Piper PA-24-260

Service difficulty reports · 54

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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 = 'PA24260'
  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 2026FA0000203Control Cable · brokenAIRCRAFT ABORTED TAKEOFF DUE TO LOW POWER. UPON INSPECTION FOUND PROPELLOR GOVERNOR CABLE BROKEN. MAINTENANCE REPLACED THE PROP CONTROL CABLE AND PROP CONTROL CABLE ROD END.Mar 20, 2026 · N9055P · Piper PA24260 · Propeller Controlling SystemSDR 2023FA0000413Stabilator · unknownON TUESDAY AUGUST 8TH AT APPROXIMATELY 2:45 PST N503JA TOOK OFF FROM KFUL ON RUNWAY 24. APPROX. 8 MIN INTO THE FLIGHT THE AIRCRAFT WAS LEVELED OFF AND TRAVELING AT APPROX. 150KTS. THE PILOT REPORTED THE AT THAT APPROX. 8 MIN MARK AFTER TAKING OFF THE AIRCRAFT Aug 14, 2023 · N503JA · Piper PA24260 · Elevator Control SystemSDR 2021FA0000027Cable Assy · frozen01/11/2021 AT 0800 THE OPERATOR DEPARTED BRANDYWINE AIRPORT (OQN) ON A VFR FLIGHT. AFTER TAKEOFF WHEN OPERATOR ATTEMPTED TO RETRACT THE LANDING GEAR, IT TRAVELED ABOUT 3/4 THE WAY UP AND THE LANDING GEAR MOTOR CIRCUIT BREAKER POPPED. PILOT IN COMMAND (PIC) LJan 29, 2021 · N9144P · Piper PA24260 · Main Landing GearSDR CA140715013Fuel Line · wrong part(CAN) AD 2011-26-04 FUEL INJECTION LINES, AND CLAMPING VISUALLY INSPECTED I.A.W. TEXTRON LYCOMING MOB NO. 342G DATED JULY 16, 2013 AS REQUIRED. FOUND FUEL STAINING FORWARD OF #6 FUEL INJECTION NOZZLE ON THE COOLING FINS OF CYLINDER NR 4. DETAIL VISUAL OF NR 6 Jul 13, 2014 · Piper PA24260 · Fuel Controlling SystemSDR 2014FA0000257Pump · pressure lossPILOT REPORTED DURING FLIGHT, THE ACFT ENGINE SHUTDOWN DUE TO FUEL STARVATION. SWITCHED TO ALTERNATE TANKS BUT COULD NOT GET THE ENGINE TO RESTART. DECLARED AN EMERGENCY AND SAFELY LANDED WITH NO ISSUES. ATTEMPTED A RESTART AND FOUND THAT THE ELECTRIC BOOMar 1, 2014 · N9081P · Piper PA24260 · Fuel Boost PumpSDR 2012FA0000353Motor · burned outELECTRIC FUEL PUMP FAILED AND CAUSED SMOKE AND BURNING SMELL IN AIRCRAFT. FUEL PUMP IS LOCATED BELOW CO-PILOT FEET FLOOR PANELS. PUMP HAD 27.2 TOTAL AIRFRAME HOURS OF OPERATION SINCE O/H. CURRENT FLIGHT WAS PATTERN WORK, WHERE PUMP WAS LEFT ON FOR ABOUT 30 Jun 6, 2012 · N9360P · Piper PA24260 · Fuel Boost PumpSDR CA120420009Stringer · cracked(CAN) DURING INSPECTION FOUND FUSELAGE RT STR 23743-05 AND LT FUSELAGE STR 23743-04 CRACKED AT THE FORWARD ENDS BELOW THE FORWARD WING ATTACH FITTINGS.Apr 20, 2012 · Piper PA24260 · Fuselage Main, Longeron/StringerSDR 2010FA0000934Spar · crackedRUDDER SPAR CRACKED AT UPPER HINGE FITTING.Sep 1, 2010 · N123PC · Piper PA24260 · Rudder, Spar/RibSDR 