N773SK

Service difficulty reports · 160

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 = 'N773SK' 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 SWIA2026012675098Rib · damagedDAMAGE ON THE LT WING CANTED RIB LOCATED AT WS398.93 WAS FOUND TO BE OUT OF LIMITS PER SRM 57-21-12. DAMAGE IS OUT OF LIMITS AND THE REPLACEMENT OF THE STRUCTURALLY SIGNIFICANT ITEM IS CLISSIFIED AS A MAJOR REPAIR. REMOVED AND REPLACED THE LT CANTED RIB AT Jan 26, 2026 · N773SK · Cndair CL6002C11 · Wing, Rib/BulkheadSDR SWIA2025102000017Hinge · damagedFOUND PAX DOOR HINGE (FUSELAGE SIDE) HAS SEVERAL LUGS WITH INNER SURFACE WEAR DAMAGE. (FILED CLOSED)COMPLIED WITH REO 670-53-21-2718 DATED: 2025-10-17 REV -- TEMPORARY DISPOSITION FOR WEAR DAMAGE TO PASSENGER DOOR HINGE LUGS (FUSELAGE SIDE). COMPLIED WITH TOct 17, 2025 · N773SK · Cndair CL6002C11 · Fuselage, Door HingeSDR SWIA20250813007Windshield · crackedCAPTAIN WINDSHIELD CRACKED (FLIGHT 5844 - FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 30628908 WITH THE FOLLOWING CORRECTIVE ACTION: "COMPLIED WITH TASK CARD 56-220-1000-SKY (CL600-2C11) CRJ-550 COCKPIT WINDSHIELD/SIDE WINDOW INSTALLATION. OPSAug 7, 2025 · N773SK · Cndair CL6002C11 · Flight Compartment WindowsSDR SWIA2025080800007Windshield · crackedCAPTAIN WINDSHIELD CRACKED (FLIGHT 5844) THIS IS CURRENTLY A WORK IN PROGRESS.Aug 7, 2025 · N773SK · Cndair CL6002C11 · Flight Compartment WindowsSDR SWIA202265905None · crackedWHILE PERFORMING DETAILED VISUAL INSPECTION OF THE BULKHEAD WEBS FS202.75 AND FS235, THE FLOOR WEBBING DIRECTLY BELOW THE ADG RESTOW PUMP WAS FOUND TO BE CRACKED BEYOND LIMITS OF SRM 53-11-43, AND HAS BEEN DETERMIND TO BE A MAJOR REPAIR. REF CP 24911707 FOR OJun 7, 2022 · N773SK · Cndair CL6002C10 · Fuselage Main, BulkheadSDR SWIA202265835None · crackedCRACK FOUND ON THE RH AFT DRAG ANGLE ON THE VERTICAL STAB TO EMPENAGE ATTACHMENT. CRACK STARTS AT FWD EDGE OF RH AFT DRAG ANGLE AND EXTENDS APROX. 0.281" AFT IN THE CORNER OF THE ANGLE. DAMAGE IS OUT OF LIMITS PER SRM 55-31-00. / HAS BEEN DETERMINED TO BE A MMay 31, 2022 · N773SK · Cndair CL6002C10 · Ventral StructureSDR SWIA202265834None · crackedCRACK FOUND ON THE LH AFT DRAG ANGLE ON THE VERTICAL STAB TO EMPENAGE ATTACHMENT. CRACK STARTS AT FWD EDGE OF LH AFT DRAG ANGLE AND EXTENDS APROX. 0.7515" AFT IN THE CORNER OF THE ANGLE. DAMAGE FOUND TO BE OUT OF LIMITS PER SRM 55-31-00. / IT HAS BEEN DETERMIMay 31, 2022 · N773SK · Cndair CL6002C10 · Ventral StructureSDR SWIA202265833None · crackedCRACK FOUND ON THE LH FWD DRAG ANGLE ON THE VERTICAL STAB TO EMPENAGE ATTACHMENT. CRACK STARTS AT AFT EDGE OF THE LH FWD DRAG ANGLE AND EXTENDS APROX. 