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 DL73S954627Spring · brokenWHEN MAKING TURNS, CONTROL YOKE DOES NOT RETURN TO CENTER. IT MUST BE MANUALLY CENTERED. ROUND AILERON RETURN SPRINGS FOR MANUAL YOKE CENTERING BROKEN. REPLACED SPRINGS. OPERATION NORMAL.SDR SIMA953271Bell Crank Assy · worn bearingORD - DURING ACCOMPLISHMENT OF EO E9-2700-001 INSP OF AILERON CONTROL SYS, FOUND PENDULAR LEVER ASSY AT LT WING RIB STA NRS 16, 14, 13, AND 8, RT WING RIB STA NR 21 FAILED TOLERANCE REQUIREMENTS. RT WING BELL CRANK ASSY AT RIB STA NR 27 HAS EXCESSIVE MOVEMENTSDR 95ZZZX6815Bushing · mismanufacturedAILRON HAD EXCESSIVE PLAY. CLEVIS ROD END BUSHING HAD EXCESSIVE PLAY. WHEN NEW BUSHINGS, P/N 63900-119, WERE INSTALLED, THE OUTSIDE DIAMETER OF BUSHING WAS TOO SMALL (FELL OUT OF HOLE IN CLEVIS). NEW CLEVIS, P/N 554 687, WAS CHECKED AND THE BUSHING COULD BESDR 95ZZZX6625Crank Assy · worn bearingORD - DURING ACCOMPLISHMENT OF EO E9-2700-001 INSP OF AILERON CONTROL SYS, FOUND PENDULAR LEVER ASSY AT LT WING RIB STA NRS 16, 14, 13, AND 8, RT WING RIB STA NR 21 FAILED TOLERANCE REQUIREMENTS. RT WING BELL CRANK ASSY AT RIB STA NR 27 HAS EXCESSIVE MOVEMENTSDR 95ZZZX6624Crank Assy · worn bearingORD - DURING ACCOMPLISHMENT OF EO E9-2700-001 INSP OF AILERON CONTROL SYS, FOUND PENDULAR LEVER ASSY AT LT WING RIB STA NRS 16, 14, 13, AND 8, RT WING RIB STA NR 21 FAILED TOLERANCE REQUIREMENTS. RT WING BELL CRANK ASSY AT RIB STA NR 27 HAS EXCESSIVE MOVEMENTSDR 95ZZZX6623Rod Assy · bentORD - DURING ACCOMPLISHMENT OF EO E9-2700-001 INSP OF AILERON CONTROL SYS, FOUND PENDULAR LEVER ASSY AT LT WING RIB STA NRS 16, 14, 13, AND 8, RT WING RIB STA NR 21 FAILED TOLERANCE REQUIREMENTS. RT WING BELL CRANK ASSY AT RIB STA NR 27 HAS EXCESSIVE MOVEMENTSDR 95UAL900265Lever Assy · wornAILERON AUTOPILOT ACTUATOR LEVER ASSEMBLY WAS FOUND WITH SHEAR FASTENERS SHEARED. ONE FASTENER MAINTAINED CONNECTION BETWEEN THE POWER CONTROL UNIT AND THE LEVER ASSEMBLY. THE PLAY IN THE ASSEMBLY ELONGATED THE HOLES OF THE LEVER ATTACH HOLES AND CAUSED DRIFSDR SWIA95685Control Cable · wornLT AILERON CABLE OUTBOARD OF NACELLE IS WORN. REPLACED BOTH AILERON CABLES FOR LT AILERON.SDR CA951215022Panel · gouged(CAN)WITH REFERENCE TO AL-95-06, INSPECTION OF LOWER JAM QUADRANT, PANELS IN ROLL SPOILER 532DB (LH) AND 632DB (RH) AND FOUND GOUGED.SDR CA951215021Panel · gouged(CAN)WITH REFERENCE TO AL-95-06, INSPECTION OF LOWER JAM QUADRANT PANELS, PANEL 532DB (LH) AND 632DB (RH) FOUND GOUGED.SDR CA951215020Panels · gouged(CAN)WITH REFERENCE TO SDA AL-95-06, INSPECTION OF LOWER JAM QUADRANT PANELS CLAMP FOUND RUBBING ON ACCESS PANELS 532DB (LH) AND 632DB (RH).SDR 96ZZZX250Bearing · wornAILERON HAD EXCESSIVE PLAY. WHEN CLEVIS ROD END WAS REMOVED, BEARING FELL OUT OF BELLCRANK. BEARING WAS ALSO VERY WORN INSIDE RACE WITH BOTH AXIAL AND RADIAL PLAY. BELLCRANK WAS REPLACED 4-6-94 DUE TO SAME PROBLEM. INSTALLED NEW BEARING, PN 452603, INTO BESDR 96ZZZX249Bellcrank · wornAILERON HAD EXCESSIVE PLAY. WHEN