N926EV

Service difficulty reports · 195

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 = 'N926EV' 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 SWIA202266418None · failedL 14TH DUCT WARNING INFLIGHT. QRH PROCEDURE DID NOT EXTINGUISH. (FLIGHT #4157 FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 25424973 WITH THE FOLLOWING CORRECTIVE ACTION: "VISUALLY INSPECTED LH 14TH STAGE DUCTING WHILE 14TH STAGE BLEED AIR SYSep 2, 2022 · N926EV · Cndair CL6002B19 · Pneumatic SystemSDR SWIA202053949Strap · corrodedPRESSURE FLOOR STRAP AT FS 559.000 FROM RBL 27 TO PRESSURE FLOOR SILL IS CORRODED. C-CHECK RO 11/11/2020. REMOVED DAMAGED FLOOR STRAP AND INSTALLED A NEW PRESSURE FLOOR STRAP, IAW CRJ 200 SRM.Oct 16, 2020 · N926EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202053890Floorbeam · corrodedAT RBL 9 FS 513.00 INBOARD FLANGE OF FLOOR BEAM CORRODED. C-CHECK RO 11/11/2020. REPAIR WAS ACCOMPLISHED, IAW MHIRJ REO. NO WEIGHT AND BALANCE CHANGE REQUIRED. M-337 AND TASK CARD ATTACHED.Oct 11, 2020 · N926EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA202053948Plate · corrodedPLATE FOR PASSENGER DOOR FWD ANCHOR FITTING IS CORRODED. C-CHECK RO 11/11/2020. RECEIVED NEW PLATE VERIFIED TO BE P/N 600-38061-11 CRJ 200 AIPC, REF JOB 9784381 OP 139 MX TRANS NR 21619598 FOR PLATE INSTALLATION.Oct 3, 2020 · N926EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA202053926Skin · looseRT OUTBOARD FLAP UPPER SKIN HAS LOOSE & SMOKING RIVETS ON THE AFT SPAR BETWEEEN F/STA 234 & 245 AND ON F/STA 245 BETWEEN AFT SPAR & TE. C-CHECK RO 11/11/2020. REPAIRED RT OUTBOARD FLAP UPPER SKIN, IAW REO. NO WEIGHT OR BALANCE CHANGE. M-337 AND TASK CARD ASep 29, 2020 · N926EV · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA202053885Former · corrodedFOUND PAX DOOR FORMER 601R318078-3 TO BE CORRODED. C-CHECK RO 11/11/2020. INSTALLED PAX DOOR FORMER AT FS 329.75, IAW CRJ 200 AMM. COMPLETED TASK CARD AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE, REFERENCE CONTINUATION FOR WORK PERFORMED.Sep 25, 2020 · N926EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA202053947Nut · corrodedLT FLAP HINGE BOX AT WS 220.00 NUT CORRODED ON AFT OUTBOARD SIDE OF BRACKET. C-CHECK RO 11/11/2020. REMOVE AND REPLACED NUT P/N MS17825-7 ON LT HINGE BOX AT WS 220.00 OUTBOARD SIDE, IAW CRJ 200 AMM. REMOVED AND REPLACED NUT P/N MS17828-7 ON LT HINGE BOX AT Sep 24, 2020 · N926EV · Cndair CL6002B19 · Wing, Control Surface Attach FittingsSDR SWIA202053946Nut · corrodedRT FLAP HINGE BOX AT WS 220.00 NUT CORRODED ON AFT INBOARD AND OUTBOARD SIDE OF BRACKET AND FWD BRACKET. C-CHECK RO 11/11/2020. REMOVED AND REPLACED RT HINGE BOX AT WS 220.00, THE NUTS ON INBOARD AND OUTBOARD SIDE OF BRACKET AND THE FWD BRACKET, IAW CRJ 200 Sep 24, 2020 · N926EV · Cndair CL6002B19 · Wing, Control Surface Attach FittingsSDR SWIA202053945Nut · corrodedLT FLAP HINGE BOX AT WS 