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 2009FA0000641Cable · frayedDURING INSP THE LT AILERON CABLE (PN-0510105-360) WAS FOUND WORN AND FRAYED WHERE IT CONTACTS THE NYLON PULLEY IN THE CEILING AT FS 65.33. PULLEYS ROTATE FREELY, HOWEVER, CABLE DOESN'T PROVIDE ENOUGH "TRACTION" TO ROTATE IT WHEN THE AILERON CONTROL IS MOVED FJul 22, 2009 · N394ER · Cessna 172SSDR 2009FA0000640Cable · frayedDURING A ROUTINE INSP RT AILERON DIRECT CABLE (PN-0510105-360) WAS FOUND WORN AND FRAYED WHERE IT CONTACTS NYLON PULLEY IN THE CEILING AT FS 65.33. PULLEYS ROTATE FREELY, HOWEVER, CABLE DOESN'T PROVIDE ENOUGH "TRACTION" TO ROTATE IT WHEN AILERON CONTROL IS MOJul 22, 2009 · N394ER · Cessna 172SSDR 2009FA0000639Cable · frayedDURING INSP RT AILERON BALANCE CABLE (PN-0510105-365) WAS FOUND WORN AND FRAYED WHERE IT CONTACTS THE NYLON PULLEY IN THE CEILING AT FS 65.33. PULLEYS ROTATE FREELY, HOWEVER, CABLE DOESN'T PROVIDE ENOUGH "TRACTION" TO ROTATE IT WHEN THE AILERON CONTROL IS MOVJul 22, 2009 · N394ER · Cessna 172SSDR 2009FA0000637Cable · frayedDURING INSP RT AILERON PRIMARY CABLE (PN-0510105-360) WAS FOUND WORN AND FRAYED WHERE IT CONTACTS NYLON PULLEY IN THE CEILING AT FS 65.33. PULLEYS ROTATE FREELY, HOWEVER, CABLE DOESN'T PROVIDE ENOUGH "TRACTION" TO ROTATE IT WHEN AILERON CONTROL IS MOVED FROM Jul 22, 2009 · N452ER · Cessna 172SSDR 2009FA0000636Cable · frayedDURING A ROUTINE INSP THE RT AILERON CABLE (PN-0510105-365) WAS FOUND WORN AND FRAYED WHERE IT CONTACTS THE NYLON PULLEY IN CEILING AT FS 65.33. PULLEYS ROTATE FREELY, HOWEVER, CABLE DOESN'T PROVIDE ENOUGH "TRACTION" TO ROTATE IT WHEN THE AILERON CONTROL IS MJul 22, 2009 · N452ER · Cessna 172SSDR 2009FA0000634Cable · frayedDURING A ROUTINE INSP THE LT AILERON PRIMARY CABLE (PN-0510105-360) WAS FOUND WORN AND FRAYED WHERE IT CONTACTS THE NYLON PULLEY IN THE CEILING AT FS 65.33. THE PULLEYS ROTATE FREELY, HOWEVER, CABLE DOESN'T PROVIDE ENOUGH"TRACTION" TO ROTATE IT WHEN THE AILEROJul 22, 2009 · N452ER · Cessna 172SSDR SWIA200922311Rod · corrodedLEFT AILERON TRIM RODS CORRODED. (C CHECK) REPLACED RODS PER AMM.Jul 20, 2009 · N251YV · Emb EMB120ERSDR AALA20090718DFW01Servo · leakingCENTER HYDRAULIC RESERVOIR LIGHT AND CENTER HYDRAULIC QUANTITY EICAS MESSAGE WITH AN INDICATION OF .38RF CENTER QUANTITY. PRESSURE WAS STABLE AT 2890 TO 2910 POUNDS PER SQUARE INCH. BOTH QUANTITY AND PRESSURE REMAINED UNCHANGED THROUGHOUT APPROACH AND LANDINGJul 18, 2009 · N622AA · Boeing 757223SDR 2009FA0000742Aileron · misriggedDURING THE ANNUAL INSP, IT WAS NOTED THAT BOTH AILERONS WERE DEFLECTED DOWN 6 DEGREES WHEN THE CONTROL YOKE WAS LEVEL. THE AILERON DEFLECTION DID NOT MEET THE DEFLECTION LIMIT IN THE TYPE CERT DATA. THE AIRPLANE WAS PAINTED IN 2005. THERE IS NO RECORD OF TJul 14, 2009 · N5094R · Cessna 172MSDR 2009FA0000831Control