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 A6WA200840364Rudder Pedal · inoperativeNO DIRECTIONAL CONTROL ON TAKEOFF WITH RUDDER PEDALS. ABORTED TAKEOFF. AIRSPEED NOT REGISTERED. BRAKE TEMPS 4,3,2,4. PERFORMED TAXI TEST WITH CREW ASSISTANCE IAW 09-20-00 AT 60 KNOTS. NO DEFECTS NOTED. A/C GOOD FOR SERVICE. (K)Apr 27, 2008 · N411ZW · Cndair CL6002B19SDR CALA0800362Support Bracket · crackedFIRST OFFICER RUDDER PEDAL ASSY, SUPPORT SHAFT BRACKET CRACKED. FABRICATED NEW 69-15295-3 RUDDER PEDDLE BRACKET PER BAC DWG 69-15295.Apr 25, 2008 · N19638 · Boeing 737524SDR ZZDA2008095Control Quadrant · brokenCAPTAIN'S FOOT PEDAL ADJUSTMENT BROKE LOOSE AND PEDALS NOT AT FULL EXTENSION WITH NO ADJUSTMENT BACK AVAILABLE. REMOVED & REPLACED RUDDER PEDAL ADJUSTMENT QUADRANT ASSEMBLY. CHECKS GOOD IAW MM 27-21.Apr 24, 2008 · N943AT · Boeing 717200SDR SWIA200819878Rod End · corrodedRUDDER II ROD ENDS HAVE SURFACE CORROSION. (FOUND AT C-CHECK) REPLACED UPPER AND LOWER RUDDER II CONTROL ROD ENDS IAW AMM 27-21-02 Apr 21, 2008 · N301YV · Emb EMB120ERSDR KL13037Bellcrank · crackedRUDDER BELLCRANK FOUND DEFORMED AND CRACKED AT RUDDER TORQUE TUBE ATTACHMENT.Apr 14, 2008 · N787KL · Swrngn SA227BCSDR C2XA08CL046Pressure Switch · faultyCLE FLIGHT 2285 CLE-MHT - THE CREW REPORTED RUDDER SYSTEM NR 1 AND NR 2 INOP, AND RUDDER YAW DAMP INOP MESSAGES ILLUMINATED ON THE ECIAS DISPLAY. AN EMERGENCY WAS DECLARED AND THE A/C LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NRApr 7, 2008 · N11137 · Emb EMB145XRSDR CHQA200800072Pressure Switch · inoperativeFLIGHT 5284, STL TO BDL, DURING CRUISE AT FL340, THE CREW RECEIVED A RUDDER SYS 1-2 INOP EICAS MESSAGE, FOLLOWED BY AUTOPILOT AND YAW DAMPER FAIL. THE QRH WAS FOLLOWED AND THE RUDDER 2 BUTTON WAS RELEASED WHICH THEN RESTORED POWER TO THE RUDDER 1 SYSTEM. THEApr 4, 2008 · N380SK · Emb EMB135KLSDR AALA200800695Module · failedAUA INFLIGHT T2106/22MAR CCS TO MIA - CREW REPORTED SMOKE IN COCKPIT. LANDED AUA WITHOUT INCIDENT. FOUND RUDDER TRIM MODULE FAILED DURING FLIGHT. REPLACED RUDDER TRIM MODULE AND INSPECTED WIRING HARNESSES AND COCKPIT SYSTEMS. SYSTEM GROUND CHECKED NORMAL OMar 22, 2008 · N70072 · Airbus A300B4605RSDR UPS08M52082Arm · damagedINSPECTION TYPE:2C 4 RUDDER PEDAL ARM ASSEMBLIES REQUIRE NDT FOR PREVIOUSLY DRILLED LOCK FASTENER HOLES. REMOVED LOCK FASTENER, PERFORMED FP INSPECTION, NO CRACKS NOTED, APPLIED ALODINE TO HOLES, INSTALLED HLT334-6-22 FASTENERS AND HL386-6 COLLARS AND MARKED Mar 21, 2008 · N256UP · Doug MD11FSDR A6WA200840224Control System · malfunctionedON TAKEOFF ROLL, FULL RUDDER DEFLECTION UNABLE TO MAINTAIN CENTERLINE. ABORTED TAKEOFF AT APPROXIMATELY 60 KNOTS, MAX BTMS READING = 2. CROSSWING ABOUT 10 KNOTS. OPS CHECK OF NWS IAW 32-51-00. OP CHECK GOOD. PERFORMED OPS CHECK OF