264.00 NUT CORRODED ON AFT INBOARD AND OUTBOARD SIDE OF BRACKET. C-CHECK RO 11/11/2020. REMOVED AND REPLACED LT HINGE BOX INBOARD & OUTBOARD NUTS (P/N MS17825-7) AT WS 264.00, IAW CRJ 200 AMM. TORQUE WRENCH WVACT 10147, CAL DUE 30 SESep 24, 2020 · N926EV · Cndair CL6002B19 · Wing, Control Surface Attach FittingsSDR SWIA202053944Nut · corrodedRT FLAP HINGE BOX AT WS 264.00 NUT CORRODED ON AFT INBOARD SIDE OF BRACKET. C-CHECK RO 11/11/2020. REMOVE AND REPLACE NUT ON RT FLAP HINGE BOX AT WS 264.00 ON AFT INBOARD SIDE OF BRACKET, IAW CRJ 200 AMM. TORQUE WRENCH WVACT 10147, CAL DUE 30 SEPT 21.Sep 24, 2020 · N926EV · Cndair CL6002B19 · Wing, Control Surface Attach FittingsSDR SWIA202053943Bracket · corrodedRT FLAP HINGE BOX AT WS 178.00 NUT CORRODED ON AFT OUTBOARD SIDE OF BRACKET. C-CHECK RO 11/11/2020. REMOVE AND REPLACE RT FLAP HINGE BOX AT WS 178.00 THE NUT ON THE AFT OUTBOARD SIDE OF THE BRACKET, IAW CRJ 200 AMM. TORQUE WRENCH WVACT 10147, CAL DUE 30 SEPSep 24, 2020 · N926EV · Cndair CL6002B19 · Wing, Control Surface Attach FittingsSDR SWIA202053942Bracket · corrodedPAX DOOR SURROUND STRUCTURE BRACKET CONNECTORS FWD AND AFT CORRODED BETWEEN FS 319.70 ND FS 333 AND BETWEEN STGR 17L AND STGR 18L. C-CHECK RO 11/11/2020. REMOVED FWD AND AFT CONNECTOR BRACKETS, IAW CRJ-200 SRM 51-42-06. LOCATED, DRILLED, AND INSTALLED NEW Sep 24, 2020 · N926EV · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA202053925Fitting · crackedWINDSHIELD CENTER POST LOWER FITTING IS CRACKED FROM THE LOWER VERTICAL EDGE TO THE FIRST LOWER FASTENER HOLE ON THE RT & LT SIDES. FAIL DETAILED VISUAL INSPECTION. C-CHECK RO 11/11/2020. REMOVED AND REPLACED WINDSHIELD CENTER POST RT AND LT LOWER FITTING FSep 24, 2020 · N926EV · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA202053924Angle · corrodedPAX DOOR SURROUND STRUCTURE ANGLE CORRODED BETWEEN FS 310 AND FS 319.70 BETWEEN STGR 17L AND STGR18L. C-CHECK RO 11/11/2020. REMOVED DAMAGED PAX DOOR SURROUND STRUCTURE ANGLE AND INSTALLED A NEW ANGLE, IAW CRJ 200 SRM. COMPLETED TASK CARD FORM M-337 ATTACHESep 24, 2020 · N926EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202053884Intercostal · corrodedFOUND PAX DOOR INTERCOSTAL DD4 TO BE CORRODED IN MULTIPLE LOCATIONS. C-CHECK RO 11/11/2020. INSTALLED SERVICEABLE PAX DOOR INTERCOSTAL DD4, IAW CRJ 200 SRM. COMPETED TASK CARD AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE, REFERENCE CONTINUATION CARD FSep 24, 2020 · N926EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA202053883Former · corrodedFOUND PAX DOOR AFT FORMER TO BE CORRODED IN MULTIPLE LOCATIONS. C-CHECK RO 11/11/2020. INSTALLED SERVICEABLE PAX DOOR AFT FORMER, IAW CRJ 200 SRM. COMPLETED TASK CARD AND ATTACHED COMPLETED FOR 337. NO WEIGHT CHANGE, REFERENCE CONTINUATION CARD FOR WORK PESep 24, 2020 · N926EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA202053876Floor Skin · corrodedLT