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 98ZZZX1925Yoke · crackedDURING ANNUAL INSPECTION, FOUND RIGHT CONTROL YOKE CRACKED, BUT TAPED OVER. REPLACED YOKE WITH SERVICEABLE UNIT.SDR 98ZZZX2441Housing · looseFOUND CONTROL YOKE WELD ASSEMBLY BEARING HOUSING AT BASE FOR ELEVATOR ROD CONNECT IS LOOSE. WELD INSTEAD OF PRESS FIT MAY SOLVE PROBLEM.SDR AU980474Screw · dislodged(AUS) RT CONTROL COLUMN SCREW P/N NAS22014 WAS FOUND ADRIFT ALONG WITH GLIDE P/N 0760651-2 AND PLUG P/N 0760681-1. THE LT CONTROL COLUMN WAS CHECKED AND ITS SCREW WAS ALSO FOUND TO BE LOOSE.SDR 98ZZZX2440Bearing · looseFOUND BEARING HOUSING AT BASE OF YOKE LOOSE. HOUSING IS PRESSED IN. A WELD MAY PREVENT THIS.SDR 98ZZZX1467Yoke · failedCONTROL YOKE FAILURE ON LANDING. CONTROL YOKE BROKE, FAILED IN UPPER LEFT SIDE. AIRCRAFT MANUFACTURED IN 1963. SUSPECT CAUSE EXTREME AGE OF PLASTIC PART. AIRCRAFT AND CONTROL YOKE TT 2,800 HOURS.SDR CA980406003Control Column · corroded(CAN) WHILE PAINT STRIPPING THE CONTROL COLUMN A PIN HOLE APPEARED. REMOVING THE ALUMINUM PLUG, A LINE OF CORROSION WAS FOUND HALF WAY AROUND THE INSIDE OF THE COLUMN AT THE HEIGHT OF THE PLUG. CORROSION WAS THROUGH AT THE PIN HOLE AND GRADUALLY LESS TO THE SDR CA980403006Wheel · broken(CAN) DURING FLIGHT TRAINING IN SPINS THE COPILOT'S CONTROL WHEEL RIGHT HANDLE CRACKED OFF. AIRCRAFT RETURNED TO BASE. REPLACED.SDR CA980325002Cyclic Control · cracked(CAN) CRACK 1/16TH TO 1/8TH OF AN INCH FOUND ON UPPER RELIEF SLOT OF CYCLIC.SDR 98ZZZX966Sprocket Assy · crackedPILOT REPORTED YOKE POSITION 30 DEGREES OFF FROM LEVEL FLIGHT. PERFORMED VISUAL INSPECTION, FOUND PRIMARY SPROCKET ASSEMBLY WELD TO AFT CRACKED RESULTING IN NO AILERON CONTROL. RECOMMEND NDT PERIODICALLY.SDR CA980317056Coll Pitch Cntr · corroded(CAN) PILOT COLLECTIVE TUBE P/N 369H7354 HAD 2 AREAS OF EXCESSIVE WEAR AND ONE AREA OF EXCESSIVE CORROSION. COLLECTIVE FRICTION GRIP AREA HAD .007 WEAR AND THROTTLE FRICTION AREA HAD .008 WEAR. CORROSION WAS FOUND ON THE BOTTOM END OF TUBE WHERE TUBE FITS INTOSDR CA980302001Casting · loose(CAN) LOOSE RIVETS FOUND THAT HOLD THE TOP CASTING TO THE BOTTOM CONTROL COLUMN ASSEMBLY. SEE IPC FIGURE NR 46. SUBMITTER SUGGESTS THAT THE PILOT USING THE SEAT BELT AS A GUST LOCK MAY BE THE CAUSE.SDR 98ZZZX473Yoke · crackedUPON REMOVAL OF BOTH CONTROL YOKES, FOUND CRACKS RUNNING FROM HOLDING PIN TO BACK OF CONTROL YOKE. LOCATION OF CRACKS ARE SIMILAR IN LOCATION AS TO PIPER PA-28 AD 64-06-06 AND PIPER SL 396, SKETCH B. SUSPECT CAUSE IS AGING. SUBMITTER STATED AD SHOULD BE ISSSDR 98ZZZX189Yoke Shaft · fouledDURING ANNUAL INSPECTION, FOUND UP ELEVATOR TRAVEL BELOW LIMIT BY 30 PERCENT - 18 DEGREES UP - 26 DEGREES PLUS 1 MINUS ZERO DEG. INSPECTION FOUND 'TINNERMAN' TYPE HOSE CLAMP CAUGHT INBETWEEN LT YOKE SHAFT P/N 0713667-1, AND LT CONTROL WHEEL SUPPORT