N795SK

Service difficulty reports · 78

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 = 'N795SK' 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 SWIA2026070976608Pitot Tube · contaminatedUNRELIABLE AIRSPEED INDICATION ON LT, CA SIDE. ASSOCIATED MESSAGES INCLUDED CAUTION MESSAGES: MACH TRIM & EFIS COMP MON, STATUS MESSAGES: RUD LIMIT FAULT, STAB FAULT, RT & LT FADEC FAULT 2. ON POST WALK AROUND, DEBRIS FOUND IN CA SIDE PITOT TUBE. (FLIGHT 5541)Jul 9, 2026 · N795SK · Cndair CL6002C11 · Pitot/Static SystemSDR SWIA2026051276198Skin · damagedPERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO FUSLEAGE SKIN LOCATED BETWEEN FS 581.00 - FS 597.00 AND STRG 24R - STRG 25R DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM. PERFORMED PERMANENT DOUBLER REPAIR INSTALLATION TO FUSLEAGE SKIN LOCATED BETWEEN FS 581May 12, 2026 · N795SK · Cndair CL6002C11 · Fuselage Main, Plate/SkinSDR SWIA2026060876197Skin · damagedPERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO FUSLEAGE SKIN LOCATED BETWEEN FS 1000.00 - FS 1015.00 AND STRG 25R - STRG 26R DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM. PERFORMED PERMANENT DOUBLER REPAIR INSTALLATION TO FUSLEAGE SKIN LOCATED BETWEEN FS May 12, 2026 · N795SK · Cndair CL6002C11 · Fuselage Main, Plate/SkinSDR SWIA2026051276196Skin · damagedPERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO LH FWD FUSLEAGE SKIN LOCATED BETWEEN FS 394.00 - FS 409.00 AND STRG 13L - STRG 14L DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM (DETERMINED TO BE A MAJOR REPAIR) PERFORMED PERMANENT DOUBLER REPAIR INSTALLATIOMay 12, 2026 · N795SK · Cndair CL6002C11 · Fuselage Main, Plate/SkinSDR SWIA2026051276195Skin · damagedPERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO RH FWD FUSLEAGE SKIN LOCATED BETWEEN FS 394.00 - FS 409.00 AND STRG 13R - STRG 14R DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM (DETERMINED TO BE A MAJOR REPAIR) PERFORMED PERMANENT DOUBLER REPAIR INSTALLATIONMay 12, 2026 · N795SK · Cndair CL6002C11 · Fuselage Main, Plate/SkinSDR SWIA2026060876194Skin · damagedPERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO UPPER FUSLEAGE SKIN LOCATED BETWEEN FS 830.40 - FS 847.00 AND STRG 1L - STRG 0 DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM (DETERMINED TO BE A MAJOR REPAIR) PERFORMED PERMANENT DOUBLER REPAIR INSTALLATION TOMay 12, 2026 · N795SK · Cndair CL6002C11 · Fuselage Main, Plate/SkinSDR SWIA2026030275989Intercostal · mechanic errorINTERCOSTAL AT FS 533 BETWEEN STGR 26L-27 FOUND TO HAVE DOUBLE DRILLED HOLE. PERFOMED MAJOR REPAIR OF INTERCOSTAL AT FS 533 BETWEEN STGR 26L-27 IAW SRM 531-42-06-001-001-A01 REV. 38D AND REO 670-53-32-174 REV.