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 0003369874Drain Valve · cloggedROLL CONTROL RESTRICTED IN FLIGHT IN BOTH AUTOPILOT AND MANUAL. THE FLIGHT CREW PERFORMED ROLL CONTROL RESTRICTION COM PROCEDURE. DESCENDED TO WARMER TEMPERATURES AND PROBLEM CLEARED. FLIGHT LANDED AT DESTINATION WITHOUT INCIDENT. MAINTENANCE REPLACED THE Sep 3, 2000 · N783NC · Doug DC951SDR COMA0060706Link · wornAIRCRAFT WANTS TO ROLL RIGHT. REQUIRES EXCESSIVE LWD TRIM. REPLACED WORN HARDWARE AT RIGHT HAND AILERON TO PCU CONNECTION.Sep 1, 2000 · N988CA · Cndair CL6002B19SDR AU000742Control Cable · separated(AUS) RIGHT AILERON CABLE SEPARATED FROM PULLEY AT RIGHT PULLEY SET LOCATED IMMEDIATELY INBOARD OF THE AILERON BELLCRANK. NO DAMAGE TO PULLEY OR CABLE. (X)Sep 1, 2000 · Cessna 207ASDR 20000906SH001Pulley · frozenLEFT REAR AILERON CABLE RUNNING ALONG THE OUTSIDE OF CABLE PULLEY AT WING ROOT. NO WEAR PATTERN APPARENT ON PULLEY SLOT INDICATING THAT THE CABLE WAS NEVER ON THE PULLEY SINCE MANUFACTURE. THE PULLEY WAS ALSO FROZEN. SUBMITTER STATED THEY HAVE FOUR NEW PA28RAug 31, 2000 · N773FT · Piper PA28R201SDR AU000779Aileron · seized(AUS) AILERONS JAMMED DURING CRUISE. AILERONS FREED DURING DESCENT. INVESTIGATION COULD FIND NO CAUSE OF JAMMING. SUSPECT ICING. (X)Aug 28, 2000 · Cessna 340CESSNASDR 20000913SH033Control Cable · frayedCABLE FRAYED AT FUSELAGE. RIGHT AILERON BALANCE CABLE. (X)Aug 28, 2000 · N4133D · Piper PA28181SDR 20000913SH032Control Cable · frayedLEFT AILERON FORWARD CABLE FRAYED. (X)Aug 28, 2000 · N4128X · Piper PA34220TSDR AU000852Bellcrank · faulty(AUS) PCA BELLCRANK SHEAR RIVETS FAILED. FOUND DURING INSPECTION IAW EI 767-027-0112 AND FAA AD 2000 17-05.Aug 26, 2000 · Boeing 767238SDR CA001004015Servo · failed(CAN) AILERON SERVO WILL NOT DISENGAGE WITH SERVO SWITCHED OFF. UNABLE TO DISENGAGE AUTO PILOT. AILERON SERVO AND NR 1 DIRECTIONAL GYRO CHANGED.Aug 25, 2000 · Doug DC932SDR EIA2000043Actuator · failedKLAX - AFTER TAKEOFF, RIGHT OUTBOARD AILERON NOT LOCKED WITH FLAPS UP. REPLACED RIGHT AILERON LOCKOUT ACTUATOR PER MM 27-11-16. (M)Aug 25, 2000 · N482EV · Boeing 747212BSDR AU000853Bellcrank · faulty(AUS) PCA BELLCRANK SHEAR RIVETS FAILED. FOUND DURING INSPECTION IAW EI 767-027-0112 AND FAA AD 2000-18-05.Aug 25, 2000 · Boeing 767338SDR 20000911SH029Control Cable · frayedLEFT HAND BALANCE CABLE FRAYED, NEW CABLE INSTALLED. (X)Aug 24, 2000 · N4177R · Piper PA34220TSDR 20000912SH027Control Cable · frayedRIGHT HAND AILERON BALANCE CABLE FRAYED AT WING ROOT PULLEY. (X)Aug 23, 2000 · N9299E · Piper PA34220TSDR GAIA00569Duct · crackedDISCREPANCY: DURING HEAVY CHECK