JASC 2722

Service difficulty reports · 284

Reports filed under 2722 · Rudder Actuator, newest first.

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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 = '2722'
  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 CALA2013111292847Actuator · failedAUTOPILOT ADJUSTMENT TEST FAILS CTR RUDDER SERVO TEST. REPLACED CTR RUDDER ACTUATOR. ACCOMPLISHED TESTS REQUIRED FOR ACTUATOR REPLACEMENT.Nov 11, 2013 · N564UA · Boeing 757222SDR CALA2013102992477Actuator · malfunctionedNEEDED FOUR UNITS OF LT TRIM FOR CLIMB & CRUISE. CDGMM ACCOMPLISHED RUDDER & RUDDER TRIM CHECKED IAW MM 27-00-97 P601 STEPS 5B & C 3 & ITEM 6 A & C. IN ADDITION ACP MM 27-21-00 FIG 106 STEPS 1 THRU 4, NO FAULTS FOUND. INSTALLED RUDDER PCA ACTUATOR IAW AMM. Oct 27, 2013 · N672UA · Boeing 767322SDR CALA2013100791795Actuator · faultyHYD QTY DECREASED, RTFL. HYD QTY DECREASED, QTY STABLE WITH EDP DEPRESSURIZED & ACMP OFF, POS 145 01=L,02=R, FRM CODE 29 11 10. EICAS LT HYD QTY WITH QTY .48 PUMPS TURNED OFF QTY GOES DOWN FURTHER. R & R LT HYD SYS RUDDER PCA IAW AMM 27-21-02, OPERATIONS & Oct 7, 2013 · N675UA · Boeing 767322SDR CALA2013100491759Actuator · leakingHYDRAULIC FLUID LEAKING ON TOP OF TAIL CONE FROM RUDDER DRAIN, FOUND ON WALK AROUND. DURING INSPECTION OF RUDDER PCA AREA, FOUND UPPER RUDDER PCA ACTUATOR LEAKING FROM ROD END .Oct 4, 2013 · N656UA · Boeing 767322SDR CALA2013100791769Actuator · leakingHYD FLUID LEAKING ON TOP OF TAIL CONE FROM RUDDER DRAIN. DURING INSPECTION OF RUDDER PCA AREA, FOUND UPPER RUDDER PCA ACTUATOR LEAKING FROM ROD END .Oct 3, 2013 · N656UA · Boeing 767322SDR CA140208002Pcu · failed(CAN) DURING CLIMB NR 1 RUDDER HYDRAULIC CAUTION ILLUMINATED. RETURN TO FIELD. MAINTENANCE REPLACED RUDDER PCU.Aug 29, 2013 · Bombdr DHC8401SDR CA130426002Pca · leaking(CAN) WHILE TAXIING FOR DEPARTURE THE ACFT DEVELOPED A LEAK FROM THE LT HYD SYS AND RETURNED TO THE GATE. CTR, LT HYD SYS, RUDDER PCA REPLACED IAW J/C B767-27-21-02-422-038-8A98. INDEPENDENT CHECK CARRIED OUT.Apr 25, 2013 · Boeing 767333SDR SCNA20130320062Bolt · brokenMAIN RUDDER PCU BOLT BROKEN IN LINKAGE. FOUND DAMAGE TO HINGE RIB 66.42 AND 56.48. BLENDED OUT DAMAGE. RE-INSTALLED NEW MAIN RUDDER PCU. PERFORMED PENETRANT INSPECTION. AREA PREPPED AND PRIMED.Mar 20, 2013 · N816SY · Boeing 7378Q8SDR CA130318018Actuator · leaking(CAN) OVERWEIGHT LANDING DUE TO AIRBORNE RETURN ACCOUNT