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 2011FA0000164Spinner · looseSKULL CAP SPINNER BECAME LOOSE AND DEPARTED THE ACFT. EVIDENCE OF THE SPINNER ABRADING THE .041 SS SAFETY WIRE AT THE HEAD OF THE RETAINING BOLTS WAS EVIDENT. TORQUE ON THE WOODEN PROPELLER BOLTS HAD NOT BEEN CHECKED FOR PROPER TORQUE SINCE NEW. SINCE THE SSDR NSVA2010221Spinner · malfunctionedJUST AFTER LEVELING OFF IN CRUISE THE FLIGHT ATTENDANT REPORTED TO THE CAPTAIN THAT PASSENGER SEATED IN 5F INFORMED HER THAT SPARKS APPEARS TO BE COMING FROM THE NUMBER 2 ENGINE. SHE THEN VISUALLY VERIFIED THAT SPARKS ARE COMING FROM THE INTAKE AREA. THE CAPSDR 2010FA0001221Support · brokenWITH ENGINES RUNNING, PILOT NOTICED PIECES COMING OUT OF SPINNER. DURING INSP, DISCOVERED THAT THE LT SPINNER SUPPORT WAS COMING APART. AND SEVERAL PIECES FELL ON THE GROUND. THE SPINNER WAS NOT PROPERLY SHIMMED CAUSING THE SPINNER SUPPORT TO BE LOOSE AND VISDR 2010FA0001183Bulkhead · cracked(O2GS) CRACK WAS FOUND PROTRUDING FROM PROP ATTACH BOLT HOLES IN THE FWD SPINNER BULKHEAD.SDR 2010FA0001184Bulkhead · cracked(OG5S) CRACK WAS FOUND PROTRUDING FROM PROP ATTACH BOLT HOLES IN THE FWD SPINNER BULKHEAD.SDR CA100723002Spinner · crackedWHEN SPINNER REMOVED CRACKS FOUND MIGRATING FROM SPINNER BULKHEAD MOUNTING HOLES TO PROPELLER. CRACKS FOUND ON 6 OF THE BOLT HOLE ATTACH POINTS. CRACKS FOUND ON THE SPINNER FILLET PLATES. A NEW PART WAS PURCHASE AND INSTALLED.SDR 2010FA0000666Bulkhead · crackedFWD SPINNER BULKHEAD AND SPINNER DOME FOUND CRACKED. THIS WAS THE NEW DESIGN MFG FWD SPINNER BULKHEAD PN C2367 WITH THE MFG ADAPTER PLATE PN A1235 INSTALLED. SEVERAL CRACKS WERE FOUND AROUND THE ATTACH HOLES ON THE BULKHEAD PANEL. TOTAL TIME ON SPINNER DOME ANSDR CA100629001Bulkhead · crackedFWD PROPELLER SPINNER BULKHEAD FOUND CRACKED IN MULTIPLE PLACES AROUND BOLT HOLES. FOUND ON ROUTINE INSP. THIS IS BECOMING A COMMON PROBLEM.SDR 2010FA0000573Support · crackedSPINNER SUPPORT, MANY CRACKS AROUND AREA OF PROPELLER HUB MOUNT.SDR 2010FA0000572Support · crackedSPINNER SUPPORT, MANY CRACKS AROUND HUB MOUNT.SDR CA100527003Bulkhead · cracked(CAN) FORWARD SPINNER BULKHEAD FOUND CRACKED AROUND 3 BOLT HOLES DURING ROUTINE INSPECTION.SDR CA100607007Bulkhead · crackedBULKHEAD CRACKED PERPENDICULAR TO PROPELLER BOLT HOLES.SDR 2010FA0000269Spinner · destroyedAFTER TAKE OFF, AT ABOUT 500 AGL, MAJOR VIBRATION, THEN MINOR VIBRATION UNTILL LANDING, ABOUT 3 MINUTES. MINOR DAMAGE TO PAINT AND ENGINE BAFFLING, PROPELLER REMOVED AND SENT OUT FOR 100 HOUR CHECK . NO APPARENT DAMAGE TO PROPELLER OR ENGINE.SDR 2010FA0000231Spinner · crackedWHILE INSPECTING THE FWD PROP SPINNER BULKHEAD, CRACKS WERE FOUND. LOOKING FURTHER IT WAS NOTICED THE CTR HOLE IN THE SPINNER DID NOT LINE UP WITH THE CTR OF THE PROP. AFTER REMOVING THE PROP, IT WAS FOUND THE EDGE DISTANCE FROM THE 6 BOLT HOLES TO THE CTR OSDR CA100205003Bulkhead · cracked(CAN) SMALL HAIRLINE CRACKS DISCOVERED ON THE FWD SPINNER BULKHEAD AROUND 3 OF THE 6 BOLT HOLES THAT SECURE THE PROPELLER TO THE ACFT. (TC 20100205003)SDR CA100122008Bulkhead · cracked(CAN) WHILE DOING A 200HR INSP, AME NOTICED THAT THE SPINNER SCREWS WERE LOOSE AND THE SPINNER WAS CRACKED. SPINNER WAS REMOVED AND IT WAS NOTICED THAT THE REAR BULKHEAD WAS CRACKED BY THE PROP BLADE. THIS WAS THE NEW STYLE OF SPINNER AND REAR BULKHEAD - HEAVISDR CA091102011Bulkhead · shorted(CAN) CREW NOTED ON APPROACH THE THE NR 2 PROP DEICE A PHASE IS INOP. (JL2 - NR 1 "B" PHASE PROP HEAT LIGHT NOT ILLUMINATING WITH PROP HEAT). TR117. NR 2 PROP BULKEAD RING ASSY AND BRUSH BLOCK FOUND SHORTED. REPLACED.SDR 2009FA0000924Bulkhead · crackedPROPELLER SPINNER FWD BULKHEAD HAS CRACKS AROUND BOLT HOLES. CAUSE IS FROM NORMAL WEAR. COULD BE PREVENTED BY INSTALLING A RING UNDER BOLTS SIMILAR TO THE ONE USED IN THE PROPELLER. INSTALLATION IAW SB NR SB221B. (K)SDR CA090901014Spinner · crackedCRACKS DISCOVERED NEAR OTBD FLANGE AND INSIDE HOLE FOR PROP SHAFT, SEVERAL RIVETS SHEARED. COULD HAVE BEEN A PROBLEM IF UNDETECTED.SDR 2009F00054Spinner · crackedSMALL CRACKS IN BULKHEAD OF SPINNER AT OUTER RADIUS SPINNER CRACKED AT BLADE SHANK CUTOUTS.SDR CA090501005Bulkhead · cracked(CAN) BULKHEAD CRACKS NEAR THE PROP BOLT ATTACH POINTS, SPINNER SUPPORT MATERIAL SEEMS TO BE TOO SOFT, IT ROTATES IN THE SPINNER, ALLOWING THE SPINNER TO VIBRATE AND CRACK THE BULKHEAD, ALL THE PROPER SHIMS AND INSTALLATION IS DONE WITH THE INSTRUCTIONS SUPPLISDR CA090411001Bulkhead · cracked(CAN) PROPELLER BULKHEAD CRACKED.SDR 2009FA0000369Spinner · crackedA NEW PROPELLER WAS INSTALLED ON 10/23/08. ON 12/29/08, AFTER 10 HOURS, (2) DIFFERENT CRACKS WERE FOUND AT MOUNTING SCREW HOLES AT THE BLADE CUT OUT IN SPINNER DOME PN: D-5769-1P. A WARRANTY REPLACEMENT WAS SENT PN: 102965P, SN 0810591C AND INSTALLED. ON 3/SDR CA090401020Bulkhead · cracked(CAN) BULKHEAD CRACKED.SDR CA090227008Bulkhead · cracked(CAN) DURING AN ANNUAL INSPECTION A TECH FOUND CRACKS AROUND THE SPACER MOUNT BOLT HEADS ON REAR FACE OF BULKHEAD. THE PROP WAS REMOVED AND PARTIALLY DISASSEMBLED REAR BULKHEAD AND FOUND SUBSTANTIAL CRACKING UNDER CENTER REINFORCING PLATE ON FWD FACE OF REAR BSDR CA090106009Spinner · cracked(CAN) FOUND DURING 100 HOUR