N317CA

Service difficulty reports · 275

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR REXA2026092501878Lamp · inoperativeTWO EMERGENCY FLOODLIGHT LAMPS INOP. R & R THE LAMPS IAW AMM 33-51-05. OPS CHECKED GOOD.Sep 24, 2026 · N317CA · Cndair CL6002C10 · Emergency LightingSDR REXA2026073001336Lamp · inoperative5 EMERGENCY FLOODLIGHT LAMPS INOP. R+R 5 EMERGENCY FLOODLIGHT LAMPS P/N OL3071BPE/GPL REF AMM 33-51-05. OPS CHECK GOOD.Jul 29, 2026 · N317CA · Cndair CL6002C10 · Emergency LightingSDR REXA2026062900982Strut · disconnectedGALLEY 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 SVCJun 28, 2026 · N317CA · Cndair CL6002C10 · Service DoorsSDR REXA2026050400447Hinge · damagedPAX 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.Apr 26, 2026 · N317CA · Cndair CL6002C10 · Fuselage, Door HingeSDR REXA2026050400446Hinge · damagedPAX 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 52-11-01Apr 26, 2026 · N317CA · Cndair CL6002C10 · Fuselage, Door HingeSDR REXA2025092300871Fadec · inoperativeAT 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 LANSep 18, 2025 · N317CA · Cndair CL6002C10 · Fuel Controlling SystemSDR REXA2025012300074Canister · leakingFUEL 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 --Jan 19, 2025 · N317CA · Cndair CL6002C10 · Fuel StorageSDR REXA2025012300089Floor Support · corrodedCORROSION 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 CORROSIONDec 6, 2024 · N317CA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR REXA2025012300088Seat Track · corrodedIN 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 53Dec 6, 2024 · N317CA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2025012300087Stringer · corrodedINITIAL 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-A01Dec 6, 2024 · N317CA · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR REXA2025012300086Beam · chafedWEAR 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. IRDec 6, 2024 · N317CA · Cndair CL6002C10 · Fuselage Main, StructureSDR REXA2025012300085Stringer · corrodedCORROSION 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-A01Dec 6, 2024 · N317CA · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR REXA2025012300084Skin · crackedCRACK 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 --Dec 6, 2024 · N317CA · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR REXA2025012300083Stringer · corrodedCORROSION 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 PERDec 4, 2024 · N317CA · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR REXA2025012300081Floor Support · corrodedCORROSION 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-A01Dec 1, 2024 · N317CA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR REXA2025012300080Stringer · corrodedCORROSION OVER STGR19R BTW FS295 / FS310 STGR19R BTW FS280 / FS319 WAS REPAIRED PER CRJ700 SRM 53-00-03-201-001-A01Dec 1, 2024 · N317CA · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR REXA2025012300078Stringer · corrodedCORROSION 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-A01Nov 28, 2024 · N317CA · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR REXA2025012300077Floor Support · corrodedCORROSION 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 PNov 28, 2024 · N317CA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR REXA2021112901022Fitting · gougedINSPECTED 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 MTCNov 22, 2021 · N317CA · Cndair CL6002C10 · Aileron Control SystemSDR REXA2021112901039Spoiler · bentRH 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 MTCNov 21, 2021 · N317CA · Cndair CL6002D24 · Drag Control SystemSDR REXA2021112901040Cable · frayedRH 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 IANov 21, 2021 · N317CA · Cndair CL6002C10 · Aileron Control SystemSDR REXA2021112901024Frame · corrodedF.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 34-5Nov 18, 2021 · N317CA · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2021112901038Stringer · corrodedCORROSION AROUND 5TH FASTENER AFT OF FS 280 ON STGR 23R. - REPAIRED STR 23R FROM FS 280-FS 310 IAW ENDEAVOR EA CRJ 753-12420.Nov 15, 2021 · N317CA · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2021112901037Stringer · corrodedCORROSION 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-A01Nov 15, 2021 · N317CA · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR REXA2021112901032Plate · gougedLOW 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/Nov 12, 2021 · N317CA · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR REXA2021112901028Intercostal · corrodedAVI 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.Nov 9, 2021 · N317CA · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2021112901027Intercostal · corrodedAVI 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 MTCNov 9, 2021 · N317CA · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2021112901035Angle · crackedAFTER 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 WNov 8, 2021 · N317CA · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2021112901033Stringer · corrodedREMOVE 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.Nov 8, 2021 · N317CA · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2021112901036Stringer Splice · corrodedFS 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 MTCNov 6, 2021 · N317CA · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2021112901026Stringer · corrodedF.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 MTCNov 6, 2021 · N317CA · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2021112901034Angle · crackedAFTER 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 MTCNov 4, 2021 · N317CA · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2021112901023Angle · corrodedF.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 MTCNov 4, 2021 · N317CA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR REXA2021112901025Stringer · corrodedF.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 Nov 3, 2021 · N317CA · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2021101400875Channel · crackedPANEL 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 SOct 5, 2021 · N317CA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR REXA2021101400867Crossbeam · corrodedF.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 Oct 5, 2021 · N317CA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR REXA2021101400866Crossbeam · corrodedF.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 Oct 5, 2021 · N317CA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR REXA2021101400865Crossbeam · corrodedF.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 Oct 5, 2021 · N317CA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR REXA2021101400876Lug · gougedR/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 670-57-61-107Oct 4, 2021 · N317CA · Cndair CL6002C10 · Wing StructureSDR REXA2021101400871None · corrodedRH 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 Oct 4, 2021 · N317CA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR REXA2021101400879Actuator · corrodedLH 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-A0Sep 27, 2021 · N317CA · Cndair CL6002C10 · Main Landing GearSDR REXA2021101400869Panel · corrodedLH 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) ISep 25, 2021 · N317CA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR REXA2021101400864Fitting · corrodedLATCH 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. STOPSep 25, 2021 · N317CA · Cndair CL6002C10 · Passenger/Crew DoorsSDR REXA2021101400863Torque Tube · corrodedLATCH 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. STOPSep 25, 2021 · N317CA · Cndair CL6002C10 · Passenger/Crew DoorsSDR REXA2021101400877Panel · corrodedCLOSING 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 MTCSep 24, 2021 · N317CA · Cndair CL6002C10 · Fuselage Main, StructureSDR REXA2021101400873Web · corrodedR/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-Sep 24, 2021 · N317CA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR REXA2021101400874Angle · corrodedFLIGHT 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-Sep 23, 2021 · N317CA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR REXA2021101400872Intercostal · corrodedP/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 SRMSep 23, 2021 · N317CA · Cndair CL6002C10 · Service DoorsSDR REXA2021101400868Angle · corrodedFS 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 MTCSep 23, 2021 · N317CA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR REXA2021101400870Angle · corrodedSERVICE 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 SSep 22, 2021 · N317CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
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