Beech S35

Service difficulty reports · 29

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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 aircraft_model_key = 'S35'
  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 2020FA0000145Turnbuckle · damagedTHE TURNBUCKLE IS LOCATED UNDER THE FLOORBOARD JUST IN FRONT OF THE REAR SPAR CARRY THROUGH ON THE RIGHT SIDE UNDER A HEAT DUCT THAT GOES THROUGH THE REAR SPAR AND SERVICES THE AREA BEHIND THE SECOND TWO SEATS IN THE ACFT. THIS AREA MAY HAVE A FIFTH AND SIXTFeb 12, 2020 · Beech S35 · Miscellaneous HardwareSDR 2020FA0000046Turnbuckle · corrodedTHE AIRCRAFT WAS IN OUR REPAIR SHOP FOR CYLINDER WORK. THE OWNER ASKED WHILE IT HERE, TO LOOK AT THE RIGHT AILERON TURNBUCKLE. THIS REQUEST WAS BASED ON INFORMATION FROM THE PUBLICATION DATED MARCH 2019. SUBSEQUENTLY, WE REMOVED THE SEATS AND FLOORBOARDS TO Jan 15, 2020 · N5618K · Beech S35 · Aileron Control SystemSDR 2020FA0000128Turnbuckle · crackedDURING ANNUAL INSPECTION DISCOVERED RT LOWER AILERON CONTROL CABLE TURNBUCKLE BARREL LOCATED UNDER AFT CABIN HEAT DUCT WAS CRACKED 3/4 INCHES LONGITUDINALLY FROM RT END. THE HEAT AIR DUCT ABOVE THIS TURNBUCKLE ASSEMBLY WAS IN A DECAYED CONDITION. RECOMMEND CJul 8, 2019 · N7972 · Beech S35 · Aileron Control SystemSDR 2019FA0000209Duct · crackedDURING THE ANNUAL INSPECTION, DUE TO A SAFETY RECOMMENDATION, THE SAFETY WIRE ON THE AILERON CABLE TURNBUCKLE WAS REMOVED TO INSPECT THE SWAGED END OF THE CROSSOVER CABLE. THE END NEAREST THE HEATER DUCT WAS FOUND TO HAVE A SIGNIFICANT CRACK. DUE TO THE AFFECTJun 13, 2019 · N977KM · Beech S35 · Aileron Control SystemSDR CA110826006Bolt · corroded(CAN) HEAD OF BOLT CORRODED.Aug 24, 2011 · Beech S35 · Wing Main, Frame StructureSDR AUS20040181Screw · wrong part(AUS) ELEVATOR CONTROL CABLE RUBBING ON SCREW. INVESTIGATION FOUND (A LONGER THAN NORMAL) SCREW HOLDING THE FORWARD CABIN FLOOR IN POSITION. INCORRECT SCREW HAD BEEN FITTED DURING REUPHOLSTERING CARRIED OUT APPROXIMATELY TWO WEEKS PREVIOUSLY. UNAPPROVED PARTMar 10, 2004 · Beech S35 · FastenersSDR 2004FA0000098Throttle Cable · inoperativeDURING LANDING PILOT REPORTED THAT HE COULD NOT RETARD THROTTLE. SUSPECT BEARINGS INSIDE CABLE ARE FREEZING UP. REMOVED AND REPLACED CABLE ASSY.Nov 22, 2003 · N277RB · Beech S35 · Power LeverSDR AUS20020653Cylinder · leaking(AUS) ENGINE CYLINDER LEAKING FROM HEAD/BARREL JOINT.Jul 3, 2002 · Beech S35 · Reciprocating Engine Cylinder SectionSDR 2002FA0000420Turnbuckle · separatedWHILE IN LEVEL FLIGHT AT 5500FT MSL, ATTEMPTING TO TURN THE AIRCRAFT LEFT WITH THE AILERON A SMALL BUMP/BANG WAS FELT. THE CONTROL WHEEL WENT FULL LEFT,AND THE AIRCRAFT COMMENCED ROLLING TO THE RIGHT. APPLICATION OF HARD RIGHT RUDDER STOPPED THE ROLL AT ABOUT Mar 26, 2002 · N2JX · Beech S35 · Aileron Control SystemSDR 2002FA0000197Bearing · inoperativeAIRCRAFT CAME IN FOR ALTERNATOR FAILURE. TESTED ALTERNERATOR SYSTEM AND DETERMINED ALTERNATOR, FAILED. REMOVED ALTERNATOR, NOTICED THAT THE COTTER KEY, NUT AND WASHER THAT HOLDS THE CLUTCH ON, WAS MISSING. FOUND CLUTCH ASSEMBLY BROKEN AND SHAFT OF ALTERNATOJan 30, 2002 · N10WR · Beech S35 · AC Generator-AlternatorSDR AU010352Control Cable · broken(AUS) AILERON THREADED CABLE AND FITTING SEPARATED APPROXIMATELY MIDWAY BETWEEN THE THREADED END AND THE SWAGED NUT.Apr 9, 2001 · Beech S35 · Aileron Control SystemSDR 20010125CW009Clip · missingDURING ANNUAL INSPECTION OF AC A VISUAL INSPECTION WAS PERFORMED ON CHAIN INSIDE THE DUAL CONTROL YOKE. CHAIN MASTER LINK PLATE AND CLIP WERE MISSING FROM LOWER LEFT CHAIN ATTACH POINT TO FITTING. RECOMMEND MORE ATTENTION IN THIS AREA UPON ANNUAL INSPECTION/Jan 25, 2001 · N354D · Beech S35 · Control Column SectionSDR 20000714SH024Blade · crackedPROPELLER SUBMITTAL FOR AD 97-18-02 INITIAL INSPECTIONS. S/N A69152 (BLADE NR 1) FOUND CRACKED IN AREA OF A/O?????? USING EDDY CURRENT INSPECTION EQUIPMENT. NOTE: A/O??????WAS OVERDUE. SUBMITTER STATED SHOULD HAVE BEEN COMPLETED NO LONGER THAN SEPT, 1999. Jun 16, 2000 · N87K · Beech S35 · Propeller Blade SectionSDR 99ZZZX3194Blade · crackedFOUND CRACK RUNNING AROUND THE CIRCUMFERENCE OF THE BLADE SHANK BETWEEN THE TWO SHOULDERS. THE PROPELLER WAS UNDERGOING THE INSPECTION FOR AD 97-18-02.Feb 12, 1999 · N5831S · Beech S35 · Propeller Blade SectionSDR 98ZZZX2000Nut · failedAT ANNUAL INSPECTION WHILE INSPECTING THE AFT EMPENNAGE AREA, FOUND 6 OF THE 16 STABILATOR SPAR ATTACHMENT NUTS CRACKED. UPON REMOVING THE NUTS FOR REPLACEMENT, ONE OF CRACKED NUTS BROKE INTO SEVERAL PIECES. THERE ARE 8 NUTS ATTACHING EACH STABILATOR SPAR TOMay 4, 1998 · N8693Q · Beech S35 · Horizontal Stabilizer, Attach FittingsSDR 98ZZZX2235Skin · wrong partBEECHCRAFT SHOP MANUAL P/N 35-590096B REVISED 3-22-96, PAGES 2-6, FIG 2-5, INDEX 12. GAUGE .032 INCH CALLS FOR A 2024-0 SKIN-FUSELAGE WHICH INDICATES A DEAD SOFT SKIN. AFTER A CONVERSATION WITH RAYTHEON BEECH TECH REP, HE REVIEWED THE PRINTS AND INDICATED THMar 24, 1998 · N64CG · Beech S35 · Fuselage Main, Plate/SkinSDR 99ZZZX654Clamp · corrodedAIRCRAFT WAS MODIFIED UNDER STC SA2556 TO INSTALL TSIO-520 ENGINE. EXHAUST CLAMP TO LEFT TURBOCHARGER FAILED DUE TO CORROSION ALLOWING HOT EXHAUST GASSES TO MELT ALL ELECTRICAL WIRING AND VOLTAGE REGULATOR ON LEFT SIDE OF FIREWALL. THIS BYPASSED MASTER SWITCJan 13, 1998 · N7WA · Beech S35 · Exhaust TurbochargerSDR 98ZZZX511Hub · misdrilledOIL FILLER HOLE ON SIDE OF HUB DRILLED IN WRONG LOCATION. REF: MCCAULEY SL1989-5 AND SL1995-14A.Jan 12, 1998 · N8835M · Beech S35 · Propeller Hub SectionSDR 97ZZZX2118Rod