2010FA0000933Spar · crackedRUDDER SPAR CRACKED AT UPPER HINGE FITTING.Sep 1, 2010 · N9353P · Piper PA24260 · Rudder, Spar/RibSDR CA091119006Housing · broken(CAN) ENG WAS RECEIVED FOR PROP STRIKE INSP. MAG WAS INSPECTED AND 4 OUT OF THE 5 HSG SCREWS WERE MISSING. MAG WAS DISASSEMBLED AND ONE OF 3 ALIGNMENT TABS IN THE DISTRIBUTOR HSG WAS BROKEN OFF. THIS CAUSED HSGS TO SHUFFLE AND LOOSEN SCREWS. SPOT WHERE THENov 19, 2009 · Piper PA24260 · Magneto/DistributorSDR 2009FA0000871Hinge · crackedTOP RUDDER HINGE CASTING CRACK AT ROLLER BRG LOCATION. (K)Oct 22, 2009 · N9338P · Piper PA24260 · Rudder StructureSDR 2009FA0000763Bulkhead · crackedFOUND AFT VERTICAL FIN SPAR TO BULKHEAD BRACKET CRACKED. STA 258.75. THIS PROBLEM HAS BEEN ADDRESSED BY AD 74-16-08 AND MFG SL 679 ON OTHER SERIES ACFT BUT NOT ON THIS ONE. (K)Aug 17, 2009 · N9364P · Piper PA24260 · Fuselage Main, BulkheadSDR 2008FA0000309Torque Tube · brokenDURING MAINTENANCE RUNUP AND TAXI CHECK AFTER MAINTENANCE THE LEFT RUDDER TORQUE TUBE BROKE OFF. IT APPEARED TO HAVE BEEN CRACKED FOR SOME TIME PRIOR TO FAILING DURING TAXI. IT IS SUGGESTED THAT THE AREA BE CLEANED AND INSPECTED WITH A 10X MAGNIFYING GLASS. AMay 7, 2008 · N9506P · Piper PA24260 · Rudder Control SystemSDR 2005FA0001223Placard · misinstalledWHEN DOING OPERATIONAL CHECK AFTER INSTALLATION OF SVS VI UPGRADE KIT ON SVA IA SYSTEM, (AD 2005-11-05). THE ON/OFF PLACARD ON ON/OFF LEVER WAS CONFUSING. WHEN LEVER VALVE WAS ON OR OPEN, IT LOOKED AS IF IT WERE (OFF) OR CLOSED ON THE PLACARD. (K)Aug 5, 2005 · N8955P · Piper PA24260 · Placards and MarkingsSDR 2005FA0001247Filter · contaminatedTHIS STATION RECEIVED REQUEST FROM REGULAR CUSTOMER, THAT WAS FERRYING AIRCRAFT. AIRCRAFT ENGINE FAILED TO MAKE FULL POWER THEN QUIT ON GROUND. CREW WAS SENT TO REMOTE AIRFIELD TO TROUBLESHOOT. AFTER EXTENSIVE TROUBLESHOOTING, FOUND FUEL INJECTORS CLOGGED BJul 29, 2005 · N8788P · Piper PA24260 · Aircraft Fuel Filter/StrainerSDR NEFSDO03Roll Pin · missingAPPROXIMATELY 2149 Z PILOT ADVISED HE BELIEVED THE AIRCRAFT LT MAIN GEAR COLLAPSED. THE SAFETY DEVICE (ROLL PIN) WAS NOT INSTALLED. THIS ALLOWED THE NUT TO ROTATE ALLOWING THE STUD TO BACK OUT OF THE CASTING. THIS CAUSED THE LT MAIN LANDING GEAR TO COLLAPSE. Jul 11, 2005 · N9167P · Piper PA24260 · Main Landing GearSDR 2005FA0000618Seal · failedUPON TRYING TO INSTALL THE SOLID OIL SEAL OVER THE CRANKSHAFT FLANGE, THE SEAL FAILED AND TOTALLY SEPERATED IN A STRAIGHT LINE 90 DEGREES TO THE FACE OF THE SEAL. VERY LITTLE FORCE WAS BEING APPLIED TO THE INSTALLING TOOL WHEN THE SEAL FAILED. THIS WAS SECONApr 25, 2005 · N9241P · Piper PA24260 · Reciprocating Engine Oil SystemSDR 2005FA0000172Strut · corrodedPERFORMING ROUTINE SERVICE, THE RT MLG STRUT WAS FOUND LEAKING 5606 HYDRAULIC FLUID. DISCOVERED THAT THE STEEL (4130) ATTACHMENT FOR THE GEAR DOOR HAD CREATED DISSIMILAR METAL CORROSION AND CREATED A PIN HOLE LEAK. THIS PART NEEDS TO BE REMOVED AND CHECKED TOct 26, 2004 · N9014P · Piper PA24260 · Main Landing Gear Strut/Axle/TruckSDR 2005FA0001126Rib · crackedCRACK WAS FOUND IN THE RIB THAT ATTACHES THE RUDDER COUNTER WEIGHTS. THIS HAS BEEN NOTICED IN THE PAST, THE FIX IS TO REPLACE RIB. PARTS NO LONGER AVAILABLE. NOTICED THIS ON AIRFRAMES WITH MORE THAN 4000 HOURS. (K)Oct 15, 2004 · N9180P · Piper PA24260 · Rudder, Spar/RibSDR 2005FA0000375Spar · crackedDURING SERVICE OF THE AIRCRAFT THE RUDDER WAS REMOVED. NOTHING WAS FOUND ABNORMAL. REMOVAL OF THE UPPER RUDDER HINGE (PN 2018300). CRACKS WERE FOUND AT THE HINGE ATTACH POINT OF THE RUDDER SPAR (2072910). (K)Oct 15, 2004 · N9180P · Piper PA24260 · Rudder, Spar/RibSDR 2005FA0000374Spar · crackedDURING SERVICE OF AIRCRAFT THE RUDDER WAS REMOVED. NOTHING WAS FOUND ABNORMAL. REMOVAL OF THE UPPER RUDDER HINGE (PN 2018300. CRACKS WERE FOUND AT THE HINGE ATTACH POINT OF THE RUDDER SPAR (2072910). (WP07200505589) (K)Oct 15, 2004 · N8544P · Piper PA24260 · Rudder, Spar/RibSDR 2005FA0000373Rib · corrodedDURING AN ANNUAL INSPECTION, MORE THAN NORMAL SURFACE CORROSION WAS FOUND ON THE RUDDER TAIL POST. UPON DISASSEMBLY OF THE RUDDER, DISSIMILAR METAL CORROSION WAS PRESENT WHERE THE STEEL STIFFENER ATTACHES TO THE LOWER RIB (PN 2072904). (WP07200505592) (K)Oct 15, 2004 · N8544P · Piper PA24260 · Rudder, Spar/RibSDR 2004FA0000711Antenna · failedDURING AN ANNUAL INSPECTION, THE ELT ANTENNA ON AIRCRAFT WAS DISCOVERED TO HAVE FAILED. THE ANTENNA FAILED AT THE BULKHEAD FITTING. IT APPEARS TO BE SIMPLY GLUED INTO THE FITTING. THIS ANTENNA P/N 450017 HAS BEEN RECENTLY UP GRADED INDICATING THE MANUFACTURJul 21, 2004 · N8900P · Piper PA24260 · Emergency Locator BeaconSDR CA040426008Release Pin · worn(CAN) ON ANNUAL INSPECTION, WAS UNABLE TO RELEASE DOOR FOR EMERGENCY GEAR EXTENSION. PIN WAS FOUND WORN, AND RETURNED TO MFG FOR REPAIR. PIN REINSTALLED AND PROBLEM REPEATED, INVESTIGATION REVEALED NOSE DOOR SYSTEM WAS RIGGED TOO TIGHT. REPEATED CALLS TO MANUFApr 26, 2004 · Piper PA24260 · Landing Gear Door Retract SectionSDR 2004FA0000017Bracket · crackedDURING RUDDER REMOVAL FOR REQUIRED MAINTENANCE, A CRACK WAS FOUND IN MIDDLE RUDDER HINGE BRACKET MOUNTED ON THE VERTICAL FIN. THE CRACK IS AT THE HINGE BEARING HOLE. DUE TO THE LOCATION, THIS CRACK WOULD NOT HAVE BEEN VISIBLE WITHOUT REMOVING