# Service difficulty reports: N655CA

A list on [N655CA](https://openairdocs.org/aircraft/N655CA.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 6 · 288 reports

- [SDR REXA2026030900231](https://openairdocs.org/sdr/REXA2026030900231.md): Lamp · inoperative · Mar 7, 2026 · N655CA · Cndair CL6002C10 · Emergency Lighting
  > EMERGENCY LIGHT BULB IN OVERHEAD PANEL 263ALC BURNED OUT. RELAMPED IAW CRJ 700 AMM 33-51-09. OPS CHECK GOOD. P/N OFF/ON=1317
- [SDR REXA2025100200898](https://openairdocs.org/sdr/REXA2025100200898.md): Control Unit · inoperative · Sep 28, 2025 · N655CA · Cndair CL6002C10 · Brake Anti-Skid Section
  > BRAKE OVERHEAT WARNING MESSAGE POSTED ON ARRIVAL AT 7,000! COMPLETED EMERGENCY CHECKLIST AND QRH PROCEDURE. RH OB BRAKE TEMP SENSOR WAS RED AND 00, DEFERRING BRAKE TEMP SENSOR IAW 32-46-1D MM02 UPDATED, PLACARD INSTALLED. ALL MAINTENANCE PROCEDURE COMPLIED WI
- [SDR REXA2025081300805](https://openairdocs.org/sdr/REXA2025081300805.md): Sensor · inoperative · Aug 11, 2025 · N655CA · Cndair CL6002C10 · Landing Gear Brake System
  > BRAKE OVHT WARNING AT 8000' 250 KTS WITH RT OTBD INDICATOR AT 00. FOLLOWED CHECKLIST AND LOWERED GEAR. NO CHANGE. UPON LANDING INDICATOR NEVER WENT ABOVE 02. R&R RHOB BRAKE TEMP SENSOR IAW AMM 32-46-01. OPS CHECK GOOD.
- [SDR REXA2023112000995](https://openairdocs.org/sdr/REXA2023112000995.md): Lamp · inoperative · Nov 19, 2023 · N655CA · Cndair CL6002C10 · Emergency Lighting
  > UPON OPS CHECK OF EMERGENCY LIGHTS FOUND LIGHT AFT OF PAX DOOR TO BE INOP AND REQUIRES REPLACEMENT PN: 8GH002473-08 REPLACED EMERGENCY LIGHT AFT OF PAX DOOR IAW CRJ 700 AMM 33-51-15-400-801-A01 & 33-51-15-710-801-A01
- [SDR REXA2023112000993](https://openairdocs.org/sdr/REXA2023112000993.md): Striker · corroded · Nov 19, 2023 · N655CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > GALLEY DOOR BOTTOM SILL STRIKER IS CORRODED AROUND FASTENER HOLES. REMOVED GALLEY DOOR BOTTOM SILL STRIKER IAW CRJ 700 SRM 51-42-06-001-001-A01. LOCATED AND DRILLED GALLEY DOOR BOTTOM SILL STRIKER IAW CRJ-700 SRM 51-40-11-001-001-A01 INSTALLED NEW SERVICEABLE
- [SDR REXA2023112000992](https://openairdocs.org/sdr/REXA2023112000992.md): Bracket · corroded · Nov 19, 2023 · N655CA · Cndair CL6002C10 · Main Landing Gear
  > MLG LOCK ACTUATOR HYDRAULIC LINE BRACKET IN RH WHEEL WELL CORRODED. REMOVED CORRODED R/H MLG WHEEL WELL HYDRAULIC LINE INTERFACE BRACKET AND INSTALLED NEW SERVICABLE BRACKET IAW CRJ 700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
- [SDR REXA2023112000991](https://openairdocs.org/sdr/REXA2023112000991.md): Bracket · corroded · Nov 19, 2023 · N655CA · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > LH MLG WHEEL WELL HYDRAULIC INTERFACE BRACKET (LOWER) CORRODED AT APPROX LBL45 AND FS797 REMOVED CORRODED L/H MLG WHEEL WELL HYDRAULIC LINE INTERFACE BRACKET AND INSTALLED NEW SERVICABLE BRACKET IAW CRJ 700 SRM 51-42-06-001-001-A01.
