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 QXEA2019090300335Unknown · malfunctionedMINOR THUMPING NOISE AND FEELING WHEN PULLING AFT ON CONTROL COLUMN FROM CAPT SIDE. NOT OBSERVED ON AFTER START FLIGHT CONTROL CHECK. ONLY LATER IN FLIGHT AND AFTER LANDING. REMOVED FROM SERVICE. PERFORMED GVI OF CONTROL COLUMN POSITION SENSORS, NO DEFECTS NSDR QXEA2019081200314Chain · lack of lubeBOTH YOKES CANTED 15 DEGS RIGHT OF CENTER ON GROUND, ON TAKE - OFF ROLL, ON CLIMB OUT. REQUIRES LEFT AILERON TRIM INPUT OT FLY LEVEL. ADDITIONALLY, NOTICED LOUD SQUEAK FROM YOKE WHEN MOVING LEFT TO RIGHT. REMOVED FROM SERVICE. REMOVED WING PANELS 532JB, 632JBSDR CA190808010Screw · wrong part(CAN) DEFECT DESCRIPTION DWG: C6CF1225 REV U. IN ASSY 3, 6 AN526-632R4 SCREWS WERE FOUND NONCONFORMING, NOT IN SAFETY OF THE ANCHOR NUT ON THE C6CF1244-3 FWD COVER OF THE C6CF1225-S7 CONTROL COLUMN CONTAIN ACTION WAS CARRIED OUT IN YYJ ON MSN AIRCRAFT NUMBER SDR AALA2019061439003Memory Device · smokeAIRCRAFT WAS GROUNDED: PILOT REPORTS SMOKE COMING FROM FIRST OFFICERS YOKE. MAINTENANCE ACCOMPLISHED CARD 05-96-70 AND FOUND F/OS CONTROL COLUMN MEMORY DEVICE AT FAULT. VISUALLY INSPECTED WIRES, FOUND OKAY. REPLACED F/OS CONTROL COLUMN DEVICE IAW AMM 33-11-00.SDR V6NA2019050701Bushing · missingWHILE INVESTIGATING PILOT REPORT OF LEFT / RIGHT AND FORWARD PLAY, DETERMINED CONTROL WHEEL DRUM BEARING (P/N MS27646-43) TO BE WORN. UPON FURTHER INVESTIGATION, DETERMINED BEARING WEAR RESULTING OF MISSING CONTROL WHEEL DRUM BUSHINGS (P/N'S 4527102086-003 ANDSDR AALA201904129007Yoke · out of adjustAIRCRAFT WAS GROUNDED: PILOT REPORTS YOKE POSITIONED ALL THE WAY LEFT DIFFICULT TO POSITION OTHER THAN LEFT. TURNED ON HYDRAULICS AND NO CHANGE. LOOKED OUTSIDE WINDOW AT WINGS, LEFT SPOILERS WERE MOSTLY ALL THE WAY UP. RIGHT WING NO SPOILERS. MAINTENANCE FOUNSDR TLOA20190415002Stop Fitting · out of positionON THE ABOVE DATE TAKE-OFF WAS ABORTED DUE TO CONTROL YOKE REFUSAL TO MOVE AFT. UPON TROUBLE SHOOTING DISCOVERED PART NUMBER 555.20.12.186 LEVER ARM FITTING PLASTIC STOP HAD EXITED THE LEVER ARM AND JAMMED THE ELEVATOR COUNTERWEIGHT, PART NUMBER 527.30.12.053,SDR TLOA20190415001Stop Fitting · out of positionON THE ABOVE DATE TAKE-OFF WAS ABORTED DUE TO CONTROL YOKE REFUSAL TO MOVE AFT. UPON TROUBLE SHOOTING DISCOVERED PART NUMBER 555.20.12.786 LEVER ARM FITTING PLASTIC STOP HAD EXITED THE LEVER ARM FITTING AND JAMMED THE ELEVATOR COUNTERWEIGHT, PART NUMBER 527.30SDR 201900165Stop Fitting · looseON THE ABOVE DATE TAKE-OFF WAS ABORTED DUE TO CONTROL YOKE REFUSAL TO MOVE