JASC 2701

Service difficulty reports · 510

Reports filed under 2701 · Control Column Section, newest first.

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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.

SDR QXEA2009021900130Control Column · out of adjustPDX - EXCESSIVE PLAY IN THE AILERONS FROM THE LT AND RT YOKE, WHILE HAND FLYING. WITH THE AUTOPILOT ENGAGED THERE WAS STILL EXCESSIVE PLAY IN BOTH AILERONS. DIVERTED TO PDX. UNEVENTFUL LANDING. ADJUSTED CONTROL COLUMN CHAINS FOR THE PILOT AND CO-PILOT YOKEFeb 16, 2009 · N402QX · Bombdr DHC8402SDR BSYA2009012Chain · looseAIRCRAFT DEPARTED LCK AND MADE A 30 DEGREE LEFT BANK, HAD A HARD TIME COMING OUT OF TURN AND HAD TO USE A LOT OF RIGHT AILERON TO MAINTAIN STRAIGHT AND LEVEL FLIGHT. MAINTENANCE FOUND CHAIN LOOSE IN CONTROL YOKES. TIGHTENED CHAIN, TEST FLIGHT GOOD.Feb 5, 2009 · N858LG · Beech 58SDR BSYA2009009Key · out of positionGOING INTO CLE PILOT NOTICED CONTROL YOKE ROCKING BACK AND FORTH. MAINTENANCE FOUND LOCKING KEY HAD FALLEN OUT, REPLACED KEY OPS CHECKS GOOD.Jan 27, 2009 · N21ES · Beech 58SDR 08FDEA04863Sensor · failedDURING T/O ROLL RECEIVED ECAM WARNING OF PITCH TRIM NOT IN T/O RANGE, REJECTED T/O. AFTER CONFIRMING PITCH TRIM PROPERLY SET (VIA PERFORMING COMPUTER NUMBERS) TESTED T/O CONFIG TEST AND STILL RECEIVED SAME WARNING ON ECAM. PITCH TRIM SHOWS IN GREEN BAND ONNov 11, 2008 · N815FD · Airbus A310324SDR SWIA200819960Bearing · bindingA SLIGHT DETENT CAN BE FELT WITH AILERON MOVEMENT. FLIGHT 3604. REPLACED RIGHT AND LEFT AILERON CONTROL YOKE BEARINGS. Aug 14, 2008 · N578SW · Emb EMB120ERSDR 2008UALA03782Control Column · vibrationVIBRATION FELT IN CONTROL COLUMN. FLIGHT DIVERTED. Jul 8, 2008 · N653UA · Boeing 767322SDR SWIA200819797Bearing · bindingCONTROL YOKE HAS A BINDING FEEL ALONG WITH AN AUDIBLE SOUND WHEN AILERONS ARE FULLY DEFLECTED. (FLIGHT NR 5999) REPLACED CAPTAINS AND FIRST OFFICERS CONTROL WHEEL SHAFT BEARINGS IAW MM 27-11-01. OPS CHECK GOOD. Jun 24, 2008 · N964SW · Cndair CL6002B19SDR CA080630002Control Column · corroded(CAN) WHILE CARRYING OUT AN ANNUAL INSP AND SEB 01-3 R1 HEAVY CORROSION WAS FOUND INTERNALLY IN CONTROL YOKE. A/C HISTORY SHOWED FRESH WATER SUBMERSION IN 1982.Jun 23, 2008 · Cessna A185FSDR DXTA200803135Control Column · ratchetingCONTROL YOKE HAS A DEAD ZONE WHEN MOVING AILERON FROM NEUTRAL POSITION THEN "RATCHETS" RESULTING IN EXCESSIVE & JERKY INPUT. (B)Jun 21, 2008 · N989QS · Cessna 750SDR 2008FA0000497Boot · misinstalledAT LOCATION WHERE CONTROL "STICK" PASSES THROUGH L/R SIDE ARM REST, THE BOOT SURROUNDING BASE OF STICK LIES OPEN TO CONTROL MECHANISMS. WHERE THE STICK ENTERS THE COCKPIT, THE LEATHER BOOT THAT IS DESIGNED TO COVER THE AREA BENEATH THE STICK, IS PARTIALLY OPENJun 20, 2008 · N896MH · Adamac A500SDR 2008UALA03323Control