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 CA960222035Panels · gouged(CAN)FOUND AS A RESULT OF SD ALERT AL-95-06 BOTH LEFT HAND (P/N 532DB) AND RIGHT HAND (P/N 632DB) PANELS GOUGED FROM LOWER JAM-SWITCH CABLE CLAMPS.SDR CA960222034Panel · gouged(CAN)FOUND AS A RESULT OF SD ALERT AL-95-06 RIGHT HAND PANEL GOUGED FROM LOWER JAM-SWITCH CABLE CLAMP.SDR CA960222033Panels · gouged(CAN)FOUND AS A RESULT OF SD ALERT AL-95-06 BOTH LEFT HAND (P/N 532DB) AND RIGHT HAND (P/N 632DB) PANELS GOUGED FROM LOWER JAM-SWITCH CABLE CLAMPS.SDR CA960222032Panels · gouged(CAN)FOUND AS A RESULT OF SD ALERT AL-95-06 BOTH LEFT HAND (P/N 532DB) AND RIGHT HAND (P/N 632DB) PANELS GOUDED FROM LOWER JAM-SWITCH CABLE CLAMPS.SDR CA960222031Panel · gouged(CAN)FOUND AS A RESULT OF SD ALERT AL-95-06 RIGHT HAND PANEL GOUGED FROM LOWER JAM-SWITCH CABLE CLAMPS.SDR CA960222030Panels · gouged(CAN)FOUND AS A RESULT OF SD ALERT AL-95-06, BOTH LEFT (P/N 532DB) AND RIGHT (P/N 632DB) PANELS GOUGED FROM LOWER JAM-SWITCH CABLE CLAMPS.SDR CA960222029Panel · gouged(CAN)FOUND AS A RESULT OF SD ALERT AL-95-06, BOTH LEFT (P/N 532DB) AND RIGHT (P/N 632DB) PANEL GOUGED FROM LOWER JAM-SWITCH CABLE CLAMPS.SDR CA960222028Panel · gouged(CAN)FOUND AS A RESULT OF SD ALERT AL-95-06 BOTH LEFT HAND (P/N 532DB) AND RIGHT HAND (P/N 632DB) PANELS GOUGED FROM LOWER JAM-SWITCH CABLE CLAMPS.SDR COMA9630036Bell Crank · seized bearingCREW REPORTS, THAT AILERONS ARE STIFF AND HARD TO MOVE. REPLACED THE LT INBD AILERON BELL CRANK ASSY.SDR COMA9660027Control Cable · lack of lubePILOTS AILERON CONTROLS SEEM TO BE EITHER LOOSE OR BINDING. INSPECTED AILERON CONTROL PATH AND FOUND NO DEFECTS. CLEANED AND LUBED AILERON CABLE PATH.SDR COEA9672801Rod End · seizedON TAKEOFF OUT OF PHOENIX, PILOT REPORTED FLIGHT CONTROL SURFACES VERY HARD TO MOVE IN-FLIGHT. ACFT RETURNED WITHOUT INCIDENT. INSPECTION REVEALED RT AILERON PUSH/PULL TUBE AFT ROD END SEIZED. MAINTENANCE REPLACED ROD END IAW CESSNA MM 27-10-01, RESET FUSELSDR DL767960286Bearing · failedON PREFLIGHT FLIGHT CONTROL CHECK, AILERON VERY STIFF TO MOVE ON BOTH PILOT CONTROL COLUMNS. FOUND BAD BEARING IN CENTERING MECHANISIM IN LEFT WHEEL WELL. REPLACED BEARING, OPERATION CHECK NORMAL.SDR UPS805356Aileron Light · illuminatedCREW REPORTED, AILERON CONTROL MANUAL LIGHT ILLUMINATED IN FLIGHT, NO LOSS OF HYD CHECKLIST COMPLETED AND LANDING UNEVENTFUL. INSPECTED AIL CABLES, PWR PACKS AND ALL ASSOCIATED SYSTEMS AND NO VISUAL DEFECTS NOTED. AIL HYD PWR SYSTEMS CHECKS NORMAL PER MM 27-SDR P5CA9600090Indicator · inoperativeRETURNED TO RAMP DUE TO IMPROPER RT OUTBOARD AILERON INDICATION. FUNCTIONAL CHECK OF ALL CONTROL SURFACES NORMAL, ALL COCKPIT INDICATIONS NORMAL IAW MM 27-00-00.SDR 9602216303Actuator · failedDURING