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 AU970212Control Rod · corroded(AUS) LH AND RH AILERON CONTROL ROD CONTAINED MEDIUM TO HEAVY CORROSION - FOUND DURING X-RAY INSPECTIONSDR 97ZZZX3134Control Cable · wornSHEATH ON RT OUTER AILERON INTERCONNECT CABLE WORN FLAT, SEVERAL PLACES. REMOVED AND REPLACED RT OUTER INTERCONNECTER CABLE, TENSIONED AND SAFTIED. GENERATED W/C NR 5039 TO C/W FUNCTIONAL CHECK OF AILERONS.SDR 97ZZZX3133Control Cable · corrodedRIGHT WING AILERON INTERCONNECT NON-SHEATHED CABLE IS CORRODED AT THE BELLCRANK AND REQUIRES CHANGE. REMOVED AND REPLACED RIGHT WING NON-SHEATHED INTERCONNECT CABLE, TENSIONED AND SAFTIED. (GENERATED W/C NR 5039 TO C/W FUNCTION CHECK OF THE AILERONS).SDR 97ZZZX3132Control Cable · wornLEFT WING AILERON INTERCONNECT SHEATHED CABLE IS WORN AND NEEDS TO BE CHANGED. REMOVED AND REPLACED LEFT WING SHEATHED CABLE, TENSIONED, AND SAFTIED. (GENERATED W/C NR 5039 FOR FUNCTIONAL CHECK OF THE AILERONS).SDR 97ZZZX3131Control Cable · corrodedRIGHT AILERON CABLES CORRODED IN WING ROOT AT PULLEYS. RE-CHECK WHEN LOOSE FOR OUTER CABLE REPLACEMENT. REMOVED AND REPLACED CENTER SECTION FORWARD AND AFT INTERCONNECT CABLES, TENSIONED, AND SAFTIED. (GENERATED W/C NR 5039 FOR FUNCTIONAL CHECK OF THE AILERSDR 97ZZZX3130Control Cable · corrodedTHE RIGHT MAIN AILERON CABLES ARE CORRODED ON PULLEY AT AIRCRAFT FRAME NR 24 WHERE CABLES EXIT THE FUSELAGE. CABLES REQUIRE CHANGING. REMOVED AND REPLACED BOTH RIGHT CENTER FUSELAGE TO WING ROOT AILERON CABLES IAW MM. GENERATED W/C FOR FUNCTION CHECK.SDR 97ZZZX3129Control Cable · corrodedRIGHT AILERON CABLES CORRODED AT BELLCRANKS IN OUTBOARD WING. REMOVED AND REPLACED BOTH RIGHT AILERON OUTBOARD CABLES IAW MM. GENERATED W/C FOR FUNCTION CHECK.SDR 97ZZZX3128Control Cable · corrodedTHE LEFT MAIN AILERON CABLES ARE CORRODED ON PULLEY AT AIRCRAFT FRAME NR 24 WHERE CABLES EXIT THE FUSELAGE (CABLES REQUIRE CHANGING). REMOVED AND REPLACED BOTH LEFT CENTER FUSELAGE TO WING ROOT AILERON CABLES IAW MM. GENERATED W/C FOR FUNCTION CHECK.SDR 97ZZZX3127Control Cable · corrodedLEFT WING HAS TWO CORRODED AILERON CABLE ENDS AT THE CONTROL QUADRANT ON REAR SPAR BETWEEN RIBS 10 AND 11. REMOVED AND REPLACED BOTH LT OUTBOARD AILERON CABLES IAW MM. GENERATED W/C FOR FUNCTION CHECK.SDR P5CA9700377Actuator · failedRIGHT OUTBOARD AILERON INDICATES NOT MOVING WITH FLAPS DOWN, VERIFIED NO MOVING BY GROUND CREW. REMOVED AND REPLACED RIGHT OUTBOARD AILERON LOCKOUT ACTUATOR PER BOEING M/M 27-11-16, OPERATIONAL CHECK PER 27-11-16.SDR HNAA9792323Aileron Controls · malfunctionedFLT 3241 - CHO-PIT - FLIGHT CONTROLS SEPARATED IN ROLL MODE DURING SHORT FINAL UNDER EXTREMELY TURBULENT CONDITIONS RESULTING IN NEUTRAL AILERON AND FULL DEPLOYED LEFT ROLL SPOILERS. INSPECTED ROLL DISCONNECT SYSTEM INCLUDING CABLES, CLUTCH MECHANISM, LEVERS SDR CALA9700234Power Contl Unit · inoperativeTHE AIRCRAFT HAD A BRIEF HISTORY OF STIFF AILERONS. MAINTENANCE FOUND THE B-SYSTEM AILERON POWER CONTROL UNIT AT FAULT. THE AILERON PCU WAS REMOVED AND REPLACED