--Mar 2, 2026 · N795SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2026022175985Hinge · gougedPASSENGER DOOR HINGE, DOOR SIDE, ALL LUGS GOUGED. REPAIRED PASSENGER DOOR HINGE, DOOR SIDE, ALL LUGS IAW SRM 52-11-01-201-007-A01.Feb 21, 2026 · N795SK · Cndair CL6002C10 · Fuselage, Door HingeSDR SWIA2026021775988Stringer · corrodedSTRINGER 25L IS CORRODED BETWEEN FS 485.00 TO 501.00 (C-CHECK RO 05/03/2026)REMOVED AND REPLACED STGR 25L BETWEEN FS 485 AND 501 WITH A NEW SERVICEABLE STGR25L P/N SH670-33254-3 IAW CRJ700 SRM 51-42-06-001-001-A01.Feb 17, 2026 · N795SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2026021775986Stringer · corrodedSTRINGER 23L IS CORRODED BETWEEN FS 485.00 AND 533. REMOVED AND REPLACED WITH NEW SERVICEABLE STGR 23L IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, AND 51-40-11-001-001-A01Feb 17, 2026 · N795SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2026021675983Intercostal · corrodedINTERCOSTAL LEFT OF STRINGER 27 BETWEEN FS 349.00 AND 379.00 IS CORRODED. REMOVED AND REPLACED THE INTERCOSTAL LEFT OF STGR 27 BETWEEN FS349 - FS364, NEW SERVICEABLE L/H INTERCOSTAL IAW SRM 51-42-06-001-001-A01 AND SRM51-42-21-001-001-A01.Feb 16, 2026 · N795SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2026021275987Hinge · gougedPAX DOOR HINGE (FUSELAGE SIDE) REQUIRES REPLACEMENT. DURING DAMAGE TOLERANCE INSPECTION FOR AFT MOST LUG LANDING FOUND A NEW HEAVY GOUGE FROM HINGE PIN LOCKING PIN. AFT MOST LUG LANDING WAS ALREADY PREVIOUSLY BLENDED, HINGE IS NOW OUT OF LIMITS. (C-CHECK RO 0Feb 12, 2026 · N795SK · Cndair CL6002C10 · Fuselage, Door HingeSDR SWIA2026011075991Drag Angle · crackedLT VERTICAL STAB AFT DRAG ANGLE SHOWS EVIDENCE OF CRACKING. REMOVED AND REPLACED L/H VERTICAL STAB AFT DRAG ANGLE WITH NEW DRAG ANGLE IAW CRJ 700 SRM 51-42-13-001-001-A01.Jan 10, 2026 · N795SK · Cndair CL6002C10 · Fuselage, Stabilizer Attach FittingsSDR SWIA2026011075984Drag Angle · crackedRH VERTICAL STAB AFT DRAG ANGLE SHOWS EVIDENCE OF CRACKING. REMOVED AND REPLACED RT VERTICAL STAB AFT DRAG ANGLE WITH NEW DRAG ANGLE P/N AV670-21186-004 IAW CRJ 700 SRM 51-42-21-001-001-A01Jan 10, 2026 · N795SK · Cndair CL6002C10 · Fuselage, Stabilizer Attach FittingsSDR SWIA202507150622Skin · chafedCHAFING FOUND ON LOWER FUSELAGE SKIN BETWEEN FS977.00 AND FS985.00 STGR 27 DUE TO CONTACT ON AFT FAIRING PANEL C-CHANNEL. REMOVED CHAFING FOUND ON LOWER FUSELAGE SKIN BETWEEN FS977.00 AND FS985.00 STGR 27 REF CRJ700 SRM 51-12-00-001-001-A01. FOUND AREA TO BEJun 22, 2025 · N795SK · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR SWIA20250715610Diaphragm · crackedCRACKED DIAPHRAGM AT FS724.00 BETWEEN RBL36.00 AND BL45.00. REMOVED AND REPLACED DIAPHRAGM AT FS724.00 BETWEEN RBL36.00 AND BL45.00. REF SRM 51-42-21-001-001-A01 REV 38 AND DWG SH670-36115 REV -A. COMPLIE WITH TASK CARD 51-900-1002-SKY.Jun 10, 2025 · N795SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2025033100028Windshield · crackedLEFT WINDSHIELD SHATTERED AT 17,000 FT; 3.4 PSI PRESSURE DIFFERENTIAL. (FLIGHT 5988 - FILED CLOSED)REMOVED AND REPLACED CA WINDSHIELD PER CRJ-700 AMM 