# Service difficulty reports: N903XJ

A list on [N903XJ](https://openairdocs.org/aircraft/N903XJ.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 · 234 reports

- [SDR REXA2025060900636](https://openairdocs.org/sdr/REXA2025060900636.md): Beam · chafed · Apr 30, 2025 · N903XJ · 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 WAS MANUFACTURED PER EA CRJ953-19287 REV. C & EA NO CRJ953-19339 REV. IR AND WERE REPLACED PER CRJ900 SRM 51-42-06-001-0
- [SDR REXA2025060900646](https://openairdocs.org/sdr/REXA2025060900646.md): Doubler · chafed · Apr 29, 2025 · N903XJ · Cndair CL6002D24 · Trailing Edge Flaps
  > INITIAL INSPECTION: SEVERAL NICKS AND WEAR AT RH WING INB FLAP LOWER SKIN PANEL LOCATED BTW FLS 15.00 AND FLS65.50. SEVERAL NICKS AND WEAR AT RH WING INB FLAP LOWER SKIN PANEL LOCATED BTW FLS 15.00 AND FLS65.50 WERE BLEND-OUT AND EVALUATED OUT OF LIMITS THEREF
- [SDR REXA2025060900645](https://openairdocs.org/sdr/REXA2025060900645.md): Drag Angle · cracked · Apr 29, 2025 · N903XJ · Cndair CL6002D24 · Vertical Stabilizer
  > CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD / AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TR
- [SDR REXA2025060900644](https://openairdocs.org/sdr/REXA2025060900644.md): Drag Angle · cracked · Apr 29, 2025 · N903XJ · Cndair CL6002D24 · Vertical Stabilizer
  > CRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD / AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00) RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD / AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DAT
- [SDR REXA2025060900643](https://openairdocs.org/sdr/REXA2025060900643.md): Door Sill · cracked · Apr 29, 2025 · N903XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK ON AFT RH DOOR LANDING AT FS 188.00 (LATCH CUT OUT OF ACCESS DOOR 212AR AFT RH DOOR LANDING AT FS 188.00 (LATCH CUT OUT OF ACCESS DOOR 212AR WAS FABRICATED AND REPLACED PER EA CRJ953-19228 REV. IR AND DWG: CC670-33151 REV -D
- [SDR REXA2025060900642](https://openairdocs.org/sdr/REXA2025060900642.md): Floorbeam · corroded · Apr 29, 2025 · N903XJ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > CORROSION ON FLOOR PANEL ANGLE SUPPORT LOCATED BTW FS280.00 AND LBL9.00 TO RBL9.00. CORROSION ON FLOOR PANEL ANGLE SUPPORT LOCATED BTW FS280.00 AND LBL9.00 TO RBL9.00 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-00-00-101-001-A01 AND WAS REPLACED PER CRJ900
- [SDR REXA2025060900641](https://openairdocs.org/sdr/REXA2025060900641.md): Mount · corroded · Apr 29, 2025 · N903XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON ANGLE MOUNTING LOCATED BTW FS319.00/FS349.00 AND STGR 17RH AT SERVICE DOOR SURROUND ANGLE MOUNTING LOCATED BTW FS319.00/FS349.00 AND STGR 17RH AT SERVICE DOOR SURROUND WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-23-101-002-A02 AND WAS REPLACE
- [SDR REXA2025060900639](https://openairdocs.org/sdr/REXA2025060900639.md): Support Strap · corroded · Apr 29, 2025 · N903XJ · Cndair CL6002D24 · Aerodynamic Fairings
  > CORROSION AT SUPPORT STRUCTURE STRAP BTW FAIRING ACCESS PANEL 193AL & 193AR TO FAIRING ACCESS PANEL 193AB. CORROSION AT SUPPORT STRUCTURE STRAP BTW FAIRING ACCESS PANEL 193AL & 193AR TO FAIRING ACCESS PANEL 193AB WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-0