CLEVIS ROD END WAS REMOVED, BEARING FELL OUT OF BELLCRANK. BEARING WAS ALSO VERY WORN INSIDE RACE WITH BOTH AXIAL AND RADIAL PLAY. BELLCRANK WAS REPLACED 4-6-94 DUE TO SAME PROBLEM. INSTALLED NEW BEARING, PN 452603, INTO BESDR DL767954374Spring · brokenON TAXI OUT, CHECKING CONTROLS F/O SIDE AILERONS EXTREMELY STIFF, VERY DIFFICULT TO MOVE. AFTER INSPECTION FOUND SPRING (P/N 69881284-2), BROKEN ON F/O AILERON DRUM ASSY (P/N 253T1142-3).SDR 96ZZZM352Cable · corrodedAILERON INTERCONNECT CABLE HAS CORROSION AT WING ROOT PULLEYS. REMOVED AND REPLACED BOTH CENTER SECTIONS OF AILERON INTERCONNECT CABLE IAW MM 27-11-44. REF W/C 6004 FOR FUNCTIONAL TEST OF AILERON CONTROLS.SDR SWIA95681Rod End · failedWHILE ON APPROACH, HEARD A POP AND LOST HALF OF AILERON CONTROLS. ON POST FLIGHT INSPECTION, FOUND TOWARD ROD END ON LT AILERON BELL CRANK TO BE BROKEN. REMOVED AND REPLACED BOTH FORWARD AND AFT ROD END ON LT AILERON BELL CRANK, TRAVEL CHECK GOOD.SDR CA951120006Control Cable · worn(CAN) DURING INSPECTION THE RIGHT AILERON CABLE WAS FOUND TO BE PARTIALLY WORN AT STA. YW170.SDR CA951120004Control Cable · worn(CAN) BOTH LEFT AND RIGHT AILERON CABLES WERE FOUND WORN 40 TO 50 PERCENT AT PULLEY AT STA. YW404.SDR CA951120003Control Cable · worn(CAN) LEFT AILERON CABLE FOUND 50 PERCENT WORN AT FAIRLEAD AT YW155.SDR 95ZZZM767Control Cable · wornDURING INSPECTION, THE RIGHT WING AILERON CABLE WAS FOUND TO BE WORN BY A PULLEY AT YW 170 RT. THE CABLE WAS REPLACED ON FIELD AVIATION COMPANY WORKORDER NR 21978 AT C-CHECK. (M)SDR 95ZZZM766Control Cable · wornDURING INSPECTION, THE LEFT WING AILERON CABLE WAS FOUND TO BE WORN 50 PERCENT BY A FAIRLEAD AT YW 155 LEFT. THE CABLE WAS REPLACED ON FIELD AVIATION COMPANY WORKORDER NR 21978 AT C-CHECK.SDR 95ZZZM764Control Cable · wornDURING INSPECTION, THE LEFT AND RIGHT WING AILERON CABLES WERE FOUND TO BE WORN 40 TO 50 PERCENT BY A PULLEY AT YW 404. THE CABLES WERE REPLACED ON FIELD AVIATION COMPANY WO NR 21978 AT C-CHECK.SDR EIAA9557Control Cable · out of adjJFK - LOG PAGE: F 03234 - AILERON CONTROL TO RIGHT BINDING, NO DIFFERENCE FLAPS RETRACTED/EXTENDED. RIGGED LOAD LIMIT INPUT CABLE REF M6670, RIGGED BACK DRIVE LOAD LIMIT ROD REF M6671, ADJUSTED RT AILERON INBD INPUT ROD REF 6672, OPS CHECK PER 27-11-00. (X)SDR CA960116001Link · broken(CAN)AILERON CHAIN LINK BROKE IN FLIGHT. PILOT ABLE TO LAND. FAILURE POSSIBLY CAUSED BY WORK HARDENING OF SHANK OF LINK WHICH CAUSED IT TO FRACTURE, POSSIBLY BECAUSE OF USE OF 'VICE-GRIPS' TO ADJUST AILERON TENSION. EVIDENCE TO THIS FOUND ON OTHER END OF LINK SDR PLG11595G1Roll Trim Tab · out of adjustFLT NR 4743 - PSM - AFTER TAKEOFF, THE AIRCRAFT ROLLED TO THE LEFT REQUIRING STANDBY TRIM TO MAINTAIN STRAIGHT AND LEVEL FLT. THE AIRCRAFT DIVERTED TO MHT LANDING WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT AND RERIGGED THE MAIN ROLL TURN TASDR 95ZZZX6917Control Cable · wornINSPECTION FOUND SEVERELY WORN RT AND LT UPPER AILERON CABLES RIGHT INSIDE THE WING ROOT WHERE CABLE ROLLS