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 COMA9960272Pcu · leakingRIGHT AILERON OUTBOARD PCU LEAKING BEYOND LIMITS. REPLACED PCU.SDR 99ZZZX2525Cables · chafedWHILE PERFORMING A UNIFORMITY INSPECTION. FAA INSPECTORS DISCOVERED THE LT AND RT LOWER AILERON CABLES FRAYED WHERE THEY EXIT THE LOWER WING SKIN AT THE FAIRLEAD, APROXIMATELY 4 INCHES FROM THE THIMBLE EYE SPLICE. FAA INSPECTORS DISCOVERED THE LT AND RT LOWERSDR 99ZZZX2398Rod End · brokenDURING FLIGHT, LT AILERON WOULD NOT RESPOND TO CONTROLS. FOUND AFT LT ROD END BROKEN AT AFT SIDE OF LOCKNUT AND BEARING END FROZEN AND IMMOVABLE, EVEN AFTER REMOVAL. PILOT NOTICED AILERONS LOCKED ON GROUND WITH SEAT BELTS WITH LEFT AILERON DOWN POSITION WHENSDR 99ZZZX2640Rod · corrodedCORROSION LEFT WING AILERON PUSH/PULL ROD AND ROD END. 2-6-90: DATE OF MFG. TT ON AIRCRAFT: 2,400 HOURS.SDR UPS99229806Fitting · corrodedINSPECTION TYPE:C+SI, RIGHT I/B AILERON TAB PUSHROD MAST FITTING CORRODED. RIGHT I/B AILERON TAB MAST IS REPLACED IAW SRM 51-30-2.SDR C2XA99BT042Bracket · brokenDURING SCHEDULED EA 2710-01012 IN NEWARK, MAINTENANCE FOUND RIGHT OUTBOARD AILERON ROD END MOUNT BRACKET BROKEN. MAINTENANCE REMOVED AND REPLACED MOUNT BRACKET AND RETURNED AIRCRAFT TO SERVICE. (M)SDR 99ZZZX2348Bolt · looseON PRE-FLIGHT, PILOT COULD NOT MOVE AILERONS TO LEFT. UPON INVESTIGATION, FOUND LT AILERON UPSTOP BOLT BACKED OUT LEAVING ONLY A 4 DEGREE TRAVEL. FOUND STOP NUT LOOSE, BUT HELD IN PLACE BY TORQUE PUTTY. RE-ADJUSTED STOP TO OBTAIN PROPER TRAVEL PER SM AND CSDR SIMA991112Control Link · corrodedSAW - DURING MBV-1 INSPECTION, FOUND THE RIGHT AILERON TRIM TAB DUAL LOAD PATH CONTROL LINK EXFOLIATED. REMOVED AND REPLACED THE CONTROL LINK IAW JIC 271172-RAI-10000-002. AIRCRAFT RETURNED TO SERVICE. (M)SDR REXA99008Bearing · corrodedAILERONS HARD TO TURN TO THE LEFT. REMOVED AND REPLACED LEFT AND RIGHT TOWER MOUNT BEARINGS. (M)SDR 99ZZZX2170Bushing · wornOLD BUSHING IS PLASTIC MATERIAL. WEARS AND BECOMES BRITTLE. CAUSES EXCESS AILERON PLAY. DIFFICULT TO INSPECT AND WORK ON. LOCATION TOP OF CONTROL COLUMN FORWARD UNDER INSTRUMENT PANEL. NEW BUSHING UNIVAR PN 52119 IS MADE OF METAL. SUBMITTER STATED PLASTSDR MWEA99177Bushing · wornBUSHING WORN IN LT WING AILERON SECTOR SUPPORT. FABRICATED REPAIR BUSHINGS.SDR COMA9960146Dampener · leakingDURING C-CHECK, FOUND LEFT AILERON FLUTTER DAMPENER LEAKING. REPLACED FLUTTER DAMPENER.SDR AU990389Bearing · contaminated(AUS) AILERON FEEL, CENTERING AND TRIM MECHANISM SUPPORT BEARINGS CONTAMINATED WITH DIRT AND GRIT.SDR COMA9960154Bracket · brokenLEFT AILERON WILL NOT TRAVEL TO FULL DOWN 20.8 DEGREES. TRAVEL STOPS AT 