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 DXTA2020101404209Unknown · unknownUPON REACHING THE AIRCRAFT AND CONNECTING BATTERIES WE PLACED EMERGENCY LIGHTS INTO ARM POSITION, PER POWER ON CHECKLIST. NO EMERGENCY LIGHTS ILLUMINATED. PLACED SWITCH INTO ON POSITION, NO LIGHTS ILLUMINATED. CONNECTED BATTERIES AND PERFORMED THE EMERGENCYSDR DXTA2020101204198Warning Message · false activationCLIMB OUT GOT NOSE DOOR OPEN RT. QHR COMPLIED WITH. RETURN TO KDAL. POST FLIGHT SAW BOTTOM RIGHT LATCH POPPED OUT. CYCLED ALL LATCHES, CASS EXTINQUISHED. TALKED TO MC TOLD THEM LOCKING SIDE OF LATCH NEEDS ADJUSTING. BARELY TAPPED CLOSING LATCH AND IT POPSDR DXTA202010054170Wire Harness · brokenUPON CLOSING CABIN DOOR COULD NOT GET "CABIN DOOR OPEN" AMBER CAS TO GO OUT. CHECK DOORS CAS TURNED WHITE. TRIED AOB PROCEDURE AND USING OVERRIDE WITH THE SAME RESULT. SIGN OFF. INSPECTED DOOR WIRING NOTING HARNESS APPEARED TO BE PINCHING IN THE UPPER STEPSDR DXTA2020100504170Warning Light · illuminatedUPON CLOSING CABIN DOOR COULD NOT GET "CABIN DOOR OPEN" AMBER CAS TO GO OUT. "CHECK DOORS" CAS TURNED WHITE. TRIED AOB PROCEDURE AND USING OVERRIDE WITH THE SAME RESULT.SDR DXTA2020100404166Warning Light · false activationAT FLIGHT ALTITUDE, "NOSE DOOR OPEN L" AMBER LIGHT ILLUMINATED. LIGHT EXTINGUISHED UPON LANDING AT DIVERSION AIRPORT. SIGN OFF. ARRIVED AT THE AIRCRAFT WITH THE MESSAGE NOT PRESENT. CHECKED RECENT FAULT MESSAGES AND FOUND CODE 1420 "NOSE DOOR OPEN L" WHICHSDR 2020F00421Doubler · crackedCRACK DAMAGE REPAIR OF NOSE LANDING GEAR WHEEL WELL (NWW), FRAME WEB, AND DOUBLERS, FS 75. TEXTRON AVIATION STANDARD REPAIR SR-680A-ATA53-25890 DATED 06/01/2020 WITH FAA FORM 8100-9 DATED 06/01/2020.SDR DXTA2020100304162Door · bindingWHEN OPENING THE MAIN CABIN DOOR THE DOOR TEMPORARILY HANGS UP BEFORE FALLING TO THE FULL OPEN POSITION. SEEMS TO BE RUBBING ON THE BLACK GUILD BLOCK ON THE INSIDE OF THE DOOR FRAME. SIGN OFF. GAINED ACCESS AND WAS ABLE TO DUPLICATE ISSUE. ADJUSTED THE FWDSDR JGVR20201001001Skin · debondedVERTICAL STAB AFT SPAR LT UPPER ANGLE HAS 2 AREAS OF VERIFIED INTERGRANULAR CORROSION. MECHANICALLY BLENDED 2 AREAS ON VERTICAL STAB AFT SPAR LT UPPER ANGLE, IAW CESSNA 680 SRM 51-70-02. EVALUATED AREA AND FOUND TO BE OUT OF SRM LIMITS. PERFORMED TEXTRON FISDR 2020F00420Doubler · 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 2020F00419Skin · corrodedREPAIR OF CORROSION AND CHAFING ON HORIZONTAL UPPER AND LOWER SKINS. TEXTRON AVIATION ENGINEERING REPAIR LETTER DQ27201M1 DATED 09/30/2020. HORIZONTAL