- [SDR REXA2023112000990](https://openairdocs.org/sdr/REXA2023112000990.md): Retainer · corroded · Nov 19, 2023 · N655CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > AVI DOOR FWD R/H SEAL RETAINER IS CORRODED. REMOVED SEAL RETAINER IAW CRJ- 700-SRM-51-42-06-001-001-A01. LOCATED, DRILLED AND INSTALLED NEW SEAL RETAINER P/N CC670-38663-5 IAW CRJ-700-SRM-51-40-11-001-001-A01 AND 51-42-06-001-001-A01.
- [SDR REXA2024011200069](https://openairdocs.org/sdr/REXA2024011200069.md): Skin · chafed · Nov 18, 2023 · N655CA · Cndair CL6002C10 · Ailerons
  > FOUND LOWER OB FIXED LEADING EDGE OF LH AILERON TO BE CHAFED REMOVED LOWER OB FIXED LEADING EDGE SKIN ATTACHED TO LH AILERON IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. LOCATED AND DRILLED LOWER OB FIXED LEADING EDGE SKIN PN: CC670-13054-1 A
- [SDR REXA2024011200068](https://openairdocs.org/sdr/REXA2024011200068.md): Floor Support · corroded · Nov 17, 2023 · N655CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > R/H FLOOR SILL IS CORRODED BETWEEN F.S. 280 TO F.S. 295. REMOVED R/H FLOOR SILL BETWEEN FS 280 TO 310 IAW CRJ-700 SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01, AND 51-42-21-001-001-A01. LOCATED AND DRILLED NEW SERVICEABLE R/H FLOOR SILL (P/N SH670-32172-5) F
- [SDR REXA2024102501006](https://openairdocs.org/sdr/REXA2024102501006.md): Bracket · cracked · Nov 1, 2023 · N655CA · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR BRACKET CRACKED AT APPROX FS323 UNDER ACCESS PANEL 832AB. LOCATED, MATCH DRILLED AND INSTALLED NEW SERVICEABLE BRACKET P/N 601R31902-556 IAW CRJ 700 SRM 51-41-04-001-001-A01 AND 51-40-11-001-001-A01.
- [SDR REXA2024022600213](https://openairdocs.org/sdr/REXA2024022600213.md): Web · corroded · Nov 1, 2023 · N655CA · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR FWD WEB IS CORRODED IN MULTIPLE LOCATIONS AROUND PANELS. LOCATED, MATCH DRILLED AND INSTALLED NEW SERVICEABLE FWD STAIR WEB PN 601R317071-12S IAW CRJ 700 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.
- [SDR REXA2024110101357](https://openairdocs.org/sdr/REXA2024110101357.md): Stringer · corroded · Oct 30, 2023 · N655CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER 21R IS CORRODED BETWEEN FS 319.00 AND 333.00. REMOVED CORRODED STRINGER FROM F.S. 280 TO F.S. 333. INSTALLED A SERVICEABLE STRINGER, P/N SH670-31636-1. IAW CRJ-700 SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01.
- [SDR REXA2024102501005](https://openairdocs.org/sdr/REXA2024102501005.md): Stringer · corroded · Oct 27, 2023 · N655CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER CORRODED AT STGR20R BETWEEN FS364 AND FS394. INSTALLED 2 SECTIONS OF NEW STGR 20R P/N SH670-31405-2 BETWEEN FS 364 TO FS 469, IAW CRJ700 SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01 AND ENDEAVOR AIR EA CRJ753-15613
- [SDR REXA2024102500959](https://openairdocs.org/sdr/REXA2024102500959.md): Angle · cracked · Oct 27, 2023 · N655CA · Cndair CL6002C10 · Passenger/Crew Doors
  > PASSENGER DOOR INNER HANDLE ANGLE Ï¿½CÏ¿½ FOUND TO BE CRACKED LOCATED DRILLED AND INSTALLED NEW SERVICEABLE ANGLE Ï¿½CÏ¿½ P/N:601R318072-1 ON SAME SERVICEABLE INNER HANDLE ASSY IAW CRJ700 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01
- [SDR REXA2024102500958](https://openairdocs.org/sdr/REXA2024102500958.md): Cleat · corroded · Oct 26, 2023 · N655CA · Cndair CL6002C10 · Passenger/Crew Doors
  > PASSENGER DOOR CLEAT BETWEEN DD6 AND FRAME FOUND TO BE CORRODED LOCATED DRILLED AND INSTALLED NEW SERVICEABLE PASSENGER DOOR CLEAT ON FWD SIDE DD6 AND FRAME P/N:600-31902-269 IAW CRJ700 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01
- [SDR REXA2022102700935](https://openairdocs.org/sdr/REXA2022102700935.md): Angle · corroded · Oct 26, 2023 · N655CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > PASSENGER DOOR MID CAP ANGLE IS CORRODED REMOVED MID CAP ANGLE IAW CRJ700 SRM 51-41-02-001-001-A01 AND INSTALLED NEW MID CAP ANGLE P/N SH670-31825-9S IAW CRJ-700 SRM 51-41-02-001-001-A01.
