N744EV

Service difficulty reports · 326

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 = 'N744EV' 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 SWIA202052837Tie Down · corrodedFWD CARGO BAY TIEDOWN MOUNT PLATE CORRODED, AS MARKED, FS 533 BETWEEN STGRS 22L/23L. C-CHECK RO 9/27/2020. COMPLETED REO FOR FWD CARGO BAY TIE DOWN MOUNT PLATE BRACKET. SEE CONTINUATION CARD FOR WORK PERFORMED.Aug 25, 2020 · N744EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA202052836Stringer · corrodedFWD CARGO BAY STRINGER CORRODED, AS MARKED, FS 533-STGR 22L. C-CHECK RO 9/27/2020. REMOVED AND INSTALLED NEW STRINGER SECTION FWD CARGO BAY STRINGER FS 533-STGR 22L, REF CRJ-700 SRM AND DWG. SEE CONTINUE CARD FOR MORE DETAILS. ALL CHECK GOOD. COMPLIED WIAug 25, 2020 · N744EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA202052834Strap · corrodedLT EMER EXIT SURROUND, LOWER INNER STRAP HAS CORROSION. C-CHECK RO 9/27/2020. REPAIRED CORROSION ON LT EMERGENCY EXIT SURROUND LOWER INNER STRAP, IAW CRJ 700 SRM. BLEND OUT WAS WITHIN LIMITS. SEE CONTINUATION CARD FOR DETAILS.Aug 24, 2020 · N744EV · Cndair CL6002C10 · Emergency ExitsSDR SWIA202052833Skin · gougedPAX DOOR OUTER SKIN UPPER FWD CORNER HAS NUMEROUS GOUGES AND SCRAPES. C-CHECK RO 9/27/2020. REPAIRED DAMAGE TO PAX DOOR OUTER SKIN UPPER FWD CORNER, REF CRJ700 SRM AND COMPLIED WITH ALL STEPS OF REO. NO DEFECTS NOTED. COMPLIED WITH TASK CARD.Aug 24, 2020 · N744EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWIA202052832Seat Track · corrodedRT FLOOR SEAT TRACK RAIL AT APPROX FS 485-FS 581 HAS CORROSION. C-CHECK RO 9/27/2020. REMOVED CORROSION ON RT FLOOR SEAT TRACK RAIL AT APPROX FS 485-FS 581, REF CRJ-700 SRM. MEASURED AND EVALUATED SEAT TRACK, FOUND TO BE OUT OF LIMITS AND HAS MORE THAN ONE Aug 24, 2020 · N744EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA202052831Seat Track · corrodedRT FLOOR SEAT TRACK RAIL AT APPROX FS 581-FS 683 HAS CORROSION. C-CHECK RO 9/27/2020. REMOVED AND REPLACED FLOOR TRACK AT APPROX FS 581-683 ON THE RT SIDE, REF CRJ700 AMM.Aug 24, 2020 · N744EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA202052830Seat Track · corrodedLT FLOOR SEAT TRACK RAIL AT APPROX FS 581-FS 683 HAS CORROSION. C-CHECK RO 9/27/2020. REMOVED AND REPLACED LT FLOOR SEAT TRACK AT APPROX FS 581-FS 683, REF CRJ-700 SRM.Aug 24, 2020 · N744EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA202052829Seat Track · corrodedLT FLOOR SEAT TRACK RAIL AT APPROX FS 485-FS 581 HAS CORROSION. C-CHECK RO 9/27/2020. REMOVED AND REPLACED LT FLOOR TRACK RAIL AT APPROX FS 485-581, REF CRJ700 AMM.Aug 24, 2020 · N744EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA202052828Seat