Cable · frayedCABLE IS FRAYED WHERE IT PASSES NEXT TO THE FLAP SELECTOR HANDLE UNDER THE CENTER FLOORBOARD TUNNEL. DIFFICULT TO SEE DEFECT WITHOUT REMOVING FLAP SELECTOR HANDLE. CABLE FRAYED APPROX 50 PERCENT AT THIS LOCATION. IT IS NOTED THAT WHEN THE FLAP IS EXTENDED TJul 12, 2009 · N9290P · Piper PA44180SDR CA090708003Control Cable · frayed(CAN) UPON REMOVAL OF LT WING, BOTH FWD AND AFT AILERON CABLES WERE FOUND WITH BROKEN STRANDS AT WING STA 71.125. CABLES RUN THROUGH REAR RIB OF WING, AND RUN OVER A PHENOLIC CABLE GUARD. CHAFFING WITH THIS GUARD IS CAUSE OF STRANDS BEING BROKEN. THERE IS Jul 7, 2009 · Cessna 172SSDR KY7A14756Control Cable · wornALL FOUR AILERON PRIMARY CONTROL CABLES FOUND WORN, SEVERING SEVERAL STRANDS AT WING STATION 50.021 WHERE IS PASSES IN FRONT OF THE OUTBOARD FLAP BELLCRANK. ONE CABLE HAD 3 OF THE 7 STRANDS SEVERED. CABLES WERE COVERED WITH GREASE AND GRIME MAKING IT DIFFICULTJul 6, 2009 · N404MG · Cessna 404SDR 2009FA0000600Control Cable · frayedDURING A ROUTINE INSP, THE AILERON CABLE PN-051105-360 WAS FOUND WORN WITH BROKEN STRANDS AT THE PULLEY CLUSTER IN THE CENTER CEILING AT FS-65.33.Jul 1, 2009 · N463ER · Cessna 172SSDR 2009FA0000599Control Cable · frayedDURING A ROUTINE INSP, AILERON CABLE PN-051105-365 WAS FOUND WORN WITH BROKEN STRANDS AT THE PULLEY CLUSTER IN THE CENTER CEILING AT FS-65.33.Jul 1, 2009 · N463ER · Cessna 172SSDR 2009FA0000598Control Cable · frayedDURING A ROUTINE INSP, THE AILERON CABLE PN-051105-360 WAS FOUND WORN WITH BROKEN STRANDS AT THE PULLEY CLUSTER IN THE CTR CEILING AT FS-65.33.Jul 1, 2009 · N463ER · Cessna 172SSDR 2009FA0000556Cable · frayedRT WING UPPER AILERON CABLE HAS BROKEN STRANDS. INSTALLED NEW CABLE PN 5000008-94CR.Jun 23, 2009 · N425DM · Cessna 425SDR 2009FA0000524Control Cable · frayedDURING AN ANNUAL INSP, MECHANIC FOUND A WORN AILERON CONTROL CABLE PN-0510105-360 AT THE PULLEY CLUSTER (PULLEY PN S378-4) IN THE CENTER OVERHEAD CEILING AREA. THE CABLE MUST BE ROTATED SO ACCESS CAN BE GAINED WHERE THE CABLE REST ON THE PULLEY AT THE SIX O’CJun 16, 2009 · N376ER · Cessna 172SSDR 2009FA0000523Control Cable · frayedDURING AN ANNUAL INSP, MECHANIC FOUND A WORN AILERON CONTROL CABLE PN-0510105-365 AT THE PULLEY CLUSTER (PULLEY PN S378-4) IN THE CTR OVERHEAD CEILING AREA. THE CABLE MUST BE ROTATED SO ACCESS CAN BE GAINED WHERE THE CABLE REST ON THE PULLEY AT THE SIX O’CLOCKJun 16, 2009 · N376ER · Cessna 172SSDR 2009FA0000522Control Cable · frayedDURING AN ANNUAL INSP, MECHANIC FOUND A WORN AILERON CONTROL CABLE, PN-0510105-364, AT THE PULLEY CLUSTER (PULLEY PN S378-4) IN THE CTR OVERHEAD CEILING AREA. CABLE MUST BE ROTATED SO ACCESS CAN BE GAINED WHERE CABLE REST ON THE PULLEY AT THE SIX O’CLOCK POSIJun 16, 2009 · N376ER · Cessna 172SSDR CA090615009Aileron Sys · malfunctioned(CAN) FACTORY