2.115" FWD IN THE CORNER OF THE ANGLE. DAMAGE IS OUT OF LIMITS PER SRM 55-31-00. IT HAS BEEN DETERMINED TO BEMay 31, 2022 · N773SK · Cndair CL6002C10 · Ventral StructureSDR SWIA202265924None · crackedDURING GVI AFTER A HIGH LOAD LANDING EVENT ( AMM 05-51-01) SUBTASK B., FOUND LH OVERWING WING TO FUSELAGE FAIRING PANEL 171CL TO HAVE A CRACK IN THE PANEL RUNNING THROUGH A RIVET HOLE OF THE LOWER AFT STIFFNER. (FILED CLOSED)REMOVED AND REPLACED LH OVERWING May 30, 2022 · N773SK · Cndair CL6002C10 · Fuselage Structure (General)SDR SWIA202163278None · blockedREMOVE LOWER SECTOR FRAME AT FS319.70 TO F.O.M (C-CHECK RO 12/26/2021) REMOVED LOWER SECTOR FRAME AT FS319.70 BETWEEN STRG 25L TO STGR 23R TO FOM. REF CRJ-700 SRM 51-42-06-001-001-A01. / AND INSTALLED SAME LOWER SECTOR FRAME WITH NEW SPLICE AT FS319.7Dec 7, 2021 · N773SK · Cndair CL600* · Fuselage Main, FrameSDR SWIA202163277None · gouged* LEFT WING REAR SPAR AT APPROX. WS 58.00, HAS GOUGE ( PREVIOUS DAMAGE ) ON SPAR INBOARD OF INBOARD GROUND SPOILER ACTUATOR ROD ATTACHMENT POINT. (C-CHECK RO 12/26/2021) COMPLIED WITH REO MHIRJ REO 670-57-51-469 REV --, DATED: 2021-12-12 REPAIR FOR LH WDec 6, 2021 · N773SK · Cndair CL600* · Wing SparSDR SWIA2021122963276Channel · corrodedTCAS OMNIDIRECTIONAL ANTENNA CHANNEL IS CORRODED (C-CHECK RO 12/26/2021) REMOVED AND REPLACED TCAS OMNIDIRECTIONAL ANTENNA CHANNEL WITH NEW SERVICEABLE CHANNEL ASSY. P/N:SH670-32364-5 REF DRAWING SH670-30023 REV G DATED 2017/06/14 AND CRJ 700 SRM 51-42Dec 5, 2021 · N773SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA202163275None · corrodedA-BAY STGR 27 FS280-FS310 CORRODED (C-CHECK RO 12/26/2021) REMOVED AND INSTALLED NEW A-BAY NEW STGR 27 FS280-FS310 REF CRJ700 SRM 51-42-21-001-001-A01,CRJ700 SRM 51-42-06-001-001-A01,DWG#SH670-31630 REV K COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKDec 5, 2021 · N773SK · Cndair CL600* · Fuselage Structure (General)SDR SWIA202163274None · corrodedINTERCOSTAL AT STRINGER 20R FS349.00 €“ 364.00 HAS CORROSION. (C-CHECK RO 12/26/2021) EVALUATED CORROSION ON INTERCOSTAL AT STRINGER 20R FS349.00 €“ FS364.00 FOUND TO BE OUT OF LIMITS, CORROSION EXCEEDS 30% OF OVERALL LENGTH REF. CRJ700 SRM 53-00-00-Dec 2, 2021 · N773SK · Cndair CL600* · Fuselage Main, Longeron/StringerSDR SWIA202163273None · dentedUPON REMOVAL OF STRINGER FOUND DENT