# Service difficulty reports: N914XJ

A list on [N914XJ](https://openairdocs.org/aircraft/N914XJ.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 · 223 reports

- [SDR REXA2026092201871](https://openairdocs.org/sdr/REXA2026092201871.md): Bulb · inoperative · Sep 18, 2026 · N914XJ · Cndair CL6002D24 · Emergency Lighting
  > SERVICE DOOR FLOOR FLOOD LIGHT EMERGENCY INOP R/R BULBS OPC GOOD IAW CRJ900 AMM 33-51-00. P/N OL3071BPEGPL
- [SDR REXA2026073001313](https://openairdocs.org/sdr/REXA2026073001313.md): Angle · cracked · Sep 3, 2025 · N914XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > AFTER ANGLE AND GUSSET REMOVAL:CRACK ON ANGLE BTW RBL12 AND FS280.00 WAS FOUND ANGLE BTW RBL12 AND FS280.00 WAS FABRICATED PER EA NO: CRJ953-20093 REV IR AND WAS REMOVED/INSTALLED WITH NRC 00145
- [SDR REXA2026073001311](https://openairdocs.org/sdr/REXA2026073001311.md): Floor Support · corroded · Sep 3, 2025 · N914XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR SUPPORT BTW FS280/FS265 AND RBL12 AT CABIN FLOOR STRUCTURE DUE TO EXCESSIVE CORROSION ON FLOOR SUPPORT BTW FS280/FS265 AND RBL12 AT CABIN FLOOR STRUCTURE WAS REPLACED PER CRJ900 SRM 51-10-06-001-001-A01 AND SRM 51-42-21-001-001-A01
- [SDR REXA2026073001307](https://openairdocs.org/sdr/REXA2026073001307.md): Door · cracked · Sep 3, 2025 · N914XJ · Cndair CL6002D24 · Landing Gear Doors
  > CRACK ON FWD MEMBRANE OF INBD DOOR AT LH MLG INBD DOOR AT LH MLG P/N: KBA670-10500-31 S/N: 15149 WAS REMOVED PER CRJ-900 AMM 32-12-01-000-802-A04 AND TS #: 005834B-R1 AND SERVICEABLE LH MLG INBD DOOR P/N: KBA670-10500-31, S/N: 15095 WAS INSTALLED PER CRJ-900 A
- [SDR REXA2026073001305](https://openairdocs.org/sdr/REXA2026073001305.md): Fitting · corroded · Sep 3, 2025 · N914XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > AFTER BRUSH REMOVAL: CORROSION AND WEAR ON SEATTLEMENT AREA WAS FOUND. CORROSION AND WEAR ON SEATTLEMENT AREA WAS EVALUATED OUT OF LIMITS THEREFORE THEY WERE REPLACED PER CRJ-900 SRM 51-10-06-001-001-A01 AND AMM 20-21-00-910-801- A01
- [SDR REXA2025092500896](https://openairdocs.org/sdr/REXA2025092500896.md): Rib · cracked · Sep 3, 2025 · N914XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACKED BAT RIB AT WS 14.50 OUTER WING, RH MLG WHEEL WELL TRUNNION AREA. BAT RIB AT WS 14.50 OUTER WING, RH MLG WHEEL WELL TRUNNION AREA WAS FABRICATED PER EO CC670-10611 SNIEO S01 IN ACCORDING TO DWG CC670-10611 REV -B THEREFORE WAS REPLACED PER CRJ-900 SRM
- [SDR REXA2025092500895](https://openairdocs.org/sdr/REXA2025092500895.md): Step · cracked · Sep 3, 2025 · N914XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > AFTER FWD HANDRAIL SUPPORT FITTINGS REMOVAL, CRACK ON PASSENGER DOOR STAIR FWD SIDE PANEL WAS FOUND PASSENGER DOOR STAIR FWD SIDE PANEL WAS REPAIRED PER CRJ900 SRM 52-11-04-201-004-A01
- [SDR REXA2025092500894](https://openairdocs.org/sdr/REXA2025092500894.md): Step · cracked · Sep 3, 2025 · N914XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > AFTER AFT HANDRAIL SUPPORT FITTINGS REMOVAL, CRACK ON PASSENGER DOOR STAIR AFT SIDE PANEL WAS FOUND PASSENGER DOOR STAIR AFT SIDE PANEL WAS REPAIRED IAW SRM 52-11-04-201-004-A01.