AFT. UPON TROUBLE SHOOTING DISCOVERED PART NUMBER 555.20.12.786 LEVER ARM FITTING PLASTIC STOP HAD EXITED THE LEVER ARM FITTING AND JAMMED THE ELEVATOR COUNTERWEIGHT, PART NUMBER 527.30SDR HALA2019040500176Disconnect Unit · malfunctionedDURING YOKE FOR AND AFT MOVEMENT CLUNKING SOUND AND BINDING FELT. RE-SET CONTROL COLUMN DISCONNECT PER B717 AMM 27-31-10-440-801, PERFORMED VISUAL INSP OF ELEVATORS AND YOKE SYS ON GROUND, OPS CK FOR FREEDOM OF MOVEMENT, NO BINDING NOTED, ALL INDICATIONS ON DSDR CA190327002Controller · intermittent(CAN) CAPTAIN NOSE DOWN TRIM SWITCHED INTERMITTENT O CAN FEEL ISSUE WITHIN SWITCH ASSY. WHEN CYCLED O REPLACED CAPTAINS SIDE STICK CONTROLLER.SDR AALA2019032979036Module · shortedAIRCRAFT RETURNED TO THE GATE DUE TO POSSIBLE SMOKE FROM THE FIRST OFFICER YOKE. THE AIRCRAFT WAS GROUNDED. MAINTENANCE THOUBLESHOT IAW WDM 33-11-21 AND FOUND THE FIRST OFFICER CONTROL COLUMN MEMORY DEVICE INTERNALLY SHORTING. REMOVED AND REPLACED THE MEMORSDR QXEA2018092400345Sensor · malfunctionedVIBRATION IN CONTROL COLUMN + FLOOR WHEN PULLING YOKE AFT + RELEASING FORWARD ALSO SOME NOISE. REMOVED FROM SERVICE. REPLACED LT CONTROL COLUMN COMMAND POSITION SENSOR REF AMM 27-33-01-000/400-801A. RETURNED TO SERVICE.SDR AALA2018042500004Control Column · fodAIR INTERRUPT DUE TO AILERON BINDING. DURING ACCOMPLISHMENT OF ATBT FOUND DEBRIS IN F/OS CONTROL WHEEL, CLEARED DEBRIS OPERATIONS CHECKS GOOD OK FOR SERVICE. AIRCRAFT WAS GROUNDED.SDR HALA2018032700125Damper · brokenCAPTAIN`S CONTROL STICK, SEEMS TO HAVE DECREASED CONTROL FEEL WHEN APPLYING LT AILERON VS APPLYING RT AILERON. FIRST OFFICER`S STICK HAD NORMAL FEEL. REMOVED THE CAPTAIN`S STICK IAW AMM 27-92-41. THE INTERNAL DAMPENER FOUND BROKEN. REPLACED THE CAPTAIN`SSDR CALA2018020900539Yoke · arcedELECTRICAL ARCING AND SMOKE EMINATING FROM FIRST OFFICERS YOKE BY LEFT HANDLE. REPLACED YOKE REMINDER OP CHECKED GOOD, NO OTHER DAMAGE NOTED.SDR 2018FA0000047Handle · brokenCO-PILOTS CONTROL STICK SHELL BROKEN DURING AIRCRAFT CLIMB.SDR MTNA201801110002HTorque Tube · corrodedCORROSION FOUND IN THE ELEVATOR CONTROL COLUMN TORQUE TUBE.SDR SIMA20180102002Sensor · failedELEVATOR FEELS LIKE IT`S GRINDING FROM HALF NOSE DOWN TO FULL NOSE DOWN. SMOOTH ON NOSE UP. ONLY ON CAPTAIN`S SIDE. FOUND THE CONTROL COLUMN COMMAND POSITION SENSOR TO BE MAKING GRINDING NOISE AND VIBRATION. REMOVED AND REPLACED THE CONTROL COLUMN COMAND POSDR SIMA20180101003Control Column · bindingDURING DESENT, CONTROL COLUMN ON BOTH SIDES STUCK IN A TURN . SNAPPED THOUGH BIND. REPEATED IN A LEFT TURN , CONTINUED