INSPECTION, CRACK IS QUITE VISABLE TO THE NAKED EYE.SDR 2009FA0000357Spinner · crackedA NEW PROPELLER WAS INSTALLED ON 10/23/2008. ON 12/29/2008, AFTER 10 HOURS, 2 DIFFERENT CRACKS WERE FOUND AT MOUNTING SCREW HOLES AT THE BLADE CUTOUT IN SPINNER DOME PN D-5769-1P. A WARRANTY REPLACEMENT WAS SENT PN D-5769-1P. A WARRANTY REPLACEMENT WAS SENTSDR CA081215004Bulkhead · cracked(CAN) CRACKS PERPENDICULAR TO PROP BOLT HOLES READILY VISIBLE TO THE NAKED EYE.SDR CA081215003Spinner · cracked(CAN) CRACKS PERPENDICULAR TO TOP OF PROP BOLT HOLES BARELY VISIBLE TO THE NAKED EYE, CONFIRMED WITH LPI.SDR COEA0803917Spinner · crackedMAJOR REPAIR, LT ENGINE PROPELLER SPINNER IS CRACKED AT 3 BOLT HOLES AND OTHER HOLES SHOW SIGNS OF WEAR. FOUND AT COE MAJOR REPAIR LT ENGINE PROPELLER SPINNER IS CRACKED AT 3 BOLT HOLES AND OTHER HOLES SHOW SIGNS OF WEAR. CUT OUT 3 CRACKED CORNERS AND MADE RSDR 2008FA0000587Dome · crackedTHE SPINNER ASSY FAILED IN FLIGHT ON A 2.2 HR FLIGHT LEG. APPROXIMATELY 1.5 HRS INTO THE FLIGHT A SMALL SHUDDER WAS FELT AND ALL INDICATION CHECKED NORMAL. THE AC COMPLETED THE FLIGHT AND IT WAS NOTED THAT 4" X 4" SECTION OF THE SPINNER BROKE OFF. THE COWLING SDR CA080807007Support · broken(CAN) PLASTIC SPINNER SUPPORT CRACKS AND BREAKS INSIDE SPINNER CAUSING VIBRATION, SEEMS PLASTIC IS SOFTER DURING THE HOT SUMMER MONTHS AND FLEXES MORE.SDR CA080805013Bulkhead · cracked(CAN) DURING ANNUAL INSP FWD SPINNER BULKHEAD WAS FOUND TO BE CRACKED AT SCREW ATTACHMENT HOLE. NEW PART WAS ORDERED FROM MFG IAW APPLICABLE PARTS CATALOGUE. NEW PART RECEIVED WAS STAMPED WITH CORRECT PN AS ORDERED, BUT WAS PHYSICALLY DIFFERENT IN DEPTH AND SDR 2008FA0000444Bulkhead · crackedDURING A 100 HR INSPECTION, PROPELLER SPINNER FWD BULKHEAD WAS FOUND TO BE CRACKED FROM A PROP BOLT HOLE OUT TOWARD THE OUTER EDGE OF THE BULKHEAD, APPROX 1.5 INCH LONG. THE PROP BOLTS AND THE BULKHEAD WERE REMOVED FRO THE AIRCRAFT. CLOSER INSPECTION SHOWED TSDR 2008FA0000413Bulkhead · crackedREPEATED FINDINGS OF CRACKS AT EDGE OF WASHER FOOT PRINT. ALLOY CHANGE, OR HARDWARE CHANGE MAY HELP. (K)SDR CA080418004Plate · damaged(CAN) RECEIVED A CALL REGARDING DAMAGE THAT OCCURRED TO THE PROP BACKING PLATED ON A TURBO BEAVER WE COMPLETED REG, C-FOEU. THIS DAMAGE IS THE RESULT OF OUR INSTALLATION OF OUR PROP POSITION TRANSMITTER MOD STCSA 98-46, VT2E 1623. IDENTIFIED THE PROBLEM TO BESDR CA080707008Spinner · cracked(CAN) WHILE DOING AN INSP, PROP SPINNER WAS FOUND CRACKED. THE CRACK STARTED FROM THE THE SCREW HOLES. A NEW SPINNER WAS INSTALLED AND THE PROP WAS BALANCED.SDR 2008FA0000119Bulkhead · crackedTHE FORWARD