18 DEGREES. FOUND AILERON PCU ATTACHMENT BRACKET CRACKED. REMOVED AND REPLACED LEFT AILERON ASSEMBLY WITH SERVICEABLE UNIT.SDR DHL9970164DPulley · corrodedAT D-CHECK, LEFT WING I/B AILERON / TURN AROUND PULLEY CASTING IS PITTED AT THE TOP AND BOTTOM OF CASTING. REMOVED AND REPLACED PULLEY PER MM 57-42-0.SDR 99FDEA00124Warning Light · illuminatedAIL DEFLECT DISAG LVL 2 ALERT ON FLAP RETRACTION, STAYED ON SLAT RETRACTION, GOES AWAY WHEN FLAPS EXT FOR LANDING. A/C RELEASED FOR SERV PER MEL/CDL 27-2 CATEGORY C EXP 4APR99 FCC1-FCC2 REPT NO FAULTS LAST LEG. PERF'D FCC1/FCC2 AIL SYS TEST PER MM 22-00-00-8SDR TWRA9909Rod · crackedDURING 'A' INSPECTION, FOUND THE FORCE LIMITER ROD CONNECTING THE L/R AILERON PROGRAMMER CRACKED (TWO PLACES). REMOVED AND REPLACED ROD ASSY. (M)SDR CA990413014Control Rod · corroded(CAN) INTERNAL CORROSION OF CONTROL RODS WAS FOUND. THE AILERON CONTROL ROD (RT) WAS CORRODED THROUGH AT ROD-END INBOARD TO ATTACHMENT LUG AT AILERON BELLCRANK. (WING ROOT AREA). PN F-52036 EXTERNAL CORROSION OF 50 PERCENT OF WALL THICKNESS WAS FOUND ON BOTSDR AT9900325Bracket · corrodedSCHEDULED INSPECTION AT AERO CORP, FL, FOUND THE LEFT HAND WING AILERON RUN AROUND CABLE PULLEY BRACKET CORRODED. REMOVED AND REPLACED LEFT HAND AILERON BUS CABLE RUN AROUND PULLEY BRACKET IAW DC9 MM 27-10-0 AND 20-16-0. RIG AND OPERATIONAL CHECK GOOD IAW DCSDR COMA9960121Aileron · wornRIGHT AILERON NEEDS TO BE REPLACED DUE TO FAILING THE BACKLASH CHECK. REPLACED RIGHT AILERON.SDR COMA9960120Aileron · wornLEFT AILERON NEEDS TO BE REPLACED DUE TO FAILING THE BACKLASH CHECK. REPLACED LEFT AILERON.SDR UPS99228976Fitting · corrodedINSPECTION TYPE-C, LT WING I/B AILERON TURN-AROUND PULLEY FITTING AT PULLEY BOLT HOLE IS CORRODED. REMOVED CORRODED PULLEY FITTING, DRILLED UP NEW FITTING AND INSTALLED IAW MM 20-10-20, SRM 51-30-05, 51-30-02.SDR CA990330074Actuator · failed(CAN) AILERON LOCKOUT MESSAGE ON ENGINE INDICATING AND ALERT AND CREW ALERT SYSTEM ON CLIMB AND DESCENT. REPLACED RT AILERON LOCKOUT ACTUATOR.SDR 99ZZZX1377Bearing · roughAILERONS FELT A LITTLE STIFF IN FLIGHT. CHECKED FOR FREEDOM OF MOVEMENT AND GROUND BY MOVING AILERONS UP AND DOWN BY HAND. NO ABNORMALITIES NOTED. WHILE RESTRICTING AILERON MOVEMENT BY HOLDING PRESSURE ON THE AILERON SURFACE, ROUGH BEARINGS WERE NOTED. ALLSDR 99ZZZX1376Bearing · roughAILERONS FELT A LITTLE STIFF IN FLIGHT. CHECKED FOR FREEDOM OF MOVEMENT AND GROUND BY MOVING AILERONS UP AND DOWN BY HAND. NO ABNORMALITIES NOTED. WHILE RESTRICTING AILERON MOVEMENT BY HOLDING PRESSURE ON THE AILERON SURFACE, ROUGH BEARINGS WERE NOTED. ALLSDR COMA9960093Dampener · leakingDURING