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 SIMA983495Crank Lever · looseDFW - DURING COMPLIANCE OF AD 93-12-10, FOUND CRANK LEVER IN RIGHT WING AT RIB 22 WITH LOOSE BEARING. REMOVED AND REPLACED CRANK LEVER. AIRCRAFT RETURNED TO SERVICE. (M)Dec 15, 1998 · N420AT · Aerosp ATR72212SDR SIMA983494Crank Lever · looseDFW - DURING COMPLIANCE OF AD 93-12-10, FOUND CRANK LEVER IN LEFT WING AT RIB 15 WITH LOOSE BEARING. REMOVED AND REPLACED CRANK LEVER. AIRCRAFT RETURNED TO SERVICE. (M)Dec 15, 1998 · N420AT · Aerosp ATR72212SDR SIMA983493Bellcrank · looseDFW - DURING COMPLIANCE OF AD 93-12-10, FOUND BELLCRANK IN RIGHT WING AT RIB 26 WITH LOOSE CENTER BEARING. REMOVED AND REPLACED BELLCRANK. AIRCRAFT RETURNED TO SERVICE. (M)Dec 15, 1998 · N420AT · Aerosp ATR72212SDR 98FDEA00740Disagree Light · activated98-298 - AILERON DEFLECTION DISAGREE ALERT AT SLAT RETRACT. ALERT DISAPPEAR FOR 1 MIN THEN RETURN ON THE CONFIG PG NO AILERON DEFLECTION SHOW ON CLEAN WING. A/C DEFER PER MEL 27-2 METHOD A.Dec 9, 1998 · N609FE · Doug MD11FSDR ORJA98307Controls · grindingIN RNO - RETURN TO GATE, DURING TAXI CHECKS GRINDING NOISE HEARD UNDER COCKPIT FLOOR WHEN AILERONS CHECKED. UPON RETURN TO GATE INSPECTED ALL CABLES IN E/E BAY UNDER COCKPIT FLOOR FOUND NO GRINDING NOISES OPERATED AILERON SYSTEM NUMEROUS TIMES RT AND LT. LT Dec 7, 1998 · N824RA · Doug DC982SDR 99ZZZX134Control Cable · out of rigDURING ROUTINE DAILY CHECK, AILERON WING CABLE TENSION WAS FOUND TO BE SO LOW THAT THE CABLES WERE DRAGGING ON THE LOWER SURFACE OF THE WING TRAILING EDGE. TENSION CHECKED 15 POUNDS. MAINTENANCE MANUAL CHAPT 27-10-00 PG 501 SPECS TENSION AT 35 PLUS OR MINUS Dec 7, 1998 · N787QS · Cessna 650SDR 99ZZZX133Control Cable · out of rigDURING ROUTINE DAILY CHECK, AILERON WING CABLE TENSION WAS FOUND TO BE SO LOW THAT THE CABLES WERE DRAGGING ON THE LOWER SURFACE OF THE WING TRAILING EDGE. TENSION CHECKED 19 POUNDS. MAINTENANCE MANUAL CHAPTER 27-10-00 PG 501 SPECS TENSION AT 35 PLUS OR MINUDec 7, 1998 · N789QS · Cessna 650SDR 99ZZZX131Control Cable · out of rigDURING ROUTINE DAILY CHECK, AILERON WING CABLE TENSION WAS FOUND SO LOW THE CABLES WERE DRAGGING ON THE LOWER SURFACE OF THE WING TRAILING EDGE. TENSION CHECKED 18 POUNDS. MAINTENANCE MANUAL CHAPT 27-10-00 PG 501 SPECS TENSION AT 35 PLUS OR MINUS 5 POUNDS ATDec 7, 1998 · N779QS · Cessna 650SDR 99ZZZX168Rod · looseON TAKEOFF JUST AFTER LIFT-OFF, PILOT NOTICED AILERON CONTROLS WERE HARD TO MOVE. SHORTLY AFTER THE PILOT NOTICED THE RT AILERON WAS NOT WORKING, RETURNED TO AIRPORT. UP ON A MAINTENANCE CHECK, NOTED THE CONTROL ROD FOR THE RT AILERON CONTROL WAS LOOSE. REMDec 4, 1998 · N7342B · Beech E35SDR AU981635Pushrod · broken(AUS) PILOT REPORTED THAT FLIGHT CONTROLS SEEMED SLOPPY WHILE INSPECTING THEM PRIOR TO FLIGHT. INSPECTION FOUND RIGHT AILERON PUSH-PULL ROD HAD BROKEN.Nov 23, 1998 · Bnorm BN2A8SDR SWAA982964Doubler · crackedDURING SCHEDULED D CHECK, FOUND CRACK IN AILERON QUADRANT DOUBLER AT BS 678, LBL AND RBL 25, WL 206. REPLACED PER BOEING SRM.Nov 19, 1998 · Boeing 7372H4SDR DLL19982379Servo · failedDURING APPROACH HAD DIFFICULTY FLYING STRAIGHT WITHOUT UNUSUALLY SEVERE RT AILERON AND RUDDER INPUTS SPI SHOWED LT OUTBD AILERON STUCK AT 8 UNITS UP. MTC IN PROGRESS LT AILERON NO MOVEMENT. REPLACED LT O/B AILERON SERVO, OPS CHECKS NORMAL.Nov 17, 1998 · N764DA · Lkheed 10113853SDR 99ZZZX163Support · crackedAFTER REMOVING SUPPORT ASSY ON A DC-8 INBOARD AILERON, CRACKS WERE NOTED ON 3 SUPPORT ASSEMBLIES. THE CRACKS WERE NOTED ON THE UPPER HOLES WHERE THE FITTING ASSEMBLY ATTACHES TO THE AFT SPAR OF THE INBOARD AILERON.Nov 11, 1998 · Doug DC852SDR 98ZZZX4687Actuator · leakingEXTERNAL LEAKAGE INTO WING TRAILING EDGE CAVITY. REPLACED ACTUATOR.Nov 10, 1998 · N38WP · Cessna 650SDR CA981113015Aileron · failed(CAN) ON APPROACH TO TORONTO AT FL 60 WITH FLAPS AT 5, SPEED BRAKES FULLY EXTENDED, SELECTED FLAPS AT 15, AIRCRAFT SHARP ROLL TO RIGHT, AILERONS 3 INDICIES LEFT TO KEEP A/C WING LEVEL, FLAPS RETURNED TO 5, NORMAL, NO ROLL, BACK TO FLAPS 15 DEGREES, SAME RESPONov 1, 1998 · Boeing 767233SDR DL73K982223Control Cable · frayedRT AILERON BINDING AT FULL RT TRAVEL. INSP FOUND AILERON CABLE SEGMENT ABSB-4 FRAYED. MANUFACTURED & INSTLD NEW CABLE SEGMENT ABSB-4 PER M/M. REPLD 2 EA AILERON BUS CABLE PULLEYS AT APPROX STA RBL 60. RIGGED AILERON BUS CABLES AND OPS CKD, ADJUSTED FIRST OOct 27, 1998 · N311DL · Boeing 737232SDR CA981125092Control Cable · frayed(CAN) THE AILERON CONTROL CABLE AT PULLEY STA 151.50 WAS FOUND WITH 4 OF 7 BROKEN STRANDS.Oct 26, 1998 · Bag BAE146200ASDR 98FDEA00665Disagree Light · malfunctioned98-254 - DURING FLAP RETRACTION, REVD LEVEL 2 AILERON DISAGREE ALERT. PERF AILERON DEFLECTION ADJUST TEST IAW 27-16-00-5. TOOK AILERON POS MEAS NEUTRAL, FULL THROW AND DEFLECT POS. COMPARED SENSOR READOUT DURING TEST, ALL WITHIN LIMITS. OPS CK SEVERAL TIMEOct 21, 1998 · N609FE · Doug MD11FSDR COMA9860316Controls · wornRIGHT AILERON FAILED BACKLASH CHECKS. REPLACED AILERON.Oct 18, 1998 · N941CA · Cndair CL6002B19SDR AU981625Control Cable · worn(AUS) RIGHT WING AILERON CONTROL CABLE P/N 82700522-001 WORN - FOUND DURING RE-TENSIONING.Oct 14, 1998 · Dhav DHC8102SDR AU981624Control Cable · worn(AUS) RIGHT WING AILERON CONTROL CABLE P/N 82700517-001 WORN - FOUND DURING RE-TENSIONING.Oct 14, 1998 · Dhav DHC8102SDR AU981623Control Cable · worn(AUS) RIGHT WING AILERON CONTROL CABLE WORN - FOUND DURING RE-TENSIONING.Oct 14, 1998 · Dhav DHC8102SDR AU981622Control Cable · worn(AUS RIGHT WING AILERON CONTROL CABLE WORN - FOUND DURING RE-TENSIONING.Oct 14, 1998 · Dhav DHC8202SDR COMA9860306Control Sys · wornFOUND RIGHT AILERON BACKLASH TOLERANCE OUT OF LIMITS ON BOTH SYSTEMS. REPLACED AILERON.Oct 12, 1998 · N920CA · Cndair CL6002B19SDR COMA9860305Control Sys · wornLEFT AILERON