- [SDR REXA2022102700932](https://openairdocs.org/sdr/REXA2022102700932.md): Former · corroded · Oct 26, 2023 · N655CA · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR FORMER CORRODED AT FS329.41 AND BETWEEN DD5 AND DD6 REMOVED FORMER IAW CRJ 700 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01. LOCATED AND DRILLED NEW SERVICEABLE FORMER AT FS 329.41 BETWEEN DD6 AND DD5 P/N 601R318078-3 IAW CRJ 700 SRM 51-40-1
- [SDR REXA2022102700931](https://openairdocs.org/sdr/REXA2022102700931.md): Panel · corroded · Oct 26, 2023 · N655CA · Cndair CL6002C10 · Passenger/Crew Doors
  > PASSENGER DOOR TOP STEP PANEL CORRODED. REMOVED AND REPLACED PASSENGER DOOR TOP STEP P/N 601R317075-3
- [SDR REXA2022102700933](https://openairdocs.org/sdr/REXA2022102700933.md): Panel · corroded · Oct 25, 2023 · N655CA · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR AFT WEB IS CORRODED. LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE AFT STAIR WEB PN 601R317071-11 IAW CRJ 700 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001- A01
- [SDR REXA2022102700919](https://openairdocs.org/sdr/REXA2022102700919.md): Hinge · damaged · Oct 25, 2023 · N655CA · Cndair CL6002C10 · Fuselage, Door Hinge
  > "UPON REMOVAL OF PAX DOOR (REF. MWC HN00109662) FOUND ALL FUSELAGE SIDE PAX DOOR HINGE LUG INNER SURFACES TO BE WORN BEYOND THE.295"" ALLOWABLE LIMIT STATED IN CRJ 900 SRM 53-21-23-201-010-A01. REMOVED AND REPLACED PASSENGER DOOR HINGE (FUSELAGE SIDE) IAW CRJ
- [SDR REXA2022102600915](https://openairdocs.org/sdr/REXA2022102600915.md): Channel · cracked · Oct 25, 2023 · N655CA · Cndair CL6002C10 · Engine Thrust Reverser
  > LH UPPER TRANS-COWL LATCH COAMING CHAFED. LATCH DOOR AFT C CHANNEL PN: CN624-2048-201 CRACKED AND GOUGED BEYOND LIMITS. REPLACE. LOCATED AND DRILLED NEW SERVICEABLE PART P/N CN624-2048-201 IAW CRJ700 SRM 51-41-11-001-001-A01 AND INSTALLED IAW CRJ700 SRM 51
- [SDR REXA2022102600914](https://openairdocs.org/sdr/REXA2022102600914.md): Doubler · chafed · Oct 25, 2023 · N655CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > "LH UPPER TRANS-COWL LATCH COAMING CHAFED. FABRICATED NEW SERVICEABLE LATCH DOOR COAMING DOUBLER FROM 2024-T42 0.063"" ALUMINUM SHEET PO# W91989, IAW CRJ 700 SRM 51-24-36-001-001-A01 AND 51-24-21-001-001-A01, AND 51-40-11-001-001-A01. REFERENCED DRAWING CN624-
- [SDR REXA2024102501004](https://openairdocs.org/sdr/REXA2024102501004.md): Retainer · cracked · Oct 24, 2023 · N655CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > PAX DOOR MID AFT SEAL RETAINER FOUND TO BE CRACKED LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE PAX DOOR AFT MID SEAL RETAINER IAW CRJ 700 SRM 51-40-11-001-001-A01, SRM 51-42-06-001-001-A01 AND SRM 51-42-13-001-001-A01. P/N 601R318714-3
- [SDR REXA2024102501003](https://openairdocs.org/sdr/REXA2024102501003.md): Intercostal · corroded · Oct 24, 2023 · N655CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > PAX DOOR DD4 INTERCOSTAL CORRODED BETWEEN FS311.75 AND FS320.163 LOCATED DRILLED AND INSTALLED NEW SERVICEABLE PAX DOOR FWD INTERCOSTAL AT DD4 P/N:601R318093-1 IAW CRJ700 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01
- [SDR REXA2024110101355](https://openairdocs.org/sdr/REXA2024110101355.md): Angle · cracked · Oct 23, 2023 · N655CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > L/H AFT SIDE OF F.S. 280 BULKHEAD 4TH FROM BOTTOM STIFFENER ANGLE IS CRACKED. REPAIRED IAW ENDEAVOR AIR EA# CRJ753-15671, REV B, DATED 10/22/2023.