PROTRUDING ON FUSELAGE SKIN AT FS319.70 TO FS333.00 STRINGER 25R. (C-CHECK RO 12/26/2021) EVALUATED DENT AT STRINGER 25R BETWEEN FS319.70 TO FS333.00. DENT MEASURES 6.20€? L 0.013€? D AND 0.20€? W. WITH A W/D RADec 1, 2021 · N773SK · Cndair CL600* · Fuselage Structure (General)SDR SWIA202163272None · corrodedCORROSION ON PAX DOOR FRAME FS313.56 BETWEEN DD4 AND DD5 INTERCOSTAL (C-CHECK RO 12/26/2021) PAX DOOR FRAME FS313.56 BETWEEN DD4 AND DD5 INTERCOSTAL HAS CORROSION ON MORE THAN ONE ELEMENT. OUT OF LIMIT REF CRJ 200 SRM 52-00-00 AND REO 670-52-11-010 REV.Nov 24, 2021 · N773SK · Cndair CL600* · Fuselage Main, Longeron/StringerSDR SWIA202163271None · corrodedRH FLOOR SILL BETWEEN FS 280-FS319.70 HAS SEVERAL SPOTS OF CORROSION (C-CHECK RO 12/26/2021) INSTALLED NEW RH FLOOR SILL BETWEEN FS 280-FS319.70 REF CRJ700 SRM 51-42-06-001-001-A01, CRJ700 SRM 51-42-13-001-001-A01, CRJ700 SRM 51-42-21-001-001-A01 AND DNov 23, 2021 · N773SK · Cndair CL600* · Fuselage Internal Mounting StructureSDR SWIA2021122963270Support · corrodedRIGHT HAND NOSE JACKING SUPPORT AT APPROX. FS 265.00 TO FS 280.00 IS CORRODED. (C-CHECK RO 12/26/2021) EVALUATED CORROSION ON RIGHT HAND NOSE JACKING SUPPORT FS265.00 - FS280.00. OUT OF LIMITS. DAMAGE IS ON MORE THAN ONE ELEMENT. SKIN ATTACH ELEMENT ANDNov 22, 2021 · N773SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA202163269None · gougedAPPROXIMATELY FS333 & FS349 BETWEEN STGR 21R AND STGR 19R BELOW SERVICE DOOR HAS PREVIOUS POSSIBLE DENT/GOUGED PAINTED REQUIRES EVALUATION AND REPAIR (C-CHECK RO 12/26/2021) COMPLIED WITH DOUBLER REPAIR TO SKIN LAP JOINT BETWEEN FS333-FS364 AND STG 18Nov 21, 2021 · N773SK · Cndair CL600* · Fuselage Main, FrameSDR SWIA202163268None · corrodedCORROSION ON UNION SPLICE AT STR 25R BETWEEN FS 319.70 AND FS 349.00 (C-CHECK RO 12/26/2021) REPLACED UNION SPLICE AT STR 25R BETWEEN FS 319.70 AND FS 349.00 REF CRJ700 SRM 51-42-06-001-001-A01 AND DWG SH670-32420 REV E. COMPLIED WITH SKYWEST TASK CARNov 19, 2021 · N773SK · Cndair CL600* · Fuselage Main, FrameSDR SWIA202163267None · corrodedCORROSION ON STR 25R BETWEEN FS 319.70 AND FS 333.00 (C-CHECK RO 12/26/2021) INSTALLED NEW STRINGER 25R PN SH670-31212-2 FS280.00 - FS333.00 CRJ700 SRM 51-42-06-001-001-A01, CRJ700 SRM 51-42-21-001-001-A01 & DRAWING SH670-31630 REV. K, DATED 2017/11/2Nov 19, 2021 · N773SK · Cndair CL600* · Fuselage Main, KeelSDR SWIA202163266None · corrodedCORROSION ON STRG 26L BETWEEN FS 319.70 TO FS 333.00 (C-CHECK RO 12/26/2021) REPLACED STRG 