RUDDER CONTROL SYSTEM IAMar 20, 2008 · N453AW · Cndair CL6002B19SDR QXEA200800296Power Supply · intermittentPDX- FLIGHT 2594 (PDX-BIL). ON TAKEOFF ROLL RECEIVED A "CONFIG RUDDER" WARNING. RUDDER TRIM WAS SHOWING CENTERED AND IN THE GREEN. "TAKEOFF CONFIG OK" WAS DISPLAYED AT THE START OF THE TAKEOFF ROLL. RETURNED TO THE FIELD AND ACCOMPLISHED A UNEVENTFUL LANDINMar 14, 2008 · N602QX · Cndair CL6002C10SDR WGEA200800047Rudder · out of adjustAIRCRAFT REQUIRES 100 PERCENT RWD AT 252 KTS, WITH 16 PERCENT LEFT RUDDER. REFERENCE WORK ORDER 1602, NR-00001. PER TSR 27-030508G, REV C. AIRCRAFT IS WITHIN SPECIFICATION AND NO FURTHER MAINTENANCE ACTION IS REQUIRED AT THIS TIME ON STATED CONDITION.Mar 13, 2008 · N163DJ · Eclips ECLIPSEEA500SDR CA080317009Rudder Bar · cracked(CAN) PILOT NOTED LT PILOTS RUDDER PEDAL WAS NOT IN IT`S CORRECT POSITION. THE RUDDER BAR WHICH IS A WELDMENT WAS FOUND TO BE CRACKED AT THE ATTACHMENT POST FOR THE LT RUDDER PEDAL.Mar 2, 2008 · Cessna 152SDR DXTA20082909B-Nut · looseAT THROTTLE ADVANCE FOR T/O, AT 75 PERCENT N1 HAD ABRUPT FULL RT RUDDER DEFLECTION. OPERATED BOTH ENGINES AND PERFORMED FUNCTIONAL TEST OF RUDDER BIAS SYSTEM, OPS CHECKS NORMAL. NO RUDDER DEFLECTION NOTED AND NO AIR LEAKS NOTED UNDER EACH ENGINE PYLON AREA. BMar 2, 2008 · N875QS · Raythn HAWKER800XPSDR 2008UALA01143Pcu · leakingON PREFLIGHT, FOUND FLUID LEAKING DOWN RIGHT SIDE OF TAILCONE. FOUND INTERNAL HYD FAILURE OF LT RUDDER PCU. REPLACED LT RUDDER PCU. Mar 2, 2008 · N544UA · Boeing 757222SDR 2008UALA01167Pdu · malfunctionedA/C REQUIRES 4 UNITS R RUDDER TRIM, A-S 255 IAS FL370 CRUISE 4.0 RWD. REPLACED RUDDER RATIO CHANGER, PREVIOUSLY REPLACED TE FLAP PDU CONTROL VALVE OUTBD CHECK VALVE ADJUSTED RIG OF RUDDER RATIO CHANGER, RUDDER RIG FOUND TO BE OUT OF LIMITS ADJUSTED POGO ROD OFeb 29, 2008 · N553UA · Boeing 757222SDR DXTA20082889Computer · faultyYD FAIL UPPER B CAS MESSAGE DISPLAYED WHILE CLIMBING THROUGH APPROX FL240. COULD NOT VERIFY DISCREPANCY AT THIS TIME. DUE TO PRIOR HISTORY, REMOVED SUSPECTED FAULTY YSAC COMPUTER. PERFORMED OPS CHECKS WITH NO DISCREPANCIES NOTED AT THIS TIME. ALL WORK PERFFeb 19, 2008 · N946QS · Cessna 750SDR DL764080246Rudder Pedal · out of adjustDURING FLT CONTROL CHECK, F/O RT RUDDER PEDAL HITS THE AFT STOP COVER. RTB ADJ RUDDER PEDALS TO NML CONFIG. RAN PEDALS FULL LT AND RT PEDAL DOES NOT HIT THE SHROUD. PEDALS ARE EVEN ALL POS AND IND NML.Feb 19, 2008 · N832MH · Boeing 767432ERSDR A6WA200840100Rudder · malfunctionedUNCOMMANDED FULL RT RUDDER AT HIGH ALTITUDE CLIMB 280 KNOTS WITH YAW DAMPER ENGAGED, STEPPED ON RUDDER TO CORRECT AND TRIMMED BACK IN POSITION, PROCEEDED NORMALLY. (K)Feb 15, 2008 · N417AW · Cndair CL6002B19SDR UPS08651670Yaw Damper · inoperativeA/C YAWED CONTINUOUSLY LT AND RT AT HIGH SPEEDS. T/S