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 CA190314019Mau · inoperative(CAN) MODULAR ACQUISITION UNIT (MAU), FAILED AND CAUSED THE FLAP ASSYMETRY INDICATION TO COME ON IN THE COCKPIT, THE CREW REACTED BY RETURNING TO THE AIRPORT. THE AIRCRAFT AT 14000 FT IN A CLIMB. THE TROUBLESHOOTING THAT FOLLOWED RESULTED IN DETERMINING THAT Feb 14, 2019 · Boeing 737200SDR 2019FA0000147Control Cable · crackedFLIGHT CONTROL CABLE FOUND CRACKED DURING ANNUAL INSPECTION. AD 2013-02-13/PIPER SB 1245A PREVIOUSLY COMPLIED WITH. 2000 HOUR 7 YEAR INSPECTION NOT DUE AT THE TIME THE CRACK WAS FOUND. CRACK BECAME EVIDENT WHEN A SLIGHT BENDING LOAD WAS PLACED ON THE CONTROL Feb 1, 2019 · N428M · Piper PA28181SDR ANCF20190214701Computer · abnormalAFTER TAKEOFF CLIMB AND APPROACH AIRCRAFT ON MANUAL FLIGHT KEPT TRIMING BACK NOSE KEPT GOING UP, MANUAL CORRECTIONS HAS TO BE DONE CONSTANTLY // CORRECTIVE ACTION: JAN 28. IN ACCORDANCE WITH AMM 27-96-00-710-02A OPERATIONAL TEST OF THE THS ACTUATOR ELECTRICAL Jan 27, 2019 · N595EL · Airbus A318112SDR AALA201901289049Warning Horn · activatedABORTED TAKEOFF AT INITIAL POWER UP ABOUT 20KTS ON TAKEOFF ROLL. CREW RECEIVED A TAKEOFF AURAL WARNING CONFIGURATION HORN AND LIGHT. RETURNED TO THE GATE. MAINTENANCE EVALUATED, PERFORMED A CHECK OF TAKE OF CONFIGURATION IAW AMM 31-51-00, AIRCRAFT WAS CLEARED Jan 26, 2019 · N955AN · Boeing 737823SDR VNAA2019011511102Control Unit · unknownSUPPLEMENTAL INFORMATION: MX C/W FUNCTIONAL CHECK OF HSTCU IAW CRJ200 AMM. FUNCTIONAL CHECK GOOD. OPS CHECK GOOD. OCF CHECK GOOD.Jan 15, 2019 · N218PS · Cndair CL6002B19SDR AALA2019010228002Switch · faultedTAKE OFF CONFIGURATION LIGHT ILLUMINATED AFTER THE POWER WAS ADVANCED TO TAKEOFF POWER. REJECTED TAKEOFF, THE AIRCRAFT WAS CONFIGURED PROPERLY. TRIM IN GREEN TAKEOFF BAN, FLAPS AT 01 DEGREES. BRAKES OFF, SPEED BRAKE LEVER STOWED, AT ARM. THE AIRCRAFT WAS Dec 27, 2018 · N907AN · Boeing 737823SDR P5CA2018120700371Warning Message · false activationLOW SPEED ABORTED TAKEOFF (30KTS) IN NRT DUE TO CONFIG WARNING. CAPT REPORTED STAB TRIM WAS ON THE EDGE OF GREEN BAND. SLIGHT ADJUSTMENT MADE TO STAB TRIM AND DEPARTED. REPORTED UPON ARRIVAL TO NGO.