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 HNAA200901200394Pulley · wornABORTED TAKE-OFF DUE TO EXTREMELY STIFF AND HARD TO MOVE AILERONS. R&R SPOILER CABLE PULLEY ABOVE BAG BAY DOOR WHICH WERE FOUND TO BE GRINDING NOISE. CHECKED AILERON SPOILER CABLE TENSION IAW 27-12-00.Jan 7, 2009 · Dhav DHC8102SDR A6WA200940005Unknown · unknownFLIGHT CONTROLS TAKE 2 TO 3 TIMES THE NORMAL AMOUNT OF PRESSURE TO MOVE SURFACE TO LIMITS WITH ALL HYD PUMPS ON. ONLY AILERONS AND ELEVATORS, RUDDER IS NORMAL, IN FLIGHT OR ON THE GROUND WITH AUTOPILOT OFF FROM BOTH CAPTS AND FO`S SIDE. C/W AWAC AMM SUP 2006Jan 6, 2009 · N464AW · Cndair CL6002B19SDR 2009FA0000039Brake · failedALL (4) ASSYMETRY BRAKES WERE REMOVED FROM THE ACFT IN OCT 2008, MODIFIED AND REINSTALLED. SINCE THAT TIME THE LT FLAP BRAKE FAILED AFTER 6 WEEKS IN SERVICE. THE 2ND BRAKE FAILED WITH 3 MONTHS IN SERVICE. (K)Jan 2, 2009 · N500E · Bombdr BD7001A10SDR DXTA2008123003450Unknown · unknownEXCESSIVE LEFT RUDDER TRIM NEEDED TO MAINTAIN COORDINATED STRAIT LEVEL FLIGHT.Dec 29, 2008 · N983QS · Cessna 750SDR DXTA2008120103380Unknown · unknownACFT WAS DESCENDING THROUGH FL 380 WHEN FLYING PILOT MOMENTARILY LOST PITCH CONTROL.Nov 30, 2008 · N275QS · Amd FALCON2000SDR DXTA2008111003347Unknown · out of trimAFTER LEVELING OFF AT 10,000FT, AIRCRAFT WAS SEVERLY OUT OF TRIM.Nov 9, 2008 · N999QS · Cessna 750SDR YENA200810110109Computer · failedFLT 1119, BUF-FLL, ACCELERATING ABOVE 10000FT THE AIRCRAFT BANK 4-5 DEGREES LEFT IN LEVEL FLIGHT. NO FUEL IMBALANCED NOTED, BUT THE LEFT AILERON FLOATING UP ABOVE THE DOUBLE TICK MARKS & THE RUDDER INPUT WAS 2.5 DEGREES RIGHT. DIVERTED TO IAD. DECLARED EMERNov 8, 2008 · N599JB · Airbus A320232SDR YENA200811110108Computer · failedFLT 1119, BUF-FLL, ACCELERATING ABOVE 10000FT THE AIRCRAFT BANK 4-5 DEGREES LEFT IN LEVEL FLIGHT, NO FUEL IMBALANCED NOTED, BUT THE LEFT AILERON FLOATING UP ABOVE THE DOUBLE TICK MARKS & THE RUDDER INPUT WAS 2.5 DEGREES RIGHT. DIVERTED TO IAD. DECLARED EMERGNov 8, 2008 · N599JB · Airbus A320232SDR KCSA08072Unknown · malfunctionedAPPROXIMATELY 2:20 INTO FLIGHT, A/P DID NOT FOLLOW ROLL COMMAND IN INS OR HDG MODES. AFTER A/P DISCONNECT, UNABLE TO ROLL AIRCRAFT TO CHANGE HEADING MANUALLY WITH AILERONS. SPEED BRAKES WOULD NOT EXT.Nov 7, 2008 · N715CK · Boeing 747209BSDR RU3A003Control Cable · chafedPROBLEM ON 3 AIRCRAFT WITH EXCESSIVE WEAR, WHERE THE CABLES GO THROUGH THE PHENOLIC RUB STRIPS. THIS WAS FOUND DURING CABLE REMOVAL TO FACILITATE OTHER MAINTENANCE, WHEN THE CABLES ARE INSTALLED