STABILIZER UPPER AND LOWER SKIN DAMAGE (CHAFING/CORROSION).SDR 2020F00418Doubler · gougedSCREW GOUGES, AFT CABIN, ESCAPE HATCH INTERIOR SURROUND, FS 400-FS 430. ACCOMPLISHED TEXTRON AVIATION FIELD REPAIR FR-680-0235-8382 REV-, DATED SEP 17, 2020 AND FAA FORM 8100-9 DATED 9/18/2020. FIELD REPAIR-SCREW GOUGES, AFT CABIN, ESCAPE HATCH INTERIOR SURSDR 2020F00417Stringer · corrodedCORROSION, FUSELAGE, DROP AISLE, FS 164 TO FS 209. ACCOMPLISHED TEXTRON AVIATION FIELD REPAIR FR-680-0235-8359 REV-, DATED SEP 9, 2020 AND FAA FORM 8100-9 DATED 9/11/2020. FIELD REPAIR-CORROSION, FUSELAGE, DROP AISLE, FS 164 TO FS 209.SDR 2020F00412Skin · corrodedAPU STINGER SKIN DAMAGE (CORROSION). ACCOMPLISHED TEXTRON AVIATION ENGINEERING LETTER DQ27131M1, DATED SEPTEMBER 24, 2020; 680A-0040 (N503QS) APU STINGER SKIN DAMAGE (CORROSION).SDR DXTA2020092804144Battery Pack · inoperativeEMERGENCY LIGHTS DO NOT ILLUMINATE WHEN SWITCH IS PLACED TO ARM WITH BATTERIES OFF. FOUND DURING PREFLIGHT. R & R THE NR 1 EMERGENCY BATTERY, CHARGED BATTERY WITH AIRCRAFT SYSTEM ON PERFORMED OPERATIONAL CHECK, ALL CHECKED GOOD. WORK DONE, IAW CE-680 CHAPT SDR DXTA2020092804145Light · unknownEMERGENCY EXIT LIGHT ABOVE THE CABIN DOOR REMAINED ON AFTER SHUTDOWN. SIGNOFF. REMOVED CENTER PEDESTAL PANEL 224BR TO GAIN ACCESS TO THE NR 1 EMERGENCV INERTIAL SWITCH. ONCE SWITCH WAS RESET THE CABIN DOOR EMERGENCY EXIT LIGHT TURNED OFF. PERFORMED OP CHECSDR 2020FA0000423Web · crackedSTANDARD REPAIR CRACK DAMAGE, NOSE LANDING GEAR WHEEL WELL (NWW), FRAME, WEB, AND DOUBLERS, FS 75. FIELD REPAIR SR-680A-ATA53-25890 REV- DATED 6/1/2020 WITH FAA FORM
8100-9.SDR DXTA2020090927041Battery Pack · inoperativeEMERGENCY LIGHTS WILL NOT ILLUMINATE WITH EMER SWITCH IN ON POSITION. DUPLICATE WRITE UP. SIGNOFF. PERFORMED OPS CHECKS OF THE EMERGANCY LIGHTING. OPS CHECKED PASSED. PERFORMED EMERGENCY BATTERY CHARGING FOR AN HOUR WITH GPU AND REMOVED GPU GAINED ACCESS SDR DXTA2020092604132Latch · bindingMAIN CABIN DOOR WILL NOT LATCH CLOSED. DOOR WILL RAISE NORMALLY, BUT CAN NOT CLOSE HANDLE FROM INSIDE OR OUTSIDE. SIGNOFF. PERFORMED CABIN DOOR OPS CHECK AND FOUND THE CABIN DOOR LATCH TO BE JAMMED. REMOVED FWD AND AFT DOOR COVER, FWD AND AFT STEP COVER, LSDR DXTA2020092604133Track · defectiveLEFT SIDE LAV DOOR IS OFF TRACK AND STUCK IN PARTIALLY EXTENDED POSITION. SIGN OFF. INSTALLED A NEW POPUP CARRIER TRACK AND A NEW POPDOWN CARRIER TRACK IN THE LEFT AFT DIVIDER POCKET DOOR. MX IAW CE-680 MM 25-20-10, OPS CHECK GOOD.SDR DXTA202009254129Wire · damagedDURING AND AFTER APU START UP IN