- [SDR REXA2024102500957](https://openairdocs.org/sdr/REXA2024102500957.md): Intercostal · corroded · Oct 23, 2023 · N655CA · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR DD5 INTERCOSTAL CORRODED BETWEEN FS335.963 AND FS347.25 LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE PAX DOOR DD5 INTERCOSTAL BETWEEN FS 335.963 AND FS 347.25 IAW CRJ 700 SRM 51-40-11-001-001-A01 AND SRM 51-42-06-001-001-A01.
- [SDR REXA2024102500956](https://openairdocs.org/sdr/REXA2024102500956.md): Intercostal · corroded · Oct 23, 2023 · N655CA · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR DD1A INTERCOSTAL CORRODED BETWEEN FS 335.963 AND FS 347.25 LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE PAX DOOR AFT DD1A INTERCOSTAL BETWEEN FS 335.963 AND FS 347.25 P/N 601R31902-317A IAW CRJ 700 SRM 51-40-001-001-A01 AND SRM 51-42-06-001-001-A01.
- [SDR REXA2022102600916](https://openairdocs.org/sdr/REXA2022102600916.md): Plate · chafed · Oct 20, 2023 · N655CA · Cndair CL6002C10 · Passenger/Crew Doors
  > PASSENGER DOOR AFT UPPER CENTERING PLATE IS CHAFED. PASSENGER DOOR UPPER CENTERING PLATE IS HEAVILY CHAFED AND DAMAGE MEASURE.053 DEEP. UPPER CENTERING PLATE IS OUT OF REPAIRABLE LIMITS OF CRJ 700 SRM 52-11-06-201-001-A01 AND REQUIRES REPLACEMENT. LOCATED,
- [SDR REXA2022102600906](https://openairdocs.org/sdr/REXA2022102600906.md): Intercostal · corroded · Oct 20, 2023 · N655CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > PASSENGER DOOR DD5 INTERCOSTAL CORRODED BETWEEN FS311.75 AND FS320.163 REPAIRED PASSENGER DOOR DD5 INTERCOSTAL CORRODED BETWEEN FS311.75 AND FS320.163 IAW ENDEAVOR EA CRJ752-15628
- [SDR REXA2024102501002](https://openairdocs.org/sdr/REXA2024102501002.md): Intercostal · corroded · Oct 19, 2023 · N655CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > INTERCOSTAL 20R BETWEEN FS 349 AND FS 364 IS HEAVILY CORRODED INSTALLED NEW INTERCOSTAL P/N: SH670-31994-1. STRG# 20 ON F.S. 349. TO F.S. 364 IAW CRJ 900 SRM 51-42-06-001-001-A01. AND SRM 51-42-21-001-001-A01.
- [SDR REXA2024102500955](https://openairdocs.org/sdr/REXA2024102500955.md): Handle · cracked · Oct 19, 2023 · N655CA · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR INNER HANDLE IS CRACKED REMOVED CRACKED INNER HANDLE. LOCATED DRILLED AND INSTALLED NEW SERVICEABLE INNER HANDLE PN 600-31887-15 IAW CRJ 700 SRM 51-40-11-001-001-A01 AND AMM 52-11-02-400-809-A01.
