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.

SDR SIMA2018112616006Pressure Switch · failedRUDDER SYS 1-2 INOP OVER 180 KNOTS. DID NOT HAVE AN OVERWEIGHT LANDING.-C/A-REF FIM 27-22-00-810-804-A, RPL'D SYS 2 RUDDER PERSSURE SW IN REF TO AMM 27-23-04 & OPS CHKED RUDDER SYS OK IN REF TO AMM 27-23-00. NO FAULT & LEAK FOUND.Nov 16, 2018 · N909AE · Emb EMB145LRSDR SIMA2018112016004Pressure Switch · inoperativeRUD DER SYS 1-2 INOP OVER 180 KNOTS.EMERGENCY DECLARED DID NOT HAVE AN OVERWEIGHT LANDING.FLT CONT.-C/A-REF FIM 27-22-00-810-804-A, RPL'D SYS 2 RUDDER PERSSURE SW IN REF TO / AMM 27-23-04 & OPS CHKED RUDDER SYS OK IN REF TO AMM 27-23-00. NO FAULT & LEAK FOUNDNov 16, 2018 · N922AE · Emb EMB145LRSDR F3LA2018103100475Control Cable · corrodedDISCREPANCY: REFERENCE N/R 2168N511 RUDDER LT OUTBOARD CABLE RUSTED LOCATED UNDER DUMMY BEAM Y503.2. CORRECTIVE ACTION: CABLE FWD CONNECTION REMOVED AND REPLACED WITH NEW CABLE IAW AMM 27-21-61 PB401 AND AMM 27-21-820-002-A./END/Oct 24, 2018 · N202FR · Airbus A320214SDR YADA2018103000179Control Cable · corrodedRUDDER CABLE FOUND FRAYED AND SEVERELY CORRODED AT A ROUTINE INSPECTION.Oct 24, 2018 · N113A · Beech 1900CSDR F3LA2018101800457Not Reported · malfunctionedABORTED TAKE-OFF FOR RUDDER JAM/DIFFICULT DIRECTIONAL CONTROL. THE AIRCRAFT WAS GROUNDED DUE TO THE EVENT. MX PERFORMED YAW DAMP SYS TEST AMM 22-63-00-710-001-A, ADIRS SYS TEST AMM 34-14-00-740-004-A, AFS TEST AMM 22-91-00-710-001-A, AUTO CHANGEOVER FUNCTION AOct 14, 2018 · N201FR · Airbus A320214SDR HNAA2018101100254Pressure Switch · malfunctionedDURING T/O ROLL RUD SYS 2 INOP DISPLAYED ON EICAS AT APPROX 95 KTS. R&R NR 2 RUDDER PRESSURE SWITCH IAW AMM 27-23-04. OPS AND LEAK CHECK GOOD. OK FOR SERVICE.Oct 10, 2018 · N633AE · Emb EMB145LRSDR HNAA2018101100253Pressure Switch · malfunctionedAT 400 FEET AGL AT TAKEOFF YD FAILED AND RUD SYS 1/2 INOP CAUTION MSG PRESENTED. RAN QRH WHEN RUD SYS 2 DESELECTED RUD SYS 1 CAME BACK ON LINE. YD RE-ENGAGE AND IT STAYED ONLINE. T/S IN REF TO FIM 27-22-00-810-804-A FOUND RUD SYS 2 PRESS SW FAIL. R&R RUD SYSTEOct 10, 2018 · N602AE · Emb EMB145LRSDR JGVR20181009001Torque Tube · migratedWHILE ATTEMPTING TO ADJUST CABLE TENSIONS FOR A LOW CABLE TENSION SQUAWK, THE TECHNICIAN RAN OUT OF ADJUSTMENT IN THE TURN BARREL. UPON FURTHER INVESTIGATION IT WAS NOTED THAT THE RUDDER TORQUE TUBE P/N 500-15623-001 HAD MIGRATED OUT OF THE LT BEARING COVER P/Oct 9, 2018 · N225AS · Emb EMB500SDR CALA2018100802070Motor · malfunctionedDURING FLT CONTROL RUDDER STANDBY CHECK WITH HYDRAULIC "A" SWITCH ON LOW PRESSURE LIGHT IS ON. R/R STBY RUDDER SOV MOTOR IAW 27-21-94...OPS AND LEAK CK GOOD -END-Oct 8, 2018 · N39726 · Boeing 737724SDR AALA2018091179004Control Servo · failedCREW DECLARED AN EMERGENCY DUE TO A RUDDER FLUTTER DURING CLIMB OUT. ALL INDICATIONS WERE NORMAL. CREW SLOWED THE AIRCRAFT AS REQUIRED. FLIGHT CONTINUED TO DESTINATION AND LANDED WITHOUT FURTHER INCIDENT. THE AIRCRAFT WAS GROUNDED. THE RUDDER FLUTTER STASep 6, 2018 · N818AW · Airbus A319132SDR DXTA2018090401375Shutoff Valve · faultyDURING TAKE OFF 10KTS BEEFIER V1 AIRCRAFT PULLED HARD RIGHT, CORRECTED WITH FULL LEFT RUDDER MAINTAINED CONTROL, ROTATED MADE NORMAL CLIMB, CRUISE, DESCENT, LANDING OK. REMOVED AND REPLACED RUDDER BIAS ACTUATOR AND RUDDER BIAS CONTROL VALVE OPS AND LEAK CHECKSAug 31, 2018 · N662QS · Cessna 560XLSDR HALA2018082600403Warning System · false activationAIR TURN BACK, AFTER TAKEOFF RUDDER RATIO EICAS MESSAGE DISPLAYED WITH RUDDER RATIO DISCRETE LIGHT ILLUMINATED. PERFORMED FIM TASK 27-09 FAULT TREE 814. NO FAULTS NOTED. RUDDER OPS NORMAL. OK FOR SVC.Aug 26, 2018 · N580HA · Boeing 76733ASDR AALA2018082989027Rudder · vibrationVIOLENT UNCOMMANDED YAW DURING TAKEOFF ROLL. MAINTENANCE ACCOMPLISHED AN EVALUATION, CONFIRMS EVENT, AND ACCOMPLISHED SATISFACTORY RUDDER SYSTEM TESTS IAW AMM 27-21-00.Aug 24, 2018 · N994NN · Boeing 737823SDR AALA201808163006Module · defectiveAIR RETURN ORD ACCOUNT FLIGHT CONTROL ISSUE. EMERGENCY WAS DECLARED AND FLIGHT LANDED OVERWEIGHT WITHOUT INCIDENT. UNABLE TO CONTROL RUDDER, TRIM STUCK 2-5 UNITS TO RIGHT, UNABLE TO CENTER, LANDED 5 UNITS TO THE LEFT. THE AIRCRAFT WAS GROUNDED. REPLACED AILAug 13, 2018 · N342PM · Boeing 737823SDR AALA2018081659020Actuator · defectiveEMERGENCY WAS DECLARED AND FLIGHT LANDED WITHOUT INCIDENT. UNABLE TO CONTROL RUDDER, TRIM STUCK 2-5 UNITS TO RIGHT, UNABLE TO CENTER, LANDED 5 UNITS TO THE LEFT. THE AIRCRAFT WAS GROUNDED. REPLACED AILERON AND RUDDER TRIM CONTROL MODULE IAW AMM 27-11-94, ANDAug 12, 2018 · N342PM · Boeing 737823SDR HALA2018080900366Warning Light · false activationRUDDER RATIO EICAS MESSAGE AND DISCREET LIGHT ILLUMINATED DURING TAKE OFF ROLL, AND REMAINED ON FOR THE DURATION OF FLIGHT. PERFORMED FIM 27-21-804, 27-09 F/T 803, & 27-00 FT 814 SYSTEM OK, OK TO CONTINUE.Aug 8, 2018 · N594HA · Boeing 767332SDR HALA0218080800361Warning Light · false activationDURING TAKEOFF AT ROTATION, AMBER EICAS FOR RUDDER RATION