INSTALLED BELLCRANK WAS NOTED AS BEING VISUALLY DIFFERENT. WHEN COMPARED TO A SERVICABLE PART FROM STOCK, IT APPEARS THAT THE STOP LUG ON THE LT (ONLY) WAS WELDED INCORRECTLY AT MFG. THE AILERON RIGGING IS CORRECT, WITH THE STOP ADJUSTED TO GIVEJun 15, 2009 · Cessna 208BSDR CA090616010Bearing · failed(CAN) DURING CLEANING OF NAV LIGHT LENS ON THE RT WING IT WAS NOTICED THAT THE NR 4 AILERON HINGE ARM HAD A FRESH SIGN OF IMPACT IN THE GREASE. WHEN THE AILERON WAS PULLED ON WITH LIGHT FORCE AT THE END, IT WAS FOUND THAT THERE WAS APPROX 1" OF MOVEMENT IN THEJun 11, 2009 · Dhav DHC8314SDR UALA2009060201590Actuator · faultyAILERON LOCKOUT MESSAGE. REMOVED & REPLACED RT OUTBOARD AILERON LOCKOUT ACTUATOR. OPS CHECK GOOD.Jun 2, 2009 · N659UA · Boeing 767322SDR 2009FA0000711Turnbuckle · missingDURING MX THE TURNBUCKLE LOCKING CLIPS WERE FOUND MISSING FROM AILERON CONTROL CABLES A1A-1 AND A1A-2. INSTALLED LOCKING CLIPS. (K)May 29, 2009 · N767KS · Boeing 76724QERSDR UALA2009060101583Fseu · faultyAILERON LOCKOUT LIGHT ON DURING TAXI. REPLACED RIGHT STAB TRIM-AIL LOCKOUT MODULE M525 AS PRECAUTION AND REPLACED FLAP-SLAT ELECTRONICS UNIT (FSEU) BECAUSE FAULTED BY RT SAME ON INBOUND LEG. ALL UNITS CHECK OKAY.May 29, 2009 · N659UA · Boeing 767322SDR 2009FA0000437Cable · frayedTHE OPERATOR HAS A FLEET OF 172S AIRCRAFT. THIS IS A COMMON CONDITION. THIS AILERON CABLE WAS WORN BADLY AT THE CENTER OF THE CABIN ROOF, WHERE IS PASSES THROUGH A PULLEY. THERE WERE MANY STRANDS WORN AND SEVERAL BROKEN STRANDS.May 27, 2009 · N481ER · Cessna 172SSDR 2009FA0000436Control Cable · frayedTHIS AILERON CABLE WAS WORN BADLY AT THE CENTER OF THE CABIN ROOF WHERE IS PASSES THROUGH A PULLEY. THERE WERE MANY STRANDS WORN AND SEVERAL BROKEN STRANDS.May 27, 2009 · N452ER · Cessna 172SSDR 2009FA0000435Control Cable · frayedTHIS AILERON CABLE WAS WORN BADLY AT THE CENTER OF THE CABIN ROOF, WHERE IS PASSES THROUGH A PULLEY. THERE WERE MANY STRANDS WORN AND SEVERAL BROKEN STRANDS.May 27, 2009 · N464ER · Cessna 172SSDR 2009FA0000434Control Cable · frayedTHIS AILERON CABLE WAS WORN BADLY AT WS 71.125 AND 100.50 . THERE WERE MANY STRANDS WORN AND SEVERAL BROKEN STRANDS.May 27, 2009 · N446ER · Cessna 172SSDR 2009FA0000433Control Cable · frayedTHIS AILERON CABLE WAS WORN BADLY AT THE CENTER OF THE CABIN ROOF, WHERE IS PASSES THROUGH A PULLEY. THERE WERE MANY STRANDS WORN AND SEVERAL BROKEN STRANDS.May 27, 2009 · N477E · Cessna 172SSDR UALA2009052001448Actuator · malfunctioned"AIL LOCK" LIGHT ON AT LOW SPEED. EICAS MSG AILERON LOCKOUT DISPLAYED. OUTBD AILERONS DID NOT INDICATE NORMAL-LOCKED OUT-BOTH. REPLACED AILERON LOCKOUT ACTUATOR, OPS CHECKS GOOD.May 20, 2009 · N661UA · Boeing 767322SDR CA090521002Aileron · contaminated(CAN) CREW DECLARED EMERGENCY DUE TO LWD CAUTION AT FL 270 (RT AILERON