JASC 2710

Service difficulty reports · 2,967

Reports filed under 2710 · Aileron 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 = '2710'
  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 IPXA1M67996Actuator · failedATB, AUTO PILOT WILL NOT ENGAGE T/S C/O AND FOUND AT FCC2 "AILERON EHV-LOB"AT FAULT. R & R LT OTBD AILERON ACTUATOR IAW AMM 27-13-30-4. C/O RTS TEST OF FCC1 AND FCC2. TEST PASSED.Jul 19, 2011 · N254UP · Doug MD11FSDR UALA2011071903687Aileron · out of adjustLATERAL TRIM OUT OF LIMITS AT 350 F0 1.8R, 250 F0 1.0R 180 F5 0.5R, 160 F20 0, 140 F25 0.2R, 130 F30 0. ADJUSTED THE FLAP SHIMS AND SPOILER GAPS PER MM. CREW REPORTS LATERAL TRIM AT FLAPS 20 AND 25 IS OUT OF LIMITS. WITH RUDDER SET AT ZERO THE REQUIRED LATEJul 17, 2011 · N577UA · Boeing 757222SDR UALA2011071203494Actuator · looseNO LAND 3 & LEFT AUTO PILOT INOPERATIVE. ACCOMPLISHED MCDP BITE, LAST FLT FAULTS SHOWS "AIL SRVO-FCC L. FLIGHT CONTROL COMPUTER NIS EZEJL, PCN 481-9097. INSTALLED FCC PER MM, NO HELP. STILL FAILING "AIL SERVO FCC L. RMV'D LEFT UPPER LCCA. NEW LCCA IN PLJul 12, 2011 · N646UA · Boeing 767322SDR UALA2011071103460Actuator · leakingHYD LEAK AT RT OUTBOARD AILERON. REPLACE OUTBOARD AILERON INBOARD ACTUATOR. NEED TO COMPLETE INSTALLATION OF NEW ACTUATOR (INBOARD POSITION). BEGIN AT MM. REPLACED ACTUATOR IAW MM.Jul 11, 2011 · N644UA · Boeing 767322SDR UALA2011070603351Pcu · faultyFLT CTL SYSTEM FAULT DISPLAYED ON STATUS. AHM SHOWS LEFT INBD FLAPERON PCU COMMAND ISSUE. REF MSG 27-10300 FIM TASK 27-11 TASK 814. REPLACED LEFT INBD FLAPERON PCU PER MM. OPS CHECK GOOD, LEAK CHECK GOOD & TEST PASSED. CYCLED FLAPS & AILERONS, NO MESSAGES Jul 5, 2011 · N774UA · Boeing 777222SDR WRNA201100007Warning System · activatedAFTER TAKEOFF DURING CLIMB, FLAP/SLAT RETRACTION LEVEL 2 ALERT "AIL DEFLECT DISAG" CODE ON. FOLLOWED PROCEDURES, DUMPED FUEL TO GET TO APPROVED LANDING WT. RETURNED TO AIRFIELD, LANDING NORMAL. DEFLECTED AILERONS MEL'D IAW 27-13-2, ASSIGNED DMI 6872. A/C RJul 5, 2011 · N951AR · Doug MD11FSDR UALA2011070503291Transmitter · faultyLEFT INBD AILERON NOT RESPONDING NORMALLY DURING PRE TAKEOFF CHECK. AILERON POSITION INDICATING SYS INOP. VISUAL CONFIRMATION REQUIRED BEFORE EACH FLIGHT. REPLACED LEFT INBD AILERON POSITION TRANSMITTER PER MM.Jul 3, 2011 · N175UA · Boeing 747422SDR UALA2011070103266Actuator · defectiveCREW REPORT: C HYD SYS MAINT MSG. ELECT C1 PUMP PRESSURE IS 2690 PSI, C2 ELECT PUMP PRESSURE IS 2410 AND ADP PRESSURE IS 2990 PSI. REPLACED CENTER HYD PRESS TRANSMITTER, NO HELP. WITH CENTER WING HYD SHUTOFF VALVE OFF, ELEC HYD PRESSURES RETURNED TO ABOVE Jul 1, 2011 · N654UA · Boeing 767322SDR UALA2011070103265Actuator · defectiveLEFT INBD AILERON INBD ACT REQUIRES REPLACEMENT. INSTALLED NEW ACTUATOR PER MM. SYSTEM WITHIN TOLERANCE.Jul 1, 2011 · N654UA · Boeing 767322SDR USAA2011072600034Bolt · damaged2S CHECK - PROTECTIVE TREATMENT MISSING ON BOLT OF ACTUATOR OUTBOARD SIDE AT RIGHT AILERON AT WS 12870, RIB 24. REPLACED BOLT OF ACTUATOR OUTBOARD SIDE AT RIGHT AILERON AT WS 12870, RIB 24 IAW A319 AMM 27-14-51.Jun 30, 2011 · N723UW · Airbus A319112SDR USAA2011072600033Bolt · damaged2S CHECK - PROTECTIVE TREATMENT MISSING ON BOLT OF ACTUATOR INBOARD SIDE AT RIGHT AILERON AT WS 12277, RIB 23. REPLACED BOLT OF ACTUATOR INBOARD SIDE AT RIGHT AILERON AT WS 12277, RIB 23 IAW A319 AMM 27-14-51.Jun 30, 2011 · N723UW · Airbus A319112SDR SIMA201118102Fitting · wornDURING MAINTENANCE BASE VISIT FOUND THE RIGHT AILERON PCA ATTACH BRACKET ON AILERON HAS WORN BUSHING HOLES. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT AILERON PCA BRACKET IAW EO EM-27MR-112. THE AIRCRAFT WAS RETURNED TO SERVICE.Jun 29, 2011 · N815AE · Emb EMB135KLSDR NX4R000014Control Cable · frayedTHE AILERON CABLE PN-0510105-364 WAS FRAYED AND WORN SHOWING BROKEN STRANDS AT FUSELAGE STATION 65.33 WHERE THE CABLES PASS THOUGH THE 3 CEILING MOUNTED NYLON PULLEYS.Jun 28, 2011 · N483ER · Cessna 172SSDR SIMA201117905Fitting · gougedDURING MAINTENANCE BASE VISIT INSPECTION FOUND THE LEFT AILERON DAMPER FITTING GOUGED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED FITTING IAW EO EM-27MR-112. THE AIRCRAFT WAS RETURNED TO SERVICE.Jun 25, 2011 · N815AE · Emb EMB135KLSDR SIMA201117904Fitting · wornDURING MAINTENANCE BASE VISIT INSPECTION FOUND THE LEFT AILERON POWER CONTROL ACTUATOR FITTING HAS WORN OUT BUSHING HOLES. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED FITTING IAW EO EM-27MR-112. THE AIRCRAFT WAS RETURNED TO SERVICE.Jun 25, 2011 · N815AE · Emb EMB135KLSDR 2ARF201106001Control Cable · bindingDURING FLIGHT AILERONS CONTROLS TEST, THE AILERONS CONTROL WERE NOT RETURNED TO NEUTRAL POSITION. MX PERSONNEL PERFORMED THE AILERON SYS INSPECTION IAW MM 27-11-00 DETECTING JAMMED THE AILERON CONTROL CABLES IN BOTH DIRECTIONS; SO THE RT WING REAR DRUMS OF AILJun 23, 2011 · N848SH · Doug DC983SDR BGSR20110628001Cable · frayedCOMPLIED WITH SAIB: CE-11-36 (5-31-2011) ON FRAYED AILERON CABLES AND NOTED THAT AILERON BALANCE CABLE WAS WEARING AND FEW BROKEN STRANDS OF CABLE. REMOVED DEFECTIVE CABLE AND SERVICED WITH NEW PN: MC0510105-364 AND MC0510105364365 CABLE ASSEMBLIES IAW CHAPTEJun 23, 2011 · N2225A · Cessna 172SSDR NX4R000020Control Cable · frayedDURING A ROUTINE INSP, THE AILERON RT DIRECT CABLE, PN-0510105-360 WAS FOUND FRAYED WITH MANY BROKEN STRANDS WHERE IS PASSES THROUGH THE NYLON PULLEY (S394) IN THE CENTER CEILING AT FS 65.33.Jun 22, 2011 · N483ER · Cessna 172SSDR CHQA201100230Recovery Unit · malfunctionedWHILE DESCENDING INTO KCAE ON AUTO PILOT, CREW RECEIVED AND AP MISS TRIM MESSAGE ON EICAS. WHEN THE QUICK DISCONNECT WAS PUSHED INITIALLY THE ROLL CONTROL WAS FROZEN. THE CREW THEN MANUALLY FORCED THE AILERONS OVER TO FREE THEM AND THE AIRCRAFT