JASC 2700
Service difficulty reports · 1,745
Reports filed under 2700 · Flight Control System, 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 jasc_code = '2700' 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 jasc_code = '2700' 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 GTIA020360Control Quadrant · corrodedFTW - FOUND RUDDER AND ELEVATOR CABLE QUADRANT AFT OF PRESSURE BULKHEAD STATION 1338 -X30 CABLE KEEPER AND QUADRANT CORRODED AND BLUEWATER STAINED. REPLACED CABLE KEEPER PINS ON RUDDER AND ELEVATOR CABLE QUADRANT. (M)SDR GTIA020257Switch · inoperativeDTW - FLT 56 - PRIMARY TRIM ON F/O SIDES STOP WORKING ON APPROACH INTO DTW HANDLES WERE USED AFTER LANDING, LEFT AND RIGHT ELECTRIC TRIM SWITCH AND HANDLES MANUAL TRIM INOPERATIVE. REMOVED AND REPLACED PRIMARY TRIM MOTOR. OPS CHECK GOOD IAW MD80 MM 27-40-01.SDR AUS20020328Control Cable · worn(AUS) ALL AILERON SYSTEM CABLES AND FLAP CABLES (4OFF) HAD BROKEN STRANDS OR WERE WORN EXCESSIVELY.SDR VNAA0203042Damper · failedTHIS IS AN AMENDMENT TO VNAA0203038. MAINTENANCE INSPECTED AND REPLACED THE RUDDER DAMPER AND LIMIT ACTUATOR IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 27-00-00. A FUNCTIONAL CHECK FLIGHT WAS PERFORMED AND THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.SDR SPAA0200051Panel · delaminated#5 SPOILER PANEL HAS AREAS OF DELAMINATION NOTED ON PREFLIGHT MAINTENANCE CHECK.SDR 2002FA0000311Cotter Pin · brokenDURING ROUTINE CABIN INSPECTION THE COTTER PIN THAT CONNECTS THE PILOT RT PEDAL AND THE TOE BRAKE CLEVIS TO THE BRAKE MASTER CYLINDER WAS FOUND MISSING AT THE TOP OF THE ASSEMBLY. UPON FURTHER INSPECTION THE WASHER WAS ALSO MISSING AND THE PIN WAS BACKING OUTSDR P5CA0200655Plug · missingPDU NR 4 DRAIN PLUG MISSING. INSTALLED PLUG AND FILLED PDU IAW 12-13-12. PDU RAN OK.SDR 2002FA0000286Control Cable · wornDURING A ROUTINE INSPECTION THE RT AND LT FORWARD STABILATOR CABLE WERE FOUND WORN AND FRAYED. THE AILERON RIGHT AND LEFT BALANCE CABLES WERE ALSO FOUND IN A SIMILAR CONDITION. THE WORN AND FRAYED PARTS OF THE CABLES WERE FOUND AT PULLEYS FAIRLEADS OR ANY PLSDR 2002FA0000285Control Cable · wornDURING A ROUTINE INSPECTION THE RT AND LT FORWARD STABILATOR CABLES WERE FOUND WORN AND FRAYED. THE AILERON RIGHT AND LEFT BALANCE CABLES WERE ALSO FOUND IN A SIMILAR CONDITION. THE WORN AND FRAYED PARTS OF THE CABLES WERE FOUND AT PULLEYS FAIRLEADS OR ANY PSDR 2002FA0000289Control Cable · wornDURING A ROUTINE INSPECTION THE RIGHT AND LEFT FORWARD STABILATOR CABLE WERE FOUND WORN FRAYED. THE AILERON RIGHT AND LEFT BALANCE CABLES WERE ALSO FOUND IN A SIMILAR CONDITION. THE WORN ANDFRAYED PARTS OF THE CABLES WERE FOUND AT PULLEYS FAIRLEADS OR ANY PLSDR 2002FA0000275Control Cable · wornDURING A ROUTINE INSPECTION THE RIGHT AND LEFT FORWARD STABILATOR CABLE