ASSY STOPPSDR AU971545Torque Tube · separated(AUS) PILOTS SIDE CONTROL COLUMN TORQUE TUBE BROKE OFF AT RIVETED JOINT DURING FLIGHT.SDR 97ZZZX4749U-Joint · wornDURING ANNUAL INSPECTION, PILOT SIDE CONTROL HAD EXCESS LOOSE MOTION. THE U-JOINT THAT CONNECTS THE CONTROL WHEEL SHAFT TO THE YOKE WAS WORN ENOUGH, THAT IT WAS SOON TO BE HAZARDOUS TO FLIGHT SAFETY. SUMITTER STATED THIS IS THE FOURTH ONE SEEN IN THIS SHAPE.SDR 97ZZZX4314Bearing · failedPILOT'S CONTROL COLUMN FORWARD SUPPORT ROLLER BEARING FAILED AND CAUSED AILERON CONTROL BINDING IN-FLIGHT.SDR 98ZZZX212Roller · flat spotDURING SCHEDULED INSPECTION, FOUND EXCESSIVE VERTICAL MOVEMENT OF BOTH PILOT AND COPILOT FLIGHT CONTROL COLUMNS. SUBSEQUENT INVESTIGATION FOUND BOTH CONTROL COLUMNS REAR SUPPORT BEARING LOWER ROLLERS FLAT SPOTTED. REPLACED LOWER ROLLERS, ECCENTRIC BOLTS ANDSDR 97ZZZX4817Wheel · brokePILOT CONTROL YOKE BROKE, LEFT SIDE BOTTOM, IN LANDING FULL STALL CONDITION. PLASTIC MAY HAVE AGED. AIRCRAFT IS A 1962 MODEL AND HAS BEEN PARKED OUTSIDE MOST OF THE TIME.SDR 98ZZZX211Roller · loosePILOT REPORTED 'YOKE OR AILERON CABLES BINDING WHEN ROLLING OUT OF A TURN TO THE RIGHT'. INSPECTED THE AILERON CONTROL SYSTEM INCLUDING CABLE ROUTING AND TENSION, PULLEYS, TURNBUCKLES, AND CONTROL RODS WITH NO FINDINGS. FOUND COPILOT'S CONTROL COLUMN REAR SUSDR CA970811011Column · cracked(CAN) WHILE INSPECTING CONTROL COLUMN ON A REGULAR INSPECTION, AN EXCESSIVE WEAR WAS NOTED, A SLIGHT VERTICAL FORCE APPLIED ON THE CONTROL WHEEL, BROKE THE COLUMN IN TWO PARTS.SDR 97ZZZX4154Bolt · loosePILOT'S AND COPILOT'S CONTROL COLUMN ASSY HAD EXCESSIVE PLAY AND CLICKING WAS HEARD WHEN PRESSURE APPLIED TO OPPOSITE CONTROL COLUMN. PLAY WAS NOTICED IN FORWARD AND AFT OF INBD AND OTBD PRESSURE. BOLTS WERE FOUND LOOSE AND NO TORQUE PUTTY WAS PRESENT ON BOLSDR AU970729Control Column · broken(AUS) CONTROL COLUMN HAND GRIP BROKENSDR AU970551Torque Tube · cracked(AUS) CONTROL COLUMN TORQUE TUBE HOUSING CRACKED - AIRCRAFT IS MODIFIED WITH AN `ULTIMATE WING' INSTALLED - THIS WING HAS FULL SPAN AILERONS WITH INCREASED CHORDSDR 97ZZZX4668Control Wheel · brokeTHE CONTROL WHEEL COMPLETELY BROKE BETWEEN THE OUTER GRIP AND THE HUB. PILOT REPORTED THE BROKEN PART TO THE FLIGHT SCHOOL AFTER FLYING AT THE AIRFIELD ON A DAY WITH HIGH CROSS-WINDS. THE BROKEN CONTROL WHEEL WAS REPLACED WITH A SERVICEABLE PART.SDR 97ZZZX4033Wheel · brokeCOPILOT'S CONTROL WHEEL BROKE APPROXIMATELY IN HALF WITH THE OUTBOARD HALF SEPARATING FROM THE INBOARD. THE INBOARD HALF REMAINED ATTACHED TO THE TUBE. THIS HAPPENED WHEN THE INSTRUCTOR WAS CORRECTING THE PILOT'S CROSS-WIND LANDING TECHNIQUE. THE LAST ANNUASDR 97ZZZX2577Shaft · misdrilledYOKE CONTROL SHAFT FITTED AND DRILLED IMPROPERLY. WAS CHANGING OUT CONTROL U-JOINT, FOUND THIS DEFECTIVE CONTROL SHAFT. HAVE HAD ACFT FOR 