LANDED WITHOUJun 22, 2011 · N258JQ · Emb EMB145LRSDR NX4R000018Control Cable · frayedDURING A ROUTINE INSP, THE AILERON LT DIRECT CABLE WAS FOUND FRAYED WITH MANY BROKEN STRANDS WHERE IS PASSES THROUGH THE NYLON PULLEY (S394) IN THE CENTER CEILING AT FS 65.33.Jun 21, 2011 · N368ER · Cessna 172SSDR NX4R000015Control Cable · frayedDURING A ROUTINE INSP THE AILERON RT DIRECT CABLE PN-0510105-364 WAS FOUND FRAYED WITH MANY BROKEN STRANDS WHERE IS PASSES THROUGH THE NYLON PULLEY (S394) IN THE CENTER CEILING AT FS 65.33.Jun 21, 2011 · N368ER · Cessna 172SSDR CHQA201100227Actuator · malfunctionedDURING FLIGHT, THE FLIGHT CREW REPORTED THAT THE AILERONS LOCKED IN STRAIGHT AND LEVEL FLIGHT, FOLLOWED BY AILERON MIS-TRIM. THE CREW HAD TO FORCE THE AILERONS TO GET AUTO PILOT TO DISENGAGE. DURING APPROACH, THE AILERONS LOCKED AGAIN BUT THE CREW WAS ABLE TJun 19, 2011 · N258JQ · Emb EMB145LRSDR CHQA201100225Feel Unit · malfunctionedDURING THE FLIGHT TO KSDF WITH THE AUTO PILOT ON MEL, THE FLIGHT CREW REPORTED THAT THE AILERONS LOCKED UP SEVERAL TIMES DURING FLIGHT. THE AIRCRAFT LANDED WITHOUT INCIDENT IN KSDF. MAINTENANCE INSPECTED THE AILERON CABLES AND FOUND NO DEFECTS. THE AILERON Jun 16, 2011 · N258JQ · Emb EMB145LRSDR CHQA201100224Computer · malfunctionedWHILE DESCENDING THROUGH 5,000FT INTO KDCA THE CREW REPORTED AN AILERON MIS TRIM MESSAGE ON EICAS. THE AUTO PILOT WAS THEN TURNED OFF AND REPORTED THAT THE AILERONS WERE LOCKED. THE CREW WAS ABLE TO FREE THE AILERONS BY FORCING THE AILERONS TO MOVE. THE AIRJun 16, 2011 · N258JQ · Emb EMB145LRSDR NX4R000019Control Cable · frayedDURING A ROUTINE INSP THE AILERON RT DIRECT CABLE PN-0510105-364 WAS FOUND FRAYED WITH MANY BROKEN STRANDS WHERE IS PASSES THROUGH THE NYLON PULLEY (S394) IN THE CENTER CEILING AT FS 65.33.Jun 14, 2011 · N368ER · Cessna 172SSDR HALA2011061300264Actuator · faultedETOPS SIGNIFICANT SYSTEM - "AIL LOCK" LIGHT ON OVERHEAD AND AILERON LOCKOUT ON EICAS DISPLAY ON. PERFORMED FIM IAW 27-09-00. FOUND OAL ACTUATOR FAULT FIM 27-11-002 (M479). R & R RT OAL OTBD AILERON ACTUATOR IAW AMM 27-11-44. OPS CHECK GOOD. PANEL 561 SECURJun 13, 2011 · N587HA · Boeing 76733ASDR IPXA11M67202Aileron · warning lightAILERON DEFLECT DISAGREE AT FLT 290 DESCENDED TO FLT 150 TO RUN QRH CHECKLIST. WARNING WENT AWAY BUT CAME BACK CLIMBING THRU FLT 250. ATB DUE TO SIL DEFLECT DISAGREE. R & R RT OTBD AILERON DEFLECTION IAW AMM 27-16-02-4. ALL TESTS SATISFACTORY.Jun 11, 2011 · N288UP · Doug MD11FSDR CHQA201100221Servo · inoperativeCREW REPORTED THAT DURING CLIMB, AT 22,000 FEET, LOST AILERON CONTROL AND THE CONTROL WAS LOCKED. WITH EXCESSIVE FORCE, THE CREW FREED THE AILERON CONTROL. THE CREW RETURNED TO KSDF AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE AILERON SERVO MOTOR. Jun 10, 2011 · N258JQ · Emb EMB145LRSDR UALA2011060802832Control Valve · leakingLT WING OTBD