- [SDR REXA2025092500893](https://openairdocs.org/sdr/REXA2025092500893.md): Support Plate · cracked · Sep 3, 2025 · N914XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK ON TWO CORNERS OF JB-6 SUPPORT PLATE IN THE FWD EQUIPMENT BAY. A NEW SUPPORT PLATE WAS MANUFACTURED IAW EA CRJ953-20095, REV A, AND REPLACED IAW SRM 51-42-06-001-001-A01.
- [SDR REXA2025092500892](https://openairdocs.org/sdr/REXA2025092500892.md): Door Frame · corroded · Sep 3, 2025 · N914XJ · Cndair CL6002D24 · Fuselage Main, Structure
  > CORROSION ON DOOR POST RBL12, BS 280 LOWER SECTION OF THE BULKHEAD, THE DOOR POST WAS REPAIRED PER SRM 53-11-10-201-006-A01.
- [SDR REXA2025092500891](https://openairdocs.org/sdr/REXA2025092500891.md): Floorbeam · cracked · Sep 3, 2025 · N914XJ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > CRACKED CENTER COCKPIT FLOORBEAM, RBL 12, BS 280. THE FLOORBEAM WAS REPAIRED PER REO 690-53-11-2050 REV -.
- [SDR REXA2025092500890](https://openairdocs.org/sdr/REXA2025092500890.md): Door Frame · corroded · Sep 3, 2025 · N914XJ · Cndair CL6002D24 · Fuselage Main, Structure
  > CORROSION ON DOOR POST REPAIR DOUBLER AT LBL 12, BS 280, LOWER SECTION OF THE BULKHEAD. THE DOOR POST WAS REPAIRED IAW SRM 53-11-10-201-006-A01.
- [SDR REXA2025092500889](https://openairdocs.org/sdr/REXA2025092500889.md): Attach Angle · cracked · Sep 3, 2025 · N914XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > CRACK ON ATTACH ANGLE INNER SKIN-TO-AFT SIDE PANEL AT PASSENGER DOOR EXTERNAL STRUCTURE. ATTACH ANGLE WAS REPAIRED PER SRM 52-11-04-201-002-A01.
- [SDR REXA2025092500887](https://openairdocs.org/sdr/REXA2025092500887.md): Cover · cracked · Sep 3, 2025 · N914XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > BROKEN FORWARD UPPER COVER AT PASSENGER DOOR FORWARD UPPER COVER AT PASSENGER DOOR WAS REPAIRED PER EA CRJ952-20089 REV IR.
- [SDR REXA2026073001312](https://openairdocs.org/sdr/REXA2026073001312.md): Hinge · corroded · Aug 31, 2025 · N914XJ · Cndair CL6002D24 · Fuselage, Door Hinge
  > CORROSION ON BUSHING BORE LH/RH HINGE FITTINGS AT NLG W/W AREA (2EA) WAS FOUND LH/RH HINGE FITTINGS AT NLG W/W AREA (2EA) WERE REPLACED PER CRJ900 SRM 51-42-21-001-001-A01
- [SDR REXA2025092500886](https://openairdocs.org/sdr/REXA2025092500886.md): Angle · cracked · Aug 31, 2025 · N914XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACKED ANGLE BETWEEN LBL 12, BS 280. THE ANGLE WAS REPLACED IAW SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, AND SRM 51-42-10-001-001-A01.