THE WEAR AREAS CAN'T BE SEEN. THERE IS NO INSPECTION REQUIRED FOct 22, 2008 · Lear 60LEARSDR CHQA200800190Trim System · malfunctionedAFTER ROTATION ON TAKE-OFF, THE FLIGHT CREW RECEIVED A MAIN PATCH TRIM INOPERATIVE MESSAGE ON EICAS. THE BACK TRIM SYS FUNCTIONED NORMALLY AND TERE WAS NO RUN-AWAY TRIM SITUATION. THE QRH WAS FOLLOWED BUT THE MAIN TRIM WOULD NOT OPERATE. THE AIRCRAFT LANDED BOct 2, 2008 · N382SK · Emb EMB135KLSDR HXS2008F00000Bracket · crackedON THE BOTTOM SIDE OF THE FOOT PEDAL CONTROLS, ON BOTH THE RT AND LT SIDES, THERE IS A BRACKET THAT IS PART OF THE FOOT PEDAL BELLCRANK ASSY, THE LT BRACKET PN 350A21136324, HAS A CRACK IN IT. THE RT BRACKET, SAME PN, CRACKED ALL THE WAY THROUGH WHICH ALLOWED Sep 29, 2008 · N403AE · Snias AS350B3SDR 08FDEA04012Unknown · unknownRUDDER TRIM WOULD NOT OPERATE, NOTICED DURING CRUISE FLIGHT, INOP WITH A/P ON AND OFF. DEBRIEFED FLIGHT CREW IN DETAIL. IN CRUISE FLIGHT, WITH AUTO PILOT IN COMMAND THEY NOTICED THEY COULD NOT GET THE RUDDER TRIM TO OPERATE, NO FAULTS ON PANEL OR ECAM, INDSep 24, 2008 · N654FE · Airbus A300F4605RSDR SIMA200826602Unknown · vibrationON FLIGHT 4108 CREW REPORTED A FLUTTER/VIBRATION IN THE FLIGHT CONTROLS DURING ALL PHASES OF FLIGHT. STARTED AT 150KTS, VIBRATION FELT WITH GEAR IN UP OR DOWN POSITION. VIBRATION FELT WITH AUTO PILOT ON AND OFF, PACKS ON, CREW NOTED THE VIBRATION THROUGH FLISep 20, 2008 · N843AE · Emb EMB135KLSDR 2008UALA05776Bypass Valve · leakingFOUND LEADING EDGE BYPASS VALVE (V10059) LEAKING, CRACKED CASTING. CRACK (FATIGUE) IN CASTING. REPLACED LEADING EDGE BYPASS VALVE.Sep 17, 2008 · N550UA · Boeing 757222SDR GLQ2008F00000Nut · damagedROUTINE INSPECTION OF TRANSIENT ACFT REVEALED BOTH UPPER PULLEY FWD BEARING RETAINER CAP ATTACH BOLT NUTS LOOSE-APPROX Q.5 THREADS ONLY ENGAGED. THESE WERE SERVICEABLE USED NUTS. THREAD MARKINGS NOTED IN LOCK AREA. NUTS STILL EXHIBIT LOCKING CAPABILITY. FRAMESep 11, 2008 · N6143K · Hughes 269CSDR 2008UALA05486Unknown · unknownTHE "AIL LOCK" LIGHT ON AT HIGH SPEED. EICAS MSG "AILERON LOCKOUT" DISPLAYED. OUTBOARD AILERONS INDICATED MOVEMENT - UNLOCKED BOTH.Aug 26, 2008 · N658UA · Boeing 767322SDR GAJ2008F00000Pulley · frozenTHE COPILOT RETRACTABLE STEP MALFUNCTIONED DUE TO PULLEYS FREEZING. FWD PULLEY IS HARD TO SEE ON AFT NOSE GEAR WELL AND IS IN A VERY DIRTY ENVIRONMENT. THE REAR PULLEY IS IMPOSSIBLE TO SEE. THE REAR PULLEY STOPPED ROTATING (FROZE) CAUSING SEVERE WEAR TO THE CAAug 25, 2008 · N7067Z · Cessna T210MSDR DXTA200803235Unknown · unknownON DEPARTURE AFTER