FOUND: RIGHT HAND WING NR 6 SLAT INTERNAL RIB OUTBD OF ANTI-ICE DUCTING TUBE IS CRACKED (SLAT STA 161) CORRECTIVE ACTION: FABED DOUBLER REPAIR IAW SRM 57-30-3. STOP DRILL CRACK IAW SRM 51-10-1 INSTALLED DOUBLER REPAIR IAW SRM 57Aug 22, 2000 · N6810 · Boeing 727223SDR CA001004022Computer · failed(CAN) ECAM MESSAGE ''F/CTL SPR FAULT'' CAME ON SHORTLY AFTER REACHING CRUISE ALTITUDE. SPOILER ELEVATOR COMPUTER REPLACED AND CHECKED SERVICEABLE AS PER 767 MAINTENANCE MANUAL.Aug 21, 2000 · Airbus A320211SDR 20000911SH027Control Cable · frayedAILERON BALANCE CABLE FRAYED. LOCATED UNDER THE REAR SEATS. (X)Aug 21, 2000 · N4139A · Piper PA28181SDR CA000830029Aileron · jammed(CAN) THE FLIGHT CREW REPORTED AFTER TAKEOFF THE RIGHT AILERON APPEARS TO BE JAMMED. ON DESCENT, THE AILERON CAME UN-JAMMED AND APPEARED TO BE NORMAL.AILERON SERVO REPLACED AS PRE-CAUTIONARY MEASURE.Aug 20, 2000 · Cndair CL6002B19SDR QXEA0002386Bellcrank · gougedPDX- GOUGES IN LEFT HAND AILERON DUAL INPUT QUADRANT BELLCRANK ABOVE LOCKOUT ACTUATOR CYLINDER. REPAIRED IAW FOKKER SRM 51-10-4 AND HORIZON AIR EA 4-27-115.Aug 19, 2000 · N479AU · Fokker F28MK4000SDR SWIA971938Aileron · malfunctionedHEAVY AND SLUGGISH ROLL CONTROL IN AILERON. RETURNED TO LAX. INSPECTED AILERONS, FOUND NOTHING PROTRUDING. ALSO INSPECTED ALL BOLTS, ALL ARE SECURE. CONTROL YOKES FEEL NORMAL. OPS CHECKS GOOD.Aug 18, 2000 · N579SW · Emb EMB120ERSDR COMA0060647Aileron · stuckRIGHT AILERON APPEARS TO BE JAMMED. DURING DESCENT AILERON CONTROL RETURNED TO NORMAL. INSPECTED AILERON CONTROLS AND FOUND NO DEFECTS. COULD NOT DUPLICATE. AIRCRAFT FLIGHT CHECK SATISFACTORY.Aug 17, 2000 · N917CA · Cndair CL6002B19SDR 20000925SH038Control Cable · frayedAILERON BALANCE CABLE FRAYED. LOCATED UNDER THE REAR SEATS. (X)Aug 15, 2000 · N4142Q · Piper PA28181SDR 20000925SH031Control Cable · frayedLEFT HAND AILERON BALANCE CABLE FRAYED AT WING ROOT PULLEY. (X)Aug 15, 2000 · N4123C · Piper PA34220TSDR 20000925SH030Control Cable · frayedRIGHT HAND AILERON BALANCE CABLE FRAYED AT WING ROOT PULLEY. (X)Aug 15, 2000 · N4123C · Piper PA34220TSDR 20000911SH038Control Cable · frayedLEFT HAND AILERON BALANCE CABLE FRAYED AT WING ROOT PULLEY. (X)Aug 15, 2000 · N4123C · Piper PA34220TSDR 20000911SH037Control Cable · frayedRIGHT HAND AILERON BALANCE CABLE FRAYED AT WING ROOT PULLEY. (X)Aug 15, 2000 · N4123C · Piper PA34220TSDR 20000911SH026Control Cable · frayedAILERON BALANCE CABLE FRAYED. LOCATED UNDER THE REAR SEATS. (X)Aug 15, 2000 · Piper PA28181SDR 00FDEA00523Relay · failedLEVEL 2 ALERT IN-FLT AILERON DEFLECT DISAGREE. *S/D* REMOVED AND REPLACED RELAY R2-5060 