- [SDR REXA2025060900638](https://openairdocs.org/sdr/REXA2025060900638.md): Skin · chafed · Apr 29, 2025 · N903XJ · Cndair CL6002D24 · Trailing Edge Flaps
  > SEVERAL NICKS AND WEAR ON LOWER SKIN OF LH INBOARD FLAP FLS 15.00 TO FLS 65.5 AT LH WING. SEVERAL NICKS AND WEAR ON LOWER SKIN OF LH INBOARD FLAP FLS 15.00 TO FLS 65.5 AT LH WING WERE BLEND OUT PER CRJ900 SRM 51-12-00-001-001-A01, PREVIOUS REPAIR BTW FSL 15 T
- [SDR REXA2025060900637](https://openairdocs.org/sdr/REXA2025060900637.md): Angle · corroded · Apr 29, 2025 · N903XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > INITIAL INSPECTION: CORROSION ON ANGLE MID CAP AT PASSENGER DOOR SURROUND STRUCTURE. DUE TO EXCESIVE DAMAGE ON ANGLE MID CAP AT PASSENGER DOOR SURROUND STRUCTURE WAS REPLACED PER CRJ-900 SRM 53-00-00-101-001-A01 AND SRM 51-41-02-001-001-A01
- [SDR REXA2025032400352](https://openairdocs.org/sdr/REXA2025032400352.md): Lamp · inoperative · Mar 20, 2025 · N903XJ · Cndair CL6002D24 · Emergency Lighting
  > LEFT EXTERIOR EMERGENCY LIGHT AFT OF AFT EMERGENCY EXIT DOOR (OVERWING) INOP R/R EXTERNAL EMERGENCY LIGHT IAW AMM 33-51-15. OPS CHECK GOOD
- [SDR REXA2024110101409](https://openairdocs.org/sdr/REXA2024110101409.md): Frame · cracked · Jan 16, 2024 · N903XJ · Cndair CL6002D24 · Fuselage Main, Frame
  > L/H F.S 235 FRAME IS VISUALLY CRACKED AND REQUIRES REPLACEMENT. REMOVED AND REPLACED IAW IAW CRJ 900 SRMS 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
- [SDR REXA2024062400478](https://openairdocs.org/sdr/REXA2024062400478.md): Frame · cracked · Jan 15, 2024 · N903XJ · Cndair CL6002D24 · Fuselage Main, Frame
  > WHILE PERFORMING SB 670BA-53-045 REV G FOUND L/H FRAME AT FS220 TO BE CRACKED. FAILED NDT! INDICATION MARKED ON THE PART AND AREA MARKED WITH RED TAPE. REMOVED AND REPLACED IAW IAW CRJ 900 SRMS 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A
- [SDR REXA2024020500151](https://openairdocs.org/sdr/REXA2024020500151.md): Frame · cracked · Jan 15, 2024 · N903XJ · Cndair CL6002D24 · Fuselage Main, Frame
  > WHILE PERFORMING SB 670BA-53-045 REV G FOUND R/H FRAME AT FS220 TO BE CRACKED. FAILED NDT. INDICATIONS MARKED ON THE PART AND AREA MARKED WITH RED TAPE. REMOVED AND REPLACED IAW IAW CRJ 900 SRMS 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-
- [SDR REXA2024102500966](https://openairdocs.org/sdr/REXA2024102500966.md): Support · corroded · Jan 12, 2024 · N903XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > WHILE PERFORMING ENDEAVOR AIR EO# R53595 / SB670BA-53-061 FOUND CORROSION AT R/H F.S. 792.00 ON SILL DECK. REPAIRED DAMAGE I.A.W. MHIRJ REO 690-53-41-444 REV. --, DATED 2024-02-01
- [SDR REXA2024102500965](https://openairdocs.org/sdr/REXA2024102500965.md): Support · corroded · Jan 12, 2024 · N903XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > WHILE PERFORMING ENDEAVOR AIR EO# R53595 / SB670BA-53-061, FOUND CORROSION AT R/H F.S. 801.25. REPAIRED DAMAGE I.A.W. MHIRJ REO 690-53-41-444 REV. --, DATED 2024-02-01
- [SDR REXA2024062400477](https://openairdocs.org/sdr/REXA2024062400477.md): Door Frame · cracked · Jan 11, 2024 · N903XJ · Cndair CL6002D24 · Fuselage Main, Structure
  > R/H FWD EMERGENCY EXIT DOOR HAS VISIBLE CRACK ON UPPER AFT LUG FRAME. REPAIRED IAW MHIRJ REO 690-52-21-152 REV -- DATED 2024-02-02.
