JASC 2720
Service difficulty reports · 3,131
Reports filed under 2720 · Rudder 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 = '2720' 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 = '2720' 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 RU3A201906185024Warning Light · false activationNON ROUTINE REPORT OF RUDDER BOOST LT ON INTERMITTENTLY. MAINTENANCE PERSONNEL COULD NOT DUPLICATE ON GROUND. MAINTENANCE CHECKED CANNON PLUGS, WIRING, AND PERFORMED OPS CHECK OF RUDDER BOOST SYSTEM, SYSTEM CHECKS GOOD.SDR CA190730026Control Cable · corroded(CAN) DURING A SCHEDULED INSPECTION, THE LH FWD RUDDER CABLE P/N 100-617-4413-D01, AND RH FWD RUDDER CABLE P/N 100-4415-D01 WERE REPLACED DUE TO EXCESSIVE CORROSION. BOTH CABLES REPLACED WITH NEW TO RECTIFY. ALL WORK PERFORMED IAW THE APPLICABLE MAINTENANCE PUSDR CALA2019061400946Warning Light · false activationRUDDER RATIO EICAS ON TAKEOFF ROLL AFTER V1..FOLLOWED FIM, L HYD PSI NORMAL. PERFORMED RUDDER RATIO CHANGER MODULE BITE PROCEDURE. REF FIM 27-21-00-815-804 AND FIM 27-09-00-815-814. OPS CHECK NORMAL. NO FAULTS NOTED. ALSO PERFORMED GENERAL VISION INSPECTION OFSDR GTIA2019061003406Servo · out of limits"ON CLIMB OUT, AIRFRAME VIBRATION NOTED AT 12,000 AND 26,000 FEET. AP OFF THEN USING RUDDER TRIM ALEVIATED THE PROBLEM TEMPORARLLY, BUT VIBRATION RETURNED. CLIMING TO 36,000 FEET, WE DID NOT GET THE VIBRATION AGAIN. COMPANY VIBRATION REPORTING SHEET COMPLETED.SDR AALA201906049019Feel Unit · faultedAIRCRAFT WAS GROUNDED: STRONG VIBRATION IN RUDDER PEDALS 2000' AGL BEFORE GEAR EXTENSION TO 500' AGL GEAR DOWN VIBRATION CONTINUED 20 SECONDS AFTER AUTOPILOT OFF. PEDALS LEFT AND RIGHT BOTH SIDES CAPT & FO MOVING 3/8" DISPLACEMENT. PUSHING ON BOTH PEDALS WOULDSDR 2019FA0000164Control Quadrant · looseTHE QUADRANT ON RUDDER TORQUE TUBE WAS FOUND TO HAVE MOVEMENT BETWEEN THE TUBE AND THE QUADRANT. UPON LAST INSTALLATION A INDEX LINE WAS PLACED ON THE TUBE AND QUADRANT. WITH THE GUST LOCK ON AND THE RUDDER PEDALS MOVED BY AN INDIVIDUAL THERE WAS MOVEMENT OF TSDR 2019FA0000163Control Quadrant · looseTHE QUADRANT ON RUDDER TORQUE TUBE WAS FOUND TO HAVE MOVEMENT BETWEEN THE TUBE AND THE QUADRANT. UPON LAST INSTALLATION A INDEX LINE WAS PLACED ON THE TUBE AND QUADRANT. WITH THE GUST LOCK ON AND THE RUDDER PEDALS MOVED BY AN INDIVIDUAL THERE WAS MOVEMENT OF TSDR 2019FA0000162Control Quadrant · looseTHE QUADRANT ON RUDDER TORQUE TUBE WAS FOUND TO HAVE MOVEMENT BETWEEN THE TUBE AND THE QUADRANT. UPON LAST INSTALLATION A INDEX LINE WAS PLACED ON THE TUBE AND QUADRANT. WITH THE GUST LOCK ON AND THE RUDDER PEDALS MOVED BY AN INDIVIDUAL THERE WAS MOVEMENT OF TSDR 2019FA0000161Control Quadrant · looseTHE QUADRANT ON RUDDER TORQUE TUBE WAS FOUND TO HAVE MOVEMENT BETWEEN THE TUBE AND THE