# Service difficulty reports: N317CA

A list on [N317CA](https://openairdocs.org/aircraft/N317CA.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 · 275 reports

- [SDR REXA2026092501878](https://openairdocs.org/sdr/REXA2026092501878.md): Lamp · inoperative · Sep 24, 2026 · N317CA · Cndair CL6002C10 · Emergency Lighting
  > TWO EMERGENCY FLOODLIGHT LAMPS INOP. R & R THE LAMPS IAW AMM 33-51-05. OPS CHECKED GOOD.
- [SDR REXA2026073001336](https://openairdocs.org/sdr/REXA2026073001336.md): Lamp · inoperative · Jul 29, 2026 · N317CA · Cndair CL6002C10 · Emergency Lighting
  > 5 EMERGENCY FLOODLIGHT LAMPS INOP. R+R 5 EMERGENCY FLOODLIGHT LAMPS P/N OL3071BPE/GPL REF AMM 33-51-05. OPS CHECK GOOD.
- [SDR REXA2026062900982](https://openairdocs.org/sdr/REXA2026062900982.md): Strut · disconnected · Jun 28, 2026 · N317CA · Cndair CL6002C10 · Service Doors
  > GALLEY SERVICE DOOR WILL NOT OPEN FROM INSIDE OR OUTSIDE FOUND SERVICE DOOR UPLOCK STRURT DISCONNECTED RECONNECTED UPLOCK STRUT ASSY IAW AMM 52-41-02. CHECKED GOOD. OK FOR SVC
- [SDR REXA2026050400447](https://openairdocs.org/sdr/REXA2026050400447.md): Hinge · damaged · Apr 26, 2026 · N317CA · Cndair CL6002C10 · Fuselage, Door Hinge
  > PAX DOOR HINGE (FUSELAGE) FOUND OVERSIZED HOLES AT HINGE LINE RESULTING IN PAX DOOR NOT ALIGNING WHEN CLOSED. REQUIRED REPLACEMENT. REPLACED PAX DOOR HINGE (DFUSELAGE) ISW SRM 53-21-23.
- [SDR REXA2026050400446](https://openairdocs.org/sdr/REXA2026050400446.md): Hinge · damaged · Apr 26, 2026 · N317CA · Cndair CL6002C10 · Fuselage, Door Hinge
  > PAX DOOR HINGE (DOOR) DURING INSTALL PIN BECAME STUCK IN PIANO HINGE ON DOOR SIDE RESULTING IN PAX DOOR NOT ALIGNING WHEN CLOSED. REQUIRES REPLACEMNET. PN: 601R318073-5 REPLACED PAX DOOR HINGE (DOOR) IAW SRM 52-11-01
- [SDR REXA2025092300871](https://openairdocs.org/sdr/REXA2025092300871.md): Fadec · inoperative · Sep 18, 2025 · N317CA · Cndair CL6002C10 · Fuel Controlling System
  > AT FL 310 AND WE WERE TOLD TO DESCEND DOWN TO 11,00. WE HAD A R ENGINE FLAME OUT AND LOST OUT R ENGINE, R FADEC FAULT AND L FADEC FAULT STATUS MESSAGE CAME ON. OUR RIGHT ENGINE LIT BACK UP. R/L FADEC FAULT STATUS MSG CAME IN AND OUT ITERMITTENTLY. AFTER WE LAN
- [SDR REXA2025012300074](https://openairdocs.org/sdr/REXA2025012300074.md): Canister · leaking · Jan 19, 2025 · N317CA · Cndair CL6002C10 · Fuel Storage
  > FUEL LEAK AT LH WING SLAT TRACK CANISTER NO.3 (SLAT TRACK 1-3) WS 148.00, LH MAIN FUEL TANK FRONT SPAR. SLAT TRACK CANISTER NO.3 (SLAT TRACK 1-3) WS 148.00, LH MAIN FUEL TANK FRONT SPAR WAS REPAIRED REO 670-57-- 42-19 REV --
- [SDR REXA2025012300089](https://openairdocs.org/sdr/REXA2025012300089.md): Floor Support · corroded · Dec 6, 2024 · N317CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION ON BEAM BTW FS 985.00/ FS 1088.00 AND LBL 27 AT AFT CARGO FLOOR STRUCTURE FLOOR BEAM BTW FS 985.00/ FS 1069.75 AND LBL 27 WAS REPAIRED PER CRJ700 SRM 53-00-41-201-001-A01 AND FLOOR BEAM LBL 27 BTW FS 1069.75/FS 1088.00 WAS INSPECTED AND NO CORROSION
