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 MASA200602638Fadec · malfunctionedASH 7120 CHS. RUDDER HARD OVER PROTECTION MESSAGE. MX RESET FADEC WITH CREW MESSAGE CLEARED.Nov 28, 2006 · N855MJ · Emb EMB145LRSDR MASA200602639Warning System · malfunctionedASH CAE. RTL FAULT STATUS. MX RESET.Nov 28, 2006 · N512MJ · Cndair CL6002C10SDR MASA200602635Warning System · malfunctionedASH 2606 IAH. RUDDER LIMIT FAULT STATUS. CONTRACT MX PERFORMED SPOST2. NO FURTHER DEFECTS NOTED.Nov 27, 2006 · N922FJ · Cndair CL6002D24SDR 2007FA0000143Control Cable · brokenRUDDER CONTROL CABLE BRAKES DURING FLIGHT TRAINING WHILE PERFORMING FORWARD SLIP MANEUVER ON FINAL APPROACH. INITIAL INSPECTION SHOWS CABLE BROKE JUST FORWARD OF TERMINAL END AT THE LOWER BELL CRANK. FURTHER INSPECTION REVEALED THE CAUSE OF FAILURE TO BE CORNov 26, 2006 · N1653V · Cessna 172MSDR MASA200602617Warning System · malfunctionedASH 2671 CLT. RUDDER LIMIT FAULT. MX PERFORMED SPOST. NO FURTHER DEFECTS NOTED.Nov 24, 2006 · N912FJ · Cndair CL6002D24SDR SIMA200633106Warning System · malfunctionedAT 80 KNOTS RECEIVED RUDDER SYSTEM 1 INOP MESSAGE, ABORTED TAKEOFF. RUDDER SYSTEM 2 INOP MESSAGE. AOM CHECKLIST FOLLOWED AND BOTH SYSTEMS RESET. ACCOMPLISHED EMB FIM TASK 27-22-00-810-804-A WITH NO DEFECTS NOTED. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT BNov 22, 2006 · N829AE · Emb EMB135KLSDR CA061120006Rudder Pedal · cracked(CAN) DURING REPLACEMENT OF THE FUEL SHUTOFF VALVE THE LT FRONT RUDDER/BRAKE PEDAL WAS FOUND CRACKED BETWEEN THE BRAKE PEDAL UPRIGHT AND THE OB PEDAL HINGE. THE DEFECT APPEARS TO BE CAUSED BY BRAKING FORCES APPLIED BY THE FLIGHT INSTRUCTOR IN THE REAR SEAT, THNov 20, 2006 · Bbavia 7GCBCSDR ZB0R20060003Bar · crackedDURING PROGRESSIVE INSPECTION, FOUND PILOT LT RUDDER BAR CROSS-OVER JOINT CRACKED AT WELD.Nov 20, 2006 · N15143 · Piper PA28R200SDR 4517711182006Force Sensor · malfunctionedON TAKEOFF ROLL, ABOVE 80 KTS, ACFT KICKED HARD LT THEN RT, ALSO HAD THE GREEN RB FLASH ON. MAINTENANCE PERFORMED T/S AND SUSPECTS THE FORCE SENSORS MOUNTED ON THE RUDDER PEDAL ASSEMBLY. REPLACED LT AND RT FORCE SENSORS AND SB 45-22-6 INCORPORATED. OPS CHECKNov 18, 2006 · N431FX · Lear 45LEARSDR 06FDEA04017Unknown · malfunctionedON APPROACH, BEFORE AND AFTER SLATS EXT, RUDDER PEDALS WERE EXTREMELY LOOSE. TRAVEL BETWEEN PEDALS WAS - 3-4" EACH WITH NO RUDDER MOVEMENT. ALSO NO RESISTANCE IN THE FIRST 3-4" OF PEDAL TRAVEL. VERIFIED 3-4" OF RUDDER PEDAL MOVEMENT BEFORE ANY MOVEMENT ONov 15, 2006 · N586FE · Doug MD11SDR MASA200602573Warning System · malfunctionedASH 2946 PHX. RUD LIMIT FAULT. PERFORMED SPOST/CPOST, OPS CK GOOD.Nov 13, 2006 · N931LR · Cndair CL6002D24SDR MASA200602548Control Unit · malfunctionedASH 7117 IAD. RUDDER LIMIT FAULT STATUS MESSAGE. MX RESET SSCU AND PERFORMED SYSTEM TEST WITH NO FAULTS NOTED.Nov 8, 2006 · N506MJ · Cndair CL6002C10SDR MASA200602540Warning System · malfunctionedASH 7200 RDU. RUDDER LIMIT FAULT