C-CHECK, FOUND LEFT AILERON FLUTTER DAMPENER LEAKING AROUND PISTON SIGHT GLASS. REPLACED FLUTTER DAMPENER.SDR COMA9960080Link · wornLEFT AILERON FAILS BACKLASH CHECKS. REPLACED BOTH PCU LINKS.SDR AU990143Control Cable · misinstalled(AUS) LT AILERON FORWARD CONTROL CABLE (UPPER) FOUND TO BE ON THE WRONG SIDE OF THE CABLE KEEPER.SDR AALA990171Casting · crackedTUL - RIGHT INBOARD AILERON ACTUATOR CASTING IS CRACKED AT FORWARD LOWER INBOARD LOCATION. ACCOMPLISHED INTERIM REPAIR PER ESO 7349 DAGED 2-9-99. (M)SDR DHL9980549CBracket · crackedAT C-CHECK, RT WING AILERON POWER PACK COMPARTMENT DRIVE SECTOR QUADRANT BASE CRACKED LOWER O/B HOLE. REMOVED AND REPLACED BRACKET PER MM 27-13-2.SDR DHL99721002Controls · malfunctionedWHEN AILERON INPUT IS APPLIED A NULL AREA OF 10 DEGREES LEFT AND RIGHT IS DETECTED WITH NO ROLL RESPONSE. AILERON TRIM SET 1 UNIT RT, RUDDER 0. INSPECTED AILERON MOVEMENT, NO DEFECT NOTED AND CHECK LOST MOTION DEVICE, FOUND TO BE WITHIN LIMITS PER MM 22-61-5SDR 99ZZZX812Support · bindingCONTROL YOKE STICKING ON FLAREOUT AT LANDING. FOUND LEFT GUIDE SUPPORT WAS PUSHED UP TO GIVE CLEARANCE FOR ROLLER ON CONTROL YOKE ASSY THAT WAS BINDING WHEN IT CAME OUT OF GUIDE ASSY. ALSO, FOUND RIGHT GUIDE ASSY HAS BEEN SPREAD APART TO GIVE CLEARANCE FOR FSDR 99ZZZX1393Guide · malfunctionedDURING INSPECTION FOUND LEFT UPPER YOKE ROLLER DISENGAGING FROM SUPPORT GUIDE. REPLACED YOKE ASSY AND LEFT GUIDE SUPPORT. OPS CHECKS NORMAL.SDR 99ZZZX1392Yoke Assy · malfunctionedDURING INSPECTION FOUND LEFT UPPER YOKE ROLLER DISENGAGING FROM SUPPORT GUIDE. REPLACED YOKE ASSY AND LEFT GUIDE SUPPORT. OPS CHECKS NORMAL.SDR 99ZZZX1391Guide Assy · malfunctionedLEFT UPPER SIDE OF CONTROL YOKE ROLLER IS DISENGAGING FROM SUPPORT GUIDE WHEN SIDE PRESSURE IS APPLIED TO YOKE. CESSNA HAS FOUND THAT THE CONTROL YOKES IN ARE NOT WELDED CORRECTLY. REPLACED YOKE AND LEFT GUIDE SUPPORT, OPS CHECKS NORMAL.SDR 99ZZZX1390Yoke Assy · malfunctionedLEFT UPPER SIDE OF CONTROL YOKE ROLLER IS DISENGAGING FROM SUPPORT GUIDE WHEN SIDE PRESSURE IS APPLIED TO YOKE. CESSNA HAS FOUND THAT THE CONTROL YOKES IN ARE NOT WELDED CORRECTLY. REPLACED YOKE AND LEFT GUIDE SUPPORT, OPS CHECKS NORMAL.SDR 99ZZZX1010Switch · failedDUE TO A NO TAKEOFF WARNING ILLUMINATING AT 90 KNOTS, THE CREW REJECTED TAKEOFF. MAINTENANCE DISCOVERED A LOOSE PROXIMITY SWITCH AT THE AILERON/SPOILER DISCONNECT HANDLE. ADJUSTED PROXIMITY SWITCH AND PERFORMED OPS CHECK. MAINTENANCE RETURNED AIRCRAFT TO SESDR DL72W990134Bearing · rustedDURING TAXI CONTROL CK WAS NORMAL, AFTER T/O AILERONS WERE VERY HEAVY AND ABRUPT MOVEMENT CAUSED WHAT FELT LIKE MANUAL REVERSION. GROUND