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 EGI2008F00000Control Tube · shearedPILOT REPORTED TO MAINTENANCE THAT THE ELEVATOR HAD AN EXCESSIVE AMOUNT OF TRAVEL AND THE CYCLIC SEEMED TO BE SLIGHTLY STIFF FORE AND AFT. TROUBLESHOOTING PERFORMED BY MAINTENANCE AND FOUND THE ELEVATOR CONTROL TUBE SHEARED AT THE SHEAR PIN WHICH IS LOCATED ISDR YENA2007124Computer · malfunctionedFLT NR 802, FLL-JFK, DIVERTED TO MCO, AIRCRAFT EXPERIENCED VERY HEAVY VIBRATION 17000-28000 FEET AT VARIOUS SPEEDS 270KTS-330KTS, UNABLE ISOLATE TO VIA VIBRATION CHECK LIST. PERFORMED INSPECTION AND OPERATION CHECK OF NOSE LANDING GEAR AND DOORS. NO DISCREPASDR USAA920071320Unknown · malfunctionedFLT 1985 - BUF-CLT - UNCOMMANDED ROLL - AT FL 370 AUTO PILOT NR 1 KICKED OFF WITH AIRCRAFT ROLL LEFT AT 5 DEG. MANUALLY CONTROLLED A/C. ENG PARAMETERS NORMAL, YAW DAMPER NORMAL, RUDDER FREE AND CENTERED. TRIED BOTH AUTO PILOTS TO NO AVAIL. HAD CW/PITCH STEESDR DXTA200702649Unknown · unknownA LARGE AMOUNT OF FORWARD ELEVATOR TRIM WAS REQUIRED AFTER TAKEOFF. ALSO DURING DESCENT THE TRIM WAS ALL THE WAY FORWARD AGAINST THE STOP. INSPECTED SYSTEM. FOUND HARDWARE FOR ELEV TRIM CONTROL WHEEL BACKED 3/4 OF THE WAY OUT, ALLOWING ELEV TRIM INDICATOR DRSDR 2007UALA04697Warning Light · illuminatedSTAB TRIM LIGHT ILLUMINATED AFTER T/O,TRIM FELT LIKE REDUCED RATE.
SDR A6WA200740644Unknown · unknownDURING APPROACH TO MHT, NOSE UP TRIM OF 9.2 UNITS REQUIRED TO MAINTAIN NORMAL GLIDE PATH. FLIGHT CONTROLS HEAVIER THAN NORMAL, ESPECIALLY ELEVATOR. AILERONS FEEL HEAVY ALSO. NO UNUSUAL WEATHER CONDITIONS. ALL HYDRAULIC NORMAL. ELEVATOR TRIM ON GO AROUND OSDR 2007UALA04604Trim System · failedON CLIMBOUT AT 17K LOST MAIN ELEC NOSE DOWN TRIM PER CAPTAIN.
