JASC 6113
Service difficulty reports · 364
Reports filed under 6113 · Propeller Spinner 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 = '6113' 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 = '6113' 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 RTE2007F00000Bulkhead · crackedDURING ROUTINE PHASE INSPECTION, FOUND FWD PROP BULKHEAD ASSY TO BE CRACKED IN SEVERAL PLACES, ALL NEAR THE BOLT HOLES AND NEARBY RADIUS. HAVE FOUND SEVERAL IN THE SAME CONDITION ON THIS AND OTHER AC. SUSPECT EITHER IMPROPER HEAT TREATING DURING MFG AND OR ISDR CA061017007Bulkhead · cracked(CAN) ON PILOT WALK AROUND THE SPINNER ASSY WAS NOTED TO BE LOOSE. UPON INSPECTION IT WAS OBSERVED THAT THE FWD SPINNER BULKHEAD WAS CRACKED. THIS WAS MOST LIKELY CAUSED BY PILOTS PUSHING ON THE SPINNER WHEN GROUND HANDLING THE AIRCRAFT. (TC NR 20061017007)SDR CA061018008Spinner · dented(CAN) GOOSE HIT THE OB SIDE OF THE LT PROP SPINNER. DAMAGE WAS MINIMAL TO THE SPINNER WHERE THE BLADE CUT OUT IS. THERE WAS ALSO MINIMAL DAMAGE TO THE CHIN COWL PN 27-63026-053. DAMAGE ON BOTH UNITS WERE COVERED BY THE SRM LIMITS OF .3750 DEGREES 4. (TC NR SDR FAA63837Spinner · crackedRT PROPELLER SPINNER CRACKED. CRACKS ORIGINATE FROM 1ST SCREW HOLE ADJACENT TO BLADE OPENING. THIS IS THE 2RD OCCURANCE OF THIS DEFECT. PROBABLE CAUSE UNKNOWN.SDR FAA1012002Balance Weight · tornPROPELLER WAS BALANCED IN PLACE. 10 FLIGHT HOURS LATER, IN CRUISE OVER WYOMING EN ROUTE TO OSHKOSH, SIGNIFICANT VIBRATION OCCURRED, CAUSING DIVERSION TO THE NEAREST AIRPORT. UPON LANDING, BYSTANDERS RAN TOWARD THE AIRPLANE TO EFFECT RESCUE, ASSUMING THE AIRPSDR CA060913001Bulkhead · cracked(CAN) DURING CHANGEOVER FROM FLOATS TO WHEELS, AND DURING THE CHANGE FROM SEAPLANE PROP TO WHEELPLANE PROP , CLOSER INSPECTION OF THE FORWARD PROP SPINNER BULKHEAD REVEALED NUMEROUS CRACKS. THESE CRACKS WERE RADIATING FROM THE PROP ATTACHMENT BOLT HOLES, TO THSDR CA060724007Bulkhead · cracked(CAN) THIS BULKHEAD HAS CRACKS DIRECTLY ABOVE THE BOLT HOLES APPROXIMATELY ONE INCH LONG RADIALY ALONG THE INNER BEND RADIUS ABOVE THE BOLT HOLE BUT NOT INTERSECTING THE BOLT HOLE. (TC NR 20060724007)SDR CA060724006Bulkhead · cracked(CAN) THIS BULKHEAD HAS CRACKS DIRECTLY ABOVE THE BOLT HOLES APPROXIMATELY ONE INCH LONG RADIALY ALONG THE INNER BEND RADIUS ABOVE THE BOLT HOLE BUT NOT INTERSECTING THE BOLT HOLE. (TC NR 20060724006)SDR CA060714007Support · cracked(CAN) DURING 100 HR INSP REMOVED SPINNER AND FOUND THE INNER SUPPORT CRACKED. (TC NR 20060714007)SDR CA060711008Bulkhead · cracked(CAN) THE SPINNER FORWARD BULKHEAD WAS INSTALLED NEW ONE YEAR EARLIER, WITH THE NEW HEAVIER MATERIAL SPINNER IAW SNL03-9 (ALTERNATE PROPELLER SPINNER INSTALATION) THE FWD BULKHEAD HAS CRACKS OF APPROXIMATLY 1.5 INCHES EACH COMING ACROSS EACH PROP BOLT HOLE ATSDR 2006FA0000668Spinner · brokenRT PROPELLER WAS OVERHAULED AND INSTALLED