(<P>NGO MAINTENANCE PERFORMED TEST OF STAB INDICATION SYSTDec 7, 2018 · N498MC · Boeing 74747UFSDR HALA2018111900593Indicator · detachedF/CTL FLAPS FAULT ECAM RAN ECAM PERFORMED EMERG LANDING. PER FLT CREW. // T/S PER A330 TSM 27-50-00-810-816A. FOUND OVER TORQUE INDICATOR RELEASED ON INPUT GEARBOX 5 LH (5053CV). REQUIRES DRAIN AND FILL ROTARY ACTUATOR (5055CV) AND INPUT GEARBOX (5053CV). Nov 18, 2018 · N379HA · Airbus A330243SDR HNAA2018110800277None · nonePDIS 644 05-50 1925362 06NOV18 SYR CLOSE FLAP OVERSPEED NOTED 45 DEG A7 157 KTS 28482 00 RNR FACT 06NOV18 14:22 SYR FLAP OVERSPEED NOTED AND WITH-IN LIMITS OF AMM 05-50 Nov 6, 2018 · N644AE · Emb EMB145LRSDR CALA2018110502311Actuator · no test(A3NB-27-4-6031) REMOVE AND REPLACE THE THSA. REFER TO AAR N/R: 9611965. CHANGED DUE TO A FAILED JAMMING TEST AND A LEAK. REMOVED & REPLACED THSA IAW A319 AMM 27-44-51-000-001 & AMM 27-4 4-51-400-001. PERFORMED THSA ELECTRICAL CONTROL OPS TEST IAW A31 9 AMM 27Nov 5, 2018 · N804UA · Airbus A319131SDR FDEA201811013079Computer · failedCLIMBING THROUGH FL200, RECEIVED A LEVEL 2 STAB OUT OF TRIM WARNING. SWITCHED AUTOPILOT IAW QRH. AUTOPILOT 2 WOULD DISCONNECT BECUASE OF STAB TRIM INOPERATIVE. AUTOPILOT 1 CONTINUED TO DISPLAY STAB OUT OF TRIM. INTERROGATED BOTH FCCS. NR 1 FCC HAS NO FNov 1, 2018 · N590FE · Doug MD11FSDR GTIA2018110202932Adiru · malfunctionedCAPTAIN & FIRST OFFICER FMA AND AIRSPEED INDICATIONS DISAPPEARED AT 100 KTS DURING TAKEOFF AND APPEARED. AFTER LIFTOFF, FDS & AUTOTHRUST STOPPED FUNTIONING AND AIRCRAFT REVERTED TO ALTERNATE LAW. ECAM NAV STDBY AOA FAULT APPREARED ON ENG SHUTDOWN. R & R ADIROct 23, 2018 · N530NK · Airbus A319132SDR VNAA2018090311101Unknown · malfunctionedDURING CLIMBOUT, CAPTAIN NOTICED THAT THE FLIGHT CONTROLS WERE ACTING SLUGGISH REQUIRING 3 TO 4 TIMES THE AMOUNT OF FORCE NEEDED TO MAKE THE AIRCRAFT TURN. DID NOT FOLLOW THE QRH AND THE STATION DECLARED AN EMERGENCY. THE AIRCRAFT LANDED WITHOUT INCIDENT. Sep 3, 2018 · N546FF · Cndair CL6002C10SDR F3LA2018082800411Unknown · unknownPILOT REPORTED AN UNCOMMANDED LATERAL YAW TO THE RIGHT AFTER TAKEOFF ROLL, SPEED OF 10 KTS. MAINTENANCE COMPLETED TROUBLESHOOTING IAW TSM 05-50-00-810-823-A. BOTH NLG TIRES DAMAGED AND REPLACED IAW AMM 32-41-12 PB 401. NR 1 MLG TIRE DAMAGED, REPLACED THE NAug 23, 2018 · N228FR · Airbus A320214SDR CALA2018081701799Not Reported · lack of lubeAIRCRAFT DIFFICULT TO CONTROL IN THE ROLL AXIS. FELT LIKE MANUAL REVISION. HYD NORMAL, AP OF OIL SERVICE ACCOMPLISHED. PREFORMED FIM 27-11-00-810-804, AND AMM 27-11-810-804, LUBRICATED ALL POINTS FROM THE FLIGHT DECK TO THE WHEEL WELL. FOUND NO BINDING OK FAug 11, 2018 · N12225 · Boeing 737824SDR