Column · stiffCREW REPORTS EXCESSIVE CONTROL COLUMN FORCE REQUIRED FOR PITCH.Jun 11, 2008 · N914UA · Boeing 737522SDR DXTA200803066Computer · false activationAT CRUISE ALTITUDE FL410 A PULSATING THUMP COULD BE FELT IN BOTH CONTROL COLUMNS. INSPECTED, ALL PANELS, FLT CONTROLS DOORS ETC. NO DEFECTS NOTED. REMOVED AND REPLACED RT AOA COMPUTER IAW MM 34-14-01 C/W FT OF AOA SYSTEM PER SAME OPS CHECK GOOD.May 18, 2008 · N950QS · Cessna 750SDR A6WA200840401Control Column · looseREQUEST INSPECTION OF FIRST OFFICER`S CONTROL COLUMN FOR SUSPECTED EXCESSIVE PLAY IN NEUTRAL POSITION. PERFORMED OPS CHECK OF ELEVATOR CONTROL SYSTEM USING PITCH FEEL CHECK IAW AWAC SUPPLEMENT 2006-004A. OPS CHCEK GOOD. NO DEFECTS NOTED. (A)May 13, 2008 · N433AW · Cndair CL6002B19SDR BB08084Control Column · bindingPHL FLT 0703 FRA TO PHL - DURING THE FLIGHT, THE FIRST OFFICER'S CONTROL WHEEL WAS BINDING WHILE USING THE AILERONS. THE FLIGHT CONTINUED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE IS CURRENTLY INSPECTING THE AIRCRAFT.May 8, 2008 · N252AU · Boeing 7672B7SDR DXTA200803016Yoke · lockedIN FLIGHT W/SPOILERS DEPLOYED, AC PITCHED FWD, YOKE LOCKED UP AND ROLL AUTHORITY WAS LOST UNTIL SPOILERS WERE STOWED. INSPECTED SPOILERS AND SPOILER CABLES, NO DEFECTS NOTED. DEPLOYED SPOILERS WITH HYDRAULIC POWER AND CHECKED YOKE FOR FREEDOM OF MOVEMENT, CHEApr 24, 2008 · N153QS · Beech 400ASDR 2008UALA02163Bolt · out of rigCAPTAIN'S ELEVATOR CONTROLS FEEL HEAVY. CREW COMMENTS: EXCESSIVE BACK PRESS REQUIRED ON TO. 3.3 SET OVER 6 UNITS REQUIRED TO TRIM OUT PRESSURE. OK IN FLT. FOUND CAPTAINS AFT QUADRANT STOP BOLT OUT OF RIG. REMOVED ONE WASHER AT STOP BOLT. RECHECKED AFTER RIApr 14, 2008 · N517UA · Boeing 757222SDR GUUA04040803Control Column · obstructedFLT NR 9188, ON FINAL APPROACH CONTROL COLUMN JAMMED. REQUIRED STRENGTH OF BOTH CREW MEMBERS TO OVER COME. MAINT DETERMINED THAT A WIRE BUNDLE FROM UNDER AND FWD OF THE INSTRUMENT PANEL WAS INTERFERING WITH THE CONTROL COLUMN. THE WIRE BUNDLE WAS POSITIONEApr 4, 2008 · N231YV · Beech 1900DSDR DXTA20082960Sprocket · obstructedJAMMED ELEVATOR TRIM TAB ON DEPARTURE. FOUND FOD WEDGED IN CHAIN SPROCKET AREA OF PEDESTAL. REMOVED FOD, NO DAMAGE NOTED, CLEANED AND LUBED TRIM COMPONENTS, OPS CHECK AND TRAVEL CHECKS GOOD AT THIS TIME. REF. CE560 M/M 27-31-00.Mar 23, 2008 · N374QS · Cessna 560CESSNASDR SWIA200819324Bearing · roughFLT 5951 - BOTH CONTROL YOKES FEEL ROUGH WHEN MOVED TO THE RIGHT. REPLACED CAPTAINS CONTROL WHEEL SHAFT BEARINGS IAW CRJ 700 MM 27-31-01 AND 27-11-01. Mar 5, 2008 · N710SK · Cndair CL6002C10SDR SWIA200819320Bearing · roughFLT 6272 - AILERON FLIGHT CONTROLS DO NOT FEEL SMOOTH AT LOWER AIRSPEEDS. REPLACED FIRST OFFICERS CONTROL COLUMN BEARINGS PER AMM 27-11-01. OPS CHECK GOOD.Mar 4, 2008 · N771SK · Cndair CL6002C10SDR