JAMMED) FLIGHT DIVERTED BECAUSE OF AN AILERON JAM. DURING CLIMB TO FL270 MESSAGE "AP LWD" APPEARED - DISAPPEARED AND APPEARED SHORTLY AFTER AGAIN. CREW DISCONNECTED AUTOPILOT FOR CHECK OFMay 19, 2009 · Cndair CL6002C10SDR UALA2009051901418Actuator · faultyAILERON LOCKOUT EICAS AND OVERHEAD LT ON. REPLACED RT OTBD AILERON LOCKOUT ACTUATOR.May 18, 2009 · N648UA · Boeing 767322SDR UALA2009051501381Module · faultyAIL LOCK LT ON AT LOW SPEED. EICAS MSG AILERON LOCKOUT DISPLAYED. OTBD AILERONS INDICATED NORMAL, UNLOCKED. REPLACED RT STAB TRIM-AILERON LOCKOUT MODULE. OPS TEST NORMAL.May 14, 2009 · N659UA · Boeing 767322SDR CA090514005Bearing · seized(CAN) DURING FUNCTION CHECKS AFTER A PCU REPLACEMENT, A BINDING NOISE WAS HEARD COMING FROM THE RT AILERON. THE RT AILERON PCU OUTPUT LINKS (PN 27295-5 IPC 27-14-01, FIG. 1-175A) WERE TAKEN APART. THE OTBD PCU OUTPUT LINK BRG WAS SEIZED SO THAT THE BOLT WAS ROMay 13, 2009 · Cndair CL6002B19SDR UALA2009051101340Control Cable · lack of lubeCREW REPORTS DURING FLT CONT CHK, WHEN AILERONS DEFLECTED JUST OVER HALFWAY TO THE LT, A DEFINITE RESISTANCE IS FELT IN THE CONTROL WHEEL. TURNING CONTROL WHEEL TO THE RT IS NORMAL. CLEANED AND LUBED CABLES AND PULLEYS. CYCLED CAPTS AND FOS YOKES APPROX 30 TIMay 9, 2009 · N672UA · Boeing 767322SDR HALA2009050600170Aileron · out of rigACFT FLYS OUT OF TRIM OVER 1 1/2 DEGREE RT AILERON OVER 2 DEGREE RT RUDDER. ACFT WANTS TO ROLL LEFT CONSTANTLY. REMOVED SCREWS FOR LEFT WING PANELS 561BB, 561AB, AND 552HB. RE-RIGGED LT INBD AILERON PER AMM 27-11-08. CLOSED ACCESS PANELS 561BB, 561AB AND 5May 6, 2009 · N585HA · Boeing 7673G5SDR UALA2009050601303Actuator · faultyTHE "AIL LOCK" LT ON AT LOW SPEED. EICAS MSG AILERON LOCKOUT DISPLAYED. OUTBOARD AILERONS DID NOT INDICATE NORMAL - LOCKED OUT - BOTH. LEFT SAM FAULTS RIGHT LOCK OUT ACTUATOR, CONFIRMED ACTUATOR AT FAULT. REPLACED RT LOCK OUT ACTUATOR. OP CHECK GOOD.May 5, 2009 · N659UA · Boeing 767322SDR DL76L090817Indicator · inoperativeLEFT ELEVATOR INDICATION INOP, FWD TO MCO AND PLACARD PER MEL 27-08-01. REP CHK C/W OK FOR SERVICE.May 1, 2009 · N197DN · Boeing 767332SDR DXTA2009050103628Trim System · malfunctionedENROUTE, RECEIVED A (A AMBER BOX) ON THE PFD, FOLLOWED BY A RT ROLL TRIM RUNAWAY. FOLLOWED THE EMERGENCY CHECKLIST, DISCONNECTED TRIM AND PULLED CB. INSPECTED AND FOUND RIGHT SPOILER UP 10 DEGREES AND LEFT AT NEUTRAL, AND INSPECTED ACTUATOR WITH NO DEFECTS. Apr 30, 2009 · N138QS · Raythn 400ARAYTHEONSDR DXTA2009042903621Feel Unit · malfunctionedAT FL390 WITH AUTO PILOT ON ACFT APPEARED TO BE DUTCH ROLLING. WITH AP OFF, ACFT AILERONS ARE VERY STIFF & DIFFICULT TO OPERATE. ROLLS STARTED AT 2 DEGREES & FINALLY WAS DOING 15 DEGREES. SAT WAS -60 AND DECENDED TO FL 270. PROBLEM GREATLY REDUCED WITH TEMP SAApr 28, 2009 · N712QS · Gulstm 200SDR 