Track · corrodedRT FLOOR SEAT TRACK RAIL AT APPROX FS 349-FS 485 HAS CORROSION. C-CHECK RO 9/27/2020. REMOVED CORROSION ON RT FLOOR SEAT TRACK RAIL AT APPROX FS 349-FS 485, REF CRJ-700 SRM. MEASURED AND EVALUATED SEAT TRACK, FOUND TO BE OUT OF LIMITS, AND HAS MORE THAN ONEAug 24, 2020 · N744EV · Cndair CL6002C10 · Fuselage, Powerplant Attach FittingsSDR SWIA202052827Seat Track · corrodedLT FLOOR SEAT TRACK RAIL AT APPROX FS 379-FS 485 HAS CORROSION. C-CHECK RO 9/27/2020. REMOVED AND REPLACED LT FLOOR SEAT TRACK RAIL AT APPROX FS 379-485, REF CRJ700 AMM.Aug 24, 2020 · N744EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA202052826Seat Track · corrodedRT SIDE SEAT TRACK RAIL AT APPROX FS 573-FS 669.40 HAS CORROSION. C-CHECK RO 9/27/2020. REMOVED CORROSION DAMAGE ON RT SEAT TRACK RAIL AT APPROX FS 573-FS 669.40, REF CRJ-700 SRM. SEE CONTINUATION CARD FOR DETAILS.Aug 24, 2020 · N744EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA202052825Seat Track · corrodedRT SIDE SEAT TRACK RAIL AT APPROX FS 485-FS 573 HAS CORROSION. C-CHECK RO 9/27/2020. REPLACED WITH NEW RT SIDE SEAT RAIL TRACK AT APPROXIMATELY FS 485.00-FS 573.00, REF CRJ700 AMM.Aug 24, 2020 · N744EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA202052824Seat Track · corrodedRT SIDE SEAT TRACK RAIL AT APPROX FS 379-FS 485 HAS CORROSION. C-CHECK RO 9/27/2020. REMOVED & REPLACED WITH NEW RT SEAT TRACK RAIL AT APPROX FS 379.00-FS 485.00, REF CRJ700 AMM. SEE CONTINUATION CARD FOR DETAILS.Aug 24, 2020 · N744EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA202052823Seat Track · corrodedRT SIDE SEAT TRACK RAIL AT APPROX FS 784-FS 855 HAS CORROSION. C-CHECK RO 9/27/2020. RT SIDE SEAT TRACK RAIL FS 784-FS 855 CORROSION FOUND TO BE OUT OF LIMITS, IAW CRJ700 SRM. REMOVED AND REPLACED SEAT RAIL, IAW CRJ 700 SRM. SEE CONTINUATION CARD FOR WORK Aug 24, 2020 · N744EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA202052822Seat Track · corrodedRT SIDE SEAT TRACK RAIL AT APPROX FS 713-FS 763 HAS CORROSION. C-CHECK RO 9/27/2020. REPLACED RT SEAT TRACK RAIL APPROX FS 713.00-FS 763.00, REF CRJ 700 SRM. SEE CONTINUATION CARD FOR DETAILS.Aug 24, 2020 · N744EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA202052821Seat Track · corrodedLT SIDE SEAT TRACK MOUNTING CHANNEL AT APPROX FS 784-FS 855 HAS CORROSION. C-CHECK RO 9/27/2020. REMOVED & REPLACED WITH NEW LT SIDE SEAT TRACK MOUNTING CHANNEL AT APPROX FS 784-FS 855, REF CRJ 700 SRM. SEE CONTINUATION CARD FOR DETAILS.Aug 24, 2020 · N744EV · Cndair CL6002C10 · Fuselage, Powerplant Attach FittingsSDR SWIA202052820Seat Track · corrodedLT SIDE SEAT TRACK RAIL AT APPROX FS 784-FS 855 HAS GOUGES AND CORROSION. C-CHECK