N709SK

Service difficulty reports · 207

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 = 'N709SK' 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 SWIA2026022575290Windshield · crackedWINDSHIELD CRACKED ENROUTE. RAN QRH. NO PRESSURIZATION ISSUES. (FLIGHT 6394 - FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 31750315. REMOVED AND REPLACED LH CA WINDSHIELD IAW TASK CARD 56-220-1000-SKY AND REFERENCING APPLICABLE STEPS OF AMM 56Feb 16, 2026 · N709SK · Cndair CL6002C10 · Flight Compartment WindowsSDR SWIA2026021765290Windshield · crackedCA, WINDSHIELD CRACKED ENROUTE. RAN QRH. NO PRESSURIZATION ISSUES. (FLIGHT 6394) OPEN.Feb 16, 2026 · N709SK · Cndair CL6002C10 · Flight Compartment WindowsSDR SWIA2025111400001Windshield · arcedCA SIDE OUTER WINDSCREEN ARCING THEN SHATTERED WHEN WINDSHIELD HEAT WAS TURNED OFF (FLIGHT 4908 - FILED CLOSED) REPLACED CA SIDE WINDOW IN REF TO AMM 56-12-01-400-801, SEE ATTACHED TASK CARD 56-220-1000-SKY. WINDOW HEAT AND PRESSURIZATION CHECK GOOD.Nov 11, 2025 · N709SK · Cndair CL6002C10 · Flight Compartment WindowsSDR SWIA2025111100001Windshield · crackedCAPTAIN SIDE OUTER WINDSCREEN ARCING THEN SHATTERED WHEN WINDSHIELD HEAT WAS TURNED OFF. (FLIGHT 4908) OPEN.Nov 11, 2025 · N709SK · Cndair CL6002C10 · Flight Compartment WindowsSDR SWI2025F00703Wire Harness · brokenL BLEED DUCT WARNING IN FLIGHT AT ABOUT 16,000FT. QRH COMPLIED WITH. RETURNED TO FIELD. PASSENGER O2 MASKS DEPLOYED. (FLIGHT 6221) TROUBLESHOT L BLEED DUCT AND FOUND CONNECTOR AT MT137 UNSERVICEABLE AND PIG TAIL WIRING HARNESS AT CONNECTOR MT203P1 BROMay 30, 2025 · N709SK · Cndair CL6002C10 · Engine Bleed Air System WiringSDR SWI2025F00652Extractor · faultedL BLEED DUCT WARNING MESSAGE ON CLIMB OUT (FLIGHT 6200 - FILED CLOSED)INTERROGATED MDC AND FOUND CHANNEL A FLAGGING MT137 AT 80%. PERFORMED INSPECTION OF L/H BLEED DUCTING SYSTEM IN REFERENCE WITH FIM 36-21-01 AND FOUND MULTIPLE LEAK POINTS. FOUND L/H WATER EXMay 21, 2025 · N709SK · Cndair CL6002C10 · Engine Bleed Air SystemSDR SWIA20250113111Light · smokeSMOKE EMITTED FROM FO FORWARD FLOOD LIGHT DURING CLIMB OUT. (FLIGHT 5005 - FILED CLOSED) TROUBLESHOT SMOKE IN THE COCKPIT IN REFERENCE TO FIM 21-21-00-810-806. FOUND SMOKE TO BE COMING FROM THE FO SIDE FACIA PANEL FLOOD LIGHT. INSPECTED THE FLOOD LIGHT AJan 11, 2025 · N709SK · Cndair CL6002C10 · Flight Compartment LightingSDR SWIA202501130049Door Frame · corrodedSERVICE DOOR SURROUND STRUCTURE FS319.00 TO FS349.00 STR 18R HAS SIGNS OF CORROSION AS MARKED (C-CHECK RO 12/31/2024 - FILED CLOSED) BLENDED CORROSION ON SERVICE DOOR LOWER MOUNTING ANGLE IAW CRJ700 SRM 51-21-06. FOUND TO BE OUT OF LIMITS IAW CRJ700 SRMNov 7, 2024 · N709SK · Cndair CL6002C10 · Fuselage Main, StructureSDR SWIA2025011307Door · gougedDEEP BARE METAL GOUGE WEAR IN RH MAIN LANDING GEAR DOOR ON THE AFT OUTBOARD CORNER OF THE DOOR ADJACENT TO THE SWEEP BELT BRUSHES (C-CHECK RO 12/31/2024 - FILED