- [SDR REXA2022102700926](https://openairdocs.org/sdr/REXA2022102700926.md): Bracket · corroded · Oct 19, 2023 · N655CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FWD BAGGAGE BAY, MACHINED BRACKET CORRODED AT APPROX FS533 AND LBL24 INSTALLED BRACKET,MACHINED P/N SH670-33390-1 AT FWD BAGGAGE BAY FS 533, LBL 24, IAW CRJ-700 SRM 51-42-21-001-001-A01
- [SDR REXA2022102700923](https://openairdocs.org/sdr/REXA2022102700923.md): Stringer · corroded · Oct 19, 2023 · N655CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STGR 21R IS CORRODED BETWEEN FS 364 AND FS 379 INSTALLED NEW STRINGER 21R F.S. 333 TO F.S. 379 IAW CRJ-700 SRM 51-42-06-001-001-A01
- [SDR REXA2024110101354](https://openairdocs.org/sdr/REXA2024110101354.md): Web · damaged · Oct 17, 2023 · N655CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > LH FS280 - REMAINING PORTION OF LOWER WEB HAS MULTIPLE SHEARED FASTENERS AND POSSIBLE INCORRECT OR ALTERNATE FASTENERS INSTALLATED AT THE COCKPIT FLOOR. COMPLIED WITH ALL STEPS OF REO 670-53-11-1892 REV -- 2023-10-06.
- [SDR REXA2024110101353](https://openairdocs.org/sdr/REXA2024110101353.md): Web · damaged · Oct 17, 2023 · N655CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > RH FS280 - REMAINING PORTION OF LOWER WEB HAS MULTIPLE SHEARED FASTENERS AND POSSIBLE INCORRECT OR ALTERNATE FASTENERS INSTALLATED AT THE COCKPIT FLOOR. COMPLIED WITH ALL STEPS OF REO 670-53-11-1892 REV -- 2023-10-06.
- [SDR REXA2024110101352](https://openairdocs.org/sdr/REXA2024110101352.md): Floorbeam · corroded · Oct 17, 2023 · N655CA · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > LEFT, RIGHT, AND CENTER 280 CROSSBEAM CORRODED AT TOP CAP AS MARKED. REMOVED CORRODED F.S. 280 CROSSBEAM AND INSTALLED A NEW F.S. 280 CROSSBEAM P/N CC670-34175-7. IAW CRJ-700 SRM 53-11-41-201-003-A01.
- [SDR REXA2024102501001](https://openairdocs.org/sdr/REXA2024102501001.md): Support · chafed · Oct 16, 2023 · N655CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > "AFT CARGO DOOR TRACK SUPPORT CROSSBEAM IS CHAFED FROM LIFT CABLES. TRIMMED TO FIT NEW CROSSBEAM AND DRILLED UP NEW FASTERNER HOLES AS REQUIRED AFTER HEAT TREAT PROCESS FOR SUPPORT CROSSBEAM PART # MM670-35502-6 FROM.063"" 7075-""T-6"" MATERIAL (AFTER HEAT TR
- [SDR REXA2024110601425](https://openairdocs.org/sdr/REXA2024110601425.md): Bracket · corroded · Oct 15, 2023 · N655CA · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR DD6 BRACKET FOUND TO BE CORRODED. LOCATED DRILLED AND INSTALLED NEW SERVICEABLE BRACKET ON FWD INTERCOSTAL DD6 P/N:601R318084-1 IAW CRJ700 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.
- [SDR REXA2024110101351](https://openairdocs.org/sdr/REXA2024110101351.md): Floorbeam · cracked · Oct 15, 2023 · N655CA · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > FS 280 CROSSBEAM FLOOR PANEL SUPPORT ANGLE (J ANGLE) IS CRACKED ON BOTH R/H AND L/H SIDE, REQUIRES REPLACEMENT. LOCATED AND DRILLED REPLACEMENT FLOOR CHANNEL SUPPORT PN CC670-33292-13 IAW CRJ 700 SRM 51-40-11-001-001-A01. REF. BARCODE IDENTIFIER HN110081 FOR I
- [SDR REXA2024110101350](https://openairdocs.org/sdr/REXA2024110101350.md): Angle · corroded · Oct 15, 2023 · N655CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > WEB FLOOR PROTECTORS (4EA) ON GALLEY DOOR SILL CORRODED. REPLACED 4 EACH ANGLES P/N SH670-31982-1 AND ATTACHED TO 4 EACH WEB PROTECTOR MOUNTS IAW CRJ 700 SRM 5123-00-001-001-A01 AND IAW CRJ 700 SRM 51-40-11-001-001-A01.
- [SDR REXA2024102501000](https://openairdocs.org/sdr/REXA2024102501000.md): Former · corroded · Oct 15, 2023 · N655CA · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR AFT FORMER AT FS 347.27 IS CORRODED ON INNER FLANGE AT DD6 INTERCOSTAL. INSTALLED NEW SERVICEABLE PAX DOOR AFT FORMER P/N 601R318034-5S AT FS 347.27 IAW CRJ 700 SRM 51-42-06-001-001-A01.
