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 SIMA200417201Yoke · vibrationDURING CLIMB AND MOST OF FLIGHT INTO MQT, CREW NOTED A SLIGHT VIBRATION ON BOTH YOKES. NOTE: VIBRATION WAS AT AIRSPEEDS OF 230-310. AUTO PILOT ON/OR OFF HAD NO AFFECT. REPLACED LEFT AILERON BUSHING AND HARDWARE. PASSED FUNCTIONAL CHECK FLIGHT. AIRCRAFT RETSDR AUS20040487Bearing · faulty(AUS) FIRST OFFICER'S CONTROL WHEEL BEARING NOTCHY.SDR 04154653Nut · looseDURING AIRCRAFT OPERATION THE CREW REPORTED THE FIRST OFFICERS YOKE BINDING. THE YOKE NUT WAS FOUND LOOSE AND RETORQUED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT RETURNED TO SERVICE.SDR SWIA200413362Nut · looseAUDIBLE AND TACTILE CLICK/RUDDER AT 30 DEGREES YOKE INPUT; BOTH DIRECTIONS. FERRIED TO SLC. TORQUED THE PILOT'S CONTROL YOKE CENTER SHAFT NUTS IAW CRJ MM 27-11-01. OPS CHECKS GOOD.SDR MWEA040082Control Column · inoperativeCREW REPORTED COLUMN DISCONNECT. RECONNECTED CONTROL COLUMN, OPERATIONS CHECK GOOD.SDR UG8AGM0413Yoke · incorrectCONTROL YOKES SHOW 25 DEGREE RT BANK DURING STRAIGHT AND LEVEL. RT AILERON IS UP AND LT ELEVATOR IS UP. PITCH CONTROL FORCE FEELS NORMAL. AMOUNT OF ELEVATOR/AILERON DISPLACEMENT INCREASES WITH SPEED. TROUBLESHOOTING FLIGHT CONTROL SYSTEMS IN PROGRESS. AIRSDR AUS20040387Control Column · binding(AUS) FIRST OFFICER'S CONTROL COLUMN ELL FITTING CHAFING ON TRANSFER MECHANISM FORK. TRANSFER MECHANISM WAS FOUND TO HAVE A PRESERVICE BULLETIN FORK FITTED INSTEAD OF A POST SERVICE BULLETIN FORK.SDR AUS20040295Bushing · galled(AUS) CONTROL WHEEL SHAFT BUSHING GALLED AGAINST WELD PENETRATION ON INNER FACE OF CONTROL COLUMN SLEEVE.SDR SWAA040945Bearing · bindingAILERON CONTROL SLOPPY. LARGE DEAD BAND IN AILERONS. REMOVED AND REPLACED CAPT'S AILERON CONTROL WHEEL DRUM BEARINGS AND CAPT'S CONTROL COLUMN BEARINGS PER MM.SDR 2004F00104Control Column · inoperativeDURING A PHASE INSPECTION A SQUEAK WAS NOTED DURING MOVEMENT OF FLIGHT CONTROL COLUMN. INVESTIGATION REVEALED. LOOSE RIVETS BETWEEN THE CONTROL T COLUMN AND BEARING PLATES AT THE POINT WHERE THE CONTROL COLUMN ATTACHES TO THE AIR FRAME AND PIVOTS. MFG ISSUESDR GAIA04047OPControl Column · bindingDURING CRUISE FLIGHT, A BINDING OF THE CONTROL YOKE WAS NOTED IN A ROLL TO THE RIGHT. SPOILERS WERE CYCLED AND ABOVE PROBLEM WAS CORRECTED BUT LATER DID RETURN. FLT WAS COMPLETED AND AN UNEVENTFUL LANDING WAS MADE. INSPECTED AND CHECK FLIGHT CONTROLS AILEROSDR SWIA200412968Control Wheel · lack of lubeAILERONS HESITATE, THEN MOVE A LOT WHEN TURNED TO LEFT. CANNOT DUPLICATE ON GROUND, ONLY INFLIGHT, FEELS LIKE THEY ARE RUBBING AGAINST SOMETHING. TORQUED FORWARD CONTROL WHEEL SHAFT NUT ON BOTH RIGHT AND LEFT CONTROL WHEELS AND LUBED BEARINGS PER MM 27-11-01SDR 04058653Yoke · interferenceDURING AIRCRAFT OPERATION THE CREW REPORTED A SLIGHT BUMP IN YOKE MOVEMENT WHEN ROTATING FROM LEFT TO RIGHT. A SATISFACTORY FUNCTIONAL CHECK OF THE YOKE WAS PERFORMED AND NO DEFECTS WERE FOUND. AIRCRAFT WAS RETURNED TO SERVICE.SDR 