INSTALLED FABRICATED SEAT TRACK AT LBL 9 F.S 847+48 TO F.S. 985.IAW CRJ 900 AMM 53-00-49-400-801-A07
- [SDR REXA2022091602100](https://openairdocs.org/sdr/REXA2022091602100.md): Angle · cracked · Sep 12, 2022 · N919XJ · Cndair CL6002D24 · Vertical Stabilizer
  > VERTICAL STAB. LH AFT DRAG ANGLE HAS POSSIBLE CRACK REPLACD ANGLE PER CRJ 900 SRM 55-31-00-201-001-A01
- [SDR REXA2022092202136](https://openairdocs.org/sdr/REXA2022092202136.md): None · corroded · Sep 10, 2022 · N919XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON RH SIDE SEAT RAIL BETWEEN FS 847.00+14-867.00. INSTALLED NEW SEAT RAIL IAW CRJ900 AMM 53-00-49-400-801-A07.
- [SDR REXA2022091602103](https://openairdocs.org/sdr/REXA2022091602103.md): Cleat · corroded · Sep 7, 2022 · N919XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR CLEAT COMMON TO INTERCOSTAL DD6 AND FORMER, FS320 IS CORRODED. REPLACED CLEAT AND FORMER PER CRJ 900 SRM 51-42-06-001-001-A01 AND CRJ 900 SRM 51-42-15-001-001-A01
- [SDR REXA2022091602102](https://openairdocs.org/sdr/REXA2022091602102.md): None · chafed · Sep 7, 2022 · N919XJ · Cndair CL6002D24 · Wing, Control Surfaces
  > RH I/BD FLAP PANEL 684ET IS CHAFED REPLACED PANEL PER CRJ900 SRM 51-40-11-001-001-A01
- [SDR REXA2022091602101](https://openairdocs.org/sdr/REXA2022091602101.md): Panel · chafed · Sep 7, 2022 · N919XJ · Cndair CL2151A10 · Engine Thrust Reverser
  > TRANSCOWL PANEL 443BT IS CHAFED REPLACED PANEL PER CRJ900 SRM 51-12-00-001-001-A01
- [SDR REXA2022091502099](https://openairdocs.org/sdr/REXA2022091502099.md): Flap · chafed · Sep 7, 2022 · N919XJ · Cndair CL6002D24 · Wing, Control Surfaces
  > LEFT WING INBOARD FLAP LEADING EDGE PANEL 584ET IS CHAFED. REPLACED PANEL PER CRJ900 SRM 51-40-11-001-001-A01
- [SDR REXA2019101481477](https://openairdocs.org/sdr/REXA2019101481477.md): Actuator · tripped · Oct 8, 2019 · N919XJ · Cndair CL6002D24 · Leading Edge Slat Actuator
  > SLATS FAIL" CAUTION MESSAGE ON APPROACH TO MKE. RAN QRH. MESSAGE REMAINED. SLATS STUCK AT 0, FLAPS FUNCTIONED NORMALLY. NOTED SLAT ACTUATORS NR 3, 4, AND 6 ON LH SIDE AND 5 ON RH SIDE TRIPPED. SUSPECTED WATER IN LH NR 3 SLAT ACTUATOR. REMOVED AND REPLACED LH
- [SDR REXA2019082101249](https://openairdocs.org/sdr/REXA2019082101249.md): Light · damaged · Aug 21, 2019 · N919XJ · Cndair CL6002D24 · Emergency Lighting
  > EMERGENCY TRACK LIGHTING DAMAGED AT ROW 9. REMOVED AND REPLACD DAMAGE FLOOR TRACK LIGHTING IAW AMM 33-51-01. FLOOR TRACK LIGHTING OK FOR SVC IF NECESSARY. P/N OFF/ON - PL1100LH07 P/N OFF/ON - PLI315LH00
- [SDR REXA2018122801366](https://openairdocs.org/sdr/REXA2018122801366.md): Stringer · corroded · Dec 28, 2018 · N919XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STRINGER 26L AND 26R FROM FS= 280 TO FS= 330 AT MAIN AVIONICS COMPARTMENT. CORROSION LEVEL 2 ON STRINGER 26L AND 26R FROM FS= 280 TO FS= 330 WAS EVALUATED AND FINDING IT OUT OF LIMITS PER SRM 53-21-03-101-002-A04 AT MAIN AVIONICS COMPARTMENT. STR
- [SDR REXA2018122801360](https://openairdocs.org/sdr/REXA2018122801360.md): Stringer · corroded · Dec 28, 2018 · N919XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > INITIAL INSPECTION. CORROSION ON STRINGER 27 FROM FS= 280 TO FS= 295, ALSO ON STRINGER 27 FROM FS= 333 TO FS= 353 AT MAIN AVIONICS COMPARTMENT. (E/E) (TCI: 100-09)COMPLETE: SUMMARY OF NRC 00101: CORROSION LEVEL 2 ON STRINGER 27 FROM FS= 280 TO FS= 295, ALSO ON
- [SDR REXA2018122601361](https://openairdocs.org/sdr/REXA2018122601361.md): Seat Track · corroded · Dec 26, 2018 · N919XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > INITIAL INSPECTION: CORROSION ON SIDE SEAT RAILS IN SECTIONS [ FS= 572 TO FS= 661+16, STR 15L/R ] [ FS= 661+16 TO FS= 661+90, STR 15L/R ] [ FS=661+90 TO FS=720, STR 15R ] AT PAX CABIN. (CPAX) (TCI: 53-20-217). COMPLETE: SUMMARY OF NRC 00116: NEW SIDE SEAT RA
- [SDR REXA2018122201367](https://openairdocs.org/sdr/REXA2018122201367.md): Floorbeam · corroded · Dec 22, 2018 · N919XJ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > CORROSION ON FLOORBEAM LBL9 STA FS 1033 AT AFT CARGO COMPARTMENT. FLOORBEAM LBL9 STA FS=1033 AT AFT CARGO COMPARTMENT WAS REPAIRED PER REO 670-53-00-029 REV "A".
- [SDR REXA2018122201365](https://openairdocs.org/sdr/REXA2018122201365.md): Floorbeam · corroded · Dec 22, 2018 · N919XJ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > CORROSION ON FLOORBEAM LBL27 STA FS=1032 AT AFT CARGO COMPARTMENT. FLOORBEAM LBL27 STA FS=1032 AT AFT CARGO COMPARTMENT WAS REPAIRED PER REO 670-53-00-029 REV "A".

Next page: https://openairdocs.org/aircraft/N919XJ/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 = 'N919XJ' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N919XJ/reports

---
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