N917EV

Service difficulty reports · 231

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 = 'N917EV' 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 SWIA2025100700030Floor Support · corrodedCOCKPIT FLOORBOARD 221ALF FORWARD SUPPORT ANGLE HAS CORROSION. (C-CHECK RO 10/06/2025) REMOVED AND REPLACED THE FORWARD SUPPORT INTERCOSTAL ANGLE (P/N 600-33110-667) AT COCKPIT FLOORBOARD 221ALF REF REO 601R-53-11-4012 REV--, DATED 2025-08-22, REO 601R-53-11-Jul 30, 2025 · N917EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2025F01418Skin · damagedFOUND THROUGH HOLES ELONGATED AT RH ELEVATOR WING TIP STRUCTURE 30515409 (C-CHECK RO 10/06/2025)COMPLIED WITH REPAIR TO RH H-STAB TIP FAIRING ATTACHMENT HOLES REF REO 601R-55-11-800 REV -- DATED: 2025-09-04. COMPLIED WITH SKYWEST TASK CARD: 51-900-1003-SKY.Jul 19, 2025 · N917EV · Cndair CL6002B19 · Elevator, Plate/SkinSDR SWIA2025100700719Floor Support · corrodedLH PRESSURE FLOOR SILL ANGLE HAS AN EXISTING REPAIR BETWEEN FS 449.85 AND FS 461.50 AT LBL 42 WHERE TWO AREAS OF CORROSION WERE BLENDED OUT REQUIRING REPLACEMENT OF REPAIR DOUBLER. (CAMP# 30512586) (C-CHECK RO 10/06/2025)REMOVED AND REPLACED -1 DOUBLER OF EXJul 19, 2025 · N917EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2025100700618Floor Support · corrodedLH PRESSURE FLOOR SILL ANGLE CORRODED FROM FS409+128 TO FS559. (C-CHECK RO 10/06/2025)REMOVED CORROSION ON THE LEFT-HAND PRESSURE FLOOR SILL ANGLE, AT FS409+128 TO FS559.00, AND EVALUATED AS WITHIN LIMITS. RECEIVED AND COMPLIED WITH ALL STEPS OF REO 601R-53-Jun 18, 2025 · N917EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2025100700609Hinge · damagedPASSENGER DOOR PIANO HINGE HALF ON FUSELAGE SIDE, PITTING ON THE FORWARD LUG, HR00552377 (C-CHECK RO 10/06/2025)REMOVED AND REPLACED PAX DOOR PIANO HINGE (P/N 600-31529-15) ON FUSELAGE SIDE REF REF 601R-53-21-814 REV C, DATED 2017-08-02, REO 601R-53-21-6Jun 9, 2025 · N917EV · Cndair CL6002B19 · Fuselage, Door HingeSDR SWIA2025F01426Hinge Fitting · chafedRH ELEV CENTER HINGE FITTING (#3 ON HSTAB) CHAFFED AT BOTTOM BY FLUTTER DAMPER SHAFT AREA (MARKED) (C-CHECK RO 10/06/2025)RH ELEVATOR CENTER HINGE FITTING (#2 ON HSTAB) CHAFFED AT BOTTOM. REMOVED DAMAGE AT RH ELEVATOR CENTER HINGE FITTING (#2 ON HSTAB). REF: Jun 5, 2025 · N917EV · Cndair CL6002B19 · Elevator StructureSDR SWIA2025100700605Hinge Fitting · damagedRH ELEV CENTER HINGE FITTING (#3 ON HSTAB) BOTH LOBES HAVE TOOLING DAMAGE (MARKED) (C-CHECK RO 10/06/2025)REMOVED TOOLING DAMAGE ON THE RIGHT-HAND CENTER ELEVATOR, HINGE FITTING #2 (#3 FROM INBD TO OUTBD), AND EVALUATED AS 'OUT-OF-LIMITS'. RECEIVED AND COMPJun 5, 2025 · N917EV · Cndair CL6002B19 · Elevator StructureSDR SWIA2025100700603Attach Fitting · corrodedRH WING FWD ATTACHMENT FITTING FOR HINGE BOX AT WS80.5 IS CORRODED. (C-CHECK RO 10/06/2025) REMOVED CORROSION AT RH WING FWD ATTACHMENT FITTING FOR HINGE BOX AT WS80.5 PER CRJ200 SRM 