BACKLASH IS OUT OF TOLERANCE. REPLACED AILERON.Oct 11, 1998 · N920CA · Cndair CL6002B19SDR CA981030008Actuator · failed(CAN) AILERON LOCK OUT MESSAGE ON ENGINE INDICATING AND CREW ALERT SYSTEM AT 11,500 FEET AT 260 KNOTS. CHECK LIST COMPLETED, MESSAGE DISAPPEARED AT FLAP SELECTION 1 AT 210 KNOTS. CHANGED LEFT AND RIGHT AILERON LOCK-OUT ACTUATORS, SYSTEM SERVICEABLE.Oct 11, 1998 · Boeing 767209SDR UPS98228010Casting · corrodedINSPECTION TYPE:C ON REMOVAL OF LT INB AILERON TURNAROUND PULLEY, PULLEY CASTING FOUND CORRODED AT LWR LUG. REPLACED LT I/B TURNAROUND CASTING IAW SRM 51-30-02 AND MM 20-10-20.Oct 8, 1998 · N936UP · Boeing 727108CSDR AU981327Rod · corroded(AUS) RIGHT AILERON PUSH/PULL ROD FROM THE OUTBOARD WING BELLCRANK TO THE AILERON SEVERELY CORRODED AND STRESS CRACKED.Oct 8, 1998 · Sctaiv PIONEERSER3SDR CA981113012Bearing · sticking(CAN) RECURRING REPORTS OF AILERONS FAIL TO CENTER, FEEL+CENTERING MECHANISM REPLACED. SUBMITTER STATED FOUND SB 727-27-0154 CAPT AILERON DISCONNECT ASSEMBLY BEARING IMPROPERLY INSTALLED. REPAIRED.Oct 7, 1998 · Boeing 72727CSDR 99ZZZX112Control Cable · frayedDURING ANNUAL INSPECTION, TOP OF TUNNEL BETWEEN PILOT AND PASSENGERS SEAT WAS REMOVED. P/N 62701-002 AILERON CABLE, BOTH LT AND RT FOUND FRAYED. THE DAMAGE WAS BEHIND 2 METAL ROLLER PULLEYS THAT BOTH CABLES PASSED UNDER. PULLY P/N 62825-00. DAMAGE HARD TO Oct 4, 1998 · N8294W · Piper PA28180SDR CA981116005Control Cable · frayed(CAN) WHEN FLAPS WERE LOWERED, THE AILERON CABLES WERE FOUND FRAYED MIDWAY DOWN. BOTH LEFT AND RIGHT SIDE.Oct 1, 1998 · Cessna 421CSDR CA980930004Control Cable · chafed(CAN) AILERON CABLE FOUND WITH BROKEN STRANDS. ON REMOVAL, NUMEROUS STRANDS WERE FOUND WORN AND BROKEN.Sep 21, 1998 · Cessna 305ASDR P5CA9801478Valve · leakingINFLIGHT NR 3 HYDRAULIC QUANTITY DECREASED AT 1 GAL PER HOUR RATE. DEPRESSURIZED SYSTEM, FLUID LOSS STOPPED. SYSTEM DEPRESSURIZED UNTIL DESCENT. TROUBLESHOOTING CONFIRMED LEAK IN RIGHT HAND FLIGHT CONTROL SHUTOFF VALVE. VALVE REPLACED IAW BMM 27-13-01 PG 4Sep 20, 1998 · N858FT · Boeing 747123SDR DL76G981935Rod End · brokenROD END ON CONTROL ROD BETWEEN RT AIL LCCA AND RT LCCA TORQUE TUBE BROKEN. REPLACED INPUT ROD ASSY.Sep 17, 1998 · N169DZ · Boeing 767332SDR 98ZZZX4557Balance Cable · brokenDURING AN ANNUAL INSPECTION, DISCOVERED A FLAT SHINEY SPOT ON THE BOTTOM OF THE RIGHT AILERON BALANCE CABLE. THE LOCATION OF THE CABLE IN QUESTION IS IN THE RIGHT WING ROOT AREA JUST INBD OF THE WHEELWELL. UPON FURTHER INSPECTION, CABLE WAS FOUND TO HAVE SEVSep 10, 1998 · N92208 · Piper PA32R301SDR 98ZZZX4090Bolt · improper partWHILE PERFORMING AN INITIAL INSPECTION ON A NEW AIRCRAFT, DISCOVERED SEVERAL PLACES HAD INCORRECT OR IMPROPERLY INSTALLED HARDWARE. THE FORWARD BOLT ATTACHING THE LOWER CABIN DOOR HINGE HAD BEEN IMPROPERLY DRILLED AND INSTALLED SO THAT IT PREVENTED THE DOOR FSep 4, 1998 · N778AC · Bbavia 8GCBCSDR 