UNTILL THE ACFT SLOWED TO 220. BOTH COLUMNS WOULD BIND IN BOTH LT AND RT TURNS . IT TOOK GOOD AMOUNT OF PRESSURE TO SNAP PAST THE BIND SDR SIMA20180101004Sensor · failedAILERONS BINDING AND SNAPS WHEN TURNING AND BANKING. REMOVED AND REPLACED THE FIRST OFFICER`S CONTROL YOKE MIDDLE POSITION SENSOR IAW AMM 27-66-01.SDR 2017FA0000623Universal Joint · separatedUPON LANDING FLARE TO TOUCHDOWN AT 0C0, THE PILOT EXPERIENCED A COMPLETE LOSS OF FLIGHT CONTROLS. ONCE THE WHEELS CAME INTO CONTACT WITH THE RUNWAY, THE PILOT WAS ABLE TO REACH TO COPILOT SIDE YOKE FOR CONTROL. THERE WAS NO INJURIES OR DAMAGE TO THE AIRCRAFT.SDR DALA2018020600712Lever · bindingAT FLARE FOR LANDING, ELEV CONTROL MAN ILLUMINATED AND YOKE CONTROL OF ELEVATOR FELT FROZEN OR JAMMED. DID NOT FEEL MERELY UN BOOSTED AND HYDRAULIC ELEVATOR CONTROL DID NOT INDICATE OFF. TROUBLESHOT AND FOUND LEFT SIDE LEVER ASSEMBLY BINDING. CAUSING MANUAL RSDR 2017FA0000500Control Stick · crackedCO-PILOT CONTROL STICK HANDLE CRACKED AND SEPARATED.SDR 2017FA0000304Universal Joint · brokenTHIS PART CONNECTS THE PILOT'S CONTROL YOKE TO THE FLIGHT CONTROL CABLE SYSTEM ON THIS AIRCRAFT. THE NEWLY INSTALLED UNIVERSAL FAILED WHILE THE PILOT WAS ACCOMPLISHING A FINAL FLIGHT CONTROL CHECK PRIOR TO TAKEOFF. THERE WAS NO INDICATION OF DIFFICULTY OR FAILSDR RJEF20170614001Feel Unit · lack of lubeUPON ARRIVAL, THE PILOT REPORTED THAT DURING ROTATION AND AP DISCONNECT FOR LANDING, CONTROL COLUMN DOES NOT FEEL FREE. MAINTENANCE PERSONNEL PERFORMED FAULT ANALYSIS IAW FIM 27-10-00-810-803-A, FOUND ABNORMAL MOVEMENT CONDITION ON THE CONTROL COLUMN OF THSDR 2017FA0000041Elevator · frozenAFTER BEING IN THE COLD, THE ELEVATOR CONTROL BECAME INCREASINGLY HARD TO CONTROL SUSPECTED GREASE IN THE COLD TEMPS.SDR ECPR2016082972735Bar · brokenON PREFLIGHT THE STUDENT PILOT REPORTED THAT THE CONTROL SYSTEM DID NOT FEEL RIGHT. MAINTENANCE PERSONNEL INSPECTED THE CONTROL WHEEL SYSTEM AND FOUND THAT THE UPPER HORIZONTAL PORTION OF THE PN 62703-033, TEE BAR ASSEMBLY WAS FOUND DETACHED FROM THE VERTICALSDR AALA20160727004Control Column · smokeSMOKE WAS OBSERVED COMING FROM THE FIRST OFFICER`S CONTROL YOKE AT THE NUMBER WHEEL. AN ELECTRICAL ODOR WAS ALSO NOTED AND THE YOKE WAS REPORTED TO BE WARN TO THE TOUCH. AIRCRAFT GROUNDED. MAINTENANCE REMOVED AND REPLACED THE CONTROL COLUMN REMINDER ASSEMBLYSDR COEA2016050650911Bracket · corrodedHEAVY CHECK COE/MINOR REPAIR: LEVEL 2 CORROSION ON PILOTS SIDE CONTROL COLUMN STOP BRACKET ASSEMBLY. REPLACED WITH OEM PART.SDR A6WA201643775Unknown · malfunctionedFLIGHT 3882 