FOUND M509 RT UPR YAW DAMPER SERVO LVDT RESISTANCE VALUE ABNORMAL AND M317 O/B SPOILER NR 12 PCA LVDT PIN 8 SHROTED TO CASING. BOTH M509 RT UPPER YAW DAMPER SERVO AND M317 O/B SPOILER NR 12 PCA REPLACED. YFeb 14, 2008 · N315UP · Boeing 76734AFSDR CA080214001Rudder Pedal · corroded(CAN) IT HAS BEEN NOTICED THAT ALTHOUGH THIS AREA IS LUBRICATED IAW THE MFG MAINT SCHEDULE WITH LPS2, THIS AREA CONTINUOUSLY CORRODES TO THE POINT THAT IT AFFECTS THE POSITIONING OF THE RUDDER PEDALS. (TC NR 20080214001)Feb 12, 2008 · Diamon DA20C1SDR CA080211013Pcu · malfunctioned(CAN) TASK NR RJ2-27-900-714 FOR THE BACKLASH AND FUNCTIONAL CHECK OF RUDDER CONTROL SYS WAS CARRIED OUT ON THIS AC DURING A HEAVY MAINT CHECK. TEST RESULT PARAMETERS WERE FOUND BEYOND LIMITS. FURTHER INVESTIGATION DURING RECTIFICATION LEAD TO THE DISCOVERY OFFeb 10, 2008 · Cndair CL6002B19SDR HALA0800037Bearing · frozenRUDDER PEDAL BINDING LEFT AND RIGHT ON BOTH CAPT'S AND FO'S RUDDER PEDALS. RIGHT RUDDER NOT RETURNING TO NEUTRAL. TROUBLESHOT PER FIM 27-21-00, FIG 107. FOUND BEARING FROZEN ON FEEL, CENTERING, AND TRIM MECHANISM (IPC 27-21-10-01, ITEM 408). REMOVED AND REFeb 9, 2008 · N598HA · Boeing 767332SDR CA080211001Transducer · failed(CAN) THE AC WAS DISPATCHED ON A MEDIVAC FLIGHT AND UPON STARTING THE TAKEOFF ROLL AN UNCOMMANDED RUDDER INPUT WAS FELT BY THE PILOTS. THE AC RETURNED TO THE HANGER WHERE MAINT BEGAN TO TROUBLESHOOT THE PROBLEM. IT WAS DISCOVERED THAT THE LT RUDDER BOOST TRANSFeb 7, 2008 · Beech 300BEECHSDR DXTA200802826Actuator · inoperativeRUDDER LIMIT FAIL B 89 PERCENT. REPLACED LOWER LIMIT (B) ACTUATOR IAW CH 27-23-00. OPS CHECK GOOD.Feb 3, 2008 · N903QS · Cessna 750SDR SWIA200819171Actuator · malfunctionedFLT 3677 - AFTER DEPARTURE, THE RUDDER PEDALS FELT STIFF. REPLACED BLUE SYSTEM RUDDER ACTUATOR. OPS CHECKS GOOD IAW 27-22-00, PN 388140-1003, SN/OFF 4995.Jan 31, 2008 · N568SW · Emb EMB120ERSDR DXTA200802812Actuator · malfunctionedON CLIMB OUT, PASSING THROUGH 10,000 FT AND 250 KIAS , RUDDER LIMIT FAIL-B CAS MESSAGE LIMIT WAS FAILED AT 26 PERCENT. TROUBLESHOT: REPLACED ACTUATOR A IAW MM CHAP 27-23-00 OPS CHECK GOOD.Jan 30, 2008 · N986QS · Cessna 750SDR CA080128004Control Cable · stuck(CAN) DURING INSP, THE LT RUDDER CABLE WAS FOUND SNAGGED ON THE WATER RUDDER CABLE PULLEY GUARD. (TC NR 20080128004)Jan 28, 2008 · Airtrc AT802ASDR MASA200800065Pcu · malfunctionedASH FLT 9700 PHX-PHX - RT RUDDER INPUT UNCOMMANDED ON LANDING WITH THE AUTO PILOT OFF. REMOVED AND REPLACED PCU RUDDER.Jan 24, 2008 · N17358 · Cndair CL6002B19SDR C2XA08IA030Pressure Switch · inoperativeIAH - FLIGHT 2191, THE CREW REPORTED THAT THE AIRCRAFT VEERD SHARP LEFT, AND RECEIVED A RUDDER 1&2 INOP EICAS MESSAGE. THE AIRCRAFT RETURNED TO THE GATE WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE RUDDER 1&2 PRESSURE SWITCHES, OPERATIONALLY CHJan 22, 2008 · N12934 · Emb EMB145EPSDR PNSA080103Unknown · malfunctionedON CLIMBOUT REALIZED HAD LITTLE IF NO LT RUDDER. DECLARED EMERGENCY BECAUSE OF FLIGHT CONTROL MALFUNCTION. LANDING WAS UNEVENTFUL.Jan 18, 2008 · N41NE · Swrngn SA227ACSDR YENA2008007Servo Control · excess playFLT 501, EWR-FLL, ON DESCENT LATERAL VIBRATION FELT IN COCKPIT, APPLICATION OF RUDDER INPUT CAUSED VIBRATION TO CEASE. VIBRATION FELT FROM 340 TO -100. ACCOMPLISHED AMM TASK 05-50-00-02 (AIRFRAME VIBRATION SURVEY) FOUND EXCESSIVE PLAY ON RUDDER TRAILING EDGEJan 18, 2008 · N558JB · Airbus A320232SDR SIMA200802108Pressure Switch · malfunctionedON FLIGHT 3509 CREW REPORTED YAW DAMPER FAIL AND AUTO PILOT KICKED OFF DURING CLIMB FOLLOWED BY RUDDER SYSTEM 1/2 INOP EICAS MESSAGE. CREW ELECTED TO RETURN TO DFW FOR MAINTENANCE DECLARED EMERGENCY PRIOR TO LANDING. AIRCRAFT REMOVED FROM SERVICE. REMOVED AJan 18, 2008 · N928AE · Emb EMB145LRSDR DXTA200802751Limiter · malfunctionedRUD LIMIT FAIL A AMBER CAS ILLUMINATED AFTER TAKEOFF AT APPROX 15000 FT. LIMIT WAS 22 PERCENT. R & R RUDDER TRAVEL LIMITERS IAW MM CH 27-23-00. OPS CK GOOD IAW CE 27-20-00Jan 8, 2008 · N919QS · Cessna 750SDR 2008UALA00128Transducer · faultyRUDDER RATIO LIGHT ILLUM IN FLIGHT. EICAS MSG RUDDER RATIO DISPLAYED. REPLACED LEFT ELEC HYD PUMP CONTROL PRESS SWITCH AND INSPECTED CONNECTOR, NO DEFECTS FOUND. REPLACED RUDDER RATIO LVDT. OP CHECK NORMAL, OSCILATION CHECK NORMAL.Jan 7, 2008 · N671UA · Boeing 767322SDR DXTA200702736Limiter · failedTHE AMBER (RUDDER LIMIT FAIL B) CAS MESSAGE ILLUMINATED IN FLIGHT AND REMAINED ON WITH SHUTDOWN. RUDDER LIMITER FAILED AT 67 PERCENT. REMOVED & REPLACED T.R. SWITCH.Jan 1, 2008 · N998QS · Cessna 750SDR SWIA200719020Actuator · malfunctionedFLT 5436 - UNABLE TO DEPRESS RIGHT RUDDER PEDAL ON TAKEOFF. REPLACED BLUE ACTUATOR WITH A SERVICEABLE UNIT. OPS CHECKS GOOD. NO LEAKS NOTED, PN: 308190-1003, SN OFF: 0614. Dec 30, 2007 · N289YV · Emb EMB120ERSDR 20071227209Pressure Switch · corrodedDURING TAKEOFF ROLL THE RUDDER PEDALS KICKED HARD LT CAUSING LOSS OF DIRECTIONAL CONTROL. ABORTED TAKEOFF AND TAXIED TO RAMP. MX PERFORMED A RUDDER BOOST TEST AND NOTED DURING RUN-UP THAT THE RT ENGINE RUDDER BOOST DID NOT RESPOND. THE LT ENGINE RUN-UP CAUSDec 27, 2007 · N209CM · Beech B200SDR DXTA200702715Accumulator · leakingRUD STBY SYS FAIL (AMBER) ILLUMINATED 2 TIMES DURING FLIGHT. FOUND RUDDER STBY ACCUMULATOR GAGE TO BE LEAKING INTERNALLY. REMOVED AND REPLACED GAGE WITH NEW IAW CE-750 M/M CHAP 29-10-04. SERVICED ACCUMULATOR TO 2000 PSI OAW CE-750 M/M CHAP 12-10-16. NO LEAKS Dec 25, 2007 · N941QS · Cessna 750SDR MASA200700918Switch · out of positionASH FLT 2925 ICT- OVERNIGHT, RT RUDDER TRIM WAS INTERMITTENT. MX