# Service difficulty reports: N691CA

A list on [N691CA](https://openairdocs.org/aircraft/N691CA.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 · 242 reports

- [SDR REXA2026072801202](https://openairdocs.org/sdr/REXA2026072801202.md): Lamp · inoperative · Jul 26, 2026 · N691CA · Cndair CL6002D24 · Emergency Lighting
  > OVERHEAD EMERGENCY LIGHT INOP @ ROW 17. R/R BULB OPC GOOD IAW CRJ900 AMM 33-51-09
- [SDR REXA2026060900962](https://openairdocs.org/sdr/REXA2026060900962.md): Charger · inoperative · May 30, 2026 · N691CA · Cndair CL6002D24 · Emergency Lighting
  > MULTIPLE FWD GALLEY AREA AND FORWARD PASSENGER AREA EMERGENCY LIGHTS INOP. DURING TROUBLESHOOTING, BORROWED KNOWN GOOD BATTERY CHARGER ASSY FROM 15153. ONCE KNOWN GOOD BATTERY CHARGER ASSY WAS INSTALLED IN THE #1 POSITION (CRJ 900 AMM 33-51-17-400--802-A02),
- [SDR REXA2026052600610](https://openairdocs.org/sdr/REXA2026052600610.md): Bearing · damaged · May 22, 2026 · N691CA · Cndair CL6002D24 · Ailerons
  > FOUND 1 EA. R/H AILERON SIDE BEARING LUG LABELED H TO BE PREVIOUSLY OVERSIZED REPAIRED IAW CRJ 900 MHIRJ REO 690-57-61-514 REV -- DATED 2026-05-08
- [SDR REXA2026052200605](https://openairdocs.org/sdr/REXA2026052200605.md): Bushing · damaged · May 22, 2026 · N691CA · Cndair CL6002D24 · Ailerons
  > FOUND 4EA. R/H AILERON SIDE BUSHING LUGS LABELED B,C,F,AND G TO BE PREVIOSLY OVERSIZED REPAIRED IAW CRJ 900 MHIRJ REO 670-57-61-237 REV -- DATED 2017-07-25
- [SDR REXA2026052600609](https://openairdocs.org/sdr/REXA2026052600609.md): Seat Track · corroded · May 21, 2026 · N691CA · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > PAX FLOOR SEAT TRACK AT RBL9 CORRODED AT FS349. REPAIRED IAW MHI RJ REO 670-53-00-589 REV -D 2025-08-20.
- [SDR REXA2026052600608](https://openairdocs.org/sdr/REXA2026052600608.md): Seat Track · corroded · May 21, 2026 · N691CA · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > PAX FLOOR SEAT TRACK AT LBL9 CORRODED AT FS379. REPAIRED IAW MHI RJ REO 670-53-00-589 REV -D 2025-08-20.
- [SDR REXA2026052600607](https://openairdocs.org/sdr/REXA2026052600607.md): Bushing · damaged · May 11, 2026 · N691CA · Cndair CL6002D24 · Ailerons
  > FOUND RT AILERON SIDE LUG LABELED -C- TO BE ABOVE 4TH OVER PER GREO 670-57-61-237 BY 0.0225, COMPLIED WITH REPAIR OF BUSHING LUG MARKED C IAW MHIRJ REO 690-57-61-518 REV -- DATED 2026-05-22.
- [SDR REXA2026060100894](https://openairdocs.org/sdr/REXA2026060100894.md): Fitting · cracked · Apr 24, 2026 · N691CA · Cndair CL6002D24 · Emergency Exits
  > LEFT AFT OVERWING EMERGENCY EXIT DOOR THE UPPER FORWARD ALIGNMENT SPIGOT FITTING STRUCTURE NEAR THE BASE IS CRACKED REPAIRED LH AFT OVERWING EMERGENCY EXIT IAW MHIRJ REO 690-52-21-228 REV -- DATED 2026-05-25 AND MHIRJ REO 670-52-21-103 REV -- DATED 2024-11-06.