56-11-01. OPS CHECK AND LEAK CHECK GOOD AT THIS TIME. A/C OKAY FOR SERVICE. C/W CRJ 700 COCKPIT WINDSHIELD Mar 28, 2025 · N795SK · Cndair CL6002C10 · Flight Compartment WindowsSDR SWIA202161129None · crackedFLOOR BEAM RBL 12.0 AT FS 232.0 IS CRACKED AT BOTTOM SIDE. (C-CHECK RO 9/21/2021) PERFORMED PERMANENT REPAIR TO RBL12.00 FLOOR BEAM IN REF REO 670-53-11-1727, REV --, DATED 2021-09-07. ALL STEPS COMPLETED AT THIS TIME. ST 51-900-1002-SKY COMPLETE. SEE CAug 25, 2021 · N795SK · Cndair CL6002C10 · Fuselage Structure (General)SDR SWIA202161128None · crackedUPON REMOVAL OF RIVETS ON FWD RH UPPER SKIN BETWEEN FS 169 AND FS 172 FOUND FASTENER HOLE CRACKED (C-CHECK RO 9/21/2021) REMOVED AND REPLACED FWD RH UPPER SKIN P/N CC670-33107-2 PO# T000062212/1 IN REF DWG CC670-33040, REV G, CRJ700 SRM 51-42-06-001-00Aug 20, 2021 · N795SK · Cndair CL6002C10 · Fuselage Structure (General)SDR SWIA202161127None · corrodedRH FLOOR SILL FS280 TO FS319, ATTACH ANGLE STN 319.7, PART# SH670-31503-1 IS CORRODED. (C-CHECK RO 9/21/2021) CORROSION IS 100% THROUGH ATTACH ANGLE STN 319.7 ON RH FLOOR SILL FS280 TO FS319 AND IS OUT OF LIMITS REF CRJ700 SRM 53-00-00-101-001-A01. REMOAug 18, 2021 · N795SK · Cndair CL6002C10 · Fuselage Structure (General)SDR SWIA202161126None · corrodedRH FLOOR SILL FS280 TO FS319, SPLICE ANGLE STGR 17R, PART# SH670-31580-1 IS CORRODED. (C-CHECK RO 9/21/2021) CORROSION IS 100% THROUGH SPLICE ANGLE STGR 17R ON RH FLOOR SILL FS280 TO FS319 AND IS OUT OF LIMITS REF CRJ700 SRM 53-00-00-101-001-A01. REMOVEAug 18, 2021 · N795SK · Cndair CL6002C10 · Fuselage Structure (General)SDR SWIA202161125None · corrodedRH COCKPIT FLOOR BEAM ATTACHING FLANGE TO FWD SIDE OF FS.280 DOOR POST RBL12 IS CORRODED AND CRACKED (C-CHECK RO 9/21/2021) REMOVED AND REPLACED RH COCKPIT FLOOR BEAM RBL12 IN REF CRJ700 SRM 53-11-43-201-003-A01. SEE CONTINUATION CARD FOR WORK PERFORMEDAug 7, 2021 · N795SK · Cndair CL6002C10 · Fuselage Structure (General)SDR SWIA202161124None · corrodedRH FS.280 LOWER WEB HAS CORROSION AT FLOOR LEVEL RBL9. (C-CHECK RO 9/21/2021) PERFORMED PERMANENT REPAIR TO RH F.S.280.00 LOWER WEB IN REF CRJ700 SRM 53-11-10-201-004-A01. SEE CONTINUATION CARD FOR WORK PERFORMED. TASK CARD 51-900-1002-SKY COMPLETE.Aug 7, 2021 · N795SK · Cndair CL6002C10 · Fuselage Structure (General)SDR SWIA202161123None · corrodedLH FS.280 LOWER WEB HAS CORROSION AT FLOOR LEVEL LBL9. (C-CHECK RO 9/21/2021) PERFORMED PERMANENT REPAIR TO LH F.S.280.00 LOWER WEB LBL9 IN REF CRJ700 SRM 53-11-10-201-004-A01. SEE CONTINUATION CARD FOR WORK PERFORMED. TASK CARD 51-900-1002-SKY COMPLETEAug 7, 2021 · N795SK · Cndair CL6002C10 · Fuselage Structure (General)SDR SWIA202161122None · corrodedREPLACE LH AND RH FS.280 FLOOR CROSSBEAMS WITH NEW DUE TO OUT OF LIMIT CORROSION. (C-CHECK RO 9/21/2021) -REMOVED & INSTALLED NEW FS.280 L/H AND R/H FLOOR BEAMS IN REF CRJ700 SRM 51-42-06-001-001-A01, CRJ700 