PER SMP. REMOVED AND REPLACED FLAP HANDLE POS TRANSMITTER PER MD-11 MM 27-54-03. OPS CK OK.Aug 6, 2000 · N606FE · Doug MD11FSDR 20000911SH036Control Cable · frayedRIGHT HAND AILERON BALANCE CABLE FRAYED. LOCATED UNDER THE REAR SEATS. (X)Jul 25, 2000 · N4132D · Piper PA28181SDR 20000809SH023Control Cable · frayedRIGHT AILERON BALANCE CABLE FRAYED. LOCATED UNDER THE REAR SEATS. (X)Jul 25, 2000 · N4144P · Piper PA28181SDR 20000809SH022Control Cable · frayedRIGHT AILERON BALANCE CABLE FRAYED. LCOATED UNDER THE REAR SEATS. (X)Jul 25, 2000 · N4132D · Piper PA28181SDR 20000809SH025Control Cable · frayedRIGHT AILERON BALANCE CABLE FRAYED AT WING ROOT PULLEY. (X)Jul 24, 2000 · N4142N · Piper PA34220TSDR 20000809SH020Control Cable · frayedLEFT AILERON BALANCE CABLE FRAYED, LOCATED UNDER THE REAR SEATS. (X)Jul 19, 2000 · N9299B · Piper PA28181SDR 20000809SH018Control Cable · frayedLEFT AILERON BALANCE CABLE FRAYED, LOCATED UNDER THE REAR SEATS. (X)Jul 19, 2000 · N4163W · Piper PA28181SDR 00FDEA00477Controller · malfunctionedON LEVEL OFF RECEIVED DEFLECT AILERON ALERT, CK SYS DISPLAY SHOWED AILERON DEFLECTED IN CR AT .84. MEL 27-2 DEFLECTION AILERON SYS - INOP PER METHOD A ALL. AILERONS CONFIRM NOT DEFLECTED. *S/D* REACTIVATED DEFLECTION AILERON SYS PER MXP:27-2 IAW MD-11 WDM Jul 19, 2000 · N615FE · Doug MD11FSDR CA000720004Control Cable · frayed(CAN) WHILE CARRYING OUT AN 800 HOUR INSPECTION, THE RT AILERON CABLE WAS FOUND TO BE FRAYED. THE DAMAGE TO THE CABLE WAS LOCATED AT THE PULLEY WHERE THE CABLE GOES THROUGH THE COCKPIT FLOOR BY THE COPILOT SEAT. THE 800 HOUR INSPECTION REQUIRES THAT YOU INSJul 14, 2000 · Dhav DHC3SDR CA000713017Hinge · cracked(CAN) - CRACKS FOUND ON SEVERAL CONTROL SURFACE HINGE ON AIRCRAFT OPERATED IN THE U.K. - CRACKS VISABLE AS BUBBLED PAINT EXPOSED ON LOWER SURFACE.- ON REMOVAL OF PAINT, CRACK WAS FOUND RUNNING FROM HINGE PIN HOLE TO SURFACE. - PRESSED HINGE BUSHING WAS REMJul 13, 2000 · Diamon DA20A1SDR 0002943253Controller · malfunctionedDURING APPROACH AT 1500 FEET AGL AND FULLY CONFIGURED FOR LANDING, THE FIRST OFFICER DISCONNECTED THE AUTOPILOT AND AIRCRAFT ROLLED 30 - 40 FEET RIGHT. FIRST OFFICER PUT IN FULL LEFT CONTROL STICK WITH SMALL AMOUNT OF RUDDER AND AIRCRAFT ROLLED BACK 20 - 30 FJul 13, 2000 · N353NW · Airbus A320212SDR 20000809SH014Control Cable · frayedRIGHT AILERON BALANCE CABLE FRAYED LOCATED UNDER THE REAR SEATS. (X)Jul 13, 2000 · N4130W · Piper PA28181SDR QXEA0002042Actuator · misinstalledPDX- UNABLE TO INSTALL STEEL WASHER BETWEEN OUTBOARD SIDE OF BEARING IN THE AILERON ACTUATOR HOUSING AND AILERON HINGE BRACKET DUE TO