N765SK

Service difficulty reports · 185

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 = 'N765SK' 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 SWIA202157348Intercostal · corroded*CORROSION ON INTERCOSTAL BETWEEN FS 349.00 €“ 364.00, STGR 27 €“ 26R (C-CHECK RO 4/3/2021) REPLACED LATCH PIN INTERCOSTAL BETWEEN FS349-FS364 STR27-26R REF SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01 AND DWG SH670-32050 REV.J. LEAK TEST GOOD. CMar 6, 2021 · N765SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA202157347Stringer · corroded*CORROSION ON STGR 25L, BETWEEN FS 319.00 €“ 333.00 (C-CHECK RO 4/3/2021) REMOVED AND INSTALLED "NEW" STRINGER 25L LOCATED BETWEEN FS280 - FS333 AS REQ'D IAW, CRJ700 SRM 51-42-21-001-001-A01, CRJ700 SRM 51-42-06-001-001-A01 & DRWG SH670-31630 REV. K. RESMar 6, 2021 · N765SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA202157346Floor Support · corrodedFLOOR SILL R/H SIDE AT FS 280 TO FS 319.70 HAS AREAS OF CORROSION. (C-CHECK RO 4/3/2021) REPLACED RH FLOOR SILL AT FS280.00-FS319.70 STR17R REF SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01 AND DWG SH670-32170 REV. V. COMPLIED WITH SKYWEST TASK CARD Mar 6, 2021 · N765SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA202157368Doubler · corroded*CORROSION ON RAD ALT ANTENNA DOUBLER BETWEEN FS 1000.00 - 1015.00, STGR 27 - 26L (C-CHECK RO 4/3/2021) REMOVED 2EA. CORRODED SHIMS ON RAD ALT ANTENNA DOUBLER AND INSTALLED 2EA NEW SHIMS WITH PN MM670-70327-001 AND MM670-70329-001 WERE INSTALLED ON RAD ANMar 5, 2021 · N765SK · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR SWIA202157367Seat Track · corroded*CORROSION ON FLOOR SEAT TRACK RBL 9 BETWEEN FS 847.00 €“ 977.00. AREAS MARKED. (C-CHECK RO 4/3/2021) REMOVED AND REPLACED SEAT TRACK RBL 9.0, SEAT TRACK FOUND TO BE OUT OF ALLOWABLE LIMITS AFTER CORROSION REMOVAL IAW CRJ700 AMM 53-00-49-400-801-A17Mar 5, 2021 · N765SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA202157366Seat Track · corroded*CORROSION ON FLOOR SEAT TRACK LBL 9 BETWEEN FS 847.00 €“ 977.00. AREAS MARKED. (C-CHECK RO 4/3/2021) REMOVED AND REPLACED SEAT TRACK LBL 9.0, SEAT TRACK FOUND TO BE OUT OF ALLOWABLE LIMITS AFTER CORROSION REMOVAL IAW CRJ700 AMM 53-00-49-400-801-A17Mar 5, 2021 · N765SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA202157345Floor Support · corroded*CORROSION ON LH FLOOR SILL BETWEEN FS 985.00 - 1000.00. AREAS MARKED. (C-CHECK RO 4/3/2021) REPLACED LH FLOOR SILL (INTERCOSTAL PN MM670-35657-001) AT FS989-FS1000 LH REF REO 670-53-61-1838 REV -- DATE 2021-03-09 AND CRJ700 SRM 51-42-06-001-001-A01. NO NMar 5, 2021 · N765SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA202157344Slider · nicked*LH NACELLE LOWER TRANSLATING COWL OTBD SLIDER HAS NICKS/GOUGES. MARKED. (C-CHECK RO 4/3/2021) COMPLIED WITH REO 670-54-21-1433 