4,500 HOURS AND PRIOR TO THAT, NO RECORD OF CONTROL COLUMN BEING APART. ASSUME IT WAS DRILLED IMPROPERLY AT FACTORY. SSDR CA970421071Bearings · stiff(CAN) PILOT REPORTED THE CONTROL COLUMN WAS STIFF IN FLIGHT. UPPER BEARING WAS FOUND STIFF AND HARD TO TURN.SDR 97ZZZX1453Cover · corrodedDURING ANNUAL INSPECTION, DISCOVERED SEVERE CORROSION ALONG SEAMS OF CONTROL COLUMN COVER.SDR CA970306006Yoke · cracked(CAN) CONTROL YOKE CRACKED JUST ABOVE ELEVATOR ATTACH BEARING. REPLACED.SDR COMA9720015Bearing · wornDURING COMPLIANCE OF A.D. 97-02-02 PER S/B 227-27-041, THE COPILOT'S CONTROL COLUMN ROLLER BEARING FAILED THE TORQUE CHECK. THE BEARING AND THE DOUBLER IT IS ATTACHED TO WERE REPLACED.SDR COMA9720012Bearing · wornDURING COMPLIANCE OF A.D.97-02-02 PER S/B 227-27-041, THE PILOT'S CONTROL COLUMN ROLLER BEARING FAILED THE TORQUE CHECK. THE BEARING AND THE DOUBLER IT IS ATTACHED TO WERE REPLACED.SDR COMA9720011Bearing · wornDURING COMPLIANCE OF A.D. 97-02-02 PER S/B 227-27-041, THE COPILOT'S CONTROL COLUMN ROLLER BEARING FAILED THE TORQUE CHECK. THE BEARING AND THE DOUBLER IT IS ATTACHED TO WERE REPLACED.SDR COMA9720008Bearing · wornDURING COMPLIANCE OF A.D. 97-02-02 PER S/B 227-27-041, THE COPILOT'S CONTROL COLUMN ROLLER BEARING FAILED THE TORQUE CHECK. THE BEARING AND THE DOUBLER IT IS ATTACHED TO WERE REPLACED.SDR COMA9720007Bearing · wornDURING COMPLIANCE OF A.D.97-02-02 PER S/B 227-27-041, THE PILOT'S CONTROL COLUMN ROLLER BEARING FAILED THE TORQUE CHECK. THE BEARING AND THE DOUBLER IT IS ATTACHED TO WERE REPLACED.SDR 98ZZZX550Yoke · failedWHILE CHECKING ELEVATOR TRAVEL, YOKE BROKE WHEN BROUGHT UP AGAINST ELEVATOR STOP LEAVING BROKEN PART IN HAND. RECOMMEND PULL TEST.SDR 97ZZZX400Control Bridge · crackedDURING ANNUAL INSPECTION, FOUND BRACKET CRACKED AT REAR CONTROL STICK ATTACHMENT ON THE CONTROL BRIDGE PART. FAILURE OF PART IN THIS AREA WOULD CAUSE LOSS OF AILERON AND ELEVATOR CONTROL.SDR CA970106006Control Stick · rubbing(CAN) RUBBING BETWEEN P/N 20-2704-08-00 CONTROL STICK SUPPORT AT THE PILOTS LOCATION AND BOLT P/N AN364-428 AT END OF CONTROL ROD. APPEARS THAT THE NEW PARTS INSTALLED IN AIRCRAFT AT LATER DATES HAD A LARGER "LIGHTENING" HOLE AND THUS NO RUBBING.SDR COMA9660179Nut · looseCOPILOTS CONTROL YOKE IS CATCHING AT EXTREME ENDS OF TRAVEL. RETORQUED THE CONTROL YOKE RETAINING NUT. FLIGHT CONTROL SYSTEM FUNCTION CHECK NORMAL.SDR 97ZZZX4155Bolt · looseBOTH PILOT'S AND COPILOT'S CONTROL COLUMN ASSY HAD EXCESSIVE PLAY. WHEN PRESSURE WAS APPLIED TO OPPOSITE COLUMN, FORWARD AND AFT OR INBOARD AND OUTBOARD, FOUND BOLTS HAD EXCESSIVE PLAY AND CLICKING NOISE WAS HEARD. (NO PUTTY WAS ON ANY BOLTS). TOTAL AIRCRAFSDR 96ZZZX5110Support · crackedDURING ROUTINE 100-HOUR INSPECTION, FOUND BOTH RT AND LT YOKE SUPPORTS CRACKED IN RADIUS OF BEND WHICH FORMS AFT FLANGE OF SUPPORT. THE