RO 9/27/2020. REMOVED & REPLACED SEAT TRACK A NEW LT SIDE SEAT TRACK RAIL APPROX AT FS 784.00-FS 855.00, REF CRJ 700 SRM. SEE CONTINUATION CARD FOR DETAILS.Aug 24, 2020 · N744EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA202052819Seat Track · corrodedLT SIDE SEAT TRACK MOUNTING CHANNEL AT APPROX FS 741-FS 763 HAS CORROSION. C-CHECK RO 9/27/2020. CORROSION REMOVED FROM LT SIDE SEAT TRACK MOUNT CHANNEL FS 741-FS 763, REF CRJ SRM. SEE CONTINUATION CARD FOR WORK COMPLETED.Aug 24, 2020 · N744EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA202052818Skin · corrodedFS 939.00 FS 969.00 STRG 21 LT 21 RT CORROSION ON EXTERIOR SKIN AROUND SEVERAL FASTENERS, MARKED. C-CHECK RO 9/27/2020. BLENDED-OUT CORROSION AT FS 939.00 FS 969.00 STRG 21 LT 21 RT CORROSION ON EXTERIOR SKIN AROUND SEVERAL FASTENER, REF CRJ-700 SRM, WITHIAug 24, 2020 · N744EV · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR SWIA202052817Diaphragm · crackedFS 909.00 STRG 24LH DIAPHRAGM CRACKED BOTTOM CORNER, MARKED. C-CHECK RO 9/27/2020. REPAIRED CRACK AT FS 909.00 STRG 24LH, DIAPHRAGM BOTTOM CORNER BY COMPLYING WITH REO. SEE CONTINUATION CARD FOR DETAILS.Aug 24, 2020 · N744EV · Cndair CL6002C10 · Fuselage Main, StructureSDR SWIA202052816Door Sill · corrodedCARGO DOOR SURROUND STRUCTURE SILL CORRODED MULTIPLE AREAS, AS MARKED. C-CHECK RO 9/27/2020. EVALUATED CARGO DOOR SILL OUT OF LIMITS. REMOVED AND REPLACED CARGO DOOR LOWER SILL, REF CRJ700 SRM AND DWG. NO LEAKS NOTED. COMPLIED WITH TASK CARD.Aug 24, 2020 · N744EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA202052815Door Frame · crackedCARGO DOOR SURROUND STRUCTURE FS 1047 BETWEEN STGRS 12L/13L, DOOR FRAME STRUCTURE BRACKET HAS SUSPECTED CRACK, AS MARKED. C-CHECK RO 9/27/2020. REMOVED AND INSTALLED NEW BRACKET, GUSSET, AND INTERCOSTAL, REF CRJ700 SRM, AND DWG. NO LEAKS NOTED. COMPLIED WIAug 24, 2020 · N744EV · Cndair CL6002C10 · Fuselage Main, StructureSDR SWIA202052814Nut Plate · damagedCARGO DOOR SURROUND STRUCTURE FS 1000 ABOVE SILL, NUTPLATE HAS BROKEN RIVET, AS MARKED. C-CHECK RO 9/27/2020. REMOVED AND REPLACED 1 EA NUTPLATE RIVET AT FS 1000 ABOVE SILL, REF CRJ700 SRM.Aug 24, 2020 · N744EV · Cndair CL6002C10 · Cargo/Baggage DoorsSDR SWIA202052813Retainer · crackedRT TRU AFT LATCH RETAINER IS POSSIBLY CRACKED, FLAGGED. C-CHECK RO 9/27/2020. REMOVED AND REPLACED WITH NEW RT TRU DOOR LAND, REF CRJ-700 SRM 51-42-06-001-001-A01 AND MHIRJ REO COMPLIED WITH.Aug 23, 2020 · N744EV · Cndair CL6002C10 · DoorsSDR SWIA202052812Hinge Fitting · damagedRT AILERON CENTER HINGE FITTING INBOARD LUG HAS SMALL NICK ON THE LOWER SURFACE. C-CHECK RO 9/27/2020. REPAIRED NICK DAMGE TO RT AILERON, CENTER