SRM 51-42-13-001-001-A01, CRJ700 SRM 51-42-2Aug 7, 2021 · N795SK · Cndair CL6002C10 · Fuselage Structure (General)SDR SWIA202161121None · corrodedCOCKPIT RH DOOR POST ENTRANCE HAS CORROSION AT FLOOR LEVEL RBL9. (C-CHECK RO 9/21/2021) INSTALLED PERMANENT REPAIR TO COCKPIT RH DOOR POST AT RBL11 IN REF CRJ700 SRM 53-11-10-201-006-A01. SEE CONTINUATION CARD FOR WORK PERFORMED. TASK CARD 51-900-1002-SAug 6, 2021 · N795SK · Cndair CL6002C10 · Fuselage Structure (General)SDR SWIA202161120None · corrodedCOCKPIT LH DOOR POST ENTRANCE HAS CORROSION AT FLOOR LEVEL LBL9. (C-CHECK RO 9/21/2021) INSTALLED PERMANENT REPAIR TO COCKPIT LH DOOR POST AT LBL11 IN REF CRJ700 SRM 53-11-10-201-006-A01. SEE CONTINUATION CARD FOR WORK PERFORMED. TASK CARD 51-900-1002-SAug 6, 2021 · N795SK · Cndair CL6002C10 · Fuselage Structure (General)SDR SWIA202161119None · damagedRH LEADING EDGE SKIN PANEL 622BR DAMAGED AT INB BOTTOM SIDE. (MARKED). (C-CHECK RO 9/21/2021) RH LEADING EDGE SKIN PANEL 622BR INB BOTTOM SIDE REPAIRED GOUGE REF. REO 670-57-41-469 REV.--, DATED 2021-09-01, IS IN LIMITS OF TEMPORARY REPAIR VALID FOR 800Aug 5, 2021 · N795SK · Cndair CL6002C10 · Wing StructureSDR SWIA202161118None · chafed* PAX DOOR HINGE, FUSELAGE SIDE HAS NUMEROUS LUG LANDINGS CHAFFED/GOUGED FROM AFT OF LUG #14 TO LAST LUG LANDING (MARKED) (C-CHECK RO 9/21/2021) BLENDED OUT CHAFE/GOUGE ON PAX DOOR HINGE (FUSELAGE SIDE) AT LUGS LANDING FROM #14 TO #27 REF. CRJ-700 SRM 5Aug 5, 2021 · N795SK · Cndair CL6002C10 · Fuselage Structure (General)SDR SWIA202161117None · gouged* PAX DOOR HINGE, FUSELAGE SIDE HAS LUGS GOUGED AT # 18 & # 24 (MARKED) (C-CHECK RO 9/21/2021) BLENDED OUT GOUGE ON PAX DOOR HINGE (FUSELAGE SIDE) AT LUGS # 18 AND # 24, REF. CRJ-700 SRM 53-21-23-201-010-A01, PARAGRAPH A. (1). ORIGINAL THICKNESS AT #18 Aug 5, 2021 · N795SK · Cndair CL6002C10 · Fuselage Structure (General)SDR SWIA202161116None · corroded* CORROSION ON GALLEY 1 OUTBOARD FWD FLOOR MOUNT (MARKED) (C-CHECK RO 9/21/2021) REPLACED GALLEY #1 OUTBD FWD FLOOR MOUNT. REF CRJ700 SRM 51-42-20-001-001-A01 & DWG SH690-32120 REV AL. COMPLIED WITH TASK CARD 51-900-1002-SKY.Aug 5, 2021 · N795SK · Cndair CL6002C10 · Fuselage Structure (General)SDR SWIA202161115None · corroded* CORROSION ON GALLEY 1 INBOARD FWD FLOOR MOUNT (MARKED) (C-CHECK RO 9/21/2021) REPLACED GALLEY #1 INBD FWD FLOOR MOUNT, REF CRJ700 SRM 51-42-20-001-001-A01 AND DWG SH690-32120 REV AL. COMPLIED WITH TASK CARD 51-900-1002-SKY.Aug 5, 2021 · N795SK · Cndair CL6002C10 · Fuselage Structure (General)SDR SWIA202161114None · corroded* CORROSION ON FWD ENTRY STORAGE AFT INBOARD FLOOR MOUNT (MARKED) (C-CHECK RO 9/21/2021) REPLACED ENTRANCE STORAGE AFT INBD FLOOR MOUNT. REF CRJ700 SRM 51-42-20-001-001-A01 & DWG SH690-32120 REV AL. COMPLIED WITH TASK CARD 51-900-1002-SKY.Aug 5, 2021 · N795SK · Cndair CL6002C10 · DoorsSDR SWIA202161113None · corroded* CORROSION ON FWD