IAW MM 27-11-71, PAGE 401. AN ADJUSTMENT/TEST WAS PERFORMED ON THE AILERON PCU IAW MM 27-11-71, SDR 97ZZZX1899Pcu Filter Cap · burstTHE FILTER CAP BURST UNDER WORKING CONDITIONS FOR THE AILERON PCU. THE ALUMINUM FILTER CAPS ARE WEAKER THAN THE STEEL ONES. IT IS RECOMMENDED THAT ALUMINUM CAPS BE REPLACED COMPLETELY BY STEEL FILTER CAPS.SDR GTIA9700224Control Cable · frayedYIP - LEFT WING - AILERON CABLE FRAYED NEAR FAIR LEAD AT APPROXIMATELY STA XRS 353. MANUFACTURED AND INSTALLED CABLE, TENSIONED AND SAFTIED IAW DC-9 MM CHAPTER 27-10-0 PAGES 9 AND 10, AND CABLE TENSION CHART. (X)SDR 97ZZZX1178Control Cable · frayedREMOVED PANEL AT FLAP OUTBOARD HINGE AREA. INSPECTED AFT CABLE FOR WEAR WHERE IT GOES OVER ANTI-CHAFE BOX. THIS IS SECOND AIRCRAFT THAT AILERON CABLE WAS FOUND FRAYED AT THIS POINT.SDR GLBA97104Control Cable · wornAILERON CONTROL CABLES ARE WORN. REMOVED AND REPLACED AILERON CONTROL CABLES. (X)SDR COMA9710131Servo · bindingAILERONS BINDING AND NOISY WHEN MOVED LT OR RT. REPLACED THE AUTO PILOT SERVO. PART TOTAL CYCLES, 20,917.SDR 97ZZZX829Bracket · crackedTHE LOWER RT AILERON BELLCRANK BRACKET WAS CRACKED JUST ABOVE FORWARD AND REAR ATTACH BOLTS. SUSPECT CAUSE TAIL INTO WIND AND NO CONTROL LOCK.SDR CA970219006Control Cable · frayed(CAN) WHILE COMPLYING WITH FAIRCHILD 'B' INSPECTION, LEFT AILERON CONTROL CABLE WAS FOUND WITH THREE BROKEN STRANDS WHERE THE CABLE RUNS THROUGH THE PHENOLIC GUIDE BLOCK ATTACHED TO THE FUSELAGE BULKHEAD AT STATION 227-271. FAA AD 87-02-02 CALLS FOR CHECKS EVESDR P5CA9700219Connector · dirtyRIGHT OUTBOARD AILERON FAILED TO UNLOCK WITH FLAPS EXTENDED ON TAXI OUT FOR DEPARTURE. CLEANED CANNON PLUG ON RIGHT HAND AILERON LOCK OUT ACTUATOR.SDR P5CA9700153Connector · dirtyRIGHT OUTBOARD AILERON LOCK ACTUATOR FAILED TO OPERATE DURING TAXI. CLEANED CANNON PLUG AT ACTUATOR, OPERATIONAL CHECK OK PER BOEING MAINTENANCE MANUAL 27-11-00.SDR 97ZZZX801Control Cable · frayedAILERON CONTROL CABLES WHERE THEY PASS THROUGH WHEELWELLS APPEARED RUSTY, BUT NO BROKEN STRANDS. WHEN REMOVED TO INSPECT PER AC 43-13-1A, CHAPTER 4, PARA 198, AND FIGURE 4.14, MANY BROKEN STRANDS APPEARED.SDR 97ZZZX800Control Cable · frayedAILERON CONTROL CABLES WHERE THEY PASS THROUGH WHEELWELLS APPEARED RUSTY, BUT NO BROKEN STRANDS. WHEN REMOVED TO INSPECT PER AC 43-13-1A, CHAPTER 4, PARA 198, AND FIGURE 4.14, MANY BROKEN STRANDS APPEARED.SDR 97ZZZX799Control Cable · frayedAILERON CONTROL CABLES WHERE THEY PASS THROUGH WHEELWELLS APPEARED RUSTY, BUT NO BROKEN STRANDS. WHEN REMOVED TO INSPECT PER AC 43-13-1A, CHAPTER 4, PARA 198, AND FIGURE 4.14, MANY BROKEN STRANDS APPEARED.SDR ABXA9700813Bracket · corrodedDURING C-CHECK, THE RT AILERON PULLEY BRACKET IN THE WHEEL WELL WAS FOUND CORRODED. THE BRACKET WAS REPLACED IAW DC9 MM.SDR SIMA9700301Idler Arm · loose bearingDFW - DURING COMPLIANCE OF REPETITIVE INSPECTION OF AILERON CONTROL SYSTEM (AD 93-22-10), MAINTENANCE FOUND THE IDLER ARM IN THE LEFT WING OUTBOARD HAD A LOOSE BEARING. IDLER ARM ASSY WAS REMOVED AND REPLACED. OPERATIONAL