OF STRONG IRRITATING DIRTY SOCK ODOR EMANATING THROUGHOUT CABIN/FLIGHT DECK. SEQUENCED PACKS, UNABLE TO ELIMINATE ODOR. ACFT LANDED APPROXIMATELY 600 KGS OVER MAXIMUM LANDING WEIGHT. BOROSCOPE INSP C/OMar 16, 2013 · Emb ERJ170200SUSDR UALA2013030501312Actuator · faultyCREW REPORTS OVERHEAD R HYD 'QTY' LIGHT ILLLUMINATED WITH ASSOCIATED EICAS MESSAGE. RIGHT SYSTEM HYD QTY AT .46. CREW FOLLOWED QRH 130.3 AND TURNED OFF RIGHT SYSTEM HYDRAULIC PUMPS. REPLACED BOTTOM RUDDER PCA PER MM. FILLED RIGHT HYDRAULIC RESERVOIR TO NORMMar 3, 2013 · N667UA · Boeing 767322SDR UALA2013030501303Actuator · leakingRRCM P/N 3800022-108 S/N 0521 LEAKING. REMOVED AND REPLACED RUDDER RATIO CHANGER ACTUATOR IAW B757 27-21-13-002-001 AND 27-21-13-402-032. LEAK AND OPS CHECK GOOD IAW B757 AMM 27-21-00.Mar 2, 2013 · N522UA · Boeing 757222SDR UALA2013020700745Pcu · leakingUPPER RUDDER PCU IS LEAKING. 60-90 DROPS PER MINUTE. REMOVED UPPER RUDDER PCU. INSTALLED RUDDER SERVO IAW MM 27-24-51-400-001-A. OPS CHECKED IAW 27-24-00-710- 001-A. OPS CHECKED OK, NO LEAKS NOTEDFeb 6, 2013 · N407UA · Airbus A320232SDR UALA2013012200382Seal · leakingHYD FLUID LEAKING FROM RUDDER DRAIN HOLE. HEAVY LEAK TO RUNNING LEAK WITH HYD SYSTEM PRESSURIZED. DURING LEAK CHECK FOUND LEFT RUDDER PCU HAD NO SYSTEM PRESSURE. FOUND RIGHT RUDDER PCA LEAKING FROM ROD-END SEAL WITH CENTER SYS PRESSURIZED, DID NOT LEAK WITHJan 21, 2013 · N662UA · Boeing 767322SDR UALA2013010700092Actuator · leakingFOUND PUDDLE OF HYDRAULIC FLUID ON GROUND BELOW TAIL AREA. APPEARS TO BE RUNNING DOWN SIDES OF LOWER LEADING EDGE OF RUDDER. FOUND UPPER RUDDER PCM, LOWER ACTUATOR LEAKING 60 DROPS PER MINUTE. NEW ACTUATOR INSTALLED.Jan 5, 2013 · N127UA · Boeing 747422SDR DALA12013449008Actuator · crackedRUDDER LIMITER ACTUATOR ATTACH TO STA 1510 FRAME IS CRACKED AT 2:30 POSITION. CRACKED EMPENNAGE. REMOVED FASTENER. NDT CRACK. END TO END .92". REMOVED ALL ATTACHING HARDWARE, CUT FRAM AT 1:00 POSITION RT SIDE FOR FRAME REPAIR. HFEC. DAMAGE CONTAINED. FORNov 18, 2012 · N908DE · Doug MD88SDR UALA2012111606577Pca · faultyRUDDER PCU STATUS MSG WON'T CLEAR. INOPED PER MEL ATTEMPTED MT 27-21-00, NO HELP. PASSES SINGLE SYSTEM PROCEDURE PER MEL. T/S PER MM. FOUND LOWER PCA CAUSING THE MSG. NO PARTS BOS. REPLACED LOWER RUDDER PCA IAW MM.Nov 16, 2012 · N541UA · Boeing 757222SDR UALA2012090605044Actuator · faultyRUDDER RATIO CHANGER PART NUMBER 3800022-105 CURRENTLY