SWIA200819289Bearing · roughFLT 5802 - RESISTANCE FELT IN THE FIRST OFFICERS YOKE AILERON MOVEMENT. REPLACED THE CONTROL YOKE SHAFT SUPPORT BEARINGS IAW MM 27-11-01. OPS CHECK GOOD.Feb 29, 2008 · N965SW · Cndair CL6002B19SDR SWIA200819287Bearing · roughCLICKING NOISE IN RIGHT YOKE WHEN AILERONS MOVED TO FULL TRAVEL, FLIGHT NR 3932. REPLACED BEARINGS IN RIGHT YOKE IAW MM 27-11-01. OPS CHECK GOOD.Feb 28, 2008 · N447SW · Cndair CL6002B19SDR 2008FA0000220Control Wheel · brokenON TAXI FROM REFUELING PILOT WAS MAKING A LT TURN IN FRONT OF HANGER. PULLED CONTROL WHEEL FULL AFT (TO TAKE WEIGHT OFF OF FRONT WHEEL) CONTROL WHEEL BROKE OFF IN HIS HAND. (OUTSIDE TEM APPROX 20 DEGREES) BREAK WAS FROM LWR LT (7 OCLOCK) TO UPPER RT (2 OCLOCFeb 22, 2008 · N34264 · Cessna 172ASDR 2008UALA00829Unknown · unknownCREW REPORTS, YOKE HAS A BUMP WHEN MOVING. FULL FORWARD TO AFT APPROX 3 INCHES AFT OF THE ELEVATOR FORWARD STOPS.Feb 14, 2008 · N332UA · Boeing 737322SDR DXTA200802790Control Column · vibrationVERY HIGH DEGREE OF VIBRATION IN CONTROL COLUMN AND YOKE AT ALL SPEEDS ABOVE 250 KNOTS AND AT ALL ALTITUDES ABOVE THAT SPEED. PERFORMED ELEVATOR AND ELEVATOR TRIM CABLE TENSION CHECK, PERFORMED FREE PLAY CHECK ON RT/LT AILERON, ALSO PERFORMED INSPECTION OF CAJan 22, 2008 · N639QS · Cessna 560XLSDR 2008FA0000018Yoke · misinstalledWHILE DOING AN ANNUAL, FOUND LOOSENESS IN THE YOKE FOR AND AFT MOVEMENT. AFTER MUCH CHECKING, FOUND THE LOOSENESS TO BE BETWEEN THE YOKE LEVER ASSY 1767033-7 AND 1767037-2 WHICH IS THE SHAFT. ALSO THERE WAS LOOSENESS BETWEEN THE SHAFT 1767037-2 AND THE QUADRAJan 8, 2008 · N30673 · Cessna 177BSDR 2007UALA05303Control Column · malfunctionedCAPTAIN'S ELEVATOR CONTROLS FEEL HEAVY. CREW COMMENTS: VERY HEAVY ELEVATOR AT TAKEOFF ROTATION. GW AT T/O WAS 236.0, VR WAS 158KTS. TRIM 4.6 ANU. FORCE MEASURMENT FOR AILERON WHEEL TRAVEL RT 26 LBS AND LT 27 LBS REF AMM 27-11-00. LIMITS EXCEEDS MAX OF 21Dec 26, 2007 · N506UA · Boeing 757222SDR DXTA200702688Switch · inoperativeAFTER TAKEOFF PITCHTRIM FAILED AT 2000 FT AGL, PITCH TRIM WOULD NOT LEAVE GREEN ARC. FOUND PILOTS PITCH TRIM SWITCH INOP. REMOVED PILOTS YOKE ASSY. PN 128284060-13 SN 0039 AND INSTALLED NEW PILOTS YOKE ASSY. PN 128384060-13, SN 0076. IAW CMM 27-10-15 OPERATIODec 18, 2007 · N101QS · Beech 400ASDR TRAX200701552Yoke · bindingFELT A POP AND BINDING WHEN TURNING YOKE TO THE LEFT. EXCESSIVE FORCE OR STRENGTH NEEDED TO TURN YOKE LEFT ALSO. A/C RETURNED TO DAY AFTER T/O. EMERGENCY DECLARED. FLT 4434 DEL 61 MINS. NC FLT 4434 CX.Oct 21, 2007 · N936EV · Cndair CL6002B19SDR FDKA200710554Unknown · unknownFDM 6031 ATL (1305 PHX LCL) - YOKE CATCHING ON SOMETHING, MOVEMENT NOT SMOOTH. MX FOUND YOKE MOVEMENT SMOOTH. NO CLICK NOTED WHEN GUSTLOCK C/B IS PULLED.Oct 17, 2007 · N844MJ · Emb EMB145LRSDR