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 SIMA971831Idler Arm · loose bearingDFW - DURING COMPLIANCE OF ENGINEERING ORDER EO-2700-001 REPETITIVE INSPECTION OF AILERON CONTROL SYSTEM, AD 93-22-10, MTX FOUND ONE IDLER ARM IN LT WING BEHIND ENGINE EXHAUST PIPE WITH LOOSE BEARINGS. IDLER ARM REMOVED AND REPLACED AND OPS CHECK WAS SATISFACSDR ABXA9701388Bracket · crackedWHILE COMPLYING WITH 'D' INSPECTION, FOUND THE LEFT LATERAL CONTROL MIXER BRACKET CRACKED AND CORRODED. REPLACED LEFT LATERAL CONTROL MIXER BRACKET IAW DC-9 MAINTENANCE MANUAL CHAPTERS 20-16-0 AND 27-61-4.SDR AU971035Quadrant · contaminated(AUS) RH WING OUTBOARD AILERON LOWER QUADRANT BEARING WATER INGRESSSDR SIMA9701712Bellcrank · loose bearingDFW - DURING COMPLIANCE OF AD 93-22-10 REPETITIVE INSPECTION OF AILERON CONTROL SYSTEM, MX FOUND A BELLCRANK IN RIGHT WING AT THE AILERON WITH A LOOSE CENTER BEARING. BELLCRANK REMOVED AND REPLACED, AND OPS CHECK SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. SDR GLBA97102Control Cable · wornAILERON CONTROL CABLES ARE WORN. REMOVED AND REPLACED AILERON CONTROL CABLES. (X)SDR GLBA97106Control Cable · wornAILERON CONTROL CABLES ARE WORN. REMOVED AND REPLACED AILERON CONTROL CABLES. (X)SDR 97ZZZX2868Servo · leaksLEFT AILERON SERVO LEAKED EXCESSIVELY IN-FLIGHT, CAUSED LOSS OF NR 1 HYDRAULIC SYSTEM. SUBMITTER BELIEVES PISTON O-RING SEALS RUPTURED OR ROLLED. NOT SURE UNTIL INVESTIGATED.SDR CA970715018Control Cable · worn(CAN) AILERON CABLE VIBRATING ON REAR WING STRUT CAUSES WEAR ON BOTH THE AILERON CABLE AND THE STRUT. SUBMITTER STATES THAT THE OLDER WOODEN SUPPORTS DID NOT EXPERIENCE THIS PROBLEM. IT ONLY OCCURRED WITH THE NEW PLASTIC SUPPORTS.SDR GLBA97103Control Cable · wornAILERON CONTROL CABLES ARE WORN. REMOVED AND REPLACED AILERON CONTROL CABLES. (X)SDR 97ZZZM858Spring · corrodedRIGHT WING AILERON/SPOILER CAM BOX SPRING CORRODED. REMOVED AND REPLACED RIGHT WING AILERON/SPOILER CAM BOX SPRING.SDR GLBA97105Control Cable · wornAILERON CONTROL CABLES ARE WORN. REMOVED AND REPLACED AILERON CABLES. (X)SDR CA970610012Bracket · worn through(CAN) FAIRLEAD BRACKET ON LEFT REAR SPAR AT STATION 243 HAD BEEN WORN THROUGH BY AILERON CONTROL. ALSO FAIRLEAD AT STATION 207. (SEE SDR 970605009.)SDR CA970605009Bracket · worn through(CAN) FAIRLEAD BRACKET ON LEFT REAR SPAR STATION 207 HAD BEEN WORN THROUGH BY AILERON CONTROL CABLE. FAIRLEAD AT STA. 243 ALSO (SEE SDR 970610012).SDR DL76S971018Actuator · wornRT I/B AILERON POSITION VARIES BETWEEN 30 TO 50 DEGREES GREATER THAN LEFT I/B AILERON. OCCASIONALLY GREATER THAN 50 DEGREES DEFLECTION OBSERVED, THIS OCCURED DURING ALL PHASES OF FLT. MADE INFLT CK FOR POSSIBLE SPOILER FLOAT NEGATIVE RESULTS. REPLACED