AUTOPILOT WAS DISCONNECTED AND AIRCRAFT HAD FLOWN TO LEVEL FLIGHT AILERON & ELEVATOR SEEMED TO BE LOCKED IN POSITION.Aug 21, 2008 · N721QS · Gulstm 200SDR IXX2008F00088Actuator · defectiveFLIGHT ATN103/KWRI TO PANC - DURING CRUISE FROM KWRI BOTH PILOT`S AND COPILOT`S YOKE TRIM SWITCHES INOPERATIVE. THE CREW DIVERTED TO KTOL AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED RT LONG TRIM ACTUATOR, OPERATIONAL CHECK GOOD IAW 27-41-10. ACFT WAS Aug 18, 2008 · N721CX · Doug DC872FSDR 2008UALA04309Actuator · faultedELAC 1 & 2 PITCH FAULT. RTFL. REPLACED THS ACTUATOR. ACCOMPLISHED SUCCESSFUL TEST FLIGHT. A/C OKAY FOR SERVICE. Aug 15, 2008 · N460UA · Airbus A320232SDR YENA2008076Computer · failedFLT 233, SLC-LGB, AFTER TAKEOFF ACFT SUFFERED A L&R AIL FAULT WITH ACFT ONLY ABLE TO FLY IN ALTERNATE LAW. PER PFR MSGS ELAC AIL ORDER DISAGREE & ELAC 2 AIL ORDER DISAGREE WERE FOUND. PER TSM 27-93-00-810-949 STEP 4A. ELAC (2CE1) NEEDS REPLACING. PERFORMED Aug 10, 2008 · N603JB · Airbus A320232SDR 26N2008F00005Selector · unknownCREW REPORTED AILERONS FROZE AFTER FLYING THROUGH MOISTURE. 07/25/2008 AC REPOSITIONED TO SERVICE CENTER FOR FURTHER EVALUATION AND RESOLUTION. MFG HEAVILY INVOLVED WITH THIS ISSUE. (K)Aug 4, 2008 · N1693L · Cessna 510SDR 2008UALA04063Unknown · unknownCREW REPORT: W-RUDDER TRIM ZEROED, AIRCRAFT ROLLS RIGHT ON ROTATION. LEVEL FLIGHT REQ 2.5 UNITS LEFT RUDDER. *S/D* ACCOMPLISHED OPS CHK OF RUD PER AM 27-21-00. ALSO CHECKED SYS PER AMM 27-21-00 ITEM THRU PG 524 ITEM I ALL CHECKS NORMAL. REF AMIS PTT SEQ Jul 29, 2008 · N598UA · Boeing 757222SDR DXTA200803200Module · malfunctionedRUDDER LIMIT FAIL B CAS MESSAGE CAME ON IN FLIGHT. LIMITED TO 26 PERCENT. RE-RACKED LOGIC MODULES NK111ND NK112 IAW MM 45-24-10. SYSTEM OPS CHECKED GOOD PER MM 27-20-00.Jul 27, 2008 · N916QS · Cessna 750SDR DXTA200803197Unknown · vibrationON CLIMB FELT VIBRATION IN ALL CONTROLS AND COCKPIT SEATS. (A)Jul 24, 2008 · N390QS · Cessna 560CESSNASDR RAIA00807015Unknown · unknownFLT 5574 - RIC - DURING LANDING AT 50 FT ALTITUDE, THE CREW REPORTED THAT THE PLANE YAWED TO THE LT WITH A 15-20 DEGREE ROLL TO THE LT. NO WIND GUST REPORTED. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE AUTOPILOT SYSTEM AND PERFORMED A DETAILED VISUAL Jul 19, 2008 · N820HK · Emb EMB145SDR YEN2008F00014Computer · faultedAIR RETURN TO DEPARTURE AIRPORT, L AIL FAULT, RAIL, FAULT RT AFTER TAKEOFF, NO AUTO PILOT ALT LAW, NO OTHER INDICATIONS, REMOVED AND REPLACED NR 1 ELAC IAW MM 27-30-34-000. OPS CHECK GOOD. (K)Jul 7, 2008 · N646JB · Airbus A320232SDR 2008UALA03705Unknown · unknownLANDED UNDER AMBER ALERT DUE TO FLAP/RUDDER PROBLEM.Jul 4, 2008 · N672UA · Boeing 767322SDR 2008UALA02725Control Unit · faultyAIL SERVO FAULT, LAF DEGRADED L AIL AMBER HALF BOX B, R AIL AMBER HALF BOX G. REPLACED ELAC 1, ALL OPS TESTS WERE NORMAL. May 10, 2008 · N408UA · Airbus A320232SDR 2008UALA02716Sdac · malfunctionedF-CTL ELAC 1 FAULT AND ELAC 2 FAULT. REPLACED SDAC NR 2, OPS TESTS OK. NOMay 8, 2008 · N496UA · Airbus A320232SDR DT1R200800001Lever · damagedOPENED THE ACCESS PANEL UNDER THE CO-PILOT'S SEAT, FOUND THE YAW TRIM LEVER (PN 109-0020-47-7 NSN) DETACHED FROM THE YAW TRIM MOTOR SHAFT. NO DAMAGE NOTED TO THE MOTOR SHAFT. THE LEVER WAS INTACT BUT DAMAGED AT THE POINT WHERE IT CONTACTS THE SHAFT, BUT HAD May 8, 2008 · N167JC · Agusta A109SSDR 2008UALA02547Unknown · unknownVERTICAL FLUTTER IN INTERVALS OF THREE DURING ALL PHASES OF FLIGHT.May 1, 2008 · N370UA · Boeing 737322SDR AALA200801147Fitting · damagedAFW - DRIVE ARM FITTING ASSEMBLY JOINT 2A HAS BEEN BORED TO 1.714 INCH. BEYOND ALLOWABLE DIMENSION OF CMM 27 57 97 REPAIR 2.2. REPAIRED PER ENGINEERING INSTRUCTIONS.Apr 28, 2008 · N793AN · Boeing 777223SDR 2008UALA02141Unknown · unknownUNCOMMANDED DUTCH ROLL DURING ENTIRE APPROACH. ACCOMPLISHED AILERON DAMP ING CHECK, POWERED UP SYSTEM AND CHECKED SPOILERS FOR FLOAT, EFC S CHECK,CAT 3 CHECK COMPLETED, NO MSG OR FAULTS FOUND, REPLACED BOTH FAC 1 AND 2 AS PRECAUTIONARY. THIS EVENT NEVER REApr 12, 2008 · N806UA · Airbus A319131SDR 2008UALA01769Computer · faultedF-CTL ELAC 2 FAULT ON UPPER ECAM. PERFORMED RESET AND RECURRED. ELAC INTERMITTANT, BAD MPS BOARD INTERNAL. REPLACED ELAC 2, ALL TESTS NORMAL.Mar 28, 2008 · N404UA · Airbus A320232SDR 2008UALA01695Unknown · unknownPER CREW WHEN ONLY ELEVATOR MOVEMENT, HAD TOO MUCH RESISTANCE. WHEN ONLY AILERON MOVEMENT, RIGHT SIDE TOO MUCH RESISTANCE. WITH SPOILERS DEPLOYED AILERONS OK. ELEVATORS ALWAYS HAD TOO MUCH RESISTANCE.Mar 25, 2008 · N221UA · Boeing 777222SDR UALA2008111301673Computer · failedELAC 1 FAULT DISPLAYED ON UPPER ECAM SCREEN, - F-CTL. ELAC 1 FAILURE. REPLACED ELAC 1. ACCOMPLISHED OPS TESTS, OK.Mar 24, 2008 · N436UA · Airbus A320232SDR 2008UALA01673Computer · malfunctionedELAC 1 FAULT DISPLAYED ON UPPER ECAM SCREEN. F-CTL CAUSE, ELAC 1 FAILURE. REPLACED ELAC 1, ACCOMPLISHED OPS TESTS, OK.Mar 24, 2008 · N436UA · Airbus A320232SDR USAA920080606Computer · malfunctionedFLT 363 - PHX-SMF - UNSCHEDULED LANDING - CREW REPORTED AN ELECTRICAL BURNING SMELL IN THE COCKPIT JUST AFTER AN