CHECKS AFTER LANDING SHOWS HEAVIER THAN NORMAL. FAST INPUT STILL SHOWS TENDENCY TO LOCK UP. REPLACED AILERON CENTERING SSDR CA990203024Actuator · failed(CAN) ENGINE INDICATING AND CREW ALERT SYSTEM MESSAGE AILERON LOCK OUT, OVERHEAD LIGHT. CHANGED RT AILERON LOCK ACTUATOR AND SLAT/AILERON MODULE, SYSTEM CHECKED SERVICEABLE.SDR ABXA9900023Controls · fodDURING DESCENT, AIRCRAFT WOULD NOT TURN TO THE LEFT. PILOT REPORTED FEELING SOMETHING 'SNAP'. AFTERWARDS, AIRCRAFT WAS VERY SLUGGISH TURNING TO THE LEFT. TURNED OK TO RIGHT. CREW DECLARED EMERGENCY, LANDING WAS UNEVENTFUL. *S/D* VISUALLY INSPECTED LEFT ASDR ARWA990105Bolt · wornMIA - FLT 9627 - ON PRE-FLIGHT, FOUND RT AILERON INBD TO OTBD SECTION 2 INCH SPLIT. TROUBLESHOT, FOUND EYE BOLT ATTACHING INBD/OTBD AILERON LOOSE AND WORN. REPLACED SAME IAW 211-11-02. OPERATIONAL PER MM 27-11-02. (X)SDR AU990004Control Cable · worn(AUS) AILERON CABLES SHOWED EXCESSIVE WEAR OVER PHENOLIC BLOCK FORWARD OF FLAP BAY - ESPECIALLY THE LEFT SIDE.SDR AU990003Control Cable · worn(AUS) AILERON CABLES SHOWED EXCESSIVE WEAR OVER PHENOLIC BLOCK FORWARD OF FLAP BAY - ESPECIALLY THE LEFT SIDE.SDR CA990203019Servo · malfunctioned(CAN) FLIGHT CONTROL AILERON SERVO FAULT WITH ASSOCIATED UNCOMMANDED ROLL TO ABOUT 20 DEGREES, INDICATION LEFT AILERON B SERVO IN AMBER ON ELEVATOR/AILERON COMPUTER 1. CENTRALIZED D FAULT DISPLAY SYSTEM FAULTED B-MODE VALVE 33C23. REPLACED LT AILERON B SERVOSDR QXEA9900297Bracket · corrodedPDX - AILERON PULLEY CLUSTER BRACKET HAS CORROSION STARTING AT PULLEY ATTACH BOLT. REPAIRED IAW FOKKER MM 27-11-00, PAGE 602, PARAGRAPH 3C (1).SDR EIA990097Control Cable · frayedDURING C-CHECK, LEFT AILERON CONTROL CABLE FOUND FRAYED AND ROUTED INCORRECTLY, NRC A-55. REPLACED CABLE AND RIGGED IAW MM 27-10-03. (M)SDR 9811009750Control Cable · frozenAT ALTITUDE, AILERONS FROZE IN POSITION WITH A MAXIMUM OF 10 DEGREES BANK WITH FULL YOKE FORCE APPLIED. AT 250 FT ABOVE GROUND LEVEL FULL AILERON CONTROL BECAME AVAILABLE AND AIRCRAFT LANDED AT DESTINATION WITHOUT INCIDENT. SUSPECT ICE ACCUMULATION ON AILEROSDR COMA9860403Dampener · leakingRIGHT AILERON FLUTTER DAMPENER LEAKING OUT OF LIMITS. REPLACED FLUTTER DAMPENER.SDR COMA9860404Dampener · leakingLEFT AILERON FLUTTER DAMPENER LEAKING OUT OF LIMITS. REPLACED FLUTTER DAMPENER.SDR VTZA98370Pin · chaffedFLT - 6524 - ROC-JFK - DURING APPROACH, AIRCRAFT MADE AN SCHEDULED LANDING WITH ONE DISCREPANCY WHICH WAS TRIM WARNING LIGHT ILLUMINATED. AIRCRAFT WENT TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND RESET AILERON TRIM TAB PIN, OPS CHECK OK. AIR
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