STATUS MESSAGE. MX RESET THE SYSTEM.Nov 6, 2006 · N502MJ · Cndair CL6002C10SDR FDKA200611315Indicator · malfunctionedFDM 6201 JFK-SYR (1155 PHX LCL). RUDDER DEFLECTION TO THE LEFT IS ONLY 9 DEGREES. MX REMOVED AND REPLACED PFCS.Nov 5, 2006 · N805LR · Dhav DHC8101SDR MASA200602528Control Unit · malfunctionedASH 7225 RDU. RUDDER LIMIT STATUS MESSAGE. MX RESET SSCU SYSTEM. FAULT CLEARED. SYSTEM OPERATED NORMALLY.Nov 3, 2006 · N512MJ · Cndair CL6002C10SDR MASA200602526Transmitter · defectiveASH 7260 ORD. PILOT REPORTED THAT THE RUDDER INDICATION WAS NOT SHOWING FULL TRAVEL TO EITHER THE LEFT OR RIGHT SIDE. MX REPLACED THE POSITION TRANSMITTER.Nov 3, 2006 · N75991 · Cndair CL6002B19SDR CA061102004Rudder · stiff(CAN) AIRCRAFT WAS BEING TAXIED TO THE RAMP FROM THE HANGER. THE PILOT NOTICED THAT THE RUDDER CONTROLS FELT STIFF. THE PILOT DECIDED TO RETURN TO THE HANGER AND ADVISE MAINTENANCE. THE AIRCRAFT IS BEING EXAMINED AT THIS TIME AND WILL UP-DATE THIS SDR WHEN A Nov 2, 2006 · Cessna 208BSDR MASA200602517Warning System · malfunctionedASH 2643 CLT. CAPTAIN REPORTED RUDDER LIMIT FAULT STATUS MESSAGE. MX RESET SYSTEM AND OPS CHECKED GOOD.Oct 31, 2006 · N927LR · Cndair CL6002D24SDR MASA200602515Warning System · malfunctionedASH 2643 CLT. RUDDER LIMIT FAULT. MX PERFORMED SPOST. NO FURTHER DEFECTS NOTED.Oct 31, 2006 · N927LR · Cndair CL6002D24SDR 2006FA0001131Rudder Pedal · looseUPON INVESTIGATING LOOSE RUDDER PEDALS, THE ASSEMBLY WAS DISASSEMBLED AND IT WAS NOTED THAT THE SHAFT HAD BEEN DOUBLE DRILLED WITH THE HOLES OVERLAPING. THE AIRCRAFT WAS CERTIFICATED JANUARY 2002; THE AIRCRAFT NOW HAS 1015.4 HOURS, TIME IN SERVICE. (K)Oct 30, 2006 · N304E · Beech A36SDR MASA200602500Warning System · malfunctionedASH 2946 SEA. RUDDER CONFIG WARNING MESSAGE ON T/O ROLL. SYSTEM RESET NO FURTHER ACTION REQUIRED.Oct 28, 2006 · N907FJ · Cndair CL6002D24SDR DXTA200601688Yaw Damper · inoperativeYAW DAMP IN DESCENT YAWS AIRCRAFT FROM SIDE TO SIDE. TURNED OFF AND BACK ON. THE UNCOMMANDED YAWING CONTINUED. TURNED OFF AND FLEW WITHOUT IT. REMOVED AND REPLACED YAW DAMPER IAW F-2000 M/M 22-105. OPERATIONAL TEST GOOD.Oct 28, 2006 · N298QS · Amd FALCON2000SDR MASA200602491Warning System · malfunctionedASH 7486 ORD. PILOT REPORTED RUDDER LIMIT FAULT STATUS MSG. MX RESET SYSTEM, OPS GOOD.Oct 26, 2006 · N512MJ · Cndair CL6002C10SDR SWIA200617356Control Unit · jammedRUDDER PEDALS JAMMED ON LANDING ROLL. REPLACED THE RUDDER PCU IAW MM 27-22-01 AND RII 27-300-1006. OPERATIONAL CHECKS GOOD, SN/OFF 0121.Oct 25, 2006 · N580SW · Emb EMB120ERSDR CA070731004Bellcrank · cracked(CAN) BELLCRANK HAS CRACKS ADJACENT TO AN3 BOLT HOLES. (TC NR 20070731004)Oct 23, 2006 · Cessna A185ESDR CA061027001Control Cable · misrouted(CAN) WHILE CARRYING OUT A 100 HOUR INSPECTION IT WAS DISCOVERED THAT WHEN TENSION WAS PLACED ON THE RT RUDDER PEDAL, IT WAS RUBBING AGAINST THE RT AILERON DIRECT CABLE PULLEY CLEVIS PULLEY GUARD IN THE FORWARD TUNNEL SECTION