SDR C77A200700003Module · power lossDURING FLIGHT PILOT SENT ACARS MESSAGE WAS AS FOLLOWS: DSP/MX ADS 1 FAIL MSG. RAN QRH. ALSO SPLR FLT MSG. ARE LANDING DST AFFECT. ONCE A/C LANDED IN GRB A/C WAS TOWED TO GATE. MECHANIC PERFORMED A POWER RESET, IAW AMM FIM 31-42-00-811-808A WHICH CLEARED (AVNX SDR YENA2007095Controller · malfunctionedFLT 433, BOS-MCO, ON A/P OFF DESCENT FROM 7000FT TO 2000FT FLAPS 1 SPEED 190 KT5.TO HOLD LEVEL FLIGHT LEFT AILERON WAS DISPLACED 1/3 DN. RT 1/3 UP. NR 1, 2, 3 & 4 FOR FLIGHT CONTROL CKS PERFORMED WITH NO FAULTS NOTED. PER MCC REQUEST REMOVED AND REPLACED ELASDR 2007UALA04578Computer · malfunctionedELAC 2 PITCH FAULT DISPLAYED ON UPPER ECAM SCREEN. PERFORMED RESET AND OPERATIONAL TEST OF ELAC2. OPS CHECK GOOD.SDR A6WA200740598Unknown · malfunctionedABORTED TAKEOFF PRIOR TO 80 KNOTS DUE TO TAKEOFF WARNING FOR CONFIG TRIM, CONFIG SPOILERS AT WEIGHT OF APPROXIMATELY 46,000 LBS. WHEN MESSAGE CLEARED AILERON AND RUDDER TRIM INDICATIONS FLUTTERED FROM WHITE TO GREEN. PERFORMED NUMEROUS, OPS CHECKS OF FLIGHT SDR 2007UALA04574Computer · faultyELAC 1 FAULT DISPLAYED ON UPPER ECAM SCREEN. F-CTL CREW COMMENTS: IN CLIMB SLIGHT BUMP, THEN F-CLT ELAC1 FAULT. CYCLED SWITCH ONCE PER ECAM. NO HELP. FOUND ELAC1 FAULTY/BAD CPU. REPLACED ELAC1 COMPUTER - CHECKS OK, NO REPEATS SINCE ORIGINAL.SDR 2007UALA04540Computer · faultyELAC 2 PITCH FAULT DISPLAYED ON UPPER ECAM SCREEN. ELAC2 FAULTY-NFF. REPLACED ELAC2 - ALL TESTS PASSED.SDR 2007UALA04515Computer · failedELAC 2 PITCH FAULT ECAM MESSAGE DISPLAYED AFTER PUSHBACK. TRIED CYCLING ELAC C/B AS WELL AS CONTROL SWITCH, ALL NO HELP. FOUND ELAC2 FAILURE. REPLACED ELAC2 AND MESSAGE CLEARED.SDR 2007UALA04451Computer · faultyAILERON SERVO FAULT DISPLAYED ON UPPER ECAM SCREEN. FOUND NR 1 ELAC FAULT CAUSING AIL SERVO FAULT DISPLAY. REPLACED NR 1 ELAC. OPS CHECK OK, NO REPEATS.SDR AMTA200700525Unknown · unknownEO 757-27AD-3162 AILERON CONTROL, ADDITION OF LATERAL DAMPER TO THE FIRST OFFICERS AILERON CONTROL QUADRANT. COMPLIED WITH EO 757-27AD-3162. (M)SDR 2007FA0000941Roll Servo · looseMOTOR ASSY COMING LOOSE ON SERVO MOUNT. LOOSE HARDWARE, LOOSE MOTOR. RECOMMEND SERVO TO BE INSPECTED FOR PROPER SERVO ASSY (THAT MOTOR AND HARDWARE ARE NOT LOOSE). (K)SDR 2007UALA04091Unknown · unknownAC ROLLS RIGHT WHEN FLAPS EXT BEYOND POS 1 ON AND OFF AUTOPILOT.SDR 2007UALA04092Servo · faultedELEV SERVO FAULT DISPLAYED ON UPPER ECAM SCREEN. F-CTL CREW COMMENTS: ELEV SERVO FAULTED. 10-19-07 REPLACED ELAC 1. NO REPEATS SINCE ORIGINAL.SDR 2007UALA04002Computer · faultedELAC 2 FAULT DISPLAYED ON UPPER ECAM SCREEN. 10-19-07 FOUND NR 2 ELAC FAULTY. REPLACED NR 2 ELAC COMPUTER- NO REPEATS.SDR 2007UALA03998Computer · faultedELAC 2 FAULT DISPLAYED ON LOWER ECAM. 10-19-07 FOUND ELAC NR 2 FAULT. REPLACED AND RESET ELAC 2 AND ACP AFS TEST- NO REPEATS SINCE ORIGINAL.