- [SDR REXA2025012300088](https://openairdocs.org/sdr/REXA2025012300088.md): Seat Track · corroded · Dec 6, 2024 · N317CA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > IN REF TO: AFTER SEAT RAIL REMOVAL DURING NRC: 0200, CORROSION ON FLOOR BEAM RBL 9 BTW FS= 477.00/565.00 WAS FOUND. CORROSION ON FLOOR BEAM RBL 9 BTW FS= 477.00/565.00 WAS EVALUATED PER CRJ700 SRM 53-31-43-101-001-A01 THEREFORE WAS REPAIRED PER CRJ-700 SRM 53
- [SDR REXA2025012300087](https://openairdocs.org/sdr/REXA2025012300087.md): Stringer · corroded · Dec 6, 2024 · N317CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > INITIAL INSPECTION: CORROSION ON STGR 19R BTW FS409 / FS349 (CPCP) STGR 19R BTW FS409 / FS349 WAS REPAIRED PER CRJ-700 SRM 53-00-03-201-001-A01
- [SDR REXA2025012300086](https://openairdocs.org/sdr/REXA2025012300086.md): Beam · chafed · Dec 6, 2024 · N317CA · Cndair CL6002C10 · Fuselage Main, Structure
  > WEAR WAS FOUND ON BEAM FWD AND AFT AREA AT CUTOUT OF AFT BAGGAGE BAY DOOR BEAM FWD AND AFT AREA AT CUTOUT OF AFT BAGGAGE BAY DOOR WAS REPAIRED PER EA CRJ753-18112 REV. IR
- [SDR REXA2025012300085](https://openairdocs.org/sdr/REXA2025012300085.md): Stringer · corroded · Dec 6, 2024 · N317CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STGR 19L BTW FS364 / FS379 (CPCP) CORROSION ON STGR 19L BTW FS364 / FS379 (CPCP) WAS EVALUATED OUT LIMITS PER CRJ 700 SRM 51-10-06-001-001-A01 THEREFORE WAS REPAIRED PER CRJ-700 SRM 53-00-03-201-001-A01
- [SDR REXA2025012300084](https://openairdocs.org/sdr/REXA2025012300084.md): Skin · cracked · Dec 6, 2024 · N317CA · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > CRACK IN LH FWD FUSELAGE SKIN LOCATED IN WL 79.5 AND F.S. 189.5 AT AFT LOWER CORNER OF CUTOUT ACCESS PANEL 211AL LH FWD FUSELAGE SKIN LOCATED IN WL 79.5 AND F.S. 189.5 AT AFT LOWER CORNER OF CUTOUT ACCESS PANEL 211AL WAS REPAIRED PER REO 670-53-11-2068 REV --
- [SDR REXA2025012300083](https://openairdocs.org/sdr/REXA2025012300083.md): Stringer · corroded · Dec 4, 2024 · N317CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION OVER STGR 20R BTW FS 295 / FS 310 CORROSION OVER STGR 20R BTW FS 295 / FS 310 WAS REMOVED PER CRJ-700 SRM 51-21-06-001-001-A01 AND WAS EVALUATED OUT LIMITS PER CRJ-700 SRM 53-21-03-101-002-A01 THEREFORE STGR 20R BTW FS 295 / FS 310 WAS REPAIRED PER
- [SDR REXA2025012300081](https://openairdocs.org/sdr/REXA2025012300081.md): Floor Support · corroded · Dec 1, 2024 · N317CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION WAS FOUND LOCATED IN FLOOR BEAM AT RBL 9.00 BTW FS645.00/FS661.00. FLOOR BEAM AT RBL 9.00 BTW FS645.00/FS661.00 WAS REPAIRED PER CRJ-700 SRM 53-00-41-201-001-A01