ASMF20180821007Module · failedAFTER LANDING, DURING FLAPS RETRACTION, THE SLAT DRIVE NON NORMAL CONDITION OCCURRED. MAINTENANCE PERFORMED FAULT ISOLATION PROCEDURE IAW AMM DMC-B787-A-27-81-00-00B-320A-A, TESTED CORRECT. ADDITIONALLY FLIGHT CONTROL MODULE WAS REPLACED IAW DMC-B787-A-27-02Jun 26, 2018 · N964AM · Boeing 7878SDR ASOA201805257093Control Unit · failedDURING CLIMB OUT, WHILE ACTIVATING MAIN PITCH TRIM SWITCH, ICAS WENT TO INOPERATIVE, THE MASTER WARNING WENT TO INOPERATIVE, THE MESSAGE REMAINED AFTER THE TRIM SWITCH WAS RELEASED.. MESSAGE ALSO REMAIN WAS RELEASED. ACFT RETURNED TO BASE AND MAINTENANCE RMay 25, 2018 · N11535 · Emb EMB145LRSDR N6WA201804302901Actuator · malfunctionedUNCOMMANDED YAW MOVEMENT. R & R THE YAW DAMPER ACTUATOR IAW AMM 22-22-01, OPS CHECKED GOOD.Apr 29, 2018 · N154GJ · Cndair CL6002C10SDR SIMA201804254002Unknown · malfunctionedDURING CLIMB OUT AT 20,000FT, 290 KNOTS, AN UNCOMMANDED ROLL TO THE LEFT, THEN RIGHT, 20 DEGREES WITH SHUDDER & VIBRATION. HAPPENED AGAIN 5 MINUTES LATER. TURNED AUTOPILOT OFF AND CONTINUED FOR ANOTHER 10 SECS. DIVERTED BACK TO DEPARTURE WITH NO FUTHER ISSApr 24, 2018 · N228NN · Emb ERJ170200LRSDR QMLA201804248046Flt Controls · abnormalSHORTLY AFTER LIFT-OFF, EXPERIENCED AN UNCOMMANDED LEFT & RIGHT ROLLS AT 15-20 DEGREES. HAD NO CAUTION OR SAS LIGHT INDICATIONS. RETURNED IMMEDIATELY TO BASE AND NOTIFIED MAINTENANCE. INSPECTED, CLEANED, AND APPLIED STABILANT 22 TO BOTH ELECTRICAL CONNECTORApr 22, 2018 · N93LF · Urocop EC135T2SDR A6WA2018040645752Unknown · unknownDURING DESCENT, AN UNCOMMANDED YAW AND ROLL OCCURED AT 16000 FT. RAN QRH FOR THE UNCOMMANDED YAW MOTION AND DISCONNECTED YAW DAMPERS. YAW CONTINUED ALL THE WAY TO TOUCH DOWN. INTERMITTENT LEFT AND RIGHT DUTCH ROLL.Apr 5, 2018 · N453AW · Cndair CL6002B19SDR GTIA2018032802547Computer · malfunctionedAFTER ENGINE START, FLT CNTRL FAULT SEC 3, RESET IAW ECAM THEN SMELLED BURNING ELECTRICAL COMPONENTS SPOILER ELEVATOR COMPUTERS (SEC) SEC 3. OPERATED COCKPIT LIGHTING AND CHECKED E&E, MX COULD NOT DUPLICATE THE ODOR IAW AMM 05-21-20. R & R THE SEC 3 COMar 28, 2018 · N603NK · Airbus A320232SDR VNAA2018032311101Flt Controls · unknownTHE AIRCRAFT ENCOUNTERED AN UINCOMMANDED YAW AT FL 2300 WHILE TRAVELING AT 300KTS. THE CREW RAN THE QUICK REFERANCE HANDBOOK AND DECLARED AN EMERGENCY. THE AIRCRAFT LANDED WITHOUT INCIDENT AND IS CURRENTLY IN WORK.Mar 23, 2018 · N703PS · Cndair