CLOSED) BLENDED DAMAGE ON RH MLG DOOR AT AFT OUTBOARD CORNER AND FOUND TO BE IN LIMITS IAW CNov 7, 2024 · N709SK · Cndair CL6002C10 · Landing Gear DoorsSDR SWIA20250102004Door Frame · corrodedSERVICE DOOR SURROUND STRUCTURE FS319.00 TO FS349.00 STR 18R HAS SIGNS OF CORROSION AS MARKED (C-CHECK RO 12/31/2024 - FILED OPEN) BLENDED CORROSION ON SERVICE DOOR LOWER MOUNTING ANGLE IAW CRJ700 SRM 51-21-06. FOUND TO BE OUT OF LIMITS IAW CRJ700 SRM 5Nov 7, 2024 · N709SK · Cndair CL6002C10 · Fuselage Main, StructureSDR SWIA202501020107Door · gougedDEEP BARE METAL GOUGE WEAR IN RH MAIN LANDING GEAR DOOR ON THE AFT OUTBOARD CORNER OF THE DOOR ADJACENT TO THE SWEEP BELT BRUSHES (C-CHECK RO 12/31/2024 - FILED OPEN) BLENDED DAMAGE ON RH MLG DOOR AT AFT OUTBOARD CORNER AND FOUND TO BE IN LIMITS IAW CRJNov 7, 2024 · N709SK · Cndair CL6002C10 · Landing Gear DoorsSDR SWIA2025011306Slat Track · crackedRH SLAT TRACK 1-3 HOUSING BRACKET CRACKED (C-CHECK RO 12/31/2024 - FILED CLOSED) PERFORMED REPAIR ON RH SLAT TRACK 1-3 HOUSING PER BOMBARDIER REO 670-57-42-577. REV. --. DATE: 2016-12-02. NDT PERFORMED BY BARON NDT,LLC FAA CRS# 5NDR545D. REPORT # S1118Nov 6, 2024 · N709SK · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA202501020106Slat Track · crackedRH SLAT TRACK 1-3 HOUSING BRACKET CRACKED (C-CHECK RO 12/31/2024 - FILED OPEN) PERFORMED REPAIR ON RH SLAT TRACK 1-3 HOUSING PER BOMBARDIER REO 670-57-42-577. REV. --. DATE: 2016-12-02. NDT PERFORMED BY BARON NDT,LLC FAA CRS# 5NDR545D. REPORT # S111824Nov 6, 2024 · N709SK · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA2025011300001Hinge · gougedPASSENGER DOOR PIANO HINGE DOOR SIDE LUG #1 GOUGED (C-CHECK RO 12/31/2024 - FILED CLOSED) REPAIRED DAMAGE ON LUG #1 OF PASSENGER DOOR PIANO HINGE, DOOR SIDE IAW BOMBARDIER REO 670-52-11-511 REV.C DATE: 2017/03/09. NDT PERFORMED BY BARON NDT, LLC FAANov 1, 2024 · N709SK · Cndair CL6002C10 · Fuselage, Door HingeSDR SWIA202501020101Hinge · gougedPASSENGER DOOR PIANO HINGE DOOR SIDE LUG #1 GOUGED (C-CHECK RO 12/31/2024 - FILED OPEN) REPAIRED DAMAGE ON LUG #1 OF PASSENGER DOOR PIANO HINGE, DOOR SIDE IAW BOMBARDIER REO 670-52-11-511 REV.C DATE: 2017/03/09. NDT PERFORMED BY BARON NDT, LLC FAA CNov 1, 2024 · N709SK · Cndair CL6002C10 · Fuselage, Door HingeSDR SWIA202266599None · failedGEAR DISAGREE AFTER SELECTING GEAR UP. NOSE WHEEL NOT LOCKED. (FLIGHT 4923 - FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 25627409 WITH THE FOLLOWING CORRECTIVE ACTION: "INTERROGATED MDC FOUND GEAR DISAGREE B1- 007437. TROUBLESHOT IN REF TOct 9, 2022 · N709SK · Cndair CL2151A10 · Landing Gear Door ActuatorSDR SWIA202266219None · crackedLH INTERCOSTAL PN CC670-33194-7 FOUND CRACKED UPON INSTALLATION OF THE HYDRAULIC COMPARTMENT SKIN. (FILED CLOSED) REMOVED DAMAGED INTERCOSTAL PN CC670-33194-7. FABRICATED NEW INTERCOSTAL SAME AS ORIGINAL REF CRJ 700 SRM 51-24-21-001-001-A01 AND DWG CC670-3Aug 4, 2022 · N709SK · Cndair