CRUISE, AN AILERON LOCKOUT STATUS MESSAGE APPREARED ON EICAS. AIRCRAFT DUMPED 161,000 POUNDS OF FUEL, RETURNED TO DTW, AND LANDED WITHOUT INCIDENT. REPLACED THE RIGHT OUTBOARD AILERON ACTUATOR. OPERATIONAL CHECK OK. PART TOTAL CYCLES, 2,069.SDR P5CA9600083Eye Bolts · corrodedFOUND ALL EYE BOLTS ON PUSH-PULL RODS ON CCA PROGRAMMER CORRODED, RT W/G WHEEL WELL. REMOVED CORROSION IAW SRM 53-10-01, PAINTED IAW CP 20-40-00.SDR UPS205327Rod End · corrodedWHILE IN FOR C-CHECK MAINTENANCE REPORTED, RT WING O/B ROD END CLEVIS IS PITTED. REMOVED AND REPLACED RT WING O/B AILERON ROD END CLEVISES IAW MM 57-50-11 AND 27-10-00.SDR 96ZZZX1110Bushing · seizedDURING FLIGHT, AILERON TORQUE TUBE BUSHING SEIZED IN CONTROL YOKE TUBE EFFECTIVELY LOCKING AILERONS. BUSHING AND SHAFT ARE BOTH STEEL, RELATIVELY CLOSE FITTING AND HAVE NO MEANS OF LUBRICATION EXCEPT COMPLETE DISASSEMBLY. SUBMITTER RECOMMENDS OWNERS OF THE ASDR UPS205328Hinge Fitting · corrodedWHILE IN FOR C-CHECK MAINTENANCE REPORTED, RT WING O/B AILERON CENTER HINGE FITTING PITTED AILERON SIDE. REMOVED AND REPLACED CENTER HINGE FITTING IAW 51-30-2 AND MM 27-10-31. ALSO, FOUND CRACKED RIB SUPPORT BRACKET. REMOVED AND REPLACED BRACKET IAW SRM 51-SDR P5CA9600026Actuator · inoperativeDURING TAXI OUT, ON FLIGHT CONTROL CHECK, FOUND RT AILERON WOULD NOT UNLOCK FROM HIGH SPEED MODE WITH FLAPS IN TAKEOFF POSITION. RETURNED TO BLOCKS, APPLIED HEAT TO AILERON LOCKOUT ACTUATOR AND SYSTEM BECAME OPERATIVE. OPERATIONAL CHECK GOOD IAW MM 27-11-00.SDR UPS205325Hinge Arm · corrodedWHILE IN FOR C-CHECK MAINTENANCE REPORTED, LT I/B AILERON CENTER HINGE ARM IS CORRODED AROUND BOLT HOLE. REMOVED AND REPLACED HINGE ARM IAW MM 27-10-01 AND 27-10-0.SDR DHL96801007Press Switch · intermittentAILERON MANUAL CONTROL LIGHT ILLUMINATED AFTER TAKEOFF. ABNORMAL PROCEDURES FOLLOWED. REPLACED AILERON PCU PRESSURE SWITCH PER M/M 27-10 AND OPS CHECK OK.SDR 96ZZZX1361Cable Guard · chafedTHE AILERON LOWER SECTOR PLATE, CABLE GUARD, WAS CHAFING INTO THE PULLEY BOLT OF THE EMERGENCY GEAR BRACKET (PN 6514160-109) FROM INSUFFICIENT CLEARANCE. SHIMMED AILERON SECTOR UPWARD TO PROVIDE CLEARANCE.SDR A6WR95063Control Cable · corrodedDURING SCHEDULED INSPECTION FOUND AILERON INTERCONNECT CABLES CORRODED AT WING ROOT PULLEYS. REPLACED CABLES. REFERENCE: OPERATOR CONTROL NR 96ZZZX761. (X)SDR 96ZZZX761Control Cable · corrodedDURING SCHEDULED INSPECTION FOUND AILERON INTERCONNECT CABLES CORRODED AT WING ROOT PULLEYS. REPLACED CABLES. REFERENCE: OPERATOR CONTROL NR A6WR95063.SDR 96ZZZX690Control Cable · frayedDURING REPLACEMENT OF ORIGINAL CABLES, PARTS (CABLES) UNDER BALL ATTACHMENT WERE FOUND BROKEN AND FRAYED. CABLE WAS SEVERELY KINKED DURING ORIGINAL INSTALLATION AND EVENTUALLY BROKEN. NORMAL