BULKHEAD CRACKED THROUGH THE MOUNT BOLT HOLES. THIS HAS OCCURED SEVERAL TIMES, WARRANTS ACTION. (K)SDR 2008FA0000118Bulkhead · crackedTHE FWD BULKHEAD CRACKED THROUGHT THE MOUNT BOLT HOLES. THIS HAS OCCURED SEVERAL TIMES, WARRANTS ACTION. (K)SDR 2008FA0000117Bulkhead · crackedTHE FWD BULKHEAD CRACKED THROUGH THE MOUNT BOLT HOLES. THIS HAS OCCURED SEVERAL TIMES, WARRANTS ACTION. (K)SDR 2008FA0000116Bulkhead · crackedTHE FORWARD BULKHEAD CRACKED THROUGH THE MOUNT BOLT HOLES. THIS HAS OCCURED SEVERAL TIMES, WARRANTS ACTION. (K)SDR 2008FA0000115Bulkhead · crackedTHE FORWARD BULKHEAD CRACKED THROUGH THE MOUNT MOLT HOLES. THIS HAS OCCURED SEVERAL TIMES, WARRANTS ACTION. (K)SDR 2008FA0000123Bulkhead · crackedPROP SPINNER FWD, BULKHEAD CRACKED NEAR MOUNT BOLTS. PART PROBABLY NOT STURDY. RECOMMEND PART BE MADE OF THICKER METAL DOUBLER INSTALLED. ALSO, IT APPEARED THAT MOUNT BOLT HOLES MAY BE TOO LARGE. (K)SDR TRBA2007109Screw · looseLOST NR 2 OIL PRESSURE IN FLIGHT. INDICATION ON CAP AND OIL PRESSURE SWITCH. NR 2 ENGINE SHUT DOWN IN FLIGHT AS PER AOM VOL 1. POST FLIGHT INSPECTION REVEALED OIL DRIPPING FROM ENGINE IN LARGE PUDDLE AND COVERING SIDE OF A/C. FOUND ACTUATOR ASSEMBLY PLUG ASDR CA070802005Bulkhead · cracked(CAN) THIS AIRCRAFT HAS HAD ALL THE AFT BULKHEAD AND HEAVIER SPINNER UPGRADES AND HAS HAD IT ALL ASSEMBLED IAW THE LATEST SB. CRACKS WERE FOUND FORMING PARALLEL FROM THE PROP BOLT HEAD CONTACT SURFACE ON (3) OF THE (6) HOLES. HAVE TO LOOK VERY CAREFULLY AS THESDR CA070704007Bulkhead · cracked(CAN) BULKHEAD IS CRACKED AROUND SEVERAL OF THE PROP THROUGH BOLT HOLES. (TC NR 20070704007)SDR CA070704008Bulkhead · cracked(CAN) CRACKED AROUND SEVERAL OF THE PROP BOLT THROUGH HOLES. (TC NR 20070704008)SDR CA070717009Bracket · broken(CAN) V-BRACKET OF SPINNER BROKE ON ONE SIDE, THAT CAUSED OFFSET OF SPINNER WHICH CAUSED VIBRATION AND DECIDED TO CONDUCT A PRECAUTIONARY LANDING ON A FARMERS FIELD. NO FURTHER DAMAGE. (TC NR 20070717009)SDR CA070313002Bulkhead · cracked(CAN) THIS AIRCRAFT HAS HAD ALL THE AFT BULKHEAD AND HEAVIER SPINNER UPGRADES AND HAS HAD IT ALL ASSEMBLED IAW THE LATEST SB. CRACKS WERE FOUND FORMING PARALLEL FROM THE PROP BOLT HEAD CONTACT SURFACE ON (3) OF THE (6) HOLES. YOU HAVE TO LOOK VERY CAREFULLY ASSDR CA061218019Bulkhead · cracked(CAN) THIS AIRCRAFT HAS HAD ALL THE AFT BULKHEAD AND HEAVIER SPINNER UPGRADES AND HAS HAD IT ALL ASSEMBLED IAW THE LATEST SB. THE (FORWARD SPINNER BULKHEAD) IS CRACKED AGAIN WITH LESS THEN 50 HOURS TSN, CRACKS RADIATING .2500 TO 1 INCH FROM 3 OF THE 6 HOLES.
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