- [SDR REXA2022102700927](https://openairdocs.org/sdr/REXA2022102700927.md): Stringer · corroded · Oct 14, 2023 · N655CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER 24R HAS SEVERAL AREAS OF CORROSION ON UPPER SURFACE OF ATTACHED FLANGE BETWEEN FS280.00 AND FS319.70. LOCATED AND DRILLED NEW SERVICEABLE STRINGER 24R PN: SH670-31212-2U BETWEEN FS 280 TO 333 IAW CRJ 700 SRM 51-40-11-001-001-A01 AND INSTALLED STR. 24
- [SDR REXA2022102700924](https://openairdocs.org/sdr/REXA2022102700924.md): Nut Plate · corroded · Oct 14, 2023 · N655CA · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > NUT PLATE BRACKET IS CORRODED AT FS 533, STRINGER 25R REMOVED AND INSTALLED NEW SERVICEABLE NUT PLATE BRACKET (PLATE) PN SH670-34081-11 AT F.S.533 STRINGER 25R.
- [SDR REXA2022102700928](https://openairdocs.org/sdr/REXA2022102700928.md): Gusset · deformed · Oct 13, 2023 · N655CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > GUSSET P/N CC670-33467-2 AT FS280.00, RBL 11.0 HAS AN ELONGATED HOLE. INSTALLED NEW SERVICEABLE GUSSET P/N CC670-33467-2 AT FS280.00, RBL 11.0 IAW CRJ 700 SRM 51-42-06/21-001-001.
- [SDR REXA2022101900900](https://openairdocs.org/sdr/REXA2022101900900.md): Stringer Splice · corroded · Oct 13, 2023 · N655CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER 24R JOINT PIECE HEAVILY CORRODED AT FS333 LOCATED AND DRILLED NEW SERVICEABLE STRINGER 24R SPLICE PN: SH670-32429-4S AT FS 333 IAW CRJ 700 SRM 51-40-11-001-001-A01 AND INSTALLED NEW STR 24R JOINT PIECE AT FS333 IAW CRJ 700 SRM 51-42-06-001-001-A01 AND
- [SDR REXA2022101300880](https://openairdocs.org/sdr/REXA2022101300880.md): Strap · corroded · Oct 12, 2023 · N655CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > AFT BELLY FAIRING SUPPORT STRUCTURE AT FS 879 SHOWS SINGES OF CORROSION ON PANEL MATING SURFACE, SPLICE AND PEALING PAINT ON UPR ATTACH ANGLES BETWEEN LBL 45 TO RBL 45. FABRICATED 1 EA. LEFT HAND STRAP AND DRILLED UP (FABRICATED OUT OF ALLOY 2024T-3.032 P0 # G
- [SDR REXA2022101300879](https://openairdocs.org/sdr/REXA2022101300879.md): Strap · corroded · Oct 12, 2023 · N655CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > AFT BELLY FAIRING SUPPORT STRUCTURE AT FS 879 SHOWS SIGNS OF CORROSION ON PANEL MATING SURFACE, SPLICE AND PEALING PAINT ON UPR ATTACH ANGLES BETWEEN LBL 45 TO RBL 45. FABRICATED 1 EA. RIGHT HAND STRAP AND DRILLED UP (FABRICATED OUT OF ALLOY 2024T-3.032 P0 # G
- [SDR REXA2022101300875](https://openairdocs.org/sdr/REXA2022101300875.md): Stringer · corroded · Oct 11, 2023 · N655CA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > STGR 27 IS CORRODED BETWEEN FS 517 AND FS 533. RECEIVED NEW STGR 27 P/N SH670-33237-3A, LOCATED AND DRILLED ON PLACE AT STGR 27 IAW CRJ700 SRM 51-40-11-001-001-A01 AND INSTALLED STRINGER 27 WITH P/N SH670-33237-3A FROM FS517 THRU FS645 IAW CRJ700 SRM 51-42-06
- [SDR REXA2022101300874](https://openairdocs.org/sdr/REXA2022101300874.md): Stringer · corroded · Oct 11, 2023 · N655CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STGR 25L IS CORRODED BETWEEN FS 485 AND FS 501. INSTALLED NEW STRINGER AT STGR 25L BETWEEN FS 469 AND FS 485,BETWEEN FS 501 AND FS 517. IAW CRJ700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01

Next page: https://openairdocs.org/aircraft/N655CA/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 = 'N655CA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N655CA/reports

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