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 UALA2011121406865Handle · out of adjustCAPTS RUDDER ADJUSTMENT CATCHES AT FULL FWD POSITION THEN MOVES OKAY. MAINT TEXT: PROBLEM HAPPENS AT FULL FORWARD ADJ WHEN TURNING TO BRING PEDALS AFT. ADJUSTED RUDDER PEDAL HANDLE, OPS CHECKS NORMAL.Dec 13, 2011 · N589UA · Boeing 757222SDR HALA2011121100578Warning Light · false activationETOPS SIGNIFICANT SYS - RUDDER RATIO LIGHT ILLUMINATED IN FLIGHT. EICAS MESSAGE "RUDDER RATIO" DISPLAYED. PERFORMED FIM 27-21-00. NO FAULTS NOTED. ACFT IS OK TO CONTINUE. ACFT IS OK FOR SERVICE.Dec 11, 2011 · N580HA · Boeing 76733ASDR CA111212015Module · bypassing(CAN) DURING TAXI WHEN FLAPS EXTENDED HYD A SYS PRESS WENT TO 1500 PSI & BOTH A SYS LOW PRESS LIGHTS CAME ON. UPON REMOVAL OF RUDDER MODULE FOUND TEFLON BACK UP RING OUT OF PLACE & WOUND UP INSIDE THE LINE FITTING PORT. REPAIR VENDOR REQUESTED TO SEND STRIP Dec 8, 2011 · Boeing 727260SDR ASOA2011120800013Pressure Switch · inoperativeDURING CLIMB THE CREW REPORTED A RUDDER OVERBOOST INDICATION ON THE EICAS DISPLAY. THE ACFT RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT WHERE MX REPLACED THE RUDDER NR 1 PRESSURE SWITCH, PERFORMED OPS CHECKS AND CLEARED THE DISCREPANCY.Dec 8, 2011 · N21197 · Emb EMB145XRSDR A6WA201141060Rudder · bindingDURING FLIGHT CONTROL CHECK OF RUDDER, LOUD CLICKING NOISE HEARD LT AND RT, SLIGHT BINDING FELT. RETORQUED PIVIOT BOLTS, NO FIX, ITEM PLACED ON DIL FOR 500 FLT HOURS IAW SUP 06-037, REF DIL 203798/13.Dec 3, 2011 · N446AW · Cndair CL6002B19SDR UALA2011120506677Actuator · malfunctionedCAPTAIN'S RUDDER PEDAL SPRING IS NOT RETURNING PEDALS TO OUT POSITION. REPLACED CAPTAIN'S PEDAL POSITION ACTUATOR. CHECKED OPERATION FOUND GOOD.Dec 2, 2011 · N849UA · Airbus A319131SDR UALA2011120206629Actuator · failedCAPTAIN'S & FIRST OFFICER'S RUDDER PEDALS WILL NOT RELEASE AND EXTEND WHEN EXTENDED. REPLACED CAPTAIN'S RUDDER PEDAL ADJUSTER ACTUATOR.Dec 2, 2011 · N854UA · Airbus A319131SDR UALA2011113006589Rudder · vibrationRUDDER VIBRATION ISSUE.Nov 30, 2011 · N489UA · Airbus A320232SDR UALA2011112706528Buffer · stuckCAPTAIN'S RUDDER PEDAL ADJUSTMENT RESET IS STICKING. REPLACED CAPTAIN RUDDER PEDAL POSITION BUFFER, OPS CHECKED OKAY.Nov 27, 2011 · N494UA · Airbus A320232SDR UALA2011112706480Buffer · faultyF/O RUDDER PEDALS DO NOT SELF ADJUST OUT. REPLACED RUDDER PEDAL POSITION BUFFER, OPS CHECKED OKAY.Nov 27, 2011 · N494UA · Airbus A320232SDR UALA2011112706474Snubber · faultedCAPTAIN'S RUDDER PEDALS DO NOT AUTO ADJUST OUT. LUBED ACTUATOR PEDALS OPS CHECK NORMAL. PROBLEM RECURRED. REPLACED SNUBBER.Nov 27, 2011 · N840UA · Airbus A319131SDR