End · wornWHILE PERFORMING AD 97-06-11, ALL 4 RUDDERVATOR ROD ENDS WERE FOUND WORN AND ONE WITH CORROSION. SB NR 2668 PERTAINS TO THIS SUBJECT.Apr 28, 1997 · N8604Q · Beech S35 · Elevator Control SystemSDR 97ZZZX1920Crankcase · crackedDURING ANNUAL INSPECTION, CRANKCASE AT NR 2 CYLINDER BASE STUD FOUND CRACKED FOUR INCHES LONG. THIS IS A LIGHT CASE ENGINE.Apr 15, 1997 · N8604Q · Beech S35 · Reciprocating Engine Power SectionSDR 96ZZZX5214Bladder · bafffle crumbleFUEL BLADDER INNER BAFFLING DISENTEGRATING INTO SAND-SIZE PARTICLES. PARTICLES FOUND AT SUMP AND STRAINER. COULD CAUSE FUEL STARVATION. DETERMINED TO BE INNER BAFFLE FOAM.Sep 6, 1996 · N3MG · Beech S35 · Fuel StorageSDR 96ZZZX4952Horn · brokenSHORTLY AFTER TAKEOFF, PLANE STARTED TO SHUDDER VIOLENTLY. PILOT THOUGHT PROPELLER TIP BROKE. AN IMMEDIATE EMRGENCY LANDING WAS MADE ON AN INTERSECTING RUNWAY. UPON INSPECTION, LEFT TRIM TAB HORN FOUND BROKEN AND TRIM WIRE LOOSE PART BROKE MIDWAY BETWEEN RVAug 10, 1996 · N6851Q · Beech S35 · Rudder, Tab StructureSDR 96ZZZX4154Flap Follow-Up · seizedFLAPS FAILED TO EXTEND. FOUND AUTOPILOT FOLLOW-UP IN LEFT WING SEIZED IN THE AFT POSITION ALLOWING THE ACTUATING WIRE TO MOVE OVER FLAP MICROSWITCH AND NOT ALLOWING FLAP TO EXTEND. LUBRICATED SHAFT OF FOLLOW-UP AND SYSTEM OPERATES CORRECTLY. NEW SERVO FOLLOJul 10, 1996 · N5826K · Beech S35 · Trailing Edge Flap Control SystemSDR 96ZZZX3801Pump · port pluggedFUEL PUMP REPLACED TO C/W BEECH SB N2526, REV II. WORKING WHEN REMOVED. FOUND OVERFLOW/RELIEF PORT PLUGGED WITH MATERIAL THAT APPEARS TO BE RUST.Apr 29, 1996 · N8992M · Beech S35 · Fuel Boost PumpSDR 95ZZZX5211Window · sealed shutANNUAL INSPECTION FOUND BOTH LT AND RT EMERGENCY ESCAPE WINDOWS HAD BEEN SILICONED SHUT BY PERSONS UNKNOWN, APPARENTLY IN AN ATTEMPT TO SEAL THE WINDOW AGAINST THE WEATHER. THE SILICONE WAS SO HEAVILY APPLIED THAT ONLY BY PRYING FROM THE OUTSIDE WITH A GASKETSep 8, 1995 · Beech S35 · Emergency ExitsSDR 95ZZZX3734Blade · crackedDEFECT IS IN THE DOUBLE SHOULDER OF THE 3 BLADES WHERE IT IS RETAINED BY THE CLAMP.Jul 21, 1995 · N333SM · Beech S35 · Propeller Blade SectionSDR 95ZZZX3733Blade · crackedDEFECT IS IN THE DOUBLE SHOULDER OF THE 3 BLADES WHERE IT IS RETAINED BY THE CLAMP.Jul 21, 1995 · N333SM · Beech S35 · Propeller Blade SectionSDR 95ZZZX3732Blade · crackedDEFECT IS IN THE DOUBLE SHOULDER OF THE 3 BLADES WHERE IT IS RETAINED BY THE CLAMP.Jul 21, 1995 · N333SM · Beech S35 · Propeller Blade SectionSDR 95ZZZX3620Uplock Cable · brokenFOUND LANDING GEAR UPLOCK CABLE BROKEN. SUBMITTER STATED TENSION MUST BE CHECKED EACH ANNUAL WITH LANDING GEAR IN UP AND LOCKED POSITION.Jul 1, 1995 · N6810Q · Beech S35 · Landing Gear Retraction/Extension System
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