PRESSURE FLOOR SILL SKIN AT FS 518.00 AND FS 522.00 IS CORRODED. C-CHECK RO 11/11/2020. REPAIRED LT PRESSURE FLOOR SILL SKIN AT FS 518.00 AND FS 522.00 CORROSION, IAW BOMBARDIER REO. REFERANCE CONTINUATION FOR WORK PERFORMED.Sep 24, 2020 · N926EV · Cndair CL6002B19 · Fuselage Floor PanelSDR SWIA202053923Floor Support · corrodedLT PRESSURE FLOOR SILL IS CORRODED AT (2) LOCATIONS ON THE FLOOR SKIN, (1) LOCATION ON THE FLOOR DOUBLER AND THE FLOOR STRAP SPANNING LBL 27.00 AND FLOOR SILL IS CORRODED IN NUMEROUS LOCATIONS. DAMAGE IS BETWEEN FS 544.00 AND FS 559.00. C-CHECK RO 11/11/2020Sep 23, 2020 · N926EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202053922Floor Support · corrodedLT PRESSURE FLOOR SILL IS CORRODED AT (5) LOCATIONS ON THE FLOOR SKIN BETWEEN FS 473.15 AND FS 513.00. C-CHECK RO 11/11/2020. REPAIRED LT PRESSURE FLOOR SILL AT (5) LOCATIONS ON THE FLOOR SKIN BETWEEN FS 473.15 AND FS 513.00, IAW BOMBARDIER REO WEIGHT AND BASep 23, 2020 · N926EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202053921Floor Support · corrodedLT PRESSURE FLOOR SILL IS CORRODED AT (1) LOCATION ON THE FLOOR SKIN BETWEEN FS 449.85 AND FS 473.15. C-CHECK RO 11/11/2020. REMOVED LT PRESSURE FLOOR SILL CORROSION AT (1) LOCATION ON THE FLOOR SKIN BETWEEN FS 449.85 AND FS 473.15, IAW BOMBARDIER REO. WEIGSep 23, 2020 · N926EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202053920Floor Support · corrodedLT PRESSURE FLOOR SIL IS CORRODED AT (3) LOCATIONS ON THE FLOOR SKIN BETWEEN FS 424.00 AND FS 449.85. C-CHECK RO 11/11/2020. REMOVED LT PRESSURE FLOOR SILL CORROSION AT (3) LOCATIONS ON THE FLOOR SKIN BETWEEN FS 424.00 AND FS 449.85, IAW BOMBARDIER REO. WEISep 23, 2020 · N926EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202053919Floor Support · corrodedLT PRESSURE FLOOR SILL IS CORRODED AT (2) LOCATIONS ON THE FLOOR SKIN BETWEEN FS 409.00 AND FS 424.00. C-CHECK RO 11/11/2020. REMOVED LT PRESSURE FLOOR SILL CORROSION AT (2) LOCATIONS ON THE FLOOR SKIN BETWEEN FS 409.00 AND FS 424.00, IAW BOMBARDIER REO. WESep 23, 2020 · N926EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202053918Floor Support · corrodedRT CABIN PRESSURE FLOOR SILL HAS (1) AREA OF CORROSION ON THE SILL SKIN, (1) AREA OF CORROSION ON THE SILL DOUBLER AND (1) AREA OF CORROSION ON THE FLOOR STRAP THAT SPANS RBL 27.00 AND THE PRESSURE FLOOR SILL. DAMAGE IS BETWEEN FS 544.00 AND FS 559.00. C-CHESep 23, 2020 · N926EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202053917Floor Support · corrodedRT PRESSURE FLOOR SILL HAS (3) AREAS OF CORROSION ON THE SILL SKIN BETWEEN FS 529.00 AND FS 544.00. C-CHECK RO 11/11/2020. REPAIR WAS ACCOMPLISHED IAW BOMBARDIER REO. NO WEIGHT AND BALANCE CHANGE, M-337 AND TASK CARD ATTACHED.Sep 23, 2020 · N926EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202053916Floor Support · corrodedRT CABIN PRESSURE FLOOR SILL HAS (2) AREAS OF