SDR DXTA200702502Warning Light · false activationDURING APPROACH, THE FLAPS WERE SELECTED TO 15. THE STAB MISCOMPARE LIGHT ILLUMINATED. EMER CHECKLIST ACCOMPLISHED. ONCE FLAP HANDLE WAS SELECTED TO 35 DEGREES THE STAB MISCOMPARE LIGHT WENT OUT AFTER 5 SECONDS. PERFORMED THE TWO POSITION HORIZONTAL STABILIZSDR 2007UALA03932Computer · faultyELAC 2 PITCH FAULT DISPLAYED ON UPPER ECAM SCREEN, F-CTL. *S/D* SEC NR 2 AND RELAY 36CE3 FAULT. REPLACED SEC NR 2 AND RELAY 36CE3, OPS CHECK GOOD.SDR A6WA200740541Unknown · unknownLONGITUDINAL OSCILLATIONS BEGAN CLIMBING THRU APPROX 26,000 FT FOR APPROX 30 SECONDS OSCILLATIONS RETURNED IN LEVEL CRUISE FLIGHT AT 33,000 WITH AUTOPILTO ON OR OFF. OSCILLATION STOPPED WHEN BEGAN DESCENT.SDR CA070917005Unknown · multiple fail(CAN) AIRCRAFT EXPERIENCED FLAP FAILURE ON PREPARATION FOR LANDING, THEN FLEW APPROXIMATELY A FURTHER 10 MINUTES ATTEMPTING,UNSUCCESSFULLY, TO DEPLOY THE FLAPS. ON TOUCHDOWN THE THRUST REVERSERS (TR) DID NOT DEPLOY WHEREUPON THE CREW RECYCLED THE TR ARM SWITCHSDR 2007UALA03628Computer · faultedELAC 1 FAULT DISPLAYED ON UPPER ECAM SCREEN. F-CTL CREW COMMENTS: ATTEMPTED 2 RESETS, NO JOY. 10-11-07 FOUND ELAC NR 1 FAULTED. REPLACED ELAC NR 1.SDR 2007UALA03579Rod End · wornMODERATE AIRFRAME VIBRATION DURING CLIMB 320KT - 14000 STOPPED AT 300. *S/D* ELEVATOR SERVO CONTROL ROD END (LT) OUT OF RIG. REPLACED BOTH ELEVATOR SERVO ROD ENDS AND PERFORMED ELEV FREEPLAY CHECK. ALL NORMAL, NO REPEATS SINCE ORIGINAL.SDR VNAA0708023Trim Switch · stickingCREW REPORTED THE CAPTAINS TRIM SWITCH STICKING AFTER TAKEOFF. CREW ELECTED TO RETURN TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND CLEANED THE TRIM SWITCH. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT WAS RELEASED FOR SERVICE.SDR DXTA200702416Actuator · inoperativeDURING TAKEOFF ROLL APPROXIMATELY 80 KTS, YAW DAMP OFF LOWER B CAS MESSAGE. REMOVED FAILED NR 2 LINEAR ACTUATOR, INSTALLED REPAIRED NR 2 LINEAR ACTUATOR, IAW CESSNA 750 MM 27-24-00 08/23 OPPS CHECK GOOD.SDR 2007UALA03082Computer · failedFLIGHT LOST 1 AND 2 FAC ON TAKEOFF. CREW RAN ECAM AND BOTH CAME BACK. UNABLE TO DUPLICATE PROBLEM SINCE FIRST REPORT. NO REPEATS.SDR 2007FA0000618Anchor · wornANCHOR PN 0713624-2, FOUND WORN ALMOST THROUGH BY THE STEEL PIN USED TO HOLD MASTER CYLINDER. ANCHOR IS ALUMINUM WHICH WAS QUICKLY WORN OUT BY THE STEEL PIN. IF PIN BREAKS FREE FROM THE ANCHOR THE MASTER CYLINDER CAN STOP MOVEMENT OF THE RUDDER PEDAL.SDR 2007UALA02529Unknown · unknownPILOT REPORTED HEAVY ELEVATOR. COULD NOT DUPLICATE ISSUE. NO