QUADRANT. UPON LAST INSTALLATION A INDEX LINE WAS PLACED ON THE TUBE AND QUADRANT. WITH THE GUST LOCK ON AND THE RUDDER PEDALS MOVED BY AN INDIVIDUAL THERE WAS MOVEMENT OF TSDR 2019FA0000160Control Quadrant · looseTHE QUADRANT ON RUDDER TORQUE TUBE WAS FOUND TO HAVE MOVEMENT BETWEEN THE TUBE AND THE QUADRANT. UPON LAST INSTALLATION A INDEX LINE WAS PLACED ON THE TUBE AND QUADRANT. WITH THE GUST LOCK ON AND THE RUDDER PEDALS MOVED BY AN INDIVIDUAL THERE WAS MOVEMENT OF TSDR YENA201905240285Control Module · malfunctionedFLT 2667, MCO-PSE. AFTER TAKE OFF ON CLIMB OUT ECAM. AUTO FLT RUD TRV LIM SYS. COULD NOT RECOVER EITHER SYS PER THE PROCEDURE; R&R ELECTRONIC MODULE OF THE RUDDER TRAVEL LIM UNIT IAW 27-23-51. OPS CK GOOD.SDR FDEA201905211103Transducer · failedPDIS 650 27-21 2182 21MAY19 MEM OPEN U LOGPAGES:3076893 ON CLIMB OUT, RUD TRAVEL SYS 1 &2 FAULT CAME ON. FOLLOWED ECAM AND QRH. TRIED TO RESET IN ACCORDANCE WITH QRH. BOTH FAULT LIGHT'S CAME BACK ON. 21MAY19 06:51 MEM R OLD DISCREPANCY : 650 / 55-SDR AALA201905239013Module · malfunctionedAIRCRAFT WAS GROUNDED: PILOT DECLARED EMERGENCY ON ACCOUNT OF THE RUDDER RATIO LIGHT CAME ON AFTER TAKE OFF. MAINTENANCE ACCOMPLISHED RUDDER RATIO MODULE RESET. NO FAULTS NOTED. A/C OK FOR SERVICE.SDR AALA201905099003Unknown · malfunctionedAIRCRAFT WAS GROUNDED: PILOT REPORTS WHEN PRESSURE APPLIED BY F/O TO RIGHT RUDDER PEDAL DURING TAKEOFF. RIGHT RUDDER PEDAL JUMPS FORWARD ABOUT 1/2 INCH. FEELS LIKE DEAD SPACE. MAINTENANCE COMPLETED OPS CHECK OF RUDDER SERVO CONTROLS IAW AMM 27-24-00-710-002-A.SDR 2019FA0000143Rudder Bar · crackedPILOT WAS STARTED TO TAXI AND RELEASED PARKING BREAK WHEN HE HEARD SNAP SOUND FROM RUDDER PEDALS AND RIGHT SIDE RUDDER PEDAL FEEL STRANGE. PILOT STOPED TAXING AND TURN ENGINE OFF AND STARTED TO DO TROUBLE SHOOTING WHEN HE FOUND THAT RT RUDDER PEDAL WAS COMPLETSDR QXEA2019050600205Unknown · malfunctionedON TAKE OFF AND LANDING ROLL FO'S RIGHT RUDDER INPUT SLOW TO RESPOND. TO KEEP AIRCRAFT ON CENTER LINE. CAPTAIN HAD TO TAKE THE AIRPLANE ON LANDING ROLL OUT AT 70KTS TO MAINTAIN CENTER LINE WITH THE TILLER. REMOVED FROM SERVICE. PERFORMED MTX TAXI, ALL RUDDER ISDR FDEA201905030991Shutoff Valve · failedPDIS 592 29-02 3353 03MAY19 IND FACT U LOGPAGES:3094152 DURING CLIMB OUT TO FL 390 WE RECIVED A LVL 1 HYD 3 ELEV OFF ALERT NO.3 QUANTITY WAS 4.5.W/3-2 NRMP INOP. DURING CRUISE QTY LEVEL WENT TO 4.1. DESCENT INTO IND WE CONFIGURED W/FLAPS 15 ANDSDR ESMR2019050101Rudder Pedal · brokenUPON SETTING THE PARKING BRAKE THE PILOT DEPRESSED THE BRAKE PEDALS AND THE LEFT RUDDER PEDAL BROKE AND FELL OFF THE PIVOT POINT. UPON REMOVAL AND INSPECTION OF THE RUDDER PEDALS, THERE WAS SIGNIFICANT ELONGATION OF THE PIVOT HOLE FOR THE THROUGH BOLT ON BOTH SDR MTNA20190426001Switch · stuckRUDDER PEDALS LOCKED (IN NEUTRAL POSITION) ON SHORT FINAL APPROACH. THE MASTER CAUTION FLIGHT CONTROL LIGHT ILLUMINATED ON THE CENTRALIZED CREW ALERTING SYSTEM (CCAS), AND FLIGHT CONTROL TRAVEL LIMIT UNIT (TLU) FAULT LIGHT ILLUMINATED ON THE OVERHEAD PANEL. RUSDR 2019FA0000272Torque Tube · corrodedRUDDER TORQUE TUBE REQUIRES REPLACEMENTSDR AALA201904229015Spring · defectiveAIRCRAFT WAS GROUNDED: REFERENCE RUDDER PEDALS TAC ON LANDING ROLLOUT, RIGHT RUDDER PEDAL WAS MECHANICALLY STUCK I HAD TO APPY SUFFICIENT FORCE TO BREAK PAST WHATEVER WAS HOLDING IT. ACCOMPLISHED OPS CHECK TEST OF RUDDER ARTIFICAL FEEL LOADS. REMOVED AND REPLASDR 2019FA0000112Bracket · crackedPILOT'S RUDDER PEDAL CONTROL MECHANISM BRACKET ASSY CRACKED. IPC 27-20-00, FIG 10, ITEM 50, PN 72710086-001. REPORTED A BRACKET HAD BROKEN ON THEIR AIRCRAFT AND RECOMMENDED "ONE TIME INSPECTION" FOR MAINTENANCE TO INSPECT THEIR ASSIGNED AIRCRAFT. INSPECTED ASSSDR 2019FA0000111Bracket · crackedPILOT'S RUDDER PEDAL CONTROL MECHANISM BRACKET ASSY CRACKED. IPC 27-20-00, FIG 10, ITEM 50, PN # 72710086-001. REPORTED A BRACKET HAD BROKEN ON THEIR AIRCRAFT AND RECOMMENDED "ONE TIME INSPECTION" FOR MAINTENANCE TO INSPECT THEIR ASSIGNED AIRCRAFT. INSPECTED ASDR 2019FA0000110Bracket · crackedPILOT'S RUDDER PEDAL CONTROL MECHANISM BRACKET ASSY CRACKED. IPC 27-20-00, FIG 10, ITEM 50, PN 72710086-001. REPORTED A BRACKET HAD BROKEN ON THEIR AIRCRAFT AND RECOMMENDED "ONE TIME INSPECTION" FOR MAINTENANCE TO INSPECT THEIR ASSIGNED AIRCRAFT. INSPECTED ASSSDR 2019FA0000109Bracket · crackedPILOT'S RUDDER PEDAL CONTROL MECHANISM BRACKET ASSY CRACKED. IPC 27-20-00, FIG 10, ITEM 50, PN 72710086-001. REPORTED A BRACKET HAD BROKEN ON THEIR AIRCRAFT AND RECOMMENDED "ONE TIME INSPECTION" FOR MAINTENANCE TO INSPECT THEIR ASSIGNED AIRCRAFT. INSPECTED ASSSDR AALA2019041189003Limiter · malfunctionedAIRCRAFT NOT GROUNDED: PILOT REPORTS ON TAKE OFF A SIGNIFICANT RUDDER KICK WAS FELT NOT CAUSED BY WIND GUST, WAKE TURB OR RUDDER INPUT. AFTER LANDING RUD TRL LIMT 1ECAS MSG DISPLAYED. MAINTENANCE REPLACED THE RUDDER TRAVEL LIMITER IAW CARD 26L32527002.SDR QM7R201904020004Bracket · crackedONE TIME INSPECTION FOR CRACK/BREAK OF THE RUDDER CONTROL MECHANISM BRACKET. THE INSPECTION RESULTED IN IDENTIFYING A CRACK AT BOTTOM OF RADIUS.SDR QM7R201904020003Bracket · crackedONE TIME INSPECTION FOR CRACK/BREAK OF THE RUDDER CONTROL MECHANISM BRACKET. THE INSPECTION RESULTED IN IDENTIFYING A CRACK AT BOTTOM OF RADIUS.SDR QM7R201904020002Bracket · crackedONE TIME INSPECTION FOR CRACK/BREAK OF THE RUDDER CONTROL MECHANISM BRACKET. THE INSPECTION RESULTED IN IDENTIFYING A CRACK AT BOTTOM OF RADIUS.SDR QM7R201904020001Bracket · crackedONE TIME INSPECTION FOR CRACK/BREAK OF THE RUDDER CONTROL MECHANISM