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.

SDR AALA201706309023Computer · faultyAIRCRAFT WAS NOT GROUNDED. AFTER THROTTLES WERE ADVANCED FOR TAKE OFF A F/CTL ELAC2 FAULT DISPLAYED ON ECAM. TAKE OFF WAS ABORTED AT APPROXIMATELY 10 KNOTS. REMOVED AND REPLACED THE ELAC2 COMPUTER IAW AMM 27-93-34. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.Jun 28, 2017 · N189UW · Airbus A321211SDR O2GA2017062651401Trim System · lack of lubeAIRCRAFT TRIM WOULD NOT MOVE AT ALTITUDE. MAINTENANCE COMPLIED WITH AILERON TRIM LUBRICATION. SYSTEM GROUND OPERATIONAL CHECK WAS GOOD. A SUCCESSFUL OPERATIONAL CHECK FLIGHT WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE.Jun 19, 2017 · N514UP · Cessna 560XLSDR ASMF20170531005Monitor · damagedAIRCRAFT RETURNED TO PLATFORM DUE TO DURING TAKE OFF, CONFIGURATION STABILIZER ALARM WAS ACTIVED. MAINTENANCE PERSONNEL PERFORMED INSPECTION IAW FIM 31-43 TASK 867, CONFIRMING FAILURE IN IOM 003 RH OF INVALID DATA, THEREFORE THE IOM M003 RIGHT WAS REPLACED IAWMay 27, 2017 · N745AM · Boeing 7772Q8SDR AALA20170524009Unknown · unknownTAKEOFF REJECTED AT 144 KNOTS, DUE TO AN UNCOMMANDED YAW. ACCOMPLISHED INSPECTION OF RUDDER, PEDALS, STEERING, BRAKES, LANDING GEAR, WHEELS AND THRUST REVERSER. OPS CHECKED GOOD. THE AIRCRAFT WAS GROUNDED.May 24, 2017 · N966AN · Boeing 737823SDR HNAA2017052300182Flt Controls · malfunctionedAIRCRAFT WOULD NOT ROTATE AT V1, PULLED HARD TWICE AND THE NOSE WOULD NOT COME OFF THE GROUND. AIRSPEED AT REJECT WAS 105 KNOTS. FLIGHT CONTROL CHECK BEFORE AND AFTER EVENT WAS GOOD. CAUSE OF CONDITION UNKNOWN AT THIS TIME. AIRCRAFT IS IN MAINTENANCE.May 22, 2017 · N931HA · Dhav DHC8102SDR AALA201705119022Warning Light · false activationECAM CAUTION BELOW 80 KTS, ABORTED TAKE-OFF. CONDUCTED BITE CHECK, NO FAULTS NOTED. PERFORMED SATISFACTORY AUTOLAND CHECK IAW AMM 22-97-00.May 9, 2017 · N117UW · Airbus A320214SDR AALA201704259033Unknown · unknownDURING TAKE OFF ROLL, THE AIRCRAFT BEGAN PULLING TO THE RIGHT AND WAS NOT CORRECTABLE WITH RUDDER OR STEERING. TAKE OFF ABORTED AT APPROXIMATELY 30 KNOTS. NO ADVERSE INDICATIONS OR WARNINGS WERE OBSERVED ON INSTRUMENTS. CREW REVIEWED EICAS SYSTEM PAGES WITH NOApr 20, 2017 · N813AN · Boeing 7878SDR FDEA201704141200Droop Unit · out of adjustWITH POWER LEVERS EVEN THRUST, ACFT REQUIRED 1.5 DEGREES OR MORE, LEFT RUDDER TRIM. ACFT WANTED TO ROLL RT AT LEFT 1.5 DEG RUDDER TRIM, SLIP INDICATOR SHOWED ACFT REQUIRING MORE LEFT RUDDER TRIM. NO SPOILER FLOAT NOTED. ACFT SEEMS TO WANT TO ROLL TO RIApr 14, 2017 · N733FD · Airbus A300B4605RSDR A6WA201744920Unknown · unknownUNCOMMANDED YAW DURING DECENT THRU 11,000 FT WITH AUTOPILOT ON AND WITH AUTOPILOT OFF ON APPROACH. YD CAUTION, HAD TO ENGAGE YD.Apr 11, 2017 · N412AW · Cndair CL6002B19SDR 2017FA0000143Torque Tube · out of positionDURING INSPECTION OF THE