THE RUDDER FIRSDec 19, 2003 · N801PC · Piper PA24260 · Vertical StabilizerSDR 2004FA0000016Bellcrank · crackedDURING ANNUAL INSPECTION, A CRACK WAS FOUND IN THE BELLCRANK BOLT HOLE. ON CLOSER INSPECTION IT WAS FOUND THAT ALL FOUR BOLT HOLES HAD CRACKS IN VARIOUS STAGES OF PROGRESSION. THE CRACKS BEGIN AT THE END OF THE PART AND PROCEED TOWARDS THE BOLT HOLE, ONLY ONDec 19, 2003 · N801PC · Piper PA24260 · Rudder ActuatorSDR 2004FA0000623Bolt · corrodedDURING ANNUAL INSPECTION THE STABILATOR WAS REMOVED FOR FURTHER INSPECTION. THIS IS DUE TO PREVIOUS PROBLEMS ON OTHER PA24 AND PA30/39 AIRCRAFT WITH STABILATOR TORQUE TUBE AND ATTACHMENT BOLTS WITH EXCESSIVE CORROSION. BOTH BOLTS AN175C33A THAT ATTACHES THE Oct 25, 2003 · N8843P · Piper PA24260 · FastenersSDR 2004FA0000617Bolt · corrodedDURING ANNUAL INSPECTION THE STABILATOR WAS REMOVED FOR FURTHER INSPECTION. THIS IS DUE TO PREVIOUS PROBLEMS ON OTHER PA24 AND PA30/39 AIRCRAFT WITH STABILATOR TORQUE TUBE AND ATTACHMENT BOLTS WITH EXCESSIVE CORROSION. BOTH BOLTS AN175C33A THAT ATTACHES THE Sep 22, 2003 · N8921P · Piper PA24260 · FastenersSDR 2004FA0000612Bolt · corrodedDURING ANNUAL INSPECTION THE STABILATOR WAS REMOVED FOR FURTHER INSPECTION. THIS IS DUE TO PREVIOUS PROBLEMS ON OTHER PA24 AND PA30/39 AIRCRAFT WITH STABILATOR TORQUE TUBE AND ATTACHMENT BOLTS WITH EXCESSIVE CORROSION. BOTH BOLTS AN175C33A THAT ATTACHES THE May 28, 2003 · N8660P · Piper PA24260 · FastenersSDR 2004FA0000620Bolt · corrodedDURING ANNUAL INSPECTION THE STABILATOR WAS REMOVED FOR FURTHER INSPECTION. THIS IS DUE TO PREVIOUS PROBLEMS ON OTHER PA24 AND PA30/39 AIRCRAFT WITH STABILATOR TORQUE TUBE AND ATTACHMENT BOLTS WITH EXCESSIVE CORROSION. BOTH BOLTS AN175C33A THAT ATTACHES THE Oct 10, 2002 · N9073P · Piper PA24260 · FastenersSDR AUS20020745Muffler · cracked(AUS) LH MUFFLER OUTLET PIPE CRACKED AT REAR SUPPORT CLAMP.Jul 25, 2002 · Piper PA24260 · Engine Noise SuppressorSDR 2004FA0000622Bolt · corrodedDURING ANNUAL INSPECTION THE STABILATOR WAS REMOVED FOR FURTHER INSPECTION. THIS IS DUE TO PREVIOUS PROBLEMS ON OTHER PA24 AND PA30/39 AIRCRAFT WITH STABILATOR TORQUE TUBE AND ATTACHMENT BOLTS WITH EXCESSIVE CORROSION. BOTH BOLTS AN175C33A THAT ATTACHES THE Jul 7, 2002 · N8700P · Piper PA24260 · FastenersSDR 20001129SH018Strut · crackedINSPECTION OF LEFT MAIN LANDING GEAR FOUND STRUT JAMMED. HOUSING CRACKED AND LEAKING FLUID. AIRCRAFT TT, 6,763.2 HOURS. (X)Nov 14, 2000 · N4960 · Piper PA24260 · Main Landing Gear Strut/Axle/TruckSDR 20001103SH006Solenoid · faultyLANDING GEAR INOPERABLE. TROUBLESHOT SYSTEM AND FOUND GEAR SOLENOID TO HAVE INTERNAL GROUND. REPLACED