WITH A PULLEY. THERE WAS NO WORN PULLEYS. CABLE WAS SO BADLY WORN - 6 OF THE 7 BUNDLES OF STRANDS WERE BROKEN. IT IS IN AN AREA THAT IS HARD TO SEE. SSDR 95ZZZX7012Control Cable · corrodedSUBMITTER FOUND THE AILERON CABLE, JUST OUTBOARD OF THE WHEELWELLS, ALMOST RUSTED COMPLETELY THROUGH ON SEVERAL AIRPLANES. ONE HAD ONLY TWO STRANDS HOLDING. SUBMITTER STATED THE ONLY WAY TO INSPECT THESE CABLES IS TO DISCONNECT THEM AT THE AILERON BELLCRANK SDR CA951123104Cable · broken(CAN)AILERON LOCKOUT CABLE WAS FOUND BROKEN ON "A" CHECK. IT APPEARS THE CABLE JUMPED THE PULLEY AND OPERATED IN THIS STATE UNTIL IT FAILED. BROKEN CABLE WAS REPLACED AS PER MM 27-11-04.SDR CAL950984Pcu · leakingFLT NR 1790 - THE B-HYDRAULIC SYSTEM HAD A PARTIAL DROP IN QUANTITY WHILE EN ROUTE TO GSO. THE AIRCRAFT LANDED AT GSO WITHOUT INCIDENT. MAINTENANCE FOUND THE B-SYSTEM AILERON PCU LEAKING. THE AILERON PCU WAS REMOVED AND REPLACED IAW MM 27-11-71 AND OPERATIOSDR CA951109003Control Cable · worn(CAN) BOTH LEFT AND RIGHT WING AILERON LOWER CABLES WERE WORN BY PULLY AT YW400.SDR CA951108010Control Cable · worn(CAN) RIGHT WING AILERON LOWER CABLE FOUND WORN AT PULLEY STA YW190.SDR 96ZZZM6Control Cable · wornDURING INSPECTION OF AIRCRAFT, FOUND THAT THE LEFT AND RIGHT WING AILERON LOWER CABLES WERE WORN BY PULLEY AT YW 400. CABLE WAS REPLACED ON FIELD AVIATION COMPANY WORK ORDER NR 21973 AT C-CHECK.SDR 95ZZZM765Control Cable · wornDURING INSPECTION OF AIRCRAFT IT WAS NOTED THAT THE RIGHT WING AILERON LOWER CABLE WAS WORN BY A PULLEY AT YW 190RT. CABLE WAS REPLACED ON FIELD AVIATION COMPANY WORK ORDER NR 21973 AT C-CHECK. (M)SDR 95ZZZX6363Control Cable · damagedINSPECTION OF AILERON CABLE REVEALED NUMEROUS BROKEN STRANDS ON RIGHT LOWER AILERON CABLE AT STA YW177, RENDERING CABLE UNSERVICEABLE. THE CABLE WAS REPLACED AND RIGGED, A TEST FLIGHT WAS PERFORMED, AND THEN THE AIRCRAFT WAS RETURNED TO SERVICE.SDR CA951103011Control Cable · worn(CAN) AILERON CONTROL CABLE IN RIGHT HAND WING ROOT WORN DIRECTLY OUTBOARD OF SPLITTER QUADRANT.SDR CA951103010Control Cable · worn(CAN) AILERON CONTROL CABLE IN RIGHT HAND WING ROOT WORN DIRECTLY OUTBOARD OF SPLITTER QUADRANT.SDR CA951108022Cable Assembly · worn(CAN)DURING A DAILY INSPECTION, THE R/H AILERON WAS MOVED AT THE WING WHERE A RUBBING SOUND WAS HEARD. UPON INVESTIGATION, IT WAS DISCOVERED SEVERAL CABLE PASS THROUGH HOLES IN THE WING RIB WERE RUBBED BY THE CABLE. VERY LITTLE WEAR COULD BE SEEN ON THE CABLESDR P5CA9500822Aileron · locked outRETURNED TO BLOCKS DUE TO RIGHT HAND OUTBOARD AILERON LOCKED OUT WITH FLAPS AT 20 UNITS. INSPECTED RIGHT HAND OUTBOARD AILERON LOCKOUT ACTUATOR INSTRUMENTS AND WIRING. REMOVED, CLEANED, INSPECTED ELECTRICAL CONNECTIONS AND FOUND NO OBVIOUS DEFECTS, SYSTEM CHSDR CA951106203Control Cable · worn(CAN) RIGHT AILERON LOWER CABLE FOUND WORN AT PULLEY AT STA YW190. THIS CONDITION NOT VISIBLE WITH GUST LOCK ON AND AILERONS IN NEUTRAL.SDR 96ZZZM8Control Cable · wornDURING INSPECTION, FOUND THE RIGHT WING