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 SWIA201541377Control Column · failedAUTOPILOT KICKED OFFLINE. FOUND THE AILERONS TO BE UNMOVABLE. NO OTHER MESSAGES POSTED. FOLLOWED QRH AND LT AILERON REMAINED UNMOVABLE WHILE RT AILERON MOVED FREELY. CONTINUED TO DESTINATION. CONNECTED THE CONTROL YOKE. R & R THE AILERON FEEL UNIT. ALL SDR DALA2015011200197Cable · out of toleranceDURING APPROACH THE CONTROL COLUMN STICKS IN PITCH AT 140KTS WHEN COLUMN PULLED BACK, REPEATED 5 TIMES. MAINTENANCE CHECKED ELEVATOR SYS AND INSPECTED FOR BROKEN/BINDING PULLEYS IN THE UPPER TAIL, UNDER COCKPIT FLOOR, AND BAG BIN CEILINGS. NO PROBLEMS WERE FOSDR SWIA201540617Nut · undertorquedCO-PILOTS CONTROL YOKE HAS A CLICKING NOISE, FELT AT FULL TRAVEL BOTH DIRECTIONS. TORQUED CONTROL WHEEL-SHAFT INTERFACE NUT IAW REO. OPS CHECKED GOOD. NO CLICKING HEARD AT THIS TIME.SDR SIMA20141217003Control Cable · unknownVIBRATIONS FELT IN CONTROL COLUMN & FLOOR, HEARD AT FL280 & DOWN TO 7000 FT. NO CHANGE WITHOUT AUTO PILOT OFF. REMOVED AND REPLACED THE RT AFT OUTBD ELEVATOR CONTROL CABLE IAW AMM 27-31-01 AND RT ELEVATOR TENSION REGULATOR IAW AMM 27-31-01.SDR OG5R2014FA0000694Bushing · wornPILOT REPORTED CONTROL YOKES WERE GRINDING, DURING VISUAL INSPECTION FOUND SUPPORT GUIDE, FOR CONTROL YOKE BUSHING, BOTH TO BE WORN WITH SUPPORT GUIDE TO BE PENETRATING MATERIAL MORE THAN 75 PERCENT.SDR SWIA201440207Control Column · damagedDURING PERFORMANCE OF BLEEDING OF HYD SYS NR 1 & 2. D FOUND THE CO-PILOTS SIDE AILERON CONTROL COLUMN TO BE CLICKING. COMPLIED WITH RE-TORQUE OF CONTROL COLUMN "QUADRANT-SHAFT" INTERFACE NUT IAW REO. NO DAMAGE TO LOCK TAB WASHER NOTED, CLICKING CEASED. FOUNSDR SWIA201439920Bearing · wornFLIGHT CONTROLS STARTED VIBRATING AT FL 220 AT 280 WITH THE AUTOPILOT ON. AS WE STARTED TO DESCENDING BACK TO ORD AT 12000 FT THE VIBRATION BECAME LESS AND AT 10,000 FT IS WAS NORMAL. WE DID TURN THE A/P OFF IN DESCEND AROUND 18000 FT BUT THERE WAS NO CHANGESDR CA141031008Elbow · damaged(CAN) DURING A ROUTINE INSPECTION 2 OF THE 6 SCREWS SECURING CONTROL COLUMN UPPER ELBOW TO THE CONTROL COLUMN UPPER TUBE ASSY WERE FOUND LOOSE. FURTHER INVESTIGATION REVEALED THE THREADS IN THE CONTROL COLUMN UPPER ELBOW WHICH IS A MACHINED CASTING WERE STRIPSDR CA141027011Control Column · corroded(CAN) WHILE CARRYING OUT SB SEB10-3 R1 CONTROL YOLK INSPECTION, SEVERE CORROSION WAS FOUND IN THE LOWER PIVOT AREA. THE CORROSION HAS