JASC 2701
Service difficulty reports · 510
Reports filed under 2701 · Control Column Section, 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 = '2701' 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 = '2701' 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 DXTA200601726Control Unit · ratchetingCONTROL WHEEL RATCHETING. THE RATCHETING IS MORE DEFINED IN THE LT CONTROL WHEEL. REMOVED AND REPLACED AFT AILERON SECTOR PCU IAW MM CH 27-10-01.SDR RAIA00611005Control Column · roughFLT NR 5464 - STL - CONTROL COLUMN NOT TRAVELING SMOOTHLY FROM FULL FORWARD TO FULL AFT POSITIONS. MAINTENANCE PERFORMED AN INSPECTION OF THE ELEVATOR CONTROL CABLES AND PERFORMED A SYSTEM TEST OF THE AUTO PILOT SYSTEM AND STICK PUSHER. NO EVIDENCE OF BINDINSDR SIMA200630402Yoke · vibrationON APPROACH IN TO DFW, A HIGH SPEED VIBRATION WAS FELT IN THE YOKE WHEN THE FLAPS WERE SELECTED AND POWER REDUCED. NO VIBRATION NOTED ON TAKEOFF OR PREVIOUS LANDING, FLAPS SELECTED 15 AT 175 KNOTS AND CONTINUED WITH FLAPS 20 UNTIL LANDING. NO VIBRATIONS NOTESDR F3LA200600147Control Stick · unknownFLIGHT CREW REPORTED THAT UPON APPROACH, AT APPROXIMATELY 10 FT ABOVE THE RUNWAY, AIRCRAFT ABRUPTLY NOSED OVER DURING FLARE WITH FULL AFT STICK HELD (HAND-FLOWN APPROACH). NO ECAM WARNINGS OR OTHER INDICATIONS. THE FLIGHT DATA RECORDER HAS BEEN DOWNLOADED ANSDR YENA200680Yoke · slippedINTERMITTENT THUMP HEARD AND FELT BETWEEN 3,000 FT AND 15,000 FT CAN BE FELT THROUGH YOKE AND MOSTLY WITH AUTO PILOT ON. RIG PINS INSTALLED IN LT, RT AILERON QUADRANT 2 PINS TOTAL. RIG PINS INSTALLED IN CONTROL YOKES PILOT AND COPILOT FOR TROUBLESHOOTING. PERFSDR 2006FA0001051Control Stick · damagedPILOTS CONTROL STICK GRIP BECAME LOOSE AND WOULD, IF PULLED ON, COULD BECOME DETACHED FROM THE CONTROL ASSEMBLY. CHECK BOTH CONTROL GRIPS FOR LOOSE INSTALLATION AND REATTACH WITH APPROVED ADHESIVE. (K)SDR 06FDEA03415Yoke · lockedRIC MISSED APPROACH A/P OFF, SELECTED FLAPS 20, GEAR UP, 3000' SET IN ALT WINDOW. AT 1600' REDC THROTTLES FOR SPD AT THIS POINT CLB STOPPED, PF KEPT BACK PRESS, YOKE SEEMED LOCKED IN PLACE. CAPT TOOK CTL, YOKE LOCKED, COULDN`T CLB. TRIED TO TURN ON A/P, SDR DXTA200601606Bolt · unknownLT AILERON SEEM TO BIND SLIGHTLY AND MAKES `CLUCKING` SOUND WHEN MOVING UP AND DOWN. REMOVED AND REPLACED LT AILERON YOKE BEARINGS AND ALL BOLTS. OPS CHECKS GOOD WITH NO CLUNKING NOISE. ALL WORK DONE IAW CE-560 MM 27-11-01, 20-10-08.SDR HALA0600639Control Column · disconnectedBTB -COLUMN DISC- ALERT MSG CAME ON DURING TAXI. PERFORMED FIM 27-30-00 AND COLUMN WAS PHYSICALLY DISCONNECTED. RECONNECTED CONTROL COLUMN PER AMM 27-31-10, OPS CHECK