CRACKS WERE QUITE SEVERE, ONE SIDE BEING COMPLETELY SEVERED, AND THE OTHER SIDE BEING VERY CLOSE TO SEVERED. THE CRACKS ARSDR 96ZZZX5109Support · crackedDURING ROUTINE 100-HOUR INSPECTION, FOUND BOTH RT AND LT YOKE SUPPORTS CRACKED IN RADIUS OF BEND WHICH FORMS AFT FLANGE OF SUPPORT. THE CRACKS WERE QUITE SEVERE, ONE SIDE BEING COMPLETELY SEVERED, AND THE OTHER SIDE BEING VERY CLOSE TO SEVERED. THE CRACKS ARSDR CA960927006Control Column · jammed(CAN) AFTER PERFORMING SPINS AND STALLS, THE PILOT NOTED THAT HE COULD NO LONGER MOVE THE STICK FORWARD FROM THE NEUTRAL POSITION. THE TRIM WAS ALSO INEFFECTIVE. AFT MOVEMENT OF THE STICK AND TRIM WERE POSSIBLE. MAINTENANCE FOUND THAT THE RUDDER PEDAL ADJUSTMSDR 96ZZZX5133Support · crackedDURING ROUTINE 100-HOUR ANNUAL INSPECTION, FOUND BOTH RT AND LT YOKE SUPPORTS CRACKED IN RADIUS OF BEND WHICH FROMS AFT FLANGE OF SUPPORT. THE CRACKS WERE QUITE SEVERE, ONE BEING COMPLETELY SEVERED, AND THE OTHER SIDE BEING VERY CLOSE TO SEVERED. THE CRACKS SDR 96ZZZX5132Support · crackedDURING ROUTINE 100-HOUR ANNUAL INSPECTION, FOUND BOTH RT AND LT YOKE SUPPORTS CRACKED IN RADIUS OF BEND WHICH FORMS AFT FLANGE OF SUPPORT. THE CRACKS WERE QUITE SEVERE, ONE BEING COMPLETELY SEVERED, AND THE OTHER SIDE BEING VERY CLOSE TO SEVERED. THE CRACKS SDR 96ZZZX5108Support · crackedDURING ROUTINE 100-HOUR ANNUAL INSPECTION, FOUND BOTH RT AND LT YOKE SUPPORTS CRACKED IN RADIUS OF BEND WHICH FORMS AFT FLANGE OF SUPPORT. THE CRACKS WERE QUITE SEVERE, ONE SIDE BEING COMPLETELY SEVERED, AND THE OTHER SIDE BEING VERY CLOSE TO SEVERED. THE CRSDR 96ZZZX5107Support · crackedDURING ROUTINE 100-HOUR ANNUAL INSPECTION, FOUND BOTH RT AND LT YOKE SUPPORTS CRACKED IN RADIUS OF BEND WHICH FORMS AFT FLANGE OF SUPPORT. THE CRACKS WERE QUITE SEVERE, ONE SIDE BEING COMPLETELY SEVERED, AND THE OTHER SIDE BEING VERY CLOSE TO SEVERED. THE CRSDR CA960625012Sprocket · cracked(CAN) ON ANNUAL INSPECTION, FOUND CONTROL YOKE SPROCKET CRACKED AT WELD. STOP PIN LOOSE BUT STILL IN PLACE.SDR 96ZZZX2575Control Column · drain pluggedFOUND CONDENSATION DRAIN HOLE PLUGGED RESULTING IN WATER ACCUMULATION IN CONTROL COLUMN (ABOUT ONE-FOURTH CUP OF WATER RELEASED WHEN DRAIN HOLE UNPLUGGED). THIS PROBLEM HAS CAUSED ONE IN-FLIGHT FAILURE RESULTING IN SEVERELY DAMAGED AIRCRAFT. THE ALUMINUM PLUSDR 96ZZZX1268Cable Assy · bound yokeUPON PREPARATION FOR TAKEOFF, PILOT CHECKED CONTROLS AND YOKE LOCKED UP ON NEAR TO A FULL FORWARD POSITION. ROLL WAS OK. UPON INSPECTION, YOKE ELECTRICAL RIBBON ASSY FOUND BOUND IN 2 OF THE 4 YOKE TUBE ROLLERS. PHYSICAL FORCE COULD NOT DISLODGE. ROLLERS RESDR AU960059Control Column · broken(AUS) AFT CONTROL COLUMN BROKE IN AREA IN LINE WITH FORE AND AFT GUSSETWELD AND PRESS TO TALK (PTT) WIRING HOLE AT BOTTOM OF STICK
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