UNIT. P/N PIPER 487-152, MFG P/N W-R/RBM, 70-112222-3 COIL 12V DC INT. PERFORMED GEAR SWING (12 TIMES) AND SYSTEM CHECKED GOOD AT THIS TIME, 10-19-00, HOBOct 17, 2000 · N8766P · Piper PA24260 · Landing Gear SelectorSDR 20001127SH018Engine · failedENGINE FAILED CATASTROPHICALLY IN-FLIGHT AND SUBSEQUENTLY AIRCRAFT LANDED GEAR UP NEXT TO CANAL. INITIAL INSPECTION INDICATED ROD BEARING OR ROD CAP FAILURES. MANUFACTURER''S INSPECTION RESULTS ARE PENDING. (X)Oct 14, 2000 · N9005P · Piper PA24260 · Engine (Reciprocating)SDR 20000724SH016Handle · wornWHILE PERFORMING EMERG LANDING GEAR EXTENSION CHK DURING ANNUAL INSP, FOUND EMERG RELEASE MECH WOULD NOT DISENGAGE L/G FROM TRANSMISSION ASSY WHEN FLOORBOARDS AND RUGS WERE INSTALLED. THIS PREVENTED LANDING GEAR FROM BEING EXTENDED USING MANUAL/EMERG MODE. Jun 5, 2000 · N9070P · Piper PA24260 · Landing Gear Retraction/Extension SystemSDR 20000517SH018Shaft · failedRELEVANT INDICATION ON CONTROL SHAFT AT THE SPEED ADJUSTMENT SHAFT. (X)Apr 24, 2000 · N9051P · Piper PA24260 · Propeller GovernorSDR 99ZZZX3848Fitting · damagedDURING GEAR INSPECTION, EXCESSIVE MOVEMENT WAS NOTICED. REMOVED THE SIDE BRACE STUD ASSEMBLY AND DISCOVERED THE SIDE BRACE STUD HAD BEEN FORCED IN THE SIDE BRACE ASSY. THE SIDE BRACE ASSY WAS SEVERELY FRITTERED AWAY.Sep 1, 1999 · N260NC · Piper PA24260 · Landing Gear Retraction/Extension SystemSDR 99ZZZX3095Hose · mismanufacturedFULE HOSE CHANGED 3-14-97, CURE DATE/LOT NR 290 1 Q96. HOSE MANUFACTURE DATE 3-13-97. HOSE GOES FROM FUEL PUMP TO FUEL CONTROL. HOSE REMOVED TO SHORTEN LENGTH. HOSE MANDREL WOULD NOT FIT INSIDE HOSE DUE TO COLLAPSED INNER WALL OF HOSE. TT ON HOSE, 312 HOURSAug 9, 1999 · N9306P · Piper PA24260 · Aircraft Fuel Distribution SystemSDR 99ZZZX2131Angle · looseWHILE PERFORMING RECURRENT INSPECTION FOR AD 94-13-10, A CREAKING NOISE WAS HEARD COMING FROM THE ANGLES SUPPORTING THE STABILATOR TORQUE TUBE BEARING SUPPORT FITTINGS. THE SOURCE OF THE NOISE WAS NOT SPECIFIED IN THE AD. LOOSE RIVETS WERE DISCOVERED AFTER May 6, 1999 · N9219P · Piper PA24260 · Fuselage Miscellaneous StructureSDR 98ZZZX4829Flyweight · failedFLYWEIGHT BASE SEPARATED INTO 2 PIECES CAUSING LOSS OF CONTROL OF GOVERNOR AND PROPELLER.Nov 20, 1998 · N79RG · Piper PA24260 · Propeller GovernorSDR 97ZZZX3794Seal · leakSERVO WAS OVERHAULED ON APPROXIMATELY 1-28-97. COMPONENT OPERATED WITHOUT PROBLEM UNTIL 5-11-97 WHEN IT HAD ACCUMULATED 30 HOURS IN SERVICE. ON 5-11-97, EXPERIENCED IN-FLIGHT ENGINE ROUGHNESS WHICH ABATED SOMEWHAT WITH EXCESSIVELY LEANING OF THE MIXTURE. UPMay 26, 1997 · N991K · Piper PA24260 · Fuel Control/Reciprocating EnginesSDR 