OF THE FUSELAGE. THE RUBBING WAS SOct 23, 2006 · Cessna 172MSDR C2XA06IA167Switch · inoperativeMCI - FLT 2468, THE CREW REPORTED THE RUDDER 1 & 2 INOP DURING CLIMB, CRUISE, & DESCENT. THE AIRCRAFT LANDED AT MCI WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO RUDDER SYSTEM PRESSURE SWITCH, OPERATIONALLY CHECKED WITH NO DEFECTS, ANOct 20, 2006 · N14179 · Emb EMB145XRSDR MASA200602458Circuit Card · not seatedASH 2697 MDT. RUDDER LIMIT FAULT/SPOILER-STAB FAULT STATUS MESSAGES. MX RESEATED 1A AND 2A IAPS IOC CARDS. NO FURTHER DEFECTS NOTED.Oct 18, 2006 · N915FJ · Cndair CL6002D24SDR DXTA200601669Actuator · bindingRUDDER PEDAL HAVE BINDING/SHUTTERING FEEL DURING SLOW/LOW SPEED TAXI. ON TAKEOFF ROLL PEDALS FEEL STIFF AS IF YAW DAMPER WERE ENGAGED. REMOVED RUDDER BIAS ACTUATOR AND INSTALLED NEW ACTUATOR IAW THE CITATION 560XL MM CHAPTER 27-20-05. PERFORMED OPERATIONAL Oct 18, 2006 · N690QS · Cessna 560XLSDR DXTA200601698Control Switch · stickingAFTER TAKEOFF AND DURING CLIMB, THE AIRCRAFT FELT VERY SLOPPY IN THE YAW AXIS. THE AIRCRAFT WOULD NOT COORDINATE TURNS. ATTEMPTED (S) TURNS AT FL340 AND WE GOT FULL BALL DEFLECTION. TRIED BOTH FGS NO CHANGE. UPPER RUDDER CHANNEL WOULD NOT CHANGE FROM B TO Oct 9, 2006 · N978QS · Cessna 750SDR UIEA200600274Powerpack · wornATB:DUE TO MEDIUM/LIGHT VIBRATION IN RUDDER PEDALS. FLIGHT CONTROL VALVES OFF BY 1. YAW DAMPER OFF NO HELP, A/P OFF NO CHANGES. FOUND UPPER RUDDER HYD RETRACT LINE "B" NUT AND UNION LOOSE BY 2.5 TURN WITH HEAVY LEAK. TIGHTEN BACK IAW MM 27-21-15 OPS AND LEAK COct 7, 2006 · N408MC · Boeing 74747UFSDR MASA200602396Warning System · malfunctionedASH 2819 PHX. RUDDER LIMIT FAULT STATUS MESSAGE. MX RESET THE SYSTEM.Oct 5, 2006 · N942LR · Cndair CL6002D24SDR DL76L060800Bearing · bindingRUDDER PEDALS BINDING ON PRE FLT CHECK. FOUND BEARING IN RUDDER FEEL/CENTURING UNIT FROZEN. REPLACED SAME AND CHECKED OUT RUDDER FEEL AND CENTERING PER AMM 27-21-10-712-098 RUDDER AND PEDALS OPERATE NORMAL WITH FULL TRAVEL.Sep 30, 2006 · N174DN · Boeing 767332SDR EIA2006233Connector · defectiveAFTER TAKEOFF, HAD A RUDDER RATIO LIGHT CAME ON, RETURNED TO BLOCK. REPLACED SUSPECT ELECTRICAL CONNECTOR, SYSTEM OPS CHECK GOOD ON GROUND. PITOT STATIC CHECK C/W.Sep 29, 2006 · N471EV · Boeing 747273CSDR ACE092706Pulley · frozenPILOT REPORTED, THOUGHT THAT THE RUDDER HAD EXPERIENCED A -FREEZING- CONDITION WHILE IN FLIGHT (PROBLEM HAD RESOLVED ITSELF PRIOR TO LANDING). MAINTENANCE INSPECTED A KNOWN PROBLEM AREA UNDER THE CARGO FLOOR INSIDE THE CARGO DOOR (FS 505 WL 88) AT THE RUDDER Sep 27, 2006 · N111AX · Beech 1900CSDR HNAA0600118Regulator · malfunctionedON CLIMB OUT RUDDER FULL PRESSURE AND RUDDER PRESSURE CAUTION LIGHTS ILLUMINATED AND EXTINGUISHED CAME ON FOR APROXIMATELY ONE MINUTE MORE AND EXTINGUISHED AGAIN. REPLACED RUDDER DUAL PRESSURE REGULATOR PART INFORMATION TO FOLLOW.Sep 26, 2006 · N337EN · Dhav DHC8311SDR MASA200602351Pressure Switch · malfunctionedASH 