IN THE RT POSITION. ENGINE RAN TO LEAK CHECK AND FUNCTIONAL CHECK PROPELLER SYSTEM ON THE RT SIDE AND TO FULL POWER FOR APPROXIMATELY 60 SECONDS. A SLIGHT CHANGE IN THE HARMONICS WAS NOTED BUT NOT A SIGNIFICANT CHANGESDR 2006FA0000592Bulkhead · crackedDURING A 100 HOUR INSPECTION FO THE PROPELLER IT WAS NOTICED THAT THE FORWARD SPINNER BULKHEAD HAD CRACKS AROUND ALL 6 BOLT HOLES. THE PROBABLE CAUSE IS DURING THE TORQUING PROCESS THE BULKHEAD IS BEING STRESSED AND BENT AS IT IS PULLED TIGHT TO THE PROP HUB.SDR TQ0A0004Bulkhead · crackedSPINNER BULKHEAD CRACKS AT REAR SECTION AND DELAMINATION OF EPOXY.SDR 2006FA0000551Bulkhead · crackedDURING AN ANNUAL INSPECTION OF THE PROPELLER IT WAS NOTICED THAT THERE WERE CRACKS AROUND 3 OF THE BOLT HOLES OF THE FORWARD SPINNER BULKHEAD. THE PROBLEM CAUSE IS THAT THE BULKHEAD IS BEING STRESSED AND BENT AS IT IS BEING TIGHTENED AGAINST THE PROPELLER HUBSDR 2006FA0000548Bulkhead · crackedDURING AN ANNUAL INSPECTION FO THE PROPELLER IT WAS NOTICED THAT THERE WERE CRACKS AROUND 3 OF THE BOLT HOLWS OD THE FORWARD SPINNER BULKHEAD. THE PROBABLE CAUSE IS THAT THE BULKHEAD IS BEING STRESSED AND BENT AS IT IS BEING TIGHTENED AGAINST THE PROPELLER HUSDR 2006FA0000550Bulkhead · crackedDURING 100 HRS INSPECTION, FOUND FORWARD SPINNER BULKHEAD CRACKED IN 2 PLACES AROUND PROPELLER BOLT HOLES. RECOMMENDATION: DIMPLING OF BOLT HOLES. (K)SDR 2006FA0000581Bulkhead · crackedDURING ROUTINE SCHEDULED PHASE INSPECTION. FOUND FORWARD PROP SPINNER BULKHEAD CRACKED RADIALLY OUTWARD FROM MOUNTING BOLT HOLES NEXT TO BEND RADIUS. PROPELLER MOUNTING BOLT BOLT TORQUE AND INDEXING FOUND CORRECT. SUSPECT EITHER IMPROPER HEAT TREAT DURING MSDR 2006FA0000462Bulkhead · crackedDURING ROUTINE PHASE INSPECTION FWD PROP BULKHEAD FOUND TO BE CRACKED NEAR SEVERAL MOUNTING BOLT HOLES. HAVE SEEN THIS SEVERAL TIMES BEFORE. SUSPECT DEFECT IN CURRENT MFG PROCESS. (K)SDR 2006FA0000360Spinner · crackedSPINNER HAS CRACKS IN 3 PLACES NEAR SCREW HOLES ADJACENT TO PROPELLER BLADES. (K)SDR CA060211001Plate · damaged(CAN) SHEARED RIVETS ON BACKPLATE FACE. (TC NR 20060211001)SDR 2006FA0000103Plate · failedSPINNER SUPPORT PLATES RECEIVED BROKEN WITH BOLTS STILL INSTALLED ON HUB, NO OTHER BROKEN PARTS OF THIS SUPPORT PLATE ASSY WERE FOUND ON THIS PROPELLER. (K)SDR RTE2006F00002Bulkhead · crackedDURING ROUTINE SCHEDULED INSPECTION. FOUND FWD PROP SPINNER BULKHEAD CRACKED NEAR THE BOLT HOLES. NO APPARENT REASON COULD BE DETERMINED. THE PROP BOLTS WERE CORRECTLY TORQUED. THE PROP WAS CORRECTLY CLOCKED. GROUND AND FLIGHT CHECKS SHOWED NO ABNORMAL VISDR RTE2006F00001Bulkhead · crackedDURING ROUTINE SCHEDULED INSPECTION, FOUND FWD PROP SPINNER BULKHEAD CRACKED NEAR THE BOLT HOLES. NO APPARENT REASON COULD BE DETERMINED. THE PROP BOLTS WERE CORRECTLY TORQUED. THE PROP WAS CORRECTLY CLOCKED. GROUND AND FLIGHT CHECKS SHOWED NO ABNORMAL VIBSDR