- [SDR REXA2025092500885](https://openairdocs.org/sdr/REXA2025092500885.md): Receptacle · cracked · Aug 31, 2025 · N914XJ · Cndair CL6002D24 · Electrical Power System
  > CRACKED ON BOX OF THE EXTERNAL POWER RECEPTACLE AT THE FWD FUSELAGE BOX OF THE EXTERNAL POWER RECEPTACLE AT THE FWD FUSELAGE WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01, SRM 51-42-10-001-001-A01 AND SRM 51-42-21-001-001-A01.
- [SDR REXA2025092500884](https://openairdocs.org/sdr/REXA2025092500884.md): Fitting · worn · Aug 31, 2025 · N914XJ · Cndair CL6002D24 · Trailing Edge Flaps
  > WEAR ON TWO FLAP FITTINGS, STUB FAIRINGS 171DL & 172DR, RT & LT WING TRAILING EDGE. FLAP FITTINGS WERE EVALUATED, AND DUE TO EXCESIVE DAMAGE, WERE REPLACED SRM 53-00-00-101-001-A01, AMM 20-21-00-910-801-A01, AND SRM 51-42-21-001-001-A01.
- [SDR REXA2025092500883](https://openairdocs.org/sdr/REXA2025092500883.md): Support · worn · Aug 31, 2025 · N914XJ · Cndair CL6002D24 · Trailing Edge Flaps
  > WEAR ON TWO PLATE SUPPORTS OF FLAP STUB FAIRING 171DL & 172DR, RT & LT WING TRAILING EDGE. PLATE SUPPORTS WERE EVALUATED DUE TO EXCESIVE DAMAGE AND WERE REPLACED IAW SRM 53-00-00-101-001-A01, AMM 20-21-00-910-801-A01, AND SRM 51-42-21-001-001-A01.
- [SDR REXA2025092500882](https://openairdocs.org/sdr/REXA2025092500882.md): Seat Track · corroded · Aug 28, 2025 · N914XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK BETWEEN BS 367 - 382, LBL 9. DUE TO EXCESSIVE DAMAGE ON THE SEAT TRACK, REPLACED IAW SRM 53-21-49-101-001-A01, AMM 53-00-49-000-801, AND AMM 53-00-49-400-801.
- [SDR REXA2025092500881](https://openairdocs.org/sdr/REXA2025092500881.md): Seat Track · corroded · Aug 28, 2025 · N914XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK BETWEEN BS 349 - 379, RBL 9. DUE TO EXCESSIVE DAMAGE ON SEAT TRACK, REPLACED IAW SRM 53-21-49-101-001-A01, AMM 53-00-49-000-801, CONFIG A19, AND AMM 53-00-49-400-801, CONFIG A19.
- [SDR REXA2026073001310](https://openairdocs.org/sdr/REXA2026073001310.md): Bracket · corroded · Aug 22, 2025 · N914XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON HINGE(1 EA) AND BRACKETS (2 EAS) AT ACCESS PANEL 196DR CORROSION ON HINGE (1 EA) AND BRACKETS (2 EAS) AT ACCESS PANEL 196DR WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01 AND WERE EVALUATED ARE OUT LIMITS THEREFORE WERE REPLACED PER CRJ900 SRM 51
- [SDR REXA2026073001309](https://openairdocs.org/sdr/REXA2026073001309.md): Hinge · corroded · Aug 22, 2025 · N914XJ · Cndair CL6002D24 · Fuselage, Door Hinge
  > CORROSION ON HINGE(1 EA) AND BRACKETS (2 EAS) AT ACCESS PANEL 196DR CORROSION ON HINGE (1 EA) AND BRACKETS (2 EAS) AT ACCESS PANEL 196DR WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01 AND WERE EVALUATED ARE OUT LIMITS THEREFORE WERE REPLACED PER CRJ900 SRM 51
- [SDR REXA2026073001308](https://openairdocs.org/sdr/REXA2026073001308.md): Hinge · corroded · Aug 22, 2025 · N914XJ · Cndair CL6002D24 · Fuselage, Door Hinge
  > CORROSION ON HINGE(1 EA) AND BRACKETS (2 EAS) AT ACCESS PANEL 196DR CORROSION ON HINGE (1 EA) AND BRACKETS (2 EAS) AT ACCESS PANEL 196DR WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01 AND WERE EVALUATED ARE OUT LIMITS THEREFORE WERE REPLACED PER CRJ900 SRM 51
- [SDR REXA2025092500880](https://openairdocs.org/sdr/REXA2025092500880.md): Stringer · corroded · Aug 22, 2025 · N914XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > AFT CLEAN AREA, CORROSION ON STRINGER 25R BETWEEN BS 295 - 310. CORROSION ON THE STRINGER WAS EVALUATED OUT LIMITS IAW SRM 53-21-03-101-002-A04. REPLACED IAW SRM 51-42-21-001-001-A01 AND SRM 51-42-06-001-001-A01.