COMPLETELY EATEN THROUGH THE MATERIAL AND CREATED A LARGE HOLE JUST BELOW THE YOLK PIVOT HINGE.SDR SWIA201439723Nut · looseRT CONTROL COLUMN YOKE CLICKS DURING OPERATION. TORQUED RT CONTROL COLUMN QUADRANT SHAFT INTERFACE NUT IAW REO.SDR SIMA20140920001Control Column · vibrationFLIGHT CREW HEARD LOUD BANG FOLLOWED BY VIBRATION IN CONTROL COLUMN TRANSFERRED TO NRWC 645-DFW-01999. VIBRATION INSPECTION IAW WC 12-200-01, NO ABNORMAL DEFICIENCIES NOTED. THIS ACFT HAS BEEN INSPECTED TO THE EXTENT NECESSARY & FOUND TO BE IN A SAFE CONDITISDR AALA20140911011Switch · inoperativeCAPTAIN & FIRST OFFICERS YOKE STABILIZER TRIM INOPERATIVE. STABILIZER TRIM CB B10 POPPED. EMER DECLARED FLIGHT LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED CAPTAINS COLUMN CUT OUT SWITCH. SYS GND CHECKED NORMAL OPERATION CLOSED.SDR N3XR2014100100009Bushing · looseDURING TAKEOFF, THE PILOT'S CONTROL YOKE SHAFT BUSHING, MOVED AFT OF ITS MOUNTING AND WAS FREE OF THE INSTRUMENT PANEL. THE TAKEOFF WAS ABORTED. THIS OPERATOR HAS HAD 9 OCCURRENCES OF THIS FAILURE ON BOTH THE PILOT'S AND CO-PILOT'S CONTROL YOKE SHAFT. THE TSDR N3XR2014100100011Bushing · looseTHE LT CONTROL YOKE BUSHING, MOVED AFT OF THE INSTRUMENT PANEL, ALLOWING RADIAL MOVEMENT OF THE YOKE SHAFT.SDR N3XR2014100100012Bushing · looseTHE LEFT CONTROL YOKE BUSHING, MOVED AFT OF THE INSTRUMENT PANEL, ALLOWING RADIAL MOVEMENT OF THE YOKE SHAFT.SDR N3XR2014100100014Bushing · looseTHE LEFT CONTROL YOKE BUSHING, MOVED AFT OF THE INSTRUMENT PANEL, ALLOWING RADIAL MOVEMENT OF THE YOKE SHAFT.SDR N3XR2014100100013Bushing · looseTHE LEFT CONTROL YOKE BUSHING, MOVED AFT OF THE INSTRUMENT PANEL, ALLOWING RADIAL MOVEMENT OF THE YOKE SHAFT.SDR 2014FA0000658Bushing · displacedPILOT'S CONTROL YOKE ASSEMBLY SUPPORT BUSHING MOUNTED IN INSTRUMENT PANEL CAME OUT OF PLACE AND PERMITTED VERY SIGNIFICANT RADIAL FREE-PLAY OF THE CONTROL YOKE SHAFT IN THE INSTRUMENT PANEL OPENING. THE ASSY WAS DISASSEMBLED, THE BUSHING PUT BACK INTO PROPER SDR N3XR201410010010Bushing · looseDURING LANDING AND FLARE, THE LT CONTROL YOKE BUSHING, MOVED AFT OF THE INSTRUMENT PANEL, ALLOWING RADIAL MOVEMENT OF THE YOKE SHAFT.SDR CA140704006Tube · cracked(CAN) ON JULY 1, 2014, WHILE PERFORMING SB 226-27-074, LUBRICATION OF THE AILERON CONTROL CABLE CHAIN IN THE PILOT`S AND COPILOT`S CONTROL COLUMNS, THE LOWER HORIZONTAL CONTROL COLUMN TUBE WAS FOUND CRACKED AT ALL 4 CORNERS OF THE LT ACCESS PANEL