FINDINGS.SDR CA070709001Shaft · cracked(CAN) THE ROLL FORCE MODIFICATION WAS BEING INSTALLED IN THE AIRCRAFT IAW STC SA05-49. UPON TORQUING THE PILOT`S YOKE ASSEMBLY SHAFT IAW THE INSTRUCTIONS CONTAINED IN DOCUMENT K130-102-001-012, THE FLANGE ON THE SHAFT P/N 240-3140402-1 CRACKED. THE REMAININSDR DXTA200702306Control Panel · shorted10 MIN INTO FLT AT NIGHT, 12000 MSL, IN AND OUT OF CLOUDS AND RAIN, AREA ABOVE RT- SIDE FLT CONTROL PANEL SPARKED W/POPPING NOISE AND BRIEF BURNED SMELL ACCOMPAINIED BY BOTH MASTER WARNING LTS FLASHING. RAN A/C APU AND ENGINES TO VERIFY DISCREPANCY, COULD NOTSDR HALA0700271Unknown · unknownETOPS SIGNIFICANT SYSTEM, AIRCRAFT REQUIRES 4 UNITS OF LEFT RUDDER TRIM TO KEEP THE AILERON TRIM INDICATOR AT ZERO ONLY DURING CLIMB AND DESCENT. AT CRUISE, ALL TRIM SETTINGS ARE NORMAL. T/S PER FIM 27-21-00. OPERATED RUDDER TRIM FULL LT AND RT. RUDDER TRISDR 2007UALA02180Unknown · vibrationENCOUNTERED HIGH SPEED BUFFET AT FL260 AT 320 KNOTS. FLT ATTENDANT REPORTED UP & DOWN MOTION WORST IN AFT CABIN. *S/D* COMPLETED ELEVATOR PLAY CHECKS- ALL GOOD - RIGGED ELEV 5 DEG NOSE DOWN. NO REPEATS SINCE 21 JUNE.SDR DXTA200702283Unknown · unknownPCU MONITOR CB POPPED AND FLIGHT CONTROL FAULT EICAS MESSAGE APPEARED DESENDING THROUGH 6000 FT RUDDER FLT CONTROL SHUT OFF SW ALSO ILLUMINATED. [07-12-07] T/S TO BAD ELEVATOR OUTOBARD PCU ("B" SYS) REMOVED AND REPLACED PCU. PERFORMED RIG CHECKS. SYSTEM LEAKSDR DXTA200702277Unknown · unknownAIRCRAFT CONSTANTLY ROLLS LT AND RT IN LEVEL CRUISE. WORSE AT HIGHER ALTITUDE AND HIGHER SPEED. [07-11-07] RESET RT AILERON DROOP TO SPEC. AND ADJUSTED AILERON SERVO CABLES. IAW 750 MM. 22-10-01. ADJUSTED FEEL BUNGEE IAW 750 MM. 27-11-05. ADJUSTED UPPER RUDSDR DXTA200702226Unknown · unknownAIRCRAFT MADE A SUDDEN YAW TO THE RT AT 105 KTS, ROTATED AT 108 KTS. C/W CHECKS OF FLIGHT CONTROLS, BRAKES AND TIRE PRESSURES. THE RT TIRES WORN TO NEAR LIMITS. NO OTHER DISCREPANCIES NOTED. ALL WORK ACCOMPLISHED IAW MM 5-00-00.SDR 070119Button · stickingDURING CLIMB-OUT FROM LAS, LEADING EDGE SLATS WOULD NOT RETRACT. FLIGHT CREW ELECTED TO RETURN TO LAS FOR A NORMAL LANDING, NO EMERGENCY PROCEDURE WAS PERFORMED. MAINTENANCE DEPARTMENT PERSONNEL INSPECTED AND FOUND THE FLAP/SLAT LOCK OUT BUTTON STICKY. THE SDR DXTA200702207Unknown · unknownAIRCRAFT WOULD NOT ROTATE WITH STICK FULL AFT. (M2B) PERFORMED HIGH ENERGY STOP INSPECTION REF MM 5-50-01, NO DEFECTS NOTED. MEASURED ELEVATOR UP AND DOWN TRAVEL, TRAVEL NORMAL. ELEVATORS MOVED WITH EASE. PERFORMED ELEVATOR CONTROL SYSTEM TRAVEL