HINGE FITTING, INBOARD LUG, REF CRJ-700 SRM AND REO. SEE CONTINUATION FOR DETAILS.Aug 22, 2020 · N744EV · Cndair CL6002C10 · AileronsSDR SWIA202052811Roll Pin · migratedROLL-PIN IN PAX DOOR HINGE HAS MIGRATED AND GOUGED THE LAST (AFT) LUG LAND ON THE PAX DOOR HINGE FUSELAGE SIDE. C-CHECK RO 9/27/2020. PAX DOOR HINGE FUSELAGE SIDE FOUND TO BE OUT OF LIMITS. ALL LUGS INNER HOLES ARE OVER SIZES TOOL NR TUC8495, IAW BOMBARDIERAug 20, 2020 · N744EV · Cndair CL6002C10 · Fuselage, Door HingeSDR SWIA202052810Skin · chafedCHAFE IN EXTERNAL FUSELAGE SKIN AFT OF CIRCUMFERENTIAL JOINT AT FS 977 AND STGR 27. C-CHECK RO 9/27/2020. BLENDED OUT CHAFE, FOUND TO BE IN LIMITS. RESTORED FINISH, IAW MHIRJ REO AND CRJ700 SRM.Aug 19, 2020 · N744EV · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR SWIA202052809Skin · chafedCHAFE IN EXTERNAL FUSELAGE SKIN FWD OF CIRCUMFERENTIAL JOINT AT FS 977 AND STGR 27. C-CHECK RO 9/27/2020. BLENDED OUT CHAFE, FOUND TO BE OUT OF LIMITS, REQUESTED ENGINEERING. COMPLIED WITH MHIRJ REO. RESTORED FINISH IAW CRJ700 SRM. ALL STEPS OF THE REO COAug 19, 2020 · N744EV · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR SWIA202052808Drag Angle · crackedLT V/STAB TO FUSELAGE ATTACHMENT DRAG ANGLE AFT POSSIBLE CRACK, MARKED. C-CHECK RO 9/27/2020. PERFORMED NDT INSP OF LT V/STAB TO FUSELAGE ATTACHMENT AFT DRAG ANGLE. FOUND AFT DRAG ANGLE CRACKED, REF CRJ-700 NDT. PERFORMED REO REPAIR TO V/STAB TO FUSELAGE AAug 19, 2020 · N744EV · Cndair CL6002C10 · Vertical StabilizerSDR SWIA202052807Drag Angle · crackedLT V/STAB TO FUSELAGE ATTACHMENT DRAG ANGLE FWD POSSIBLE CRACK, MARKED. C-CHECK RO 9/27/2020. PERFORMED NDT INSP OF LT V/STAB TO FUSELAGE ATTACHMENT FWD DRAG ANGLE. FOUND AFT DRAG ANGLE CRACKED, REF CRJ-700 NDT. PERFORMED REO REPAIR TO V/STAB TO FUSELAGE AAug 19, 2020 · N744EV · Cndair CL6002C10 · Vertical StabilizerSDR SWIA202052806Skin · gougedAFT CARGO DOOR ENTRANCE EXTERIOR SKIN GOUGED FWD LOWER CORNER, MARKED. C-CHECK RO 9/27/2020. PERFORMED GOUGE REPAIR ON AFT CARGO DOOR CUT OUT SKIN FWD LOWER CORNER BY COMPLYING WITH REO DISPOSITION STEPS 1-4. SEE CONTINUATION CARD FOR DETAILS. COMPLIED WITAug 19, 2020 · N744EV · Cndair CL6002C10 · Cargo/Baggage DoorsSDR SWIA202052805Skin · gougedAFT CARGO DOOR ENTRANCE EXTERIOR SKIN GOUGED AFT LOWER CORNER, MARKED. C-CHECK RO 9/27/2020. PERFORMED GOUGE REPAIR ON AFT CARGO DOOR CUT OUT SKIN AFT LOWER CORNER BY COMPLYING WITH REO. DISPOSITION STEPS 1-4. SEE CONTINUATION CARD FOR DETAILS. COMPLIED WAug 19, 2020 · N744EV · Cndair CL6002C10 · Cargo/Baggage DoorsSDR SWIA202052804Skin · damagedSKIN BEHIND LEFT WING LEADING EDGE PANEL 522HZ HAS ELONGATED HOLE. C-CHECK RO 9/27/2020. EVALUATED