GOOD, MSG CLEARED.SDR IXXA06SMN273STorque Tube · wornDURING ROUTINE C CHECK INSPECTION FOUND CONTROL COLUMN TORQUE TUBE WITH DEEP WEAR. REPLACED DAMAGED TORQUE TUBE. CLEANED, TREATED AND PRIMED AREA. IAW SRM 51-1-21, SRM 51-1-20D. SRM 51-1-8B. SRM 51-1-21, SRM 51-1-20D, SRM 51-3-1, AND SRM 27-267 REV. 2 DATE 0SDR TRAX200600559Yoke · vibrationAT AN ALTITUDE OF 10000 FT, FELT A VIBRATION ON THE LEFT YOKE. WITH A AIRSPEED OF 290 KIAS. RECEIVED A TURN TO CAE AND ON THE APPROACH WITH THE AUTOPILOT OFF IT HAPPENED AGAIN. A/C RETURNED TO CAE AFTER T/O, EMERGENCY WAS DECLARED, FLTS 4321, 4586 CX.SDR DXTA200601489Yoke · bindingYOKE CONTROL BINDING WHEN DISPLACING LEFT. ADD MORE PRESSURE, YOKE WOULD MOVE. CHECKED CABLE TENSIONS, ALL CHECKED GOOD. REMOVED AND INSPECTED AILERON PUSH RODS AT AILERON FOUND BEARING TO BE TIGHT. CLEANED AND LUBED BEARINGS. REINSTALLED PUSHRODS SYSTEM,SDR DJFA2006272Yoke · stuckTXKF - KPBI, THE CREW ABORTED TAKE OFF AFTER DISCOVERING THE CONTROL YOKE PITCH AXIS WAS LOCKED. UNDER THE ADVISEMENT OF GULFSTREAM ENGINEERING AND A FIELD SERVICE REPRESENTATIVE, MAINTENANCE PERFORMED A THOROUGH VISUAL INSPECTION OF THE GAMMA TUBES FOR EVSDR CA060627005Roller · dislodged(CAN) CO-PILOTS CONTROL YOKE GUIDE ROLLER ASSY FELL OUT AND ON INVESTIGATION WAS FOUND THAT WRONG SIZE BOLT WAS INSTALLED. FURTHER INVESTIGATION OF THE REST OF THE FLEET IT WAS FOUND THAT 2 OTHER ACFT HAD THE WRONG BOLT PN AND SIZE INSTALLED. CORRECT BOLT INSTSDR MASA200601617Unknown · unknownASH 7347 ORD - CREW REPORTED CLICKING NOISE FROM FO YOKE DURING ELEVATOR MOVEMENT. MX INSPECTED THE SYSTEM, NO DEFECTS NOTED.SDR CA060608003Shaft · damaged(CAN) ON INSP, IT WAS FOUND THAT THE RT AND LT CONTROL WHEELS WERE LOOSE ON THE CONTROL SHAFTS. AVION RESEARCH STC 00709LA HAD PREVIOUSLY BEEN INSTALLED TO REPLACE THE CONTROL WHEELS, HOWEVER, THE INSTALLATION INSTRUCTIONS CW-8001 REV1 FEB26/98 DO NOT ADDRESS SDR SWIA200616664Yoke · malfunctionedCONTROL YOKE MAKES CLICKING NOISE WHEN ELEVATOR IS DEFLECTED UP AND DOWN. REPLACED BOLTS AND NUTS CONNECTING RIGHT CONTROL COLUMN TORQUE TUBE TO ELEVATOR DISCONNECT MECHANISM IAW AMM 27-32-01. OPERATIONAL CHECK GOOD.SDR CWQR2006009Cable Assy · damagedDURING A SCHEDULED MAINTENANCE VISIT BEFORE REPLACING A CABLE ASSEMBLY ON A THE CABLE TERMINAL END WAS FOUND TO HAVE BEEN DRILLED TO A DEPTH OF .3750-.5 INCH AT AN ANGLE AND DAMAGED THE THREADS. THIS CABLE ASSEMBLY WAS ORDERED FROM AND DOCUMENTED AS NEW.SDR ASMF200603001Control Column · obstructedAIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF THE FLIGHT CONTROLS TEST WAS NOT SATISFACTORY. DURING REVIEW, IT WAS DETECTED AN