ENTRY STORAGE FWD INBOARD FLOOR MOUNT (MARKED) (C-CHECK RO 9/21/2021) REPLACED ENTRANCE STORAGE FWD INBD MOUNT. REF CRJ700 SRM 51-42-20-001-001-A01 & DWG SH690-32120 REV AL. COMPLIED WITH TASK CARD 51-900-1002-SKY.Aug 5, 2021 · N795SK · Cndair CL6002C10 · DoorsSDR SWIA202161112None · corroded* CORROSION ON RH FLOOR SILL FS280-FS319.70 (MARKED) (C-CHECK RO 9/21/2021) REPLACED RH FLOOR SILL FROM FS280 - FS319. REF CRJ700 SRM 51-42-06-001-001-A01, REF CRJ700 SRM 51-42-13-001-001-S01, REF CRJ700 SRM 51-42-21-001-001-A01 & DWG SH670-32170 REV V.Aug 5, 2021 · N795SK · Cndair CL6002C10 · Fuselage Internal Mounting StructureSDR SWIA202161111None · corroded* CORROSION ON PAX DOOR MID CAP ANGLE (MARKED) (C-CHECK RO 9/21/2021) REMOVED AND REPLACED PAX DOOR MID CAP ANGLE REF. DWG SH670-31810 REV. Y AND CRJ700 SRM 51-42-06-001-001-A01. PERFORMED OPERATIONAL TEST OF THE PASSENGER DOOR REF. CRJ-700 AMM 52-11-00Aug 5, 2021 · N795SK · Cndair CL6002C10 · DoorsSDR SWIA202161110None · corrodedCOCKPIT FLOOR SUPPORT AT FS.280 BETWEEN LBL9 AND RBL9 HAS CORROSION. (C-CHECK RO 9/21/2021) REMOVED AND REPLACED WITH NEW COCKPIT FLOOR SUPPORT AT FS.280 BETWEEN LBL9 AND RBL9 HAS CORROSION REF CRJ-700 SRM 51-42-06-001-001-A01,SRM 51-42-21-001-001-A01 Aug 4, 2021 · N795SK · Cndair CL600* · Fuselage Floor PanelSDR SWIA202161109None · corroded*FS.265 FRAME FWD OF INTERNAL FWD JACK FITTING HAS CORROSION (MARKED) (C-CHECK RO 9/21/2021) REPLACED FS265 LOWER STIFFENEING ANGLE. REF CRJ700 SRM 51-42-06-001-001-A01 AND DWG CC670-34020 REV A. COMPLIED WITH TASK CARD 51-900-1002-SKY. NO LEAKS NOTED,Aug 4, 2021 · N795SK · Cndair CL6002C10 · Fuselage Main, FrameSDR SWIA202161108None · chafedRH UPPER TRANSCOWL FWD OTBD EDGE CHAFFED (C-CHECK RO 9/21/2021) ACCOMPLISHED REPAIR TO CHAFED EDGE OF RH UPPER TRANSCOWL IAW ALL STEPS OF REO 670-54-21-1028 REV NC, DATED 2009-06-15. COMPLIED WITH TASK CARD 51-900-1002-SKYAug 4, 2021 · N795SK · Cndair CL6002C10 · Engine Exhaust SystemSDR SWIA202161107None · corroded* PASSENGER DOOR LOWER SILL LOWER FLOOR SUPPORT ANGLE HAS CORROSION. (C-CHECK RO 9/21/2021) REMOVED AND REPLACED PASSENGER DOOR LOWER SILL LOWER FLOOR SUPPORT ANGLE WITH NEW REF. CRJ-700 SRM 51-42-06 -001-001-A01, 51-42-21-001-001-A01 AND DWG SH670-3181Aug 3, 2021 · N795SK · Cndair CL6002C10 · DoorsSDR SWIA202161106None · crackedFWD EQUIPMENT COMPARTMENT - SUSPECTED CRACK IN DECK SKIN UNDER AND OUTBOARD OF L/H FWD EQUIPMENT BAY BRAKE ACCUMULATOR GAGES - VISIBLE ON TOP AND ALSO FROM FWD HYDRAULICS COMPARTMENT - APROX FS 192 WL 79.5 (C-CHECK RO 9/21/2021) COMPLIED WITH REO 670-53Jul 29, 2021 · N795SK · Cndair CL6002C10 · DoorsSDR SWIA202161105None · crackedFWD EQUIPMENT COMPARTMENT - ADG HAND PUMP DOUBLER HAS SUSPECTED TEMPORARY REPAIR TO CRACK UNDERNEATH - VISIBLE FROM ADG COMPARTMENT (C-CHECK RO 9/21/2021) REPAIRED IAW REO 670-53-11-509 REV E DATED 2018-02-08. SEE ATTACHED CONTINUATION