ILLUMINATED. COMPLIED WITH QRH AND CONTINUED. COMPLIED WITH FIM 27-21 F/T 804, 27-09 F/T 803, & 27-09 F/T 814 THE SYSTEM OK, OK TO CONTINUE.Aug 5, 2018 · N594HA · Boeing 767332SDR TQOA2019F00035Bearing · destroyedPILOT REPORTED THAT HE HAD DIFFICULTY MOVING THE RUDDER SO THE PILOT DECLARED AN EMERGENCY LANDING AND LANDING SAFELY. WHILE INSPECTING THE RUDDER SYSTEM, THE BOTTOM BEARING WAS FOUND TO BE IN PIECES WHICH CAUSE EXCESSIVE PLAY WHEN RUDDER WAS IN MOTION.Jul 30, 2018 · N959PA · Dhav DHC3SDR BQVD2018080100001Bar · brokenPILOTS LEFT "RUDDER BAR WELD ASSEMBLY (CESSNA IPC DESCRIPTION)" BROKE (CRACKED) ALLOWING THE VERTICAL RUDDER PEDAL POST TO SEPARATE FROM THE HORIZONTAL CROSS OVER TUBE. THE BREAK WAS LOCATED ON THE HORIZONTAL PORTION BELOW THE VERTICAL POST.Jul 27, 2018 · N5088L · Cessna 152SDR HALA2018072600404Warning System · false activationETOPS SIGNIFICANT SYSTEM - RUDDER RATIO ON STEADY AT 1500 FT AND 160 KTS. RESET RUDDER RATIO CIRCUIT BREAKER. PERFORMED RUDDER RATIO CHANGER MODULE BITE PROCEDURE PER FIM 27-09 FT 814 NO FAULTS NOTED OK FOR SERVICE.Jul 25, 2018 · N580HA · Boeing 76733ASDR 9JLA2018080919551Position Sensor · defectiveDURING FLIGHT CONTROL CHECKS, PRIOR TO FLIGHT, IT WAS DISCOVERED THAT THE UPPER RUDDER CHANNEL B FAILED THE PRE-FLIGHT CHECKS. THE UPPER RUDDER POSITION WOULD STAY FULLY DEFLECTED UNTIL RESET. THE MAINTENANCE FOUND THE CHANNEL B RUDDER POSITION SENSOR DEFECTIJul 15, 2018 · N119RM · Cessna 750SDR SWIA2018073044881Control Panel · failedRUDDER TRIM WENT FULL NOSE LEFT ONCE WE GOT TO CRUISE. (FLT 2975) FO: 7/16/18 CLOSED / REMOVED AND REPLACED AILERON RUDDER TRIM CONTROL PANEL IAW AMM. OPS CHECK GOOD AT THIS TIME.Jul 15, 2018 · N703SK · Cndair CL6002C10SDR AALA2018070659001Actuator · inoperativeRUDDER TRIM ISSUE. EMERGENCY DECLARED, AND LANDED. THE AIRCRAFT WAS GROUNDED. NUMEROUS EICAS MESSAGES DISPLAYED AFTER TAKEOFF. CONFIG SYS, THRUST ASYM COMP, AND RUDDER TRIM ALL WERE INOPERATIVE. INSTALLED RUDDER TRIM ACTUATOR IAW AMM 27-21-07. OPS CHECKEJul 2, 2018 · N789AN · Boeing 777223SDR HALA2018062700311Warning Light · false activationAFTER TAKE OFF, RUDDER RATIO MESSAGE DISPLAYED ON EICAS, WITH ASSOCIATED DISCRETE LIGHT ILLUMINATED. HYDRAULIC PRESSURE NORMAL. PREFORMED FIM 27-09 FAULT TREE 814, RUDDER RATIO CHANGER MODULE BITE. NO FAULTS NOTED. OK TO CONTINUE.Jun 26, 2018 · N594HA · Boeing 767332SDR DALA2018062804240Rod · corrodedCORROSION ON ROD P/N NAS354-4-270 AND ROD-END P/N XREP3F4S181. ROD AND ROD-END 2EA