CL6002C10 · Fuselage Structure (General)SDR SWIA202266350None · crackedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA77564-670-53-11-1796 N709SK MXCODEID61545-PR - LEFT FORWARD ELECTRICAL BAY DOOR 211AL SURROUND SKIN AFT LOWER CORNER SHOWING EVIDENCE OF CRACK. COMPLIED WITH TEMPORARY DISPOSITION FOR CRACKS TO HYDRAULIC SKIN PANEL ANDJul 28, 2022 · N709SK · Cndair CL6002C10 · Electrical/Electronic Compartment DoorsSDR SWIA2021081060227Skin · damagedADDITIONAL DAMAGE FOUND ON RUDDER L/H SKIN BTWN. RS98.750 & RS110.278. (C-CHECK RO 8/6/2021) REPAIRED L/H SIDE RUDDER SKIN DAMAGE REF REO 670-55-41-090 REV -- 2021-07-26. COMPLIED WITH SKYCARD 51-900-1002Jul 21, 2021 · N709SK · Cndair CL6002C10 · Rudder, Plate/SkinSDR SWIA2021081060226Angle · debondedLT UPPER TRANSCOWL, Z ANGLE DISBONDED AND HAS THREE LOOSE FASTENERS. (C-CHECK RO 8/6/2021) PERFORMED REPAIR FOR CRACK DAMAGE TO THE LH ENGINE UPPER TRANSCOWL INNER SKIN IAW ALL STEPS OF REO 670-54-21-1458 REV -- DATED 2021-07-23. / C/W TASK CARD 51-900-Jul 9, 2021 · N709SK · Cndair CL6002C10 · Nacelle/Pylon, Main FrameSDR SWIA2021081060225Stringer · corrodedCORROSION ON UPPER SURFACE OF STGR17R AT APPROXIMATE FS310.00 -5". (C-CHECK RO 8/6/2021) REPAIRED CORROSION TO UPPER SURFACE OF STGR17R AT FS310.00-5" IAW REO 670-53-21-2080 REV-- 2021-07-10. COMPLIED WITH SKYWET TASK CARD 51-900-1002-SKYJul 6, 2021 · N709SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2021081060228Intercostal · corrodedCORROSION PRESENT ON INTERCOSTAL BETWEEN FS581.00-FS597.00 AND STGR 23L-22L (C-CHECK RO 8/6/2021) BLENDED, EVALUATED: ORIGINAL THICKNESS- 0.080", REMAING THICKNESS- 0.069", MATERIAL LOSS- 0.011", MATERIAL LOSS ALLOWABLE- NONE. OUT OF LIMITS. REF CRJ700Jun 24, 2021 · N709SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2021081060233Drag Angle · crackedPAX DOOR AFT DRAG ANGLE CRACKED NEAR POWER ASSIST PULLEY (C-CHECK RO 8/6/2021) REMOVED AND REPLACED PAX DOOR AFT DRAG ANGLE, P/N 601R31772-5S. REF CRJ 700 SRM 51-42-06-001-001-A01Jun 18, 2021 · N709SK · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWIA2021081060224Intercostal · corrodedPAX DOOR INTERCOSTAL DD5 (FWD) CORRODED (C-CHECK RO 8/6/2021) REPLACED PAX DOOR INTERCOSTAL AT DD5 (FWD) REF DWG 601R31702 REV N, CRJ 700 SRM 51-42-06-001-001-A01. COMPLIED WITH 51-900-1002-SKY, ALL CHECKS GOODJun 18, 2021 · N709SK · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWIA2021081060223Cleat · corrodedPAX DOOR ATTACH CLEAT AT FS313.56 FRAME AND DD4 (FWD) CORRODED (C-CHECK RO 8/6/2021) REPLACED PAX DOOR ATTACH CLEAT AT FS313.56 AND DD4 FWD, REF CRJ700 SRM 51-42-06-001-001-A01 C/W TASK CARD 51-900-1002-SKY, ALL CHECKS GOODJun 18, 2021 · N709SK · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWIA2021081060222Door Frame · corrodedPAX DOOR FRAME AT FS313.56 BETWEEN DD4 AND DD5 (FWD) CORRODED (C-CHECK RO 8/6/2021) PAX DOOR FRAME AT FS313.56 BETWEEN DD4-DD5 FWD REPLACED REF DWG 