26L FROM FS 280.00 TO FS333.00 REF DWG SH670-31630 REV K,CRJ700 SRM 51-42-06-001-001-A01 AND CRJ700 SRM 51-42-21-001-001-A01 LEAK CHECK GOOD COMPLIED WITH SKYWENov 19, 2021 · N773SK · Cndair CL600* · Fuselage Main, KeelSDR SWIA202163265None · corrodedCORROSION ON PAX DOOR FRAME FS327.763 BETWEEN INTERCOSTAL DD6 AND DD7A (C-CHECK RO 12/26/2021) PAX DOOR FRAME FS327.763 BETWEEN INTERCOSTAL DD6 AND DD7A HAS CORROSION ON MORE THAN ONE ELEMENT. OUT OF LIMIT REF CRJ 200 SRM 52-00-00 AND REO 670-52-11-010 Nov 19, 2021 · N773SK · Cndair CL600* · Fuselage Structure (General)SDR SWIA202163264None · corrodedCORROSION ON INTERCOSTAL DD7A (C-CHECK RO 12/26/2021) REMOVED CORRODED PAX DOOR INTERCOSTAL DD7A AND INSTALLED NEW PAX DOOR INTERCOSTAL DD7A REF CRJ 700 SRM 51-42-06-001-001-A01 AND BOMBARDIER DWG 601R31702 REV N. COMPLIED WITH SKYWEST TASK CARD 51-900-Nov 19, 2021 · N773SK · Cndair CL600* · Fuselage Main, Longeron/StringerSDR SWIA202163263None · corrodedCORROSION ON INTERCOSTAL DD6 MID (C-CHECK RO 12/26/2021) PAX DOOR INTERCOSTAL MID DD6 HAS CORROSION ON MORE THAN ONE ELEMENT. OUT OF LIMIT REF CRJ 200 SRM 52-00-00 AND REO 670-52-11-010 REV. NC DATED 2002-02-25. REMOVED PAX DOOR INTERCOSTAL DD6 MID REF Nov 19, 2021 · N773SK · Cndair CL600* · Fuselage Main, Longeron/StringerSDR SWIA202163262None · corrodedCORROSION IN INTERCOSTAL DD4 AFT (C-CHECK RO 12/26/2021) PAX DOOR INTERCOSTAL AFT DD4 HAS CORROSION ON MORE THAN ONE ELEMENT. OUT OF LIMIT REF CRJ 200 SRM 52-00-00 AND REO 670-52-11-010 REV. NC DATED 2002-02-25. REMOVED CORRODED PAX DOOR INTERCOSTAL DDNov 19, 2021 · N773SK · Cndair CL600* · Fuselage Main, Longeron/StringerSDR SWIA202163260None · corrodedCORROSION ON INTERCOSTAL DD4 FWD (C-CHECK RO 12/26/2021) PAX DOOR INTERCOSTAL FWD DD4 HAS CORROSION ON MORE THAN ONE ELEMENT. OUT OF LIMIT REF CRJ 200 SRM 52-00-00 AND REO 670-52-11-010 REV. NC DATED 2002-02-25. REMOVED CORRODED PAX DOOR INTERCOSTAL DDNov 19, 2021 · N773SK · Cndair CL600* · Fuselage Main, Longeron/StringerSDR SWIA202163259None · corrodedCORROSION ON INTERCOSTAL DD3 AFT (C-CHECK RO 12/26/2021) PAX DOOR INTERCOSTAL AFT DD3 HAS CORROSION ON MORE THAN ONE ELEMENT. OUT OF LIMIT REF CRJ 200 SRM 52-00-00 AND REO 670-52-11-010 REV. NC DATED 2002-02-25. REMOVED CORRODED PAX DOOR INTERCOSTAL DDNov 19, 2021 · N773SK · Cndair CL600* · Fuselage Main, Longeron/StringerSDR SWIA202163258None · corrodedCORROSION ON INTERCOTAL DD2 MID (C-CHECK RO 12/26/2021) PAX DOOR INTERCOSTAL MID DD2 HAS CORROSION ON MORE