- [SDR REXA2025092500879](https://openairdocs.org/sdr/REXA2025092500879.md): Stringer · corroded · Aug 22, 2025 · N914XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STRINGER 26R LOCATED BTW BS 295 - 310. THE STRINGER WAS REPLACED DUE TO EXCESSIVE DAMAGE IAW SRM 51-10-06-001-001-A01, SRM 51-42-21-001-001-A01, SRM 51-42-06-001-001-A01, AND SRM 51-42-10-001-001-A01.
- [SDR REXA2025092500878](https://openairdocs.org/sdr/REXA2025092500878.md): Doubler · cracked · Aug 22, 2025 · N914XJ · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > CRACK ON DOUBLER ON FWD EQUIPMENT COMPARTMENT INTERNAL STRUCTURE BTW BS 193, S16L, ADG RESTOW PUMP AREA, DOUBLER ON FWD EQUIPMENT COMPARTMENT INTERNAL STRUCTURE BTW FS 193.00 AND STGR 16L REPLACED IAW SRM 53-11-43-201-001-A01.
- [SDR REXA2025091800870](https://openairdocs.org/sdr/REXA2025091800870.md): Skin · worn · Aug 22, 2025 · N914XJ · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > WEAR ON FUSELAGE SKIN BTW FS 913 TO FS 927 STGR 27. FUSELAGE SKIN BTW FS 913 TO FS 927 STGR 27 WAS REPAIRED PER REO 670-53-00-290 REV. F AND INSPECTION REQUIREMENTS FOR 40,000 FLIGHT CYCLES PER SDIR 670-53-00-290
- [SDR REXA2026073001306](https://openairdocs.org/sdr/REXA2026073001306.md): Stiffener · cracked · Aug 19, 2025 · N914XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK IN STIFFENER AT ACCESS 172CR. STIFFENER (P/N: SH670-39397-3) AT ACCESS 172CR WAS FABRICATED PER EA NO: CRJ953-19937 REV IR AND REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01
- [SDR REXA2025092500876](https://openairdocs.org/sdr/REXA2025092500876.md): Floor Support · corroded · Aug 19, 2025 · N914XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR SUPPORT BTW BS 280 - 319, RBL47. CORROSION ON FLOOR SUPPORT WAS EVALUATED OUT LIMITS IAW SRM 51-10-06-001-001-A01, REPLACED THE FLOOR SUPPORT IAW SRM 51-42-06-001-001-A01 AND SRM 51-42-10-001-001-A01.
- [SDR REXA2025070900714](https://openairdocs.org/sdr/REXA2025070900714.md): Lamp · inoperative · Jul 3, 2025 · N914XJ · Cndair CL6002D24 · Emergency Lighting
  > RH AFT EXTERNAL EMERGENCY LIGHT INOP RELAMPED RH AFT EXTERNAL EMERGENCY LIGHT IAW AMM 33-51-15 R/R LENSE FOR RH AFT EXTERNAL EMERGENCY LIGHT IAW CRJ900 AMM 33-51-15 OPC GOOD.
- [SDR REXA2022113002617](https://openairdocs.org/sdr/REXA2022113002617.md): Pressure Deck · corroded · Nov 28, 2022 · N914XJ · Cndair CL6002D24 · Fuselage Main, Structure
  > RIGHT PRESSURE DECK CORRODED. INSTALLED A NEW PRESSURE DECK IAW SRM 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.