INSUFFICIANT CLEARANCE. REPAIRED IAW HORIZON AIR EA 4-27-111.Jul 10, 2000 · N491US · Fokker F28MK4000SDR AU000549Pin · missing(AUS) LT INBOARD AILERON LOWER HALF PCA SUMMING LEVER/INPUT ROD PIVOT LINK PIN MISSING.Jul 10, 2000 · Boeing 767238SDR 20000829SH002Rod End · destroyedWHILE PERFORMING AEROBATICS (1/2 SNAP TO LEFT) THE LEFT AILERON DEPARTED AIRCRAFT. INVESTIGATION REVEALED CENTER AILERON HINGE HAD FAILED. LOW CYCLE FATIGUE. AIRCRAFT DESIGNER TO PERFORM A RE-EVALUATION OF THE HINGE DESIGN. AIRCRAFT IS LICENSED ''EXPERIMENJul 7, 2000 · N112KG · Amtr S300D2SDR F3LA00141Link · corrodedDURING C-7 CHECK, INSPECTION REPORTED CORROSION ON AILERON ACTUATOR REACTION LINK AROUND BEARING RETAINER AND A CRACK ON BEARING BOSS. MAINTENANCE REPLACED AILERON ACTUATOR REACTION LINK WITH NEW LOWER ASSY PER MM 27-11-101. (M)Jul 6, 2000 · N270FL · Boeing 7372L9SDR 20000809SH017Control Cable · frayedLEFT AILERON BALANCE CABLE FRAYED. LOCATED UNDER THE REAR SEATS. (X)Jul 5, 2000 · N4161Z · Piper PA28181SDR 20000809SH016Control Cable · frayedLEFT AILERON BALANCE CABLE FRAYED, LOCATED UNDER THE REAR SEATS. (X)Jul 5, 2000 · N4149Y · Piper PA28181SDR AU000513Bolt · loose(AUS) AILERON PULLEY PN S378-4 TO CENTER CONSOLE ATTACHMENT BOLT HAD THE NUT MISSING AND THE INCORRECT WASHER SPACING UNDER THE PULLEY GUARDS. (X)Jul 3, 2000 · Cessna 150MSDR CA000724020Bellcrank · cracked(CAN) THE RIGHT AILERON CONTROL BELLCRANK LOWER ANGLE WAS FOUND CRACKED DURING INSPECTION.Jun 27, 2000 · Piper PA28R200SDR SWIA971841Pcu · malfunctionedAFTER FLAPS WERE RETRACTED FOLLOWING TAKEOFF, AC ROLLED RIGHT, AILERON TRIM HAD TO BE DEFLECTED 50 PERCENT OF ITS TRAVEL TO MAKE AC FLY STRAIGHT. NOTE: FUEL WAS BALANCED. REMOVED AND REPLACED THE RIGHT AILERON TO PCU LINKS IAW MM 271415. MX REQUEST AN INFLJun 24, 2000 · N407SW · Cndair CL6002B19SDR UPS00232976Cartridge · out of adjINSPECTION TYPE:N/A ATB-AILERON BINDING T/S PER MM CHAPT 27-10-00 PG 102,106,AND 107 ADJUSTED AILERON SPRING CARTRIDGE PER MM 27-10-00 OPS CHECKS GOOD ***SUPPLEMENTAL MRR***Jun 23, 2000 · N906UP · Boeing 72730CSDR 20000809SH012Control Cable · frayedLEFT AILERON BALANCE CABLE FRAYED LOCATED UNDER THE REAR SEATS. (X)Jun 16, 2000 · N4122F · Piper PA28181SDR SIMA1782Control Rod · corrodedSAW - DURING MBV-2 INSPECTION, MAINTENANCE FOUND THE LEFT AILERON TRIM TAB CONTROL ROD CORRODED ON THE AFT END. THE CONTROL ROD WAS REMOVED AND REPLACCED IAW ATR JIC 27-11-72 RAI 1000-002. OPERATIONAL CHECK WAS SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVIJun 13, 2000 · N135MQ · Aerosp ATR42300
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