CORROSION ON THE SILL SKIN BEWTEEN FS 513.00 AND FS 529.00. C-CHECK RO 11/11/2020. REMOVED CORROSION AND TREATED AREA, IAW BOMBARDIER REO. NO WEIGHT AND BALANCE CHANGE. M-337 AND TASK CARD ATTACHED.Sep 23, 2020 · N926EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202053915Floor Support · corrodedRT CABIN PRESSURE FLOOR SILL HAS (4) AREAS OF CORROSION ON THE SILL SKIN BETWEEN FS 484.00 AND FS 513.00. C-CHECK RO 11/11/2020. REPAIRED RT CABIN PRESSURE FLOOR SILL (4) AREAS OF CORROSION ON THE SILL SKIN BETWEEN FS 484.00 AND FS 513.00. REMOVED CORROSIONSep 23, 2020 · N926EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202053914Floor Support · corrodedRT PRESSURE FLOOR SILL HAS (1) AREA OF CORROSION ON THE SILL SKIN AT FS 461.00. C-CHECK RO 11/11/2020. RT PRESSURE FLOOR SILL CORROSION WAS REMOVED AND TREATED, IAW BOMBARDIER REO, AS DOCUMENTED ON ATTACHED CONTINUATION CARD. NO WEIGHT AND BALANCE CHANGE, MSep 23, 2020 · N926EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202053913Floor Support · corrodedRT PRESSURE FLOOR SILL HAS (3) AREAS OF CORROSION ON THE SILL SKIN BETWEEN FS 424.00 AND FS 439.00. C-CHECK RO 11/11/2020. REPAIR TO RT PRESSURE FLOOR SILL WAS COMPLETED, IAW BOMBARDIER REO, AS DOCUMENTED ON ATTACHED CONTINUATION CARD. M-337 AND TASK CARD ASep 23, 2020 · N926EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202053889Floor Support · corrodedLT PRESSURE FLOOR SILL SKIN PANEL AT FS 473.15 LBL 36 IS CORRODED. C-CHECK RO 11/11/2020. COMPLIED WITH BOMBARDIER REO AND MHIRJ REO. COMPLETED TASK CARD AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE, REFERENCE CONTINUATION FOR WORK PERFORMED.Sep 23, 2020 · N926EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202053882Door Frame · damagedFOUND PAX DOOR FRAME ON FWD SIDE TO HAVE MULTIPLE OVERSIZED HOLES. C-CHECK RO 11/11/2020. INSTALLED SERVICEABLE PAX DOOR FWD FRAME, IAW CRK 200 SRM. COMPLETED TASK CARD AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE, REFERENCE CONTINUATION CARD FOR WORKSep 23, 2020 · N926EV · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA202053881A/C Pack · corrodedFOUND PAX DOOR LOWER AFT INTERCOSTAL TO BE CORRODED. C-CHECK RO 11/11/2020. INSTALLED SERVIEABLE PAX DOOR LOWER AFT INTERCOSTAL, IAW CRJ 200 SRM. COMPLETED TASK CARD AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE, REFERENCE CONTINUATION CARD FOR WORK PESep 23, 2020 · N926EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA202053880A/C Pack · corrodedFOUND PAX DOOR INTERCOSTAL TO BE CORRODED ON AFT SIDE. C-CHECK RO 11/11/2020. INSTALLED SEVICABLE PAX DOOR INTERCOSTAL, IAW CRJ 200 SRM. COMPLETED TASK CARD AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE, REFERENCE CONTIUATION CARD FOR WORK PERFORMED.Sep 23, 2020 · N926EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA202053879Intercostal · corrodedFOUND PAX DOOR INTERCOSTAL DD3 TO BE