HNAA0700212Yoke · stuckFLIGHT CONTROL YOKE HUNG UP MOMENTARY DURING APPROACH. PILOT STATED THAT THE YOKE HANG UP HAPPENED IMMEDIATELY AFTER AUTO PILOT WAS DISENGAGED AND DURING ROLL. INSPECTED ENTIRE AILERON AND SPOILER CABLE CIRCUIT NO DEFECTS NOTED. PERFORMED GN OPS OF AUTO PILOct 6, 2007 · N827EX · Dhav DHC8102SDR SWIA200718764Yoke · lack of lubeFLT 2912 - FIRST OFFICERS YOKE MAKES A CLICKING NOISE. CLEANED AND LUBRICATED YOKE ASSEMBLY, BEARINGS AND PULLEYS. NO DEFECTS NOTED.Oct 6, 2007 · N494CA · Cndair CL6002B19SDR 2007UALA03699Yoke · looseYOKE HAS 1.5 UNITS OF PLAY IN-FLIGHT (LOOSE FEEL) BOTH LEFT AND RIGHT. PERFORMED CHECK OF CONTROL WHEEL PLAY AND BACKLASH. CHECKED AILERON TRIM ACTUATOR MOVEMENT. CHECKED AILERON CONTROL CABLES AA, AB,ACBA AND ACBB.NO DEFECTS FOUND.CONTROL WHEEL AILERON COSep 13, 2007 · N933UA · Boeing 737522SDR CA071029002Clamp · loose(CAN) PRIOR TO PUSHBACK, WHEN TOE BRAKES WERE PRESSED TO RELEASE PARK BRAKE, THE CONTROL COLUMN YOKE MOVED AFT APPROX 1 INCH. REF: LOAD CELL INSTALLATION. THE CLAMP IS INSTALLED ON THE CONTROL COLUMN ROD ASSY ON THE TAPERED SECTION OF THE ROD. THE CLAMP CANNOTAug 15, 2007 · Emb ERJ170200SUSDR A6WA200740459Yoke · looseUNUSUAL NOISE HEARD WHEN FIRST OFFICER YOKE TURNED. MORE NOTICEABLE WHEN TURNED RIGHT. ALSO NOTED THROUGH FLOOR ON CAPTAINS SIDE. RETORQUED FIRST OFFICERS YOKE REF SB CRJ-SL-27-045 REV A AND M 27-11-01. OPERATIONAL CHECK GOOD. (M)Aug 11, 2007 · N465AW · Cndair CL6002B19SDR SWIA200718545Bearing · wornFLT 5922 - AILERONS FEEL STIFF WHEN MOVED TO THE LEFT IN FLT. REPLACED LT CONTROL COLUMN SHAFT BEARING PER AMM CH 27-31-01. OPS CHECK GOOD AT THIS TIME.Jul 24, 2007 · N766SK · Cndair CL6002C10SDR SIMA200720101Yoke · stickingCONTROL YOKE FEELS LIKE IT IS JAMMING WHEN MOVING LEFT AILERON.Jul 19, 2007 · N918AE · Emb EMB145LRSDR SIMA200719702Control Column · stuckDURING TAXI CHECK, FLIGHT CONTROL JAMMED WHEN MOVING LEFT AILERON CONTROL COLUMN UN-JAMMED AFTER FEW MINUTES. RETURNED TO THE BLOCK.Jul 13, 2007 · N918AE · Emb EMB145LRSDR SWIA200718479Shaft · looseFLT 6757 - WHILE ON FINAL, FIRST OFFICER REPORTS THAT THE AILERONS FELT STIFF AND STICKY. RETORQUED FORWARD AND AFT NUTS ON CONTROL YOKE SHAFT IAW AMM 27-31-01.Jul 11, 2007 · N766SK · Cndair CL6002C10SDR 2007FA0000599Control Column · fracturedON SECOND FLT OF DAY, & WHILE STILL ON AERO-TOW, PILOT WHO WAS FLYING FROM THE REAR SEAT WITH A NON-PILOT PASSENGER IN FRONT, NOTICED THAT IT REQUIRED APPROXIMATELY 20 DEGREES OF RT-STICK CORRECTION TO MAINTAIN LEVEL FLT. PILOT ALSO OBSERVED AILERONS TO BE INJun 16, 2007 · N4446Y · Grob G103ATWINIISDR DXTA200702259Unknown · unknownON TAKEOFF WHEN CONTROL YOKE PULLED BACK FOR ROTATION , SOMETHING APPARENTLY TRIED TO JAM CAUSING MOMENTARY INCREASE IN RESISTANCE. JAM STOPPED AND CONTROLS BROKE FREE