601R31702 REV N, CRJ 700 SRM 51-42-06-001-001-A01. COMPLIED WITH 51-900-1002-SKY, ALL CHECKS GOODJun 18, 2021 · N709SK · Cndair CL6002C10 · Fuselage Main, StructureSDR SWIA2021081060221Intercostal · corrodedPAX DOOR INTERCOSTAL DD2 (FWD) CORRODED (C-CHECK RO 8/6/2021) REPLACED PAX DOOR INTERCOSTAL DD2 (FWD) REF DWG 601R31702 REV. N AND CRJ700 SRM 51-42-06-001-001-A01. COMPLIED WITH 51-900-1002-SKY, ALL CHECKS GOODJun 18, 2021 · N709SK · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWIA2021081060220Hinge Fitting · chafed*VERTICAL STABILIZER. RUDDER LOWER CENTER HINGE FITTING, IS CHAFED ON THE UPPER SURFACE OF THE "BEARING HOUSING" AREA. (MARKED (C-CHECK RO 8/6/2021) REPAIRED CHAFE ON VERTICAL STABILIZER CENTER HINGE FITTING UPPER SURFACE. REF MHI RJ AVIATION REO 670-55Jun 18, 2021 · N709SK · Cndair CL6002C10 · Rudder StructureSDR SWIA2021081060235Web · corroded*AREAS OF CORROSION ON PAX DOOR FWD WEB STEP PANEL LANDINGS (C-CHECK RO 8/6/2021) REMOVED CORROSION ON PAX DOOR FWD WEB. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACE PAX DOOR FWD WEB PANEL P/N 601R317071-11. REF CRJ 700 SRM 51-42-06-001-001-A01 AND CJun 15, 2021 · N709SK · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWIA2021081060232Angle · corroded*CORROSION PAX DOOR STOPPER BOLT MOUNT CLIP (C-CHECK RO 8/6/2021) REMOVED CORROSION ON PAX DOOR STOPPER BOLT MOUNT CLIP. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED PAX DOOR STOPPER BOLT MOUNT CLIP. SEE CONTINUATION FOR DETAILS. REF CRJ 700 SRM 51-4Jun 15, 2021 · N709SK · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWIA2021081060219Intercostal · corroded*CORROSION ON PAX DOOR INTERCOSTAL FWD DD3 (C-CHECK RO 8/6/2021) PAX DOOR INTERCOSTAL AT DD3 FWD REPLACED, REF CRJ700 SRM 51-42-06-001-001-A01 AND DWG 601R31702 REV N, C/W TASK CARD 51-900-1002-SKY, ALL CHECKS GOODJun 15, 2021 · N709SK · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWIA2021081060218Intercostal · corroded*CORROSION ON PAX DOOR INTERCOSTAL AFT DD5 (C-CHECK RO 8/6/2021) REPLACED PAX DOOR INTERCOSTAL AT AFT DD5 REF DWG 601R31702 REV N, CRJ 700 SRM 51-42-06-001-001-A01. COMPLIED WITH 51-900-1002-SKY, ALL CHECKS GOODJun 15, 2021 · N709SK · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWIA2021081060217Stringer · corrodedSTGR21R IS CORRODED BETWEEN FS349.00 TO FS364.00 (C-CHECK RO 8/6/2021) REMOVED AND REPLACED NEW STGR 21R P/N SH670-31383 REF CRJ700 SRM 51-42-06-001-001-A01 AND DWG SH 670-31350 REV A. COMPLIED WITH TASK CARD 51-900-1002-SKY AND FORM M M-337 PERFORME LEJun 14, 2021 · N709SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2021081060216Angle · corrodedPAX DOOR AFT CAP ANGLE P/N: SH670-31821-4 FOUND CORRODED. (C-CHECK RO 8/6/2021) REMOVED AND REPLACED WITH NEW PAX DOOR AFT CAP ANGLE IAW BOMBARDIER DWG SH670-31810 REV. AE AND SRM TASK 51-42-06-001-001-A01. COMPLIED WITH TASK CARD 51-900-1002-SKY.Jun 11, 2021 · N709SK · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWIA2021081060215Angle · corrodedPAX DOOR FWD CAP ANGLE P/N: SH670-31821-3 FOUND CORRODED. (C-CHECK RO 8/6/2021) REMOVED AND REPLACED WITH NEW PAX DOOR FWD CAP ANGLE IAW BOMBARDIER DWG SH670-31810 REV. AE AND SRM TASK 51-42-06-001-001-A01. COMPLIED WITH TASK CARD 51-900-1002-SKY.Jun 11, 2021 · N709SK · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWIA2021081060214Angle · corrodedPAX DOOR LOWER KIKPLATE ANGLE FOUND CORRODED. (C-CHECK RO 8/6/2021) REMOVED AND REPLACED WITH NEW PAX DOOR LWR KIKPLATE ANGLE IAW BOMBARDIER DWG SH670-31810 REV. AE, CRJ700 SRM TASK 51-42-10-001-001-A01 AND SRM TASK 51-42-21-001-001-A01. COMPLIED WITH TJun 11, 2021 · N709SK · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWIA2021081060213Floorbeam · crackedSUSPECTED CRACK ON COCKPIT LH FLOORBEAM AT LBL12 JUST FWD OF FS280.00 (C-CHECK RO 8/6/2021) CRACK VERIFIED. REMOVED AND INSTALLED NEW SECTION OF LH FLOORBEAM FROM FS 280.00 TO FS 268.00 REF CRJ700 SRM 53-11-43-201-003-A01. NO NDT DEFECTS NOTED. COMPLIEDJun 11, 2021 · N709SK · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SWIA2021081060212Floorbeam · crackedSUSPECTED CRACK ON COCKPIT RH FLOORBEAM AT RBL12 JUST FWD OF FS280.00 (C-CHECK RO 8/6/2021) CRACK VERIFIED. REMOVED AND INSTALLED NEW SECTION OF RH FLOORBEAM FROM FS 280.00 TO FS 268.00 AT RBL12 REF CRJ700 SRM 53-11-43-201-003-A01. NO NDT DEFECTS NOTED.Jun 11, 2021 · N709SK · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SWIA2021081060211Floorbeam · corrodedFOUND CORROSION ON LH CROSSBEAM FS 280.00 (C-CHECK RO 8/6/2021) REMOVED AND REPLACED LH CROSSBEAM P/N CC670-34094-1. REF: CRJ-700 SRM 51-42-06-001-001-A01, CRJ-700 SRM 51-42-13-001-001-A01, CRJ-700 SRM 51-42-21-001-001-A01, CRJ-700 SRM 51-42-22-001-001-Jun 11, 2021 · N709SK · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SWIA2021081060210Floorbeam · corrodedFOUND CORROSION ON RH CROSSBEAM FS 280.00 (C-CHECK RO 8/6/2021) REMOVED AND REPLACED RH CROSSBEAM P/N CC670-34094-2S @ FS280.00. REF: CRJ-700 SRM 51-42-06-001-001-A01, CRJ-700 SRM 51-42-13-001-001-A01, CRJ-700 SRM 51-42-22-001-001-A01, AND DRAWING CC670Jun 11, 2021 · N709SK · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SWIA2021081060209Skin · corrodedFS280-FS282.86 CIRCUMFERENTIAL JOINT HAS EVIDENCE OF CORROSION FROM STGR26R-STGR25R. (C-CHECK RO 8/6/2021) REPAIRED CIRCUNFERENTIAL JOINT AT FS 280.00 - FS 282.86 BETWEEN STGR 26R - STGR 25R REF REO 670-53-21-2066 REV -- DATED 2021-06-28 AND CRJ700 SRM Jun 9, 2021 · N709SK · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR SWIA2021081060208Skin · damagedREPAIR THE L/H HORIZONTAL STABILIZER UPPER SKIN PER REO 670-5-11-330 REV -- DATED 2017-08-24 (C-CHECK RO 8/6/2021) COMPLIED WITH REPAIR TO THE L/H UPPER HORIZIONTAL STABILIZER SKIN PER REO 670-55-11-330 REV -A DATED 2021-06-30. SEE CONTINUE CARD FOR DETJun 9, 2021 · N709SK · Cndair CL6002C10 · Horizontal Stabilizer, Plate/SkinSDR