- [SDR REXA2022112102595](https://openairdocs.org/sdr/REXA2022112102595.md): Fitting · cracked · Nov 18, 2022 · N914XJ · Cndair CL6002D24 · Fuselage Main, Attach Fittings
  > WHILE PERFORMING SB 670BA-53-045 FOUND L/H 220 FRAME TOP FITTING P/N CC67-51720-1 TO BE CRACKED. REMOVED AND REPLACED IAW CRJ 900 SRMS 51-40-11-001-001-A01, AND 51-42-06-001-001-A01.
- [SDR REXA2022112102594](https://openairdocs.org/sdr/REXA2022112102594.md): Frame · cracked · Nov 18, 2022 · N914XJ · Cndair CL6002D24 · Fuselage Main, Frame
  > NDT FOUND ONE INDICATION ON L/H FS220 FRAME BETWEEN STGR 13L & 14L APPROX 0.125IN LONG EXTENDING OUT OF FASTENER HOLE AS MARKED. REMOVED AND REPLACED IAW CRJ 900 SRMS 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.
- [SDR REXA2022111602560](https://openairdocs.org/sdr/REXA2022111602560.md): Battery Pack · inoperative · Nov 14, 2022 · N914XJ · Cndair CL6002D24 · Emergency Lighting
  > FOUND THE FOLLOWING EMERGENCY EXIT LIGHTS INOP: EMERGENCY EXIT SIGNS ON CEILING AND EXIT ROW 13 AND CEILING LIGHTS AFT OF ROW 13. REMOVED AND REPLACED BATTERY PACKS @PS43 AND PS38 IAW CRJ900 AMM 33-55-17. ALL CHECKS GOOD.
- [SDR REXA2022052600987](https://openairdocs.org/sdr/REXA2022052600987.md): Angle · corroded · May 19, 2022 · N914XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > PASSENGER DOOR UPPER SILL ANGLE HAS MULTIPLE SPOTS OF CORROSION REMOVED AND REPLACED SILL ANGLE IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-41-02-001-001-A01
- [SDR REXA2022052600986](https://openairdocs.org/sdr/REXA2022052600986.md): Angle · corroded · May 19, 2022 · N914XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > PASSENGER DOOR LOWER SILL ANGLE HAS MULTIPLE SPOTS OF CORROSION REMOVED AND REPLACED SILL ANGLE IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01
- [SDR REXA2022052701031](https://openairdocs.org/sdr/REXA2022052701031.md): Splice · corroded · May 11, 2022 · N914XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > STRINGER 22L AND STRINGER SPLICE IS CORRODED FROM FS 319.70 TO 333.00. REMOVED AND REPLACED STRINGER 22L AND STRINGER SPLICE IAW CRJ 900 SRMS 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-21-001-001-A01, AND 53-00-03-201-001-A02.
- [SDR REXA2022052701025](https://openairdocs.org/sdr/REXA2022052701025.md): Stringer · corroded · May 11, 2022 · N914XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > STRINGER 22L AND STRINGER SPLICE IS CORRODED FROM FS 319.70 TO 333.00. REMOVED AND REPLACED STRINGER 22L AND STRINGER SPLICE IAW CRJ 900 SRMS 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-21-001-001-A01, AND 53-00-03-201-001-A02.
- [SDR REXA2022052600999](https://openairdocs.org/sdr/REXA2022052600999.md): Doubler · corroded · May 11, 2022 · N914XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > BELOW THE FLOOR, ANTENNA DOUBLER IS CORRODED BETWEEN FS 295-FS 310 AT STRINGER 27. REMOVED AND REPLACED DOUBLER IAW CRJ 900 SRMS 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.
- [SDR REXA2022052701017](https://openairdocs.org/sdr/REXA2022052701017.md): Web · corroded · May 2, 2022 · N914XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FS 280 BULKHEAD WEB CORRODED (R/H SIDE). REPAIRED FS 280 RIGHT LOWER BULKHEAD WEB IAW CRJ 900 SRM 53-11-10-201-004-A01.