98ZZZX3967Control Cable · corrodedATW - THE CENTER SECTION MAIN AILERON INTERCONNECT CABLES ARE CORRODED AT THE WING ROOT AREA. REMOVED AND REPLACED MAIN AILERON INTERCONNECT CENTER CABLES. GEN W/C FOR FUNCTIONAL TEST.Sep 2, 1998 · N179US · Bag BAE146200ASDR 98ZZZX3960Control Cable · corrodedATW - THE RIGHT MAIN AILERON CENTER SECTION OF CABLES ARE CORRODED AT THE LOWER PULLEY IN THE WING ROOT JUST AFT OF FRAME NR 29. REMOVED AND REPLACED THE RIGHT AILERON CENTER SECTION MAIN AILERON CONTROL CABLES. GEN W/C FOR FUNCTIONAL TEST.Sep 2, 1998 · N179US · Bag BAE146200ASDR 98ZZZX3449Bracket · brokenUPPER RIGHT AILERON PULLEY BRACKET BROKE. OLD UNDETECTED CRACK. PARTIAL LOSS OF AILERON CONTROL. BRACKETS CANNOT BE INSPECTED PROPERLY WITHOUT REMOVAL. SUGGEST ONE TIME INSPECTION.Aug 31, 1998 · N1867N · Cessna 120SDR COMA9860239Link · wornC-CHECK INSPECTION, RIGHT HAND AILERON OUTBOARD PCU LINK HAS EXCESS PLAY. REPLACED LINK.Aug 17, 1998 · N917CA · Cndair CL6002B19SDR 98ZZZX3579Control Cable · misinstalledDURING PHASE NR 1 ENGINE RUN, NOTICED A SLIGHT GRINDING NOISE WHEN PILOT'S CONTROL WHEEL WAS TURNED LT OR RT. A SLIGHT AMOUNT OF 'RATCHETING' COULD ALSO BE FELT IN THE WHEEL. BEYOND THAT, THE CONTROL WHEEL MOVED FREELY WITH NO BINDING. AFTER REMOVING PILOT'Aug 17, 1998 · N781C · Swrngn SA227ACSDR COMA9860226Link · wornDURING C-CHECK, FOUND RIGHT AILERON PCU LINKS TO HAVE EXCESSIVE PLAY. REPLACED BOTH LINKS.Aug 16, 1998 · N937CA · Cndair CL6002B19SDR RAIA980808Bearing · looseDURNG PRE-TAKEOFF CHECK, CREW NOTED RESTRICTION IN AILERON MOVEMENT. INSPECTION REVEALED THE ROLLER BEARING MIGRATED OUT OF THE CONTROL LINK. MAINTENANCE INSTALLED A NEW BEARING IAW SRM 51-70-02. (M)Aug 12, 1998 · N553HK · Jetair JETSTM4101SDR 98ZZZX4239Control Cable · twistedTHE AILERON CABLES IN THE RIGHT WING WERE FOUND WRAPPED AROUND EACH OTHER BETWEEN THE WING ROOT PULLEYS AND THE PULLEY AT THE OUTBOARD FLAP HINGE ARM.Aug 12, 1998 · N778AC · Bbavia 8GCBCSDR COMA9860225Hinge · wornC-CHECK INSPECTION, RIGHT HAND AILERON HINGE POINTS HAS EXCESSIVE PLAY. REPLACED AILERON.Aug 7, 1998 · N940CA · Cndair CL6002B19SDR COMA9860224Control Mech · wornCHECK INSPECTION, LEFT AILERON HAS EXCESSIVE PLAY. REPLACED AILERON.Aug 7, 1998 · N940CA · Cndair CL6002B19SDR 98ZZZX3274Control Cable · frayedAILERON CABLE FRAYED WHERE IT WENT OVER A PULLEY. PULLEY WAS NOT MOVING.Aug 6, 1998 · N4743Q · Cessna A185ESDR COMA9860213Bearings · wornDURING C-CHECK INSPECTION, FOUND RIGHT AILERON HAS WORN BEARINGS. REPLACED AILERON.Aug 2, 1998 · N916CA · Cndair CL6002B19SDR COMA9860215Pully · frozenDURING C-CHECK INSPECTION, FOUND RIGHT AILERON CABLE PULLY IS FROZEN. REPLACED PULLY.Aug 1, 1998 · N916CA · Cndair CL6002B19SDR COMA9860214Links · wornC-CHECK TASK 002-27-690-100, RIGHT AILERON PCU LINKS ARE WORN AND CHAFED. REPLACED LINKS.Aug 1, 1998 · N916CA · Cndair CL6002B19
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