AILERON LOWER CABLE WAS WORN BY A PULLEY AT YW 190. IT SHOULD BE NOTED THAT THIS CONDITION IS NOT VISIBLE WITH THE GUST LOCK ENGAGED AND THE AILERONS IN NEUTRAL POSITION. CABLE WAS REPLACED ON FIELD AVIATION COMPANY WOSDR 96ZZZM7Control Cable · wornDURING INSPECTION, FOUND THAT THE RIGHT WING AILERON LOWER CABLE WAS WORN BY A PULLEY AT YW 190. IT SHOULD BE NOTED THAT THIS CONDITION IS NOT VISIBLE WITH THE GUST LOCK ENGAGED AND THE AILERONS IN NEUTRAL. THE CABLE WAS CHANGED ON FIELD AVIATION COMPANY WORSDR A6WR95048Bracket · corrodedDURING COMPLIANCE WITH SB 57-47, FOUND 2 EACH AILERON SERVO TAB BRACKETS CORRODED IN SPOT FACE AREA. REPLACED BRACKETS. (X)SDR SIMA952891Bearing · looseDFW - DURING COMPLIANCE OF ENGINEERING ORDER E9-2700-001 REPETITIVE INSPECTION OF AILERON CONTROL SYSTEM (AD 93-22-10). MAINTENANCE FOUND THE NR 4 IDLER ARM IN THE LEFT WING WITH A LOOSE BEARING. IDLER ARM WAS REMOVED AND REPAIRED BY INSTALLING A NEW BEARINGSDR CA951215018Bolt · worn(CAN)AT THE AILERON CABLES CONNECTION IN THE FUSELAGE AT THE FORWARD EXTREMITY OF LEVER ASSEMBLY P/N C2CF161A BOLT SHOWED SIGNS OF WEAR BY THE LINK CONTROL CABLE P/N C2CF307.SDR 96ZZZM624Control Cable · corrodedLEFT AILERON INTERCONNECT CABLE C2C-D IS CORRODED BEYOND MAINTENANCE MANUAL LIMITS, CABLE 63C AND 63B TURN BUCKLE HAS BARREL UNSAFETIED AND SLACKENED. REMOVED AND REPLACED LEFT AILERON INTERCONNECT CABLE IAW 146 MM 27-11-44 THROUGH STEP N6 PG 414. GENERATED SDR C2XA95CL120Control Cable · out of adjFLT NR 3747 - PWM-EWR - AILERON CABLE BANGING ON SIDE OF CONTROL COLUMN COVER, CAPTAIN'S SIDE. AIRCRAFT RETURNED TO PWM. MAINTENANCE ADJUSTED CAPTAIN'S AILERON CONTROL CABLE, NON-REGULATED LOOP IAW ATR JIC 27-11-14. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERSDR SWIA95628Contl Cables · out of adjustDURING PREFLIGHT CONTROL CHECK, FOUND EXCESSIVE PLAY IN CONTROLS, COPILOT WOULD MOVE WHILE CAPT WOULD REMAIN STATIONARY. INSPECTED AILERON CABLES FROM CONTROL COLUMN TO BELL CRANK, FOUND NORMAL. FOUND CABLE TENSION TO BE BELOW, ADJUSTED CABLES TO CORRECT TENSDR 9514783229Controller · malfunctionedDURING CRUISE, EXPERIENCED SEVERAL UNCOMMANDED AILERON ROLLS. THE RIGHT AILERON APPEARED TO MOVE ON THE ECAM PICTORIAL WHILE THE LEFT WAS STABLE. ALSO, RECEIVED ELAC 1 FAULT. AIRCRAFT CONTINUED TO SAN AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE CSDR 95ZZZX6697Pushrod · corrodedPUSHROD WAS CORRODED FROM INSIDE OUT, ABOUT MID-WAY DOWN LENGTH OF PUSHROD. CAUSED BY LACK OF CORROSION PROTECTION ON INSIDE OF PUSHROD. FOUND WHEN PUSHROD WAS REMOVED FROM C/W NEW NDT INSPECTION REQUIREMENT. ON VISUAL INSPECTION, FOUND .1250 INCH DIAMETER SDR AALA951720Control Cable · brokenDFW - DURING B-CHECK, LEFT AILERON TRIM LEFT WING DOWN CABLE FOUND BROKEN AND LEFT AILERON TRIM RIGHT WING DOWN CABLE WAS FOUND BIRD CAGED. REPLACED LEFT AILERON TRIM LEFT WING DOWN AND LEFT AILERON TRIM RIGHT WING DOWN CABLES. ACCOMPLISHED RIGGING AND SYSTE
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