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 CA050503014Aileron · dirty(CAN) AFTER T/O, RAIN CONDITIONS, CLIMBING INTO BELOW FREEZING TEMP, AILERONS BECAME STIFF. QRH CHECKS COMPLETED, FLIGHT CONTINUED. REMOVED WING PANELS, INSPECTED CABLE CONDITION FOR DRYNESS, WHITE POWDER. IF FOUND, REMOVED POWDER AND LUBRICATE IN FULL.. INSDR DXTA200500705Aileron · stuckHAD A "CATCH" IN THE ROLL CONTROL TURNING TO THE RIGHT, CONTROLS HEAVIER AFTER OR BEYOND THE CATCH. INSPECTED AILERON ROLL SPOILER SYSTEM BETWEEN CONTROL YOKES AND PCU'S. NO DEFECT NOTED. PERFORMED AILERON AND AILERON/SPOILER DISCONNECT CHECK IAW 750 MM, 27SDR YENA200529Actuator · malfunctionedAIRCRAFT EXPERIENCED WING FLUTTER ON CLIMB-OUT PASSING 6000 FT STEADY 250KIAS WHILE TURNING. NO ABNORMAL YAW, NO ABNORMAL INDICATION ON FLIGHT CONTROL ECAM PAGE. NO ABNORMAL INDICATION ON HYD ECAM PAGE. ONSET OF FLUTTER WAS FASTER AT HIGHER SPEED. MAX SPEEDSDR DL76G050239Actuator · leakingC-HYDRAULIC QUANTITY DECREASED IN FLIGHT. REPLACED O-RING ON NR 4 SPOILER ACTUATOR.SDR SWIA200514878Bearing · noisyNOISES CAN BE HEARD AND FELT WHILE MAKING AILERON INPUTS WITH THE CAPTIAN'S YOKE. REPLACED LEFT AILERON TORQUE TUBE BRACKET BEARING IAW AMM 27-11-05. OPERATIONAL CHECK GOOD.SDR 05FDEA00903Stud · corrodedRIGHT WING O/B AILERON ACTUATOR MOUNTING LWR I/B & O/B MOUNTING STUDS FOUND CORRODED. RT WING O/B AILERON ACTUATOR MOUNTING LWR I/B & O/B MOUNTING STUDS REMOVED AND REPLACED STUDS AS PER MM20-50-02.SDR 05FDEA00902Stud · corrodedRIGHT WING O/B AILERON ACTUATOR MOUNTING UPPER O/B STUD FOUND CORRODED. REMOVED AND REPLACED ON THE RT WING O/B AILERON ACTUATOR MOUNTING UPPER O/B STUD AS PER MM 20-50-02.SDR AU510001613Aileron · fod(AUS) RAG LODGED BETWEEN LT OB AILERON BALANCE CABLE PULLEY AND CABLE LOCATED BELOW CABIN FLOOR. FOD. PERSONNEL/MAINTENANCE ERROR. (CASA NR 510001613)SDR 2005FA0000482Manifold · brokenFILTER BOWL MOUNTING PORT IS BROKEN OFF AT THE BASE OF THREADS. FATIGUE. (MECHANIC LEB, JOB NR 194521) (K)SDR 2005FA0000650Hinge · crackedON ROUTINE PHASE INSPECTION, MECHANIC FOUND HINGE ON LT AILERON TRIM TAB CRACKED AT ATTACH POINT FOR PUSH PULL ROD. CAUSE AT THIS TIME UNKNOWN, NO RECOMMENDATIONS AT THIS TIME. (K)SDR 2005FA0000649Hinge · crackedON ROUTINE INSPECTION, MECHANIC FOUND HINGE ON LT AILERON TRIM TAB CRACKED AT ATTACH POINT FOR PUSH PULL ROD. CAUSE AT THIS TIME UNKNOWN, NO RECOMMENDATIONS AT THIS TIME. (K)SDR 2005FA0000648Hinge · crackedON ROUTINE PHASE INSPECTION, MECHANIC FOUND HINGE ON RT AILERON TRIM TAB CRACKED AT ATTACH POINT FOR PUSH PULL ROD. CAUSE AT THIS TIME UNKNOWN, NO RECOMMENDATIONS AT THIS TIME. (K)SDR DHL2005740005Structure · dentedRT WING INBD AILERON TAB IS DENTED ON LOWER SURFACE WING STA 430 WBL 269. CUT OUT DENT AT RT WING INBD AILERON TAB LOWER SURFACE APPROX 1 INCH DIA. FABRICATED FILLER APPROX 1 INCH DIA AND DOUBLER APPROX 3 INCH DIA FROM .010 2024T3 PO NR 