BRACKET. THE INSPECTION RESULTED IN IDENTIFYING A CRACK AT BOTTOM OF RADIUS.SDR AALA2019040219025Pcu · faultyAIRCRAFT WAS GROUNDED: PILOT REPORTS FLIGHT DIVERSION TO LGA ON ACCOUNT OF AN UNCOMMANDED RUDDER DEFLECTION WHILE AT CRUISE. UPON LANDING, THE CREW RECEIVED A "FLIGHT CONTROL - NO DISPATCH" MESSAGE. MAINTENANCE REMOVED AND REPLACED THE LOWER RUDDER POWER CONTRSDR CA191017018Grommet · debonded(CAN) OPERATOR REPORTED, GROMET DISBONDED FROM FRAME, SLID DOWN THE RUDDER CONTROL CABLE TO THE PULLEY BLOCKING IT IN THE REAR BAY. (TC# 20191017018)SDR K6JY2019040800001Bracket · crackedRUDDER CONTROL BRACKET ASSEMBLY P/N: 72710086-001 CRACKED AT PILOT'S RUDDER PEDAL'S ADJUSTMENT MECHANISM ASSEMBLY P/N 72710311-055. THE BRACKET APPEARS TO HAVE MATERIAL FATIGUE AT THE INBD ANGLE RUN-OUT OF THIS MACHINED PART. CRACK IS LOCATED IN THE RADII OF TSDR RAIA2019032200001Button · defectiveRUDDER SYSTEM 1-2 INOP MESSAGE AFTER YAW DAMPER FAIL MESSAGE. WENT AWAY, CAME BACK THEN WENT AWAY. SYS 1 PRESSURE 3100. SYSTEM 2 3000. REFER TO DISCREPANCY 1, LOG PAGE 471478. R & R RUDDER SHUT OFF PUSH BUTTONS FOR SYSTEM 1 AND 2. OPS CHECK GOOD. MORE INFORMATSDR CA190315012Regulator · failed(CAN) AFTER TAKEOFF RUDDER PRESS AND RUDDER FULL PRESS CAUTION LIGHTS ILLUMINATED. AIRCRAFT DIVERTED. ON APPROACH WHEN FLAPS WERE EXTENDED THE CAUTION LIGHTS WENT OUT. MAINTENANCE REPLACED THE RUDDER PRESSURE REGULATOR PN 237900-3001, SN 0327 AND THE RUDDER PUSDR RJEF20190301001Servo Control · unserviceableDURING FLIGHT LRC638 FROM SAL TO CUN THE PILOT REPORTED AIRFRAME VIBRATION AND RETURNED TO SAL FOR MAINTENANCE. AFTER AN UNEVENTFUL LANDING THE PILOT REPORTED: 1)"STRONG VIBRATION DURING CLIMB AND LEVEL FLIGHT", FOR THIS REPORT MAINTENANCE PERSONNEL PERFORMED SDR JJBA201902252012Actuator · leakingHYD 1 LO QTY EICAS IN FLIGHT FOLLOWED BY HYD SYS 1 FAIL MESSAGE. FOUND UPPER RUDDER ACTUATOR LEAKING. VERIFIED WITH SYS 1 PRESSURIZED. #1 HYD QUANTITY WAS NOT AT ZERO ON THE SERVICING GAUGE. PILOT SAID PRESS STARTED FLUXING TO ZERO 15 TO 20 MIN PRIOR TO SHUTDOSDR 2019F00022Pulley · failedDURING A SCHEDULED 200FH INSPECTION AS REQUIRED BY CHAPTER 05-00-00, THE LEFT LOWER RUDDER PULLEY, IT WAS NOTICED THAT THE LOWER LEFT RUDDER PULLEY WAS APPROXIMATELY 1/4" HIGHER THEN THE RIGHT PULLEY. UPON REMOVAL OF THE PULLEY, THE BEARING AND RACE WAS FROZENSDR YENA201902170080Not Reported · malfunctionedFLT 821, HDN-LGB. RUDDER FELT HEAVY DURING FLT CONTROL CK BUT MOVED NORMALLY, WHILE LEVELING AT 340, A/C EXPERIENCED SIDE LOAD AND ROLL CONSISTENT W/ YAW DAMPER FAIL, NO ECAMS NOTED, RUDDER CENTERED IN CRUISE FLT TRIM L 1.5 AT TIME OF EVENT, NOW L 0.4, FL 340,SDR DXTA2019021322016Actuator · out of limitsDURING TAKEOFF AND CLIMB COPILOTS RIGHT OUT BOARD PEDAL COULD NOT BE MOVED. WITH AUTO