- [SDR REXA2025012300080](https://openairdocs.org/sdr/REXA2025012300080.md): Stringer · corroded · Dec 1, 2024 · N317CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION OVER STGR19R BTW FS295 / FS310 STGR19R BTW FS280 / FS319 WAS REPAIRED PER CRJ700 SRM 53-00-03-201-001-A01
- [SDR REXA2025012300078](https://openairdocs.org/sdr/REXA2025012300078.md): Stringer · corroded · Nov 28, 2024 · N317CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STRINGER 21R BTW FS349 TO FS 364 ON INTERNAL STRUCTURE STRINGER 21R BTW FS 339.00 TO FS 379.00 ON INTERNAL STRUCTURE WAS REPLACED PER CRJ700 SRM 51-42-06-001-001-A01
- [SDR REXA2025012300077](https://openairdocs.org/sdr/REXA2025012300077.md): Floor Support · corroded · Nov 28, 2024 · N317CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION ON BEAM BTW FS 985.00/ FS 1088.00 AND RBL 27 AT AFT CARGO FLOOR STRUCTURE BEAM BTW FS 985.00/FS1056.25 & BTW FS 1070/ FS 1088.00 WAS RE-INSPECTED, NO DAMAGE WAS FOUND PER CRJ700 SRM 51-26-00-001-001-A01 AND BEAM BTW FS1056.25/FS1074.75 WAS REPAIRED P
- [SDR REXA2021112901022](https://openairdocs.org/sdr/REXA2021112901022.md): Fitting · gouged · Nov 22, 2021 · N317CA · Cndair CL6002C10 · Aileron Control System
  > INSPECTED THE L/H WING AILERON BUSHING BORE AT WS 295.50 AND FOUND DAMAGE IN THE TOP CENTER OF THE INBD BUSHING BORE - REPAIRED LH AILERON BUSHING BORE AT WS 295.50 IAW MHIRJ REO 670-57-51-456 REV A DATED 2021-11-15 WVAC EMP STAMP # 776 MTC
- [SDR REXA2021112901039](https://openairdocs.org/sdr/REXA2021112901039.md): Spoiler · bent · Nov 21, 2021 · N317CA · Cndair CL6002D24 · Drag Control System
  > RH OUTBOARD MULT-FUNCTION SPOILERS CENTER HINGE ON LEADING EDGE IS BENT - REPAIRED RH OB MFS IAW MHIRJ REO 670-57-73-048 DATED 2021-11-17 WVAC EMP STAMP # 776 MTC
- [SDR REXA2021112901040](https://openairdocs.org/sdr/REXA2021112901040.md): Cable · frayed · Nov 21, 2021 · N317CA · Cndair CL6002C10 · Aileron Control System
  > RH AILERON FUSELAGE O/B CABLE FRAYED IN CRITICAL FATIGUE AREA CLOSE TO AFT QUADRANT - REMOVED & REPLACED RH AILERON CABLE IAW CRJ 700 AMM 27-11-00. REMOVED & REPLACED REAR RH QUADRANT IAW CRJ 700 AMM 27-11-10. RIGGING & OPS CHECK OF AILERON TRIM SYS IS GOOD IA
- [SDR REXA2021112901024](https://openairdocs.org/sdr/REXA2021112901024.md): Frame · corroded · Nov 18, 2021 · N317CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > F.S. 333 FRAME IS CORRODED BETWEEN STGR 25L TO STGR 26R - FOUND OUT OF LIMITS. COMPLIED WITH STEPS CRJ-700 SRM 53-00-06-201-006-(A01) DISCONNECTED & CONNECETED LOWER ATC L-BAND IAW CRJ700 AMM 34-54-01-000/400-801(A01) PERFORMED FUNCTIONAL CHECK IAW CRJ700 34-5
- [SDR REXA2021112901038](https://openairdocs.org/sdr/REXA2021112901038.md): Stringer · corroded · Nov 15, 2021 · N317CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION AROUND 5TH FASTENER AFT OF FS 280 ON STGR 23R. - REPAIRED STR 23R FROM FS 280-FS 310 IAW ENDEAVOR EA CRJ 753-12420.