WERE FOUND WORN AND FRAYED. THE AILERON RIGHT AND LEFT BALANCE CABLES WERE ALSO FOUND IN A SIMULAR CONDITION. THE WORN AND FRAYED PARTS OF THE CABLES WERE FOUND AT PULLEYS, FAIRLEADS OR SDR 2002FA0000274Control Cable · wornDURING A ROUTNE INSPECTION THE RIGHT AND LEFT FORWARD STABILATOR CABLE WERE FOUND WORN AND FRAYED. THE AILERON RIGHT AND LEFT BALANCE CABLES WERE ALSO FOUND IN A SIMILAR CONDITION. THE WORN AND FRAYED PARTS OF THE CABLES WERE FOUND AT PULLEYS, FAIR LEADS OR SDR 2002FA0000273Control Cable · wornDURING A ROUTINE INSPECTION THE RIGHT AND LEFT FORWARD STABILATOR CABLE WERE FOUND WORN AND FRAYED. THE AILERON RIGHT AND LEFT BALANCE CABLES WERE ALSO FOUND IN A SIMILAR CONDITION. THE WORN AND FRAYED PARTS OF THE CABLES WERE FOUND AT PULLEYS, FAIR LEADS OSDR UC22002F00003Control Cable · frayedFOUND THE RIGHT AND LEFT FORWARD STABILATOR CONTROL CABLES FRAYED AND WORN DURING A 100 HOUR INSPECTION.SDR UC22002F00002Control Cable · frayedFOUND THE RIGHT AND LEFT FORWARD STABILATOR CONTROL CABLES FRAYED AND WORN DURING A 100 HOUR INSPECTION.SDR UC22002F00001Control Cable · wornFOUND RIGHT AND LEFT FORWARD STABILATOR CONTROL CABLES FRAYED AND WORN DURING A 100 HOUR INSPECTION. .SDR UC22002F00000Control Cable · frayedFOUND RIGHT AND LEFT FORWARD STABILATOR CONTROL CABLES FRAYED AND WORN DURING A 100 HOUR INSPECTION.SDR 2002FA0000224Control Cable · frayedFOUND THE RT AND LT FORWARD STABILATOR CONTROL CABLES FRAYED AND WORN DURING A 100 HOUR INSPECTION.SDR MEX2002024Valve · leakingFLT 913 - MTY-MEX - AIRCRAFT ARRIVED TO PLATFORM WITH HYDRAULIC FLUID LEAK IN THE LEFT WING. IT WAS CHECKED AND THE LEAK WAS FOUND AT SPOILER PCA NR 3 LEFT SIDE, EHSV BODY. CANCELLED THE PRESSURE AND RETURN PORTS AND DISCONNECTED THE ELECTRIC CONNECTOR OF THSDR HEEA077729Actuator · failedACTUATOR WILL NOT ALLOW AARS PITCH CHANNEL TO COME ON LINE.SDR CA020117016Control Unit · malfunctioned(CAN) AIRCRAFT RETURNED BACK TO GATE AFTER PUSH BACK. NO ECAM INDICATION OF RUDDER TRIM AND NO PEDESTAL INDICATION. TROUBLESHOOTING WAS CARRIED OUT PER CATTS ,SDR DHL2002805027Angle · crackedN/R 0146RHT WING INTERNAL SLOT ANGLE HAS A 3" CRACK @ XFS 257.50SDR IXXA0100077OCable · brokenENROUTE FROM ANC TO SEA, AFTER TAKEOFF THE FLIGHT CREW NOTICED A SIGNIFICANT AIRCRAFT ROLL TO THE LEFT AND REQIURED RUDDUR INPUT. THE FLIGHT RETURNED TO ANC FOR AN UNVENTFUL LANDING. MANITHEANCE INSPECTED THE AIRCRAFT WHICH REVEALED A SEGMENT OF THE LEFT WING SDR VNAA0111013Aileron · jammedAILERONS MOMENTARILY JAMMED IN FLIGHT. JERKED FREE AND CONTROLS REMAINED STIFF. FLIGHT 4064 RETURNEDTO PIT. MAINTENANCE VISUALLY INSPECTED AILERON CONTROL CABLES AND PULLEYS IN ACCORDANCE WITH DORNIER MAINTENANCE JIC 27-11-03. NO DEFECTS NOTED. PERFORMEDSDR RAIA00110009Vane · failed7071-STL-RIGHT STALL CAPTION LIGHT CAME ON