UALA2011112706514Buffer · failedF/O RUDDER PEDALS DON`T ADJUST PROPERLY. REPLACED F/O RUDDER PEDAL ADJUSTMENT BUFFER, OPS CHECKED OKAY.Nov 25, 2011 · N482UA · Airbus A320232SDR HALA2011112400539Warning Message · illuminatedETOPS SIGNIFICANT SYS - RUDDER RATIO EICAS MESSAGE DISPLAYED IN FLIGHT. PERFORMED BITE PROCEDURES OF RUDDER RATIO CONTROL MODULE, IAW FIM 27-09-00/101 FIG 106B. NO FAULTS AT THIS TIME.Nov 24, 2011 · N580HA · Boeing 76733ASDR UALA2011112306453Actuator · faultedTROUBLESHOT RUDDER TRIM PROBLEM & FOUND TRIM OUT BY 1.25 INCH AT RUDDER INDEX PLATE. LIMIT .010 PER AMM ITEM NR 9A & NR 9B. ITEM LIMIT SHOULD REFLECT .100 PER AMM. ADJUSTED RUDDER PCA PER MM. REPLACED PCA ON ACCOUNT OF MAKING LOUD NOISE WHEN POWERED, REPLANov 23, 2011 · N653UA · Boeing 767322SDR UALA2011112306448Actuator · failedCAPTAIN'S RUDDER PEDALS STUCK OR JAMMED. REMOVED & REPLACED PEDAL ADJUSTER ACTUATOR, OPS CHECKED OKAY.Nov 22, 2011 · N847UA · Airbus A319131SDR QXEA2011112201239Rudder · frozenON FINAL APPROACH AT 4000 FT. -5 DEG C IN ICING CONDITIONS FOUND RUDDER FROZEN IN PLACE. CREW TRIED TO MOVE RUDDER AND IT REQUIRED FORCEFUL PULL TO BREAK FREE. THEN NORMAL. LANDING UNEVENTFUL. RUDDER CABLE RUNS WERE INSPECTED, KICK PANELS AROUND RUDDER PEDNov 18, 2011 · N437QX · Bombdr DHC8402SDR QXEA2011112201238Summing Unit · malfunctionedIN LEVEL CRUISE FL250, POWER REDUCED AND RT RUDDER APPLIED. RUDDER PEDAL DEFLECTED A SMALL DISTANCE AND THEN STOPPED. FELT LIKE A LIMIT TO TRAVEL. PFCS SHOWED ABOUT A HALF A NEEDLE WIDTH OF DEFLECTION. RUDDER TRIM FELT LIKE IT WAS WORKING PROPERLY. CREW Nov 18, 2011 · N436QX · Bombdr DHC8402SDR QXEA2011112201244Feel Unit · malfunctionedGOING THRU 11,000 FT AFTER SELECTING THE AUTO PILOT OFF AND LEVELING WHILE LEFT TURN AT 10,000 FT THE LEFT RUDDER WAS JAMMED. AFTER APPLYING PRESSURE THE JAM BROKE FREE. RUDDER RESPONDED AND EXCESSIVE LEFT YAW. RUDDER REMIANED NORMAL FOR REMAINDER OF FLIGHT WNov 18, 2011 · N429QX · Bombdr DHC8402SDR UALA2011112106404Buffer · defectiveCAPT RUDDER PEDALS FAIL TO MOVE FORWARD FROM MOST EXTENDED POSITION AS WELL AS MOST. REPLACED RUDDER PEDAL BUFFER, OPS CHECK GOOD.Nov 17, 2011 · N480UA · Airbus A320232SDR QXEA2011112101236Rudder · bindingWHILE F/O FLYING ON FINAL AND CONFIGURED, NOTED THE RIGHT RUDDER STUCK. WHILE APPLYING MORE PRESSURE IT BROKE FREE AND HAD NORMAL RUDDER MOVEMENT FOR REMAINDER OF FLIGHT. BINDING STARTED WITH AUTOPILOT ON AND CONTINUED AFTER IT WAS SELECTED OFF, LANDING UNENov 17, 2011 · N443QX · Bombdr DHC8402SDR HALA2011111600527Warning Light · false activationETOPS SIGNIFICANT SYS - BTB EICAS RUDDER RATIO LIGHT ON AFTER ENGINE START. RESET