PILOT AND YAW DAMP OFF FROM COPILOTS SIDE RIGHT RUDDER (OUTBOARD PEDAL) COULD NOT BE MOVED. FROM PILOT SIDE INFLIGHT WITH AUTO PILOT AND YAW DAMP OFF RIGHT PEDAL COULD WHEN PSDR DALA2019021200918Bracket · crackedCAPTAIN SIDE RUDDER PEDAL BRACKET ASSY CRACKED. CONTACT PLANNING TO ATTACH EM 2720-01088-0701. REPLACED CAPT'S RUDDER PEDAL BRACKET ASSY. PER AMDS W/C 2720-10188-0701. (LP0941511)SDR RAIA201902020002Pressure Switch · failedRUDDER SYSTEM 1-2 INOP EICAS WITH AP DISCONNECT PARTIAL REVERSIONARY LANDING. ENERGIZED THE AIRCRAFT WITH HYD POWER, SELECTED RUDDER 1 & 2 ON, CYCLED RUDDER 15 TIMES, RUDDER SYSTEM 1-2 INOP MESSAGE DID NOT DISPLAY. DEFERRED YAW DAMPENER. R&R BOTH RUDDER PRESSUSDR DALA2019012200398Pushrod · corrodedCORROSION ON RUDDER LIMITER PUSHROD P/N NAS354-4-270. RUDDER LIMITER PUSHROD P/N NAS354-4-270 WAS REPLACED PER AMM 27-23-02-420-801 AND WAS ADJUSTED PER AMM 27-26-01-820-801. (LP# 0912831)SDR 2019FA0000014Control Cable · obstructedDURING A PRELIMINARY INSPECTION, LOCATED AT REPAIR STATION. IT WAS FOUND TO HAVE THE RT RUDDER CABLE, IN THE TAIL CONE, ROUTED UP AGAINST THE AIR CONDITIONER BRACKET AND WIRE BUNDLE ASSEMBLY POSITIVE TERMINAL FOR THE AIR CONDITIONER SYSTEM LOCATED IN THE RT AFSDR AALA201812289003Control Servo · excess playEXCESSIVE PLAY IN THE RUDDER CONTROL SERVO, BLUE SYSTEM. REPLACED THE RUDDER CONTROL SERVO IAW AMM 27-24-51.SDR 2018FA0000530Spring · brokenWHILE TAXI FOR TAKE OFF, THE LEFT RUDDER RETURN SPRING P/N 0310196-5 BROKE AT THE FORWARD ATTACHMENT HOOK, CAUSING LOSS OF DIRECTIONAL CONTROL ON THE GROUND AND THE AIRCRAFT TO EXIT THE TAXI WAY INTO THE GRASS MEDIAN. THE AIRCRAFT IS USED FOR TRAINING APPOX. 1SDR DALA2018121107135Fitting · leakingSHIP 9209 - SMKE / FUME - WHILE TAXIING, CABIN BEGAN TO FILL WITH LIGHT/WHISPY WHITE SMOKE. STOPPED WHILE TAXIING. TURNED OFF R A/C SUPPLY SWITCH. WENT NO FURTHER AS WE TAXIED AND PULLED INTO THE GATE. LEFT ENGINE AND APU WERE ONLY ITEMS RUNNING. FOUND HYD FLUSDR 2018FA0000491Control Cable · chafedDURING INSPECTION IT WAS FOUND THAT THE LH AND RH AFT UPPER SECTION OF RUDDER CABLES WERE CHAFED BEYOND LIMITS. IT WAS NOTED THAT THE CHAFING IS HAPPENING AT THE FAIRLEADS/CABLE SUPPORTS. THE CABLE TENSION IS 5 LBS SO THE CABLES LAY ON THE FAIRLEADS, THEREFORESDR ANCF20181226501Servo Control · vibrationRARE VIB WITH NOISE FELT AT COCKPIT, FWD CABIN (INTERMITENTLY). DURING DESCENT FL 260 AP ON AND OFF WITH AIRBRAKES DEPLOYED LIGHT VIB. VIB AT AFT CABIN WAS FELT DURING CRUISE, BUT INITIATING DESCENT THE VIB INCREASED ITS INTENSITY // CORRECTIVE ACTION: NOV 27.SDR V6NA2019012403Torque Tube · corrodedAT SCHEDULED INSPECTION, DISCOVERED RUDDER TORQUE TUBE CORRODED. REPLACED RUDDER TORQUE TUBE WITH NEW.
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