AIRPLANE, AFTER REPAIR, DISCOVER THAT THE BOLT WAS DAMAGED RIGHT CHANNEL TUNNEL AGAIN. AFTER ISSUE ANALYSIS AT THE AIRPLANE, DISCOVER THAT THE TORQUE TUBE HAD AXIAL DISPLACEMENT. WHEN TORQUE TUBE IS IN RIGHT END PIER POSITION THE BMar 24, 2017 · Piper PA34220TSDR RU3A20170322005Control Cable · interferenceLIGHT INTERFERENCE BETWEEN THE EMPENNAGE CONTROL CABLES AND THE LOWER PORTION OF FRAME PASS-THRU.Mar 22, 2017 · N73 · Beech 300BEECHSDR O2GA2017032785801Trim System · frozenPITCH, AILERON, AND RUDDER TRIM FROZEN IN FLIGHT. DESCENDING THROUGH 15,000 FT TEMPERATURE OF +3 DEGREES C, TRIM WORKED FINE. AUTO PILOT RE-ENGAGED AND FLIGHT WAS CONTINUED. MAINTENANCE INSPECTED TRIM SYSTEM NO DEFECTS NOTED. PERFORMED THE REQUIREMENTS OF NTMar 20, 2017 · N858UP · Beech B300SDR VNAA2017031700009Warning Message · false activationELEVATOR SPLIT CAUTION MESSAGE. PERFORMED OPERATIONAL CHECKS AND CABLE TENSION CHECKS, NO DEFECTS NOTED.Mar 17, 2017 · N574NN · Cndair CL6002D24SDR O2GA2017032451501Indicator · out of adjustAFTER TAKE-OFF WITH TRIM INDICATOR IN T.O. POSITION, THE "NO TAKEOFF" WARNING HORN SOUNDED. NOSE DOWN TRIM REQUIRED TO KEEP AIRCRAFT BALANCED. TRIM INDICATOR DID NOT AGREE WITH TRIM POSITION. MAINTENANCE ADJUSTED THE ELEVATOR TRIM INDICATOR. TRAVEL, RIGGING ANMar 12, 2017 · N515UP · Cessna 560XLSDR ANCF2017030201Unknown · malfunctionedDURING APPROACH AFTER SELECTING LG DOWN A/P DISCONNECTED AUTOMATICALLY AND A/C BECOME ON DIRECT LAW WITH NO FAILURE INDICATION WHEN G/AROUND AND WITH LG RETRACTED. A/C BECOME ON NORMAL LOW AGAIN (RA+2) WORKED PROPERLY. DUE FAILURE MSG IN PFR AFS ELAC 2. TROUBLMar 2, 2017 · N862AV · Airbus A320214SDR AALA201702249010Warning Message · activatedAT 120KTS, CONFIGURATION WARNING & M/W. ABORTED TAKEOFF, BELIEVE TRIM WAS INADVERTENTLY ACTIVATED DURING THE TAKEOFF ROLL. THRUST REVERSERS USED. BRAKING NORMAL. MAINTENANCE ACCOMPLISHED SATISFACTORY OPERATIONAL CHECKS IAW AMM 05-51-14 AND AMM 27-41-00. AIRCFeb 23, 2017 · N206UW · Boeing 7572B7SDR CALA2017020300243Computer · faultyNR 2 ENGINE FIRE LIGHTS ON WITHOUT AURAL WARNINGS REPORTED BY CREW. EMERGENCY DECLARED. R & R NR 1 FLIGHT WARNING COMPUTER AND NR 2 FLIGHT WARNING COMPUTER, IAW AMM 31-53-54, OPS NORMAL.Feb 3, 2017 · N417UA · Airbus A320232SDR YENA201701270050Computer · malfunctionedDURING CLIMB, CRUISE AND DESCENT WITH THE AUTOPILOT ON OR OFF, THE AIRCRAFT WAS TURNING LEFT. WITH AUTOPILOT ON L1.4 UNITS OF RUDDER TRIM. UNCOMMANDED JERKS ON RUDDER WITH AUTOPILOT OFF. NO APPARENT FLT CONTROL FAULTS ON FLT CONTROL PAGE OR HYD PAGE. ; PER TSJan 27, 2017 · N638JB · Airbus A320232SDR SWIA201743019Yaw Damper · malfunctionedWITH YAW DAMPERS ENGAGE, THE ACFT YAWED LEFT HARD. YAW DAMPER DISENGAGED, ACFT CONTINUED TO WANDER. REMOVED AND REPLACED LT YAW DAMPER LINEAR ACTUATOR. OPS CHECKED GOOD.Jan 26, 2017 · N426SW · Cndair