CHECK WAS SATISFACTORY. AIRCRAFT WASDR ABXA9700810Bracket · corrodedDURING C-CHECK, THE LT AILERON PULLEY BRACKET IN WHEEL WELL WAS FOUND CORRODED. THE BRACKET WAS REPLACED IAW DC9 MM.SDR DL73K970138Controls · stiffAILERONS STIFF, NO BINDING FELT BUT RESISTANCE TO CONTROL WHEEL MOVEMENT GREATER THAN NORMAL. REPLACED 'A' AND 'B' SYSTEMS RETURN FILTERS, CHECKED ROLL FORCE TRANSMITTER AND VISUALLY INSPECTED PULLEYS AND CABLES.SDR 97ZZZX760Rod Attach · nut missingDURING C-CHECK INSPECTION OF THE LEFT OUTBOARD AILERON CONTROL ROD TO AILERON, INSPECTION REVEALED THE ATTACH BOLT'S NUT, WASHER, AND COTTER PIN WERE NOT INSTALLED (MISSING). THE BOLT MIGRATED APPROX .125 INCH OUTBOARD. SUSPECT DURING AILERON INSTALLATION, TSDR 97ZZZX616Torque Tube · wornUPON PERFORMING SB 1124-27-129 AND AD 96-24-11, FOUND WEAR INDICATED PER AD AND SB. FURTHER INSPECTION INDICATED GROOVES ON THE BOTTOM OF THE TUBE CAUSED BY THE EDGES OF THE ROLLERS. PILOT STATED THAT THE OTHER TUBE PREVIOUSLY REPLACED HAD THE SAME GROOVES ISDR 97ZZZM436Bracket · wornRIGHT AILERON INTERCONNECT CABLE CHAFING CABLE GUARD AND PULLEY BRACKET OF AILERON TRIM SYSTEM, ABOVE NR 4 FLAP TRACK. BRACKET AND CABLE ARE WORN. REPLACED ABOVE RIGHT AILERON INTERCONNECT PULLEY BRACKET W/C'S FOR WORN GUARD, DISTANCE TUBE AND RIGGING CHECKS.SDR ABXA9700867Bracket · corrodedDURING C-CHECK, THE AILERON BUS PULLEY BRACKET WAS FOUND CORRODED. THE BRACKET WAS REPLACED IAW DC9 MM 20-16-0.SDR SIMA9700151Idler Arm · loose bearingDFW - DURING COMPLIANCE OF EOE0-2700-001 (AD 93-22-10) REPETITIVE INSPECTION OF AILERON CONTROL SYSTEM, MAINTENANCE FOUND INBOARD IDLER ARE BEARING RIGHT WING LOOSE IN ARM. IDLER ARM ASSY WAS REMOVED AND REPLACED. OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SESDR 97UAL900058Connector · failedAILERON LOCKOUT LIGHT APPEARED DURING CLIMB AT APPROXIMATELY 300 KNOTS. THE AIRCRAFT CONTINUED TO JFK. FOUND SHORT AT LEFT AILERON ACTUATOR CONNECTOR. REPLACED THE CONNECTOR. PERFORMED OPERATIONAL CHECK.SDR 97UAL900026Control Mech · out of adjustAILERON TRIM EXCEEDS ONE UNIT LEFT WING. *S/D* FOUND THE RIGHT AILERON OUT OF RIG. RERIGGED RIGHT AILERON AND THE SYSTEM CHECKED OK.SDR 97ZZZX532Control Cable · frayedUPON INSPECTION OF AIRCRAFT CONTROL SYSTEMS, FOUND LEFT AILERON CABLE AT WS 57.00, WHERE THE CABLE PASSES THROUGH GUIDING PULLEY, WORN AND WITH BROKEN STRANDS ABOUT .50 INCH OF LENGTH. THIS CRS MAINTAINS A FLEET OF 17 LIKE TRAINING AIRCRAFT.SDR 97UAL900060Bearing · wornINBOARD AILERONS BINDED AT CRUISE ALTITUDE IN THE MANUAL MODE, AND WERE SMOOTH WITH THE AUTOPILOT CONNECTED. THE BEARING WAS GRITTY AND WORN. REPLACED BEARING ON FEEL AND CENTERING SPRING MECHANISM. INSPECTED CABLE RUNS IN E/E BAY AND BOTH LEFT AND RIGHT WISDR VTZA97072Control Cable · out of adjFLT 6481 - EWR-IAD - DURING CRUISE, MADE AN SCHEDULED LANDING AT IAD WITH ONE DISCREPANCY WHICH WAS BOTH YOKES HAVE EXCESSIVE PLAY, YOKES MOVE APPROX .75 INCH BEFORE AILERONS MOVE. AIRCRAFT WENT TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND ADJSDR TC8A96074Power Bypass · out of adjustON TAXI DURING CONTROL CHECK, AILERONS WENT INTO MANUAL REVERSION AND SYSTEM PRESS 800 PSI. ADJUSTED LT AND RT AILERON POWER BYPASS IAW DACO MM 27-5-2, OPS CHECKS GOOD.SDR 96UAL900995Control Wheel · lack of lubeTAKEOFF WITH 5 DEGREE FLAPS AILERON CONTROL VERY STIFF TO THE RIGHT WITH 'A' SYSTEM PRESSURE, NORMAL TO THE LEFT. *S/D* LUBED CAPTAINS AND FIRST OFFICERS CONTROL WHEEL YOKE SPADES. CYCLED CONTROL WHEEL TO WORK IN LUBRICANT. CONTROL WHEEL OPERATES SMOOTHLY.SDR P5CA9601255Spring · crackedON TAXI IN, FIRST OFFICERS CONTROLS STIFF. FOUND AILERON LOAD LIMITER SPRING BROKEN. REPLACED AILERON LOAD LIMITER AND OPERATIONAL CHECKED PER BOEING MAINTENANCE MANUAL 27-11-05.SDR DL72L962781Control Module · leakingSHORTLY AFTER T/O, AILERON SYS-A LIGHT ACCOMPANIED BY A LOSS OF SY-A HYD FLUID, APPROX 2 MIN AFTER. FOUND AILERON FLIGHT CONTROL MODULE LEAKING. REPLACED SAME, CHECKS NORMAL.SDR VTZA96458Yoke Cable · out of adjustFLT 6150 - IAD-EWR - DURING CRUISE, MADE A SCHEDULED FLIGHT WITH ONE DISCREPANCY WHICH WAS ONE INCH PLAY TO THE LEFT AND RIGHT IN YOKE CONTROLS WITH NO AILERON RESPONSE. AIRCRAFT WETN TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTION AND ADJUSTED YOKESDR WRLA96056Aileron Controls · failed testDURING TAXIING OUT, FLIGHT CREW NOTED RIGHT OUTBOARD AILERON FAILED CONTROL TEST. FLIGHT CREW ELECTED TO RETURN TO GATE. AIRCRAFT RETURNED TO GATE WITHOUT FURTHER INCIDENT. MAINTENANCE CREW PERFORMED AILERON TEST SEVERAL TIMES, EACH TIME SYSTEM PASSED WITH SDR CA970206016Turnbuckle · cracked(CAN) THREE CRACKS AT THE LEFT HAND THREAD END OF THE TURNBUCKLE BARREL WERE FOUND EXTENDING INWARD 0.50 INCHES ON TWO CRACKS AND 0.65 INCHES.SDR 9627052716Casting · failedDURING CLIMB AIRFRAME STARTED TO BUFFET. A VISUAL INSPECTION OF THE WINGS SHOWED THE INBOARD AILERONS FLUTTERING ABOUT TWO INCHES IN MOVEMENT ON BOTH WINGS. AIRCRAFT DUMPED FUEL AND RETURNED TO DTW AND LANDED WITHOUT INCIDENT. REPLACED LEFT HAND AILERON BELSDR ABXA9700365Damper Crank · corrodedDURING C-CHECK, THE AILERON DAMPER CRANK WAS FOUND CORRODED. THE DAMPER WAS REPLACED IAW DC-9 MM 27-10-4.SDR 97ZZZX172Bellcrank · wrong partDURING RIGGING CHECK AT ANNUAL INSPECTION FOUND THAT AILERONS COULD NOT REACH FULL TRAVEL UP OR DOWN. THE LT AILERON TRAVEL 21 DEGREES UP AND 11 DEGREES DOWN AND THE RT AILERON TRAVEL ONLY 13 DEGREES UP AND 18 DEGREES DOWN. INV. FOUND INCORRECT BELLCRANK INSSDR CA961220013Control Cable · frayed(CAN) LEFT HAND LOWER INBOARD AILERON CABLE FOUND CHAFING ON CLAMP P/N DSC70-40. CLAMP WAS INSTALLED IMPROPERLY SECURING SHROUD P/N DSC213-15, ON TO REFUEL/TRANSFER LINE AT LEFT HAND AFT SPAR STN YW196.SDR VTZA96427Trim Jack · lack of lubeFLT 6561 - GSO-IAD DURING CRUISE CRUISE, EXPERIENCED SLIGHT RESISTANCE TO AILERON TRIM PILOT INPUTS. AIRCRAFT LANDED AT IAD WHERE THE MAINTENANCE TECHNICIANS TROUBLESHOT THE DISCREPANCY AND FOUND THAT THE AILERON TRIM JACK NEEDED TO BE LUBRICATED. LUBRICATED
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