- [SDR REXA2024062400476](https://openairdocs.org/sdr/REXA2024062400476.md): Lug · cracked · Jan 11, 2024 · N903XJ · Cndair CL6002D24 · Emergency Exits
  > R/H AFT EMERGENCY EXIT DOOR HAS VISIBLE CRACK ON UPPER AFT LUG FRAME. REPAIRED IAW MHIRJ REO 690-52-21-151 REV -- DATED 2024-02-02.
- [SDR REXA2024021200184](https://openairdocs.org/sdr/REXA2024021200184.md): Structure · corroded · Jan 11, 2024 · N903XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > WHILE PERFORMING ENDEAVOR AIR EO# R53595 / SB670BA-53--061 FOUND CORROSION AT LH FS801.25 REPAIRED IAW MHIRJ REO 690-53-41-433 REV -- DATED 2024-02-01.
- [SDR REXA2024021200183](https://openairdocs.org/sdr/REXA2024021200183.md): Deck Plate · corroded · Jan 11, 2024 · N903XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > WHILE PERFORMING ENDEAVOR AIR EO# R53595 / SB670BA-53--061 FOUND CORROSION AT LH FS 792 ON SILL DECK. REPAIRED IAW MHIRJ REO 690-53-41-433 REV -- DATED 2024-02-01.
- [SDR REXA2024062400475](https://openairdocs.org/sdr/REXA2024062400475.md): Lug · cracked · Jan 10, 2024 · N903XJ · Cndair CL6002D24 · Emergency Exits
  > WHILE REMOVING LH AFT PASSENGER EMERGENCY EXIT DOOR FOUND FWD LUG CRACKED. REPAIRED IAW MHIRJ REO 690-52-21-153 REV -- DATED 2024-02-02.
- [SDR REXA2024102500962](https://openairdocs.org/sdr/REXA2024102500962.md): Diaphragm · cracked · Jan 8, 2024 · N903XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > WHILE COMPLYING WITH SB 670SH-53-043 REV C WE HAVE DISCOVERED L/H FS 768 DIAPHRAGM TO BE CRACKED AT LOWER BEAM TO DIAPHRAGM LOCATION ON THE I/B VERTICAL FACE. DRILLED AND INSTALLED NEW SERVICEABLE L/H DIAPHRAGM FS 768 PN SH670-36145-5 IAW CRJ-900 SRM 51-40-11-
- [SDR REXA2022012000148](https://openairdocs.org/sdr/REXA2022012000148.md): Charger · inoperative · Jan 18, 2023 · N903XJ · Cndair CL6002D24 · Emergency Lighting
  > UPON INTERIOR INSPECTION NOTED MULTIPLE EMERGENCY LIGHTS OUT IN CABIN, POWERED BY BATTERY PACK #1 REMOVED AND REPLACED #1 BATTERY CHARGER IAW AMM 33-51-17, AND REMOVED AND REPLACED #1 EPSU BATTERY PACK IAW AMM 33-51-17, ALL OPS TEST GOOD, NO DEFECTS NOTED AT
- [SDR REXA2022012600111](https://openairdocs.org/sdr/REXA2022012600111.md): Retainer · corroded · Jan 17, 2022 · N903XJ · Cndair CL6002D24 · Service Doors
  > AVI DOOR FWD SEAL RETAINER IS CORRODED. "REMOVED AND REPLACED AVI DOOR SEAL RETAINER IAW CRJ900 SRM 51-42- 06-001-001-A01, 51-40-11-001-001-A01 AND AMM 52-42-07-000/400-801-A01 LEAK CHECK GOOD
- [SDR REXA2022012600125](https://openairdocs.org/sdr/REXA2022012600125.md): Angle · corroded · Jan 15, 2022 · N903XJ · Cndair CL6002D24 · Wing Main, Frame Structure
  > RH WHEEL WELL TIRE BUST PANELS SUPPORT ANGLES ARE CORRODED "REMOVED, LOCATED, DRILL RH WHEEL TIRE ANGLE AND INSTALLED IAW CRJ-900 SRM, 51-23-00-001-001-A01, 51-42-21-001-001-A01, 51-40-11-001-001-A01, AMM 28-11-00-790-801-A01. LEAK CHECK GOOD. WVAC EMP STA
- [SDR REXA2022012600122](https://openairdocs.org/sdr/REXA2022012600122.md): Frame · corroded · Jan 15, 2022 · N903XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FRAME CORRODED AT FS 661+62 BETWEEN STGR 26L AND STGR 26R "REPAIRED FRAME AT FS 661+62 STR 26L AND 26R IAW EA CRJ953-12625. WVAC EMP STAMP # "