51-21-06 AND PERFORMED REPAIR PER REO 601R-57-21-3951 REV -- DATED 2025-07-Jun 3, 2025 · N917EV · Cndair CL6002B19 · Wing, Attach FittingsSDR SWIA2025F01425Hinge Fitting · chafedLH WING HINGE BOX AFT FITTINGS ARE CHAFED AT WS264. (C-CHECK RO 10/06/2025)BLENDED DAMAGE FROM LH HINGE BOX AFT ATTACHMENTS AT WS264, OUT OF LIMITS, COMPLIED WITH ROTOPEEN AND RESTORE OF FINISH REF REO 601R-57-21-3939 REV-- DATED 2025-06-19 COMPLIED WITH SKYWJun 2, 2025 · N917EV · Cndair CL6002B19 · Wing Main, Frame StructureSDR SWIA2025100700602Frame · crackedINTERIOR FRAME CRACK AT FS333 BETWEEN STGR 0-1L, HN00246106 (C-CHECK RO 10/06/2025) COMPLIED WITH REPAIR TO FRAME FS333.00 BETWEEN STGR 0 - 1L REF REO 601R-53-21-3750 REV -- DATE 2025-07-04 REPAIR STEPS 1-13. COMPLIED WITH TASK CARD 51-90-1003-SKY.Jun 2, 2025 · N917EV · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA2025F01417Skin · dentedFS625.00 - FS640.00 STRG 25LH - 26LH EXTERIOR FUSELAGE SKIN DENT (C-CHECK RO 10/06/2025) REPAIRED EXTERIOR FUSELAGE SKIN DENT AT FS625.00 - FS640.00 STRG 25LH - 26LH REF REO 601R-53-61-8362 REV--, DATED 2025-08-01. COMPLIED WITH ALL STEPS. COMPLIED WITH TASKMay 30, 2025 · N917EV · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA2025F01416Floorbeam · crackedFS280.00 LBL 9, THE INBD FLOOR BEAM TO CROSS BEAM ATTACH ANGLE CRACKED (MARKED) (C-CHECK RO 10/06/2025) REMOVED AND REPLACED CLIP, AT FS280.00 LBL 9 FLOOR BEAM, PN: 601R31113-54 REF DWG NO. 601R31113 REV AD AND, CRJ 200 SRM 51-41-21. AND COMPLIED WITH SKY CAMay 30, 2025 · N917EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA2025100700530Skin · dentedFS625.00 - FS640.00 STRG 26LH - 27, INTERIOR FUSELAGE SKIN DENT, PROTRUDING EXTERNALLY (MARKED) (C-CHECK RO 10/06/2025)REPAIRED INTERIOR FUSELAGE SKIN DENT, PROTRUDING EXTERNALLY AT FS625.00 - FS640.00 STRG 26LH - 27 REF REO 601R-53-61-8362 REV-- DATED 2025-May 30, 2025 · N917EV · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA2025F01424Skin · chafedLWR WING PLANK IS CHAFED AT RBL45 FROM CONTACT WITH THE WING TO BODY FAIRING (C-CHECK RO 10/06/2025)BLENDED OUT CHAFING DAMAGE TO COMPLY WITH REO 601R-57-21-880, REV -D, 2017/03/06, NOTE 1. AND ORIGINAL THICKNESS IN BLENDED AREA IS .300",.350" ,.260", AND .19May 29, 2025 · N917EV · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA2025F01423Spar · damagedRH WING FWD SPAR WEB HAS TOOLING DAMAGE AT TWO LOCATIONS BETWEEN WS 66 €“ 85 (APPROX.) AND ONE LOCATION AT WS 178 (APPROX.) (C-CHECK RO 10/06/2025)REPAIRED GOUGE DAMAGE TO RH WING INBOARD AND OUTBOARD FRONT SPAR WEBS, 2 EA LOCATIONS BETWEEN WS65.75-WS85.00 May 29, 2025 · N917EV · Cndair CL6002B19 · Wing SparSDR SWIA2025F01422Attach Angle · damagedSERVICE DOOR SILL ATTACH ANGLE AT FS333 REQUIRES REPLACEMENT. (C-CHECK RO 10/06/2025)REMOVED AND REPLACED THE SERVICE DOOR SILL ATTATCH ANGLE REF DWG 601R32004 REV L AND CRJ200 SRM 51-42-06 AND 51-42-21.COMPLIED WITH 51-900-1003 SKY.May 29, 2025 · N917EV · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR SWIA2025F01421Angle · damagedSERVICE DOOR SILL FLOOR ANGLE REQUIRES REPLACEMENT (C-CHECK RO 10/06/2025)REMOVED AND REPLACED THE SERVICE DOOR SILL ANGLE REF DWG 601R32003 REV AR AND CRJ200 SRM 51-42-13.COMPLIED WITH 51-900-1003 SKY900080May 29, 2025 · N917EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2025F01420Angle · damagedSERVICE DOOR SILL ANGLE (601R-38303-239) REQUIRES REPLACEMENT. (C-CHECK RO 10/06/2025)REMOVED AND REPLACED THE SERVICE DOOR SILL ANGLE (P/N 601R38303-239) REF DWG 601R38303 REV AR AND CRJ200 SRM 51-42-21.COMPLIED WITH 51-900-1003-SKY.May 29, 2025 · N917EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2025100700529Skin · chafedLWR WING PLANK IS CHAFED AT LBL45 FROM CONTACT WITH THE WING TO BODY FAIRING (C-CHECK RO 10/06/2025) BLENDED OUT CHAFING DAMAGE ON LWR WING PLANK AT LBL 45. REF CRJ200 SRM 51-12-00. AND ORIGINAL THICKNESS IN BLENDED AREA IS .300", .350" ,AND .260" REF. CRJ 20May 29, 2025 · N917EV · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA2025100700527Fitting · gougedTHE LH SCREWJACK FITTING ON THE HORIZONTAL STAB IS GOUGED. (C-CHECK RO 10/06/2025)BLENDED OUT GOUGES ON LH SCREWJACK FITTING ON THE HORIZONTAL STAB REF CRJ200 SRM 51-12-00 AND REPAIRED IAW MHIRJ REO 601R-55-11-794, REV --, 2025-06-24 AND COMPLIED WITH TASK May 27, 2025 · N917EV · Cndair CL6002B19 · Horizontal Stabilizer Miscellaneous StructureSDR SWIA2025F01415Stringer · crackedSTGR3L CRACKED JUST AFT OF FS280.00. (C-CHECK RO 10/06/2025) REMOVE AND REPLACED CRACKED ANGLE AND CLIPS AT STGR 3L JUST AFT OF FS 280 REF DWG 600-31522 REV G AND CRJ200 SRM 51-42-06 AND 51-42-21.COMPLIED WITH 51-900-1003 SKY.May 22, 2025 · N917EV · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR SWIA2025100700522Stringer · crackedSTGR3L CRACKED AT FS379.00. (C-CHECK RO 10/06/2025) REMOVED AND REPLACED STGR 3L BETWEEN FS364.00 TO FS394.00 REF CRJ-200 SRM 51-42-06 AND DWG 601R31016 REV D. COMPLIED WITH TASK CARD 51-900-1003-SKY. SEE CONTINUATION FOR DETAILS.May 22, 2025 · N917EV · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR SWIA2025100700520Fitting · gougedRIGHT ELEVATOR INBOARD HINGE OUTER PCU FITTING GOUGED AS MARKED ON LOWER SIDE NEXT TO FASTENER (C-CHECK RO 10/06/2025) REPAIRED AND COMPLIED WITHALL STEPS REO 601R-55-21-608 REV-- DATED: 2025-06-19 COMPLIED WITH REO 601R-55-21-608 REV-- DATED: 2025-06-19 STEMay 20, 2025 · N917EV · Cndair CL6002B19 · Elevator StructureSDR SWIA2025F01419Seat Track · corrodedSEAT RAIL BEAM RBL27 FS589 TO FS621, AREAS OF CORROSION, HN00241675 (C-CHECK RO 10/06/2025)REMOVED AND REPLACED FLOOR BEAM SECTION AT RBL 27.0 BETWEEN F/S 589 TO F/S 621 IAW CRJ 200 SRM 53-00-43 AND REO 601R53-61-3778 REV. B DATED 2016-12-19.COMPLIED WITH May 13, 2025 · N917EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2025100700513Seat Track · corrodedSEAT RAIL BEAM RBL9 FS589 TO FS621, AREAS