2009FA0000345Control Cable · brokenAILERON CABLE SWAGE BROKE, CAUSING LOSS OF AILERON CONTROL.Apr 27, 2009 · N934V · Beech V35BSDR UALA2009042401188Pcu · failedFLAPERON POWER CONTROL UNIT (LEFT OUTBOARD) DOES NOT FOLLOW COMMAND. DB- PRIMARY FLIGHT COMPUTER (RIGHT) MSG-2710301 LATCHED TA MODE. REPLACED O/B FLAPERON PCU. ACPD MAT TEST AND TEST PASSED.Apr 24, 2009 · N215UA · Boeing 777222SDR CA090417001Control Cable · interferenceDURING DAILY PREFLIGHT INSPECTION RUBBING SOUNDS HEARD UNDER CABIN FLOOR WHEN MOVING CONTROL YOLK LEFT AND RIGHT (ROLL AXIX). INVESTIGATION OF SOUND REVEALED THAT TWO SCREWS (P/N S1021Z8-10) HOLDING STAINLESS STEEL SCUFFBOARD PLATE (P/N 04130264-4) TO CABIN FApr 16, 2009 · Cessna 150FSDR UALA2009041701122Actuator · faultyAILERON LOCKOUT EICAS CAME ON DESCENT PASSING 250KTS. REPLACED LT AILERON LOCKOUT ACTUATOR. OPS CHECK GOOD.Apr 16, 2009 · N664UA · Boeing 767322SDR CALA2009041400200Control Cable · out of rigUPON DEPARTURE AT ANC NOTICED CONTROL COLUMN VERY STIFF IN ROLL CONTROL, F/O AGREED. UPON LANDING IN SEA HAD CONTROL PROBLEM (ROLL) ALMOST UNABLE TO CONTROL A/C. FOUND CABLE TENSION LOW ON BOTH LT AND RT AILERON BODY CABLES, RIGGED AILERON BODY CABLES PER AMApr 14, 2009 · N18220 · Boeing 737824SDR CA090423003Control Panel · contaminated(CAN) CREW DECLARED EMERGENCY DUE TO AILERON JAM - LWD CAUTION ON FLIGHT, AP LWD CAUTION MESSAGE. AFTER DISENGAGEMENT OF THE AP, ACFT NEEDED VERY STRONG FORCE TO ROLL. NEARLY IMPOSSIBLE. SUDDENLY THE AILERONS BECAME FREE AND ACFT WAS NORMAL TO CONTROL WITH NOApr 1, 2009 · Cndair CL6002B19SDR HALA2009040100121Logic Card · malfunctionedETOPS SIGNIFICANT SYSTEM, BTB: AIL LOCK OVERHEAD PANEL LIGHT ON NO EICAS MESSAGE. PERFORMED FIM 27-11-00 FIG 104. NO FAULTS FOUND, PERFORMED AILERON L/O TEST, CHECKED OK REPLACED N10394 ANNUNCIATOR LOGIC CARD ASSY MM 33-16-02 OPS CK OK.Apr 1, 2009 · N587HA · Boeing 76733ASDR 2009FA0000267Control Rod · bentBOTH AILERON CONTROL TUBES P/N 50-521128-12 WERE BENT AND DISTORTED. REMOVAL OF TUBES FROM BELLCRANK AND AILERON NECESSARY FOR INSPECTION. SUSPECT DAMAGE INCURRED DUE TO GUST LOCK NOT BEING USED.Apr 1, 2009 · N549BR · Beech C90SDR CA090331004Screw · missing(CAN) THE PILOT NOTED HIS AILERON CONTROLS WERE SLUGGISH DURING FLIGHT AND THE CONTROL WHEEL WAS OFF CENTER DURING LEVEL FLIGHT. DURING ROUTINE INSPECTION, IT WAS FOUND THAT THE UPPER AILERON PULLEY BRACKET SCREW AND NUT WERE MISSING. THE PULLEY BRACKET WAS SLMar 20, 2009 · Cessna 150HSDR 2009FA0000239Bearing · wornTHE BUSHING PN 101-521046-5 THAT HOLDS THE BEARING PN4A INSIDE THE RT AILERON BELLCRANK PN 101-521046-3 WAS FOUND LOOSE IN THE BELLCRANK AND INDUCED A LOSS MOTION OF APPROX .75 INCH AT THE T/E WITH THE RIG PINS INSTALLED.Mar 20, 2009 · N6507B · Beech 200BEECH
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