- [SDR REXA2022012600121](https://openairdocs.org/sdr/REXA2022012600121.md): Support Angle · corroded · Jan 15, 2022 · N903XJ · Cndair CL6002D24 · Wing Miscellaneous Structure
  > TIRE BURST SUPPORT ANGLE LH SIDE FOR PROTECTIVE COVERING CORRODED "REMOVED & REINSTALLED PANEL 541AB IAW CRJ900 AMM 28-11-01-000/400-802 (A02) LEAK TEST GOOD IAW CRJ900 AMM 28-11-01-400-802-A01. REMOVED, DRILLED, LOCATED, & INSTALLED SERVICABLE TIRE BURS
- [SDR REXA2022012600109](https://openairdocs.org/sdr/REXA2022012600109.md): Panel · corroded · Jan 15, 2022 · N903XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR AFT STAIR WEB CORRODED TCI 52-10-301 "REMOVED, LOCATED, DRILLED AND INSTALLED PAX DOOR AFT STAIR WEB IAW CRJ-900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, CRJ-900 AMM 52-11-07-400-802-A01, 52-11-00-710-801-A02. OPS CHECK GOOD. WVAC
- [SDR REXA2022012600134](https://openairdocs.org/sdr/REXA2022012600134.md): Floorbeam · corroded · Jan 9, 2022 · N903XJ · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > "FLOORBEAM AT LBL 27 HAS MULTIPLE SPOTS OF CORROSION BETWEEN FS 1000 TO FS 1031. " "REPAIRED FLOOR BEAM AT LBL27 BETWEEN FS 1000 AND FS 1031 PIAW CRJ 900 SRM 53-00-41-201-001-A03. WVAC EMP "
- [SDR REXA2022012600120](https://openairdocs.org/sdr/REXA2022012600120.md): Stringer · corroded · Jan 9, 2022 · N903XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > STRINGER 27 CORRODED BETWEEN FS 501.00 AND FS 517.00 RECEIVED & C/W EA CRJ953-12617 REV. IR WVAC EMP STAMP # MTC
- [SDR REXA2022012700173](https://openairdocs.org/sdr/REXA2022012700173.md): Panel · cracked · Jan 2, 2022 · N903XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "PAX DOOR FWD STAIR WEB HAS NUMEROUS AREAS OF CORROSION AND CRACKS. " "LOCATED, DRILLED AND INSTALLED FWD WEB IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-13-001-001-A01. WVA
- [SDR REXA2022012600127](https://openairdocs.org/sdr/REXA2022012600127.md): Drain · corroded · Dec 30, 2021 · N903XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > LH FLOOR SILL HAS MULTIPLE SPOTS OF CORROSION FROM FS 969 TO FS 1000. "REMOVED CORROSION ON SILL FS 969-985 WITHIN LIMITS IAW SRM 53-00-45-201-001-A01. REMOVED/REPLACED SILL FS 985-1000 IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A
- [SDR REXA2022012700168](https://openairdocs.org/sdr/REXA2022012700168.md): Drag Angle · cracked · Dec 28, 2021 · N903XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > "PAX DOOR FWD DRAG ANGLE IS CRACK AND HAS OVERSIZE HOLES, P/N: 601R31772-6. " " LOCATED AND DRILLED NEW PAX DOOR FWD DRAG ANGLE P/N 601R31772-6$ IAW CRJ900 SRM 51-40-11-001-001-A01. REMOVED
- [SDR REXA2022012700167](https://openairdocs.org/sdr/REXA2022012700167.md): Drag Angle · corroded · Dec 28, 2021 · N903XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > "PAX DOOR AFT DRAG ANGLE HAS OVERSIZE HOLES AND IS CORRODED, P/N: 601R31772-5. " "LOCATED AND DRILLED NEW AFT DRAG ANGLE P/N: 601R31772-5S IAW CRJ 900 SRM 51-40-11-001-001-A01. INSTALLED NEW ANGLE IAW CRJ 9
- [SDR REXA2022012600108](https://openairdocs.org/sdr/REXA2022012600108.md): Skin · corroded · Dec 28, 2021 · N903XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > "PAX DOOR INNER SKIN CORRODED IN MULTIPLE LOCATIONS ON BOTH I/B AND O/B SURFACES. " "REPLACED PAX DOOR INNER SKIN IAW CRJ900 SRM 51-42-06-001-001-A01, 51-42-10-001-001-A01.