THAN ONE ELEMENT. OUT OF LIMIT REF CRJ 200 SRM 52-00-00 AND REO 670-52-11-010 REV. NC DATED 2002-02-25. REMOVED FS 329 .50 CORRODED INTERCOSTAL DNov 19, 2021 · N773SK · Cndair CL600* · Fuselage Main, Longeron/StringerSDR SWIA202163257None · corrodedPAX DOOR LOWER SILL CLOSING FITTING AT FS314.00 HAS INTERGRANULAR CORROSION IN MULTIPLE LOCATIONS. (C-CHECK RO 12/26/2021) FOUND PAX DOOR LOWER SILL CLOSING FITTING OUT OF LIMIT , REPLACED WITH NEW PN SH670-31840-3 PO# T-62897 REF CRJ 700 SRM 51-42-06-0Nov 18, 2021 · N773SK · Cndair CL600* · DoorsSDR SWIA2021122963256Angle · corrodedPAX DOOR LOWER SILL KICKPLATE ANGLE HAS INTERGRANULAR CORROSION IN SEVERAL LOCATIONS. (C-CHECK RO 12/26/2021) FOUND PAX DOOR LOWER SILL KICKPLATE ANGLE OUT OF LIMIT , REPLACED WITH NEW PN SH670-31875-7 PO# T-62190 REF CRJ 700 SRM 51-42-06-001-001-A01 ANNov 18, 2021 · N773SK · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWIA202163255None · corrodedPAX DOOR LOWER SILL MID CAP ANGLE HAS INTERGRANULAR CORROSION AROUND SEVERAL SCREW HOLES. (C-CHECK RO 12/26/2021) FOUND PAX DOOR LOWER SILL MID CAP ANGLE OUT OF LIMIT , REPLACED WITH NEW PN SH670-31825-9 PO# 10236-0015 REF CRJ 700 SRM 51-41-02-001-001-ANov 18, 2021 · N773SK · Cndair CL600* · DoorsSDR SWIA202163254None · crackedRH WING SLAT TRACK CANISTER 1-3 CRACKED (C-CHECK RO 12/26/2021) COMPLIED WITH REPAIR ON THE RH SLAT TRACK CANISTER 1-3 PER BOMBARDIER REO 670-57-42-577 REV -- DATED 2016-12-02, COMPLIED WITH SKYWEST TASKCARD 51-900-1002-SKY, LEAK CHECK GOOD AND OPS TESNov 17, 2021 · N773SK · Cndair CL600* · Wing, Fuselage Attach FittingsSDR SWIA202163253None · damagedR/H AILERON AFT SPAR #2 I/B HINGE FITTING BUSHING BORE IS PITTED (C-CHECK RO 12/26/2021) REMOVED AND REPLACED R/H AILERON AFT SPAR #2 I/B HINGE FITTING BUSHING. COMPLIED WITH REO 670-57-51-464 REV-- DATED 2021-11-24. / COMPLIED WITH SKYWEST TASKCARD 51-Nov 16, 2021 · N773SK · Cndair CL600* · Rudder, Spar/RibSDR SWIA202163252None · crackedPAX DOOR AFT FORMER FS347.25 CRACK (C-CHECK RO 12/26/2021) REMOVED CRACK AFT FORMER FS347.25 REF CRJ 700 SRM 51-42-06-001-001-A01 AND CRJ 700 SRM 51-42-21-001-001-A01. INSTALLED NEW PAX DOOR AFT FORMER AT FS 347.7 PN 601R318034 -5 REF CRJ 700 SRM 51-42Nov 16, 2021 · N773SK · Cndair CL600* · DoorsSDR SWIA202163251None · wornRUDDER VERTICAL STABILIZER CENTER UPPER HINGE BEARING WORN (C-CHECK RO 12/26/2021) REMOVED CENTER RUDDER HINGE, UPPER HINGE AND DISASSEMBLED FITTING BY REMOVING FASTENERS AND REMOVED OLD BEARING, REASSEMBLED