WERE REPLACED PER AMM 27-26-01-420-801. ROD AND ROD-END 2EA WERE ADJUSTED PER AMM 27-26-01-820-801 FUNCTIONAL TEST OF THE RUDDER THROW LIMITER WAS PERFORMED PER MD90 AMM 27-26-0Jun 24, 2018 · N921DN · Doug MD9030SDR DXTA2018062000194Support Rod · brokenDURING THE TAIL CONE REMOVAL FOR ELEVATOR CONTROL CABLE INSPECTION FOUND THE LT ROD ASSY FOR THE RUDDER TORQUE TUBE DAMAGED. PN AFFECTED WAS 3836-2.Jun 20, 2018 · N360QS · Emb EMB505SDR QXEA2018061500219Spring · separatedEXCESSIVE LEFT RUDDER TRIM NEEDED TO CENTER BALL AT APPROACH SPEED, RUDDER TRIM NEEDLE WAS DEFLECTED TO THE FIRST NOTCH TO MAINTAIN COORDINATED FLIGHT. LANDING UNEVENTFUL. REMOVED FROM SERVICE. FOUND THE RUDDER FEEL TRIM UNIT RETURN SPRING SWAGED COLLAR SEJun 12, 2018 · N451QX · Bombdr DHC8402SDR SIMA201806065001Switch · malfunctionedRUDDER SYS 1 - 2 INOPERATIVE MESSAGE ILLUMINATED ON EICAS DURING FLIGHT. REMOVED AND REPLACED THE NR 2 SWITCH IAW MM 27-23-04. OPS CHECKED GOOD, NO MESSAGE ON EICAS.Jun 5, 2018 · N844AE · Emb EMB135KLSDR DBCA2018060640002Coupler · failedCREW CALLED SAYING THEY HAVE A COMPUTER ISSUE WITH RUDDER DEFLECTION NOTIFICATION ON GROUND DURING PREFLIGHT INSPECTION. DETERMINED THE POSITION TRANSMITTER FLEXIBLE COUPLER WAS UNSERVICEABLE. REPLACED THE FLEXIBLE COUPLER WITH NEW. OPS CHECKED GOOD.Jun 4, 2018 · N504W · Cessna 750SDR 2018FA0000182Cable · brokenRIGHT RUDDER PEDAL ADJUSTMENT CHANNEL THAT CONNECTS COCKPIT RUDDER PEDAL TO RUDDER CABLE WAS FOUND BROKEN AT FWD END OF ADJUSTMENT TRACK, CAUSING THE RT RUDDER CABLE TO BECOME DISCONNECTED FROM RUDDER PEDAL. APPEARED AS THOUGH RUDDER PEDAL ADJUSTMENT PIN WAS May 31, 2018 · N6215P · Thrush S2RH80SDR RJEF20180522001Limiter · inoperativeDURING TAXI, THE AIRCRAFT HAD A FAILURE MESSAGE FOR THE AUTO FLT RUDDER TRV LIMIT SYS AND RETURNED TO THE GATE. MAINTENANCE PERFORMED A FAULT ANALYSIS IAW TSM 22-61-00-810-803, REPLACED THE TRAVEL LIMITATION UNIT IAW AMM 27-23-51 PB401, PERFORMED AN OPS TESMay 19, 2018 · N479TA · Airbus A319132SDR F3LA2018052100340Feel Unit · malfunctionedLEFT RUDDER PEDAL FEELS TO BE BINDING ON LANDING. REMOVED AND REPLACED ARTIFICIAL FEEL UNIT IAW AMM 27-23-41, PB401. OPS CHECKED GOOD. NO BINDING NOTED.May 18, 2018 · N948FR · Airbus A319112SDR HALA208051700237Module · malfunctionedRUDDER RATIO EICAS AND DISCRETE LIGHT. PERFORMED FIM 27-21 F/T 804. RESET LEFT AND RIGHT RUDDER CHANGE MODULES. OPERATED SYSTEM, NO MESSAGES. OK FOR SERVICE.May 16, 2018 · N594HA · Boeing 767332SDR ASOA201805114029Hinge