- [SDR REXA2022012700172](https://openairdocs.org/sdr/REXA2022012700172.md): Fitting · corroded · Dec 24, 2021 · N903XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > MACHINED FITTING BTW FS 645 & FS 661, STR 24R TO 25R IS CORRODED. "REMOVED AND INSTALLED MACHINE FITTING IAW CRJ SRM 51-42-06-001- 001-A01 AND 51-42-21-001-001-A01. REMOVED AND REINSTALLED INTERCOSTAL IAW CRJ900 SRM 51-42-06-001-001-A01. BLEND
- [SDR REXA2022012700171](https://openairdocs.org/sdr/REXA2022012700171.md): Retaining Clip · corroded · Dec 24, 2021 · N903XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > PAX DOOR LOWER CENTER FS 327. CLIP IS CORRODED P/N: 601R318058-1. "LOCATED AND DRILLED NEW CLIP, P/N 601R 318058-1 IAW CRJ 900 SRM 51-40-11-001-A01. INSTALLED NEW CLIP IAW CRJ 900 SRM 51-42-06-001-A01, REV38 7/25/21.
- [SDR REXA2022012700170](https://openairdocs.org/sdr/REXA2022012700170.md): Doubler · cracked · Dec 24, 2021 · N903XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR DOUBLER FOR PULL IN CAM UPPER AFT SIDE IS CRACK, P/N:318094-2 "LOCATED AND DRILLED NEW PAX DOOR DOUBLER FOR PULL IN CAN P/N 601R318094-2, IAW CRJ900 SRM51-40-11-001-001-A01. REMOVED AND REPLACED DOUBLER, IAW CRJ900 SRM51-42-06-
- [SDR REXA2022012700169](https://openairdocs.org/sdr/REXA2022012700169.md): Cleat · corroded · Dec 24, 2021 · N903XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "PAX DOOR ON FWD SIDE CLEAT AT DD6 FS 320.163 IS CORRODED, P/N: 600-31902-275. " "LOCATED AND DRILLED CLEAN P/N 600-31902-269, IAW CRJ 900 SRM 51-40-11-001-001-A01. INSTALLED NEW CLEAT IAW CRJ 900 SRM 51-42-06-001-
- [SDR REXA2022012700163](https://openairdocs.org/sdr/REXA2022012700163.md): Rail · corroded · Dec 24, 2021 · N903XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "RH SIDE WALL SEAT RAIL #5 HAS SEVERAL AREAS OF CORROSION ALONG THE LENGTH OF THE RAIL (FS 661.00+90). " "REMOVED, FABRICATED AND INSTALLED SEAT RAIL IAW CRJ 900 AMM 53-00-49-000-801-A07 AND 900 SRM 53-00-49-201-002-A01. W
- [SDR REXA2022012700160](https://openairdocs.org/sdr/REXA2022012700160.md): Rail · corroded · Dec 24, 2021 · N903XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > RH SIDE WALL SEAT RAIL #4 HAS 1 AREA OF CORROSION AT FS 661.00. "REMOVED, FABRICATED AND INSTALLED SEAT RAIL IAW CRJ 900 AMM 53-00-49-000/400-801-A07 AND CRJ900 SRM 53-00-49-201-002-A01. WVAC EMP # "
- [SDR REXA2022012700159](https://openairdocs.org/sdr/REXA2022012700159.md): Rail · corroded · Dec 24, 2021 · N903XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "RH SIDE WALL SEAT RAIL #3 HAS SEVERAL AREAS OF CORROSION ALONG THE LENGTH OF THE RAIL (FS 565.00). " " REMOVED, FABRICATED AND INSTALLED SEAT RAIL IAW CRJ 900 AMM 53-00-49-000/400-801-A01 AND CRJ900 SRM 53-00-49-201-002-A
- [SDR REXA2022012700158](https://openairdocs.org/sdr/REXA2022012700158.md): Rail · corroded · Dec 24, 2021 · N903XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > RH SIDE WALL SEAT RAIL #8 HAS 6 AREAS OF CORROSION ALONG THE LENGTH "REMOVED AND REPLACED SEAT RAIL IAW CRJ 900 AMM'S 53-00-49-000/400-801-A07 WVAC EMP STAMP
