Textron 680A
Service difficulty reports · 2,672
Newest first. General aviation reporting is voluntary.
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 aircraft_model_key = '680A' 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.
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 aircraft_model_key = '680A' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR JGVR20201214001Spar Cap · corrodedREMOVED EXISTING HI-LOC FASTENERS AND BLENDED CORRODED AREA OF THE LT AFT WING SPAR LOWER CLIP LOCATED IN THE LT MAIN LANDING GEAR WHEEL WELL. PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. CLEANED, TREATED, PRIMED REPAIR AREA, INSTALLED EXISTING FASTENESDR ZLWA20210111001Brake · lockedUPON LANDING IN KASE, BOTH LEFT HAND MAIN LANDING GEAR TIRES RUPTURED. SUSPECTED BRAKE LOCK UP DUE TO FREEZING.SDR DXTA2020121004452Connector · looseCABIN DOOR OPEN CAS MESSAGE CAME ON IN FLIGHT WHEN REACHING FL 400. PERFORMED CABIN DOOR OPEN QRH. LIGHT STAYED ON THE WAY THROUGH LANDING. FOUND ELECTRICAL CONECTOR PC058 ON CABIN DOOR LATCHING PAWL PROXIMITY SWITCH SC007 LOOSE. RESECURE CONNECTOR AS REQUSDR DXTA2020121004453Latch · unsecureAPPROX 5 MIN AFTER TAKEOFF, BAGGAGE DOOR OPEN CAS MESSAGE ILLUMINATED. RAN QRH, FOUND FORWARD TOP BAGGAGE LATCH VERY SLIGHTLY RAISED AFTER LANDING. VERIFIED THAT CAS MESSAGE EXTINGUISHES WHEN ALL LATCHES WERE RE-LATCHED. SIGN OFF. CHECKED ALL LATCHES ON BASDR 2020F00486Skin · chafedREPAIR LOWER SKIN CHAFED FROM ANTI-ICE CROSS-FLOW VALVE. ACCOMPLISHED TEXTRON AVIATION STANDARD REPAIR SR-680A-ATA53-22175 DATED 07/19/2019, STANDARD REPAIR - 680A ALL S/N LOWER SKIN CHAFE FROM ANTI-ICE CROSS-FLOW VALVE. WITH FAA FORM 8100-9 DATED 07/19/2019SDR JGVR20201208001Spar · corroded2 AREAS OF CONFIRMED CORROSION ON VERTICAL STAB SPAR RT AFT SPAR CLIP. MECHANICALLY AND HAND SANDED 1 AREA OF CORROSION LOCATED ON VERTICAL STAB RT AFT SPAR CLIP ON UPPER END AT 1ST RIVET AND 1 AREA OF CORROSION LOCATED 3RD RIVET BELOW UPPER RUDDER HINGE ON RSDR 2020F00485Doubler · crackedREPAIR TO NOSE LANDING GEAR WHEEL WELL CRACKS. TEXTRON AVIATION STANDARD REPAIR SR-680A-ATA53-25890 DATED 06/01/2020, STANDARD REPAIR-CRACK DAMAGE, NOSE LANDING GEAR WHEEL WELL (NWW), FRAME, WEB, AND DOUBLERS, FS 75. WITH FAA FORM 8100-9 DATED 06/01/2020.SDR DXTA2020120504438Landing Gear · malfunctionedARRIVING TJSJ SELECTING GEAR DOWN POSITION WE HAD A GEAR DISAGREE R AMBER CASS MESSAGE. WE RAN THE QRH X2 THAT TOOK US TO N1 LANDING GEAR WILL NOT EXTEND, WE RAN THAT CHECK LIS,T WE BLEW DOWN THE BOTTLE IT FAILED TO EXTEND, WENT TO THE BACK AND BLEW MAIN GEARSDR DXTA2020120504434Handle · lack of lubeMED HANDLE IS DIFFICULT TO OPERATE. SIGN OFF. LUBED AND OPERATED HANDLE