TEST AND FOUNDSDR NSVA20070108Control Quadrant · malfunctioned"FI STOP OPEN" ILLUMINATED IN FLIGHT UPON GEAR UP. PERFORMED FAULT ISOLATION OF FI STOP AMBER LIGHT ON SHEET 2 FIG 102. FOUND TO FAIL RELAY CONT CHECK. REMOVED AND REPLACED RELAY 20GA STILL NO FIX, CHECKED WIRES AT DOWN LOCK SWITCH HARNESS, FOUND OPEN GROUNSDR DXTA200702083Unknown · unknownCRUISING AT 9,000 FEET WITH A/P ON, THE TRIM CLACKER CAME ON CONTINUOUSLY TO FULL NOSE DOWN, THEN THE FGC A FAILED AND KICKED OFF A/P. REPLACED FAILED ECM. OPS CHECKED OK. IAW. CE 750 M/M 27-40-00.SDR 070088Unknown · unknownFLIGHT 479 FAR/LAS - THE FLIGHT CREW REPORTED THAT AT 250KIAS, AERODYNAMICALLY "CLEAN", THE 'ELEVATOR POWER ON' ANNUNCIATOR ILLUMINATED MOMENTARILY. SIMULTANEOUSLY, THERE WAS A "JOLT" TO THE AIRPLANE. THE FLIGHT CONTINUED TO LAS, THE FLIGHT CREW MADE NO MENTSDR WX0A070069Flt Controls · unknownFLIGHT 461 PIA/LAS. THE FLIGHT CREW REPORT, INFLIGHT AP DISCONNECT DUE TO ROLL CONTROL (YOKE) STUCK DISCOVERED ROLL CONTROL TRIM STUCK (UNTIL 1000 FT AGL LAST CHECK OF THIS FUNCTION. UPON LANDING AFTER TOUCHDOWN, FULL RIGHT AILERON CONTROL WAS MADE WITH LEFTSDR DXTA200702025Unknown · unknownWHEN SWITCHING FROM FGS (A) TO FGS (B) THE CLACKER COMES ON IMMEDIATELY AND DOES NOT STOP. THE STAB DOES NOT MOVE. SWITCHING BACK TO FGS (A) CANCELS THE CLACKERS. REMOVE AND REPLACED FGC CONTROLLER WITH REPAIRED UNIT FROM HONEYWELL RS LV2R992K PER CESSNA 750 SDR AMW083149Spring · brokenAFTER LANDING, THE CAPT REPORTED THAT THE AIRCRAFT PULLED TO THE RIGHT. AIRCRAFT WAS TAKEN OUT OF SERVICE AND REPAIRED. REMOVED AND REPLACED INTERCONNECT SPRING.SDR DJFA2007027Unknown · unknownTRIP NR 1152283/ CREW REPORTED AT FLIGHT LEVEL 380 IN CLEAR SKYS AND SMOOTH AIR A LOUD NOISE SOUNDED AND RANG OUT THROUGHOUT THE AIRCRAFT. AIRCRAFT PITCHED DOWN MOMENTARILY AND CREW DISENGAGED THE AP AFTER WHICH THE AIRCRAFT RETURNED TO NORMAL LEVEL FLIGHT. SDR A6WA200740091Flt Controls · unknownABORTED TAKEOFF AT 110 KNOTS. FLIGHT CONTROLS FELT UNRESPONSIVE IN ROLL, CONTROL YOKE FULL LT DEFLECTION, AIRCRAFT STILL WANTED TO ROLL RT. MAX BTMS = 5, TOW =40,800. INSPECTED AILERON RUDDER, ELEVATOR FLAPS, SPOILERONS, STAB TRIM, RUDDER TRIM AND AILERON TSDR DXTA200701988Unknown · unknownON 2 SEPERATE T/O ROLLS AT 60-70 KTS BOTH YD AND MACH TRIM CAME OFF. T.O.S WERE BOTH ABORTED . NOTE: PITOT HEAT INDICATED WORKING AND WAS LT ON FROM TAXI OUT TO T/O ROLL. (EST 20-25 MIN BY 2ND T.O. ATTEMPT) PLANE WAS SITTING IN HEAVY RAIN FOR SEVERAL HRS.
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