2004FA0000287Control Wheel · crackedA CRACK WAS FOUND IN THE CO-PILOT CONTROL WHEEL WHEN IT WAS REMOVED. THE BOTTOM OF THE WHEEL FROM FRONT TO REAR THROUGH THE PIN HOLE. THIS CRACK IS NOT VISABLE FROM THE OUTSIDE.SDR CA040219005Control Column · cracked(CAN) CONTROL COLUMN FOUND CRACKED IN THREE LOCATIONS WHEN SB 3/39 CW.SDR A6WA200340207Yoke · looseCHECKED THAT PLAY EVIDENT IN CONTROL YOKE PITCH AXIS IS WITHIN ACCEPTABLE LIMITS. COMPLIED WITH AMM TASK 27-32-00-720-801. FOUND CONTROL YOKE BACKLASH AT .28 DEGREES. BACKLASH LIMITS ACCEPTABLE. (M)SDR W322004F00000Yoke · crackedPILOT REPORTED THAT DURING LANDING FLARE, THE YOKE SNAPPED RESULTING IN A GO AROUND. AFTER INITIAL INSPECTION, YOKE WAS FOUND CRACKED COMPLETELY THROUGH ON UPPER LEFT HAND CORNER. YOKE MATERIAL APPEARS TO MANUFACTURED FROM PLASTIC, SUGGEST REMOVAL OF ALL PLASDR F3LA200300154Yoke · frozenON FINAL APPROACH, FLIGHT CREW REPORTED YOKE FROZE UP IN TURN (ROLL ONLY). INSPECTED CASE DRAIN FILTERS IAW MM 29-15-91, AND FOUND NO DISCREPANCIES. REMOVED AND REINSTALLED NR 2 ENG. CASE DRAIN PLUG TO INSPECT IAW MM 29-15-00 AND FOUND NO DISCREPANCIES. VISSDR 038431Control Column · vibrationDURING CLIMB OUT AND CRUISE FLT 4514 FROM PIT TO LYH EXPERIENCED ABNORMAL RAPID VIBRATION IN CONTROL YOKES. CREW WAS ADVISED TO RETURN TO PIT, NO INCIDENT.SDR 013042Yoke · vibrationON CLIMBOUT, A STRONG (FWD-AFT) VIBRATION WAS FELT ON THE CAPTAIN YOKE. CREW LEVELED OFF AT 2000 FT, VIBRATION CONTINUED FROM 150-200 KTS. CREW REDUCED SPEED TO 180 KTS, RETURNED TO FIELD WITH VIBRATION CONTINUING UNTIL FLAPS RETRACTED.SDR SWIA200312612Shaft · damagedTRIED TO MOVE YOKE TO THE LT AND IT WAS BOUND UP AND WOULD NOT GO TO THE LT. REPLACED BELLCRANK SHAFT IAW MM 31-30-10. OPS CHECK GOOD.SDR 038191Control Column · vibrationSHORTLY AFTER TAKEOFF CREW EXPERIENCED SEVERE FLIGHT CONTROL VIBRATION PRIMARILY IN THE PITCH AXIS AND SOME IN ROLL, A MECHANIC WAS IN THE JUMPSEAT AND COMFIRMS THE YOKES WERE VIOLENTLY VIBRATING. CAPT REPORTED IT FELT LIKE HE WAS FIGHTING THE AUTOPILOT. AUTSDR 03316678Bearing · out of adjustDURING UNKNOWN PHASE OF AIRCRAFT OPERATION THE CONTROL COLUMN WAS REPORTED CLICKING AND BUMPING UPON ELEVATOR MOVEMENT. THE FAULT WAS TRACED TO LT FORWARD AND AFT YOKE MOUNTING NUTS ON THE FIRST OFFICERS CONTROL COLUMN. THE NUTS WERE RETORQUED PER A BOMBARDISDR COMA0370040Bearing · stickingFLIGHT 9463, DURING SMALL BANK TURNS, STICKING CAN BE FELT IN AILERONS. REPLACED THE CONTROL WHEEL BEARINGS IN COPILOTS CONTROL YOKE.SDR COMA0370039Control Column · bindingFLIGHT 5877 AILERON CONTROLS WERE BINDING DURING FLIGHT. LOOSENED AND THEN RETORQUED CO-PILOTS CONTROL YOKE. NO DEFECTS NOTED.SDR USAASB03179Control Column · stiffEN ROUTE FROM CLT TO RDU, CREW REPORTED STIFF FLIGHT CONTROLS, ELEVATOR AND AILERONS. FEELS SOMEWHAT LIKE MANUAL REVERSION. DURING FLARE ON FINAL, THE CONTROL COLUMN BOUND FOR A MOMENT AND THEN BROKE FREE. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCSDR 2003FA0001067Sprocket · damagedAT ANNUAL INSPECTION, FOUND BACKUP STOP PIN ON PILOT SIDE CONTROL SPROCKET TO BE DAMAGED. FURTHER INVESTIGATION REVEALED THAT THE SPROCKET TOOTH LOCATED AT THE STOP PIN WAS BROKEN OUT OF THE SPROCKET. POSSIBLE CAUSE IS STRESS FRACTURE AT THE WELD OF THE STOPSDR 255031Yoke · excess playEXCESSIVE PLAY IN ALL QUADRANTS IN CAPTAINS YOKE BOTH PITCH AND ROLL AXIS.SDR 52753Bracket · out of positionON FLIGHT 5541 FROM LATROBE PENNSYLVANIA TO PITTSBURGH PENNSYLVANIA, AFTER TAXI OUT THE RIGHT AILERON TRAVEL HAS A CATCH AND A NOISE. THE CREW RETURNED TO GATE WITH NO FURTHER INCIDENT. MAINTENANCE INSPECTION REVEALED THE COVERING IN THE COCKPIT OVER THE CONSDR 2003FA0000895Control Wheel · brokenCONTROL WHEEL BROKE ON LT TOP .7500 INCH FROM CORNER ON LIFT OFF VX ON PILOTS SIDE. THIS IS THE OLD SQUARE CONTOL WHEEL AND IS ORIGINAL PART, 40 YEARS OLD. BROKEN CONTROL WHEEL SHATTERED, PUSH TO TALK SWITCH FASTENED TO CONTROL AT SAME LOCATION. CONTROL WHESDR P5CA0300897Plate · defectiveDURING FLT CNTRL CK, FELT A THUMP AND CLICK IN LEFT TURN - FORE AND AFT MOVEMENTS. REMOVED CAPT CONTROL COLUMN -REMOVED AND REPLACED PLATE ASSY - REINSTALLED COLUMN AND TESTED NRML IAW AMM 27-31-04/05.SDR 2003FA0000794Screw · backed outTHE SCREW THAT HOLDS THE CONTROL WHEEL TO THE YOKE BACKS OUT ON BOTH THE PILOT AND COPILOTS WHEEL. WHEN THE SCREW BACKS OUT ENOUGH, IT FALLS OUT ALLOWING THE WHEEL TO ROTATE FREELY AROUND THE YOKE. THIS RESULTS IN NO FLIGHT CONTROL INPUT. THIS INCIDENT HAPPSDR 2003FA0000793Screw · backed outTHE SCREW THAT HOLDS THE CONTROL WHEEL TO THE YOKE WAS FOUND TO BE BACKED OUT ON BOTH THE PILOT AND CO-PILOTS WHEEL BY A .2500 TURN. WHEN THE SCREW BACKS OUT ENOUGH, IT FALLS OUT ALLOWING THE WHEEL TO ROTATE FREELY AROUND THE YOKE. THIS RESULTS IN NO FLIGHT SDR 2003FA0000792Screw · backed outTHE SCREW THAT HOLDS THE CONTROL WHEEL TO THE YOKE WAS FOUND TO BE BACKED OUT ON BOTH THE PILOT AND COPILOTS WHEEL BY A .2500 TURN. WHNE THE SCREWS BACKS OUT ENOUGH, IT FALLS OUT ALLOWING THE WHEEL TO ROTATE FREELY AROUND THE YOKE. THIS RESULTS IN NO FLIGHT SDR 2003FA0000791Screw · backed outTHE SCREW THAT HOLDS THE CONTROL WHEEL TO THE YOKE WAS FOUND TO BE BACKED OUT ON THE PILOTS WHEEL BY A .2500 TURN. WHEN THE SCREW BACKS OUT ENOUGH, IT FALLS OUT ALLOWING THE WHEEL TO ROTATE FREELY AROUND THE YOKE. THIS RESULTS IN NO FLIGHT CONTROL INPUT. PRSDR 2003FA0000790Screw · backed outTHE SCREW THAT HOLDS THE CONTROL WHEEL TO THE YOKE WAS FOUND TO BE BACKED OUT ON THE PILOTS WHEEL BY A .2500 TURN. WHEN THE SCREW BACKS OUT ENOUGH, IT FALLS OUT ALLOWING THE WHEEL TO ROTATE FREELY AROUND THE YOKE. THIS RESULTS IN NO FLIGHT CONTROL INPUT. PRSDR 2003FA0000789Screw · backed outTHE SCREW THAT HOLDS THE CONTROL WHEEL TO THE YOKE WAS FOUND TO BE BACKED OUT ON THE PILOTS WHEEL BY A .2500 TURN. WHEN THE SCREW BACKS OUT ENOUGH, IT FALLS OUT ALLOWING THE WHEEL TO ROTATE FREELY AROUND THE YOKE. THIS RESULTS IN NO FLIGHT CONTROL INPUT. PRSDR 2003FA0000788Screw · backed outTHE