FLIGHT WITH APU BLEED OFF WE HAD AN ELECTRICAL SMOKE SMELL COMING FROM THE COCKPIT GASPERS. AFTER SHUTDOWN OF THE APU THE SMELL WENT AWAY. SIGN OFF. UPON INSPECTION FOUND FOUR WIRES EXHIBITING A BURNED/CHAFED APPEARANCE. DSDR DXTA2020092304121Light · faultedWHEN EMERGENCY LIGHT SWITCH IS PLACED IN ARM POSITION, EMERGENCY LIGHTS WILL NOT ILLUMINATE. EMERGENCY LIGHTS DO ILLUMINATE WITH SWITCH IN ON POSITION. POWERED ON AIRCRAFT AND APPLIED EXTERNAL POWER. PERFORMED OPERATIONAL CHECK OF EMERGENCY LIGHTING SYSTEM.SDR 2020F00375Support Frame · crackedNOSE LANDING GEAR WHEEL WELL FRAME CRACK.SDR JGVR20200922001Drag Angle · corrodedLEFT WING AFT DRAG ANGLE HAS 2 AREAS OF VERIFIED CORROSION ALONG OUTBOARD EDGE AND 8 AREAS OF VERIFIED CORROSION ON MIDDLE DRAG ANGLE OUTBOARD EDGE. RIGHT UPPER WING AFT DRAG ANGLE HAS 1 AREA OF VERIFIED CORROSION ALONG OUTBOARD EDGE AND 7 AREAS OF VERIFIED CSDR DXTA2020092104114Switch · malfunctionedMAIN CABIN DOOR EXIT SIGN AND LIGHT UNDER SEAT 10 WILL NOT EXTINGUISH WHEN EMER LIGHTS ARE TURNED OFF. SIGN OFF. RESET INERTIA SWITCH NO 1. OPS CHECK GOOD, ALL WORK DONE I.A.W. CE680A AMM CHAPTER 33-50-11.SDR DXTA2020092004111Spring · brokenMAIN CABIN DOOR HEAVY TO CLOSE. CABIN DOOR MAKES NUMEROUS CREAKING NOISES AS IT CLOSES. REMOVED AND REPLACED BOTH LUBRICATED SPRINGS DUE TO BROKEN AND CRACKED SPRINGS. RIGGED CABLE TENSIONS, OPERATIONS CHECK GOOD, DOOR CLOSES MUCH EASIER. ALL WORK DONE, IASDR DXTA2020091904105Light · unknownLOWER EXIT LIGHTS ON EITHER SIDE OF MAIN CABIN DOOR DO NOT ILLUMINATE DURING EMERGENCY LIGHT TEST. THEY ILLUMINATE WHEN BATTERY POWER ON AND EMERGENCY LIGHT SWITCH TO ON. OPERATED EMERGENCY LIGHTS BOTH WITHOUT MAIN SHIP BATTERIES AND WITH BATTERIES CONNECTEDSDR 2020FA0000414Rib · crackedLT PYLON AFT RIB P/N: 7412315-19 IS CRACKED, REFERENCE TEXTRON AVIATION ENGINEERING MEMO DQ27074 DATED: 18/SEP/2020.SDR 2020F00398Frame · crackedNLG MID FRAME CRACK. ACCOMPLISHED NETJETS RFTS-104151 REV 0 DATED 03SEP20; N361QS (S/N 680-0235) NLG MID FRAME CRACK PERMANENT REPAIR.SDR EBVR20200915001Structure · corrodedFOUND DURING CABIN INTERNAL ZONAL INSPECTION, FOUND SEVERAL SPOTS OF CORROSION ON STRUCTURE UNDER THE CENTER DROP AISLE PANELS. PERFORMED AQRD REPAIR ERO-966932 REVISION A DATED SEP 10 2020 AT FUSELAGE FLOOR F.S. 157.SDR DXTA2020091404086Actuator · failedON DESCENT, STARTED TO SMELL A LIGHT BURNING SMELL IT WAS FOLLOWED BY AN AMBER BLD AIR O TEMP R CAS MESAGE. WE RAN THE CHECKLIST AND THE CAS MESSAGE WENT OUT. THE SMELL WENT AWAY. AFTER A FEW MINUTES THE BURNING SMELL