CUTOUT. THE SDR 2014FA0000448Sprocket · brokenCAPTAIN`S CONTROL COLUMN SPROCKET WAS FOUND TO HAVE A BROKEN TOOTH. APPEARS TO HAVE BEEN CRACKED/BROKEN FOR SOME TIME.SDR N3XR2014100100015Bushing · looseTHE LEFT CONTROL YOKE BUSHING, MOVED AFT OF THE INSTRUMENT PANEL, ALLOWING RADIAL MOVEMENT OF THE YOKE SHAFT.SDR N3XR2014100100016Bushing · migratedTHE LT CONTROL YOKE BUSHING MOVED AFT OF THE INSTRUMENT PANEL, ALLOWING RADIAL MOVEMENT OF THE YOKE SHAFT.SDR DXTA2014042505744Control Column · chafedLEFT PILOT CONTROL COLUMN HAS CHAFING MARKS FROM THE AILERON CABLE INSIDE COLUMN. RIGHT COPILOT CONTROL COLUMN HAS CHAFING MARKS FROM THE AILERON CABLE INSIDE COLUMN. REMOVED CHAFFED PILOT CONTROL COLUMN P/N 4AS5320110-501, NSN AND PERFORMED MINOR REPAIR BY SDR DXTA2014042505743Control Column · chafedLEFT AND RIGHT CONTROL COLUMNS CHAFED FROM THE AILERON CABLES INSIDE COLUMNS. REMOVED CONTROL COLUMNS, REWORKED IAW EO4AS5320110-502A02. REINSTALLED CONTROL COLUMNS IAW AMM 27-10-06 AND EO4AS5320110-502A02.SDR DXTA2014042505742Control Column · chafedLEFT PILOT CONTROL COLUMN HAS CHAFING MARKS FROM THE AILERON CABLE INSIDE COLUMN. REMOVED PILOT'S CONTROL COLUMN. MACHINED AND BLENDED DAMAGED AREA. ALODINED AND PRIMED AS REQUIRED. RE-INSTALLED PILOT'S CONTROL COLUMN. PERFORMED ALL FLIGHT CONTROL TRAVEL TSDR 2014FA0000111Screw · looseCOMPLIED WITH SB SEB-27-01. SEVERAL DAYS LATER, ACFT WAS FLOWN AND THE ELEVATOR CONTROL BECAME INCREASINGLY STIFF DURING THE FLIGHT TO THE POINT OF LOCKING UP. THE ACFT RETURNED AIRPORT AND MADE AN UNEVENTFUL LANDING. DURING INSPECTION, TENSION WAS RESET ONSDR OG5S2014FA0000071Bearing · looseBEARING OUTER RACE ON LOWER CONTROL YOKE ASSY BECAME LOOSE AND ROTATED, CAUSING FWD AND AFT PLAY IN THE ELEVATOR MOVEMENTS FELT IN THE YOKE.SDR CA140124005Universal Joint · cracked(CAN) WHEN CONTROL YOKE U WAS REMOVED FROM THE ACFT FOR REPAIRS TO SUPPORT STRUCTURE A CRACK WAS FOUND ON BOTH TOP AND BOTTOM SIDES OF CO-PILOT CONTROL YOKE UNIVERSAL JOINT STARTING FROM THE BOLT HOLES AND PROGRESSING TO THE AFT END OF THE U-JOINT. THESE CRACSDR OG5S2014011400019Bearing Race · looseBOTTOM OF CONTROL YOKE ASSY, FOUND BEARING OUTER RACE LOOSE IN YOKE ASSY. CAUSING FWD AND AFT PLAY ON ELEVATOR INPUTS. MFG INFORMED US THAT THERE IS NO CURRENT REPAIR TO THE CONTROL YOKE OTHER THEN REPLACEMENT OF THE CONTROL YOKE.SDR CA140113009Bolt · loose(CAN) DURING LINE MAINTENANCE THE AMES FOUND THAT THE F/O`S YOKE