SEVERAL TIMES WITH NO DEFECTS NOTED, ALL WORK IAW CE-680A 5PM 20-40-00.SDR DXTA2020120404430Trim System · out of rigEXCESSIVE BACK PRESSURE NEEDED FOR ROTATION. THE HORIZONTAL STAB INDICATIONS SEEMS TO NOT MATCH COCKPIT INDICATIONS. ALL OTHER FLIGHT CONDITIONS ARE NORMAL AND FREE OF MOVEMENT. NORMAL TAKE OFF POSITION CALCULATED AND EXCESSIVE FORCE NEEDED FOR ROTATION. VSDR JGVR20201125001Skin · corrodedREPAIRED CORRODED AFT LOWER TAILCONE SKINS LOCATED ADJACENT AND UNDER THE AFT FUSELAGE-TO-WING CHIN FAIRING BY: R & R AFT CHIN FAIRINGS, BLENDING CORRODED AREAS, PERFORMING NDT, TREATING BLENDED AREAS, AND FABRICATING AND INSTALLING REPAIR DOUBLERS AND SHIMS, SDR JGVR20201124001Web · corrodedBENDED CORRODED AREA AT FS 548.5 RIB WEB LOCATED AT BONDING STRAP ATTACHMENT, PERFORMED NDT AND REPORTED RESULTS FOR REPAIR DISPOSITION. CLEANED, TREATED, PRIMED AND APPLIED CIC TO REPAIR AREA, IAW TEXTRON REPAIR MEMO.SDR 2020F00472Skin · corrodedCORROSION ON WING SKIN. ACCOMPLISHED TEXTRON AVIATION ENGINEERING LETTER DQ11111 DATED NOV 2020.SDR 2020F00455Skin · out of alignmentMISALIGNED HOLES COMMON TO THE HEATED LEADING EDGE SKIN AND THE REPLACEMENT DIFFUSERS. ACCOMPLISHED TEXTRON AVIATION LETTER DQ27749 DATED NOV 8, 2020; 680-0126, N359QS, REPAIR RECOMMENDATION.SDR 2020F00454Spar Cap · damagedVERTICAL FIN AFT SPAR CAP (LEFT SIDE) DAMAGE. ACCOMPLISHED TEXTRON AVIATION LETTER DQ27908M1 DATED NOV 19, 2020; 680-0126 (N359QS) VERTICAL FIN AFT SPAR CAP (LEFT SIDE) DAMAGE.SDR DXTA2020112104386Proximity Switch · failedMAIN DOOR OPEN AMBER CAS MESSAGE DOOR OPEN. ILLUMINATED WITH DOOR CLOSED AND LOCKED. CHECKLIST FOLLOWED. MESSAGE DID NOT CLEAR AND IS CYCLING ON AND OFF. CORRECTIVE ACTION: REMOVED CABIN DOOR PROXIMITY SWITCHES PIN: S2800-1257 AND S2800-1256. REMOVED CABISDR DXTA2020112104384Motor · defectiveTHE MAIN CABIN DOOR WILL ONLY PARTIALLY RAISE BEFORE DISENGAGING AND OPENING AGAIN. TRIED WITH BOTH THE INTERNAL AND EXTERNAL SWITCH WITH NO CHANGE. REMOVED AND REPLACED CABIN DOOR LIFT MOTOR. ALL CHECKS ARE GOOD AT THIS TIME, IAW CE680A AMM 52-15-05.SDR JGVR20201120006Structure · corrodedFOUND SEVERAL AREAS OF CONFIRMED CORROSION UNDER SEVERAL NUTPLATES ON THE V-STAB AT THE FOLLOWING LOCATIONS: 341DL 7 NUTPLATES, 341CL 5 NUTPLATES,341BL 5 NUTPLATES, 341DR 3 NUTPLATES,341CR 5 NUTPLATES, 341AL 1 NUTPLATE. REMOVE NUTPLATES AND BLEND CORROSION. SDR JGVR20201120005Skin · corrodedMECHANICALLY REMOVED 12 AREAS OF CORROSION LOCATED AT LT UPPER WING FWD, MIDDLE AND AFT DRAG ANGLES. REPAIRED CORROSION BLENDS, IAW TEXTRON ENGINEERING STANDARD REPAIR SR-680-ATA57-27245 REV-. TITLED "STANDARD REPAIR-CORROSION, WING UPPER SKINS, WS 37" DATEDSDR JGVR20201120004Drag Angle · damagedREPAIRED BLENDED AREAS ON LT AND RT WING INBOARD SKINS NEXT TO FORWARD DRAG ANGLES, PER TEXTRON FIELD REPAIR, FR-680-0230-8540 REV-. TITLED: FIELD REPAIR-CORROSION, WING, UPPER SKINS, LT/RT WS 37, DATED: 10/29/2020, SUPPORTED BY FAA FORM 8100-9 DATED: 10/29/2SDR JGVR20201120003Skin · corrodedFOUND 17 AREAS OF VERIFIED CORROSION ALONG FUSELAGE AFT CHIN FAIRING. FOUND ADDITIONAL 120 AREAS OF CORROSION UNDER AFT CHIN FAIRING. REPAIRED BLENDED AREAS OF LEVEL 2 CORROSION ON LOWER FUSELAGE SKIN UNDER AFT CHIN FAIRING BY INSTALLING REPAIR DOUBLERS. ALSDR JGVR20201120002Skin · corrodedRT LOWER WING SKIN IN GEAR WELL HAS VERIFIED CORROSION UNDER 7 FASTENERS. PERFORM TEXTRON MINOR REPAIR MEMO DQ27295M1 DATED: OCT 9, 2020 FOR RT LOWER CENTER WING SKIN. REMOVED 7 FASTENERS AND BLENDED 7 AREAS OF CORROSION ON RT LOWER WING SKIN IN GEAR WELL, ISDR JGVR20201120001Skin · corrodedFOUND 11 AREAS OF VERIFIED CORROSION ON E-EXIT OUTER SKIN. FOUND DURING TASK 52-20-00-2202 FOUND 4 ADDITIONAL SPOTS OF VERIFIED CORROSION UNDERNEATH CONTOUR RINGS OF THE E-EXIT.SDR DXTA202011180439Cabin Pressure · defectiveAT FL430 THE AMBER PRESSURIZATION FAULT CAS ILLUMINATED. WE INITIATED THE QRH PROCEDURE AI3. THE CHECKLIST CALLS FOR THE PRESSURIZATION AUTO/MANUAL BUTTON TO BE CYCLED. UPON CYCLING THE BUTTON THE CABIN CLIMBED TO 14000 FT. FROM FL430 TILL LANDING THE PRESSUSDR 2020F00447Door · delaminatedREPAIR OF RIGHT ENGINE UPPER COWL DOOR DAMAGE. TEXTRON AVIATION ENGINEERING REPAIR LETTER DQ27776M1 DATED NOV 10, 2020.SDR DXTA2020111504356Charger · failedEMERGENCY LIGHTING CONSISTING OF AFT OVER WING LIGHT, EXIT SIGN ON BULKHEAD SEAT NINE, EXIT SIGN OVERLAP, SEAT LAV OVERHEAD LIGHT ALL INOPERABLE WITH THE EMERGENCY SWITCH IN ARM AND MAIN BATTERIES OFF. ALSO WITH SWITCH IN ON POSITION AND MAIN BATTERIES OFF NOSDR DXTA2020111504357Battery Pack · inoperativeEMERGENCY LIGHTS ON RIGHT SIDE INOPERABLE. 2 RIGHT SIDE EXTERIOR OVER WING, RIGHT SIDE SHARK LIGHT, INTERIOR LAV OVERHEAD AND EXIT LIGHTS, AFT FLOOR LIGHTING, RIGHT SIDE AFT READING LIGHT ALL INOPERABLE. APU WAS RUN FOR 1/2 HOUR AND NO CHANGE TO STATUS. CORRSDR 2020FA0000501Web · crackedNETJETS REQUEST A PERMANENT REPAIR TO THE NOSE WHEEL WELL STRUCTURE CRACKING. REFERENCE TEXTRON AVIATION STANDARD REPAIR SR-680A-ATA53-25890 REV- DATED JUNE 01, 2020 AND FAA FORM 8100-9 DATED 6/1/2020. STANDARD REPAIR-CRACK DAMAGE, NOSE LANDING GEAR WHEEL WESDR JGVR20201113002Door Frame · chafedREPAIRED CHAFED E-EXIT SURROUND WEB AND FRAME AT APPROXIMATELY FS 400 PER AEROSPACE QRD ERO-967189 REV IR, TITLED "E-EXIT SURROUND WEB AND FRAME REPAIR" DATED OCT 30 2020 AND SUPPORTED BY FAA FORM 8110-3 DATED 10/30/2020.SDR JGVR20201113001Structure · corrodedREPAIRED SEVERAL AREAS OF CORROSION ON FUSELAGE DROP AISLE STRUCTURE BETWEEN FS 165 AND FS 426 PER AEROSPACE QRD ERO-967178 REV IR DATED NOVEMBER 09, 2020 AND SUPPORTED BY FAA FORM 8110-3 DATED NOVEMBER 09, 2020.SDR DXTA2020111204339Motor · defectiveOPENED CABIN DOOR AND ON THE WAY DOWN A LOUD CRACK SOUNDED INTERNALLY. ATTEMPTED TO CLOSE THE DOOR AND THE DOOR ONLY MOVED UP TOWARDS CLOSED POSITION ABOUT TWO FEET THEN STOPS. TRIED TO DISENGAGE CLUTCH TO MANUALLY CLOSE DOOR IN ORDER TO MEL AND COULD NOT DISDR DXTA2020111204337Autopilot Sys · failedWHILE LEVELING AT FL260, FO FLYING FROM RIGHT SEAT, WE NOTED THE LEFT SIDE ALTIMETER WAS READING APPROXIMATELY 300' LOW AND VSI SHOWED A DESCENT. FD MODE OFF CAS MESSAGE CAME ON AND AUTOPILOT FAILED. WE VERIFIED THAT THE RIGHT SIDE SYSTEM WAS CORRECT AND DIVSDR DXTA2020111204342Unknown · malfunctionedMAIN DOOR WILL NOT CLOSE WITH ELECTRIC POWER. POWER DOWN AND RESTART ATTEMPTED, PER AFM. DOOR STILL WILL NOT CLOSE. SIGNOFF. GAINED ACCESS TO AIRCRAFT AND PERFORMED VARIOUS OPERATIONAL CHECKS SUCCESSFULLY. DOWNLOADED ARES FILES AND SENT THEM TO TEXTRON FOSDR BWVR135625Check Valve · stickingTHE CHECK VALVE IS TO PREVENT FUEL IMBALANCE WING TO WING. WHEN CHECK VALVE IS OPERATING CORRECTLY IT IS DIRECTING FUEL FROM ONE SIDE FUEL STORAGE/DISTRIBUTION DIRECTLY TO THE OPPOSITE ENGINE. A FUEL IMBALANCE CONDITION WAS NOTED WHILE THE AIRCRAFT WAS IN MASDR JGVR202001112001Spar · corrodedVERTICAL STAB AFT SPAR LT UPPER ANGLE HAS 2 AREAS OF VERIFIED INTERGRANULAR CORROSION. MECHANICALLY BLENDED CORROSION ON VERTICAL STAB AFT SPAR RT UPPER ANGLE, ABOVE RUDDER LOWER HINGE, IAW CESSNA 680 SRM 51-70-02. FOUND BLENDED AREA TO BE OUT OF LIMITS, PERSDR JGVR20201111002Spar Cap · corrodedFOUND CORRODED AREA ON LT SPAR CAP EXTRUSION OF THE VERTICAL STABILIZER REAR SPAR. REMOVED RIVET OR ACCESS, MECHANICALLY BLENDED CORRODED AREA, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. CLEANED, TREATED, AND PRIMED REPAIR AREA AND INSTALLED NEW RIVESDR JGVR202011110202Spar · corrodedSPOT OF VERIFIED CORROSION IN LT WHEEL WELL ON AFT SPAR, LOWER SPAR CLIP. MECHANICALLY REMOVED 1 SPOT OF VERIFIED CORROSION IN LT WHEEL WELL ON AFT SPAR LOWER SPAR CLIP. FOUND CORROSION BLENDS EXCEEDING C680 SRM 51-70-02 AND SUBMITTED FINDINGS TO TEXTRON ENGSDR JGVR20201111001Spar · corrodedSPOTS OF VERIFIED CORROSION IN RT WHEEL WELL ON AFT SPAR, LOWER SPAR CLIP. MECHANICALLY REMOVED 1 SPOT OF VERIFIED CORROSION IN RT WHEEL WELL ON AFT SPAR LOWER SPAR CLIP. FOUND CORROSION BLENDS EXCEEDING C680 SRM 51-70-02 AND SUBMITTED FINDINGS TO TEXTRON ENSDR DXTA2020111104327Bolt · detachedWHEN OPENING MAIN CABIN DOOR TO EXIT PLANE, BOLT FROM HAND RAIL SEPARATED