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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
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 SDR COMA0060706Link · wornAIRCRAFT WANTS TO ROLL RIGHT. REQUIRES EXCESSIVE LWD TRIM. REPLACED WORN HARDWARE AT RIGHT HAND AILERON TO PCU CONNECTION.SDR 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)SDR 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 PA28RSDR AU000779Aileron · seized(AUS) AILERONS JAMMED DURING CRUISE. AILERONS FREED DURING DESCENT. INVESTIGATION COULD FIND NO CAUSE OF JAMMING. SUSPECT ICING. (X)SDR 20000913SH033Control Cable · frayedCABLE FRAYED AT FUSELAGE. RIGHT AILERON BALANCE CABLE. (X)SDR 20000913SH032Control Cable · frayedLEFT AILERON FORWARD CABLE FRAYED. (X)SDR AU000852Bellcrank · faulty(AUS) PCA BELLCRANK SHEAR RIVETS FAILED. FOUND DURING INSPECTION IAW EI 767-027-0112 AND FAA AD 2000 17-05.SDR 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.SDR EIA2000043Actuator · failedKLAX - AFTER TAKEOFF, RIGHT OUTBOARD AILERON NOT LOCKED WITH FLAPS UP. REPLACED RIGHT AILERON LOCKOUT ACTUATOR PER MM 27-11-16. (M)SDR AU000853Bellcrank · faulty(AUS) PCA BELLCRANK SHEAR RIVETS FAILED. FOUND DURING INSPECTION IAW EI 767-027-0112 AND FAA AD 2000-18-05.SDR 20000911SH029Control Cable · frayedLEFT HAND BALANCE CABLE FRAYED, NEW CABLE INSTALLED. (X)SDR 20000912SH027Control Cable · frayedRIGHT HAND AILERON BALANCE CABLE FRAYED AT WING ROOT PULLEY. (X)SDR 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 57SDR 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.SDR 20000911SH027Control Cable · frayedAILERON BALANCE CABLE FRAYED. LOCATED UNDER THE REAR SEATS. (X)SDR 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.SDR 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.SDR 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.SDR 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.SDR 20000925SH038Control Cable · frayedAILERON BALANCE CABLE FRAYED. LOCATED UNDER THE REAR SEATS. (X)SDR 20000925SH031Control Cable · frayedLEFT HAND AILERON BALANCE CABLE FRAYED AT WING ROOT PULLEY. (X)SDR 20000925SH030Control Cable · frayedRIGHT HAND AILERON BALANCE CABLE FRAYED AT WING ROOT PULLEY. (X)SDR 20000911SH038Control Cable · frayedLEFT HAND AILERON BALANCE CABLE FRAYED AT WING ROOT PULLEY. (X)SDR 20000911SH037Control Cable · frayedRIGHT HAND AILERON BALANCE CABLE FRAYED AT WING ROOT PULLEY. (X)SDR 20000911SH026Control Cable · frayedAILERON BALANCE CABLE FRAYED. LOCATED UNDER THE REAR SEATS. (X)SDR 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.SDR 20000911SH036Control Cable · frayedRIGHT HAND AILERON BALANCE CABLE FRAYED. LOCATED UNDER THE REAR SEATS. (X)SDR 20000809SH023Control Cable · frayedRIGHT AILERON BALANCE CABLE FRAYED. LOCATED UNDER THE REAR SEATS. (X)SDR 20000809SH022Control Cable · frayedRIGHT AILERON BALANCE CABLE FRAYED. LCOATED UNDER THE REAR SEATS. (X)SDR 20000809SH025Control Cable · frayedRIGHT AILERON BALANCE CABLE FRAYED AT WING ROOT PULLEY. (X)SDR 20000809SH020Control Cable · frayedLEFT AILERON BALANCE CABLE FRAYED, LOCATED UNDER THE REAR SEATS. (X)SDR 20000809SH018Control Cable · frayedLEFT AILERON BALANCE CABLE FRAYED, LOCATED UNDER THE REAR SEATS. (X)SDR 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 SDR 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 INSSDR 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 REMSDR 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 FSDR 20000809SH014Control Cable · frayedRIGHT AILERON BALANCE CABLE FRAYED LOCATED UNDER THE REAR SEATS. (X)SDR 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.SDR AU000549Pin · missing(AUS) LT INBOARD AILERON LOWER HALF PCA SUMMING LEVER/INPUT ROD PIVOT LINK PIN MISSING.SDR 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 ''EXPERIMENSDR 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)SDR 20000809SH017Control Cable · frayedLEFT AILERON BALANCE CABLE FRAYED. LOCATED UNDER THE REAR SEATS. (X)SDR 20000809SH016Control Cable · frayedLEFT AILERON BALANCE CABLE FRAYED, LOCATED UNDER THE REAR SEATS. (X)SDR 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)SDR CA000724020Bellcrank · cracked(CAN) THE RIGHT AILERON CONTROL BELLCRANK LOWER ANGLE WAS FOUND CRACKED DURING INSPECTION.SDR 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 INFLSDR 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***SDR 20000809SH012Control Cable · frayedLEFT AILERON BALANCE CABLE FRAYED LOCATED UNDER THE REAR SEATS. (X)SDR 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 SERVI
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