N916EV

Service difficulty reports · 214

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 = 'N916EV' 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 SWIA2026090977110Vane · out of limitsREPLACE LEFT INBD FLAP INBD VANE CAP. OPENSep 9, 2026 · N916EV · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2026030375431Bracket · damagedDAMAGE TO THE MCD PULLEY MOUNTING BRACKET AND SKIN (FLIGHT 4696) PERFORMED PERMANENT REPAIR TO PAX DOOR INNER SKIN AND FORMER AT FS347.25 AND BTW DATUM #3 AND #5 IAW REO 601R-52-11-3088 REV-- DATE 2026-03-03 STEPS 4-21. SEE CP 31820099 FOR STEPS 1 AND 2 OF RMar 3, 2026 · N916EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2025100400024Frame · dentedCOMPLY WITH REO 601R-53-11-4030, TEMPORARY REPAIR FOR DENT DAMAGE TO FRAME WEB AT BS 241.60, RBL 5.50 - RBL 11.16. COMPLIED WITH REO 601R-53-11-4030, REV-, TEMPORARY REPAIR FOR DENT DAMAGE TO FRAME WEB AT FS 241.60 AND BETWEEN RBL 5.50 €“ RBL 11.16. ENSUREOct 24, 2025 · N916EV · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA2025102700024Frame · dentedCOMPLY WITH REO 601R-53-11-4030 (LATEST REVISION) TEMPORARY REPAIR FOR DENT DAMAGE TO FRAME WEB AT FS 241.60 AND BETWEEN RBL 5.50 €“ RBL 11.16. (FILED OPEN)Oct 24, 2025 · N916EV · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA2025100401Skin · dentedONE DENTED AREA ON RT TOP FUSELAGE SKIN, DWG 601R33010. AND ONE DEFORMED AREA ON BS 241.60 FRAME. BETWEEN BS 233.276 - 241.60 BETWEEN BL 0.0 - RBL11.16. REF REO 601R-53-11-4021. REPAIRED DENTED AREA ON RT TOP FUSELAGE SKIN IAW REO 601R-53-11-4022, REV-. COOct 1, 2025 · N916EV · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA202506301112Skin · dentedTHERE IS ONE SMALL PROTRUDING DENT LOCATED IN THE BAY BETWEEN FS 589.00 AND FS 605.00 AND BETWEEN STRINGERS 25L AND 26L. (FILED CLOSED)PERFORMED A PERMANENT REPAIR TO THE AREA OF THE SKIN AND PLATING - REPAIR NO. 1 - EXTERNAL NON-FLUSH PERMANENT REPAIRS - PRENov 12, 2024 · N916EV · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA202506301107Nut Plate · corrodedCORROSION AROUND NUTPLATE SCREW HOLE AT APPROX. FS531.00 AND RBL42.70. (PRESSURE FLOOR) (FILED CLOSED)BLENDED CORROSION AROUND NUTPLATE SCREW HOLE AT APPROX FS531.00 AND RBL 42.70 (PRESSURE FLOOR) WITH REFERENCE TO SRM 51-21-06. PERFORMED UT REMAINING THICKNov 7, 2024 · N916EV · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR SWIA202506301029Bolt · seizedDURING REMOVAL OF THE LH AILERON FOUND THE ANTI ROTATION TAB BOLT SEIZED INTO THE #3 HINGE FITTING (FILED CLOSED)REMOVED AND REPLACED THE LH FITTIING, AILERON, HINGE NO.3 IN REFERENCE WITH THE CRJ-200 SRM 51-42-21, DWG 601R10003 AND DWG 601R10006. COMPLIED WOct 29, 2024 · N916EV · Cndair CL6002B19 · AileronsSDR SWIA202506301025Skin · damagedFUSELAGE BELLY SKIN AND STRUCTURE AT AFT NLG BAY BULKHEAD AT