RETURNED, SO WE JUST TURNED THE RIGHT SDR DXTA2020091404090Warning Light · false activationCLIMBING THROUGH APPROXIMATELY 15,000 FEET, ENGINE/STAB A/I WAS SELECTED ON. A SMELL OF HOT DUCTING SENSED BY BOTH CREW. IN A FEW MINUTES, "A/I INB WNG COLD" LEFT AND RIGHT AMBER CAS MSGS ANNUNCIATED. COMPLETING AMBER MSG B2 CHECKLIST, CAS EXTINGUISHED AND SDR JGVR20200914002Skin · corrodedREMOVE AND REPLACE CORRODED RT WING TRAILING EDGE SKIN P/N 6922681-70. REMOVED AND REPLACED CORRODED RT WING TRAILING EDGE SKIN BOND ASSEMBLY WITH NEW P/N 6922681-70 S/N LOT NR 29598079.SDR JGVR202009141001Skin · corrodedBLENDED MULTIPLE AREAS OF CORROSION ON LT UPPER WING SKIN AT WS 37 FROM FS 408.46 THRU 482.46. PERFORMED AN EDDY CURRENT INSPECTION AND AN ULTRASONIC THICKNESS INSPECTION ON BLENDED AREAS. REMOVED BLENDED FASTENERS AND REPLACED FASTENERS AS NECESSARY WITH HLSDR JGVR20200911001Spar · damagedA) REPAIRED BLENDED AREAS ON LT WING LOWER REAR SPAR ANGLE AT LWS 27 AND LWS 40 PER AQRD ERO-966905 TITLED "LT WING REAR SPAR ANGLE REPAIR" DATED 09/11/2020 AND SUPPORTED BY FAA FORM 8110-3 DATED 09/11/2020. 20) THE F&DT EVALUATION MUST BE COMPLETED WITHIN 12SDR 2020F00377Skin · corrodedREPAIR OF CORROSION ON RT UPPER STABILIZER SKIN. TEXTRON AVIATION ENGINEERING REPAIR LETTER DQ26909M1 RRL DATED 09/09/2020, RRL RT STABILIZER UPPER SKIN CORROSION.SDR DXTA2020090904074Filter · odorIN FLIGHT, CLIMBING THROUGH APPROXIMATELY 31000 FEET THE CREW DETECTED A DEFINITE ODOR FROM THE CONDITIONED AIR OUTLET. ODOR ASSOCIATED WITH SOMETHING OVERHEATING THOUGH NO SIGN OF SMOKE OBSERVED IN THE AIRCRAFT. ODOR WAS WITH US FOR ABOUT 10 MINUTES THEN SESDR DXTA2020090908040Wire Harness · defectiveLANDING GEAR HANDLE REMAINED LOCKED WHILE ATTEMPTING GEAR RETRACTION AFTER TAKEOFF. AMBER "WOW MISCOMPARE" ILLUMINATED SHORTLY AFTER RETRACTION ATTEMPT AND REMAINED ON UNTIL LANDING. THRUST REVERSERS AND NOSE WHEEL STEERING OPERATED NORMALLY. SIGN OFF. REMSDR JGVR20200902001Spar · corrodedLT MLG WHEEL WELL LOWER AFT SPAR HAS 2 AREAS OF VERIFIED CORROSION. REMOVED 3 EACH HI-LOKS FROM LT MLG WHEEL WELL LOWER AFT SPAR FOR ACCESS. BLENDED 2 EACH AREAS OF CORROSION ON LT MLG WHEEL WELL LOWER AFT SPAR. OTBD AREA WAS FOUND TO BE MILD SURFACE CORROSSDR DXTA2020083104036Seal · damagedLANDING GEAR WOULD NOT RETRACT AFTER TAKE OFF. COMPLIED WITH QRH AND RETURNED FOR LANDING WITH NORMAL PROCEDURES. NO UNSAFE MESSAGES NOTED. THE AMBER WOW MISCOMPARE MESSAGE APPEARED FOR 20 SEC IN THE DOWNWIND AND WENT AWAY. SIGN OFF. TROUBLESHOT SYSTEM TOSDR 2020F00373Doubler · 