- [SDR REXA2022012700151](https://openairdocs.org/sdr/REXA2022012700151.md): Rail · corroded · Dec 24, 2021 · N903XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "LBL 9 SEAT RAIL #5 HAS SEVERAL AREAS OF CORROSION AND WEAR ALONG THE LENGTH OF THE RAIL (FS 693.00). " "REPLACED SEAT RAIL LBL 9 #5 IAW CRJ 900 AMM SRM 57-00-49-000/400-801- A07, 53-00-49-201-002-A01. WVAC EMP "
- [SDR REXA2022012700148](https://openairdocs.org/sdr/REXA2022012700148.md): Rail · corroded · Dec 24, 2021 · N903XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "LH SIDE WALL SEAT RAIL #5 HAS (1) AREA OF CORROSION BETWEEN FS 693.00- 708.00 " "REMOVED, RECOUNTER SUNK AND REPLACED DISCREPANT FASTENER IAW CRJ900 SRM 51-40-11-001-001-AO1 AND SRM 51-41-02-00
- [SDR REXA2022012600144](https://openairdocs.org/sdr/REXA2022012600144.md): Rail · corroded · Dec 24, 2021 · N903XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "RBL 9 SEAT RAIL #3 HAS SEVERAL AREAS OF CORROSION ALONG THE LENGTH OF THE RAIL (FS 581.00). " "REMOVED, FABRICATED AND INSTALLED SEAT RAIL IAW CRJ 900 AMM 53-00-49-000/400-801-A07 AND SRM 53-00-49-201-002-A01.
- [SDR REXA2022012600141](https://openairdocs.org/sdr/REXA2022012600141.md): Rail · corroded · Dec 24, 2021 · N903XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "RBL 9 SEAT RAIL #5 HAS SEVERAL AREAS OF CORROSION ALONG THE LENGTH OF THE RAIL (FS 693.00). " "REMOVED, FABRICATED AND INSTALLED SEAT RAIL IAW CRJ 900 AMM 53-00-49-000/400-801-A01 AND CRJ900 SRM 53-00-49-201-002-A
- [SDR REXA2022012600139](https://openairdocs.org/sdr/REXA2022012600139.md): Rail · corroded · Dec 24, 2021 · N903XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "LBL 9 SEAT RAIL #3 HAS SEVERAL AREAS OF CORROSION ALONG LENGTH OF RAIL (FS 581.00). " "REMOVED, FABRICATED AND INSTALLED SEAT RAIL IAW CRJ 900 SRM 53-00-49-201-002-A01 AND AMM 53-00-49-000/400-801-A07. W
- [SDR REXA2022012600135](https://openairdocs.org/sdr/REXA2022012600135.md): Rail · corroded · Dec 24, 2021 · N903XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > LBL 9 SEAT RAIL #6 HAS (1) AREA OF CORROSION AT FS 847.00+16 "REMOVED, FABRICATED & INSTALLED SEAT RAIL IAW CRJ900 SRM 53-00-49- 201-002-A01 & AMM 53-00-49-000/400-801(A07) WVAC EMP # "
- [SDR REXA2022012600132](https://openairdocs.org/sdr/REXA2022012600132.md): Rail · corroded · Dec 24, 2021 · N903XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "LH SIDE WALL SEAT RAIL #3 HAS SEVERAL AREAS OF CORROSION FROM FS 565.00-661.00+16 " "CLEANED DISCREPANT AREAS OF SEALANT IAW CRJ 900 SRM 51-23-00-001- 001-A01 WVAC EMP # "

Next page: https://openairdocs.org/aircraft/N903XJ/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 = 'N903XJ' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N903XJ/reports

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