ELAC-2 FAULT. CREW WERE UNABLE TO RESET AND SUSPECTED THE BURNING SMELL WAS FROM THE ELAC (ELEVATOR AILERON COMPUTER). THE AIRCRAFT WAS DIVERTED Mar 10, 2008 · N644AW · Airbus A320231SDR 2008UALA01293Computer · failedELEVATOR-AILERON COMPUTER (ELAC) 1 INOP. FCDC1 FAULTY: SHOP FINDINGS NFF. REPLACED FCDC1, ALL OPS CHECKS WERE NORMAL.Mar 9, 2008 · N481UA · Airbus A320232SDR 2008UALA01000Control Box · faultyFLIGHT CONTROL SYSTEM MESSAGE OCCURRED IN FLIGHT. PERFORMED EXTENSIVE TROUBLESHOOTING, & CHRONIC SYSTEM REVIEW. MANY UNITS PREVIOUSLY REPLACED BUT PROB NOT ENTIRELY CORRECTED. REPLACED POWER SUPPLY ASSY & ACE L-1 A SECOND TIME. ALL TESTS PERFORMED WITH GOOFeb 22, 2008 · N792UA · Boeing 777222SDR 2008UALA00907Computer · faultyELAC 1 FAULT DISPLAYED ON UPPER ECAM SCREEN. DISCREET OUTPUTS OUT OF CALIBRATION. REPLACED ELAC NR 1, ALL OPS CHECKS PERFORMED SATIFACTORY.Feb 18, 2008 · N419UA · Airbus A320232SDR 2008UALA00719Unknown · unknownDEBRIEFED WITH FLT CREW, CAPT WAS FLYING AIRCRAFT AND AT TOUCH DOWN (MAIN LANDING GEAR WAS ON RUNWAY) CAPT RELAXED STICK TO NEUTRAL AND THEN AIRCRAFT NOSE AGGRESSIVELY PITCHED UP. UNKNOWN (UNABLE TO DUPLICATE- POST FLIGHT). NO INFO ON PFR, NO HISTORY ON PREVFeb 8, 2008 · N449UA · Airbus A320232SDR 2008UALA00608Computer · faultyELAC 2 FAULT DISPLAYED ON UPPER ECAM SCREEN. ELAC 2 FAILURE, CIRCUIT BOARD FAILURE. BOTH ELAC 1 AND ELAC 2 WERE REPLACED ON THE A/C FOR PRECAUTION. ALL SYSTEM TEST ACCOMPLISHED AND NO FAULTS NOTED. THE ELAC UNIT WAS SENT TO THALES AND SEVERAL COMPONENTS (IFeb 1, 2008 · N409UA · Airbus A320232SDR FDKA200801041Computer · malfunctionedFDM 9963 ORF-JFK (1810 PHX LCL) - COMMAND AND INDICATION OF ROLL AND YAW TRIM NOT IN SYNC WITH ACTUAL CONTROL SURFACE POSITION. MX REMOVED AND REPLACED IC-600.Jan 28, 2008 · N846MJ · Emb EMB145LRSDR 2008UALA00446Trim System · unknownLANDED UNDER AMBER ALERT DUE TO A TRIM PROBLEM. RESUBMITTED. UNKNOWN PART INFO.Jan 26, 2008 · N338UA · Boeing 737322SDR A6WA20080046Unknown · malfunctionedHIGHER THAN NORMAL BACK PRESSURE NEEDED DURING LANDING WITH YOKE. (K)Jan 23, 2008 · N460AW · Cndair CL6002B19SDR 2008UALA0027Warning System · activatedTHE "FLIGHT CONTROLS" EICAS APPEARED AFTER ENGINE START. Jan 1, 2008 · N779UA · Boeing 777222SDR DXTA200702737Actuator · leakingON TAKEOFF, GOT A STAB MISCOMPARE LIGHT AND THE HYDRAULIC PRESS LIGHT. REPLACED ACTUATOR DUE TO EXCESS LEAKAGE IN ACTUATOR IAW 560XL M/M 23-40-00. OPS AND LEAK CHECK GOOD.Jan 1, 2008 · N627QS · Cessna 560XL
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