RT INSDR 97UAL900393Actuator · failedAILERON LOCK LIGHT CAME ON DURING CLIMB AT 300 KNOTS IAS. EICAS SHOWED NO OUTBOARD AILERON MOVEMENT DURING TURN. LIGHT WENT OUT BY ITSELF AFTER 20 MINUTES AT 0.80 MACH. *S/D* AN INVALID POSITION INDICATION FROM THE LEFT AILERON LOCKOUT ACTUATOR CAUSED THE SDR P5CA9701144Control Cable · wornLHW - O/B AILERON CONTROL CABLE AA-15, AA-13 FOUND WORN OUT OF LIMIT AT WS 1300 FAIRLEAD AREA AND WS 1260 PULLEY AREA. LHW O/B AILERON CONTROL CABLE AA-15, AA-13 REPLACED PER MM 20-11-03.SDR MASA97031Aileron Trim · misinstalledYKM/SEA - FLT 7847 - AFTER REPAIRS WERE MADE TO THE AILERON TRIM SYSTEM, ACFT WAS RELEASED FOR REVENUE SERVICE. AFTER DEPARTURE FROM YKM, THE CREW ADJUSTED THE DEPARTURE SETTINGS AND DISCOVERED THE AILERON TRIM SYSTEM WAS REVERSED. THE AIRCRAFT RETURNED TO TSDR 97ZZZM844Control Cable · corrodedCENTER AILERON INTERCONNECT CABLES ARE CORRODED. REMOVED AND REPLACED BOTH CENTER MAIN AILERON INTERCONNECT CABLES, TENSIONED TO PROPER SETTING AND SAFETIED, (GEN NEW W/C FOR FUNCTIONAL TEST).SDR 97ZZZM665Pcu · crackedFLT 741 - MCO - LOST HYDRAULIC 'A' SYSTEM PRESSURE AFTER LANDING AND EXITING THE RUNWAY. QTY WENT TO ZERO. REPLACED 'A' SYSTEM AILERON PCU (PCU HOUSING FOUND TO BE CRACKED). REPLACED 'A' SYSTEM MAIN HYDRAULIC FILTER. NO EVIDENCE OF METAL CONTAMINATION WAS SDR 97ZZZM856Cam Box Spring · corrodedRIGHT WING AILERON/SPOILER CAM BOX SPRING CORRODED. REMOVED AND REPLACED RIGHT WING AILERON/SPOILER CAM BOX SPRING.SDR SIMA9701253Bellcrank · loose bearingDFW - DURING COMPLIANCE OF ENGINEERING ORDER E9-2700-001 AD 92-22-10 REPETITIVE INSPECTION OF AILERON CONTROL SYSTEM, MAINTENANCE FOUND THE OUTBOARD AILERON BELLCRANK IN THE RIGHT WING WITH THE CENTER BEARINGS LOOSE. BELLCRANK REMOVED AND REPLACED. OPS CHECK SDR P2EA97032Transfer Mech · failedPAE - AILERON TRANSFER MECHANISM (LOST MOTION DEVICE) WOULD NOT RETURN THE CONTROL WHEEL TO ZERO (0) IN COUNTER CLOCKWISE DIRECTION ON CHECK. REMOVED AND REPLACED AILERON TRANSFER MECHANISM IAW MM 27-11-61. FUNCTIONAL CHECKS OK IAW MM 27-11-61. (M)SDR 97ZZZX2867Servo · leaksLEFT AILERON SERVO LEAKING EXCESSIVELY WITH NO SYSTEM PRESSURE APPLIED OTHER THAN 21 PSI ON HYDRAULIC TANK (HEAD PRESSURE). BELIEVE PISTON O-RING SEALS SPLIT OR ROLLED. NOT SURE UNTIL AERO PRECISION REPAIR AND OVERHAUL, INC., FL, HAS HAD AN OPPORTUNITY TO INSDR 97ZZZX2788Bellcrank · crackedINSPECTION FOUND LT AILERON BELLCRANK CRACKED. REF: PIPER SB 109.SDR 97ZZZX2782Bellcrank · crackedINSPECTION FOUND LT AILERON BELLCRANK CRACKED. REF: PIPER SB 109.SDR UPS97223065Support · corrodedINSPECTION TYPE:D, LT I/B AILERON TURNAROUND PULLEY SUPPORT CASTING CORRODED. CASTING REPLACED IAW MM 20-80-01.SDR 