RTE2006F00000Bulkhead · crackedDURING ROUTINE SCHEDULED INSPECTION. FOUND FWD PROP SPINNER BULKHEAD CRACKED NEAR THE BOLT HOLES. NO APPARENT REASON COULD BE DETERMINED, THE PROP BOLTS WERE CORRECTLY TORQUED. THE PROP WAS CORRECTLY CLOCKED. GROUND AND FLIGHT CHECKS SHOWED NO ABNORMAL VIBSDR 2006FA0000005Bulkhead · crackedDURING 100 HR INSPECTION, THE FORWARD SPINNER BULKHEAD WAS FOUND TO BE CRACKED AROUND 3 OF THE 6 BOLT HOLES. CAUSE OF THE PROBLEM IS THAT WHEN THE PROP MOUNTING BOLTS ARE TORQUED TO THE LIMITS GIVEN IN THE SRM THAT THE FWD BULKHEAD GETS PULLED DOWN SLIGHTLY ISDR TQ0A0003Bulkhead · crackedSPINNER BULKHEAD CRACKED.SDR TQ0A520050003Bulkhead · crackedSPINNER BULKHEAD CRACKED.SDR TQ0A0512001Bulkhead · crackedSPINNER BULKHEAD CRACKED.SDR CA051114002Plate · cracked(CAN) PART INSTALLED DEC 03, FOUND CRACKED AT REMOVAL FOR ENGINE CHANGE.SDR 2006FA0000565Bulkhead · crackedTHIS AC WAS NEW IN 3/3/2002. LT AND RT SPINNER BULKHEADS HAVE HAD TO BE REPLACED TWICE. FIRST SET OF SPINNER BULKHEADS WERE REPLACED 12/28/2004, WITH 563.3 HOURS ON THEM. PROPS WERE BALANCED TO PREVENT FURTHER PROBLEMS. SECOND SET OF SPINNER BULKHEADS WERESDR QXEA200501225Smoke · detectedPSC FLIGHT 2101 - NOTICED SMOKE COMING FROM BEHIND NR 1 PROP SPINNER. ALL ENGINE NR 1 INDICATIONS NORMAL. MAINTENANCE REMOVED COWL HORSECOLLAR AND LOWER COWL AND OPENED SIDE DOORS AND COMBUSTION SECTION DOORS. VISUALLY INSPECTED ALL FLUID LINES AND WIRING. SDR 2005FA0001199Bulkhead · crackedDURING ANNUAL/ 100 HOUR INSPECTION, FOUND SPINNER FWD BULKHEAD CRACKED AROUND 2 HOLES OF THE MOUNTING BOLTS. BOLTS PULLING EDGES OF BULKHEAD HOLES INTO CHAMFER OF THE PROP HOLES, CREATING STRESS AROUND THESE BULKHEAD HOLES LEADING TO CRACKS. (K)SDR X6PA200500006Bulkhead · crackedLT SPINNER BULKHEAD FOUND CRACKED, PIPER P/N 453-978. 1.5 IN CRACK EXTENDING FROM LAST SPINNER ATTACH FASTENER AT 10 O’CLOCK POSITION AND ANOTHER AT 2 O’CLOCK POSITION. BOTH CRACKS RUN INWARD TOWARD BULKHEAD/PROPELLER ATTACH POINT.SDR 2005FA0001006Bulkhead · crackedDURING 100 HR INSPECTION THE FORWARD SPINNER BULKHEAD WAS FOUND TO BE CRACKED AROUND ALL SIX (6) BOLT HOLES. THINK THAT THE CAUSE OF THE PROBLEM IS THAT WHEN THE PROP MOUNTING BOLTS ARE TORQUED TO THE LIMITS GIVEN IN THE SRM AND THAT THE FORWARD BULKHEAD GETSSDR 2005FA0001005Bulkhead · crackedDURING ANNUAL INSPECTION THE FORWARD SPINNER BULKHEAD WAS FOUND TO BE CRACKED AROUND 5 OF THE SIX BOLT HOLES. THINK THAT THE CAUSE OF THE PROBLEM IS THAT WHEN THE PROP MOUNTING BOLTS ARE TORQUED TO THE LIMITS GIVEN IN THE SRM THAT THE FORWARD BULKHEAD GET PULSDR B3OR20050505Spinner · crackedPROPELLER SPINNER WAS INSPECTED DURING A PRE-FLIGHT INSPECTION AND FOUND TO HAVE A CRACK. THE CRACK WAS FROM A SCREW HOLE AND EXTENDED TO BLADE CUT-OUT. THE SPINNER WAS REPLACED AND INSPECTED AFTER ITS FIRST FLIGHT, NO CRACKS WERE FOUND OR NOTED ON THE REPLACESDR 