- [SDR REXA2021112901037](https://openairdocs.org/sdr/REXA2021112901037.md): Stringer · corroded · Nov 15, 2021 · N317CA · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > CORROSION AROUND 5TH FASTENER AFT OF FS 280 ON STRINGER 22R - REPAIRED STR 22R FROM FS 280-FS310 IAW CRJ 700 SRM 53-00-03-201-001-A01
- [SDR REXA2021112901032](https://openairdocs.org/sdr/REXA2021112901032.md): Plate · gouged · Nov 12, 2021 · N317CA · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > LOW PRESSURE GROUND CONNECTION HAS A GOUGE ON SKIN, LOWER AFT SECTION. MARKED WITH RED TAPE - COMPLIED WITH ENDEAVOR EA CRJ753-12409, REV.B DATED 11/3/21. OPS CHECK GOOD. REMOVED RED TAPE. REMOVED AND REINSTALLED COVER AND ADAPTER IAW CRJ 700 AMM 21-20-01-000/
- [SDR REXA2021112901028](https://openairdocs.org/sdr/REXA2021112901028.md): Intercostal · corroded · Nov 9, 2021 · N317CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > AVI DOOR INTERCOSTAL BETWEEN STGR 27 TO 26L IS CORRODED. - REMOVED AND REPLACED AVI BAY DOOR INTERCOSTAL BETWEEN STR 27 AND 26L IAW CRJ 700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
- [SDR REXA2021112901027](https://openairdocs.org/sdr/REXA2021112901027.md): Intercostal · corroded · Nov 9, 2021 · N317CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > AVI DOOR INTERCOSTAL AT STGR 27 IS CORRODED - REMOVED AND REPLACED AVI DOOR INTERCOSTAL AT STR 27 IAW CRJ 700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. WVAC EMP STAMP # 776 MTC
- [SDR REXA2021112901035](https://openairdocs.org/sdr/REXA2021112901035.md): Angle · cracked · Nov 8, 2021 · N317CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > AFTER DAMAGE REMOVAL ON COCKPIT DOOR POST AT RBL9 AT FLOOR LEVEL. FOUND BROKEN ANGLE (P/N CC670-33199-4) - REPLACED FS 280 ANGLE AT RBL 9 PN CC670-33199-4S IAW CRJ 700 SRM 51-42-06-001-001-A01. AND GASKET PN CC670-33467-2 IAW CRJ 700 SRM 51-42-04-001-001-A01 W
- [SDR REXA2021112901033](https://openairdocs.org/sdr/REXA2021112901033.md): Stringer · corroded · Nov 8, 2021 · N317CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > REMOVE STGR 27 AT FS 280.00 - FS 295.00 TO FACILITATE INSTALLATION OF ANTENNA DOUBLER AT FS 295.00 - FS 310.00 - REPLACED STRINGER 27 FS 280-300 IAW CRJ 700 SRM 51-40-11-001-001-A01, 51-42-21-001-001-A01, AND 51-42-06-001-001-A01.