HAD AN EXCESSIVE AMOUNT OF FORE & AFT PLAY. THE AMES INVESTIGATED AND FOUND THAT THE 6 BOLTS THAT SECURE THE YOKE TO THE LEVER PITCH, ITEM 110 IN IPC, WERE LOOSE. ALL THE BOLTS COULD BE SPUN BYSDR UHLA2014010300003Control Column · damagedPITCH CONTROL DISCONNECTED AROUND 2,000 FT ON TAKEOFF, BOTH CONTROLS SEPARATED, AOA LIMIT EICAS MESSAGE ASSOCIATED WITH DISCONNECT. R & R CONTROL COLUMN DISCONNECT DEVICE IAW AMM 27-31-06. PERFORMED OPS CHECK IAW AMM 27-31-00-710-801-A/500, OPS CHECK GOOD.SDR CALA2013123194065Boot · unsecureCAPTAIN'S SIDE STICK BOOT IS MISSING SECURING STRING ELASTIC STRAP. SECURED CAPTAIN'S SIDE STICK BOOT WITH STRING.SDR AALA20131230001Switch · failedMIA CREW REPORTED CONTROL WHEEL TRIM FAILED AFTER TAKEOFF. EMERGENCY DECLARED FLIGHT RETURNED MIA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED CAPTAIN COLUMN SWITCH M1983. SYSTEM GND CHECKED NORMAL OPERATION CLOSED.SDR CALA2013112593226Screw · looseCAPTAIN`S TRIGGER SWITCH ON CONTROL STICK IS LOOSE. TIGHTENED CAPTAIN`S TRIGGER SWITCH MOUNT SCREW.SDR CALA2013101191967Yoke · vibrationHIGH FREQ VIBRATION IN BOTH CONTROL YOKES.SDR CA131023009Structure · cracked(CAN) LOWER TUBE OF CONTROL TEE ASSY FOUND CRACKED ABOVE LOWER BEARING IN AREA OF TUBE CRIMPING . CRACKED IN 2 LOCATIONS, FORE AND AFT STARTING IN MFG WELD EXTENDING UP INTO TUBE APPROXIMATELY .7500". SUSPECT WATER FREEZING IN TUBE. CORROSION INSPECTION IN SDR YENA20130718150Position Sensor · failedAIR RETURN DUE TO ELEVATOR HAS ABNORMAL FEELING/FRICTION WHILE IN FLIGHT (NO CAS MESSAGE PRESENT). TROUBLESHOT TO CONTROL COLUMN POSITION SENSOR. R & R CONTROL COLUMN POSITION SENSOR IAW AMM 27-33-01. OPS CHECK GOOD. ACFT OK TO CONTINUE.SDR UALA2013071004809Boot · misinstalledCAPTAIN`S SIDE STICK BOOT INSTALLED INCORRECTLY. REMOVED PINCHED SECTION OF SIDE STICK BOOT, ITEM OK FOR SERVICE.SDR CA130523003Tube · loose(CAN) DURING TAKEOFF, CAPTAIN PULLED CONTROL COLUMN AFT TO ROTATE. CONTROL COLUMN TRAVELED AFT OF NEUTRAL ABOUT 1-2" THEN FELT VERY STIFF. WITH A LITTLE MORE AFT PRESSURE ON CONTROL COLUMN STIFFNESS SUDDENLY RELEASED WITH A JOLT AND ACFT PITCHED UP AND BECAMSDR FDEA201303230652Control Column · dirtyFLIGHT CONTROLS BINDING ON CAPTAIN'S SIDE DURING APPROACH. PASSED CONTROL TO F/O AND F/O'S CONTROLS WERE FINE. DURING FLARE BOTH ROLL AND PITCH BOUND UP REQUIRING VERY STRONG INPUT ON CAPTAIN'S SIDE. INSPECTED CAPTAIN'S CONTROL COLUMN QUADRANT AND FOUND ITSDR