2005FA0000516Bulkhead · brokenPROP SPINNER AFT BULKHEAD BROKE AT ONE CORNER WITH NUTPLATE, FREEING ONE AFT EDGE OF THE SPINNER WHICH BENT OUTWARD UNDER CENTRIFUGAL FORCE. (K)SDR 2005FA0000552Spinner · cracked1 INCH CRACK EMANATING FROM PROPELLER CUTOUT PARALLEL WITH THE FWD BULKHEAD.SDR 2005FA0000551Spinner · cracked1.25 INCH CRACK EMANATING FROM PROPELLER BLADE CUTOUT RUNNING PARALLEL WITH THE FORWARD BULKHEAD.SDR 2005FA0000514Spinner · crackedDURING 100 HR INSPECTION THE FORWARD SPINNER BULKHEAD WAS FOUND TO BE CRACKED AROUND 5 OF THE 6 BOLT HOLES. CAUSE OF THE PROBLEM IS THAT WHEN THE PROP MOUNTING BOLTS ARE TORQUED TO THE LIMITS GIVEN IN THE SRM THAT THE FORWARD BULKHEAD GET PULLED DOWN SLIGHTLYSDR 2005FA0000147Bulkhead · crackedDURING ANNUAL INSPECTION, FOUND PROP SPINNER FWD BULKHEAD CRACKED AROUND 2 BOLT HOLES. RECOMMENDATION: MANUFACTURE BULKHEAD STRONGER OR THICKER. (K)SDR 2005FA0000146Bulkhead · crackedDURING 100 HOURS INSPECTION, FOUND PROP SPINNER FWD BULKHEAD CRACKED SEVERAL PLACES. LOWER PROP BOLTS TORQ SETTING OR MAKE BULKHEAD STRONGER.SDR 2005FA0000099Bulkhead · crackedDURING A 100 HR INSPECTION THE FORWARD SPINNER BULKHEAD WAS FOUND TO BE CRACKED AROUND 4 OF THE 6 BOLT HOLES. THINK THAT THE CAUSE OF THE PROBLEM IS THAT THE TORQUE OF THE PROP WAS RAISED AND THE NEW TORQUE IS NOT ENOUGH TO CAUSE THE BULKHEAD AROUND THE BOLT HSDR 2005FA0000145Bulkhead · crackedDURING ANNUAL INSPECTION FOUND FWD BULKHEAD OF THE SPINNER CRACKED 5 PLACES AROUND PROPELLER BOLT HOLES. RECOMMEND: BULKHEAD MATERIAL STRONGER OR THICKER. (K)SDR 2005FA0000032Bulkhead · crackedDURING 100 HRS INSPECTION, FOUND FWD BULKHEAD OF THE SPINNER CRACKED 4 PLACES AROUND PROPELLER BOLT HOLES. RECOMMENDATION: BULKHEAD MATERIAL STRONGER OR THICKER. (WP07200507539)SDR 2005FA0000237Bulkhead · crackedDURING 100 HOUR INSPECTION OF THE PROPELLER, CRACKS NOTED AROUND ALL BOLT HOLES OF THE FWD BULKHEAD. (K)SDR WIW2004F00002Bulkhead · crackedDURING A 100 HOUR INSPECTION THE AFT SPINNER BULKHEAD WAS FOUND TO BE CRACKED ON THE CORNER BY NUTPLATE.SDR 2004FA0000860Bulkhead · crackedPILOTS REPORTED AFT SPINNER BULKHEAD CRACKED AND SPINNER DOME BENT UP SLIGHTLY. UPON INSPECTION CORNER NUTPLATE FOUND COMPLETELY BROKEN OFF BULKHEAD.SDR 2004FA0000803Bulkhead · chafedUPON ANNUAL INSPECTION, FOUND AFT SPINNER BULKHEAD (PN TCB36323011) TO BE CHAFFING AGAINST PROPELLER BLADES. ONCE REMOVED, IT WAS ALSO EVIDENT THAT CORROSION HAD FORMED ON THE PROPELLER TUB. ALSO DISCOVERED WAS MATERIAL FROM THE BULKHEAD HAD TRANSFERRED TO TSDR WIW2004F00001Spinner · crackedDURING A 100 HOUR INSPECTION OF THE PROPELLER IT WAS NOTICED THAT THERE WERE CRACKS AROUND THREE OF THE BOLT HOLES OF THE FORWARD SPINNER BULKHEAD. THE PROBABLE CAUSE IS THAT DURING THE TORQUING PROCESS THE BULKHEAD IS BEING STRESSED AND BENT AS IT IS PULLED
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