FITTING WITH NEW FASTENERS AND INSTALLED NEWNov 13, 2021 · N773SK · Cndair CL600* · Rudder/Tab, Attach FittingsSDR SWIA202163250None · corroded* FITTING AT APPROX. STGR18R FS319.70 CORRODED (C-CHECK RO 12/26/2021) REPLACED OUT OF LIMITS FITTING WITH NEW FITTING AT APPROX STGR 18R FS319.70 REF. CRJ700 SRM 51-42-21-001-001-A01 AND DRAWING SH670-31950 REV Y COMPLIED WITH SKYWEST TASK CARD 51-900Nov 13, 2021 · N773SK · Cndair CL600* · Fuselage Main, FrameSDR SWIA202163249None · corroded* BACK UP SILL AT STGR21L FS333-FS349 CORRODED (C-CHECK RO 12/26/2021) REMOVED AND INSTALLED NEW REPLACEMENT BACK UP SILL (P/N SH670-31823-1S) ONTO STGR21L BETWEEN FS333.00 AND FS349.00 USING ALL NEW HARDWARE. REF BOMBARDIER DWG# SH670-31810 REV Y AND Nov 13, 2021 · N773SK · Cndair CL600* · Fuselage Internal Mounting StructureSDR SWIA202163248None · corroded* BACK UP SILL AT STGR21L FS310-FS333 CORRODED (C-CHECK RO 12/26/2021) REMOVED AND INSTALLED NEW REPLACEMENT BACK UP SILL (P/N SH670-31822-1S) ONTO STGR21L BETWEEN FS310.00 AND FS333.00 USING ALL NEW HARDWARE. REF BOMBARDIER DWG# SH670-31810 REV Y AND Nov 13, 2021 · N773SK · Cndair CL600* · Fuselage Internal Mounting StructureSDR SWIA202163247None · corroded* FS319.70 FRAME BETWEEN STGR18L-STGR21L CORRODED (C-CHECK RO 12/26/2021) REMOVED CORRODED FRAME AT FS319.70 BETWEEN STGR'S 18L AND 21L. REF CRJ700 SRM'S 51-42-06-001-001 A01 AND 51-42-21-001-001 A01.INSTALLED NEW REPLACEMENT FRAME (P/N# SH670-31891-3S)Nov 13, 2021 · N773SK · Cndair CL600* · Fuselage Main, FrameSDR SWIA202163246None · dented*DENT ON LH OTBD FLAP LOWER EXTERNAL SKIN, LOCATED ON LOWER OTBD CORNER (C-CHECK RO 12/26/2021) REPAIRED DENT DAMAGE ON LH OTBD FLAP LOWER EXTERNAL SKIN, LOCATED ON LOWER OTBD CORNER PER CRJ 700 SRM 57-53-01-201-001-A01 REV 38 DATED JUL 25 2020 TYPE IINov 12, 2021 · N773SK · Cndair CL600* · Aileron TabsSDR SWIA202163245None · corroded*FLOOR PANEL SUPPORT ANGLE IS CORRODED. LOCATED @FS280.00, WL72.50 BETWEEN LBL9.00 AND RBL9.00 (C-CHECK RO 12/26/2021) INSTALLED NEW FLOOR SUPPORT ANGLE PN CC670-34095-1 AT FS280 BETWEEN LBL9 - RBL9 REF BOMBARDIER DWG CC670-33052 REV -G, CRJ700 SRM 51-Nov 12, 2021 · N773SK · Cndair CL600* · Fuselage Internal Mounting StructureSDR SWIA202163244None · worn*RH UPPER TRANSCOWL HAS WEAR ON COAMING. AREAS MARKED (C-CHECK RO 12/26/2021) REMOVED WORN COAMING FROM THE RH UPPER TRANSCOWL, REF CRJ700 SRM 51-42-13-001-001 A01. INSTALLED NEW REPLACEMENT COAMING (P/N CN624-2061-205) ONTO RH UPPER TRANSCOWL USING ALLNov 