LT AND RT RRCM PERFORMED FIM 27-21-00, FIG 104. NO FAULTS NOTED. OK FOR SERVICE.Nov 16, 2011 · N594HA · Boeing 767332SDR UALA2011111606280Buffer · defectiveF-O RUDDER PEDALS FAIL TO SPRING FORWARD FROM MOST EVERY POSITION FROM A LOCKED POSITION. REPLACED BUFFER PER MM, OPS CHECK GOOD.Nov 15, 2011 · N488UA · Airbus A320232SDR DXTA2011111604793Actuator · contaminatedCAPTAIN`S AND F/O RUDDER PEDALS BECAME INCREASINGLY STIFF AT HIGHER ENGINE POWER SETTINGS. FOUND RUDDER BIAS ACTUATOR CORRODED AND FULL OF WATER. REPLACED ACTUATOR IAW THE MM 27-20-05. OPS CHECKED GOOD.Nov 15, 2011 · N568QS · Cessna 560XLSDR DXTA2011111504789Limiter · failedAT 300' AGL ON DEPARTURE , RUDDER LIMIT FAIL B CAS MESSAGE ILLUMINATED. RUDDER LIMITED TO 79 PERCENT. R & R LOWER RUDDER LIMITER "B" IAW MM 27-23-00. PERFORMED OPS CHECKS IAW MM CH 27-20-00. RUDDER LIMITERS, OPS CHECKED GOOD.Nov 14, 2011 · N978QS · Cessna 750SDR UALA2011111006145Snubber · wornCAPT'S & FO'S RUDDER PEDAL BUFFER IS WORN OUT. REPLACED CAPT SIDE RUDDER PEDAL BUFFER. LUBRICATED F/O SIDE, NO HELP. REPLACED F/O'S RUDDER PEDAL SNUBBER IAW MM, OPS OKAY.Nov 10, 2011 · N415UA · Airbus A320232SDR UALA2011111106175Actuator · faultyF/O RUDDER PEDALS DO NOT MOVE TOWARD PILOT WITHOUT MANUAL ASSISTANCE. REPLACED PEDAL ADJUSTER ACTUATOR, OPS CHECK NORMAL.Nov 10, 2011 · N849UA · Airbus A319131SDR SIMA2011315001Rod End · corrodedFOR FLIGHT 4366 THE DURING UNSCHEDULED MAINTENANCE CHECK FOUND THE AFT RUDDER II LOWER CONTROL SPHERICAL ROD END CORRODED AND SEIZED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RUDDER II PUSH ROD END IAW EMB 145 AMM 27-21-08. PART NUMBENov 9, 2011 · N624AE · Emb EMB145LRSDR NOCA11111Pca · malfunctionedA/C REQUIRES 4 1/2 LEFT RUDDER TRIM FOR STRAIGHT AND LEVEL FLT WITH CONTROL WHEEL AT 0 IN CRUISE AT FL 340 MACH .80. REPLACED ALL 3 RUDDER POWER CONTROL ACTUATOR PER MM 27-21-02 REPLACED RUDDER RATIO CHANGER ACTUATOR PER MM 27-21-15 REPLACED ALL AUTOPILOT SERNov 5, 2011 · N762NA · Boeing 767319SDR UALA2011110406001Actuator · faultyCREW REPORT: CAPT RUDDER PEDDLES DON'T COME FORWARD WHEN TAB IS PULLED. REPLACED CAPT PEDAL ACTUATOR PER AMM. OPERATES NORMALLY.Nov 3, 2011 · N417UA · Airbus A320232SDR UALA2011110305962Actuator · defectiveCAPTAIN'S RUDDER PEDALS WILL NOT MOVE AFT WHEN PULL TO ADJ HANDLE IS MOVED. REPLACED CAPTAIN'S RUDDER PEDAL ACTUATOR AND LUBED IAW MM. OPS CHECK GOOD.Nov 2, 2011 · N425UA · Airbus A320232SDR UALA2011103105890Buffer · defectiveF/O RUDDER PEDALS NOT ADJUSTING PROPERLY. REPLACED -BUFFER- ACTUATOR PEDAL ADJUSTMENT, OPS OK AND RUDDER PEDALS MOVE FREELY WITH FULL RUDDER TRAVEL.Oct 29, 2011 · N444UA · Airbus