- [SDR REXA2026051200580](https://openairdocs.org/sdr/REXA2026051200580.md): Lug · damaged · Apr 24, 2026 · N691CA · Cndair CL6002D24 · Wing, Control Surface Attach Fittings
  > "R/H WING SIDE AILERON HINGE #3 (I/B) HAS A PREVIOUSLY O/S LUG LABELED ""E"". CURRENT LUG INTERNAL DIAMETER MEASURES (0.8910""). NOMINAL LUG INTERNAL DIAMETER IS (0.8750""). ENGINEERING IS REQUIRED. REPAIRED RH WING SIDE AILERON FITTING #3 IB LUG IAW MHIRJ REO
- [SDR REXA2026051200579](https://openairdocs.org/sdr/REXA2026051200579.md): Lug · damaged · Apr 24, 2026 · N691CA · Cndair CL6002D24 · Wing, Control Surface Attach Fittings
  > "R/H WING SIDE AILERON HINGE #2 (I/B) HAS A PREVIOUSLY O/S LUG LABELED ""C"". CURRENT LUG INTERNAL DIAMETER MEASURES (0.8910""). NOMINAL LUG INTERNAL DIAMETER IS (0.8750""). ENGINEERING IS REQUIRED. REPAIRED RH WING SIDE AILERON FITTING #2 IB LUG IAW MHIRJ REO
- [SDR REXA2026051200578](https://openairdocs.org/sdr/REXA2026051200578.md): Lug · damaged · Apr 24, 2026 · N691CA · Cndair CL6002D24 · Wing, Control Surface Attach Fittings
  > "R/H WING SIDE AILERON HINGE #3 (O/B) HAS A PREVIOUSLY O/S LUG LABELED ""F"". CURRENT LUG INTERNAL DIAMETER MEASURES (0.8910""). NOMINAL LUG INTERNAL DIAMETER IS (0.8750""). ENGINEERING IS REQUIRED. REPAIRED RH WING SIDE AILERON FITTING #3 OB LUG IAW MHIRJ REO
- [SDR REXA2026051200577](https://openairdocs.org/sdr/REXA2026051200577.md): Lug · damaged · Apr 24, 2026 · N691CA · Cndair CL6002D24 · Wing, Control Surface Attach Fittings
  > "R/H WING SIDE AILERON HINGE #2 (O/B) HAS A PREVIOUSLY O/S LUG LABELED ""D"". CURRENT LUG INTERNAL DIAMETER MEASURES (0.8910""). NOMINAL LUG INTERNAL DIAMETER IS (0.8750""). ENGINEERING IS REQUIRED. REPAIRED RH WING SIDE AILERON FITTING #2 OB LUG IAW MHIRJ REO
- [SDR REXA2026051200576](https://openairdocs.org/sdr/REXA2026051200576.md): Lug · damaged · Apr 24, 2026 · N691CA · Cndair CL6002D24 · Wing, Control Surface Attach Fittings
  > "L/H WING SIDE AILERON HINGE #3 (O/B) HAS A PREVIOUSLY O/S LUG LABELED ""F"". CURRENT LUG INTERNAL DIAMETER MEASURES (0.9065""). NOMINAL LUG INTERNAL DIAMETER IS (0.8750""). ENGINEERING IS REQUIRED. REPAIRED LH WING SIDE AILERON #3 FITTING OB LUG IAW MHIRJ REO
- [SDR REXA2026051200575](https://openairdocs.org/sdr/REXA2026051200575.md): Lug · damaged · Apr 24, 2026 · N691CA · Cndair CL6002D24 · Wing, Control Surface Attach Fittings
  > "L/H WING SIDE AILERON HINGE #3 (I/B) HAS A PREVIOUSLY O/S LUG LABELED "E". CURRENT LUG INTERNAL DIAMETER MEASURES (0.9065""). NOMINAL LUG INTERNAL DIAMETER IS (0.8750""). ENGINEERING IS REQUIRED. REPAIRED LH WING SIDE AILERON FITTING #3 IB LUG IAW MHIRJ REO 6
- [SDR REXA2026042900414](https://openairdocs.org/sdr/REXA2026042900414.md): Fitting · cracked · Apr 24, 2026 · N691CA · Cndair CL6002D24 · Emergency Exits
