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 JGVR20191007001Strut · deterioratedCHROME FINISH IS DETERIORATING AND PITTING IN NLG LOWER BARREL ASSEMBLY. REMOVED EXISTING LOWER BARREL ASSEMBLY AND INSTALLED NEW CUSTOMER SUPPLIED LOWER BARREL ASSEMBLY IN THE SAME LOCATION. REF. CESSNA 680 CMM 32-20-01.SDR DXTR2019091901Skin · corrodedCORROSION ON TRAILING EDGE OF LT HORIZONTAL INBD OF ELEVATOR LOCATED @ APPROXIMATELY FS 708.9 & LBL 10.0 THRU 15.0. REPAIRED IAW NJA RFTS-103563.SDR DXTR201909231Structure · corrodedCORROSION SUSPECTED ON RT UPPER AND LOWER HORZ STAB ATTACH POINTS FOR PANEL 352AC, REPAIRED IAW AQRD REPAIR RFTS-103571.SDR DXTR2019073001Skin · chafedWING ANTI-ICE CROSS FLOW VALVE IS CHAFFING ON FUSELAGE LOWER SKIN. BLENDED OUT DAMAGE TO PREPARE FOR NDT. NO CRACKS NOTED. COMPLETED STANDARD REPAIR SR-680A-ATA53-22175.SDR 2019FA0000234Skin · chafedLWR SKIN CHAFE FROM ANTI-ICE CROSS-FLOW VALVE. REF STANDARD REPAIR SR-680A-ATA53-22175; DATED: 7/19/2019.SDR DXTA2019072402664Probe · blocked1) ENGINE CONTROL FAULT L-R AMBER CAS MESSAGE AFTER TAKEOFF 2) IAS INDICATION BOTH ON ADC 2 AMBER CAS. // SIGNOFF// REMOVED AND REPLACED BLOCKED PROBE. PERFORMED PILOT PITOT PRESSURE LEAK CHECK WITH NO FAULTS NOTED. PERFORMED AOC FUNCTIONAL CHECK WITH NO FASDR CA190723005Actuator · malfunctioned(CAN) DURING THE AIRCRAFT FIRST INSPECTION DOCUMENT 12, CHAFFING WAS DISCOVERED IN THE L/H AND R/H MAIN GEAR SIDEBRACE ACTUATOR SUPPORT FITTINGS. IT WAS CAUSED BY THE ANTI ROTATION LUGS FROM THE MLG ACTUATORS ON THE OPPOSITE SIDE OF THE WEAR PLATE ASSEMBLIES PSDR CA190723010Duct · gouged(CAN) DEEP GOUGES WERE FOUND ON THE BOTTOM SIDE OF BOTH THE L/H (P/N 6914060-59) AND R/H (P/N 6914060-60) WING ANTI ICE DUCTS (REFER TO IPC 30-11-00 FIG1) WHICH WAS CAUSED BY CHAFFING. THE DUCTS RUN IN VERY CLOSE PROXIMITY TO THE L/H AND R/H LIGHT BOXES WHICH SDR DXTR20190702301Skin · damagedWING ANTI ICE CROSS FLOW VALVE STUDS HAVE DAMAGED LOWER FUSELAGE SKIN IN TWO PLACES. BLENDED, OUT DAMAGE TO PREPARE FOR NDT. NO CRACKS NOTED. COMPLETED STANDARD REPAIR SR-680A-ATA53-22175.SDR DXTA2019072102551Printed Ckt Board · defectiveALL LANDING GEAR RETRACTION DID NOT RETRACT - GEAR WOULD NOT RETRACT AFTER TAKEOFF, HOWEVER AFTER PUSHING HARD UP ON GEAR HANDLE, GEAR RETRACTED (BINDING). DURING EXTENSION GEAR CAME DOWN NORMALLY, HOWEVER BINDING TOWARDS GEAR DOWN POSITION WAS VERY NOTIECEABSDR DXTA2019071902638Not Reported · malfunctionedALL LANDING GEAR RETRACTION DID NOT RETRACT - AFTER TAKE OFF WE TRIED TO RETRACT THE GEAR. THE HANDLE POSITIONED UP BUT LANDING GEAR STAYED IN THE LOCKED DOWN POSITION. WE HAD NO CAS MESSAGES OR ANY OTHER INDICATION OTHER THAN 3 GREEN AND DOWN.SDR JGVR20190712001Rib · corrodedFOUND LEVEL 1 CORROSION IN THE LT WHEEL WELL CENTER SPAR #2 RIB DURING THE MLG CORROSION ZONAL INSPECTION. BLENDED CORROSION IN LT WHEEL WELL ON CENTER SPAR #2 RIB. FOUND CORROSION TO BE BEYOND CORROSION LIMITATIONS IAW SRM 51-70-02. REPAIRED CORROSION PER ENGSDR DXTR201907101Anti-Ice Valve · interferenceWING ANTI-ICE CROSSFLOW VALVE HAS CAUSED DAMAGE TO THE LOWER FUSELAGE SKIN. DURING INSPECTION FOUND THERE IS A CHAFFED SPOT ON THE LOWER SKIN P/N: 7411392-12 OF SKIN BOND ASSEMBLY P/N: 7411391-2 FROM A STUD PROTRUDING FROM THE ANTI-ICE CROSS FLOW VALVE THAT HASDR DXTR2019070901Anti-Ice Valve · interferenceWING ANTI-ICE CROSSFLOW VALVE HAS CAUSED DAMAGE TO THE LOWER FUSELAGE SKIN. DURING INSPECTION FOUND THERE IS A CHAFFED SPOT ON THE LOWER SKIN P/N: 7411392-12 OF SKIN BOND ASSEMBLY P/N: 7411391-2 FROM A STUD PROTRUDING FROM THE ANTI-ICE CROSS FLOW VALVE THAT HASDR DXTA2019062802542Coffeemaker · malfunctioned10 MINUTES AFTER DEPARTURE AND LEVEL AT 13,000' WE NOTICED AN ELECTRICAL BURNING SMELL. NO VISIBLE SMOKE, BUT ENOUGH ODOR TO CLEARLY IDENTIFY AN ISSUE. THE ODOR BECAME PRESENT IMMEDIATELY AND SEEMED TO BE MORE PRONOUNCED NEAR THE COCKPIT THAN THE REAR OF THESDR 2019FA0000200Truss · corrodedAPU TRUSS CORRODED. ACCOMPLISHED REPAIR TO APU TRUSS IAW ENGINEERING MEMO DQ21989RR1SDR DXTA2019062602536Uplock Switch · defectiveGEAR DISAGREE R AMBER CAS ILLUMINATED - UPON SELECTING GEAR DOWN, AN AMBER "X" APPEARED IN THE RIGHT MAIN GEAR INDICATOR POSITION ALONG WITH AN AMBER "GEAR DISAGREE R" CAS. WE RAN QRH R1, AND N1 RESULTING IN GEAR BLOWDOWN. LANDING WAS NORMAL. ENGINES WERE SDR 2019F00228Cowling · chafedLH ENGINE UPPER COWL CHAFE. REFERENCE MANUFACTURER DOCUMENT S-750-ATA51/01RD REV. A. AND ENGINEERING MEMO DQW21934M1SDR DXTA2019062412523Circuit Board · malfunctionedENGINE FIRE R RED CAS INTERMITTENT - DESCENDING THROUGH 7000FT, RED ENGINE FIRE R CAS ILLUMINATED FOR ABOUT 1 SECOND WITH ASSOCIATED AUREL MESSAGE RECOMMEND SWAPPING THE NC208 AND NC108 PCB'S. GAINED ACCESS TO PCB'S AND, REMOVED THE LJH PCB P/N: 6918632-12, SSDR DXTA2019060502465Bolt · wornDURING FLIGHT AT FL400 GOT A SEVERE UNKNOWN AIRFRAME VIBRATION. THE VIBRATION WAS FELT THROUGHOUT THE ENTIRE AIRCRAFT. THERE WERE NO ASSOCIATED CAS MESSAGES, NO UNSAVED GEAR INDICATIONS, NO SPOILER DEPLOYED INDICATIONS. THE AIRCRAFT DID NOT LAND OVER WEIGHT. PSDR CA190617025Hose · ruptured(CAN) AFTER LANDING AND EXITING THE AIRCRAFT THE CREW NOTED A PUDDLE OF OIL UNDER THE NOSE LANDING GEAR WELL. THERE WERE NO ABNORMALITIES OBSERVED BY THE CREW OTHER THAN THE LEAK. THE LEAK WAS ORIGINATED FROM THE NOSE WHEEL STEERING HYDRAULIC CENTERING FLEXIBLSDR DXTA2019053002452Unknown · odorAT TOP OF