A320232SDR 2011FA0000716Control Cable · misroutedDURING THE PERFORMANCE OF AN ANNUAL INSPECTION, FOUND THE RT RUDDERVATOR TRIM CONTROL CABLE WAS ROUTED INCORRECTLY AND HAD CUT THROUGH THE RT RUDDERVATOR CONTROL TUBE APPROX 75 PERCENT. THE TUBE ALSO HAS SIGNS OF A CRACK ORIGINATING FROM THE DAMAGED SECTION OOct 28, 2011 · N8367N · Beech V35ASDR CA111028007Pushrod · corroded(CAN) ALUM ROD WAS BEING REMOVED TO REPLACE SOME CORRODED BLIND FASTENERS AT THE LOWER END FITTING (FIXED-END, STEEL FITTING). WHEN IT WAS DISCOVERED THE ALUMINUM TUBE WAS CORRODED APPROX 45 PERCENT AROUND THE CIRCUMFRENCE OF THE ROD, AT THE END OF THE STEEL Oct 27, 2011 · Conaer LA4200SDR UALA2011103105884Lever · faultyCAPT RUDDER ADJ KNOB SLIPS WHEN APPLYING PRESSURE. REPLACED RUDDER PEDAL CRANK LEVER.Oct 27, 2011 · N548UA · Boeing 757222SDR NSVA2011290Console · corrodedDURING HEAVY CHECK, CORROSION NOTED ON BASE OF BOTH RUDDER PEDAL CONSOLES THAT IS BEYOND ALLOWABLE LIMITS.Oct 24, 2011 · N198CJ · Saab 340BSDR HALA2011102300482Warning Message · illuminatedETOPS SIGNIFICANT SYS - RUDDER RATIO EICAS WARNING AFTER ENGINE START. RESET RUDDER RATIO SYS CB G10 CHECKED RRCM TEST NORMAL ALL FOUND TO BE NORMAL. OPS CHECKED NORMAL IAW AMM 27-21-00.Oct 23, 2011 · N580HA · Boeing 76733ASDR ASOA201102018Limiter · false indicationRUDDER LIMITER CAUTION MESSAGE ILLUMINATED AFTER TAKEOFF, COMPLIED WITH QRH. EMERGENCY DECLARED, RETURNED TO DEPARTURE. COMPLIED WITH INSPECTION OF WATER TRAPS, NO MOISTURE FOUND. COMPLIED WITH SPOST 1 & 2, FAULTS CLEARED. COMPLIED WITH OPS OF SPOILER AND Oct 21, 2011 · N317CA · Cndair CL6002C10SDR UALA2011101905658Circuit Breaker · faultyRUDDER RATIO LIGHT ILLUMINATED ON THE GROUND. RUDDER RATIO LIGHT CIRCUIT BREAKER RECYCLED LIGHT WENT OUT. ACCOMPLISHED BYTE TEST PER FIM 27-09-00 BLOCK 106B. FOUND PCA FAULT BALL. AFTER RESET OF PCA BALL ON BOTH LEFT AND RTB RRC ACCOMPLISHED TEST PER MM AOct 18, 2011 · N642UA · Boeing 767322SDR NOCA20111011411Yaw Damper · damagedFIVE UNITS RUDDER TRIM REQUIRED IN NOSE LEFT DIRECTION WHILE IN CRUISE AT FL370 OAT -52 AND LEFT CROSSWIND OF 75 KTS. DURING THIRD ENCOUNTER WITH LIGHT TURBULENCE RUDDER MOVED TO THE RIGHT. RUDDER PEDALS ALSO DISPLAYED TO THE RIGHT. AILERONS COMPENSATED WITOct 11, 2011 · N762NA · Boeing 767319SDR RAIA201110100001Pressure Switch · malfunctionedDURING CLIMB THE FLIGHT CREW GOT A MESSAGE ON EICAS "RUDDER SYSTEM 1 & 2 INOP" "YAW DAMPENER INOP". AIRCRAFT RETURNED TO IAD. MAINTENANCE INSPECTED AND SWAPPED RUDDER PRESSURE SWITCHES NR 1 WITH NR 2 FOR TROUBLESHOOTING AND THEN REMOVED AND REPLACED NR 1 PROct 10, 2011 · N803HK · Emb EMB145EPSDR C2XA11RI161Pressure