AND FOUND DAMAGE ONLY ON SUPPORT ANGLE OF PANEL 522HZ. ANGLE FOUND TO BE OUT OF LIMITS, REF CRJ-700 SRM. REMOVED AND INSTALLED NEW 522HZ SUPPORT ANGLE, REF DAug 18, 2020 · N744EV · Cndair CL6002C10 · Wing, Plate/SkinSDR SWIA202052803Floor Panel · crackedCOCKPIT PANEL 222EZ IS CRACKED. C-CHECK RO 9/27/2020. REPAIRED PANEL 222EZ USING FG-778138-504 PO T47401 AND 828-3223 RESIN, PER C&D ZODIAC CMM. COMPLIED WITH TASK CARD.Aug 18, 2020 · N744EV · Cndair CL6002C10 · Fuselage Floor PanelSDR SWIA202052802Liner · damagedCARGO LINER 281KLW HAS WORN/DAMAGED COMPOSITE. C-CHECK RO 9/27/2020. REPAIRED PANEL 281KLW USING FG-778138-504 PO T47401 AND 828-3223 RESIN, PER ZODIAC AEROSPACE CMM. COMPLIED WITH TASK CARD.Aug 17, 2020 · N744EV · Cndair CL6002C10 · Cargo/Baggage DoorsSDR SWIA202052801Skin · chafedGALLEY SERVICE DOOR INTERIOR FWD SKIN IS CHAFED, FLAGGED. C-CHECK RO 9/27/2020. REMOVED CHAFE AREA ON SERVICE DOOR INTERIOR SKIN, REF CRJ700 SRM. FOUND TO BE WITHIN LIMITS, REF CRJ700 SRM. SEE CONTINUATION CARD FOR DETAILS.Aug 16, 2020 · N744EV · Cndair CL6002C10 · Galley DoorsSDR SWIA202052800Skin · chafedRT SLAT NR 3 INNER SKIN UPPER TRAILING EDGE CHAFED IN SEVERAL AREAS, MARKED. C-CHECK RO 9/27/2020. REMOVED CHAFING IN SEVERAL AREAS ON RT SLAT NR 3 INNER SKIN UPPER TRAILING EDGE, REF CRJ700 SRM. COMPLIED WITH ALL STEPS OF MHIRJ REO.Aug 16, 2020 · N744EV · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA202052799Skin · chafedRT SLAT NR 2 INNER SKIN UPPER TRAILING EDGE CHAFED IN SEVERAL AREAS, MARKED. C-CHECK RO 9/27/2020. REPAIRED CHAFE DAMAGE AT RT SLAT NR 2 INNER SKIN UPPER TRAILING EDGE, REF REO. SEE CONTINUATION CARD FOR WORK DETAILS.Aug 16, 2020 · N744EV · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA202052798Skin · chafedRT SLAT NR 1 INNER SKIN UPPER TRAILING EDGE CHAFED IN SEVERAL AREAS, MARKED. C-CHECK RO 9/27/2020. REPAIRED CHAFE DAMAGE AT RT SLAT NR 1 INNER SKIN UPPER TRAILING EDGE, REF REO. SEE CONTINUATION CARD FOR WORK DETAILS.Aug 16, 2020 · N744EV · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA202052797Skin · chafedLT AILERON UPPER LEADING EDGE CHAFED IN SEVERAL AREAS, MARKED. C-CHECK RO 9/27/2020. ORIGINAL MATERIAL THICKNESS OF LT AILERON UPPER LEADING EDGE PANEL IS 0.090? AND 0.055? CHEM MILLED POCKET, REF CRJ700 SRM. TOTAL MATERIAL REMOVED IS 0.032? MEASURED USING Aug 16, 2020 · N744EV · Cndair CL6002C10 · AileronsSDR SWIA202052796Skin · chafedLT SLAT NR 2 INNER SKIN UPPER TRAILING EDGE CHAFFED IN SEVERAL AREAS, MARKED. C-CHECK RO 9/27/2020. REWORKED CHAFE DAMAGE TO LT SLAT NR 2 TRAILING EDGE, PER REO.Aug 16, 2020 · N744EV · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA202052795Skin · erodedLT SLAT NR 3 LEADING EDGE HAS EROSION THE ENTIRE LENGTH. C-CHECK RO 9/27/2020. REMOVED EROSION DAMAGE FROM LT SLAT NR 3 LEADING EDGE, REF MHIRJ REO. SEE CONTINUATION FOR WORK DETAILS.Aug 16, 2020 · N744EV · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA202052794Skin · nickedPANEL 521AT NICKED ON OUTER SKIN, MARKED. C-CHECK RO 9/27/2020. BLENDED OUT NICK ON OUTER SKIN OF PANEL 521AT, WITHIN ALLOWABLE LIMITS. ORIGINAL .090, REMAINING .083" WITH .007" MATERIAL LOSS, REF CRJ-700 SRM AND RESTORED FINISH REF CRJ-700 SRM. SEE CONTINAug 16, 2020 · N744EV · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR SWIA202052793Panel · damagedAFT CARGO AFT RT CORNER VERTICLE GILLINER PANEL W/DECOM PANEL, SHOWS EVIDENCE OF PHYSICAL DAMAGE SEVERAL AREAS, AS MARKED. C-CHECK RO 9/27/2020. REPAIRED AFT CARGO RT CORNER VERTICLE GILLINER AREAS, AS MARKED. APPLIED GLASS CLOTH REPAIR RESIN RESTORED FINISAug 16, 2020 · N744EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2018120745339Intercostal · dentedPASSENGER DOOR INTERCOSTAL DD7 (P/N 601R318826-1) TOP FLANGE DENTED. (C-CHECK) RO: 12/06/2018 REMOVED AND REPLACED PASSENGER DOOR INTERCOSTAL DD7 IAW SRM. PRESSURIZED THE AIRCRAFT IAW AMM AND CHECKED FOR LEAKS IN THE REPAIR AREA. NO LEAKS NOTED.Nov 19, 2018 · N744EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWIA2018120745338Skin · dentedRH#2 SLAT HAS DENT AT WS178.00 - WS295.00. (C-CHECK) RO: 12/06/2018 DRESSED DENT IAW REO. OPS TEST GOOD AT THIS TIME.Oct 23, 2018 · N744EV · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA2018120745337Skin · dentedRH #1 SLAT DENT AT WS48.95 - WS178.00. (C-CHECK) RO: 12/06/2018 DRESSED DENT IN R/H #1 SLAT AT SS110.00 BACK TO ORIGINAL CONTOUR IAW REO. ALL CHECKS GOOD.Oct 22, 2018 · N744EV · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA2018120745336Skin · dentedDENT ON RHS OF FUSELAGE AT FS409 TO FS421. (C-CHECK) RO: 12/06/2018 COMPLIED WITH REPAIR TO THE DENT ON R/H FUSELAGE FS 409 TO FS 421 IAW SRM ALL STEPS. PRESSURIZED THE AIRCRAFT IAW AMM AND CHECKED FOR LEAKS AT THE REPAIR AREA. NO LEAKS NOTED.Oct 22, 2018 · N744EV · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR SWIA2018120745335Spigot · crackedLH ENGINE PANEL 433AL HAS CRACKED SPIGOT. (C-CHECK) RO: 12/06/2018 REMOVED AND REPLACED SPIGOT P/N CN624-2067-205 ON TO PANEL 433AL IAW SRM.Oct 18, 2018 · N744EV · Cndair CL6002C10 · Nacelle/Pylon StructureSDR SWIA2018120745334Panel · chafedLH ENGINE PANEL 433AL HAS CHAFING ON THE TOPHAT. (C-CHECK) RO: 12/06/2018 REMOVED AND REPLACED P/N CN624-2025-201 IAW SRM.Oct 18, 2018 · N744EV · Cndair CL6002C10 · Nacelle/Pylon, Main Frame
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