Fitting · failedTHE CREW REPORTED A LOW FREQUENCY VIBRATION THROUGH THE AIRFRAME. THE AIRCRAFT LANDED AT JAN WITHOUT INCIDENT. MX INSPECTED THE AIRCRAFT AND FOUND THAT ALL OF THE RUDDER TWO HINGE FITTINGS TO BE DAMAGED WITH THE UPPER FITTING TO BE SHEARED. REMOVED AND REPLMay 11, 2018 · N13979 · Emb EMB145LRSDR QXEA2018042500161Handle · stuckFIRST OFFICER`S RUDDER PEDAL ADJUSTMENT HANDLE WILL NOT TURN, RUDDER PEDALS WILL NOT TRAVEL FORE OR AFT. REMOVED FROM SERVICE. PERFORMED A GVI FOR FOD, NO FOD OR DEFECTS NOTED. RELEASED THE FO'S ADJUSTMENT HANDLE, VERIFIED FULL RUDDER PEDAL ADJUSTMENT TRApr 24, 2018 · N439QX · Bombdr DHC8402SDR 2018FA0000319Rudder Pedal · bindingTHE AIRCRAFT WAS BEING TURNED HARD TO THE RIGHT DURING GROUND TAXI WHEN THE LEFT RUDDER PEDAL OVER CENTERED ON THE BRAKE MASTER CYLINDER ACTUATING SHAFT. THIS CAUSED THE RUDDER SYSTEM TO BE LOCKED IN THE HARD RIGHT POSITION UNTIL THE LEFT PEDAL WAS MANUALLY PApr 19, 2018 · N176US · Tecnam P2006TSDR SIMA2018042019005Pressure Switch · inoperativeRUDDER OVERBOOST AFTER TAKE OFF. RETURNED TO DEPARTURE. PERFORMED TROUBLESHOOTING IAW FIM 27-22-10, FOUND THE NR 1 RUDDER PRESSURE SWITCH INOPERATIVE. REMOVED AND REPLACED THE PRESSURE SWITCH IAW AMM 27-23-04. OPS AND LEAK CHECKED GOOD.Apr 19, 2018 · N837AE · Emb EMB135KLSDR IPXA2018041628640Module · faultedAIR TURNBACK. AFTER TAKEOFF, THE RUDDER RATIO EICAS ILLUMINATED. FOUND THE RIGHT RUDDER RATIO CHANGER MODULE FAULTED. R & R THE MODULE IAW MM 27-09-00. OPS CHECKED GOOD IAW MM 27-21-00.Apr 12, 2018 · N323UP · Boeing 76734AFSDR IPXA2018041628639Warning Message · false activationAIR TURNBACK. RUDDER RATIO EICAS MESSAGE ENROUTE. PERFORMED FIM 27-09-00, FIG 106B, BLOCKS 1, 2, 3, 4, 5, & 6, CHECKED GOOD. PERFORMED A TEST OF THE RUDDER RATIO SYS IAW AMM 27-20-00. OPS CHECKED GOOD, NO FAULTS FOUND.Apr 12, 2018 · N302UP · Boeing 76734AFSDR ASAA2018040224116Warning System · false activationAUTO FLT RUD TRM LIM 2 ECAM GROUNDED - YES. PERFORMED RESET AND OPS TEST PER AMM 22-61-00 OPS CHECK OK. NO FAULT NOTED. THIS CLEARS MDDR 54070. MEL LIST UPDATED. MCC NOTIFIEDApr 2, 2018 · N281VA · Airbus A320214SDR HYIA20180316002Control Cable · brokenPILOT REPORTED THE LEFT RUDDER DOES NOT MOVE, A SNAP WAS HEARD WHEN MAKING A LEFT TURN. MAINTENANCE INSPECTED AND FOUND THE FORWARD LEFT RUDDER CABLE BROKEN NEAR THE FORWARD PULLEY. LAST VISUAL INSPECTION OF AREA OCCURRED 134.8 HOURS PRIOR TO FAILURE. CABLE Mar 14, 2018 · N290CA · Cessna 402CSDR JR2R20180313248Line · out of adjustRUDDER ACCUMULATOR /TRANSFER CYLINDER LWR NITROGEN LINE CHAFED INTO FRAME. REPAIRED RT FRAME AT RUDDER ACCUMULATOR CYLINDER IAW SRM 53-03 FIG4.Mar 13, 2018 · N426NV · Doug MD83SDR RU3A20180309010Pcb · looseRUDDER BOOST OFF LIGHT ILLUMINATED. RUNNING THE ABNORMAL CHECKLIST MADE NO DIFFERANCE. DISCOVERED LOOSE RELAY AND SOCKET. REPLACED LOGIC RELAY PCB. RUDDER BOOST LAMPS WORKING CORRECTLY. NO FURTHER ACTION REQUIRED.Mar 9, 2018 · N76 · Beech 300BEECHSDR N6WA2018030401Rvdt · out of rigREJECTED TAKE OFF AT 60 KNOTS BECAUSE OF ERRATIC NOSE WHEEL STEERING WITH RUDDER PEDAL. PERFORMED RIGGING OF RUDDER COMMAND RVDT IAW AMM 32-51-05, OPS CHECKED GOOD, PERFORMED TAXI CHECK IAW AMM 9-20-00, TAXI CHECKED GOOD.Mar 4, 2018 · N162GJ · Cndair CL6002C10SDR HALA2018022600049Module · malfunctionedDURING CLIMB OUT, HAD A RUDDER RATIO EICAS MESSAGE WITH ASSOCIATED DISCRETE LIGHT ILLUMINATED. HYDRAULIC SYSTEM PRESSURE ALL NORMAL. DIVERTED, PERFORMED A BITE TEST OF RUDDER RATIO CHANGER MODULE IAW FIM 27-09 814. NO FAULTS NOTED. OK FOR SERVICE.Feb 23, 2018 · N580HA · Boeing 76733ASDR JJBA20180219002Pressure Switch · failedRUDDER 1 - 2 INOPERATIVE ON EICAS. DIVERTED. R & R SYSTEM 2 PRESSURE SWITCH IAW FIM AMM. OPS CHECKED SAT.Feb 19, 2018 · N13161 · Emb EMB145XRSDR ASOA201802087008Skin · dentedTYS A/C WAS IN A A-CHECK STATUS WHEN INSPECTION FOUND THE NR 2 RUDDER WITH 3 DISTINCT DENTS ON THE TRAILING EDGE. MAINTENANCE REMOVED AND REPLACED RUDDER 2 IAW WITH TASK CARD 538087, IPC 27-21-02 FIG 02B ITEM 1. OPS CHECK GOOD AND WAS RELEASED.Feb 8, 2018 · N27200 · Emb EMB145XRSDR CA180207023Solenoid Valve · failed(CAN) AIRCRAFT REQUIRED LEFT RUDDER INPUT IN FLIGHT AND ON GROUND. MORE THAN NORMAL RUDDER TRIM REQUIRED IN FLIGHT. CORRESPONDING RUDDER BOOST SOLENOID VALVE FOUND FAILED IN OPEN POSITION CAUSING RUDDER BOOST TO ACTUATE SLIGHTLY DURING ALL PHASES OF OPERATIOFeb 2, 2018 · Beech B200SDR HSYA201802060001Cable Assy · brokenAFTER TAKEOFF, THE PILOT EXPERIENCED DIFFICULTY TURNING RIGHT TO THE ASSIGNED HEADING, FULL RIGHT RUDDER AND TRIM WAS NEEDED TO MAINTAIN CONTROL. DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE WITHOUT INCIDENT. MAINTENANCE INSPECTED THE ACFT AND FOUND THATJan 19, 2018 · N977FE · Cessna 208BSDR 2018FA0000040Bellcrank · looseRUDDER TORQUE TUBE, BELL CRANK ATTACHMENT RIVETS AND BELL CRANK SHOWING SIGNS OF BEING LOOSE. ATTACH RIVETS ARE SMOKING.Jan 16, 2018 · N153QS · Dhav DHC6*
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