CL6002B19SDR 2017FA0000007Relay · failedUNDER VFR CONDITIONS ON A VISUAL APPROACH, THE FIRST OFFICER WAS HAND FLYING. AT APPROXIMATELY 1500FT AN AURAL TRIM RUNAWAY WARNING WAS ANNOUNCED FOLLOWED BY A MASTER WARNING PITCH TRIM RUNAWAY THAT WAS ILLUMINATED ON THE CAS SCREEN. THE GEAR WAS DOWN AND Jan 9, 2017 · N817SA · Pilats PC1247ESDR A6WA2016122844678Unknown · malfunctionedUN-COMMANDED YAW ON DECENT. YD CAUTION MESSAGE. RAN QRH MESSAGE CLEARED. YD CAUTION CAME BACK ON, ON APPROACH.Dec 19, 2016 · N450AW · Cndair CL6002B19SDR HALA2016121700551Controller · malfunctionedF/O SIDE STICK FCPC 1 FAULT. REMOVED AND REPLACED FLT CONTROL STICK CONTROLLER IAW AMM 27-92-41 UP TO STEP 4G,Dec 17, 2016 · N396HA · Airbus A330243SDR VNAA2016121500029Mcu · faultySTABILIZER AND MACH TRIM FAIL MESSAGE. REMOVED AND REPLACED MCU.Dec 15, 2016 · N569NN · Cndair CL6002D24SDR VNAA2016121200022Unknown · abnormalAIRCRAFT ROLLED RIGHT UN-COMMANDED, AFTER AUTOPILOT DISCONNECTED. AILERONS OPS CHECKED NORMAL, FLAPS OPS CHECKED NORMAL, GENERAL VISUAL INSPECTION OF FLAPS LEADING EDGES WITH NO DEFECTS NOTED. PERFORMED DETAILED GENERAL VISUAL INSPECTION OF ALL FLIGHT CONTRODec 12, 2016 · N251PS · Cndair CL6002B19SDR A6WA2016120244614Flt Controls · malfunctionedUNCOMMANDED YAW ON DESCENT & APPROACH TO LAND WITH AUTOPILOT ENGAGED & WITH AUTOPILOT OFF.Dec 1, 2016 · N416AW · Cndair CL6002B19SDR UIEA2016112800905Warning Message · false activationREJECTED TAKEOFF. MASTER WARNING CONFIGURATION STAB LOW SPEED. PROBLEM CAUSED BY FLT CONTROL SYS MESSAGE. PERFOMED LCE L AND LCE R GROUND TEST IAW AMM 27-09-01 AND FOUND ALL SATISFACTORY.Nov 25, 2016 · N854GT · Boeing 74787UFSDR 2016FA0000554Bolt · not reported DURING 100 HOUR CHECK OF THE AIRPLANE (G.LANDING GEAR GROUP, POINT 36) WE DISCOVERED THAT BOLT, PN 400-672 (SECTION IX, CONTROL SYSTEM GROUP, FIGURE NR 63, INDEX NUMBER 90) DAMAGED CHANNEL-TUNEL-RIGHT, PN95599-003 (SECTION II, FUSELAGE GROUP, FIGURE NR 12, INNov 4, 2016 · Piper PA34220TSDR VQIA2017081000047Power Supply · malfunctionedDIVERTED DUE TO A FLT CONTROL SEC 3 FAULT. RESET SEC 3 POWER SUPPLY CIRCUIT BREAKER IAW TSM 24-00-00-81-08-18. ACFT OK FOR SERVICE. NO RECENT HISTORY OF SEC 3 PROBLEMS HAS BEEN NOTED ON THIS ACFT.Oct 27, 2016 · N524VA · Airbus A319112SDR QXEA2016101900653Ecu · malfunctionedTAKEOFF WARNING HORN SOUNDED DURING T/O AT ABOUT 50-60 KTS. ABORTED THE TAKEOFF AND CLEARED RUNWAY. CONTACTED DISPATCH & MX CONTROL. PERFORMED THE T/O ABORT CHECKLIST. AFTER CONSULTATION WITH MX CONTROL, WE DECIDED TO ATTEMPT ANOTHER T/O. AIRCRAFT WAS CONOct 15, 2016 · N431QX · Bombdr DHC8402SDR SIMA20161003003Unknown · malfunctionedON APPROACH CREW EXPERIENCED UNCOMMANDED ROLL OF AIRCRAFT. CREW DISCONNECTED THE AUTOPILOT AND RATE OF ROLLING DECREASED. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. PERFORMED AILERON RIGGING CHECK AND AILERON OPS CHECKED IAW AMM 27-11-00 ALSO COct 3, 2016 · N522AE · Cndair CL6002C10SDR 5TTY201609260001Transducer · failedDURING FLIGHT, THE AIRCRAFT GENERATED THE FLT CONTROL ELAC 2 FAULT MESSAGE AND DUE TO DEFERRED ELAC 1, THE AIRCRAFT WAS DIVERTED. AFTER AN UNEVENTFULLY LANDING, MAINTENANCE REPLACED THE CAPTAIN`S TRANSDUCER UNIT 4CE1 ON CAPTAIN SIDE STICK IAW TSM 27-93-00-810Sep 26, 2016 · N498TA · Airbus A320233SDR ASOA20160912049CComputer · malfunctionedTHE CREW REPORTED THE AIRCRAFT GOES INTO A ROLL AND GA MODE DURING TAKOFF AND ON APPROACH AND UNABLE TO SWITCH OUT OF IT. MAINTENANCE INSPECTED AND REPLACED THE NR 2 IC600 COMPUTER. OPS CHECKED GOOD.Sep 12, 2016 · N14180 · Emb EMB145XRSDR 2016F00183Relay · faultyALL POWER UP AND PREFLIGHT CHECKS WERE NORMAL AND THE AIRCRAFT WAS POWERED WITH A GPU PRIOR TO ENGINE START. THE CAPTAIN WAS HAND FLYING AND WAS LEVELING OFF AT 12,000FT WHEN A "MASTER WARNING" ILLUMINATED AND A AURAL WARNING OF "TRIM RUNAWAY" SOUNDED. THE PSep 3, 2016 · N816SA · Pilats PC1247ESDR GLBA2016090700610Control Cable · wornPILOT REPORTED THAT THE ELEVATOR AND AILERON CONTROLS DO NOT MOVE SMOOTHLY. MAINTENANCE R & R FWD CAPTAIN`S SIDE ELEVATOR CONTROL CABLE IAW MM 27-00-01 6, PN:120-27655-013. OPS CHECK GOOD.Sep 3, 2016 · N293UX · Emb EMB120ERSDR UIEA2016083100726Ring Gear · corrodedNRI 3295, NR 3 ROTARY ACTUATOR ASSY FIXED RING GEAR CORRODED. NR 3 REACTION RING SPLINES ARE CORRODED, NRI 3296 & NRI 3295. REMOVED AND INSTALLED NR 3 ROTARY ACTUATOR IAW AMM 27-51-11 UP TO STEP 3F, NRI 3296. R & R NR 3 REACTION RING IAW EO 6727A007.Aug 28, 2016 · N653GT · Boeing 767231SDR UIEA2016083100727Ring Gear · corrodedNR 5 ROTARY ACTUATOR HAS CORROSION ON FIXED RING GEAR, NRI 3334. NR 5 REACTION RING HAS CORROSION ON SPLINES, NRI 3333. R & R NR 5 ROTARY ACTUATOR UP TO STEP 3F IAW EO 6727A007 PT1, NRI 3334. R & R NR 5 REACTION RING IAW EO 6717A007.Aug 28, 2016 · N653GT · Boeing 767231SDR VNAA2016081700017Control Quadrant · bindingAUTO PILOT, RT WING DOWN CAUTION MESSAGE IN FLIGHT. THE CREW CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. THE ACFT WAS FERRIED TO A REPAIR FACILITY. MAINTENANCE TROUBLESHOT, R & R THE RT FEEL UNIT QUADRANT AND PERFORMED CHECKS IAW THE AMM. THE ACFTAug 17, 2016 · N509AE · Cndair CL6002C10SDR SWAA2016081854897Memory Device · smokeDURING CLIMB, SMOKE OBSERVED COMING FROM FIRST OFFICERS CONTROL WHEEL MEMORY DEVICE. R & R FIRST OFFICERS CONTROL WHEEL MEMORY DEVICE IAW MM.Aug 17, 2016 · N290WN · Boeing 7377H4SDR DALA2016080505783Actuator · failedCREW REPORTED FLT/CTL ELAC 2 PITCH FAULT FOLLOWED BY AN UN-COMMANDED PITCH TRIM IN CRUISE 30 MINUTES AFTER TAKE-OFF. +/- 0.4 DEGREES OF STAB TRIM MOVEMENT. AUTO-PILOT AUTO-DISENGAGED. FLIGHT CONTROL ALTERNATE LAW ON APPROACH WITH F/CTL ELAC1 PITCH FAULT. BAAug 3, 2016 · N338NW · Airbus A320212SDR