  > RIGHT FWD OVERWING EMERGENCY EXIT DOOR, THE UPPER AFT ALIGNMENT SPIGOT FITTING STRUCTURE NEAR THE BASE, HAS EVIDENCE OF A CRACK. REPAIRED IAW REO 670-52-21-103 REV -- DATE 2024-11-06 AND CRJ 900 SRMS 51-26-01-001-001-A01 AND 51-42-21-001-001-A01. SEE MAINTE
- [SDR REXA2026052800868](https://openairdocs.org/sdr/REXA2026052800868.md): Fitting · cracked · Apr 23, 2026 · N691CA · Cndair CL6002D24 · Fuselage Main, Structure
  > LEFT AFT OVERWING EMERGENCY EXIT DOOR THE UPPER FORWARD ALIGNMENT SPIGOT FITTING STRUCTURE NEAR THE BASE IS CRACKED. REPAIRED LH AFT OVERWING EMERGENCY EXIT IAW MHIRJ REO 690-52-21-228 REV -- DATED 2026-05-25 AND MHIRJ REO 670-52-21-103 REV -- DATED 2024-11-0
- [SDR REXA2026052800867](https://openairdocs.org/sdr/REXA2026052800867.md): Floorbeam · corroded · Apr 20, 2026 · N691CA · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > R/H FS 280 CORRODED ON BOTTOM CORNER EDGE OF THE BEAM. REMOVED DAMAGED RH FS 280.00 CROSSBEAM IAW CRJ900 SRM 51-42-06-001-001-A01. CRJ900 SRM 51-42-13-001-001-A01. AND CRJ900 SRM 51-42-22-001-001-A01. LOCATED AND DRILLED NEW RH FS 280.00 CROSSBEAM P/N:CC670-3
- [SDR REXA2026052800866](https://openairdocs.org/sdr/REXA2026052800866.md): Floorbeam · corroded · Apr 20, 2026 · N691CA · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > L/H FS 280 CROSSBEAM HAS CORRODED PIT ON TOP CORNER EDGE OF THE BEAM. REMOVED FS 280 SACRIFICIAL TITANIUM PLATE FOR ACCESS IAW CRJ-900 SRM 51-42-13-001-001-A01. REMOVED DAMAGED LH FS 280.00 CROSSBEAM IAW CRJ900 SRM 51-42-06-001-001-A01. CRJ900 SRM 51-42-13-00
- [SDR REXA2025060600630](https://openairdocs.org/sdr/REXA2025060600630.md): Lamp · inoperative · Jun 2, 2025 · N691CA · Cndair CL6002D24 · Emergency Lighting
  > RH AFT EXTERIOR EMERGENCY LIGHT INOP RELAMPED RH AFT EXTERIOR EMERGENCY LIGHT IAW CRJ 900 IPC 33-51-15. OPS TEST GOOD IAW AMM 33-51-15. P/N OFF/ON: 8GH002473-08
- [SDR REXA2025031400320](https://openairdocs.org/sdr/REXA2025031400320.md): Lamp · inoperative · Mar 13, 2025 · N691CA · Cndair CL6002D24 · Emergency Lighting
  > FOUND EMERGENCY FLOOD LIGHT BULB IN-OP AFT OF GALLEY R/R EMERGENCY FLOOD LIGHT BULB IAW CRJ 900 AMM 33-51-09-960-801 OPS CHECK GOOD. P/N ON/OFF 1317 NSN
- [SDR REXA2024101500877](https://openairdocs.org/sdr/REXA2024101500877.md): Lamp · inoperative · Oct 15, 2024 · N691CA · Cndair CL6002D24 · Emergency Lighting
  > EMERGENCY LIGHT INOP ROW 3DC RELAMP EMERGENCY LIGHT PER AMM 33-51-09 P/N ON/OFF: 1317
- [SDR REXA2024012200090](https://openairdocs.org/sdr/REXA2024012200090.md): Light · inoperative · Jan 19, 2024 · N691CA · Cndair CL6002D24 · Emergency Lighting
  > LH AFT OVERWING EMERGENCY LIGHT INOP REMOVED AND REPLACED LH AFT OVERWING EMERGENCY LIGHT IAW CRJ 900 AMM 33-51-15. OP CHECKED GOOD.