SIMA20130311005Nut · misinstalledFLIGHT 4659. ON TAXI OUT, DURING FLIGHT CONTROL CHECK, FIRST OFFICER’S YOKE BINDING LEFT AND RIGHT AND MADE A CLICKING NOISE AS WELL. AIRCRAFT REMOVED FROM SERVICE. FOUND INCORRECT TORQUE ON THE AFT NUT OF THE CONTROL WHEEL. TORQUE AFT NUT IAW 27-31-01. SDR 2013FA0000169Yoke · corrodedCONTROL YOKE FAILURE. CORRODED FROM THE INSIDE OUT BELOW THE PIVOT POINT. FAILURE WAS FOUND ON THE GROUND DURING THE PREFLIGHT AILERON AND ELEVATOR CONTROL CHECK.SDR SWIA201332769Capstan · faultyBOTH YOKES FEEL VERY STIFF WHEN PITCHING UP OR DOWN, MORE SO WHEN PITCHING UP. (FLT 5354) REPLACED STICK PUSHER CAPSTAN ASSEMBLY IAW AMM. P/N: 501-1258-01 S/N ON: 2148 S/N OFF: 2306SDR SIMA20130127005Bearing · failedFLIGHT 3728. ON ARRIVAL, NOTED THE YOKE HAD ABOUT 1/4 TO 1/8 INCH OF PLAY. IN ROLL AXIS IT RACHETS, SEEMED LOOSE AND HAS PLAY IN YOKE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED FORWARD AND AFT BEARING ON F/O CONTROL COLUMN SHAFT IAW AMM 27-31-01SDR HNAA2013012500018Pulley · stiffIN FLIGHT, WITH MORE THAN 10 DEGREES RT DEFLECTION OF THE YOKE CONTROL, FORCE WAS HEAVY. INSPECTED AND FOUND 2 GUIDE PULLEYS STIFF FOR THE RT WING. REMOVED BOTH PULLEYS. YOKES MOVE FREELY. PULLEYS REMOVED WERE AT RT SIDE OF GUSTLOCK. RE-VERFIED CABLE TENSISDR R61A2013012300001Yoke · contaminatedCREW REPORTED CAPTAIN'S YOKE PITCH TRIM IS STUCK AND RECEIVED PITCH TRIM FAIL AND AUTO PILOT FAIL MESSAGE. CREW HAD A VERY DIFFICULT TIME GETTING THE AIRCRAFT TO TRIM AND DECLARED EMERGENCY. LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED GLUE FROSDR CA130111003Bracket · damaged(CAN) THE CONTROL YOKE MAIN ATTACH BRACKETS PN 0513310-1 AND 0513310-2 IN THE CENTER CONSOLE STRUCTURE WERE FOUND TO HAVE THE MAIN PIVOT BOLT HOLES ELONGATED AND WORN CAUSING A FAIR BIT OF PLAY IN THE CONTROL YOKE ASSY.SDR UALA2012120406933Yoke · odorCREW REPORTS BURNING ELECTRIC ODOR FROM CAPT CONTROL WHEEL NEAR AILERON TRIM STICKER. MAINTENANCE CONFIRMS THAT ELECTRICAL ODOR IS COMING FROM PILOT YOKE. DOES NOT FEEL WARM TO THE TOUCH. SAMC TEXT: NO SMOKE OR HEAT EVER OBSERVED.SDR SIMA20121121005Yoke · stiffON FLIGHT 3786 THE CREW REPORTED THE YOKE VERY STIFF TO MOVE FOR ELEVATOR AND AILERON MOVEMENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED AILERON / RUDDER / ELEVATOR OPERATIONAL CHECK, GENERAL VISUAL INSPECTION OF QUADRANTS, AND TENSION CHECKS. ALSO
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