9912184, BONDED, CURESDR DHL2005740014Skin · delaminatedRT WING OB AILERON TAB IS DELAMINATED AT OB EDGE. CUT OUT DELAMINATED AREA AT RT WING OB AILERON TAB, FABRICATED FILLER AND DOUBLER, BONDED FILLER AND DOUBLER, CURED, CLEANED, PRIMED AND SEALED IAW B727 SRM 57-50-2 AND 51-40-20 FIG 30.SDR DHL2005740008Skin · dentedLT WING OB AILERON UPPER SURFACE HAS DENT WBL 490. REMOVED FASTENER AND CUT OUT DAMAGED AREA IAW B727 SRM 51-30-2 AND 57-50-5. FABBED DOUBLER AND FILLER IAW B727 SRM 57-50-51 AND 57-50-2. TREATED, PRIMED, AND INSTALLED DOUBLER AND FILLER AT L/WING OB AILEROSDR BB05022Lockout · faultyPHL FL 1237, CREW RECEIVED THE EICAS MESSAGES (AIL LOCKOUT) AND (RUDDER RATIO), AND THE ASSOCIATED LIGHTS. CREW WAS ALSO HAVING PROBLEMS WITH THE AUTO THROTTLES DISENGAGING REPEATEDLY. FLIGHT RETURNED TO PHL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCESDR DL73S050180Pcu · malfunctionedAFTER MOVING FLAPS TO 5 DEGREES SYS-A HYD QTY DROPPED TO ZERO. REPLACED LOWER A-SYSTEM AILERON PCU FOR LEAKING.SDR CA050405011Turnbuckle · cracked(CAN) ON CHANGING THE RIGHT HAND AILERON CABLE AT WING STATION 70, THE CONNECTING TURNBUCKLE WAS FOUND CRACKED PN MS21251-B5S.SDR WRLA2005083Relay · inoperativeITEM: CI217/10 ANC/TPE AIR TURNBACK DUE TO LEVEL II (AIR DEFLECT DISAG), DUMPED FUEL AND RETURNED TO BASE. REPLACED AILERON DEFLECT CONTROL RELAY R2-5060. RTS FCC 1 AND 2 ALL PASSED. RAN AILERON TO FULL DEFLECT AND CYCLED FLAPS, ALL CHECKS NORMAL.SDR CA050329011Rod · cracked(CAN) LT AILERON PUSH PULL ROD REMOVED TO CLEAN CORROSION FROM STEEL ENDS, AFTER CLEANING INSPECTION REVEALED A CRACK PROGRESSING FROM THE INNER RIVET. SUSPECT CRACK FROM AGE HARDENING OF COMPONENT, APPROXIMATELY 61 YEARS OF AGE.SDR WRNA200500003Actuator · unserviceableLT LOW SPEED AILERON FAILED TO DISCONNECT UPON SLAT RETRACTION. FUEL DUMP PROCEDURES FOLLOWED, AIRCRAFT RETURNED TO AIR FIELD, LANDING NORMAL. MANUALLY DISCONNECT LOW SPEED AILERON. LOCK OUT ACTUATOR I/A/W 27-00-00, VERIFIED ROD IS RETRACTED AND IN DISCONNECSDR CA050223009Sleeve · crimped(CAN) UPON ASSY OF NEW .0937 INCH STAINLESS STEEL CONTROL CABLES. IT WAS DISCOVERED THAT THE NICOPRESS SLEEVES WERE NOT CRIMPED SUFFICIENTLY. SOME CABLES PULL TESTED ACTUALLY PULLED APART. THE NICOPRESS TOOL WAS CALIBRATED USING THE TOOL GO/NO-GO GAUGE. IT ASDR CA050224005Clamp · obstructed(CAN) WHEN THE AILERON CONTROL WAS MOVED TO THE EXTREME LT, THE CONTROL WOULD OCCASIONALLY CATCH MOMENTARILY AND THEN RELEASE. UPON FURTHER EXAMINATION OF THE AILERON CONTROL SYSTEM, THE AUTOPILOT CLAMP ON THE LT AILERON CABLE WAS FOUND TO BE CATCHING ON THE DSDR VNAA0502001Warning Light · illuminatedDURING TAKEOFF ROLL AT PHL THE CREW OF FLIGHT 2470 RECEIVED A CONFIG AILERON WARNING WHEN THE YOKE WAS MOVED FOR CROSSWIND CORRECTION. THE CREW ABORTED THE TAKEOFF AND TAXIED BACK TO THE GATE. PSA MAINTENANCE FOUND THE AILERON TRIM SET OUT OF THE TAKEOFF RANSDR