- [SDR REXA2022033000267](https://openairdocs.org/sdr/REXA2022033000267.md): Retainer · cracked · Mar 22, 2023 · N691CA · Cndair CL6002D24 · Passenger/Crew Doors
  > FOUND THE PAX DOOR CENTER BOTTOM SEAL RETAINER TO BE DAMAGED. REMOVED AND REPLACED IAW CRJ 900 SRMS 51-42-06-001-001-A01 AND 52-11-07-201-001-A01 REPAIR TYPE 2.
- [SDR REXA2022032400266](https://openairdocs.org/sdr/REXA2022032400266.md): Intercostal · cracked · Mar 9, 2023 · N691CA · Cndair CL6002D24 · Fuselage Main, Structure
  > WHILE PERFORMING SB 670BA-53-044 REVISION G DATED JUL05/2022 FOUND INTERCOSTAL GC213-00021-7 TO BE BENT AND CRACKED. 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 REXA2022100402178](https://openairdocs.org/sdr/REXA2022100402178.md): Former · corroded · Oct 2, 2022 · N691CA · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR FWD FORMER IS CORRDED. REMOVED AND REPLACED FWD FORMER IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01
- [SDR REXA2022100402187](https://openairdocs.org/sdr/REXA2022100402187.md): Stringer · corroded · Sep 30, 2022 · N691CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON STGR 26R BETWEEN FS 1015-1031. REPAIRED IAW ENDEAVOR EA CRJ953-14232 REV. A DATED 8/8/2022.
- [SDR REXA2022100402186](https://openairdocs.org/sdr/REXA2022100402186.md): Stringer · corroded · Sep 30, 2022 · N691CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON STGR 26R BETWEEN FS 1051.30-1069.75 REPAIRED IAW ENDEAVOR EA CRJ953-14233 REV. A DATED 8/8/2022.
- [SDR REXA2022100402185](https://openairdocs.org/sdr/REXA2022100402185.md): Stringer · corroded · Sep 30, 2022 · N691CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON STRINGER 23R BETWEEN F.S. 333.00 TO F.S. 379.00. REMOVED AND REPLACED IAW CRJ 900 SRMS 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-21-001-001-A01.
- [SDR REXA2022100402184](https://openairdocs.org/sdr/REXA2022100402184.md): Stringer · corroded · Sep 30, 2022 · N691CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON STRINGER 23R BETWEEN F.S. 280.00 TO F.S. 333.00. REMOVED AND REPLACED IAW CRJ 900 SRMS 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-21-001-001-A01.
- [SDR REXA2022100402183](https://openairdocs.org/sdr/REXA2022100402183.md): Splice · corroded · Sep 30, 2022 · N691CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON SPLICE AT 23R AT F.S. 333. REMOVED AND REPLACED IAW CRJ 900 SRMS 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-21-001-001-A01.
- [SDR REXA2022100402182](https://openairdocs.org/sdr/REXA2022100402182.md): Angle · corroded · Sep 30, 2022 · N691CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > L/H FLOOR SILL ANGLE IS CORRODED BETWEEN F.S.720 TO F.S.847. REPAIRED IAW ENDEAVOR EA CRJ953-14337 REV IR DATED 8/10/22.
- [SDR REXA2022100402181](https://openairdocs.org/sdr/REXA2022100402181.md): None · corroded · Sep 30, 2022 · N691CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > RH SIDE SEAT RAIL BETWEEN FS 469-483 HAS MULTIPLE SPOTS OF CORROSION. REMOVED AND REPLACED IAW CRJ 900 SRM 53-00-49-201-002-A01 AND CRJ 900 AMM 53-00-49-400-801-A07.