DECENT, FL270 STARTED GET AN OILY SMELL IN THE CABIN. NEVER GOT "SMOKEY" BUT THERE WAS A STRONG ODOR UNTIL AROUND 2500 FT.SDR DXTA2019051702404Seal · deformedENGINE FIRE INDICATION ON RIGHT ENGINE WHILE CLIMBING OUT OF APPROXIMATELY FL190. WHEN THROTTLE WAS BROUGHT TO IDLE, THE FIRE LIGHT EXTINGUISHED IN ABOUT 3 SECONDS. AFTER LANDING, CFR CREWS COULD NOT IDENTIFY ANY HOT SPOTS WITH FLIR EQUIPMENT. COWLING FELT COOSDR DXTA2019051502396Wire Harness · defectiveLEFT MLG LANDING GEAR RETRACTION DID NOT RETRACT - LEFT LANDING GEAR WOULD NOT RETRACT, GEAR INDICATOR LIGHTS REMAINED YELLOW DOWN , ADC SSEC MISSCOMPARE EICAS MESSAGE CAME ON. RAN CHECK LIST GEAR CAME DOWN 3 GREEN THEN EICAS MESSAGE WENT AWAY , LANDED NORMAL.SDR DXTA2019051502397Uplock Switch · intermittentNLG LANDING GEAR RETRACTION DID NOT RETRACT - ON CLIMBING TO FL 430, AT FL 420 AN AMBER "GEAR DISAGREE N" EICAS MESSAGE CAME ON, AND YELLOW HASH NOSE GEAR LIGHT ILLUMINATED. IN DESCENT AT FL 230 GEAR RETRACTED AND ALL THREE WHITE UP LIGHTS CAME ON. LANDED WITHSDR 2019F00191Trunnion · out of toleranceACCOMPLISHED REPAIR OF OVERSIZED DOOR ROD PIN HOLE IN MLG TRUNNION PER ENGINEERING DEFINITION S-680-ATA32/02RD DATED FEB 28, 2014 WITH A FORM 8100-9SDR DXTA201904230182Fairing · damagedDURING CHECKLIST DAMAGE WAS FOUND TO COMPOSITE PANELS ON UNDERSIDE OF AFT FUSELAGE AREA. ACCOMPLISHED AQRD ENGINEERING REPAIR ORDER NO. ERO-103261 DATED APRIL 15, 2019; BELLY AND WHEEL BIN FAIRINGS - PERMANENT REPAIR.SDR DXTA201904230181Cap · erodedRIGHT HORIZONTAL STAB DAMAGED- RIGHT LEADING EDGE HORIZONTAL STAB APPEARS DAMAGED AT THE TIP. ACCOMPLISHED TEXTRON AVIATION ENGINEERING LETTER DQ1922M1 DATED APRIL 17, 2019; 680A-0069 (N527QS) HORIZONTAL STABILIZER RIGHT TIP CAP DAMAGE (EROSION).SDR DXTA201904230180Cap · erodedRIGHT HORIZONTAL STAB DAMAGED - RIGHT LEADING EDGE HORIZONTAL STAB APPEARS DAMAGED AT THE TIP. ACCOMPLISHED TEXTRON AVIATION ENGINEERING LETTER DQ1922M1 DATED APRIL 17, 2019; 680A-0069 (N527QS) HORIZONTAL STABILIZER RIGHT TIP CAP DAMAGE (EROSION).SDR DXTA2019042202297Switch · intermittentRIGHT MLG LANDING GEAR RETRACTION - AFTER TAKEOFF RT MAIN GEAR GREEN DOWN LIGHT REMAINED ILLUMINATED. AFTER A COUPLE MINUTES THE LIGHT WENT OUT. THE CREW IS CERTAIN THE RT GEAR WAS UP AS NORMAL. NO RED LIGHT WAS OBSERVED DURING THIS EVENT (RED INDICATED LISDR DXTA2090419802291Unknown · odorIN BOUND STARTED THE APU AT 2500' AT 200 KTS AND AS THE APU WAS POEWERING UP THE #1 MCDU WENT BLANK AND WE HAD AN ELECTRICAL SMELL IN THE COCKPIT. SHUT THE APU DOWN AND THE #1 MCDU CAME BACK 'ON'AND LANDED NORMAL. REPLACED CONDENSER BAG AND PERFORMED OPS CHSDR 2HGR2019042301Warning System · false activationFROM KAUS TO KCRQ, DURING THE