DURING TAXI. MAINTENANCE REMOVED AND REPLACED STALL VANE.SDR 2001UALA02153Computer · faultyELEVATOR AILERON COMPUTER (ELAC) NR 1 FAILURE MESSAGE DISPLAYED ON UPPER ELECTRONIC CENTRALIZED AIRCRAFT MONITORING. RESET OF THE ELAC CAUSED ELECTRICAL ODOR IN FLIGHT DECK. THE ELAC1 WAS REPLACED AND OPERATIONAL CHECK WAS GOOD. SHOP FINDINGS REVEALED INTERNSDR RAIA00110007Vane · inoperative7214-STL-RIGHT STALL CAPTION ILLUMINATED DURING TAXI. MAINTENANCE REMOVED AND REPLACED THE RIGHT STALL VANE.SDR P5CA0100593Link · brokenR.H. O/B FORE FLAP, MOST O/B SUPPORT LINK BROKEN. REMOVED & REPLACED LINK ASSY. OPS CHECK O.K.SDR 2001UALA02071SealUNSCHEDULED LANDING DUE TO A LOOSE #2 FLAP SEAL. SUPPLEMENTAL DATA UPDATE REMOVED AND REPLACED THE #2 LEADING EDGE FLAP AERODYNAMIC SEAL.SDR HEEA075977Actuator · stuckSTICKING INTERMITTENTLY IN FLIGHT.SDR GTIA010865JackscrewDTW - FOUND JACKSCREW FAILED PHASE 2 INPSECTION, REF W/C 00115 END PLAY AT .1875 INCH. REMOVED AND REPLACED JACKSCREW IAW MD80 MM 27-40-01. OPS CHECK GOOD END PLAY .003 FREE PLAY .006. (M)SDR AALA20011663Skin · corrodedTUL - FOUND CORROSION UPPER RIGHT HORIZONTAL STAB SKIN T/E BEAM 4 HINGE IN FROM STAB TIP AT ABOUT STAB STATION 115. REPAIRED CORROSION AREA AS PER ESO 11697 DATED 8-16-2001. (M)SDR 2001UALA01723Bearing · seizedRUDDER PEDALS EXTREMELY STIFF DURING APPROACH AND LANDING AFTER FIVE AND A HALF HOUR FLIGHT. SUPPLEMENTAL DATA UPDATE CAUSE: A SEIZED CAM BEARING IN THE RUDDER FEEL AND CENTERING MECHANISM CAUSED THE HEAVY FORCE CONDITION IN THE RUDDER PEDALS.CORR ECTION: SUSDR 2001UALA01720Transmission · failedLANDED UNDER AMBER ALERT DUE TO STUCK TE FLAPS. SUPPLEMENTAL DATA UPDATE REPLACED THE #4 TRAILING EDGE FLAP TRANSMISSION.SDR SIMA200123421Carriage · corrodedSBP - DURING MBV INSPECTION MAINTENANCE, FOUND THE LEFT RUDDER PEDAL CONSOLE CARRIAGE CORRODED. MAINTENANCE REMOVED AND REPLACED THE LEFT CARRIAGE IAW SAAB MM. AIRCRAFT WAS THEN RETURNED TO SERVICE. (M)SDR QXEA0101342Control Unit · malfunctionedGEG - VIBRATION LEFT SIDE OF FUSELAGE. PITCH TRIM FAIL. REMOVED AND REPLACED FLIGHT CONTROL ELECTRONIC CONTROL UNIT. OPERATIONAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE.SDR MASA01084Spoiler · brokenRIGHT FLIGHT SPOILER DEPLOY IN FLIGHT. THE CREW WAS ABLE TO OVERCOME THE ACTION OF THE SPOILER AND CONTROL THE AIRCRAFT IN FLIGHT. THE SPOILER WOULD NOT RETRACT AND WHEN THE AIRCRAFT ARRIVED AT THE GATE THE SPOILER WAS STILL FULLLY DEPLOYED AND THE ATTACHMENSDR USAASB01221SensorPIT - FLT 283 - EN ROUTE FROM PHL-PIT, AT FL200 AND 300 KNOTS, THE CAPTAIN REPORTED THE NR 3 AND NR 4 LEADING EDGE DEVICES HAD DEPLOYED IN FLIGHT WITH FLAP HANDLE IN UP POSITION. THIS CAUSED A SLIGHT ROLL IN THE AIRCRAFT. CREW DECLARED AN EMERGENCY AND SLOWESDR AALA20011526Transmitter · inoperativeMIA - FLT 922 - EN ROUTE