AIL. SERVO CONTROL VALVE LEAKING 20 DROPS PER MINUTES. LEAKING ACTUATOR ROD OUT LIMITS PER LM AND MM. REPLACED LEFT OUTBOARD AILERON SERVO CONTROL PER MM. COMPLETED INSTALLATION OF LT OTBD AILERON ACTUATOR REF AMM. ADJ AND PERFORMED OPERATIONAJun 8, 2011 · N415UA · Airbus A320232SDR CA110610005Control Cable · wornSTAINLESS STEEL AILERON CABLES FOUND WORN AT FAIRLEAD IN RT WING ABOVE ROLL SERVO, AT FAIRLEAD IN LT WING, AND AT THE 3 SMALL PULLEYS IN THE CABIN CEILING. TT 1645, RT AILERON CABLES SHOWED THIS SAME PROBLEM AT ABOUT 600 TT, CABLES WERE REPLACED AND SDR SUBMITJun 7, 2011 · Cessna 172SSDR NX4R000021Control Cable · frayedDURING A ROUNTINE INSPECTION, THE LT AILERON PRIMARY CABLE, PN-0510105-360 WAS FOUND WORN AND FRAYED IN THE CABIN CEILING WHERE IT PASSES ACROSS THE 3 SMALL NYLON PULLEYS AT FS 65.33.Jun 2, 2011 · N483ER · Cessna 172SSDR DJFA2011025Roll Pin · sheared** SUPPLEMENTAL INFORMATION ** PRIOR TO FLIGHT, CREW REPORTED LEFT SPOILERON NOT MOVING WITH FLIGHT CONTROL INPUT. MAINTENANCE PERSONNEL DISCOVERED TWO ROLL PINS SHEARED ON THE AILERON-ROLL SPOILER MIXER ASSEMBLY. THE SPOILER MIXER ASSEMBLY WAS REPLACED.May 30, 2011 · N721FL · Cessna 750SDR HALA2011052400223Control Unit · bindingAILERON CONTROL IS BINDING, REPEAT WRITE UP. LUBRICATED LT & RT CONTROL TAB CABLES & PULLEYS IAW AMM12-24-00, OPS CK OK, NO BINDING NOTED. ACCOMP RTS ON SECU ALL TEST PASSED OK FOR SVC.May 24, 2011 · N484HA · Boeing 717200SDR CA110524008Control Cable · frayedDURING SCHEDULED INSP, FOUND AILERON CABLE, PN 82700568-S001 AT RT WING STN 181 FRAYED AND STARTING TO UNRAVEL. THE POINT OF THE FAILING CABLE IS LOCATED IN A CABLE BLOCK ON THE AFT SPAR WERE ALUMINUM GUIDE ROLLERS, PN FL4C6-2 ARE IN CONTACT WITH THE CABLE. May 23, 2011 · Dhav DHC8301SDR HALA2011052300216Aileron Sys · lack of lubeAILERON CONTROL IS BINDING. LUBRICATED CONTROL TAB IAW MM 12-24--00 SECURITY AND CONTROL CHECK GOOD.May 23, 2011 · N484HA · Boeing 717200SDR HALA2011052100215Actuator · failedETOPS SIGNIFICANT SYS- AILERON LOCKOUT EICAS WARNING. REPLACED RT AILERON LOCK OUT ACTUATOR IAW AMM 27-11-44 GROUND OPS CHECK OK.May 21, 2011 · N589HA · Boeing 76733ASDR HALA2011051800209Warning Light · false activationETOPS SIGNIFICANT SYS - AILERON LOCKOUT EICAS DURING APPROACH, 160 KNTS WITH FLAPS 20 SELECTED, CONTROLS FELT NORMAL, LIGHT WENT OUT AFTER LANDING. BITE SAMS IAW FIM 27-11-00, NO FAULTS NOTED, EICAS MSG AILERON LOCKOUT CLEARED, EXTINGUISHED, OK TO CONTINUE.May 18, 2011 · N589HA · Boeing 76733ASDR UALA2011051602408Actuator · faultyMSG 27-10302 FAULTING RT INBD FLAPERON ACTUATOR. REPLACED RT INBD FLAPERON ACTUATOR. ACP FIM 27-11 TASK 816, GND TEST 27-PRIMARY FLT CONTROLS, SYSTEM TEST, "RIGHT FLAPERON POSITION" TEST FAILS! SWAPPED ACE UNITS, NO HELP. THIS TEST GENERATED MAINT MSG 27-1May 15, 2011 · N211UA · Boeing 777222SDR C2XA11TY051Unknown · malfunctionedTYS - A/C WAS ON APPROACH WHEN THE CREW REPORTED THAT THE AILERONS FELT HEAVY. MAINTENANCE PERFORMED A DVI ON FORWARD AILERON QUADRANTS AT BOTH LEFT AND RIGHT PCA'S IAW EMB 145AMM-57-11-00. NO DEFECTS NOTED AND WAS RELEASED.Apr 28, 2011 · N14562 · Emb EMB145LRSDR DXTA2011042504561Aileron Sys · inoperativeAT 40,000 FT NOTICED THE AUTOPILOT DOING BABY DUTCH ROLLS TO STAY ON COUSE. AFTER DISSCONNECTING THE AUTOPILOT FOUND NEITHER PILOT HAD CONTROL OF THE AILERONS. ACFT WOULD NOT TURN WITHOUT EXCESSIVE FORCE APPLIED TO THE YOKE. OUSIDE AIR TEMP -35 TAT. -64 SATApr 16, 2011 · N706QS · Gulstm 200SDR UALA2011041401808Actuator · faultyAFTER PUSH AILERON LOCKOUT EICAS MESSAGE. FOUND LEFT SAM HAD LEFT AILERON ACT FAULT. RESET AND DID NOT RETURN. FOLLOWED LM8279 AND REPLACED RIGHT SAM. UPON RETEST LEFT SAM FAULTED LEFT ACTUATOR. INSTALLED NEW SAM IN LEFT SIDE AND ORIGINAL BACK IN RIGHT. RETESApr 14, 2011 · N647UA · Boeing 767322SDR KGBR20110411334Bellcrank · corrodedRIGHT AILERON BELL CRANK AT WING STA 6600 UPPER BEARING HOUSING IS CORRODED.Apr 11, 2011 · N392C · Casa C212SDR CA110415002Actuator · frozen(CAN) ON APPROACH AFTER AP DISCONNECTED, FLAPS AT 45 DEGREES, COULD NOT ROLL LT FOR 8 SEC, THEN SYS FREED UP, WITH NO FURTHER PROBLEMS. OTHER PART AFFECTED: MOUNT, SERVO, AILERON NR: 822-0259-001 CAW ISSUE OPEN: RJX-CA-27-43 AD TO BE ISSUED.Apr 9, 2011 · Cndair CL6002B19SDR AALA20110409LHR01Seal · damagedLHR - INFLIGHT CDG-JFK. CREW REPORTED LEFT HYDRAULIC QUANTITY LOSS AND PRESSURE PROBLEMS. EMEREGNCY DECLARED FLIGHT DIVERTED LHR LANDED WITHOUT INCIDENT. FOUND RIGHT OUTBOARD AILERON PCA SEAL DAMAGED. REPLACED SEAL. SYSTEM GROUND CHECK NORMAL OPERATION.Apr 9, 2011 · N173AN · Boeing 757223SDR KGBR20110408321Control Quadrant · corrodedCORROSION ON UPPER SURFACE OF AILERON QUADRANT CONTROL RODS CENTER WING FS 6735.Apr 8, 2011 · N392CA · Casa C212SDR KGBR20110408Control Quadrant · corrodedRIGHT CENTER WING AILERON CONTROL QUADRANT IS CORRODED ON UPPER SURFACE FS 6735 (LEVEL 3).Apr 8, 2011 · N392CA · Casa C212SDR KGBR201104081012Control Quadrant · corrodedLEFT CENTER WING AILERON CONTROL QUADRANT IS CORRODED ON UPPER SURFACE FS 67355.Apr 8, 2011 · N392CS · Casa C212SDR 2011FA0000268Seat · failedPILOT REPORTED THAT HIS AILERON CONTROLS SUDDENLY BECAME EXTREMELY STIFF WHILE IN FLIGHT. UPON COMPLETE DISASSEMBLY, FOUND CONTROL "T" NEEDLE BRG SET TO BE COMPLETELY FAILED AND BINDING THE CONTROLS. CONTROLS WERE VERY DIFFICULT TO TURN LT TO RT. THIS WAS AApr 7, 2011 · N934TE · Amrgen AG5BSDR U2RA227DHN043Control Cable · nickedMAIN PASSENGER CABIN CABLE RUN A2B, APROX 6 INCHES FWD OF STA BS460 HAS A NICK.Apr 4, 2011 · N151GX · Boeing 7572G5SDR SWIA201125891Regulator · out of rigAILERONS BINDING. (FLT 4479) RIGGED LEFT WING TENSION REGULATOR PER AMM.Mar 31, 2011 · N435SW · Cndair CL6002B19
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