INSTALLED AND REQUIRES REPLACEMENT PER WC 5R2717147 SEQ#448. REMOVED AND REPLACED RUDDER RATION ACTUATOR PER AMM. OPS, LEAK AND RIG CHECK GOOD.Sep 5, 2012 · N552UA · Boeing 757222SDR UALA2012080904331Actuator · leakingDURING WALK AROUND, MECH NOTICED SIGN OF HYD LEAK FROM APU ACCESS DOOR. ON REMOVAL OF RUDDER ACCESS PANEL, FOUND LOWER PCA LEAKING AT THE ACTUATOR STATIC SEAL. THE LEAK IS APPROX 5 DROP PER MIN AND FOUND WITHIN LIMITS IAW AMM.Aug 8, 2012 · N657UA · Boeing 767322SDR UALA2012071603825Actuator · malfunctionedRUDDER TRIM INOPERATIVE UNTIL 22000 FT. REPLACED RUDDER TRIM ACTUATOR PER MM, SYSTEM CHECK OKAY.Jul 13, 2012 · N544UA · Boeing 757222SDR UALA2012051802841Actuator · leakingHYDRAULIC FLUID LEAKING FROM BOTTOM OF TAIL AT 10 DROPS PER SECOND. RUDDER RATIO ACTUATOR LEAKING. REPLACED RUDDER RATIO CHANGER ACTUATOR IAW MM. OPS AND LEAK CHECKED NORMAL.May 16, 2012 · N648UA · Boeing 767322SDR AJAA2012F00076Actuator · intermittentON APPROACH, THE ACFT RUDDER TRIM WENT TO FULL DEFLECTION. PILOT DECLARED AN EMERGENCY, AND LANDED SAFELY. RUDDER TRIM ACTUATOR FOUND TO BE INTERMITTENT. REMOVED AND REPLACED ACTUATOR.Apr 16, 2012 · N935SP · Pilats PC1245SDR UALA2012031201635Actuator · leakingHYDRAULIC LEAK AT RUDDER RATIO CHANGER ACTUATOR ROD SHAFT RUNNING LEAK. REMOVED RRCA. NEED TO INSTALL NEW UNIT MR27214-121 (MRDATA ENTERED).Mar 11, 2012 · N548UA · Boeing 757222SDR UALA2012030701486Seal · leakingDURING WALKAROUND, FOUND HYD LEAKING DOWN BOTH SIDES OF TAIL COMPT. CYCLED RUDDER, FOUND UPPR RUDDER PCA LEAKING OUT OF FWD SHAFT SEAL. REMOVED UPPER RUDDER PCA. SHOP REPAIRED ACTUATOR BY REPLACING FWD SHAFT SEALS. WORKING INSTALL.Mar 6, 2012 · N657UA · Boeing 767322SDR UALA2012022901269Actuator · faultyRUDDER RATIO OVERHEAD LIGHT ON AND WITH RUDDER RATIO EICAS MESSAGE. CAN BE CLEARED BY CYCLING RUDDER RATIO CB CONDITION CAN BE DUPLICATED WITH BOTH ENGS RUNNING WITH NR 1 EDP SELECTED OFF THEN BACK ON. BOTH LEFT AND RIGHT RRMC SHOW PCA YELLOW FAULT BALLS. RFeb 27, 2012 · N673UA · Boeing 767322SDR ASOA201200404Actuator · failedIN CRUISE FLIGHT, AUTOPILOT ENGAGED, RECEIVED UNCOMMANDED RUDDER INPUTS (YD 1 WAS DEFFERRED AT THE TIME) INPUTS WERE LT AND RT OF CENTER AND NEEDED FULL RUDDER DEFLECTION AT TIMES TO COUNTER THE DEFLECTION. DECLARED AN EMERGENCY AND LANDED. R & R YAW DAMPERFeb 5, 2012 · N754EV · Cndair CL6002C10SDR UALA2012011600333Actuator · faultyRUDDER RATIO LIGHT