Switch · faultyFLT 4174 RIC-CREW REPORTED RUDDER SYSTEM NR 1 INOP MESSAGE ON EICAS DURING TAKEOFF ROLL LESS THAN 40 KTS AND ABORTED TAKEOFF WITHOUT INCIDENT. RIC MX REMOVED AND REPLACED RUDDER SYSTEM NR 1 PRESSURE SWITCH IAW EMB-145 AMM 27-23-04 WITH OPERATIONAL CHECK SUCCEOct 5, 2011 · N14204 · Emb EMB145XRSDR UALA2011100505401Servo Valve · failedNO INFC FCC L RUD SERVO CMD, FAULT DURING ADFS TEST. REPLACED LEFT RUDDER ELECTRO HYDRAULIC SERVO VALVE, OPS CHECK OKAY. ACCOMPLISHED CAT III CHECK. ALL OK PER LAX MM. RETURNED AC BACK TO CAT III STATUS.Sep 29, 2011 · N677UA · Boeing 767322SDR NSVA2011247Lug · corrodedRUDDER PEDAL CONSOL ASSY LUGS ARE CORRODED. REMOVED AND INSTALLED NEW CONSOL ASSY PN: 7327200-561.Sep 28, 2011 · N350CJ · Saab 340BSDR NSVA2011246Rudder Pedal · corrodedLT RUDDER PEDAL ASSY P/N 7327200-561 CORRODED. REPLACED ASSY.Sep 26, 2011 · N350CJ · Saab 340BSDR UALA2011092605203Indicator · faultyRUDDER TRIM FAILED TO TRIM IN EITHER DIRECTION. CHECKED RUDDER TRIM AND FOUND ACTUATOR WKG OK, RUDDER TRIM POS INDICATION INOP. EICAS RUDDER TRIM POS OK. INOPED RUDDER TRIM POS INDICATION PER MEL. REPLACED RUDDER TRIM INDICATOR PER MM. OPS CHECKED OK.Sep 25, 2011 · N676UA · Boeing 767322SDR UALA2011092305138Pcu · out of adjustRUDDER TRIM NEEDS 3.5 UNITS LEFT IN LEVEL CRUISE FLT. ADJUSTED RUDDER PCU PER MM.Sep 22, 2011 · N667UA · Boeing 767322SDR UG8A2011092101Attach Fitting · crackedRUDDER TORQUE TUBE TO BELLCRANK ATTACH FLANGE IS CRACKED IN 3 PLACES AROUND THE CIRCUMFERENCE OF THE TUBE. REPLACED TORQUE TUBE AND INSTALLED CORRECTLY.Sep 20, 2011 · N911UM · Cessna 560CESSNASDR HALA2011091800404Warning Light · false activationETOPS SIGNIFICANT SYS - RUDDER RATIO DISCREET LIGHT ILLUMINATED AND RUDDER RATIO EICAS MESSAGE DISPLAYED. BITE RUDDER RATIO BOXES, NO FAULTS. RESET BOTH BOXES, RECYCLED G10 BREAKER IAW FIM 27-21-00-1. ALL CHECKS OK.Sep 18, 2011 · N594HA · Boeing 767332SDR HALA2011091600406Rudder Control · malfunctionedETOPS SIGNIFICANT SYS -RUDDER TRIM INDICATOR CTR CONSOLE. INDICATED 1.5 UNITS NOSE LT WITH EICAS & BALL CENTERED. INFO NOTED. OK FOR SERVICE IAW AMM 27-01-00-501. WHICH STATES MOST OPERATOR REPORT LESS THAN 1 UNIT AT RUDDER TRIM, HOWEVER SOME AIRPLANES REQ USep 16, 2011 · N598HA · Boeing 767332SDR USAA2011091600006Pcu · out of rigON CLIMBOUT FROM CLT WHILE FLYING THE RNAV DEPARTURE, CREW HAD TO APPLY FULL LEFT AILERON TO MAKE TURN REQUIRED FOR THE RNAV DEPARTURE. CREW REPORTED THE AIRCRAFT WAS OUT OF RIGGING. APPLIED MORE THAN 1.0 UNIT OF RIGHT RUDDER TRIM IN ORDER TO TRIM THE AIRCRASep 14, 2011 · N434US · Boeing 7374B7
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