INTERFERENCE WITH THE CONTROL WHEEL. THE AIRCRAFT WAS SENT TO THE HANGAR AND THE CONTROL WHEEL TRAVEL INTERFERENCE WAS TESTED ISDR DXTA200601246Yoke · bindingCONTROL YOKE BINDS WITH A RACHET FEEL IN FLIGHT, IT IS MORE NOTICABLE ON LEFT YOKE. WITH AUTO PILOT ENGAGED A BUMPING CAN BE FELT ON LEFT CONTROL YOKE, NOT ON RIGHT. REMOVED COCKPIT FLOORBOARDS, DETERMINED THERE WAS A SPACER BINDING ON THE LEFT AILERON SECTOSDR CA060203007Guard · looseWHILE INSTALLING ALTERNATOR/WIRING UPGRADE, IT WAS NOTICED THAT THE STRAP COVER WAS LOOSE ON THE CABLE GUARD ON THE LEFT SIDE AILERON CONTROL QUADRANT. SUBSEQUENT INSPECTION REVEALED THE RIGHT SIDE WAS ALSO LOOSE. TOP AND BOTTOM SCREWS ON THE LEFT AND RIGHT SDR SWIA200616169Yoke · lack of lubeAILERON ROLL CONTROL VERY STIFF IN BOTH CAPTAIN'S AND FIRST OFFICER'S YOKE. CLEANED AND LUBED RT TRIM CENTERING AND FEEL MECHANISM, OPERATIONAL CHECKS GOOD REF CL600 MM 27-12-10.SDR AU510001929Control Wheel · crackedCAPTAIN`S CONTROL WHEEL CRACKED AT BEND APEX.SDR AU510001881Control Wheel · crackedCONTROL WHEEL CRACKED FROM TOP BOLT HOLE.SDR AU510001853Control Column · sticking(AUS) CONTROL YOKE STICKING DURING ROLL INPUT. INVESTIGATION FOUND THE CONTROL YOKE CONTACTING THE LT DEFOG VENT. FURTHER INVESTIGATION FOUND THE BOLT HOLES CONTAINED WITHIN THE CONTROL COLUMN YOKE WERE ELONGATED. (CASA NR 510001853)SDR 2005FA0001365Yoke · brokenUPON THE FLAIR ON LANDING AT NORMAL WEIGHTS THE CONTROL YOLK BROKE AT THE OUTSIDE LT RADIUS. THIS CAUSED THE NOSE WHEEL OF THE AC TO DROP AT A GREATER SPEED THAN NORMAL AND SHIMMY WAS EXPERIENCED THE MAIN GEAR HAD JUST TOUCHED DOWN WHEN THE FAILURE OCCURRED. SDR 08032005AYoke · out of adjustBOTH YOKES ARE CANTED RIGHT IN STRAIGHT AND LEVEL FLIGHT. COMPLETED WING AND AILERON RIGGING, OPS CHECK GOOD.SDR CA050712002Bearing · unserviceableWHILE FUNCTION CHECKING THE AILERON CONTROL SYSTEM PRIOR TO FLIGHT THEY BECAME HARD TO OPERATE. THE CO-PILOT'S CONTROL COLUMN BEARING ON OUTER SURFACE OF FIREWALL WAS FOUND TO BE UNSERVICEABLE. THE NEEDLE BEARINGS HAD DEPARTED THE CAGE. THE BEARING WAS REPLSDR 06112005AControl Column · stickingELEVATOR MOMENTARILY FROZE DURING TAXI. TIGHTENED CONTROL COLUMN HARDWARE.SDR 2005FA0000868Control Column · crackedDURING ANNUAL INSPECTION CRACK WAS OBSERVED ON CONTROL COLUMN 1.0 INCHES LENGTH (49 MM). CRACK WAS CONFIRMED BY MAGNETIC PARTICLE INSPECTION. THE COMPONENT FORMS PART OF THE AC FLIGHT CONTROL SYSTEM AND IS CRITICAL TO FLIGHT. BOTH THE LT AND RT FITTING ARE SDR MWEA060230Control Column · disconnectedRUDDER LIMIT FAULT ON ENGINE AND ALERT DISPLAY AND CONTROL COLUMN DISCONNECTED. PERFORMED FAULT ISLOATION