REV -- DATE 2021-03-14. SUBSEQUENTLY DEEMED TRANSCOWL UNAIRWORTHY DUE TO OTHER DAMAGE ADDRESSED ON JOB 710231141 OP 256 CAMP 22Mar 5, 2021 · N765SK · Cndair CL6002C10 · Engine Thrust ReverserSDR SWIA202157343Stringer · corroded*CORROSION ON STGR 26L BETWEEN FS 1088.20 - 1069.75 (C-CHECK RO 4/3/2021) REPLACED DAMAGED SECTION OF STR26L BETWEEN FS1069.75 AND FS1088.20 REF SRM 53-00-03-201-001-A01 AND DWG. MM670-35007 REV W. LEAK TEST GOOD. COMPLIED WITH SKYWEST TASK CARD 51-900-10Mar 5, 2021 · N765SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA202157342Stringer · corroded*CORROSION ON STGR 27 BETWEEN FS 1015.00 - 1031.00. MARKED. (C-CHECK RO 4/3/2021) PERFORMED PERMANENT REPAIR REF MHIRJ REO670-53-61-1851 REV -- DATED 2021-03-24. LEAK TEST GOOD. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKYMar 5, 2021 · N765SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA202157341Stringer · corrodedCORROSION ON STGR 26R, BETWEEN FS 1015.00 - 1031.00. MARKED. (C-CHECK RO 4/3/2021) REMOVED CORROSION FROM STGR 26R BETWEEN FS1015.00 - FS1031.00 REF CRJ 700 SRM 51-21-06-001-001-A01. WITHIN LIMITS REF CRJ700 SRM 51-21-06-001-001-A01 AND REO 670-53-61-1849Mar 5, 2021 · N765SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA202157340Bulkhead · corrodedFS 280.0 RBL 9.0 BULKHEAD EDGE AT FLOOR LEVEL HAS EVIDENCE OF CORROSION. (C-CHECK RO 4/3/2021) INSTALLED -4 POST LOWER END AND -6 ANGLE ON RBL 9.0 FS280.0 DOOR POST REPAIR REF CRJ 700 SRM 53-11-10-201-006-A01 / COMPLIED WITH SKYWEST TASKCARD 51-900-1002Mar 5, 2021 · N765SK · Cndair CL6002C10 · Fuselage Main, BulkheadSDR SWIA202157339Bulkhead · corrodedLBL 9.0 EDGE OF BULKHEAD DOWN AT FLOOR LEVEL HAS EVIDENCE OF CORROSION. FS 280.0 (C-CHECK RO 4/3/2021) INSTALLED -3 POST LOWER END AND -5 ANGLE ON LBL 9.0 FS280.0 DOOR POST REPAIR REF CRJ 700 SRM 53-11-10-201-006-A01 / COMPLIED WITH SKYWEST TASKCARD 51-Mar 5, 2021 · N765SK · Cndair CL6002C10 · Fuselage Main, BulkheadSDR SWIA202157365Support · corrodedLOWER FUSELAGE AT FS 939.0 FAIRING SUPPORT ASSEMBLY THERE IS EVIDENCE OF CORROSION. (C-CHECK RO 4/3/2021) REMOVED AND REPLACED FAIRING SUPPORT SPLICE ANGLE WITH NEW PART # SH670-39189-1 REF CRJ700 SRM 51-42-06-001-001-A01, CRJ700 SRM 51-45-00-001-001-A01Mar 4, 2021 · N765SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA202157338Slider · nickedRH NACELLE UPPER TRANSLATING COWL OTBD SLIDER HAS NICKS/GOUGES. AREAS MARKED. (C-CHECK RO 4/3/2021) BLENDED OUT NICKS/GOUGES REF CRJ700 SRM 51-12-00-001-001-A01. FOUND TO BE WITHIN LIMITS PER REO 670-54-21-1434 REV-- DATE 2021-03-15. COMPLIED WITH TASK CAMar 4, 2021 · N765SK · Cndair CL6002C10 · Nacelle/Pylon, Main FrameSDR SWIA202157337Mount Bracket · corrodedFOUND MOUNT BRACKET ON THE O/B SIDE OF THE LH INTERNAL REAR SPAR TO THE AUXILLARY SPAR SECTION BEHIND PANEL 542AZ CORRODED. / (AREA