INSPECTION WOULD NOT SHOW DAMAGE. SUBMITTER SUGGESTS REMOVAL OF COSDR C2XA96IA015Bellcrank Brg · rustyIAH - DURING 1A CHECK INSPECTION, FOUND LEFT AILERON CONTROL SYSTEM BELLCRANK BEARING BINDING AND RUSTY. BELLCRANK LOCATED AT LEFT WING RIB 24, ACCESS THROUGH LOWER WING PANEL 523AB. MAINTENANCE REMOVED AND REPLACED THE BELLCRANK ASSEMBLY. AIRCRAFT APPROVEDSDR AU960195Control Cable · corroded(AUS) AILERON CABLES PNO 0501015-224 (2OFF) AND AILERON BALANCE CABLE PNO 0510105-13 (1OFF) CORRODED - TURNBARRELS PNO AN155B32L (1OFF), PNO AN155B165 (2OFF) AND PNO AN155B8L CORRODED - SUSPECT CAUSED BY POOR PREPARATION PRIOR TO PAINT STRIPPING AND THE USEOFSDR ABXA9600324Bearing · wornDURING C-CHECK INSPECTION, FOUND THE RIGHT AILERON TRIM TAB LINKAGE WORN. REPLACED TRIM TAB LINKAGE BEARINGS IAW DC-9 MM 20-10-1.SDR 96ZZZX618Cable Assy · misinstalledDURING ANNUAL INSPECTION, FOUND AILERON TRAVEL TO BE 14 DEGREES UP AND DOWN WHILE SPEC IS 20 DEGREES. STOPS ON AILERON BELLCRANK WERE NOT CONTACTING. UPON CLOSER INSPECTION, FOUND AILERON CABLE WEDGED BETWEEN 2 PULLEYS AT STA 51.5. THE PARTS CATALOG CALLS FSDR 96ZZZX604Control Cable · failedON NOVEMBER 11, 1995, AIRCRAFT EXPERIENCED WIND GUSTS AS HIGH AS 70 MPH FROM THE SOUTHEAST. THE AIRPLANE WAS TIED DOWN HEADING 330 DEGREES AND BOTH THE RUDDER GUST LOCK AND THE PIN IN THE YOKE WERE IN PLACE. THE NEXT DAY, THE RIGHT AILERON WAS DROOPING SLIGHSDR CA960110008Pulley · seized(CAN)AILERON PULLEY IN RIGHT HAND WING AT STA. 247.5 FOUND WITH BEARING SEIZED TO STUD AND SEVERAL BALLS MISSING. CABLE WAS WEARING INTO ONE SIDE OF GROOVE FLANGE.SDR 95UAL900325Controls · locked outAILERON LOCK OUT MESSAGE INDICATION OCCURRED AT 255 KNOTS AND 12,000 FEET DURING DESCENT. THE AILERONS EXTENDED AND LOCKED OUT. THIS INDICATION WILL BE ADDRESSED BY THE ACCOMPLISHMENT OF BOEING SERVICE LETTER 767-27-081-A.SDR 95UAL900317Controls · locked outAN AILERON LOCKOUT OCCURRED IN FLIGHT. THE EICAS DISPLAY VERIFIED THIS CONDITION. THIS INDICATION WILL BE ADDRESSED BY THE ACCOMPLISHMENT OF BOEING SERVICE LETTER 767-27-081-A.SDR SIMA953521Idler Arm · loose bearingDFW - DURING SCHEDULED COMPLIANCE OF ENGINEERING ORDER E9-2700-001R2 (REPETITIVE INSPECTION OF AILERON CONTROL SYSTEM, AD 93-22-10), THE NR 1 IDLER ARM IN THE RT WING WAS FOUND TO HAVE A LOOSE BEARING. IDLER ARM ASSY WAS REMOVED AND REPLACED. OPERATIONAL CHESDR SWIA95697Cables · wornRT AILERON CABLES WORN OUTBOARD OF NACELLE. REPLACED RT AILERON CABLES PER MM 27-00-01.SDR SWIA95696Control Cable · wornLT AILERON CABLES WORN OUTBOARD OF NACELLE. REPLACED LT AILERON CABLES PER MM 27-00-01.SDR CA960110509Actuator · failure(CAN)DURING FLIGHT - AILERON LOCKOUT - HARD FAULT. AILERON ACTUATOR CHANGED.SDR CA951218022Panel · gouged(CAN)IN