7069 DEN. RUDDER PRESS CAUTION ON PUSHBACK. MX REMOVED AND REPLACED NR 1 AND NR 2 PRESSURE SWITCHES.Sep 24, 2006 · N454YV · Dhav DHC8202SDR MASA200602332Warning System · malfunctionedASH 2946 SEA. RUDDER LIMIT FAULT STATUS. CONTRACT MX PERFORMED SPOST1. NO FURTHER DEFECTS NOTED.Sep 23, 2006 · N906FJ · Cndair CL6002D24SDR MASA200602304Warning System · malfunctionedASH 2686 MCI. RTL STATUS MESSAGE. MX PERFORMED SPOST 1/2. NO FURTHER DEFECTS NOTED.Sep 17, 2006 · N916FJ · Cndair CL6002D24SDR FDKA200609261Trim System · malfunctionedFDM 6168 JFK. CREW REPORTED THE RUDDER TRIM INOP. MX PERFORMED OPERATIONAL CHECKS OF RUDDER TRIM SYSTEM. NO DEFECTS NOTED.Sep 15, 2006 · N804LR · Dhav DHC8102SDR HALA0600711Limiter · failedBTB: FWD PITOT FAIL LEVEL 1 NO TAKEOFF ALERT. REMOVED AND REPLACED RUDDER LIMITER PITOT IAW AMM 34-1 1-02. OPS CHECK OK. LEAK CHECK OK IAW AMM 34-11-00.Sep 13, 2006 · N477HA · Boeing 767300SDR MASA200602271Control Unit · malfunctionedASH 2931 PHX. CAPTAIN REPORTED A SPOILER/STAB, PITCH FEEL, RUDDER LIMIT AND SLAT 1/2 SPEED STATUS MESSAGES. MX REMOVED AND REPLACED SFECU NR 2.Sep 12, 2006 · N939LR · Cndair CL6002D24SDR MALA060552Control Unit · malfunctionedRUDDER LIMITER ILLUMINATED INFLIGHT ABOVE 170 KTS. CAUTION CLEARED WHEN CABIN PRESSURIZED AT 3000 FT. REMOVED AND REPLACED AIR DATA ACCUSATION UNIT. ALL CHECKS GOOD.Sep 12, 2006 · N520XJ · Bac AVRO146RJ85ASDR MASA200602262Warning System · malfunctionedASH 2653 CLT. RUDDER LIMIT FAULT STATUS MSG AND SSCU 1 STATUS MSG. MX RESET THE SYSTEM.Sep 10, 2006 · N906FJ · Cndair CL6002D24SDR MASA200602234Unknown · malfunctionedASH 2710 PHX. RUDDER LIMIT FAULT AT GATE. MOC RESET THE SYSTEM WITH CREW.Sep 6, 2006 · N917FJ · Cndair CL6002D24SDR MASA200602219Pressure Switch · failedASH 7186 IAD. RUDDER SYSTEM 1 & 2 FAIL IN FLIGHT. MX R2 THE RUDDER SYSTEM 2 PRESSURE SWITCH.Sep 2, 2006 · N858MJ · Emb EMB145LRSDR UPS06647836Servo · malfunctionedUNCOMMANDED RUDDER YAW TWICE IN FLIGHT. R & R LT & RT YAW DAMPER SERVO IAW MM 22-21-02-4. LEAK CHECK RIGHT & LEFT YAW DAMPER SERVO PER TECH SERVICES. R&R RIGHT YAW DAMPER MODULE ASSY IAW MM 22-21-04-2. ALSO R&R LEFT YAW DAMPER MODULE ASSY AS PRECAUTIONARY. PAug 30, 2006 · N306UP · Boeing 767300SDR MASA200602204Warning System · malfunctionedASH 2779 PHX - RUDDER LIMIT FAULT. MX PERFORMED SPOST. NO FURTHER DEFECTS NOTED.Aug 30, 2006 · N916FJ · Cndair CL6002D24SDR CWQR200625Control Cable · brokenDURING A ROUTINE MAINTENANCE VISIT, OPERATOR REQUESTED WE INSPECT THE AFT ELEVATOR TRIM CABLES. UPON INSPECTION WE FOUND ABOUT .333 OF THE CABLE STRANDS BROKEN. TOOK CABLE TENSIONS, FOUND TO BE WITHIN LIMITS AND CABLE WAS CENTERED ON THE PULLEYS. THE CABLE APPAug 29, 2006 · N646QS · Cessna 560XLSDR FDKA200608230Servo · malfunctionedFDM 5066 PHF. CREW REPORTED YAW DAMP/ AUTO PILOT FAIL MESSAGE. MX REMOVED AND REPLACED RUDDER SERVO.Aug 25, 2006 · N828MJ · Emb EMB145LR
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