CORRODED. C-CHECK RO 11/11/2020. INSTALLED SERVICEABLE PAX DOOR INTERCOSTAL DD3, IAW CRJ 200 SRM. COMPLETED TASK CARD AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE, REFERENCE CONTIUATION CARD FOR WORK PERFORMED.Sep 23, 2020 · N926EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA202053878Intercostal · corrodedFOUND PAX DOOR INTERCOSTAL DD1 TO BE CORRODED ON AFT SIDE. C-CHECK RO 11/11/2020. INSTALLED SERVICEABLE PAX DOOR INTERCOSTAL DD1, IAW CRJ 200 SRM. COMPETED TASK CARD AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE, REFERENCE CONTINUATION CARD FOR WORK PESep 23, 2020 · N926EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA202053875Floor Support · corrodedLT PRESSURE FLOOR SILL IS CORRODED AT (4) LOCATIONS ON THE FLOOR SKIN BETWEEN FS 513.00 AND FS 544.00. C-CHECK RO 11/11/2020. REPAIRED LT PRESSURE FLOOR SILL CORROSION AT (4) LOCATIONS ON THE FLOOR SKIN BETWEEN FS 513.00 AND FS 544.00. REFERENCE CONTINUATIOSep 23, 2020 · N926EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202053868Angle · crackedFOUND PAX DOOR LATCH BOX INBOARD ANGLE TO BE CRACKED. C-CHECK RO 11/11/2020. REMOVED AND REPLACED PAX DOOR LATCH LOCK BOX INBOARD ANGLE, IAW CRJ 200 SRM.Sep 23, 2020 · N926EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA202053941Link · corrodedLT OUTBOARD GROUND SPOILER PCU LINK HAS CORRODED HARDWARE. C-CHECK RO 11/11/2020. REPLACED LT OUTBOARD GROUND SPOILER PCU LINK HARDWARE PART NUMBERS NAS-6305U-19D AND NAS6205-12D PER CRJ200 AMM. TW SN 08158140 CAL DATE 16 MAR 20 CAL DUE 31 MAR 21.Sep 22, 2020 · N926EV · Cndair CL6002B19 · SpoilersSDR SWIA202053940Bolt · corrodedLT OUTBOARD GROUND SPOILER HINGE HARDWARE IS CORRODED. C-CHECK RO 11/11/2020. INSTALLED SERVICEABLE LT WING OUTBOARD SPOILER INBOARD AND CENTER HINGES HARDWARE, IAW CRJ-200 AMM TASK.Sep 22, 2020 · N926EV · Cndair CL6002B19 · Wing, Attach FittingsSDR SWIA202053939Link · corrodedLT INBOARD GROUND SPOILER PCU LINK HAS CORRODED HARDWARE. C-CHECK RO 11/11/2020. REPLACED INBOARD GROUND SPOILER PCU LINK HARDWARE PART NUMBERS NAS-6305U-19D AND NAS6205-12D, REF CRJ200 AMM. TW SN 08158140 CAL DATE 16 MAR 20 CAL DUE 31 MAR 20.Sep 22, 2020 · N926EV · Cndair CL6002B19 · SpoilersSDR SWIA202053938Hinge · corrodedLT INBOARD GROUND SPOILER HAS CORRODED HINGE HARDWARE. C-CHECK RO 11/11/2020. INSTALLED SERVICABLE LT WING INBOARD SPOILER INBOARD AND CENTER HINGES HARDWARE, IAW CRJ-200 AMM TASK.Sep 22, 2020 · N926EV · Cndair CL6002B19 · SpoilersSDR SWIA202053937Bolt · corrodedRT OUTBOARD GROUND SPOILER PCU LINK HARDWARE IS CORRODED. C-CHECK RO 11/11/2020. REMOVED AND REPLACED RT WING OUTBOARD GROUND SPOILER PCU LINK HARDWARE, IAW CRJ-200 AMM TASK.Sep 22, 2020 · N926EV · Cndair CL6002B19 · SpoilersSDR SWIA202053936Bolt · corrodedRT OUTBOARD GROUND SPOILER HAS CORRODED HINGE HARDWARE. C-CHECK RO 11/11/2020. INSTALLED SERVICEABLE RIGHT OUTBOARD GROUND SPOILER HINGE