OF CORROSION, HN00241673 (C-CHECK RO 10/06/2025)REMOVED AND INSTALLED NEW RBL 9.0 FLOOR BEAM SECTION BETWEEN F/S 589 TO F/S 621 IAW CRJ 200 SRM 53-00-43 AND IAW REO 601R-53-61-3780 REV. A DATED 2011-07-15 COMPLIED WMay 13, 2025 · N917EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2025F01414Seat Track · corrodedSEAT RAIL BEAM LBL27 FS574 TO FS559+96, AREAS OF CORROSION, HN00241667 (C-CHECK RO 10/06/2025) REPAIRED CORROSION ON SEAT RAIL BEAM LBL27 FS574 TO 559+96 REF CRJ-200 SRM 53-00-43 AND REO 601R-53-00-912 REV -- DATE 2025-07-03, COMPLIED WITH ALL STEPS. COMPMay 12, 2025 · N917EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2025F01413Floor Support · corrodedLEFT HAND UPPER SURFACE OF PRESSURE FLOOR SILL AT FS 409+128 & 559.00 LBL36.00 HAS SEVERAL AREAS OF CORROSION (C-CHECK RO 10/06/2025) BLENDED AND REPAIRED CORROSION ON THE LEFT HAND UPPER SURFACE OF PRESSURE FLOOR SILL AT FS 409+128 & 559.00 LBL36.00 COMPLMay 12, 2025 · N917EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2025F01412Seat Track · corrodedSEAT RAIL BEAM LBL27 FS574 TO FS621, AREAS OF CORROSION, HN00241668 (C-CHECK RO 10/06/2025) REPLACED WITH NEW SEAT RAIL BEAM AT LBL27 BETWEEN FS559+112 TO 605+5 REF. CRJ200 SRM 51-42-21 AND SRM 51-42-22 AND GREO 601R-53-61-3778 REV-B DATED 2016-12-19 AND CMay 12, 2025 · N917EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2025100700512Floor Support · corrodedUPPER SURFACE OF PRESSURE FLOOR SILL STRUCTURE APROX FS450.00 HAS CORROSION AROUND FASTNER HOLE. REMOVED CORROSION ON UPPER SURFACE OF PRESSURE FLOOR SILL STRUCTURE APROX. FS450.00 AROUND FASTENER HOLE. REF CRJ200 SRM 51-21-06 AND REPAIRED IAW REO 601R-53-4May 12, 2025 · N917EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA20241221Engine · failedENGINE FAILURE ON CLIMB OUT.Dec 21, 2024 · N917EV · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR SWIA2024072200019Landing Gear · did not stowGEAR DISAGREE AND NOSE DOOR WARNINGS AFTER ATTEMPTING TO RETRACT GEAR AFTER TAKEOFF. NOSE GEAR DID NOT RETRACT. RAN QRH AND ALL GEAR EXTENDED CORRECTLY, CLEARING WARNINGS. RETURNED TO FIELD WITHOUT INCIDENT. (FLIGHT 5437 - FILED CLOSED)THIS DISCREPANCY WAS TRAJul 19, 2024 · N917EV · Cndair CL6002B19 · Nose/Tail Landing GearSDR SWIA20240213118Floor Support · corrodedFLOOR BEAM AT RBL 9.00 BETWEEN FS409.00 + 112 AND FS409.00 + 128 HAS 2 AREAS OF CORROSION NEAR THE FWD SPLICE. (C-CHECK RO 2/12/2024) REPAIRED 2 AREAS OF CORROSION NEAR THE FWD SPLICE OF THE FLOOR BEAM AT RBL 9.00 BETWEEN FS409.00 + 112 AND FS409.00 + 128 Jan 18, 2024 · N917EV · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA20240213112Bracket · crackedSTRINGER CLEAT CRACKED ON THE AFT SIDE OF THE REAR PRESURE BULKHEAD AT STGR 14R. (C-CHECK RO 2/12/2024) REMOVED AND REPLACED STRINGER CLEAT ON THE AFT SIDE OF THE REAR PRESURE BULKHEAD AT STGR 14R IN REF TO SRM 51-42-06. COMPLIED WITH FORM M-337 AND TASKJan 12, 2024 · N917EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWI2024F00115Bracket · crackedSTRINGER CLEET CRACKED ON THE AFT SIDE OF THE REAR PRESURE BULKHEAD AT STGR 14L . (C-CHECK RO 2/12/2024) REMOVED AND REPLACED STINGER CLEAT ON THE AFT SIDE OF THE REAR PRESURE BULKHEAD AT STGR 14L IN REF TO SRM 51-42-06. COMPLIED WITH FORM M-337 AND TASK CJan 11, 2024 · N917EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA20240213111Pressure Blkhd · gougedAFT PRESSURE BULKHEAD (FS621.00) FWD FACE HAS 8 GOUGES AND 7 GOUGED RIVET HEADS IN THE WEB DOUBLERS AT RBL 36.20, RBL 27.50, RBL 18.00, LBL 9.50, LBL 18.00, LBL 27.50, AND LBL 36.20. (C-CHECK RO 2/12/2024) REPAIRED 8 GOUGES AND REPLACED 7 GOUGED RIVETS IN Jan 11, 2024 · N917EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA20240213107Pressure Deck · damagedPRESSURE FLOOR AT APPROX. FS. 500, OUTBOARD OF LBL 9.00 AND CENTERED BETWEEN SUPPORT BEAM AND JUST AFT OF CABLE SUPPORT BRACKET, SKIN HAS SMALL NICK. (C-CHECK RO 2/12/2024) REPAIRED GOUGE DAMAGE TO PRESSURE FLOOR AT APPROX. FS. 500, OUTBOARD OF LBL 9.00 ANJan 7, 2024 · N917EV · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA202402013106Floor Support · corrodedFLOOR BEAM RBL9.00 BETWEEN FS. 409.00 +48 - 409.00 +128 HAS MULITPLE AREAS OF SURFACE CORROSION ON INBOARD FLOORBOARD LANDING. (C-CHECK RO 2/12/2024) REMOVED AND REPLACED FLOOR BEAM RBL9.00 BETWEEN FS. 409.00 +48 - 409.00 +128 IN REF TO SRM 51-42-34, 51-4Jan 6, 2024 · N917EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202162607None · damagedTRANSFER FROM EAML 778862 : TRANSFERRED FROM CAMP 23817432. DAMAGE FOUND TO BE ON RIGHT SIDE OF AIRCRAFT BETWEEN FS 379.00 AND FS 394.00 TO BE AS FOLLOWS: / (1-OFF) DENT DAMAGE MEASUREING 1.25" LENGTH X .075" WIDTH X 0.060" MAX DEPTH & (1-OFF) GOUGE DAMAGE MENov 13, 2021 · N917EV · Cndair CL6002B19 · Fuselage Structure (General)SDR SWIA202161171None · damagedCOMPLY WITH FORM M-337 FOR MAJOR REPAIR TO SCREW HOLE FOR ACCES PANEL 131AL SEE PARENT. (FILED CLOSED) COMPLIED WITH FORM M-337 FOR REPAIR TO SCREW HOLE SURROUND STRUCTURE FOR ACCESS PANEL 131ALSep 22, 2021 · N917EV · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA2020090252175Frame · corrodedF.S. 333 FRAME IS CORRODED FROM 23L-17L. C-CHECK RO 8/29/2020. REMOVED AND INSTALLED NEW FRAME SECTORS AT FS333.00 STRINGER 18R TO 23R IAW CRJ-200 SRM, BOMBARDIER DRAWING, AND SKYWEST CARD. COMPLETED M-337 AND M-131. WEIGHT AND BALANCE NOT AFFECTED PART FOAug 25, 2020 · N917EV · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA2020090252174Frame · corrodedF.S. 333 FRAME IS CORRODED FROM STRINGER 18R TO 17R. C-CHECK RO 8/29/2020. REMOVED AND INSTALLED NEW FRAME SECTORS AT FS333.00 STRINGER 18R TO 23R IAW CRJ-200 SRM, DRAWING AND SKYWEST CARD. COMPLETED FORM M-337. WEIGHT AND BALANCE NOT AFFECTED.Aug 25, 2020 · N917EV · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA2020090252173Floor Support · elongatedNUTPLATE HOLE