APPROACH, A "FLAP FAIL" CAS MESSAGE WAS DISPLAYED. THE APPROACH WAS CANCELLED, AFTER THE PILOTS FOLLOWED THE QRH PROCEDURES THE FAULT WENT AWAY. THE AIRCRAFT LANDING WITHOUT ANY PROBLEM.SDR DXTA2019041532256Control Unit · contaminatedPRIMARY STAB TRIM FAIL ON CLIMB OUT. CREW ACTIVATED SECONDARY TRIM AND RETURNED FOR LANDING. REMOVED AND REPLACED THE HORIZONTAL TRIM ACTUATOR AND HORIZONTAL TRIM ACTUATOR CONTROL UNIT IAW 680 AMM 27-40-00, OPERATIONAL AND TRAVEL CHECK GOOD.SDR DXTA201904032221Filter · dirtyON CLIMBOUT AND ABOUT TO LEVEL AT 22,000 FT WITH MAX POWER SET AND WING/ENGINE ANTI-ICE SELECTED ON WE GOT BOTH A/I INBOARD WING COLD L-R AND A/I WING COLD L-R CAS MESSAGES. WE RAN APPROPRIATE QRH CHECKLISTS AND APPROXIMATELY 2 MINS AFTER SELECTING BOTH LEFT SDR JGVR20190329002Axle · corrodedRT MLG TRAILING LINK AXLE IS HEAVILY CORRODED. VISUALLY INSPECTED TRAILING LINK ASSEMBLY AND FOUND AXLE CORRODED. REMOVED AXLE AND INSTALLED NEW CUSTOMER SUPPLIED AXLE. REASSEMBLED AND APPLIED SEALANT. REPAIRED IN ACCORDANCE WITH MM REVISION 28 DATED DEC 10, 2SDR DXTA2019031302159Not Reported · malfunctionedRIGHT MLG LANDING GEAR RETRACTION DID NOT RETRACT - RIGHT MAIN LANDING GEAR WOULD NOT RETRACT AS INDICATED BY BOX WITH CROSS HATCH. PERFORMED QRC AND RETURNED TO AIRPORT.SDR DXTA2019032102188Uplock Switch · inoperativeRIGHT MLG LANDING GEAR RETRACTION DID NOT RETRACT - RIGHT MAIN LANDING GESR WOULD NOT RETRACT AS INDICATED BY BOX WITH CROSS HATCH. PERFORMED QRC AND RETURNED TO AIRPORT. REMOVED & REPLACED RIGHT MLG UPLOCK SWITCH - OPS CHK GOOD.SDR DXTA2019031402159Connector · dirtyRIGHT MLG LANDING GEAR RETRACTION DID NOT RETRACT - GEAR DISSAGREE R CAS ILLUMINATED UPON GEAR RETRACTION WITH DN INDICATING ON RT MLG. **SUPPLEMENTAL INFORMATION - REMOVED RT DOWNLOCK SWITCH CONNECTOR & CLEANED CONNECTOR & SWITCH PINS WITH DEOXOT CONTACT CLEASDR DXTA2019031102141Apu · odorAPU SMOKE - AFTER STARTING UP THE APU DURING PREFLIGHT GOT SMOKE THROUGHOUT THE AIRCRAFT. ODOR WAS LIKE AN OIL SMELL. REMOVED & REPLACED APU ASSEMBLY IAW MM 49-10-00.SDR DXTA2019030602117Pushrod · out of adjustNOSE GEAR WOULD NOT EXTEND AFTER LG SELECTED DOWN. GEAR DISAGREE N CAS ILLUMINATED, AS WELL AS "NOT LOCKED" INDICATION ON THE GEAR EIS. RAN ABNORMAL AND EMERGENCY CHECKLISTS. GEAR DID NOT INITALLY EXTEND, BUT FINALLY DID AFTER 6-8 MINUTES. HAD THREE GREEN DOWNSDR DXTA2019030402107Warning System · false activationGEAR DISAGREE R AMBER CAS ILLUMINATED - AFTER GEAR RETRACTION CAS ILLUMINATED WITH AMBER BOX WITH DIAGONAL LINES THROUGH IT FOR THE RIGHT GEAR INDICATION. QRH WAS COMPLETED. ONCE GEAR WAS SELECTED DOWN WE GOT AN AMBER DN INDICATION FOR THE RIGHT MAIN GEAR FOR SDR DXTA2019021200010Drain · leaking1) HYDRAULIC FLUID LEAK - COMPLETE LEFT AND RIGHT HYDRAULIC FLUID LOSS OCCURRED AFTER TAKEOFF WITH GEAR RETRACTED. POSTFLIGHT REVEALED HYDRAULIC FLUID COMING FROM RIGHT ENGINE DRAIN MAST. NO HYDRAULIC FLUID VISIBLE AROUND LEFT OR RIGHT MAIN LANDING GEAR. 2) SDR DXTR2019020601Pcb · failedAPU FAILED TO START. REMOVED AND REPLACED APU STARTER/GEN. AS REQUIRED REF. CE-680A MM.M. 80-10-25. REMOVED AND REPLACED APU ECU IAW CE-680A MM 49-60-05-4. INITIALLY APU STARTER/GEN. PASSED CHECKS. UPON ENG SHUTDOWN APU DID NOT PICK UP LOAD. RESET APU GEN. IT SDR DXTA2019011101906Pressure Sensor · failedFUEL FILTER BYPASS LEFT CAS MESSAGE ILLUMINATED. SUPPLEMENTAL INFORMATION: REMOVED AND REPLACED LT ENGINE FUEL FILTER (PART 30B6653-01) IAW MM 73-10-03. REMOVED LT ENGINE FUEL FILTER AND IMPENDING BYPASS SWITCH FOR INSPECTION IAW MANUAL PART NR 30B7302 REVISIOSDR DXTA2019011001899Brake Sys · contaminatedCAPTAIN MLG BRAKE PEDAL SOFT/SPONGY - WHILE BRAKING ON THE RUNWAY IT FELT AS IF THERE WAS NO MORE BRAKING AVAILABLE WHILE APPLYING BOTH BRAKES. THE RIGHT PEDAL FELT SQUISHY AND HAD MORE PLAY. THE MORE I PRESSED THE BRAKE PEDALS THERE WAS NO MORE PRESSURE. SO SSDR DXTA2019010401864Bypass Switch · faultyCLIMBING THROUGH 500 FEET, THE RIGHT FUEL FILTER BYPASS LIGHT CAME ON. **SUPPLEMENTAL INFORMATION: INSTALLED NEW FUEL FILTER IMPENDING BYPASS SWITCH & REMOVED & INSPECTED FUEL FILTER - NO DEFECTS NOTED. WORK DONE IAW PWC 306D1 73-10-03. OPERATION CHK GOODSDR DXTA2019010301861Unknown · odorCOCKPIT ODOR - DESCENDING THROUGH FL190 WE BEGAN TO SMELL AN EXHAUST ODOR THAT WAS STRONG ENOUGH SO MY SIC WHO WAS FLYING PUT ON HER MASK. I DID NOT WEAR A MASK AND DEVELOPED A SLIGHT HEADACHE FROM THE ODOR. DESCENDING THROUGH 10,000 FT THE SMELL SEEMED TO DISDR DXTR2018123101Line · brokenON CLIMB OUT THROUGH 37000 FEET, THE YELLOW HYDRAULIC PRESS LOW RIGHT EICAS ILLUMINATED SEVERAL TIMES. SHORTLY AFTER THE HYDRAULIC VOLUME LOW EICAS MESSAGE APPEARED. EMERGENCY DECLARED AND AIRCRAFT DIVERTED TO KCMH. MAINTENANCE TECHS FOUND RIGHT ENGINE HYDRAULSDR DXTA2018122701832Hydraulic Line · brokenON CLIMB OUT THROUGH 37000 FEET YELLOW HYD PRESS LOW RIGHT ICAS ILLUMINATED SEVERAL TIMES. SHORTLY AFTER THE HYD VOLUME LOW EICAS MESSAGE APPEARED. APPROPRIATE CHECKLISTS WERE COMPLETED. ***SUPPLEMENTAL INFORMATION: INSTALLED A NEW RT ENGINE HYDRAULIC PUMP PRSDR ZESA2019030500000Hmu · leakingAFTER ENGINE START A LINE SERVICE ATTENDANT NOTICED FUEL COMING FROM THE RIGHT ENGINE COWLING AND LEAKING TO THE GROUND, HE SIGNALED THE PILOTS TO SHUT DOWN. A MECHANIC OPENED THE COWLING, INSPECTED THE ENGINE AND FOUND FUEL TO BE LEAKING FROM THE FUEL CONTROL
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