HARDWARE, IAW CRJ-200 AMM TASK. TORQUE WRENCH PN: WVACT204356, CALIBRATED DATE: 09-14-2020.Sep 22, 2020 · N926EV · Cndair CL6002B19 · Wing, Attach FittingsSDR SWIA202053935Bolt · corrodedRT INBOARD GROUND SPOILER PCU LINK HAS CORRODED HARDWARE. C-CHECK RO 11/11/2020. REMOVED AND REPLACED CORRODED HARDWARE ON INBOARD GROUND SPOILER PCU LINK WITH SERVICABLE P/N; NAS6305U19D, IAW CRJ-200 AMM TASK. CALIBRATED TOOL REQUIRED, TORQUE WRENCH WVACT Sep 22, 2020 · N926EV · Cndair CL6002B19 · Wing, Attach FittingsSDR SWIA202053934Hinge · corrodedRT INBOARD GROUND SPOILER HINGE HARDWARE IS CORRODED. C-CHECK RO 11/11/2020. REMOVED CORRODED HARDWARE AT RT INBOARD GROUND SPOILER HINGES AND REPLACED WITH SERVICABLE PARTS, IAW CRJ-200 AMM TASK. CALIBRATED TOOL REQUIRED, TORQUE WRENCH WVACT 0083 CAL 9/14/Sep 22, 2020 · N926EV · Cndair CL6002B19 · SpoilersSDR SWIA202053912Hinge · gougedFUSELAGE SIDE OF PASSENGER DOOR HINGE, MOST AFT LANDING HAS A DEEP GOUGE AT A PREVIOUS REPAIR. C-CHECK RO 11/11/2020. REPAIRED FUSELAGE SIDE OF PASSENGER DOOR HINGE, IAW CRJ-200 AMM SRM, BOMBARDIER REO, AND MHIRJ REO. REFERENCE CONTINUATION CARD FOR WORK PESep 22, 2020 · N926EV · Cndair CL6002B19 · Fuselage, Door HingeSDR SWIA202053895Floor Support · corrodedRT CABIN FLOOR BEAM ON RBL 9.00 HAS A HOLE CORRODED THROUGH IT AND NUMEROUS OTHER LOCATIONS WITH HEAVY CORROSION BETWEEN FS 409.00 TO FS 409.00+128. C-CHECK RO 11/11/2020. REPAIRED RT CABIN FLOOR BEAM AT RBL 9.00, HOLE CORRODED THROUGH IT AND NUMEROUS OTHER Sep 22, 2020 · N926EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202053874Cup · corrodedPAX DOOR HAND RAIL STOW CUPS ARE CORRODED. C-CHECK RO 11/11/2020. LOCATED, DRILLED, AND INSTALLED NEW FWD AND AFT STOW CUP ASSEMBLY'S, IAW CRJ-200 SRM.Sep 22, 2020 · N926EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA202053870Frame · corrodedFS 409.00 IS CORRODED ON THE FORWARD SIDE ON THE FRAME DOUBLER BETWEEN STR 26 AND STR 27 AND ON THE AFT SIDE ON THE FRAME DOUBLER. C-CHECK RO 11/11/2020. REMOVED UNSERVICEABLE FS 409.00 FRAME DOUBLER BETWEEN STR 26 AND STR 27 AND AFT SIDE ANGLE ON THE FRAME Sep 22, 2020 · N926EV · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA202053933Floorbeam · corrodedFLOOR CROSSBEAM CAP BETWEEN LBL 9.00 AND LBL 27.00 AT FS 589.00 IS CORRODED. C-CHECK RO 11/11/2020. REPLACED UNSERVICEABLE FLOOR CROSSBEAM CAP AT FS 589 BETWEEN LBL 9 AND LBL 27, IAW CRJ200 SRM.Sep 21, 2020 · N926EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA202053932Floorbeam · corrodedFLOOR CROSSBEAM CAP IS CORRODED BETWEEN RBL 9.00 AND LBL 9.00 AT FS 559.00+80. C-CHECK RO 11/11/2020. REMOVED CORRODED CROSS BEAM CAP, INSTALLED NEW SERVICEABLE FLOOR CROSSBEAM CAP BETWEEN RBL 9.00 AND LBL 9.00 AT FS 559.00+80, IAW CRJ 200 SRM REFERENCE CONTSep 21, 2020 · N926EV · Cndair CL6002B19 · Fuselage Main, Floor Beam
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