CARD FOR WORK PERJul 29, 2021 · N795SK · Cndair CL6002C10 · Fuselage Main, FrameSDR SWIA202161104None · crackedFWD EQUIPMENT COMPARTMENT - R/H DOOR AFT LATCH RECEPTICLE - SUSPECTED CRACK @ UPPER AFT RADIUS (C-CHECK RO 9/21/2021) RECEIVED NEW PART: CC670-33151-6, REMOVED DAMAGED LANDING ON FWD R/H EQUIPTMENT BAY REF CRJ-700 SRM 51-42-06-001-001-A01 AND SRM 51-42Jul 29, 2021 · N795SK · Cndair CL6002C10 · DoorsSDR SWIA202161103None · chafed* LH SLAT TRACK 3-3, TRACK IS CHAFED. FLAGGED (C-CHECK RO 9/21/2021) BLENDED THE WEAR DAMAGE ON L/H 3-3 SLAT TRACK AND FOUND TO BE WITHIN LIMITS REF REO 670-57-42-1167 REV -- DATED 2021-08-27 STEPS 1-7. COMPLIED WITH TASK CARD 51-900-1002-SKY.Jul 28, 2021 · N795SK · Cndair CL6002C10 · Wing, Fuselage Attach FittingsSDR SWIA202161102None · chafed* LH SLAT TRACK 3-1, TRACK IS CHAFED. FLAGGED (C-CHECK RO 9/21/2021) BLENDED THE WEAR DAMAGE ON L/H 3-1 SLAT TRACK AND FOUND TO BE WITHIN LIMITS REF REO 670-57-42-1171 REV -- DATED 2021-09-02 STEPS 1-7. COMPLIED WITH TASK CARD 51-900-1002-SKY.Jul 28, 2021 · N795SK · Cndair CL6002C10 · Wing, Fuselage Attach FittingsSDR SWIA202161101None · chafed* LH SLAT TRACK 2-1, TRACK IS CHAFED. FLAGGED (C-CHECK RO 9/21/2021) BLENDED OUT CHAFE ON L/H SLAT TRACK 2-1REF. CRJ-700 SRM 51-12-00-001-001-A01. C/W NDT INSPECTION REF CRJ700 / NDTM 51-20-008-230-A01 & 51-20-004-270-A01. NO DEFECTS NOTED. TUC8922 CAJul 28, 2021 · N795SK · Cndair CL6002C10 · Wing, Fuselage Attach FittingsSDR SWIA202161100None · chafed* LH SLAT TRACK 1-1, TRACK IS CHAFED. FLAGGED (C-CHECK RO 9/21/2021) BLENDED THE WEAR DAMAGE ON L/H 1-1 SLAT TRACK AND FOUND TO BE WITHIN LIMITS REF REO 670-57-42-1166 REV -- DATED 2021-08-23 STEPS 1-7. COMPLIED WITH TASK CARD 51-900-1002-SKY.Jul 28, 2021 · N795SK · Cndair CL6002C10 · Wing, Fuselage Attach FittingsSDR SWIA202161099None · chafed* RH SLAT TRACK 3-1, TRACK IS CHAFED. FLAGGED (C-CHECK RO 9/21/2021) REPAIRED RH SLAT TRACK 3-1, TRACK IS CHAFED REF CRJ-700 SRM 51-12-00-001-001-A01 AND REO 670-57-42-1162 REV -- DATED 2021-08-25,COMPLIED WITH 51-900-1002-SKY.Jul 28, 2021 · N795SK · Cndair CL6002C10 · Wing, Fuselage Attach FittingsSDR SWIA202161098None · chafed* RH SLAT TRACK 2-3, TRACK IS CHAFED. FLAGGED (C-CHECK RO 9/21/2021) BLENDED OUT CHAFE ON R/H SLAT TRACK 2-3 REF. CRJ-700 SRM 51-12-00-001-001-A01. C/W NDT INSPECTION REF CRJ700 / NDTM 51-20-008-230-A01 & 51-20-004-270-A01. NO DEFECTS NOTED. TUC8922 CJul 28, 2021 · N795SK · Cndair CL6002C10 · Wing, Fuselage Attach FittingsSDR SWIA202161097None · chafed* RH SLAT TRACK 2-1, TRACK IS CHAFED. FLAGGED (C-CHECK RO 9/21/2021) BLENDED OUT CHAFE ON R/H SLAT TRACK 2-1REF. CRJ-700 SRM 51-12-00-001-001-A01. RECIEVED REO 670-57-42-1164 REV -- DATED 2021-08-24 FROM ENGINEERING. COMPLIED WITH REO 670-57-42-1164 REJul 28, 2021 · N795SK · Cndair CL6002C10 · Wing, Fuselage Attach Fittings
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