11, 2021 · N773SK · Cndair CL600* · Engine Exhaust SystemSDR SWIA202163243None · corroded*CORROSION ON INTERCOSTAL MID DD4 (C-CHECK RO 12/26/2021) PAX DOOR INTERCOSTAL MID DD4 HAS CORROSION ON MORE THAN ONE ELEMENT. OUT OF LIMIT REF CRJ 200 SRM 52-00-00 AND REO 670-52-11-010 REV. NC DATED 2002-02-25. REMOVED CORRODED PAX DOOR DD4 MID SECTINov 11, 2021 · N773SK · Cndair CL600* · Fuselage Main, Longeron/StringerSDR SWIA202163242None · corroded*CORROSION ON INTERCOSTAL FWD DD3 (C-CHECK RO 12/26/2021) PAX DOOR INTERCOSTAL FWD DD3 HAS CORROSION ON MORE THAN ONE ELEMENT. OUT OF LIMIT REF CRJ 200 SRM 52-00-00 AND REO 670-52-11-010 REV. NC DATED 2002-02-25. REMOVED CORRODED PAX DOOR INTERCOSTAL DDNov 11, 2021 · N773SK · Cndair CL600* · Fuselage Main, Longeron/StringerSDR SWIA202163241None · corroded*AREAS OF CORROSION ON PAX DOOR FWD FRAME FS 311.75 (C-CHECK RO 12/26/2021) PAX DOOR FWD FRAME/FORMER FS311.75 HAS CORROSION ON MORE THAN ONE ELEMENT AT A GIVEN CROSS-SECTION. FOUND OUT OF LIMIT REF CRJ 200 SRM 52-00-00 AND REO670-52-11-010 REV.NC DATEDNov 11, 2021 · N773SK · Cndair CL600* · DoorsSDR SWIA202163240None · worn*LH LOWER TRANSCOWL HAS WEAR ON COAMING LEADING EDGE (C-CHECK RO 12/26/2021) REMOVED WORN COAMING FROM LH LOWER TRANSCOWL. REF CRJ700 SRM 51-42-13-001-001 A01. INSTALLED WITH NEW COAMING (P/N CN624-2061-205) ONTO LH LOWER TRANSCOWL USING NEW HARDWARE RNov 10, 2021 · N773SK · Cndair CL600* · Engine Exhaust SystemSDR SWIA202163239None · worn*LH LOWER TRANSCOWL HAS WEAR ON OTBD LEADING EDGE INNER SKIN (C-CHECK RO 12/26/2021) COMPLIED WITH REO 670-54-21-1485 REV -- DATED 2021-11-30 REPAIR TO LH LOWER TRANSCOWL WEAR ON OTBD LEADING EDGE INNER SKIN COMPLIED WITH SKYWEST TACK CARD 51-900-1002-SNov 10, 2021 · N773SK · Cndair CL600* · Engine Exhaust SystemSDR SWIA202163238None · crackedAFT CARGO DOOR HANDLE HOUSING HAS SUSPECT CRACK (MARKED) (C-CHECK RO 12/26/2021) REMOVED AND INSTALLED NEW AFT CARGO DOOR HANDLE ASSY (PN H3415-13) IN REF TO CRJ700 AMM 52-31-03-400-801-A01 AND DWG CC670-38702 REV -C. OPS TEST GOOD. HEALTH MONITORING CHNov 6, 2021 · N773SK · Cndair CL600* · DoorsSDR SWIA202163279None · chafed*LEFT WING INBOARD FLAP VANE €“ PANEL 584ET IS CHAFED. (C-CHECK RO 12/26/2021) LH WING INBD FLAP VANE PANEL 584ET DAMAGE BLENDED TO A SMOOTH CONTOUR UPON EVALUATION PANEL WAS FOUND TO BE OUT OF LIMITS PANEL WAS REPLACED WITH NEW PART.CRJ700 SRM 51-12-0Nov 5, 2021 · N773SK · Cndair CL600* · Ailerons
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