- [SDR REXA2022052601000](https://openairdocs.org/sdr/REXA2022052601000.md): Frame · corroded · May 2, 2022 · N914XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > BELOW THE FLOOR, FS 333 FRAME LOWER FLANGE IS CORRODED BETWEEN 26L STGR - STGR 27. REPAIRED FRAME AT FS 333 BETWEEN STRINGERS 25L AND 25R IAW CRJ 900 SRM 53-00-06-201-001-A03.
- [SDR REXA2022052600994](https://openairdocs.org/sdr/REXA2022052600994.md): None · corroded · May 2, 2022 · N914XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > RH SIDE SEAT RAIL AT FS 744 -752 HAS MULTIPLE SPOTS OF CORROSION. REPLACED SEAT RAIL IAW CRJ 900 AMM 53-00-49-000/400-801-A07.
- [SDR REXA2022052701015](https://openairdocs.org/sdr/REXA2022052701015.md): Stringer · corroded · May 1, 2022 · N914XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > STGR 23R IS CORRODED BETWEEN FS 379 TO FS 394. REMOVED UNSERVICEABLE STRINGER 23R AND INSTALLED A SERVICEABLE STRINGER 23R (P/N SH670-31380-1) IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.
- [SDR REXA2022052701014](https://openairdocs.org/sdr/REXA2022052701014.md): Stringer · corroded · May 1, 2022 · N914XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > STGR 20R IS CORRODED BETWEEN FS 379 TO FS 394. REMOVED UNSERVICEABLE STRINGER 20R AND INSTALLED A SERVICEABLE STRINGER 20R (P/N SH670-31405-2) IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-21-001-001-A01, AND 51-42-13-001-001-A01.
- [SDR REXA2022052701029](https://openairdocs.org/sdr/REXA2022052701029.md): Web · corroded · Apr 29, 2022 · N914XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > AFTER REMOVAL OF PASSENGER DOOR AFT WEB FOUND TO BE HEAVILY CORRODED. REMOVED AND REPLACED PASSENGER DOOR AFT WEB IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 AND 51-42-21-001-001-A01
- [SDR REXA2022052600982](https://openairdocs.org/sdr/REXA2022052600982.md): Latch · cracked · Apr 29, 2022 · N914XJ · Cndair CL6002D24 · Service Doors
  > RIGHT AFT LATCH FOR TRU DOOR FUSELAGE SKIN IS CRACKED REMOVED AND REPLACED TRU DOOR LANDING IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 AND 51-42-13-001-001-A01
- [SDR REXA2022052701030](https://openairdocs.org/sdr/REXA2022052701030.md): Striker · corroded · Apr 28, 2022 · N914XJ · Cndair CL6002D24 · Service Doors
  > CORROSION ON GALLEY SERVICE DOOR LOWER SEAL STRIKER. REMOVED AND REPLACED GALLEY SERVICE DOOR STRIKER IAW CRJ 900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01
- [SDR REXA2022052701028](https://openairdocs.org/sdr/REXA2022052701028.md): Angle · corroded · Apr 28, 2022 · N914XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON IMPACT ANGLE OF WATER WASTE SERVICE DOOR AT STRINGER 23R AND F.S. 379.00 AND 394.00. REMOVED AND REPLACED IMPACT ANGLE IAW CRJ 900 SRM 51-42-06-001-001-A01.
- [SDR REXA2022052701027](https://openairdocs.org/sdr/REXA2022052701027.md): Former · corroded · Apr 28, 2022 · N914XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > PASSENGER DOOR FORMER AT F.S.329.41 DD4 AND DD5 HAS CORROSION AROUND LIGHTNING HOLE AND PITTING REMOVED AND REPLACED PASSENGER DOOR FORMER AT F/S/329.41 IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-21-001-001-A01, AND 51-42-06-001-001-A01

Next page: https://openairdocs.org/aircraft/N914XJ/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 = 'N914XJ' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N914XJ/reports

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