SWIA200514484Actuator · malfunctionedAILERON TRIM INDICATION WOULD MOVE BOTH LWD/ RWD TRIM 0 DEGREES TO 15 DEGREES ON ITS OWN (INDICATION ONLY). REMOVED AND REPLACED AILERON ACTUATOR IAW CRJ 700 MM 27-12-01. PERFORMED OPERATIONAL CHECK IAW CRJ 700 MM 27-11-00.SDR MALA050222Tab · looseYOKE VIBRATED BACK AND FORTH AT SPEEDS OF 250KTS AND GREATER. AS THE SPEED INCREASED THE VIBRATION INCREASED. RETURNED TO DTWUPON INSPECTION FOUND MISSING HARDWARE ON LT ELEVATOR SERVO TAB CAUSING PLAY. REPLACED MISSING HARDWARE. ALL CHECKS GOOD. ALL WORKSDR SWAA050257Bearing · stickingCREW REPORTS AILERON CONTROL STICKING. REMOVED AND REPLACED RT CONTROL COLUMN BEARING PER MM.SDR 2005FA0000199Control Cable · frayedFOUND BOTH FORWARD AILERON CONTROL CABLES FRAYED. (K)SDR 757BJ0015Control Cable · frayedAILERON CABLE FRAYED AT NR 1 FLAP TRACK. REPLACED CABLE PER MM 27-00-01 AND COMPLIED WITH BOEING SB 757-27-0109.SDR 757BJ0014Control Cable · wornAILERON CABLE WORN AT THE NR 8 FLAP TRACK. REPLACED CABLE PER MM 27-00-01 AND COMPLIED WITH BOEING SB 757-27-0109.SDR 2005FA0000217Control Cable · failedPRIMARY FLIGHT CONTROL CABLES ARE FAILING INSP, DUE TO WEAR ON CONTROL CABLE FAIRLEADS IN FUSELAGE AND EMPANNAGE. DETAILED INSP IS PERFORMED AT 4800 HRS. FOLLOWING CABLES FAILE AT 1780.3 HRS. FUSELAGE AILERON CABLES, RUDDER CABLES, ELEVATOR CABLES. CAUSE ISDR 2005FA0000075Manifold · crackedMANIFOLD CRACKED AT FILTER BOWL MOUNTING PORT. FATIGUE AND OVERPRESSURIZATION. MECHANIC NH2, JOB NR 191795. (K)SDR DXTA200500522Aileron · lockedAFTER T/O FLAP RETRACTION AILERON LOCKED, VERY HARD TO MOVE. NO FLAP ASYMMETRY LIGHT. PITCH OK, PERFORMED NO FLAP LANDING AT LAX. ITEM IS UNDER INVESTIGATION.SDR XN0A1222Tensioner · lack of lubeDURING FLIGHT CONTROL CHECK LINE FOUND AILERONS TO FEEL STIFF. LUBED AILERON TENSIONER AND INPUT ROADS. OPS CHECKED NORMAL ON GROUND IAW 27-10-00.SDR CA050121007Bearing · worn(CAN) DURING MAINTENANCE INSPECTION, LT AILERON CABLE PULLEY BEARING FOUND WORN AT WINGSPAR CENTER SECTION. PULLEYS REPLACED , CABLES RE-RIGGED.SDR COMA0560031Control System · unknownFLIGHT 5134 T/O ABORTED DUE TO STIFF ELEVATOR CONTROL. COULD NOT DUPLICATE. INSPECTED ELEVATOR CONTROL SYSTEM, NO DEFECTS FOUND. FLIGHT CHECK SATISFACTORY.SDR F3LA200400118Control Cable · out of adjustFLIGHT CREW REPORTED ON SHORT FINAL APPROACH, FULLY CONFIGURED AILERON ROLL FELT TO BIND. ALL OTHER PHASES OF FLIGHT NORMAL. ADJUSTED LT AND RT AILERON BOS CABLES TO BRING LT AILERON WITHIN LIMITS.SDR MASA200400681Warning Light · false indicationASH 7240 LAX-TUS - CAPTAIN ABORTED TAKEOFF AND RETURNED TO GATE. REPORTED THAT PRIOR TO TAKEOFF ROLL, THE AIRCRAFT HAD TAKEOFF CONFIG OK AND ALL TRIMS GREEN. THEN ON TAKEOFF ROLL, RECEIVED CONFIG AILERON WARNING AND AILERON TRIM AURALS. MAINTENANCE CHECKED SDR CA041202004Control Cable · broken(CAN) DUE TO THE RISK ASSOCIATED TO BROKEN MAIN CONTROL CABLES, FOLLOWING THE BROKEN RT