CAPTAINS & FIRST OFFICERS YOKE REQUIRED EXCESSIVE FORCE TO TURN IN BOTH DIRECTIONS WITH AP ON & OFF, FLIGHT CONTROL SYNOPTIC PAGE SHOWED NORMAL, FLIGHT CONTROL CHECK PRIOR TO DEPARTURE NORMAL, HEAVY AFTER LANDING, NO ABNORMAL ISSUES WHEN AP SELECTESDR 2016FA0000152Yoke · brokenPILOT CONTROL YOKE LT HORN BROKEN OFF. BELIEVE CAUSED BY DRILLING YOKE FOR PUSH TO TALK BUTTON.SDR CA160307002Bar · cracked(CAN) THE CONTROL COLUMN TEE BAR ASSEMBLY WAS REMOVED FROM AIRCRAFT C-GQPV MODEL PA-28-140 SERIAL NUMBER 28-7725161 AT 18602.5 HOURS TTAF TO SERVICE C-GQPN MODEL PA-28-140 SERIAL NUMBER 28-7725157 DUE TO CONTROL COLUMN TEE BAR FAILURE IN FLIGHT. (REFERENCE SDRSDR AALA20160208010Control Column · jammedIN FLARE FOR LANDING, THE FIRST OFFICER`S CONTROL COLUMN MOMENTARILY JAMMED, REQUIRING EXCESSIVE FORCE TO FLARE FOR TOUCHDOWN. ACCOMPLISHED FAULT ISOLATION PROCEDURE IAW FIM TASK 27-31-00-810-801 & FOUND COLUMN MOVES FREELY. NO DEFECTS NOTED FOR CONTROL COLUSDR FDEA201601020009Yoke · excess playTURNS TO THE RT, MORE PRONOUNCED AT SPEEDS LESS THAN 300 KTS, AN APPARENT PERCEIVED BIND IN THE YOKE. THEN LET’S GO & YOKE WILL THEN MOVE. ALSO NOTICED THIS WITH AUTOPILOT ENGAGED. PLAY IN THE YOKE, CAPTAINS SIDE. PERFORMED DETAILED VISUAL INSPECTION OF AISDR 2016FA0000002Control Wheel · crackedAFTER INITIAL CLIMB THE CO-PILOT ATTEMPTED TO LOWER THE NOSE OF THE ACFT FOR CRUISE CLIMB. AS SOON AS FORWARD FORCE WAS APPLIED TO THE CONTROL WHEEL THE RT HORN CRACKED AND ARTICULATED FORWARD. CONTROL OF THE ACFT WAS TAKEN OVER BY THE F/O WHO MADE DECENT ANSDR CA151229019Spring · fractured(CAN) DURING PREFLIGHT CHECKS, CREW EXPERIENCED LIGHTER THAN NORMAL CONTROL COLUMN FORCES WITH REGARDS TO THE ELEVATOR CONTROLS. MAINTENANCE STAFF INVESTIGATED AND FOUND BOTH INNER AND OUTER SPRINGS PN 69-73360-1 AND 69-73361-1 ON THE FEEL AND CENTERING UNIT SDR CA160105006Yoke · corroded(CAN) DURING VISUAL INSPECTION OF CONTROL YOKE ASSEMBLY, PN 0760030-1, HOLE NOTED IN HORIZONTAL STEEL TUBE ON LT SIDE OF CONTROL YOKE WELDED ASSEMBLY, PN 0711850-1, APP. 2" FROM WELDED JOINT TO VERTICAL TUBE. HOLE APPROXIMATELY .2" ACROSS AND OVAL IN SHAPE. OSDR 2015FA0000611Control Wheel · crackedDURING A CHECK FLIGHT PILOT'S CONTROL YOKE CRACKED AND SEPARATED ON THE LT SIDE, ON THE LT HORIZONTAL SECTION, 1" FROM THE LT 90 DEGREE BEND FROM VERTICAL. YOKE PN IS UNKNOWN SINCE CURRENT PARTS MANUALS ONLY LIST CURRENTLY AUTHORIZED CONTROL YOKE PNS ALTHOUGHSDR YENA20150901405Dampener · dirtyFLIGHT DIVERTED, DURING T/O ROLL CONTROL COLUMN WAS VERY STIFF DURING ROTATION AFTER TAKEOFF, CONTROL