WITH INCREASED PRESSURE. INSPECTED CONTROL YOKES AND BOOTS FOR BINDING, NONE NOTED. REMOVEDJun 12, 2007 · N303QS · Cessna 560CESSNASDR CA070529007Washer · failed(CAN) DURING A SCHEDULE INSPECTION THE PILOT CONTROL WHEEL WAS FOUND TO HAVE MORE FREE PLAY THAN THE CO-PILOT. UPON FURTHER INVESTIGATION IT WAS FOUND THAT THE TAB WASHER P/N 4527102070-001 WHICH IS SECURING THE NUT P/N NAS1423-20. HAD ONLY ONE TAB BENT, TO ADMay 29, 2007 · Lear 45LEARSDR SIMA200709617Bushing · wornCAPTAIN YOKE HAS APPROXIMATELY QUARTER INCH OF DEAD SPACE WHEN MOVING ELEVATOR. REMOVED AND REPLACED BUSHING ON ELEVATOR BELL CRANK IAW EMB AMM. PERFORMED OPERATIONAL CHECKS WITH NO DEFECTS NOTED. RETURNED AIRCRAFT TO SERVICE.Apr 5, 2007 · N702AE · Emb EMB135LRSDR DXTA200702084Control Column · unknownIN CRUISE FLIGHT RT ELEVATOR DEFLECTED DOWN ON EICAS. RT AILERON DEFLECTED UP ON EICAS. CONTROL COLUMN SHOWS RT TURN DURING STRAIGHT AND LEVEL FLIGHT. C/W AILERON RIGGING I/A/W CE 750 M/M 27-10-00. TENSIONS CHECK GOOD AND OPS CHECK GOOD.Apr 5, 2007 · N970QS · Cessna 750SDR DXTA200702033Control Column · vibrationNOTICEABLE VIBRATION OF CONTROL COLUMN DURING TAKEOFF,CLIMB,REDUCED DURING. CRUISE AND BEGINS TO BE MORE NOTICEABLE DURING DECENT AND LANDING. TROUBLESHOT ELEVATOR SYSTEM. FOUND LEFT AND RIGHT ELEV. TRIM TAB BEARINGS TO HAVE EXCESSIVE PLAY. REMOVED AND REPLACMar 17, 2007 · N643QS · Cessna 560XLSDR UIEA200700139Flt Controls · bindingAT T/O WITH FLAP 20 DEGREES THE YOKE WOULD STICK AT ABOUT THE POINT OF 2 UNITS OF RIGHT AILERON TRIM. AFT FLAP WERE AT 10 DEGREES THE YOKE WOULD STICK AT THE SAME POINT, BUT TAKE LESS PRESSURE TO OVERCOME THE PROBLEM, ON APPROACH NO INDICATION OF STICKING WITMar 15, 2007 · N522MC · Boeing 7472D7BSDR SWIA200717675Control Column · obstructedAILERONS SEEM TO BIND MOMENTARILY WHEN ROLLING. MOST NOTICEABLE WHEN TURNING LEFT. RE-POSITIONED CONTROL COLUMN WIRE BUNDLE. OPERATIONAL CHECKS GOOD.Jan 16, 2007 · N703EV · Cndair CL6002C10SDR CA070517003Control Wheel · failed(CAN) EXCESSIVE PLAY IN (U) JOINT ON LT CONTROL WHEEL. (TC NR 20070517003)Dec 14, 2006 · Cessna 172PSDR UPS06M48703Control Column · unknownATB - DURING CLIMB, FEEDBACK FELT IN CONTROL COLUMN WHILE IN PITCH TRIM. ALL SPEEDS & ALTITUDE - SFC - 40K FT, 180KIAS - M.84. THIS WAS LESS PONOUNCED WHEN CONFIGURED ON FINAL THE FEEL WAS NORMAL. FOUND LT INBD ELEVATOR ACTUATOR TO BE FAULTY. REMOVED & INSTALLNov 20, 2006 · N250UP · Doug MD11FSDR DJFA2006343Nut · looseA VIBRATION WAS FELT IN THE YOKE DURING CLIMB AT FLIGHT LEVEL 350. SPEED WAS 280KTS. WENT AWAY AFTER CLIMB WAS STOPPED. FOUND NO TENSION ON CABLE AND JAM NUTS LOOSE. SYSTEM WAS RIGGED, DEFLECTION TRAVEL WAS CHECKED AND TENSIONS SET AND SECURED.Nov 16, 2006 · N824LX · Raythn HAWKER800XP
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