FOUND THE TRIM SWITCH OFF CENTER AND REPOSITIONED IT AND THE SYSTEM OP CHECKED GOOD.Dec 25, 2007 · N17275 · Cndair CL6002B19SDR C2XA07ON048Pressure Switch · faultyFLT 7652 - LAX TO LAX - FLIGHT CREW REPORTED RUDDER OVERBOOST ON CLIMBOUT OF ONT. MX PERSONNEL REMOVED AND REPLACED NR 1 RUDDER PRESSURE SWITCH. OPERATIONALLY CHECKED GOOD AND A/C WAS RETURNED FOR SERVICE IN AIRWORTHY CONDITIONS.Dec 17, 2007 · N17185 · Emb EMB145XRSDR QXEA200701879Trim Panel · failedLWS - FLIGHT 2027 - WHILE BOARDING PASSENGERS WITH GROUND POWER ON, SMOKE STARTED TO COME FROM THE TRIM INDICATOR PANEL IN THE COCKPIT. POWER TURNED OFF AND BATTERIES TURNED OFF. SMOKE STOPPED. NO INDICATION OF FIRE. FOUND CIRCUIT BREAKER POPPED. MAINTENDec 12, 2007 · N349PH · Dhav DHC8202SDR SIMA200734802Switch · failedRUDDER SYS 1 AND 2 INOP DURING FLIGHT. REMOVED AND REPLACED NUMBER 2 RUDDER PRESSURE SWITCH IAW EMB 145 AMM 27-23-04. OPS CHECK GOOD IAW EMB 145 AMM 27-23-00, AIRCRAFT RETURNED TO SERVICE.Dec 12, 2007 · N690AE · Emb EMB145LRSDR CA071212012Screw · missing(CAN) SL 550-27-14 FOUND 2 SCREWS, P/N MS350206-228, MISSING FROM PILOTS LT RUDDER SUPPORT BRACKET AND 2 LOOSE SCREWS P/N MS 350206-228 ON THE CO-PILOTS RT RUDDER SUPPORT BRACKET.CARRY OUT ACCOMPLISHMENT INSTRUCTIONS PARAGRAPH 1THRU 4. (TC NR 20071212012)Dec 11, 2007 · Cessna 550SDR DHLA200700078Rudder Control · malfunctionedLOWER RUDDER MOVED ON ITS OWN FAR TO THE LEFT AS COMPARED WITH THE UPPER RUDDER AS SEEN ON THE RUDDER POSITION INDICATORS DURING TAKEOFF ROLL. ACFT PULLED TO THE LEFT, UPPER RUDDER IND FAR RT. TRANSFERRED RUDDER POS IND TO DMI 31029 PER MEL 27-8 CAT C DDD12-Dec 8, 2007 · N750DH · Boeing 7272M7SDR FDKA200712378Rudder Control · malfunctionedFDM 6040 FLL (0851 PHX LCL) - RUDDER SYSTEM 1 INOP. MX RESET SYSTEM, NO FURTHER ACTION REQUIRED.Dec 4, 2007 · N856MJ · Emb EMB145LRSDR SIMA200734103Rudder Control · malfunctionedEMERGENCY DECLARED, RUDDER 1/2 INOP IN FLIGHT.Dec 4, 2007 · N667GB · Emb EMB145LRSDR SIMA200734104Pressure Switch · failedEMERGENCY DECLARED, RUDDER 1/2 INOP IN FLIGHT LANDED SAFELY. REMOVED AND REPLACED NR 1 RUDDER PRESSURE SWITCH IAW EMB 145 AMM 27-23-04. OPS CHECK AND LEAK CHECK GOOD. NO DEFECTS NOTED. AIRCRAFT RETURN TO SERVICE.Dec 4, 2007 · N664MS · Emb EMB145LRSDR SIMA200733908Pressure Switch · malfunctionedAIR TURN BACK FOR RUDDER SYSTEM 2 INOP MESSAGE. AIRCRAFT WAS BEING REPOSITIONED TO XNA. REMOVED AND REPLACED NR 2 RUDDER PRESSURE SWITCH IAW AMM27-73-04. LEAK AND OPS CHECK GOOD IAW AMM 27-23-00. AIRCRAFT RETURNED TO SERVICE.Dec 3, 2007 · N661JA · Emb EMB145LRSDR FDKA200712373Control Cable · bindingFDM 6032 MCO-ORF (1809 PHX LCL) - RUDDER PEDALS BINDING. MX REMOVED AND REPLACED CABLES.Dec 2, 2007 · N855MJ · Emb EMB145LR
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