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 EBVR20200828001Structure · corrodedDURING CABIN INTERNAL ZONAL INSPECTION FOUND SEVERAL SPOTS OF CORROSION ON STRUCTURE UNDER THE CENTER DROP AISLE PANELS. COMPLY WITH FLOOR REPAIRS PER AQRD ERO. FABRICATED AND INSTALLED -001 DOUBLER, -002 DOUBLER, -003 SHIM, AND FORWARD WEB AT F.S. 157 IAW ASDR JGVR20200827002Drag Angle · corrodedRT WING AFT DRAG ANGLE HAS 7 AREAS OF VERIFIED CORROSION ALONG OUTBOARD EDGE AND 6 AREAS OF VERIFIED CORROSION ON MIDDLE DRAG ANGLE OUTBOARD EDGE. REPAIRED DELAMINATED AREA ON RT WING UPPER MIDDLE DRAG ANGLE, PER S-750-ATA51-01RD REV A, DATED 17 FEB 09, SUPPOSDR JGVR20200827001Hinge Fitting · corrodedRUDDER UPPER HINGE POINT, LOWER BRACKET HAS VERIFIED CORROSION AROUND ATTACH BOLT. HAND SANDED AREA OF CORROSION LOCATED ON UPPER RUDDER HINGE, LOWER PLATE, LT SIDE. FOUND CORROSION DAMAGE TO BE LEVEL 2, PER NJA GMM 2.2.2. REMOVED AND REPLACED CORRODED LOWESDR DXTA2020082604025Uplock Switch · out of adjustDURING GEAR RETRACTION WE RECIEVED AMBER CAS "GEAR DISAGREE N". THE GEAR SYNOPTIC ON EICAS SHOWED MAIN GEAR UP, BUT NOSE GEAR HAD A SQUARE HASHED SYMBOL. CHECKLIST COMPLETED, 3 GREEN UPON GEAR EXTENSION. SIGN OFF. FOUND NLG UPLOCK SWITCH OUT OF ADJUSTMENT. SDR DXTA2020082003992Handle · bindingMAIN CABIN DOOR HANDLE IS JAMMED IN THE OPEN POSITION. UNABLE TO SECURE DOOR CLOSED. SIGN-OFF. FOUND SLIDING BOLTS HAD SLID INSIDE THE DOOR AND JAMMED THE ENTIRE DOOR MECHANISM. PERFORMED ALL RIGGING AND HEALTH CHECKS, AS PER CESSNA TEAM 680 REQUESTS. WORSDR 2020F00363Skin · corrodedAPU STINGER SKIN DAMAGE (CORROSION), REF ENGINEERING MEMO DQ26585M1 DATED AUGUST 13, 2020.SDR 2020F00362Cowling · overheatedRIGHT ENGINE UPPER COWL HEAT DAMAGE, REF ENGINEERING MEMO DQ26626 DATED AUGUST 16, 2020.SDR 2020F00361Strut · scratchedNOSE LANDING GEAR INNER BORE DAMAGE (SCRATCHES), REF ENGINEERING MEMO DQ26613M1 DATED AUGUST 14, 2020.SDR DXTA2020081703981Pin · bindingAFTER CLOSING THE MAIN CABIN DOOR THE DOOR LATCHING HANDLE WILL NOT MOVE TO THE CLOSED POSITION. RAN THE QRH WHILE PUSHING THE DOOL LIFT CANCEL BUTTON, WE NEVER GOT THE CHECK HANDLE/PUSH TO OVERRIDE LIGHT TO FLASH. PERFORMED ONE POWER UP ANOMALIES CHECK LISTSDR JGVR20200811002Frame · chafedREPLACE CHAFED FRAME JUST FWD OF E EXIT AT APPROXIMATELY F.S. 405.40 AND REPAIR SIX CHAFE MARKS ABOVE E-EXIT ON RH INTERNAL FUSELAGE STRUCTURE BETWEEN APPROX FS 404.26 AND 426.26 AND BETWEEN STRINGERS S-4R AND S-5R. REPLACED CHAFED FRAME JUST FORWARD OF E-EXIT
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