WING DOWN OB AILERON CABLE P/N 6660001-62 AT RWS 54 (REF. SDR NR 20031113014), WE DECIDED TO INSPECT THE AILERON WING CABLES MORE FREQUENTLY THAN THE 1200 HRS REQUIRED BY SDR 2004FA0000896Control Rod · faultyDURING A VISUAL INSPECTION OF THE CONTROL ROD, IT WAS DISCOVERED THE ROD DID NOT HAVE A CRIMPED SLEEVE WHICH IT SHOULD.SDR 2004FA0000895Control Rod · faultyDURING A VISUAL INSPECTION OF THE CONTROL ROD, IT WAS DISCOVERED THE ROD DID NOT HAVE A CRIMPED SLEEVE WHICH IT SHOULD.SDR QXEA200400739Connector · disconnectedPDX - FLIGHT 2201 - FLIGHT RETURNED TO GATE AFTER THE CREW NOTICED NO INDICATION ON THE RUDDER AND AILERON TRIM INDICATORS. MAINTENANCE RECONNECTED THE CANNON PLUG ON THE AILERON AND RUDDER TRIM PANEL. MAINTENANCE PERFORMED OPERATIONAL CHECKS AND THE CHECKS SDR SWIA200413997Transducer · malfunctionedDURING FFOD AILERON CHECK, FOUND LT AILERON WOULD NOT RETURN TO CENTER POSITION. INSTALLED SERVICEABLE LT AILERON POSITION TRANSDUCER IAW MM 27-15-15 OPERATIONAL CHECK GOOD.SDR XNOA1203Actuator · failedLOW SPEED AIL FAILED TO DISCONNECT AT FLAPS RET/OVERWEIGHT LANDING BELOW 360' PM. REMOVED AND REPLACED LOW SPEED AILERON LOCKOUT ACTUATOR I/A/W A300 AMM 27-11-48, OPS CK GOOD. PERFORMED OVERWEIGHT LANDING INSPECTION I/A/W A300 AMM 5-51-11, NO DEFECTS NOTED.SDR 2004UALA00979Control Cable · misroutedAILERON CONTROL CABLE FRAYED. CABLE GUIDE DAMAGED ON AILERON BUSS DRUM. DAMAGED DUE TO MISROUTING OF CABLE. SUSPECT CABLE WAS MISROUTED DURING HEAVY MAINTENANCE VISIT. BOTH ITEMS REPLACED.SDR MALA040929Bellcrank · bindingDURING FREEDOM OF MOVEMENT CHECK ON AILERON SYSTEM BINDING WAS FELT IN THE CONTROLS ACCOMPANIED BY NOISE AT THE BINDING POINTS. FURTHER INVESTIGATION REVEALED THAT THE HEAD OF THE BOLT WHICH CONNECTS THE INPUT ROD TO THE AILERON CABLE COMPENSATOR BELLCRANK WASDR MALA040789Actuator · chafedDURING C-CHECK INSPECTION IN YYC, MAINTENANCE FOUND LEFT & RIGHT AILERON QUADRANT LINEAR ACTUATOR RUBBING AGAINST FLOOR INTERCOSTAL. REPAIRED IAW EO A53206. AIRCRAFT WAS RETURNED TO SERVICE 10/27/04.SDR UPS04243405Fitting · corrodedINSPECTION TYPE:C, LEFT O/B AILERON TAB MAST FITTINGS HAVE PITTING CORROSION AROUND BUSHINGS. ON INVESTIGATION LEFT O/B AILERON TAB FITTINGS FOUND TO BE OUTSIDE LIMITS. LEFT O/B AILERON TAB REPLACED IAW 27-10-19.SDR ABXA040348Bracket · bentDECLARED EMERGENCY, DURING RT TURNS IN FLT AILERONS HARD TO MOVE IN POWERED MODE. WHEN AILERONS DEPOWERED, OPS NORM. FOUND RT FAIRLEAD BRACKET BENT & INTERFERRING WITH CABLE DUE TO BROKEN BUS AILERON CABLE RUNS. REPLACED BRACKET STA RW XRS 380. REPLACED DASDR CA041109004Control Cable · corroded(CAN) AILERON CONTROL CABLE FOUND CORRODED AT COPILOT FOOT AREA. THIS PROBLEM HAS BEEN NOTICED ON OTHER CESSNA 150. SUSPECT DIRT FROM SHOES CAUSING CORROSION. TO SEE THE CABLE YOU NEED TO REMOVE COVER (YOKE) AND MOVE AILERON TO TRAVEL LIMITS.
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