MARKED) (C-CHECK RO 4/3/2021) REMOVED AND INSTALLED NEW MOUNT ANGLE WITH PN CC670-10338-1 O/B SIDE LH INTERNAL REAR SPAR REMar 3, 2021 · N765SK · Cndair CL6002C10 · Wing, Attach FittingsSDR SWIA202157336Bracket · corrodedFOUND THE MOUNT BRACKET ON THE I/B SIDE OF THE RH INTERNAL REAR SPAR TO AUXILLARY SPAR SECTION BEHIND PANEL 642AZ CORRODED. / (AREA MARKED). (C-CHECK RO 4/3/2021) INSTALLED NEW REPLACEMENT MOUNT BRACKET (P/N CC670-10338-2)ON THE I/B SIDE OF THE RH INTERNAMar 3, 2021 · N765SK · Cndair CL6002C10 · Fuselage Main, Attach FittingsSDR SWIA202157364Structure · corroded* RH OVERWNG EXIT DOOR, HARDWARE INTERIOR ABOVE WINDOW IS CORRODED. FLAGGED (C-CHECK RO 4/3/2021) REMOVED AND REPLACED RH OVERWING EXIT DOOR HARDWARE. REF CRJ700 AMM 52-21-02-000-801-A01Mar 2, 2021 · N765SK · Cndair CL6002C10 · Emergency ExitsSDR SWIA202157335Skin · gouged*RH WING INBD FLAP HAS GOUGE ON LOWER EXTERIOR SKIN TRAILING EDGE BETWEEN APPROX WS 68.00 - 88.00. AREA MARKED. (C-CHECK RO 4/3/2021) INSTALLED -1 REPAIR DOUBLER AND -2 REPAIR FILLER ON R/H WING INBOARD FLAP LOWER SKIN REF CRJ 700 SRM 57-52-01-201-001-A01Mar 1, 2021 · N765SK · Cndair CL6002C10 · Trailing Edge FlapsSDR SWIA202157334Skin · nicked*LH WING INBD FLAP HAS NICKS ON LOWER EXTERIOR SKIN BETWEEN FLS 15.00 - 38.00 APPROX 8 INCHES FROM TRAILING EDGE. AREAS MARKED. (C-CHECK RO 4/3/2021) REPAIRED DENT AND NICK (OUT OF LIMIT) ON LH WING INBD FLAP LOWER SKIN AT FLS 15.0 - FLS 38.0 REF CRJ 700 Mar 1, 2021 · N765SK · Cndair CL6002C10 · Trailing Edge FlapsSDR SWIA202157333Floorbeam · dentedAFT BAGGAGE FLOOR CROSSBEAM AT FS1031 IS DENTED (C-CHECK RO 4/3/2021) REMOVED UNSERVICEABLE ATTACHING SUPPORT ANGLE AND INSTALLED NEW ATTACHING SUPPORT ANGLE ON CROSSBEAM AT FS1031.00 REF CRJ 700 SRM 51-42-06-001-001-A01 DWG MM670-35360 REV A. COMPLIED WIMar 1, 2021 · N765SK · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SWIA202157332Drag Angle · crackedLH V/STAB TO FUSELAGE ATTACHMENT AFT DRAG ANGLE POSSIBLE CRACK. MARKED (C-CHECK RO 4/3/2021) REMOVED UNSERVICEABLE PARTS AND INSTALLED NEW AFT DRAG ANGLE ON LH V/STAB TO FUSELAGE IAW CRJ SRM 51-42-13-001-001-A01, CRJ-700 SRM 51-42-21-001-001-A01, CRJ700 Feb 28, 2021 · N765SK · Cndair CL6002C10 · Fuselage, Stabilizer Attach FittingsSDR SWIA202157331Skin · dentedDENT LOCATED APPROXIMATELY 6 O'CLOCK ON THE LH ENGINE FAN COWL. PLEASE EVALUATE, REPAIR AS NEEDED, OR FILL AND PAINT TO REMOVE EVIDENCE OF DENT. (C-CHECK RO 4/3/2021) REMOVED DENT APPROXIMATELY 6 O'CLOCK ON THE LH ENGINE FAN COWL REF REO 670-54-14-1012 RFeb 16, 2021 · N765SK · Cndair CL6002C10 · Nacelle/Pylon, Plate/SkinSDR SWIA202051637Windshield · crackedAIRCRAFT DIVERTED TO OKC PILOTS WINDSHIELD CRACKED FLIGHT 2953. REMOVED AND REPLACED THE PILOT SIDE WINDSHIELD FOLLOWING THE APPLICABLE STEPS IN MIP 56-220-1000-SKY. REFERENCE CP: 21335653 