- [SDR REXA2022100402180](https://openairdocs.org/sdr/REXA2022100402180.md): Stringer · corroded · Sep 30, 2022 · N691CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > STRINGER 24L IS CORRODED BETWEEN FS 501.00 AND 517.00. REMOVED AND REPLACED IAW CRJ 900 SRMS 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.
- [SDR REXA2022100402179](https://openairdocs.org/sdr/REXA2022100402179.md): Frame · corroded · Sep 30, 2022 · N691CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FRAME IS CORRODED AT FS 485.00 BETWEEN STGR 24L AND 26R. REPAIRED IAW ENDEAVOR EA CRJ953-14201 ISSUE DATE 8/3/2022 REV IR
- [SDR REXA2022100302160](https://openairdocs.org/sdr/REXA2022100302160.md): Stiffener · cracked · Sep 29, 2022 · N691CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > LBL 27 FS 280 BULKHEAD STIFFENER CRACKED. REMOVED AND REPLACED STIFFENER IAW CRJ 900 SRMS
- [SDR REXA2022093002154](https://openairdocs.org/sdr/REXA2022093002154.md): Angle · cracked · Sep 28, 2022 · N691CA · Cndair CL6002D24 · Vertical Stabilizer
  > L/H VERTICAL STAB AFT DRAG ANGLE CRACKED. REMOVED AND REPLACED IAW CRJ 900 SRMS 51-40-11-001-001-A01, 51-42-13-001-001-A01, 51-42-21-001-001-A01, AND 51-42-22-001-001-A01.
- [SDR REXA2022092602143](https://openairdocs.org/sdr/REXA2022092602143.md): Web · corroded · Sep 21, 2022 · N691CA · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR FWD WEB STRUCTURE IS CORRODED. REPLACED FWD WEB STIFFNERS 6EA, TEE- STIFFNERS, GAS SPRING BEAM AND STOW CUP IAW CRJ900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01
- [SDR REXA2022092602140](https://openairdocs.org/sdr/REXA2022092602140.md): None · corroded · Sep 21, 2022 · N691CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > LH SIDE SEAT RAIL STRUCTURE BETWEEN FS 661+8-670 HAS MULTIPLE SPOTS OF CORROSION INSTALLED NEW SIDE SEAT RAIL P/N SH 690-36283-1 ON L/H BETWEEN F.S661+8 TO F.S670 WL 85.25 IAW CRJ AMM 53-00-49-400-801-CONFIG A07
- [SDR REXA2022092602139](https://openairdocs.org/sdr/REXA2022092602139.md): Intercostal · corroded · Sep 21, 2022 · N691CA · Cndair CL6002D24 · Fuselage Main, Structure
  > NOSE JACK PAD FITTING RH INTERCOSTAL CORRODED JUST FWD OF FS 280.00 REPAIRED IAW ENDEAVOR EA CRJ953-14245 REV IR DATED 8/3/22.
- [SDR REXA2022092602138](https://openairdocs.org/sdr/REXA2022092602138.md): Intercostal · corroded · Sep 21, 2022 · N691CA · Cndair CL6002D24 · Fuselage Main, Structure
  > NOSE JACK PAD FITTING LH INTERCOSTAL CORRODED JUST FWD OF FS 280.00 REPAIRED IAW ENDEAVOR EA CRJ953-14244 REV IR DATED 8/3/22.