MANUAL TASK OR RETURNED TO SERVICE WORK, LIGHTNING STRIKE OVERSPEED, CONTROL COLUMN DISCONNECTED, RUDDER LIMITER, ADJUSTED AIR DATA INERTIAL REFERENCE UNSDR 2005UALA00437Unknown · unknownRETURNED TO FIELD DUE TO A LOUD BANG IN THE CAPTAIN'S CONTROL COLUMN. THE SUBJECT DISCREPANCY WAS DUE TO A BROKEN SPRING RETAINER ON THE ELEVATOR TENSION REGULAR WHICH ALLOWED THE SUBJECT TENSION STRING TO BECOME DETACHED. THE SUBJECT TENSION REGULATOR WAS SDR MASA200500317Bearing · damagedASH 6146 LAS. ON ARRIVAL TO LAS THE CAPTAIN WROTE UP THE AILERON CONTROL BINDING LEFT TO RIGHT DURING FLIGHT. MAINTENANCE INSPECTED AND PREPARED AIRCRAFT FOR FERRY FLIGHT TO OKC. MAINTENANCE REMOVED AND REPLACED THE PILOT CONTROL WHEEL SHAFT BEARINGS.SDR MASA200500297Yoke · bindingASH 6338 SLC TO PHX. RETURN TO GATE DUE TO YOKE JAMMING/BINDING WHEN TURNED TO THE LEFT. INSPECTED PER SERVICE LETTER 22-045. COULD NOT DUPLICATE. OPS CHECKED NORMAL.SDR AU510001956Control Column · loose(AUS) RT CONTROL COLUMN LOWER ATTACHMENT RIVETS LOOSE. CONTROL COLUMN HAD APPROXIMATELY 5MM (0.196IN) FORE AND AFT MOVEMENT WHEN LOCKED. (CASA NR 510001956)SDR CA050407007Control Column · mismanufactured(CAN) THE LOWER CONTROL COLUMN IS MIS-MANUFACTURED AT THE BOTTOM TORQUE TUBE. THE STOP BOLT INSERTS AND CABLE QUADRANT SUPPORTS WERE MIS-LOCATED DURING MANUFACTURE OF THE ASSEMBLY. FINAL ASSEMBLY PROBLEMS WILL OCCUR.SDR EXO2005F00000Master Switch · shortedPILOT EXPERIENCED LOSS OF YAW DAMPERS NR1, NR2, REENGAGEMENT ATTEMPTS UNSUCCESSFUL. AUTO PILOT DISENGAGED AND COULD NOT BE RESET. IN-OP YAW DAMPER, PILOT WAS ATTEMPTING TO LEVEL AC, NO RESPONSE TO PITCH TRIM CNTRL, SECONDARY PITCH TRIM WAS ACTIVATED W/NEGATISDR DXTA200500576Control Cable · out of adjustCONTROLS ARE BINDING. WHILE MOVING THE CONTROLS LT & RT THERE IS A NOISE AND FEELING OF BINDING IN PILOT CONTROL COLUMN. AT HIGHER SPEED MORE PRONOUNCED, AT SLOWER SPEED LESS PRONOUNCED. AFTER PERFORMING DETAIL INSPECTION DETERMINE THAT SLIGHT RATCHETING MOSDR 2090405Yoke · detachedBERMUDA (BD) - JUST AFTER TAKEOFF, THE CAPTAIN'S CONTROL YOKE CAME OUT AND FELL TO THE GROUND. AT A SAFE HEIGHT THE CONTROL YOKE PIN WAS PUT BACK IN PLACE. THIS RESULTED IN A MOMENTARY LOSS OF AILERON AND RUDDER CONTROL. PENDING ENGINEERING INVESTIGATION RESDR 2005FA0000692Control Column · corrodedWHILE ACCOMPLISHING SEB ON CONTROL YOKE, FOUND WATER WHEN INSP HOLE WAS DRILLED AT BASE OF CENTER TUBE. .2500 CUP OF BLACK RESIDUE WAS FOUND WHEN TUBE WAS CUT OPEN. INSIDE OF CONTROL YOKE TUBE WAS RUSTED MODERATELY THE FULL LENGTH OF CENTER TUBE. NO LEAK INSDR 04338658Yoke · vibrationHIGH FREQ VIBE FELT THRU YOKES & GOT WORSE AS SPEED INCREASED. INTERROGATED MDC FOR ANY APPLICABLE FAULTS, NONE FOUND. PERFORMED CRJ SERVO SPIN TEST. AILERON & ELEVATOR SERVOS OK FOR SVC. PERFORMED OPS CHK OF HORIZONTAL STAB TRIM SYSTEM, NO DEFECTS NOTED. SDR SWIA200414118Nut · looseF/O'S CONTROL YOKE CLICKS WHEN FULL DEFLECTION RIGHT OR LEFT AILERONS. RETORQUED NUT ON F/O'S YOKE AS REQUIRED, OPERATIONAL CHECKS GOOD.SDR 2004FA0000846Shaft · mismanufacturedDURING 100 HR INSP AT 1V5, LT CONTOL COLUMN UNIVERSAL,P/N 62834-02, WAS REMOVED FOR REPLACEMENT DUE TO EXCESS PLAY. CONTROL COLUMN SHAFT, P/N 62716-02, WAS FOUND TO BE DRILLED (FOR THE AN-386-1-6A TAPER PIN) LESS THAN 0.025 INCH FROM AFT END OF SHAFT. HOLE ISDR 2004FA0000845Shaft · mismanufacturedDURING 100 HOUR INSP AT 1V5, LT CONTROL COLUMN, P/N 62834-02, WAS REMOVED FOR REPLACEMENT DUE TO EXCESS PLAY. UPON REMOVAL, CONTROL COLUMN SHAFT, P/N 62716-02, WAS FOUND TO BE DRILLED (FOR AN-386-1-6A TAPER PIN) LESS THAN 0.025 INCH FROM AFT END OF SHAFT. HOLSDR CALA0400651Bearing · wornTHE HORIZONTAL STABILIZER TRIM STARTED GRINDING ON APPROACH TO MSP WITH THE AUTOPILOT ENGAGED. THE AUTOPILOT WAS TURNED OFF AND THE YOKE SWITCHES WERE ACTUATED. THE CREW HEARD THE GRINDING NOISE AGAIN IN COCKPIT AND AFT GALLEY AREA, THEN THE HORIZONTAL STABISDR 2004FA0000741Bearing · stickingPILOT REPORTS THAT THE AILERON CONTROL LOCKS UP AND WILL NOT TURN IN EITHER DIRECTION AND THEN RELEASES AND RETURNS TO NORMAL. UPON INSPECTION OF AILERON SYSTEM, IT WAS FOUND THAT THE CONTROL YOKE CONNECTION BEARING WAS STICKING AND WOULD NOT RELEASE UNTIL THSDR CA040809004Spacer · loose(CAN) YOKE FOUND TO HAVE EXCESSIVE MOVEMENT DURING INSPECTION. SOURCE DETERMINED TO BE LACK OF WELDING AT LT SIDE OF LOWER BEARING CONTROL YOKE SPACER ASSEMBLY TO THE CONTROL YOKE SHAFT ITSELF. MFG HAS PROVIDED APPROPRIATE DATA TO COMPLETE THE WELDMENTS.SDR SWIA200413583Spring · brokenELEVATOR FEELS HEAVY. INSTALLED SERVICEABLE SPRING ON CAPTAINS CONTROL COLUMN. OPERATIONAL CHECK GOOD.SDR 2004FA0000587Clamp · out of positionFULL DOWN ELEVATOR WAS NOT ACHIEVED DUE TO THE FACT THAT TEMPORARY YOKE ATTACHMENTS WERE IMPEDING THE MOVEMENT OF THE FORWARD TRAVEL OF THE YOKE. AFTER A THOROUGH INSPECTION OF THE STABALATOR CONTROL SYSTEM IT WAS FOUND THAT THE CLAMP ON ATTACHMENTS WERE IMPESDR UPS04242861Yoke · malfunctionedINSPECTION TYPE: C, PERFORM A GVI OF CAPT & F/O CONTROL YOKES & ATTACHED LINKAGE, PAYING ATTENTION TO CORROSION, BINDING OR LOOSENESS OF BEARINGS. ROTATE EACH CONTROL WHEEL FULL TRAVEL LEFT & RIGHT CHECKING FOR ANY STIFFENESS, BINDING OR RATCHETING OF MOVEMEN
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