CL6002C10SDR 2018FA0000117Hinge Bracket · corrodedPROBLEM AREA BY VISUAL INSPECTION - RIGHT AND LEFT FLAP HINGE BRACKET SEVERE CORROSION AND PRONE TO CRACKS LEADING UP TO THE BOLT HOLES THAT ATTACH THE BRACKET TO THE AIR FRAME OR AT THE FLAP MOUNTING HOLES IF CORROSION PROGRESSES AND NOT DETECTED AND CAN LEADMar 23, 2018 · N579W · Cirrus SR20SDR R61A201803220402Rib · not reportedAILERONS REQUIRED UNUSUAL FORCE TO TURN PAST CENTER. CONTROLS LOCK IN PLACE UNLESS UNUSUAL FORCE IS APPLIED. DECLARED EMERGENCY, DIVERTED, AND LANDED WITHOUT INCIDENT. R & R THE LT RIB 52 IAW SRM 51-41-01. INSTALLED REINFORCEMENT DOUBLE ON FWD SIDE IAW SB170Mar 22, 2018 · N636RW · Emb ERJ170100SESDR VNAA2018032211101Flt Controls · malfunctionedDIVERTED FOR UNCOMMANDED YAW IN FLIGHT. DECLARED AN EMERGENCY AND LANDED SAFELY. UNDECLARED EMERGENCY ON THE GROUND AND TAXIED INTO THE GATE WITH NO COMPLICATIONS.Mar 22, 2018 · N703PS · Cndair CL6002C10SDR DALA2018030901536Actuator · corrodedBARE METAL AND CORROSION ON HOUSING OF LINEAR ACTUATOR MOUNTED UPPER FWD ON ELEVATOR MIXING CONTROL ON AFT ACCESSORY BAY ON TOP AND AFT OF HORIZONTAL STAB CENTER BOX. REMOVED AND REPLACED THE ASSYMETRY LIMITER ACTUATOR IAW AMM 27-31-03.Mar 2, 2018 · N674DL · Boeing 757232SDR ANCF2018020601Computer · malfunctionedHIGH VIBRATION ON INITIAL CLIMB, LT & RT AILERON FAULTS ON ECAM. DURING TAKEOFF ROLL THE VIBRATION WAS FELT ON THE NOSE GEAR. LT AND RT NWA WERE REPLACED IAW AMM 27-93-34, PB 401, ELAC 2CE1 WAS REPLACED IAW AMM 27-93-00-710A. OPS TESTED SATISFACTORY.Feb 6, 2018 · N411AV · Airbus A320214SDR SIMA20180202001Aileron · unknownBINDING IN FLIGHT CONTROLS NOTICED AT FL335 TEMP WAS -47C @ FL335 NARRATIVE: AFTER PROLONGED STABLE CRUISE FLIGHT AT FL390 DESCENT WAS GIVEN TO FL330 AT FL335 WE ENCOUNTERED LIGHT TURBULANCE IN CONJUNCTION WITH A TURN AS YOKES WAS DISPLACED LEFT TO RAISE RIGHTFeb 2, 2018 · N262NN · Emb ERJ170200LRSDR ANCF2017122901Computer · malfunctionedIMMEDIATELY AFTER TAKE OFF, THE FOLLOWS MSGS APPEARED ON ECAM (WHEN TURNING RIGHT) F/CTL R AIL FAULT F/CTL AIL SERVO FAULT AIRCRAFT TRIMMED THE RUDDER TO L3.6 -AFTER ENGINE 2 SHUTDOWN F/CLT R AIL FAULT AND ELAC 1 FAULT APPEARED. CORRECTIVE ACTION: ACC TSM 27-9Dec 29, 2017 · N596EL · Airbus A318112SDR YENA201711090889Computer · failedJUST AFTER LEVEL OFF, IN CRUISE FL 350, RECEIVED A FLT CNTL ELAC 2 FAULT. PERFORMED QRH PROCEDURE WITH UNSUCCESSFUL RESET. DIVERTED. FOR CHECK PITCH