SCREW THAT HOLDS THE CONTROL WHEEL TO THE YOKE WAS FOUND TO BE BACKED OUT ON THE PILOTS WHEEL BY A .2500 TURN. WHEN THE SCREW BACKS OUT ENOUGH, IT FALLS OUT ALLOWING THE WHEEL TO ROTATE FREELY AROUND THE YOKE. THIS RESULTS IN NO FLIGHT CONTROL INPUT. PRSDR 2003FA0000787Screw · backed outTHE SCREW THAT HOLDS THE CONTROL WHEEL TO THE YOKE WAS FOUND TO BE BACKED OUT ON THE PILOTS WHEEL BY A .2500 TURN. WHEN THE SCREW BACKS OUT ENOUGH, IT FALLS OUT ALLOWING THE WHEEL TO ROTATE FREELY AROUND THE YOKE. THIS RESULTS IN NO FLIGHT CONTROL INPUT. PRSDR 2003FA0000786Screw · undersizeTHE SCREW THAT HOLDS THE CONTROL WHEEL TO THE YOKE WAS FOUND TO BE BACKED OUT ON THE PILOTS WHEEL BY A .2500 TURN. WHEN THE SCREW BACKS OUT ENOUGH, IT FALLS OUT ALLOWING THE WHEEL TO ROTATE FREELY AROUND THE YOKE. THIS RESULTS IN NO FLIGHT CONTROL INPUT. PRSDR 2003FA0000797Screw · looseDURING FLEET-WIDE INSPECTION, FOUND SCREW THAT ATTACHES CONTROL WHEEL TO CONTROL SHAFT LOOSE. RECOMMEND DIFFERENT METHOD OF ATTACHMENT OR THE USE OF A LOCKING/SAFETY DEVICE.SDR 2003FA0000796Screw · looseDURING FLEET-WIDE INSPECTION, FOUND SCREW THAT ATTACHES CONTROL WHEEL TO CONTROL SHAFT LOOSE. RECOMMEND DIFFERENT METHOD OF ATTACHMENT OR THE USE OF A LOCKING/SAFETY DEVICE.SDR 2003FA0000795Screw · looseDURING FLEET-WIDE INSPECTION, FOUND SCREW THAT ATTACHES CONTROL WHEEL TO CONTROL SHAFT LOOSE. RECOMMEND DIFFERENT METHOD OF ATTACHMENT OR THE USE OF A LOCKING/SAFETY DEVICE.SDR 2003FA0000785Screw · looseDURING FLEET-WIDE INSPECTION, FOUND SCREW THAT ATTACHES CONTROL WHEEL TO CONTROL SHAFT LOOSE. RECOMMEND DIFFERENT METHOD OF ATTACHMENT OR THE USE OF A LOCKING/ SAFETY DEVICE.SDR 2003FA0000692Bearing · corrodedROD ASSY PN 2613440-1 LOCATED CENTER FLOOR FORWARD BY PEDESTAL FORWARD BEARING NOTED, CORRODED AND WORN TO HAVE EXCESSIVE PLAY. BEARING HAS GREASE FITTING BUT HARD TO GAIN ACCESS TO, ALSO NOTED, EXCESSIVE WATER ACCUMULATING IN THIS AREAS AND NO DRAIN HOLES NOSDR CA030611005Spring · broken(CAN) THE SPRING (P/N 1600104-1) THAT RETRACTS THE CONTROL LOCK (P/N 1613195-1) IN FLIGHT FAILED AND ALLOWED THE CONTROL LOCK ASSEMBLY TO EXTEND AND SUBSEQUENTLY PARTIALLY JAM THE CONTROL STICK. THE PILOT WAS ABLE TO DISENGAGE THE LOCK ASSEMBLY WHICH HAD JAMMESDR 2003FA0000584Bearing · wornWHILE INSPECTING THE AIRCRAFT, THE PILOTS YOKE TUBE WAS OBSERVED TO HAVE BEEN WORN DUE TO CHAFFING ON THE UNDERSIDE. THE COATING ON THE YOKE GUIDE ROLLER BEARINGS HAD WORN OFF AND THE TUBE HAD WORN ABOUT .3333 OF THICKNESS OF THE TUBE. IN ADDITION TO THE GUISDR 2003FA0000488Yoke · crackedDURING ANNUAL INSPECTION, OWNER REQUESTED YOKES BE CHANGED. BOTH YOKES WERE FOUND TO BE CRACKED ON THE LOWER SIDE, THROUGH THE HOLE FOR THE ROLL PIN. THE CONDITION WAS NOT VISIBLE WIGHOUT REMOVING EMBLEM AND YOKE, AS PLASTIC COATING ON YOKE EXTERIOR HAD NOT SDR HEEA084250Structure · crackedLT COLUMN STRUCTURE CRACKED.SDR HEEA084243Panel · crackedCONTROL COLUMN PANEL CRACKED.
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