FS 235.00 TO FS 250.00 AND BETWEEN STRINGERS 26L TO 26R DAMAGED DUE TO CONTACT WITH NLG ASSY. (FILED CLOSED)COMPLIED WITH REO 601R-53-11-3953 REV -- DATED: 2024-12-13 AND ISE-STR-24-077 SHORING MEMOOct 25, 2024 · N916EV · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA202506301023Pump · crackedLH BOOST PUMP SATELLITE HOLE ALMOST MOST FORWARD AND SLIGHTLY TO THE LEFT, HAS EDDY CURRENT CRACK INDICATION (HALF SCREEN) GOING OUTBOARD. (FILED CLOSED)REPAIRED LH BOOST PUMP SATELLITE HOLE ALMOST MOST FORWARD AND SLIGHTLY TO THE LEFT IN REF. TO REO 601R-57-Oct 23, 2024 · N916EV · Cndair CL6002B19 · Fuel Boost PumpSDR SWIA202410240003Pump · crackedLH BOOST PUMP SATELLITE HOLE ALMOST MOST FORWARD AND SLIGHTLY TO THE LEFT, HAS EDDY CURRENT CRACK INDICATION (HALF SCREEN) GOING OUTBOARD. (FILED OPEN)Oct 23, 2024 · N916EV · Cndair CL6002B19 · Hydraulic Pump (Electric/Engine), MainSDR SWIA2023050400001Unknown · warning messageCABIN ALT CAUTION, THEN CABIN ALT WARNING. RAN QRH PRESSURE DIFFERENTIAL WOULD NOT GO ABOVE 1.5. SWAPPED BLEEDS TO APU ON DESCENT DID NOT CHANGE. PASSENGER MASKS DROPPED. (FLT 5286 FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 26564546 WITH THE FOMay 1, 2023 · N916EV · Cndair CL6002B19 · Cabin Pressure IndicatorSDR SWIA2023050200001Unknown · warning messageCABIN ALT CAUTION, THEN CABIN ALT WARNING. RAN QRH PRESSURE DIFFERENTIAL WOULD NOT GO ABOVE 1.5. SWAPPED BLEEDS TO APU ON DESCENT DID NOT CHANGE. PASSENGER MASKS DROPPED. (FLT 5286 FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESSMay 1, 2023 · N916EV · Cndair CL6002B19 · Cabin Pressure IndicatorSDR SWIA202163087None · wornPAX DOOR FUSELAGE HALF PIANO HINGE WORN. THIS HAS BEEN DETERMINED TO BE A MAJOR REPAIR, FORM M-337 WILL BE REQUIIRED. REFERENCE CP23945301 ( FILED - CLOSED) NEW PAX DOOR FUSELAGE HALF PIANO HINGE INSTALLED IN REFERENCE TO CRJ200 REO 601R-53-21-656 ALSO INDec 5, 2021 · N916EV · Cndair CL6002B19 · Fuselage, Equipment Attach FittingsSDR ICRR202109010001Link · crackedABNORMAL INDICATION WAS DISCOVERED DURING ULTRASONIC TEST NDT 71-23-103 PART 4. TSN 19209.60 CSN 19729.Sep 1, 2021 · N916EV · Cndair CL6002B19 · Engine Mount SectionSDR SWIA2020091652539Bulkhead · crackedFS 202.75 CRACKED WHERE PARKING BRAKE CABLE PASSES THROUGH IT. C-CHECK RO 9/12/2020. REPAIRED THE FS 202.75 BULKHEAD BETWEEN LBL 22 & LBL 30 AT PARKING BRAKE CABLE PASS THRU, REF MHIRJ REO. ALL CHECKS GOOD, SEE CONTINUATION CARD FOR DETAILS.Aug 14, 2020 · N916EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA2020091652538Pressure Deck · crackedREPAIR CRACK IN THE PRESSURE FLOOR FS 461.00-FS 473.15 BETWEEN BL0-RBL 9, MARKED. C-CHECK RO 9/12/2020. REPAIRED THE PRESSURE FLOOR CRACK FROM FS 461-FS 473.15 LBL 9-RBL 9, REF REO CRJ200 SRM. COMPLIED WITH ST. LEAK CHECKS GOOD.Aug 13, 2020 · N916EV · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA2020091652559Access Panel · chafedFRETTING DAMAGE TO ACCESS PANEL LANDS (540AT, 540BT, 540CT) ON LT WING UPPER PLANK. C-CHECK RO 9/12/2020. BLENDED REPAIR AREA, NDT (0.197?). EVALUATED, OUT OF LIMITS, REF CRJ 200 SRM AND BOMBARDIER DRAWING.Aug 11, 2020 · N916EV · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA2020091652537Access Panel · corrodedFRETTING DAMAGE TO ACCESS PANEL LANDS 640AT, 640BT,640CT ON RT WING UPPER PLANK. C-CHECK RO 9/12/2020. BLENDED REPAIR AREA, NDT ED (0.199?), EVALUATED OUT OF LIMITS. RECEIVED/COMPLIED WITH REO-PART WITHIN LIMITS, RESTORED THE FINISH, REF CRJ 200 SRM, BOMBARAug 11, 2020 · N916EV · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA2020091652549Seat Track · corrodedCORROSION FOUND ON SEAT TRACK SECTION AT RBL 9 FS 559+110 TO 559+121. C-CHECK RO 9/12/2020. LOCATED, DRILLED, AND COUNTERSUNK NEW SEAT TRACK SECTION AT RBL 9 FS 559+110 TO 559+121, REF CRJ200 SRM AND BOMBARDIER STANDARDS MANUAL.Aug 10, 2020 · N916EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2020091652548Seat Track · corrodedCORROSION FOUND ON SEAT TRACK SECTION AT RBL 9 FS 559+86 TO 559+95. C-CHECK RO 9/12/2020. LOCATED, DRILLED, AND COUNTERSUNK NEW SEAT TRACK SECTION AT RBL 9 FS 559+86 TO 559+95, REF CRJ200 SRM AND BOMBARDIER STANDARDS MANUAL.Aug 10, 2020 · N916EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2020091652557Check Valve · inoperativeFS 621.00 PRESSURE BULKHEAD RT FLIGHT COMPARTMENT DISTRIBUTION CHECK VALVE, ONE FLAPPER ON CHECK VALVE WILL NOT CLOSE FULLY. C-CHECK RO 9/12/2020. REMOVED AND REPLACED THE RT PASSENGER COMPARTMENT PRESSURE BULKHEAD CHECK VALVE, REF CRJ200 AMM. LEAK CHECKS GAug 9, 2020 · N916EV · Cndair CL6002B19 · Air Conditioning SystemSDR SWIA2020091652556Check Valve · inoperativeFS 621.00 PRESSURE BULKHEAD LT FLIGHT COMPARTMENT DISTRIBUTION CHECK VALVE, ONE FLAPPER ON CHECK VALVE WILL NOT CLOSE FULLY. C-CHECK RO 9/12/2020. REMOVED AND REPLACED THE LT PRESSURE BULKHEAD CHECK VALVE, REF CRJ200 AMM. LEAK CHECKS GOOD.Aug 9, 2020 · N916EV · Cndair CL6002B19 · Air Distribution SystemSDR SWIA2020091652547Mount · corrodedLEFT WING AILERON POSITION TRANSMITTER HAS CORRODED MOUNT HARDWARE 3 LOCATIONS, MARKED WITH ORANGE FLAG. C-CHECK RO 9/12/2020. REMOVED AND INSTALLED NEW LEFT WING AILERON POSITION TRANSMITTER MOUNT HARDWARE, REF. CRJ 200 AMM. OPS CHECK GOOD.Aug 9, 2020 · N916EV · Cndair CL6002B19 · Wing, Attach FittingsSDR SWIA2020091652536Rib · crackedRT BATT RIB ASSY APPROX 48.3 IS CRACKED, AS MARKED. C-CHECK RO 9/12/2020. REMOVED CRACKED AND INSTALLED NEW RT BATT RIB AT WS 48.3, REF CRJ 200 SRM. FOR FASTENER TYPE AND SIZE REF DRAWINGS. SEE CONTINUATION CARD FOR DETAILS. COMPLETED TASK CARD.Aug 8, 2020 · N916EV · Cndair CL6002B19 · Wing, Rib/BulkheadSDR SWIA2020091652535Rib · crackedLT BATT RIB ASSY APPROX 48.3 IS CRACKED, AS MARKED. C-CHECK RO 9/12/2020. INSTALLED NEW LT BATT RIB AT WS 48.3 (P/N: 600-10389-1), REF CRJ 200 SRM AND DRAWINGS. COMPLIED WITH SKYWEST TASK CARD.Aug 8, 2020 · N916EV · Cndair CL6002B19 · Wing, Rib/BulkheadSDR SWIA2020091652534Door Sill · corrodedSERVICE DOOR LOWER SILL HAS CORROSION. C-CHECK RO 9/12/2020. EVALUATED, OUT OF LIMITS. REPLACED PART, REF CRJ200 SRM BOMBARDIER DRAWING. COMPLIED WITH SKYWEST TASK CARD.Aug 6, 2020 · N916EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020091652533Hinge Fitting · chafedLT CENTER HORIZONTAL STAB ELEVATOR HINGE FITTING HAVE ABRASION DAMAGE, AS MARKED. C-CHECK RO 9/12/2020. BLENDED CHAFED AREA ON THE LT CENTER HORIZONTAL STAB ELEVATOR HINGE FITTING TO A SMOOTH CONTOUR. NDT CHECKED FOR CRACKS WITH NO DEFECTS NOTED. ROTO-PEENAug 6, 2020 · N916EV · Cndair CL6002B19 · Elevator StructureSDR SWIA2020091652532Hinge Fitting · chafedRT OUTBOARD HORIZONTAL STAB ELEVATOR HINGE FITTING HAVE ABRASION DAMAGE, AS MARKED. C-CHECK RO 9/12/2020. BLENDED CHAFED AREA ON THE RT OUTBOARD HORIZONTAL STAB ELEVATOR HINGE FITTING TO A SMOOTH CONTOUR. NDT CHECKED FOR CRACKS WITH NO DEFECTS NOTED. ROTO-Aug 6, 2020 · N916EV · Cndair CL6002B19 · Elevator StructureSDR SWIA2020091652531Hinge Fitting · chafedRT CENTER HORIZONTAL STAB ELEVATOR HINGE FITTING HAVE ABRASION DAMAGE, AS MARKED. C-CHECK RO 9/12/2020. BLENDED CHAFED AREA ON THE RT CENTER HORIZONTAL STAB ELEVATOR HINGE FITTING TO A SMOOTH CONTOUR. NDT CHECKED FOR CRACKS WITH NO DEFECTS NOTED. ROTO-PEENAug 6, 2020 · N916EV · Cndair CL6002B19 · Elevator StructureSDR SWIA2020091652530Skin · gougedRT WING TRAILING EDGE RIB AT OUTBOARD END OF RT SPOILERON HAS A GOUGE ON THE UPPER SURFACE. C-CHECK RO 9/12/2020. BLENDED, NDT (NO DEFECTS) AND EVALUATED REPAIR, FOUND TO BE OUT LIMITS. COMPLIED WITH REO, REPAIR IN LIMITS, REF REO. TOOL MACT1463X DUE 31 MAAug 6, 2020 · N916EV · Cndair CL6002B19 · SpoilersSDR SWIA2020091652546Bracket · crackedLT WING-161 PANEL MOUNT BRACKET CRACKED AS MARKED AT APROX FS 468. C-CHECK RO 9/12/2020. REMOVED CRACKED MOUNT BRACKET AND INSTALLED NEW MOUNT BRACKET P/N 601R31037-61, REF CRJ200 SRM.Aug 4, 2020 · N916EV · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR SWIA2020091652545Bracket · crackedRT WING-162 PANEL MOUNT BRACKET CRACKED AS MARKED AT APROX FS 449. C-CHECK RO 9/12/2020. REPLACED RT WING PANEL 162 MOUNT BRACKET AT FS 461.00, REF CRJ200 SRM.Aug 4, 2020 · N916EV · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR SWIA2020091652544Bracket · crackedRT WING-162 PANEL MOUNT BRACKET CRACKED AS MARKED AT APROX FS 461. C-CHECK RO 9/12/2020. REPLACED RT WING PANEL 162 MOUNT BRACKET AT FS 461.00, REF CRJ200 SRM.Aug 4, 2020 · N916EV · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR SWIA2020091652543Bracket · crackedRT WING-162 PANEL MOUNT BRACKET CRACKED AS MARKED AT APROX FS 468. C-CHECK RO 9/12/2020. REPLACED RT WING PANEL 162 MOUNT BRACKET AT FS 468.00, REF CRJ200 SRM.Aug 4, 2020 · N916EV · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR SWIA2020091652542Bracket · crackedRT WING-162 PANEL MOUNT BRACKET CRACKED AS MARKED AT APROX FS 476. C-CHECK RO 9/12/2020. REPLACED RT WING PANEL 162 MOUNT BRACKET AT FS 476.00, REF CRJ200 SRM.Aug 4, 2020 · N916EV · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR SWIA2020091652529Attach Fitting · nickedLT OUTBOARD FLAP WS 220 FWD HINGE BOX ATTACHMENT LUG HAS NICKS/BURRS THAT NEED BLENDING AND TOUCH UP, AS MARKED. C-CHECK RO 9/12/2020. BLENDED LT OUTBOARD FLAP HINGE BOX FWD ATTACHMENT LUG AT WS 220.00 TO A SMOOTH CONTOUR, REF REO. COMPLIED WITH TASK CARD.Aug 4, 2020 · N916EV · Cndair CL6002B19 · Wing, Nacelle/Pylon Attach FittingsSDR SWIA2020091652528Attach Fitting · nickedLT OUTBOARD FLAP WS 220 AFT HINGE BOX ATTACHMENT LUG HAS NICKS/BURRS THAT NEED BLENDING AND TOUCH UP, AS MARKED. C-CHECK RO 9/12/2020. BLENDED LT OUTBOARD FLAP HINGE BOX AFT ATTACHMENT LUG AT WS 220.00 TO A SMOOTH CONTOUR, REF REO. COMPLIED WITH TASK CARD.Aug 4, 2020 · N916EV · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2020091652527Attach Fitting · nickedLT OUTBOARD FLAP WS 178 AFT HINGE BOX ATTACHMENT LUG HAS NICKS/BURRS THAT NEED BLENDING AND TOUCH UP, AS MARKED. C-CHECK RO 9/12/2020. BLENDED LT OUTBOARD FLAP HINGE BOX AFT ATTACHMENT LUG AT WS 178.00 TO A SMOOTH CONTOUR, REF REO. COMPLIED WITH TASK CARD. Aug 4, 2020 · N916EV · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2020091652526Bracket · crackedCLIP ON FRAME AT APPROX FS 625 ON THE LEFT SIDE OF THE AIRCRAFT IS CRACKED, FLAGGED. C-CHECK RO 9/12/2020. REMOVED AND REPLACED INTERCOSTAL CLIP BETWEEN FS 621-625 ADJACENT TO STRINGER 14 LT, REF CRJ200 SRM AND REO. COMPLIED WITH TASK CARD.Aug 4, 2020 · N916EV · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR SWIA2020091652525Bracket · crackedCLIP ON FRAME AT APPROX FS 625 ON THE RIGHT SIDE OF THE AIRCRAFT IS CRACKED, FLAGGED. C-CHECK RO 9/12/2020. REMOVED AND REPLACED INTERCOSTAL CLIP BETWEEN FS 621-625 ADJACENT TO STRINGER 14 RT, REF CRJ200 SRM AND REO. COMPLIED WITH TASK CARD.Aug 4, 2020 · N916EV · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR SWIA2020091652524Floor Support · corrodedRT FLOOR SILL HAS MULTIPLE AREAS OF CORROSION (X7) FS 280 THRU FS 409.00, CIRCLED WITH GREASE PENCIL. C-CHECK RO 9/12/2020. REPAIRED ALL MARKED AREAS OF CORROSION, BLENDS MARKED NR 1 AND NR 6 WITHIN LIMITS, REF REO ALL STEPS COMPLIED WITH. REMAINING AREAS RAug 4, 2020 · N916EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020091652558Gusset · gougedGUSSET FOR FRAME AT APPROX FS 559+48 AND APPROX STGR 6R IS GOUGED, FLAGGED. C-CHECK