97ZZZX3140Control Cable · corrodedATW - THE RIGHT MAIN AILERON CABLES AT THE WING ROOT AFT LOWER PULLEY ARE CORRODED. REMOVED AND REPLACED RIGHT MAIN AILERON CABLES IN THE FUSELAGE AND WING ROOT AREA, TENSIONED AND SAFETIED IAW BAE MM. GENERATED W/C TO C/W A FUNCTIONAL TEST OF THE AILERONS.SDR 97ZZZX2087Control Cable · frayedDURING A 100-HOUR INSPECTION, RUST WAS FOUND ON RIGHT HAND AILERON CABLE AS IT PASSED THROUGH A PULLEY AT FS 217. AFTER CLEANING RUST OFF, NOTED CABLE WAS BROKEN THROUGH HALF OF ITS STRANDS. INVESTIGATION REVEALED THE RELIEF TUBE SIX INCHES AWAY HAD A CUT ISDR SWAA970389Pulleys · lack of lubeCREW REPORTED AILERONS BINDING. AIRCRAFT RETURNED TO OAK AND MADE AN UNEVENTFUL LANDING. INSPECTED AILERON CONTROL SYSTEM, NO DEFECTS. LUBED AILERON PULLEYS PER BOEING M/M.SDR SWAA970388Pcu Valve · malfunctionedIN CRUISE, AUTOPILOT HAD 2 UNCOMMANDED HARDS ROLLS, ONE TO THE LEFT AND ONE TO THE RIGHT, ESTIMATED AT 20 TO 30 DEGREES. AUTOPILOT DISENGAGED. REPLACED B-SYSTEM AILERON PCU TRANSFER VALVE PER BOEING M/M.SDR 97ZZZX3142Cables · corrodedATW - LEFT MAIN AILERON CABLES AT LEFT WING ROOT FORWARD PULLEY ARE CORRODED. REMOVED AND REPLACED BOTH WING ROOT MAIN AILERON CABLES (LEFT), TENSIONED AND SAFETIED IAW BAE MM. GENERATED W/C FOR FUNCTIONAL TEST.SDR 97ZZZX3145Control Cable · corrodedATW - THE RIGHT AILERON INTERCONNECT SHEATHED CABLE IS CORRODED AT OUTBOARD PULLEY AND QUAD. REMOVED AND REPLACED RIGHT SHEATHED CABLE, TENSIONED, AND SAFETIED. GENERATED W/C FOR AILERON FUNCTIONAL TEST.SDR 97ZZZX3143Cables · corrodedATW - THE AILERON CENTER INTERCONNECT CABLES (BOTH) ARE CORRODED AT THE WING ROOT PULLEYS. REMOVED AND REPLACED BOTH CENTER AILERON INTERCONNECT CABLES, TENSIONED AND SAFETIED. GENERATED SEPARATE WC FOR AILERON FUNCTIONAL TEST.SDR 97ZZZX2066Cable Clamp · bolt detachedBOLT AND NUT WHICH HOLD CLAMP ON AILERON CABLE SWEGE TO PULLEY FELL OUT ON COCKPIT FLOOR ALLOWING AILERON CONTROL CABLE TO SLIP AROUND CONTROL COLUMN CENTER PULLEY. THIS CAUSED PARTIAL LOSS OF AILERON CONTROL.SDR 97ZZZX2082Bungee Spring · brokenPILOT REPORTED A LOUD POPPING SOUND AND A BIND IN THE RUDDER PEDALS. A MECHANIC PERFORMED ROUTINE INSPECTION AND FOUND UPPER FORWARD RUDDER AILERON BUNGEE SPRING HAD BROKEN IN HALF ON THE CLIP END SIDE. SUBMITTER SUGGESTED DURING ROUTINE 100-HOUR ANNUAL PROGSDR 97ZZZX1989Bellcrank · mount debondedACFT HAD UNDERGONE A 50 HOUR INSP. NO DISCREPANCIES WERE NOTED IN THE AIL SYS WHEN THE BELLCRANKS WERE INSP NOR WAS ANY SLACK NOTED IN THE AIL SYS AT THE CONTROL STICK OR THE PUSH/PULL TUBES AT EACH AIL. DURING THE FIRST FLIGHT AFTER THE INSP WHILE PRACTICINSDR 98ZZZX1724Support · crackedDURING AN ANNUAL INSPECTION, BOTH UPPER AILERON