SWIA2021081060207Skin · damagedREPAIR THE R/H HORIZONTAL STABILIZER UPPER SKIN PER REO 670-55-11-330 REV -- DATED 2017-08-24 (C-CHECK RO 8/6/2021) C/W REPAIR TO THE R/H UPPER HORIZIONTAL STABILIZER SKIN PER REO 670-55-11-330 REV -A DATED 2021-06-30, CRJ 700 SRM 51-42-06-001-001-A01,Jun 9, 2021 · N709SK · Cndair CL6002C10 · Horizontal Stabilizer, Plate/SkinSDR SWIA2021081060204Skin · corrodedFS280-FS282.86 CIRCUMFERENTIAL JOINT HAS EVIDENCE OF CORROSION FROM STGR25R-STGR23R. (C-CHECK RO 8/6/2021) REPAIRED CIRCUNFERENTIAL JOINT FS 280.00 - FS 282.86 BETWEEN STGR 23R - STGR 25R REF REO 670-53-21-2066 REV -- DATED 2021-06-28 AND CRJ700 SRM 51-Jun 8, 2021 · N709SK · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR SWIA2021081060203Skin · corrodedFS280-FS282.86 CIRCUMFERENTIAL JOINT HAS EVIDENCE OF CORROSION FROM STGR24L-STGR23L. (C-CHECK RO 8/6/2021) REPAIRED CIRCUNFERENTIAL JOINT AT FS 280.00 BETWEEN STGR 24L - STGR 23L REF CRJ700 SRM 51-42-06-001-001-A01 AND CRJ700 SRM 51-21-06-001-001-A01 REJun 8, 2021 · N709SK · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR SWIA2021081060202Skin · corrodedFS280-FS282.86 CIRCUMFERENTIAL JOINT HAS EVIDENCE OF CORROSION FROM STGR26L-STGR26R. (C-CHECK RO 8/6/2021) REMOVED CORROSION AT FS280-FS282.86 CIRCUMFERENTIAL JOINT FROM STRG26L-STRG26R. FOUND TO BE WITHIN LIMITS PER MHIRJ REO 670-53-21-2066 REV -- DATEJun 8, 2021 · N709SK · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR SWIA2021081060234Door Sill · corroded*MULTIPLE AREAS OF CORROSION ON FWD CARGO DOOR SILL. AREAS MARKED. (C-CHECK RO 8/6/2021) BLENDED, EVALUATED: ORIGINAL MATERIAL THICKNESS OF FWD CARGO DOOR SILL (INNER SKIN) P/N SH670-33773-7 IS .080€? PER CRJ700 SRM 53-31-23-001-001-A01. MINIMUM REMAINJun 7, 2021 · N709SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2021081060201Drag Angle · cracked*RH SIDE VERTICAL/FUSELAGE AFT DRAG ANGLE IS CRACKED (C-CHECK RO 8/6/2021) REPLACED R/H AFT DRAG ANGLE AT THE VERTICAL/FUSELAGE ATTACHMENT AREA REF. CRJ 700 SRM 51-42-21-001-001-A01, 51-42-22-001-001-A01, 51-42-13-001-001-A01 DWG BA670-35002 REV F / C/WJun 7, 2021 · N709SK · Cndair CL6002C10 · Vertical Stabilizer, Attach FittingsSDR SWIA2021081060200Drag Angle · cracked*RH SIDE VERTICAL/FUSELAGE FWD DRAG ANGLE IS CRACKED (C-CHECK RO 8/6/2021) REPAIRED THE R/H VERTICAL/FUSELAGE FWD DRAG ANGLE, CUT AWAY DAMAGE, FABRICATED AND INSTALLED ALL REPAIR PARTS, REF. CRJ 700 SRM 55-31-00-201-001-A01 AND CRJ 700 SRM 51-42-21-001-Jun 7, 2021 · N709SK · Cndair CL6002C10 · Vertical Stabilizer, Attach FittingsSDR SWIA2021081060199Drag Angle · cracked*LH SIDE VERTICAL/FUSELAGE AFT DRAG ANGLE IS CRACKED (C-CHECK RO 8/6/2021) REMOVED AND REPLACED NEW *LH SIDE VERTICAL/FUSELAGE AFT DRAG ANGLE REF CRJ700 SRM 51-42-13-001-001-A01, CRJ700 SRM 51-42-21-001-001-A01, CRJ700 SRM 51-42-22-001-001-A01 AND DWG Jun 7, 2021 · N709SK · Cndair CL6002C10 · Vertical Stabilizer, Attach Fittings
Back to N709SK