MIA-LPB, STABILIZER TRIM EICAS MESSAGE AND STABILIZER TRIM CAUTION LIGHT ILLUMINATED. RETURNED TO MIA LANDING WITHOUT INCIDENT. REPLACED RIGH STABILIZER TRIM MODULE TRANSMITTER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)SDR GAIA01286OPIndicator · inoperativeFLT 302 - GEG-SEA - ON DEPARTURE, INBOARD FLAPS FAILED TO RETRACT FROM TAKEOFF SETTING. AIRCRAFT MADE AN UNEVENTFUL RETURN LANDING AT GEG. FOUND INBOARD FLAP POSITION INDICATOR INOPERATIVE. REMOVED AND REPLACED INBOARD FLAP POSITION INDICATOR. OPS CHECK OFSDR HNAA0100040Valve · leakingIN FLIGHT #2 HYDRAULIC SYSTEM QUANTITY DROPPED TO 1 QUART. AIRCRAFT DIVERTED TO ISP. FOUND #2 FLIGHT SPOILER UNLOADING VALVE LEAKING. REPLACED VALVE.SDR USAASB01209Indicator · failedCLT - FLT 1528 - IN PREPARATION FOR LANDING AT CLT, FROM MIA, THE TRAILING EDGE FLAPS FAILED TO EXTEND WHEN SELECTED. THE LEADING EDGE DEVICES DID DEPLOY TO FULL EXTEND. THE FLAP POSITION INDICATOR SHOWED A SMALL SPLIT AT ONE UNIT AND THE TRAILING EDGE CIRCUSDR AUS20011057Cable · corroded(AUS) SEVERAL FLIGHT CONTROL CABLES RUSTY. THE FOLLOWING CABLES WEREFOUND TO BE UNSERVICEABLE:- 1. PNO 0400107-41 AILERON CABLE (2OFF)2. PNO 0400107-21 BALANCE CABLE 3. PNO 0400107-45 FLAP CABLE4. PNO 0400107-46 FLAP CABLES 5. PNO 0400107-30 TRIM CABLE6. PNO 0SDR USAASB01187Transmitter · faultyCLT - FLT 1157 - IN PREPARATION FOR LANDING AT CLT, FROM ORD, CREW REPORTED A SPLIT FLAP INDICATION AS FLAPS WERE STUCK AT 7 DEGREES. FLIGHT LANDED WITHOUT FURTHER INCIDENT WITH NO EMERGENCY BEING DECLARED. MAINTENANCE REMOVED AND REPLACED THE RIGHT FLAP POSSDR ABXA010366Pin · corrodedAFT HORIZONTAL STABILIZER PIN HAD CORROSION ON END AND TAB. REPLACED PINS IAW DC-9 MM 27-40-01.SDR ABXA010365Pin · corrodedFORWARD HORIZONTAL STABILIZER PIN WAS CORRODED ON END AND TAB. REPLACED PIN IAW DC-9 MM 27-40-01.SDR SIMA200116703Switch · inoperativeJAX - FLT 5248 - CREW REPORTED THE AILERON TRIM TO BE INOPERATIVE AT AN UNLEVEL POSITION. CAPTAIN NOTED IT TOOK ABOUT THIRTY POUNDS OF PRESSURE TO MAINTAIN LEVEL FLIGTH. MAINTENANCE REMOVED AND REPLACED THE TRIM CONTROL PANEL IAW ATR MM. OPS CHECK WAS GOOD SDR REXA01008Bpsu · failedFLAP FAILURE MESSAGE AND FLAPS STUCK AT 20 DEGREES. INTERROGATED FECU (FLAP ELECTRONIC CONTROL UNIT) FOUND LEFT BPSU (BRAKE POSITION SENSING UNIT) FAILURE MESSAGE. REMOVED AND REPLACED LEFT FLAP BPSU. (M)SDR 01FDEA00475Bushing · missingDURING REMOVAL OF RT WING ASA ACTUATOR FOUND THEY WERE RUBBING INTO THE WING STRUCTURE AT 3 POS. REMOVED AND REPLACED ACTUATOR RODEND BEARINGS AND BUSHING.SDR JBXA000290Warning System · malfunctionedABORTED TAKEOFF DUE CONFIG AILERON, CONFIG SPOILERS, CONFIG TRIM RED MSG. PERFORMED OPERATIONAL CHECK OF PSEU AND MDC IAW 32-61-00. NO FAULTS FOUND AT THIS TIME.
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