COLUMN WAS STILL STIFF AND VIBRATION WAS FELT DURING LT AND RT TURNS. NO VIBRATION IN NEUTRAL POSITION. VIBRATION WAS FELT WITH AND WITHOUT AUTOPILOT. STIFSDR DXTA2015083106071Pushrod · damagedA VIBRATION IN THE CONTROLS & IN THE FLOOR, NOTICEABLE IN SMOOTH AIR IN CRUISE AT FL 400. AT LOWER ALTITUDES VIBRATION GOES AWAY. FOUND ELEVATOR TRIM TABS LOOSE DUE TO WORN PUSHRODS & HARDWARE AT TRIM TAB ACTUATOR. R & R LT & RT ELEVATOR TRIM TAB INNER & SDR 2015FA0000411Yoke · damagedDURING A PHASE "A THRU D" INSPECTION, WE REMOVED THE CONTROL YOKE FLOORBOARD PROTECTIVE BOOT LT/RT SIDES. ON LT SIDE WE FOUND CORROSION, ABOUT HALFWAY DOWN THE BACK OF THE BOSS TO WHERE THE BOSS ATTACHES TO THE AIRCRAFT. INSPECTION B2 ITEM, CONTROL WHEEL SECSDR FQAR20150805085Universal Joint · separatedDURING FLIGHT, THE STUDENT PILOT SEATED AT THE LT CONTROLS NOTED THE YOKE & YOKE SHAFT HAD DISCONNECTED & NO LONGER WERE CONTROLLING THE PITCH OR ROLL. THE FLIGHT INSTRUCTOR TOOK CONTROL, HE NOTED THE AILERON TRAVEL WAS RESTRICTED BUT CONTROL COULD BE MAINTAISDR AALA20150704004Counter · faultyDURING FLIGHT, SMOKE EMITTED FROM CAPTAINS YOKE DIGITAL WINDOW. TURNED OFF MAIN PANEL LIGHTING & SMOKE CEASED. R & R CAPTAINS YOKE MEMORY COUNTER IAW AMM 20-10-11 & 33-11-00. WIRING AT COUNTER CHECKED GOOD. SYSTEM CHECKED NORMAL.SDR E4EB2015121101Control Column · corrodedCOPILOT'S CONTROL COLUMN IS EXFOLIATED THROUGHOUT. GAINED ACCESS TO CONTROL COLUMN. REPLACED COPILOT'S CONTROL COLUMN IAW AMM.SDR E4EB2015120913Control Column · corrodedCAPTAINS CONTROL COLUMN, LOWER END IS CORRODED. GAINED ACCESS. REPLACED CAPTAINS CONTROL COLUMN PN 5614272-501.SDR CA150601009Yoke · obstructed(CAN) ELEVATOR SEEMED TO JAM WHEN NOSE UP APPLIED ON LANDING BEFORE IT REACHED THE STOP. INSPECTED ELEVATOR CONTROL SYS & FOUND TRAVEL LIMITED TO 11 DEGREES NOSE UP. INSPECTED SYS FOR OPERATION & FOUND LOOSE PIECE OF PLASTIC, FOD, LODGED IN COPILOTS YOKE BOOSDR DXTA2015050806015Yoke · vibrationAFTER TAKEOFF, FIRST OFFICER FELT BINDING IN THE CONTROL YOKE & COULD FEEL IT IN HIS FEET. PASSING 230 KTS, BOTH YOKES VIBRATED & FELT IN THE COCKPIT. MOVED FLT CONTROLS, ELEVATOR & RUDDER CONTROL CABLE DAMPENER PULLEYS , RUN BLOCK WORN & GROOVED. INSPECTEDSDR 29GA2015031200001Unknown · vibrationFLIGHT LEVEL, FLIGHT WITH FLAPS 15 DEGREES AT 150 KNOTS CONTROL COLUMN SHUDDER NON STOP.SDR SWIA201540628Nut · undertorquedTHERE IS AN AILERON CLICK WHEN MOVING THE CAPTAIN`S YOKE THROUGH FULL RANGE OF TRAVEL, TORQUED PILOT CONTROL COLUMN FORWARD NUT IAW REO.
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