UIEA2016080100662Actuator · corrodedNR 2 ROTARY ACTUATOR AND REACTION RING HAS CORROSION. REMOVED AND REPLACED THE NR 2 ROTARY ACTUATOR AND REACTION RING IAW AMM 27-51-22 AND SB 767-27A0229.Aug 1, 2016 · N651GT · Boeing 767231SDR UIEA2016080100661Actuator · corrodedNR 7 ROTARY ACTUATOR AND REACTION RING IS CORRODED. REMOVED AND REPLACED THE ROTARY ACTUATOR AND REACTION RING IAW AMM 27-51-22 AND SB 767-27A0229 FIG 2.Aug 1, 2016 · N651GT · Boeing 767231SDR FDEA201608012701Actuator · malfunctionedACFT REQUIRES RVSM DUE TO ALTITUDE DEVIATIONS. IAW TSI 22-20/7202 PITCH ACTUATOR R & R AS PROBLEM STARTED AFTER ACTUATOR WAS CHANGED. REMOVED AND REPLACED THE PITCH ACTUATOR IAW WRI 22-10/7209.Aug 1, 2016 · N746FD · Airbus A300B4622RSDR IPXA2016072706377Computer · malfunctionedATB - RUDDER RATION EICAS AT 400' ILLUMINATED THROUGHOUT FLIGHT. AILERON LOCKOUT EICAS AT 400' ILLUMINATED THROUGHOUT FLIGHT. R & R C FCC IAW MM 22-11-1. OPS NORMAL. R & R L ADC IAW MM 34-12-01. OPS NORMAL.Jul 22, 2016 · N306UP · Boeing 76734AFSDR 2016FA0000426Circuit Breaker · trippedPITCH TRIM CIRCUIT BREAKER TRIPPED, AUTOPILOT FAIL CAWS ILLUMINATED.Jul 15, 2016 · N828SA · Pilats PC1247ESDR YTRA2016062417601Control Tube · debondedCONTROL TUBE IS DEBONDED FROM CLEVIS.Jun 24, 2016 · N410RL · Bell 206L4SDR AALA20160621017Unknown · vibrationAIRCRAFT WAS GROUNDED. AIR INTERRUPT, EMERGENCY DECLARED, LANDING UNEVENTFUL, ACFT OVERWEIGHT. DURING CLIMB, CONTROL WHEEL VIBRATION WAS ENCOUNTERED. VIBRATION INCREASED AS GEAR AND FLAPS WERE RETRACTED AND SPEED INCREASED THEN DECREASED AS ACFT WAS CONFIGUJun 21, 2016 · N794AN · Boeing 777223SDR HALA2016061400237Unknown · unknownRTO-AT 100KTS, ACFT PULLED HARD TO RT. FULL LT RUDDER NOT ENOUGH TO MAINTAIN CENTER LINE. NO ECAM. NO FAULTS, INSPECTION AFTER BRAKE EMERGENCY IAW AMM05-51-16-200-801-A CHECKED GOOD. ALL MLG & NLG TIRE ROTATION CHECKED GOOD & VISUAL INSPECTION CHECKED GOODJun 14, 2016 · N388HA · Airbus A330243SDR AALA20160614001Warning System · false activationAIRCRAFT WAS GROUNDED. EMERGENCY DECLARED. LANDING UNEVENTFUL. ACFT NOT OVERWEIGHT. DURING CRUISE THE FLIGHT, CONTROL B LOW PRESSURE LIGHT ILLUMINATED. ACCOMPLISHED QRH CHECK LIST. SYSTEM A, HYDRAULIC PRESSURE AND QUANTITY SHOWING NORMAL. MAINTENANCE ACCOJun 13, 2016 · N943AN · Boeing 737823SDR 3FFA2016060800001Relay · failedTROUBLESHOT AND FOUND FLAP MOTOR RELAY FAILED CLOSED WHERE IT WAS CONTINUOUSLY MAINTAINING POWER TO THE FLAP MOTOR. AFTER APPROXIMATELY 2.3 HOUR, PART 91 FLIGHT PILOT AND DOM STARTED ENGINE FOR RETURN FLIGHT HOME. APPROXIMATELY 45 SECONDS LATER THE CABIN STAJun 8, 2016 · N200TK · Beech B200SDR DALA2016052404284Jackscrew · crackedFOUND 2 CRACKS AT JACKSCREW WEB JUST BELOW GIMBAL NUT. COMPLY WITH PRI/ERA 547114-14.May 23, 2016 · N956DN · Doug MD9030
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