FOR THE PRESSURIZATION AND LEAK CHECK OF LH WINDSHIELD REQUIREAug 4, 2020 · N765SK · Cndair CL6002C10 · Flight Compartment WindowsSDR SWIA2019122647131Smoke Warning · false activationSMOKE AFT LAV WARNING MESSAGE AT V2, FLIGHT 3269. COMPLIED WITH SERVICE BULLETIN, REMOVED AND REPLACED THE LEFT ENGINE SEAL VALVE IAW AMM. PERFMOED ENGINE RUNS USING APU AIR AND ENGINE BLEED AIR. COULD NOT REPRODUCE, NO LAVATORY SMOKE WARNING MESSAGES DISPDec 23, 2019 · N765SK · Cndair CL6002C10 · Smoke DetectionSDR SWIA2019082046193Controller · failedL BLEED DUCT WARNING MESSAGE; WENT TO CAUTION. RAN QRH. RTF. CLOSED, REMOVED, AND REPLACED AILC IAW AMM. OPS CHECK GOOD NO DEFECTS NOTED AT THIS TIME.Aug 20, 2019 · N765SK · Cndair CL6002C10 · Pneumatic Indicating SystemSDR SWIA2018080644970Striker · corrodedGALLEY SERVICE DOOR LOWER SEAL STRIKER WAS CORRODED. REMOVED AND REPLACED THE SEAL STRIKER IAW SRM.Jul 23, 2018 · N765SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2018080644969Angle · corrodedGALLEY SERVICE DOOR LOWER SILL ANGLE WAS CORRODED. INSTALLED A NEW ANGLE IAW SRM.Jul 23, 2018 · N765SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2018080644968Door Sill · corrodedGALLEY SERVICE DOOR SILL WAS CORRODED. REPLACED THE DOOR SILL IAW SRM.Jul 23, 2018 · N765SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2018080644967Stringer · corrodedSTRINGER 26L BETWEEN BS 295 - 310 HAD CORROSION. REMOVED AND REPLACED THE STRINGER IAW SRM.Jul 21, 2018 · N765SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2018080644966Stringer · corrodedSTRINGER 26R BETWEEN BS 295 - 310 HAD CORROSION. REPLACED THE STRINGER IAW SRM.Jul 21, 2018 · N765SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2018080644965Stringer · corrodedSTRINGER 27 BETWEEN BS 310 - 319 HAD CORROSION. REPLACED THE STRINGER IAW SRM.Jul 21, 2018 · N765SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2018080644964Doubler · corrodedTCAS OMNIDIRECTIONAL ANTENNA DOUBLER HAD CORROSION. REPLACED THE DOUBLER IAW SRM.Jul 21, 2018 · N765SK · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR SWIA2018080644963Frame · corrodedMAIN AVIONICS BAY FRAME AT BS 319, BETWEEN STRINGERS 26R - 26L HAD CORROSION. REPAIRED THE FRAME IAW SRM.Jul 21, 2018 · N765SK · Cndair CL6002C10 · Fuselage Main, FrameSDR SWIA2018080644962Frame · corrodedMAIN AVIONICS BAY FRAME AT BS 295, BETWEEN STRINGERS 26R - 26L HAD CORROSION. REPAIRED THE FRAME IAW SRM.Jul 21, 2018 · N765SK · Cndair CL6002C10 · Fuselage Main, FrameSDR SWIA2018080644961Frame · corrodedMAIN AVIONICS BAY FRAME, BS 310, BETWEEN STRINGERS 26R - 24L HAD CORROSION. REPAIRED THE FRAME IAW SRM.Jul 21, 2018 · N765SK · Cndair CL6002C10 · Fuselage Main, FrameSDR SWIA2018080644960Frame · corrodedFRAME AT BS 319.7 BETWEEN STRINGERS 18L - 21L HAD CORROSION. REPLACED THE FRAME IAW SRM.Jul 21, 2018 · N765SK · Cndair CL6002C10 · Fuselage Main, FrameSDR SWIA2018080644959Intercostal · corrodedINTERCOSTAL STRINGER 21L FROM BS 333 - 349 HAD CORROSION. REPLACED THE INTERCOSTAL IAW SRM 51-42-06-001-001-A01.Jul 21, 2018 · N765SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2018080644958Intercostal · corrodedINTERCOSTAL AT STRINGER 21L, BS 310 - 333 HAD CORROSION. REPLACED THE INTERCOSTAL IAW SRM.Jul 21, 2018 · N765SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA201743205Skin · chafedTHE LT AILERON'S UPPER FIXED LEADING EDGE WAS CHAFED OUT OF LIMITS. REMOVED AND REPLACED THE LT AILERON UPPER IAW SRM.Mar 23, 2017 · N765SK · Cndair CL6002C10 · AileronsSDR SWIA201743207Support Angle · corrodedAFT WING TO FUSELAGE FAIRING SUPPORT FRAME LOWER ANGLE HAS CORROSION NEAR CENTER OF FRAME, BS 939. REMOVED AND REPLACED FAIRING SUPPORT LOWER ANGLE IAW SRM.Mar 21, 2017 · N765SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA201743206Latch · chafedRIGHT LOWER TRANSCOWL LATCH DOOR COAMING AND DOUBLER ARE CHAFED AT THE SPIGOT HOLE. PERFORMED PERMANENT REPAIR IAW REO.Mar 20, 2017 · N765SK · Cndair CL6002C10 · Nacelle/Pylon, Main FrameSDR SWIA201743204Panel · corrodedPANEL 832BL CORRODED. INSTALLED REPLACEMENT PANEL 832BL IAW SRM AND AMM.Mar 19, 2017 · N765SK · Cndair CL6002C10 · Fuselage Structure (General)SDR SWIA201743203Fairing · crackedRIGHT ENGINE PANEL 443BB HAS A TWO INCH CRACK AT AFT BOLT HOLE. INSTALLED REPLACEMENT HINGE LINE FAIRING SKIN IAW SRM.Mar 19, 2017 · N765SK · Cndair CL6002C10 · Nacelle/Pylon, Main FrameSDR SWIA201743202Fairing · chafedTHRUST REVERSER HINGE LINE FAIRING 433BB IS CHAFED. INSTALLED A REPLACEMENT HINGE LINE FAIRING SKIN IAW SRM.Mar 19, 2017 · N765SK · Cndair CL6002C10 · Engine Thrust ReverserSDR SWIA201541217Vane · crackedLT ENGINE LOWER INBD CASCADE HAS CRACKED VANE. REPAIRED IAW EA.May 7, 2015 · N765SK · Cndair CL6002C10 · Turbine Engine Air Inlet SectionSDR SWIA201541216Module · damagedFWD CARGO, FWD RETRIEVAL MODULE, HAS DAMAGE TO FIBERGLASS ON AFT EDGE. REPAIRED FWD RETRIEVAL MODULE IAW EA.May 7, 2015 · N765SK · Cndair CL6002C10 · Cargo CompartmentsSDR SWIA201541213Cable · chafedRT ENGINE, CABLE IS RUBBING AGAINST FIRE DETECTION ELEMENT GUIDE TUBE AT 5 O-CLOCK POSITION. REPAIRED RT ENGINE CABLE WIRE CONDUIT IAW REO.May 7, 2015 · N765SK · Cndair CL6002C10 · Engine (Turbine/Turboprop)SDR SWIA201541220Structure · crackedFWD EQUIPMENT COMPARTMENT, TRU BAY. CRACK IN FLOOR AT LT CUTOUT FOR FRAME 193. REPAIRED CRACK IN THE LT TRU BAY, STA 193 IAW REO.May 6, 2015 · N765SK · Cndair CL6002C10 · Fuselage Main, StructureSDR SWIA201541219Structure · crackedFWD EQUIPMENT COMPARTMENT, TRU BAY- CRACK IN FLOOR AT RT CUTOUT FOR FRAME 193. REPAIRED CRACK IN RT FWD TRU BAY IAW STS EA.May 6, 2015 · N765SK · Cndair CL6002C10 · Fuselage Main, Structure
Back to N765SK