- [SDR REXA2021112901036](https://openairdocs.org/sdr/REXA2021112901036.md): Stringer Splice · corroded · Nov 6, 2021 · N317CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FS 333 AND STR 26L STRINGER SPLICE IS CORRODED. - LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE STRINGER SPLICE AT FS 333 STR 26L IAW CRJ700 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01. WVAC EMP STAMP # 794 MTC
- [SDR REXA2021112901026](https://openairdocs.org/sdr/REXA2021112901026.md): Stringer · corroded · Nov 6, 2021 · N317CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > F.S. 280 TO F.S. 310 STGR 26R IS CORRODED - REMOVED AND REPLACED STRINGER SEGMENT AT 26R BETWEEN FS 280 AND FS 333 IAW CRJ700 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01 WVAC EMP STAMP # 776 MTC
- [SDR REXA2021112901034](https://openairdocs.org/sdr/REXA2021112901034.md): Angle · cracked · Nov 4, 2021 · N317CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > AFTER DAMAGE REMOVED ON COCKPIT DOOR POST AT LBL 9 AT FLOOR LEVEL FOUND BROKEN ANGLE (P/N: CC670-33199-3). - REPLACED ANGLE PN CC670-33199-3 AT LBL 9 FS 280 IAW CRJ700 SRM 51-42-06-001-001-A01. WVAC EMP STAMP # 794 MTC
- [SDR REXA2021112901023](https://openairdocs.org/sdr/REXA2021112901023.md): Angle · corroded · Nov 4, 2021 · N317CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > F.S. 280 "J" ANGLE AND FLOORBOARD FASTENERS CORRODED WITH EVIDENCE OF CORROSION BETWEEN J ANGLE AND F.S. 280 CROSSBEAM. - REMOVED AND REPLACED FS 280 J ANGLE IAW CRJ700 SRM 51-42-21-001-001-A01 AND 51-42-06-001-001-A01. WVAC EMP STAMP # 776 MTC
- [SDR REXA2021112901025](https://openairdocs.org/sdr/REXA2021112901025.md): Stringer · corroded · Nov 3, 2021 · N317CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > F.S. 280 TO F.S. 295 STGR 26L IS CORRODED - REMOVED AND REPLACED STR 26L BETWEEN FS 280 AND FS 333 IAW CRJ 700 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01 AND 51-42-21-001-001-A01 LOCATED AND DRILLED NEW SERVICEABLE STR 26L P/N SH670-31634-1S BETWEEN FS
- [SDR REXA2021101400875](https://openairdocs.org/sdr/REXA2021101400875.md): Channel · cracked · Oct 5, 2021 · N317CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > PANEL 195DL BRACKET IS CRACKED. MARKED WITH TAPE - REMOVED CRACKED CHANNEL FROM BRACKET ("T" EXTRUSION) IAW CRJ700 SRM 51-42-10-001-A01. ALODINED AND PAINTED BARE AREAS ON BRACKET IAW CRJ700 SRM 51-21-11-081-A01 AND 51-25-06-001-A01. INSTALLED C CHANNEL ONTO S
- [SDR REXA2021101400867](https://openairdocs.org/sdr/REXA2021101400867.md): Crossbeam · corroded · Oct 5, 2021 · N317CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > F.S. 280.00 CROSSBEAM HAS CORROSION ON UPPER SURFACE MULTIPLE AREAS LBL 45.0 TO RBL 45.0 - REMOVED CORROSION ON F.S. 280 CROSSBEAM IAW CRJ 700 SRM 53-00-00-101-001-A01. FOUND TO BE OUT OF LIMITS. REMOVED & REPLACED F.S. 280 CROSSBEAM IAW REO 670-53-11-579 REV