FROM ROD THAT ATTACHES TO DOOR. FLOATING ROD INHIBITS DOOR OPENING AND CLOSING PROPERLY. CORRECTIVE ACTION: INSTALLED NEW HARDWARE ON UPPER HANDRAIL SUPPORT STRUT. OPERATIONS CHECKS SDR 2020F00441Support Frame · crackedNOSE LANDING GEAR WHEEL WELL FRAME CRACKS.SDR DXTA2020110704319Battery · inoperativeALL AFT INTERIOR EMERGENCY LIGHTS AND ALL EXTERIOR LIGHTS ARE INOPERABLE. PRE-FLIGHT SIGN OFF. SPOKEN WITH PILOTS AS THEY WERE STILL ON THE FIELD AND HAS FOUND THAT AFTER POWER WAS APPLIED TO THE AIRCRAFT FOR AN EXTENDED AMOUNT OF TIME THE EMERGENCY LIGHTINGSDR 2020F00440Skin · gougedLEFT WING INBOARD FLAP DAMAGE (GOUGE). ACCOMPLISHED TEXTRON AVIATION ENGINEERING LETTER DQ27564M1 DATED NOVEMBER 4, 2020; 680A-0052 (N514QS) LEFT WING INBOARD FLAP DAMAGE (GOUGE).SDR 2020F00438Doubler · crackedCRACK DAMAGE, NOSE LANDING GEAR WHEEL WELL (NWW), FRAME, WEB, AND DOUBLERS, FS 75. ACCOMPLISHED TEXTRON AVIATION STANDARD REPAIR SR-680A-ATA53-25890 REV- DATED JUNE 01, 2020 AND FAA FORM 8100-9 DATED 6/1/2020. STANDARD REPAIR - CRACK DAMAGE, NOSE LANDING GESDR 2020F00436Frame · crackedSR-680A-ATA53-25890 MAJOR REPAIR, CRACK DAMAGE, NOSE LANDING GEAR WHEEL WELL, FRAME , WEB AND DOUBLERS FS 75.SDR 2020F00434Support Frame · crackedNOSE LANDING GEAR WHEEL WELL FRAME CRACKS.SDR DXTA2020110104330Control Unit · defectiveAT APPROXIMATELY 150' AGL THE PRIMARY TRIM FAIL LIGHT CAME ON AND THE TRIM STARTED TO RUN AWAY NOSE UP. I PRESSED THE AP/TRIM/NWS DISC BUTTON WHICH STOPPED THE NOSE TRIM UP CONDITION. DURING THE PROCESS HEAVY PRESSURE WAS REQUIRED TO STOP THE NOSE FROM RISINSDR DXTA2020103104296Battery · faultedDURING THE POWER ON CHECKLIST NONE OF THE EMERGENCY LIGHTS WOULD ILLUMINATE WITH THE SWITCH SELECTED TO ARM. THE MAIN BATTERIES WERE CONNECTED BUT OFF. THE EMERGENCY LIGHTS ILLUMINATE WITH THE EMERGENCY LIGHT SWITCH IN THE ON POSITION. SIGN OFF. TECH GAINESDR DXTA2020103004294Battery Pack · dischargedAFTER LANDING AND SHUTDOWN NOTICED THE FORWARD ZONE OF THE EMERGENCY LIGHT SYSTEM STUCK ON. SIGN OFF. WE GAINED ACCESS TO THE "G SWITCH" UP ON THE AFT PORTION OF THE CENTER PEDESTAL BY REMOVING RT SIDE PANEL FORWARD PEDESTAL. RESET "G SWITCH" AND WAS ABLE SDR JGVR20201027002Spar · corrodedMECHANICALLY REMOVED CORROSION FROM AFT SPAR, LOWER FORWARD SPAR CAP ANGLE LOCATED IN RT WHEEL WELL AT WS35. PERFORMED NDT AND REPORTED RESULTS FOR REPAIR DISPOSITION. CLEANED, TREATED AND TOP COATED REPAIRED AREA, IAW TEXTRON STRUCTURES FIELD REPAIR.SDR 2020F00431Structure · damagedRRL WINGTIP DAMAGE. ACCOMPLISHED TEXTRON AVIATION ENGINEERING LETTER DQ27497M1 RRL - DATED OCTOBER 22, 2020 680A-0162 N620QS RRL WINGTIP DAMAGE.
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