RO 9/12/2020. FOUND DAMAGES ON OVERHEAD BIN DRAG LINK GUSSET AT FRAME AT APPROX FS 559+48 AND APPROX STGR 6R OUT OF LIMIT WITH 100% MATERIAL LOSS. REPLACED GUSSET WITH NEW FAug 3, 2020 · N916EV · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA2020091652523Mount Bracket · corrodedRT FS 310/FS 319.00 STGR 17 RT OUTBOARD GALLEY MOUNT PLATE IS CORRODED, FLAGGED. C-CHECK RO 9/12/2020. REPLACED RT OUTBOARD GALLEY MOUNT PLATE BETWEEN FS 310.00 & FS 319.00 AT STGR 17, REF BOMBARDIER DWG CRJ200 SRM. COMPLIED WITH TASK CARD.Aug 3, 2020 · N916EV · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR SWIA2020091652522Skin · corrodedLEFT WING LOWER PLANK ACCESS HOLE FOR PANEL 510AB HAS PITTING AND SIGNS OF CORROSION ON THE LANDING AREA. C-CHECK RO 9/12/2020. REMOVED PITTING AND EVIDENCE OF CORROSION PART IN LIMITS. RESTORED PEEN/FINISH, COMPLIED WITH ALL STEPS OF REO, REF REO.Aug 3, 2020 · N916EV · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA2020091652521Skin · corrodedRIGHT WING LOWER PLANK ACCESS HOLE FOR PANEL 640BB HAS PITTING AND SIGNS OF CORROSION ON THE LANDING AREA. C-CHECK RO 9/12/2020. REMOVED PITTING AND EVIDENCE OF CORROSION PART IN LIMITS. RESTORED PEEN/FINISH, COMPLIED WITH ALL STEPS OF REF REO. LEAK CHECKSAug 3, 2020 · N916EV · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA2020091652520Floor Support · corrodedLT FS 409.00+128 TO FS 559.00 UPPER FLOOR SILL PANEL HAVE NUMEROUS AREAS OF CORROSION, AS MARKED. C-CHECK RO 9/12/2020. REMOVED CORROSION FROM 17 LOCATIONS ON LT UPPER FLOOR SILL PANEL BETWEEN FS 409.00+128 AND FS 559.00. ALL 17 BLEND LOCATIONS ARE WITHIN LAug 3, 2020 · N916EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020091652519Floor Support · corrodedLBL 9 HAS MULTIPLE SPOTS OF CORROSION FROM FS 409.0+128 TO FS 559.0. C-CHECK RO 9/12/2020. COMPLIED WITH REO FOR REPAIR CORROSION FROM FS 409.0+128 TO FS 559.0 LBL 9.0 FLOOR BEAM CAP INBOARD AND OUTBOARD FLANGES. COMPLIED WITH SKY CARD.Aug 3, 2020 · N916EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020091652518Floor Support · corrodedRBL 9 HAS MULTIPLE SPOTS OF CORROSION FROM FS 409.0+128 TO FS 559.0. C-CHECK RO 9/12/2020. COMPLIED WITH PERMANENT REPAIR RBL 9 FLOOR SUPPORT CORROSION FROM FS 409+128 TO FS 559, REF REO. VERIFIED ALL STEPS 1-5 COMPLIED WITH, COMPLETED TASK CARD. WEIGHT CHAug 3, 2020 · N916EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020091652517Intercostal · gougedINTERCOSTAL GOUGED AT APPROX STGR 10R ON THE FWD SIDE OF THE RT EMER DOOR SURROUND STRUCTURE. C-CHECK RO 9/12/2020. REMOVED AND REPLACED THE INTERCOSTAL AT THE EMER SURROUND STRUCTURE STR 10R, REF DRAWING CRJ200 SRM. COMPLIED WITH ST, ALL CHECKS GOOD.Aug 3, 2020 · N916EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
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