- [SDR REXA2021101400866](https://openairdocs.org/sdr/REXA2021101400866.md): Crossbeam · corroded · Oct 5, 2021 · N317CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > F.S. 280.00 CROSSBEAM HAS CORROSION ON UPPER SURFACE MULTIPLE AREAS LBL 45.0 TO RBL 45.0 - REMOVED CORROSION ON F.S. 280 CROSSBEAM IAW CRJ 700 SRM 53-00-00-101-001-A01. FOUND TO BE OUT OF LIMITS. REMOVED & REPLACED F.S. 280 CROSSBEAM IAW REO 670-53-11-579 REV
- [SDR REXA2021101400865](https://openairdocs.org/sdr/REXA2021101400865.md): Crossbeam · corroded · Oct 5, 2021 · N317CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > F.S. 280.00 CROSSBEAM HAS CORROSION ON UPPER SURFACE MULTIPLE AREAS LBL 45.0 TO RBL 45.0 - REMOVED CORROSION ON F.S. 280 CROSSBEAM IAW CRJ 700 SRM 53-00-00-101-001-A01. FOUND TO BE OUT OF LIMITS. REMOVED & REPLACED F.S. 280 CROSSBEAM IAW REO 670-53-11-579 REV
- [SDR REXA2021101400876](https://openairdocs.org/sdr/REXA2021101400876.md): Lug · gouged · Oct 4, 2021 · N317CA · Cndair CL6002C10 · Wing Structure
  > R/H AILERON BUSHING LUGS HAVE DAMAGE ON THE INNER BORE OF THE LUG - COMPLIED WITH REO STEP 1 AND 2 OF REPAIR 6 BORE OVERSIZE OF REO 670-57-61-107 REV B DATED 2019-01-14. PERFORMED LPI ON RH AILERON CENTER HINGE 4 REWORKED BORES IAW BOMBARDIER REO 670-57-61-107
- [SDR REXA2021101400871](https://openairdocs.org/sdr/REXA2021101400871.md): None · corroded · Oct 4, 2021 · N317CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > RH FLOOR SILL RBL45.0 FS 280.00 TO FS 310.00 HAS CORROSION ON UPPER SURFACE. - R/R UNSERVICEABLE FLOOR SILL (R/H FS 280 TO FS 310) WITH A SERVICEABLE SILL IAW CRJ 700 SRM 51-42-06-001-001(A01), 51-42-13-001-001(A01), AND 51-42-21-001-001(A01). WVAC EMP STAMP
- [SDR REXA2021101400879](https://openairdocs.org/sdr/REXA2021101400879.md): Actuator · corroded · Sep 27, 2021 · N317CA · Cndair CL6002C10 · Main Landing Gear
  > LH MLG SIDESTAY ACTUATOR PAINT FINISH IS DAMAGED, WITH SURFACE CORROSION. - REMOVED AND REPLACED LH MLG SIDE STAY IAW CRJ700 AMM 32-11-12-000-801-A01 AND 32-11-12-400-801-A01. LEAK AND OPS CHECKS GOOD IAW CRJ700 AMM 32-30-00-710-801-A01 AND 32-00-00-790-802-A0
- [SDR REXA2021101400869](https://openairdocs.org/sdr/REXA2021101400869.md): Panel · corroded · Sep 25, 2021 · N317CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > LH WHEEL WELL ACCESS PANEL 542AZ IS CORRODED AROUND NUMEROUS FASTENER HOLES. - REMOVED CORROSION ON PANEL 542AZ IAW CRJ 700 SRM 51-12-00-001-001-A01. FOUND TO BE OUT OF LIMITS. REPLACED PANEL, LOCATED, DRILLED AND DEBURRED PANEL IAW SRM 51-40-11-001-001(A01) I
- [SDR REXA2021101400864](https://openairdocs.org/sdr/REXA2021101400864.md): Fitting · corroded · Sep 25, 2021 · N317CA · Cndair CL6002C10 · Passenger/Crew Doors
  > LATCH MECHANISM PULL IN LEVER TORQUE TUBES CORRODED AND STOP FITTING CHAFED AND PITTED. - INSTALLED NEW PAX DOOR PULL IN LEVER TORQUE TUBE AND REINSTALLED SAME SERVICEABLE PULL IN LEVERS IAW CRJ700 AMM 52-11-02-400-806-A01. OPS CHECK GOOD. /N 601R31863-1. STOP
- [SDR REXA2021101400863](https://openairdocs.org/sdr/REXA2021101400863.md): Torque Tube · corroded · Sep 25, 2021 · N317CA · Cndair CL6002C10 · Passenger/Crew Doors