ON. PERFORMED RUDDER RATIO CHANGER MODULE TEST PER FIM 27-09-00. PCA FAULT BALL NOTED. REPLACED RUDDER RATIO CHANGER ACTUATOR PER MM, RIGGED PER MM. NO LEAKS NOTED, RIG GOOD.Jan 13, 2012 · N666UA · Boeing 767322SDR UALA2012010900215Actuator · leakingLOWER RUDDER ACTUATOR LEAKING AT PISTON. INSTALLED NEW LOWER RUDDER ACTUATOR. REMOVED MR27250-65 OFF AND -91 ON. NEED TO COMPLETE FROM STEP I-5 ON PAGE 219. COMPLETED INSTALLATION AND OPS CHECK OF RUDDER PCA SYSTEM PER MM.Jan 7, 2012 · N647UA · Boeing 767322SDR DXTA2012010304838Actuator · inoperativeTAKE OFF REQUIRED EXTRA RIGHT RUDDER PRESSURE. ON CLIMBOUT TO 14,000 FT, ACFT REQUIRED FULL RT RUDDER TRIM AND FULL RT RUDDER AND THAT WAS NOT ENOUGH FOR COORDINATED FLIGHT. ON RETURN TO AIRPORT AT LOWER POWER SETTINGS, PLANE REQUIRED HALF OF RT RUDDER TRIM SJan 4, 2012 · N647QS · Cessna 560XLSDR UALA2011122707123Actuator · leakingHYDRAULIC LEAK FROM TAIL AREA. FOUND LOWER RUDDER ACTUATOR UNIT ON UPPER RUDDER LEAKING FROM STRUT ROD. REPLACED RUDDER LWR ACTUATOR PER MM.OPS CHECKED GOOD. NO LEAKS NOTED.Dec 25, 2011 · N117UA · Boeing 747422SDR CA111221001Pcu · leaking(CAN) CREW REPORTED HYD SYS NR 1 LOW PRESSURE CAUTION MESSAGE ILLUMINATED DURING TAXI IN. EICAS HYD SYNOPTIC PAGE SHOWED NR 1 QUANTITY AT ZERO. CREW SHUTDOWN ENGINE WHILE THERE WAS STILL PRESSURE IN THE SYSTEM. AFTER ARRIVING AT THE GATE QUANTITY WAS READINGDec 16, 2011 · Cndair CL6002B19SDR CA111208004Pcu · leaking(CAN) DURING FLIGHT WHILE ON APPROACH TO AIRPORT, SMOKE AND HYDRAULIC FUMES ENTERED THE COCKPIT AND CABIN VIA THE BLEED AIR ENVIORMENTAL SYS. AN EMERGENCY LANDING WAS REQUESTED. ONCE ON THE GROUND AND OFF THE MAIN RUNWAY, THE CREW SECURED AND EXITED THE ACFT Dec 7, 2011 · Bombdr BD1001A10SDR CA111115010Actuator · damaged(CAN) TANKER 484 HAD AN EXTERNALLY LEAKING RUDDER ACTUATOR. ON DIS-ASSEMBLY IT WAS DISCOVERED THAT THE PLUGS SERVING AS STOPS FOR A CYLINDER DIVIDER ASSEMBLY WERE BROKEN OFF. THIS COLLAR SERVED TO HOUSE O RINGS & SEPARATE HYD PRESSURES FROM SYSTEMS 1 & 2. BNov 15, 2011 · Lkheed 188CSDR UALA2011101705621Actuator · leakingHYDRAULIC FLUID LEAK COMING FROM RIGHT SIDE OF VERTICAL STAB AT APPROX THE CENTER ACTUATOR VICINITY DURING ARRIVAL 1SV CHECK. HYD LEAK COMING FROM RUDDER AREA. ACTUATED RUDDER FLUID DRIPPING FROM DRAIN HOLE ON TRAILING EDGE OF RUDDER ALSO EVIDENCE FROM HINGEOct 16, 2011 · N646UA · Boeing 767322SDR UALA2011092105101Actuator · faultyUP