- [SDR REXA2022092202122](https://openairdocs.org/sdr/REXA2022092202122.md): None · corroded · Sep 20, 2022 · N691CA · Cndair CL6002D24 · Emergency Exits
  > RH SIDE SEAT RAIL BETWEEN FS 677-720 HAS MULTIPLE SPOTS OF CORROSION. INSTALLED SIDE SEAT RAIL SH690-36284-1 IAW CRJ 900 AMM 53-00-49-400-801-A07
- [SDR REXA2022092202121](https://openairdocs.org/sdr/REXA2022092202121.md): None · corroded · Sep 20, 2022 · N691CA · Cndair CL6002D24 · Emergency Exits
  > RH SIDE SEAT RAIL BETWEEN FS 571-661+13 HAS MULTIPLE SPOTS OF CORROSION. REPLACED SEAT RAIL IAW CRJ900 AMM 53-00-49-400-801-A07 AND SRM 51-40-11-001-001-A01
- [SDR REXA2022092002112](https://openairdocs.org/sdr/REXA2022092002112.md): Frame · cracked · Sep 19, 2022 · N691CA · Cndair CL6002D24 · Emergency Exits
  > R/H AFT OVERWING EXIT DOOR (S/N SBO538) TOP EDGE MEMBER IS CRACKED. REPAIRED IAW EA CRJ952-14361 REV-IR DATED: 8/26/2022.
- [SDR REXA2022092602142](https://openairdocs.org/sdr/REXA2022092602142.md): Cleat · corroded · Sep 18, 2022 · N691CA · Cndair CL6002D24 · Passenger/Crew Doors
  > INTERCOSTAL DD6 AT AFT SIDE CLEAT FOUND TO BE CORRODED. REMOVED AND INSTALLED NEW SERVICEABLE INTERCOSTAL DD6 CLEAT AT AFT SIDE IAW CRJ 900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.
- [SDR REXA2022092102132](https://openairdocs.org/sdr/REXA2022092102132.md): Angle · worn · Sep 18, 2022 · N691CA · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR AFT DRAG ANGLE HAS ELONGATED HOLES LOCATED, DRILLED AND INSTALLED PAX DOOR DRAG ANGLE TO AFT WEB IAW CRJ900 SRM 52-40-11-001-001-A01, SRM 51-42-06-001-001-A01.
- [SDR REXA2022092102131](https://openairdocs.org/sdr/REXA2022092102131.md): Angle · corroded · Sep 18, 2022 · N691CA · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR, FWD WEB DRAG ANGLE IS CORRODED. LOCATED, DRILLED, AND INSTALLED A NEW SERVICEABLE FWD DRAG ANGLE IAW CRJ900 SRM 51-40-11-001-001-A01, AND 51-42-06-001-001-A01
- [SDR REXA2022092102130](https://openairdocs.org/sdr/REXA2022092102130.md): Panel · corroded · Sep 18, 2022 · N691CA · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR, TOP STEP CORRODED.. LOCATED AND DRILLED NEW TOP PANEL P/N 601R317075-3 IAW CRJ-900 SRM 51-40-11-001-001-A01.
- [SDR REXA2022092102129](https://openairdocs.org/sdr/REXA2022092102129.md): Angle · corroded · Sep 18, 2022 · N691CA · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR ANGLE DD7A CORRODED. LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE ANGLE PN 601R317052-1 IAW CRJ 900 SRM 51-40-11-001-001-A01 AND 51-42-21-001-001-A01
- [SDR REXA2022092102126](https://openairdocs.org/sdr/REXA2022092102126.md): Stringer · corroded · Sep 18, 2022 · N691CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > MULTIPLE AREAS OF CORROSION ON STRINGER 25R BETWEEN F.S. 308.00 TO F.S. 319.00. REMOVED STRINGER 25R FROM F.S. 280-F.S.333 IAW CRJ900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01. INSTALLED STGR 25R FROM FS280 TO FS 333 IAW CRJ 900 SRM 51-42-06-001-00
- [SDR REXA2022092102125](https://openairdocs.org/sdr/REXA2022092102125.md): Stringer · corroded · Sep 18, 2022 · N691CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > MULTIPLE AREAS OF CORROSION FOUND ON STRINGER 24R BETWEEN F.S. 295.00 TO F.S. 349.00. REMOVED AND REPLACED STGR 24R BTW FS 280-333 IAW CRJ900 SRM 51-42-06-0001-001-A01.

Next page: https://openairdocs.org/aircraft/N691CA/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 = 'N691CA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N691CA/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.