CHANGE OVER OF ELAC 2 . R & R THE NR 2 ELAC IAW AMM 27-93-34. TESTED GOOD AND OPERATIONAL.Nov 9, 2017 · N586JB · Airbus A320232SDR VNAA2017110411102Warning Message · multiple failDURING APPROACH AT 3000 FT, THE ILS, LOCALIZER, AND GLIDESLOPE DISCONNECTED AND MISSED. ATC VECTORED THE ACFT AROUND TO ANOTHER RUNWAY AND THE FLIGHT CREW HAND FLEW THE APPROACH. DURING APPROACH, CREW RECEIVED OUTBOARD SPOILERON AND OUTBOARD FLIGHT SPOILERS Nov 4, 2017 · N547NN · Cndair CL6002D24SDR UIEA2017102502085Ring · corrodedFOUND CORROSION ON REACTION RING SPLINES POSITION 3. REACTION RING REPLACED.Oct 26, 2017 · N1373A · Boeing 767300SDR UIEA2017102502090Actuator · corrodedFOUND CORROSION ON ROTARY ACTUATOR POSITION 7. THE ROTARY ACTUATOR WAS REPLACED.Oct 26, 2017 · N1373A · Boeing 76731KSDR UIEA2017102502089Actuator · corrodedFOUND CORROSION ON ROTARY ACTUATOR POSITION 6. THE ROTARY ACTUATOR WAS REPLACED.Oct 26, 2017 · N1373A · Boeing 76731KSDR UIEA2017102502088Actuator · corrodedFOUND CORROSION ON ROTARY ACTUATOR POSITION 3. THE ROTARY ACTUATOR WAS REPLACED.Oct 26, 2017 · N1373A · Boeing 76731KSDR UIEA2017102502087Actuator · corrodedFOUND CORROSION ON ROTARY ACTUATOR POSITION 1. THE ROTARY ACTUATOR WAS REPLACED.Oct 26, 2017 · N1373A · Boeing 76731KSDR UIEA2017102502086Shaft · corrodedLEFT WING POSITION NR 2 SHAFT FOUND CORRODED. THE INPUT SHAFT WAS REPLACED.Oct 26, 2017 · N1373A · Boeing 76731KSDR UIEA2017102502084Ring · corrodedFOUND CORROSION ON REACTION RING SPLINES POSITION 2. THE REACTION RING WAS REPLACED.Oct 26, 2017 · N1373A · Boeing 76731KSDR UIEA2017102502081Ring · corrodedFOUND CORROSION ON REACTION RING SPLINES POSITION 7. REACTION RING WAS REPLACED.Oct 26, 2017 · N1373A · Boeing 76731KSDR UIEA2017102502080Ring · corrodedFOUND CORROSION ON REACTION RING SPLINES POSITION 1. THE REACTION RING WAS REPLACED.Oct 26, 2017 · N1373A · Boeing 76731KSDR QMLA2017100717102Warning Light · illuminatedDURING FLIGHT, THE DG, NR 2 INVERTER, AND PR SAS ILLUMINATED ON THE CAD AND THE NR 2 GENERATOR AMPS WERE RUNNING ABOUT 20 AMPS HIGHER THAN THE NR 1 GENERATOR. THE AIRCRAFT BECAME UNSTABLE LIKE IT LOST ALL OF STABILITY. GOT EVERYTHING TO CLEAR ON THE CAD. DUOct 7, 2017 · N135CJ · Urocop EC135T2SDR HNAA2017100200343Unknown · unknownAT 100 KNOTS DURING TAKE OFF, AIRCRAFT ABRUPTLY YAWED TO THE LEFT. COMPLIED WITH GVI ON NLG AND MLG. NO DEFECTS FOUND. ALL TIRE PRESSURES WERE GOOD. OK FOR SERVICE.Sep 29, 2017 · N600BP · Emb EMB145LRSDR CALA2017090803062Relay · faultyAFTER DEPARTURE, HAD A RUNAWAY NOSE UP STAB TRIM. ALSO HAD A SPEED TRIM FAIL LIGHT ON. EMERGENCY DECLARED. REPLACED THE STAB TRIM RELAY R64 AT J4 BOX. COMPLIED WITH EC/RA 2741-01216. PERFORMED BITE CHECK FOR DFCS, OPS CHECKED GOOD. PERFORMED LAND VERIFY TSep 8, 2017 · N16713 · Boeing 737724SDR AALA20170819002Yaw Damper · faultedFLIGHT DIVERTED DUE TO A YAW DAMPER FAILURE, EMERGENCY DECLARED. FIRST OFFICE FAC LOCKED UP. AUTOPILOT DISCONNECTED AT FL390, ALONG WITH ECAM MESSAGES FOR AUTO FLIGHT YAW DAMPER SYSTEM AND ALTERNATE LAW. RESET FAC 1, THEN FAC 2 FAILED TO RESTORE SYSTEM. FAAug 18, 2017 · N8001N · Airbus A319115SDR HNAA2017082100280Switch · malfunctionedIMMEDIATELY AFTER TAKEOFF, LG AIR/GRD FAIL CAUTION MESSAGE DISPLAYED ON EICAS AND PITCH TRIM MAIN INOPERATIVE WARNING MESSAGE. PITCH TRIM RUN AWAY TO NOSE DOWN. R & R THE BACKUP TRIM SWITCH AND OPS CHECKED IAW AMM 20-13-05. OPS CHECKED GOOD. COULD NOT DUPLICAAug 18, 2017 · N635AE · Emb EMB145LRSDR 2017FA0000423Cable · wrong partDURING AN ANNUAL INSPECTION, REPLACED THE FWD LEFT TRIM CABLE WITH NEW. FOLLOWING INSTALLATION, THE RT FWD TRIM CABLE APPEARED DIFFERENT FROM THE LEFT. THE CABLE APPEARED TO BE BIGGER. PINCHED THE TWO CABLES TOGETHER AND PUT THEM UNDER A MICROSCOPE AT 250 PAug 10, 2017 · Piper PA28161SDR ASOA201708061822Control Panel · malfunctionedUNCOMMANDED RUDDER DEFLECTION TO RIGHT. ACFT RETURNED TO DEPARTURE AFTER T/O. REMOVED AND REPLACED THE ALIERON-RUDDER CONTROL PANEL IAW AMM 27-12-10. OPS TESTED AILERON TRIM SYSTEM IAW AMM 27-11-00. OPS TESTED RUDDER TRIM SYSTEM IAW AMM 27-22-00. OPS TESTEDAug 6, 2017 · N716EV · Cndair CL6002C10SDR O2GA2017071950601Actuator · lack of lubeEXCESSIVE VIBRATION IN CONTROL COLUMN FELT AT HIGH SPEEDS AND LOWER ALTITUDE. MAINTENANCE FOUND EXCESSIVE TRIM TAB PLAY DUE TO ACTUATORS REQUIRING LUBRICATION. GREASED ACTUATOR'S. SUCCESSFUL OPERATIONAL CHECK FLIGHT WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVJul 9, 2017 · N506UP · Cessna 560XLSDR GTIA2017070502047Computer · malfunctionedFLIGHT CONTROL LT AILERON FAULT, RT AILERON FAULT, AND ATN LAW ECAMS APPEARED AFTER ROTATION, ELAC 1 FAULT ECAM APPEARED AFTER NR 1 ENGINE SHUTDOWN, THEN DISAPPEARED. IAW TSM 27-93-00-810-949-A, R & R THE NR 1 ELAC IAW AMM 27-93-34. OPS CHECKED GOOD. R & R Jul 5, 2017 · N621NK · Airbus A320232
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