ACCORDANCE WITH SDA AL-95-06 AND AOM 369 MINOR INTERFERENCE FOUND ON PANELS.SDR CA951215015Panel · gouged(CAN)IN ACCORDANCE WITH SDA AL-95-06 AND AOM 369 MINOR INTERFERENCE AND CHAFING FOUND ON EXISTING PANEL.SDR P5CA9500866Actuator · failedDURING FLIGHT CONTROL CHECK, RT OUTBOARD AILERON DID NOT MOVE. GATE TURN BACK. AIRCRAFT DISPATCHED TO SJU FOR LOCKOUT ACTUATOR CHANGE DUE TO STRIKE AT CAY. AILERON LOCKOUT ACTUATOR REPLACED IAW MM 27-11-16.SDR COMA9531205Controls · lack of lubeAILERONS ARE BINDING. INSPECTED AILERON SYSTEM AND NO FAULTS FOUND. LUBRICATED AILERON CENTERING CAMS AND ACFT RETURNED TO SERVICE.SDR CA951206003Panels · gouged(CAN)DURING INSPECTION FO SDA AL-95-06 BOTH LH AND RH ACCESS PANELS WERE WORN DUE TO FOULING OF ROLL SPOILER CLAMP. CLAMPS REPOSITIONED AND PANELS REPAIRED.SDR CA951206002Access Panel · fouled(CAN)INSPECTION AS PER AL-95-06 FOUND LH ROLL SPOILER CLAMP FOULING AGAINST PANEL. CLAMP REPOSITIONED AND PANEL REPAIRED.SDR SIMA953363Rod Assy · wornORD - WHILE PERFORMING INSPECTION FOR EO E9-2700-001 (INSPECTION OF AILERON CONTROL SYSTEM). FOUND LEFT WING RIB NR 24 BELL CRANK ASSY TO HAVE EXCESSIVE PLAY. LEFT WING AT RIB NR 20 ROD ASSEMBLY WAS BINDING. RIGHT WING AT RIB NR 24 BELL CRANK ASSY HAS PLAY.SDR 96ZZZM39Bell Crank · wornORD - WHILE PERFORMING INSPECTION FOR EO E9-2700-001 (INSPECTION OF AILERON CONTROL SYSTEM). FOUND LEFT WING RIB NR 24 BELL CRANK ASSY TO HAVE EXCESSIVE PLAY. LEFT WING AT RIB NR 20 ROD ASSEMBLY WAS BINDING. RIGHT WING AT RIB NR 24 BELL CRANK ASSY HAS PLAY.SDR 96ZZZM38Crank Assy · wornORD - WHILE PERFORMING INSPECTION FOR EO E9-2700-001 (INSPECTION OF AILERON CONTROL SYSTEM). FOUND LEFT WING RIB NR 24 BELL CRANK ASSY TO HAVE EXCESSIVE PLAY. LEFT WING AT RIB NR 20 ROD ASSEMBLY WAS BINDING. RIGHT WING AT RIB NR 24 BELL CRANK ASSY HAS PLAY.SDR 96ZZZM37Bell Crank · wornORD - WHILE PERFORMING INSPECTION FOR EO E9-2700-001 (INSPECTION OF AILERON CONTROL SYSTEM). FOUND LEFT WING RIB NR 24 BELL CRANK ASSY TO HAVE EXCESSIVE PLAY. LEFT WING AT RIB NR 20 ROD ASSEMBLY WAS BINDING. RIGHT WING AT RIB NR 24 BELL CRANK ASSY HAS PLAY.SDR 96ZZZM36Rod Assy · wornORD - WHILE PERFORMING INSPECTION FOR EO E9-2700-001 (INSPECTION OF AILERON CONTROL SYSTEM). FOUND LEFT WING RIB NR 24 BELL CRANK ASSY TO HAVE EXCESSIVE PLAY. LEFT WING AT RIB NR 20 ROD ASSEMBLY WAS BINDING. RIGHT WING AT RIB NR 24 BELL CRANK ASSY HAS PLAY.SDR 95FDEA01838Actuator · malfunctionedUPON FLAP/SLAT RETRACTION FOLLOWING T/O, AILERON DEFLECT DISAGREE LEVEL 2 LIGHT ILLUMINATED. PERFORMED ABNORMAL CHECKLIST IN RED BOOK PAGE 2-5-13 AND IAW CHECKLIST DUMPED FUEL AND RETURNED FOR LANDING. FOUND RT O/B AILERON FULLY DEFLECTED AND LT O/B AILERON
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