TO 6 L RUDDER TRIM IN DESCENT. ROLL FORCE CHANGES WITH SPEED. REPLACED RUDDER TRIM ACTUATOR, OPS CHECKED GOOD.Sep 21, 2011 · N667UA · Boeing 767322SDR USAA2011092700016Actuator · failedAIRCRAFT YAWED LEFT SUDDENLY AND RUDDER TRIM 1 FAULTED. ON DESCENT, MULTIPLE FAULT APPEARED - YAW DAMPER 1, RUDDER TRIM FAULT, RUDDER TRAVEL LIMITER STUCK 2 DEGREES YAW, AUTO BRAKE FAULT, STATUS PAGE NORMAL BRAKE INOPERATIVE, ECAM SHOWED ALTERNATE BRAKE. DECSep 20, 2011 · N664AW · Airbus A320232SDR USAA2011092700015Limiter · failedAIRCRAFT YAWED LEFT SUDDENLY AND RUDDER TRIM 1 FAULTED. ON DESCENT, MULTIPLE FAULT APPEARED - YAW DAMPER 1, RUDDER TRIM FAULT, RUDDER TRAVEL LIMITER STUCK 2 DEGREES YAW, AUTO BRAKE FAULT, STATUS PAGE NORMAL BRAKE INOPERATIVE, ECAM SHOWED ALTERNATE BRAKE. DECSep 20, 2011 · N664AW · Airbus A320232SDR UALA2011072703848Actuator · malfunctionedRUDDER IS HARD TO DISPLACE TO THE LEFT ON TAKEOFF ROLL. RIGHT DISPLACEMENT NORMAL. ACCOMPLISHED CHECKS FOR RUDDER PEDAL STIFFNESS PER TSM. PER TSM TASK 27-20-00-810- 801 ACCOMPLISHED OPS OF RUDDER ARTIFICIAL-FEEL LOADS. ACCOMPLISHED YAW DAMP FUNCTION TEST Jul 26, 2011 · N848UA · Airbus A319131SDR UALA2011071903653Pca · out of adjustPLANE NEEDS EXCESSIVE RT RUDDER TRIM, 3.5 UNITS. FFS MATCHED, L-EPR 1.27, R-EPR 1.22. ADJUSTED UPPER, MIDDLE AND LOWER PCA'S PER MM. ACCOMPLISHED INSPECTION OF THREE RUDDER ACTUATOR ADJUSTMENTS FOR SAFETY AND SECURITY, RIGS. ALL CHECKS OKAY.Jul 18, 2011 · N658UA · Boeing 767322SDR DXTA2011071304658Actuator · malfunctionedON INITIAL FLIGHT CONTOL CHECK, LT RUDDER FELT HARD TO PUSH. SUBSEQUENT CHECKS ON GROUND, IT PERFORMED NORMALLY. ON ROTATION PF IN RT SEAT SAID THE PLANE WAS HARD TO CONTROL AND LT RUDDER REQUIRED RUDDER TRIM OVER HALF DISPLAY TO FLY STRAIGHT AND LEVEL. R & Jul 13, 2011 · N937QS · Cessna 750SDR CA110718005Actuator · failedDURING FLIGHT, THE PILOT REPORTED THAT THE RUDDER JAMMED IN NORMAL MODE ABOVE 145 KNOTS AND FAILED BELOW 145 KNOTS TWICE. IT WAS OK IN MANUAL MODE, ACFT RIGGING CHECK OK PRESS REDUCING VALVE CHANGED, DIDN`T CURE THE SNAG. THE RUDDER ACTUATOR CHANGED, ACFT SEJul 10, 2011 · Cndair CL2156B11215SDR UALA2011071103467Actuator · faultySPOILER ON EICAS INTERMITTANTLY 2-3 TIMES DURING CLIMB. ALTITUDE WAS UPPER TEENS TO LOW 20S. REPLACED RUDDER TRIM ACTUATOR PER AMM AS CALLED OUT IN LM1108. TRIM INDICATOR READS 1 UNIT RT WITH RUDDER AT NEUTRAL AND RIG PIN R4 ALIGNED. REF AMM