97ZZZX2662Servo · seal leakENGINE ROUGHNESS DUE TO EXCESS RIGH MIXTURE. FOUND RECENT OVERHAULED SERVO TO BE AT FAULT DUE TO SEAL LEAKING FUEL INTO AIR CHAMBER. SERVO TSO SERVICE 30 HOURS. SEAL, S/N 2539561.May 26, 1997 · N991K · Piper PA24260 · Fuel Control/Reciprocating EnginesSDR 97ZZZX885Camshaft · brokenENGINE OVERSPED IN CRUISE FLIGHT AT 6,500 FEET. MAXIMUM OVERSPEED WITNESSED WAS 3,500 RPM. AIRCRAFT LANDED AT FIRST SUITABLE AIRFIELD. ON INSPECTION, CAMSHAFT WAS FOUND BROKEN IN TWO BETWEEN FORWARD BEARING AND GOVERNOR DRIVE GEAR CAUSING PROPELLER TO DECREFeb 2, 1997 · N1424N · Piper PA24260 · Reciprocating Engine Power SectionSDR 96ZZZX5562Yoke Mount · fouls yokeYOKE MOUNT CLAMP INSTALLED BY OWNER GOT FOULED IN THE POWER WIRE TO PORTABLE GPS. RESTRICTED YOKE MOVEMENT. PILOT MAKE HARD LANDING. WIRE FINALLY BROKE IN TWO ALLOWING A/C TO BE 'FLARED'. PILOTS SHOULD BE MADE AWARE TO CHECK YOKE MOVEMENT ON PRE-FLIGHT. YOct 1, 1996 · N9137P · Piper PA24260 · Global Positioning SystemSDR 96ZZZX2866Drain Valve · faultyTHE FUEL DRAIN VALVE WOULD NOT OPERATE, THE PROBLEM WAS THE VALVE ITSELF, BUT WAS NOT EVIDENT UNTIL THE OVERBOARD HOSE BECAME STIFF FROM AGE AND TEMPERATURE. WHILE INVESTIGATING, FOUND IF THE VALVE WAS OPENED BY A GREAT DEAL OF FORCE, THE VALVE COULD STICK OPMay 15, 1996 · N8632P · Piper PA24260 · Fuel StorageSDR 96ZZZX2039Ball Joint · crackedCOMPLAINTS OF STIFF THROTTLE OPERATON LED TO LUBING THROTTLE CABLE, HOWEVER, AFTER SHORT TIME, CABLE BECAME STIFF AGAIN. WHILE REPLACING CABLE, DISCOVERED THE BALL JOINT WHICH CONNECTS THE CABLE TO THROTTLE METERING ARM BENT AND CRACKED APPROXIMATELY TWO-THIRMar 25, 1996 · N8967P · Piper PA24260 · Power LeverSDR 96ZZZX785Switch · failedPILOT REPORTED SELECTING GEAR UP AND HAVING GEAR SOLENOID AND LIGHTS' CIRCUIT BREAKER TRIP. AIRCRAFT HAS A WHOLLY COWL CONVERSION FROM LOPRESTI. PILOT EXPERIENCED REDUCED RUDDER CONTROL, BUT WAS ABLE TO MAKE AN UNEVENTFUL LANDING. AIRCRAFT WAS FOUND TO HAVEJan 25, 1996 · N8665P · Piper PA24260 · Landing Gear Door Retract SectionSDR 96ZZZX710Cell · fuel weepPILOT REPORTED FUEL SMELL. INSPECTION FOUND RT INBOARD TANK WEEPING THROUGH FABRIC OF FUEL CELL ENOUGH TO GENERATE SMELL, BUT NOT ENOUGH TO LEAK OR CAUSE EXCESSIVE FUEL STAINS.Jan 16, 1996 · N8632P · Piper PA24260 · Fuel StorageSDR 95ZZZX6931Trunnion · crackedFOUND SECOND TRUNNION THAT HAS BEEN CRACKED. THIS ONE WAS THE RIGHT MLG. OTHER CRACK ON MODEL PA30, LEFT GEAR. REPLACED WITH 27053-001, WITH SPRING CLAMP DIFFERENT.Nov 22, 1995 · N8803P · Piper PA24260 · Main Landing Gear Strut/Axle/Truck
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