  > LATCH MECHANISM PULL IN LEVER TORQUE TUBES CORRODED AND STOP FITTING CHAFED AND PITTED. - INSTALLED NEW PAX DOOR PULL IN LEVER TORQUE TUBE AND REINSTALLED SAME SERVICEABLE PULL IN LEVERS IAW CRJ700 AMM 52-11-02-400-806-A01. OPS CHECK GOOD. /N 601R31863-1. STOP
- [SDR REXA2021101400877](https://openairdocs.org/sdr/REXA2021101400877.md): Panel · corroded · Sep 24, 2021 · N317CA · Cndair CL6002C10 · Fuselage Main, Structure
  > CLOSING PANEL FWD OF FLIGHT DECK FLOORBOARD AT FS 260 IS CORRODED - R/R UNSERVICEABLE CLOSING PANEL @ FS260 WITH SERVICEABLE PANEL IAW CRJ 700 SRM 51-42-06-001-001-A01. WVAC EMP STAMP #722 MTC
- [SDR REXA2021101400873](https://openairdocs.org/sdr/REXA2021101400873.md): Web · corroded · Sep 24, 2021 · N317CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > R/H AND L/H 280 BULKHEAD LOWER WEB IS CORRODED. - INSTALLED, FABRICATED, LOCATED AND DRILLED NEW LOWER RH AND LH 280 BULKHEAD WEB AND SPLICE PLATE C/W HFEC OF LH / RH 280 BULKHEAD WEBS APPLIED PAINT ON RH AND LH 280 BULKHEAD WEBS IAW CRJ 700 SRM 53-11-10-201-
- [SDR REXA2021101400874](https://openairdocs.org/sdr/REXA2021101400874.md): Angle · corroded · Sep 23, 2021 · N317CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FLIGHT DECK FLOOR BOARD SUPPORT ANGLE AT RBL18 AND LBL18 ARE CORRODED. - LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE RH AND LH FLIGHT DECK FLOORBOARD SUPPORT ANGLES AND GUSSETS IAW CRJ 700 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 AND 51-42-21-001-001-
- [SDR REXA2021101400872](https://openairdocs.org/sdr/REXA2021101400872.md): Intercostal · corroded · Sep 23, 2021 · N317CA · Cndair CL6002C10 · Service Doors
  > P/N: SH670-32075-4/SH670-32075-3. AVIONICS BAY DOOR SURROUND STRUCTURE, 2 EACH INTERCOSTALS LBL2 & RBL2 FORWARD OF DOOR STRUCTURE, CORRODED, FS349.00-FS364.00. - R/R UNSERVICEABLE L/H & R/H STRINGER 27 INTERCOSTALS WITH SERVICEABLE INTERCOSTALS IAW CRJ 700 SRM
- [SDR REXA2021101400868](https://openairdocs.org/sdr/REXA2021101400868.md): Angle · corroded · Sep 23, 2021 · N317CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FS 280.00 FWD J-ANGLE IS CORRODED. - R/R/ UNSERVICEABLE "J" ANGLE WITH A SERVICEABLE ANGLE IAW MHIRJ REO 670-53-11-579 REV B. WVAC EMP STAMP #722 MTC
- [SDR REXA2021101400870](https://openairdocs.org/sdr/REXA2021101400870.md): Angle · corroded · Sep 22, 2021 · N317CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > SERVICE DOOR SEAL STRIKER HAS AN AREA OF CORROSION ON INNER SURFACE AND (3) ELONGATED HOLES WHERE STEP PLATE ATTACHES. - REMOVED SERVICE DOOR SILL STRIKER AND L ANGLE FWD OF IAW CRJ 700 SRM 51-42-21-001-001-A01 AND 51-42-06-001-001-A01. REMOVED AND INSTALLED S

Next page: https://openairdocs.org/aircraft/N317CA/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 = 'N317CA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N317CA/reports

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