ON LT CABIN FLOOR SILL AT F.S.464 IS ELONGATED. C-CHECK RO 8/29/2020. PERFORMED A MAJOR REPAIR TO THE LT PRESSURE FLOOR SKIN IAW MHIRJ REO. COMPLETED SKYWEST TASK. COMPLETED FORM M-337. NO WEIGHT CHANGE.Jul 30, 2020 · N917EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020090252155Floorbeam · crackedF.S. 484 LT INTERCOSTAL BETWEEN LBL 27 AND LBL 36 IS CRACKED AT THE LOWER OUTBOARD CORNER. C-CHECK RO 8/29/2020. REPAIRED DAMAGED F.S.484 LT INTERCOSTAL BETWEEN LBL 27 AND LBL 36 LWR CORNER IAW MHIRJ REO AS DOCUMENTED ON CONTINUATION CARD. FORM M-337 COMPLETJul 30, 2020 · N917EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA2020090252172Buttstrap · corrodedCORROSION FOUND ON BUTT STRAP AT F.S. 333 STRINGER 27-26L. C-CHECK RO 8/29/2020. REMOVED AND INSTALLED NEW BUTT STRAP IAW CRJ 200 SRM AND BOMBARDIER DWG. COMPLIED WITH TASK CARD, M-337 COMPLETED. WEIGHT AND BALANCE NOT AFFECTED.Jul 23, 2020 · N917EV · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA2020090252171Floor Support · corrodedRT CABIN PRESSURE FLOOR SILL PANEL HAS CORROSION FROM F.S. 409+128 TO F.S. 559.00. C-CHECK RO 8/29/2020. REPAIRED RT FLOOR SILL FROM FS 409.128 TO FS 559.00 IAW REO. COMPLIED WITH SKY CARD AND FORM M-337. SEE CONTINUATION CARD FOR DETAILS OF WORK PREFORMEJul 22, 2020 · N917EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020090252170Floor Support · corrodedLBL 9 FLOOR BEAM CAP IS CORRODED BETWEEN F.S. 409 TO F.S. 409+96 ON THE INBOARD SIDE. C-CHECK RO 8/29/2020. PERFORMED A MAJOR REPAIR TO FS 409 TO FS 409+96 LBL9 FLOOR BEAM CAP IAW CRJ-200 SRM AND REO. REFERENCE BOMBARDIER DRAWING. COMPLIED WITH SKYWEST TASJul 21, 2020 · N917EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020090252169Intercostal · corrodedF.S. 349 INTERCOSTAL AT STRINGER 20R IS CORRODED. C-CHECK RO 8/29/2020. REMOVED AND INSTALLED NEW INTERCOSTAL AT FS 349 AT STRINGER 20R IAW CRJ 200 SRM AND DRAWING 601R38303. COMPLIED WITH SKYCARD AND FORM M-337. SEE CONTINUATION CARD FOR DETAILS OF WORK PJul 21, 2020 · N917EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020090252193Angle · corrodedF.S. 280 FWD J ANGLE IS CORRODED. C-CHECK RO 8/29/2020. REMOVED CORRODED FORWARD FLOOR ANGLE ( "J" ANGLE), AND REPLACED WITH NEW P/N 600-34017-351 IAW CRJ-200 SRM.Jul 20, 2020 · N917EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020090252189Seat Track · corrodedLBL9 FLOOR SEAT TRACK IS CORRODED AT F.S. 364. C-CHECK RO 8/29/2020. REMOVED AND REPLACED SEAT TRACK AT FS 364 LBL9 IAW: CRJ200-AMM.Jul 20, 2020 · N917EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2020090252185Plate · corrodedPASSENGER DOOR AFT ANCHOR FITTING SERRATED PLATE IS CORRODED. C-CHECK RO 8/29/2020. REMOVED AND REPLACED PASSENGER DOOR ANCHOR FITTING SERRATED PLATE IAW CRJ 200 AMM. ADJUSTMENT AND OPS CHECKS "GOOD".Jul 20, 2020 · N917EV · Cndair CL6002B19 · Passenger/Crew Doors
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