BELLCRANKS SUPPORT BRACKETS WERE FOUND CRACKED. AILERONS WERE NOT PROPERLY RIGGED AND BELLCRANK WAS NOT CONTACTING AFT STUDS CAUSING A TWISTING ACTION ON SUPPORTS IN WINDY CONDITIONS.SDR 98ZZZX1723Support · crackedDURING AN ANNUAL INSPECTION, BOTH UPPER AILERON BELLCRANKS SUPPORT BRACKETS WERE FOUND CRACKED. AILERONS WERE NOT PROPERLY RIGGED AND BELLCRANK WAS NOT CONTACTING AFT STUDS CAUSING A TWISTING ACTION ON SUPPORTS IN WINDY CONDITIONS.SDR AU970337Actuator · broken(AUS) LH AILERON ACTUATOR ROD OUTER SEGMENT BROKEN DUE TO OUTER BALLJOINT SEIZING - RH AILERON OUTER BALL JOINT ALSO SEIZED WITHATTACHMENT BOLT LOOSE IN BRACKET - PERSONNEL/MAINTENANCE ERRORSDR AU970341Control Cable · corroded(AUS) LH AILERON CONTROL CABLE CONTAINED SEVERE CORROSION AND FRAYING IN AREA BENEATH CLAMP BETWEEN AUTOPILOT ROLL SERVO TO CONTROL CABLESDR ABXA9700438Bracket · corrodedDURING C-CHECK, THE LEFT AILERON PULLEY BRACKET IN THE LEFT WHEEL WELL WAS CORRODED. THE PULLEY BRACKET WAS REPLACED.SDR AU970378Turnbuckle · fouled(AUS) LH REAR AILERON CABLE TURNBUCKLE BETWEEN LH REAR AILERON CABLE PNO 5815103-26 AND BELLCRANK PNO 5815114-1 INTERMITTENTLY CATCHING ON FLOOR SUPPORT BRACKETSDR 97FDEA00197Cables · rustedN0739, AILERON CONTROL CABLES RUN NUMBER 9 E-F-G, 10 E-F-G. RUSTED AND WEAR OFF LIMITS.SDR 97FDEA00196Cables · rustedN0738, SPOILER CONTROL CABLES RUN NUMBER 15 A-B-C-D-E-F, 16 A-B-C-D-E-F, 17 A-B-C-D, 18 A-B-C-D. RUST AND WEAR OFF LIMITS.SDR 97FDEA00195Cables · rustedN0737, FLAP FOLLOW UP CONTROL CABLES RUN NUMBER 165A, 165B, 166A, 166B, 167A, 167B, 168A, 168B. RUSTED AND WEAR OFF LIMITS.SDR 97FDEA00193Cables · rustedN0735, AILERON LOCKOUT CONTROL CABLE RUN NUMBER 91B. RUSTED AND WEAR OFF LIMITS.SDR GLBA97107Control Cable · wornAILERON CONTROL CABLES ARE WORN. REMOVED AND REPLACED AILERON CONTROL CABLES. (X)SDR 97ZZZX1847Control Rod · defectiveFOUND PART TO HAVE A LOT OF PLAY SIDEWAYS TO ROD MOVEMENT. ALSO, PART DID NOT PASS THE AILERON LINEAR BALL BEARING INSPECTION/CHECK PER ASTRA MM 2710-02, PAGE 601. MEASURED OUTSIDE DIAMETER OF ROD OF REJECTED PART .618 INCH. MEASURED AGAINST ANOTHER KNOWN NSDR VJ970149Bracket · crackedDURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, THE FOLLOWING WAS FOUND, LEFT WHEELWELL, FORWARD BULKHEAD, OUTBOARD PULLEY BRACKET FOR AILERON AND SPOILER CABLES LOWER OUTBOARD ATTACH LEG CRACKED. REMOVED LT AILERON AND SPOILER PULLET BRACKET, OPSDR DHL9771265DBracket · corrosionAT D-CHECK, AT INBD AILERON ATTACH TO AFT SPAR, PULLEY BRACKET HAS CORROSION AROUND PULLEY BOLT HOLE OUTBD LOWER ATTACH POINT WITH CRACK AT OUTBD FWD PULLEY. REMOVED PULLEY BRACKET AND REPLACED PER M/M 27-10-0.
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