FOR TRIM INDICATJul 10, 2011 · N676UA · Boeing 767322SDR 2011FA0000483Actuator · leakingUPPER ACTUATOR LEAKING FLUID. SUSPECT SEALS.Jul 5, 2011 · N808RT · Bombdr BD1001A10SDR 2011FA0000482Actuator · leakingLOWER ACTUATOR LEAKING FLUID.Jul 5, 2011 · N808RT · Bombdr BD1001A10SDR C2XA11TY098Pressure Switch · leakingHYDRAULIC SYSTEM 1 WENT TO AMBER ON THE EICAS DURING FLIGHT. AIRCRAFT DIVERTED INTO TYS FROM RIC. MAINTENANCE REMOVED AND REPLACED THE LT RUDDER ACTUATOR PRESSURE SWITCH AND THE HYDRAULIC LINE. SERVICED WITH HYD FLUID, OPS AND LEAK CHECKED GOOD. AIRCRAFT WJul 1, 2011 · N13958 · Emb EMB145LRSDR UALA2011062903219Actuator · leakingFOUND CENTER SYSTEM RUDDER ACTUATOR LEAKING. REMOVED CENTER SYSTEM RUDDER ACTUATOR.Jun 29, 2011 · N675UA · Boeing 767322SDR UALA2011060302711Actuator · leakingL HYD LOW ON TAXI IN RF .63 INDICATED. FOUND CENTER RUDDER PCA LEAKING ACTUATOR. APPLIED SEALANT ON THE ACTUATOR. LEAKING 26 DROP PER MN WITHIN LIMITS AS PER AMM. OK TO CONTINUE. ACCESS PANEL 324JL.Jun 2, 2011 · N657UA · Boeing 767322SDR UALA2011040701687Rod End · faultyAIRFRAME VIBRATION STARTED 16000FT (300 KNOTS). SW1416 ASSIGNED RUDDER INTEGRITY CHECK. SAMC TEXT: CREW DID NOT FILL OUT VIBE FORM BUT WAS DEBRIEFED AND SAID THAT THE VIB WAS LATERAL IN NATURE IN THE AFT GALLEY AREA POINTING AT THE RUDDER. PERFORMED SW1416Apr 6, 2011 · N457UA · Airbus A320232SDR UALA2011040401629Actuator · leakingDURING ETOPS PRE-DEPARTURE CHECK FOUND HYDRAULIC LEAK COMING FROM VERTICAL FIN. SUSPECT LEAK COMING FROM RUDDER ACTUATORS. FOUND HYDRAULIC LEAK COMING FROM CENTER RUDDER PCA ACTUATOR. FOUND LEAK WITHIN LIMITS AS PER AMM. LT HYD SYSTEM SERVICED TO FULL.Apr 3, 2011 · N644UA · Boeing 767322SDR ASOA201100649Actuator · failedUNCOMMANDED LARGE RUDDER DEFLECTION CAUSING LARGE YAWING MOMENT IN CRUISE AND ON APPROACH. AP ENGAGEMENT MADE NO DIFFERENCE. (ENROUTE, ACFT DIVERTED TO DUE TO MX -- EMERGENCY DECLARED) R & R LT AND RT YAW DAMPERS IAW AMM CH 22-22-01-000-801. PERFROMED OPS TMar 28, 2011 · N868AS · Cndair CL6002B19SDR FDEA201012154696Bearing · wornABOVE 15,000 FT THE AIRPLANE BEGAN TO SHAKE. AUTOPILOT, TURBULENCE, ENGINES, AND SPOILERS WERE ELIMINATED AS FACTORS. APPLYING EITHER RT OR LT RUDDER PRESSURE STOPPED THE SHAKING. IDENTICAL SYMPTOMS IN 2 PRIOR INSTANCES PROVED TO BE RUDDER FLUTTER DUE TO ACDec 15, 2010 · N677FE · Airbus A300F4605R
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