JASC 6111
Service difficulty reports · 1,725
Reports filed under 6111 · Propeller Blade 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 = '6111' 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 = '6111' 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 CA000801021Blade · loose(CAN) LOOSE PROPELLER BLADES.SDR 20000508SH021Bearing · crackedCRACK INDICATION ON BOTH SIDES OF BEARING. (X)SDR 20000413SH058Plate · crackedDURING SEARCH INSPECTION, 4 EACH C-6066-1 PRELOAD PLATES WERE FOUND CRACKED. ONE EACH PRELOAD PLATE WAS CRACKED IN SUCH A MANNER THAT IT BROKE DURING INSPECTION. TIME SINCE LAST INSPECTION: 2,160:30 HOURS. (X)SDR 20000413SH056Blade · crackedDURING SEARCH INSPECTION, 4 EACH C-6066-1 PRELOAD PLATES WERE FOUND CRACKED. (X)SDR CA000410006Blade · corroded(CAN) BLADE BUT CORROSSION REQUIRED APPROVED REPAIR SCHEME.SDR CA000410005Blade · delaminated(CAN) BLADE SCRAPPED DUE TO CREASE DELAMINATION.SDR 2000ZZZX844Erosion Shield · debondedDEBOND ON NR 4 BLADE. REMOVED SHIELD TO REPAIR DEBOND AT STA 25 WHICH WAS 1 FOOT BY 1.25 FOOT IN JUST THE TOP LAYER OF GLASS. REPAIRED IAW HARTZELL BSF. INSTALLED NEW EROSION SHIELD AND BOOT IAW PROCEDURE 001 AND HARTZELL MM 135F AND 143A, AND BALANCED.SDR 20000426SH020Blade · crackedUPON INSPECTION OF THE PROPELLER BLADE DURING OVERHAUL, THE PITCH KNOB ON THE BUTT OF THE BLADE WAS FOUND CRACKED. BLADE WAS RETIRED FROM SERVICE. (X)SDR 20000426SH010Erosion Shield · crackedCRACKED AND DEBONDED EROSION SHIELDS. PRELOAD LOOSE. DISASSEMBLED AND CLEANED PROPELLER. REPLACED EROSION SHIELDS BLADE NR 1 SN 1588. BLADE NR 2 SN 1590. SET PRELOADS. REASSEMBLED PROP, SET BLADE ANGLES. REV AT 14.5 INCHES, FEATHER AT 79.0 INCHES, L.P.SDR 20000426SH009Erosion Shield · crackedCRACKED AND DEBONDED EROSION SHIELDS. PRELOAD LOOSE. DISASSEMBLED AND CLEANED PROPELLER. REPLACED EROSION SHIELDS BLADE NR 1 SN 1588. BLADE NR 2 SN 1590. SET PRELOADS. REASSEMBLED PROP, SET BLADE ANGLES. REV AT 14.5 INCHES, FEATHER AT 79.0 INCHES, L.P.SDR CA000404022Blade · cracked(CAN) BLADE THREADS CRACKED S/N K67168YSSDR CA000314005Blade · corroded(CAN) CORROSION FOUND ON BLADE SHANK.SDR 20000329SH034Plate · crackedDURING ROUTINE INSPECTION, FOUR OF THE SIX PRELOAD PLATES WERE FOUND CRACKED. CRACKS STARTED AT THE PITCH CHANGE BRACKET CUT-OUT AREA AND RAN ACROSS THE FACE OF THE PLATE AND DOWN THE OUTSIDE DIAMETER. (X)SDR AU000605Blade · cracked(AUS) PROPELLER WOULD NOT RETURN TO FINE PITCH FROM COURSE PITCH AT ENGINE SPEEDS BELOW 2200 RPM AND WOULD REMAIN IN COURSE PITCH AFTER FINE PITCH SELECTED.DURING PROPELLER DISASSEMBLY, THE NR 3 BLADE WAS FOUND CRACKED AT THE BLADE ROOT AROUND APPROXIMATELY HASDR 2000ZZZX842Shield · debondedEROSION SHIELD DEBOND BLADE NR 3, SN 1172. REMOVED AND REPLACED EROSION SHIELD IAW PROCEDURE 001 AND HARTZELL MM. STATIC BALANCED PROPELLER IAW HARTZELL CMM.SDR CA000313010Blade · cracked(CAN) A 3 INCH LONG CRACK HAS BEEN FOUND ON A BLADE TIP. INSTALLED A NEW PROP.SDR 20000331SH024Blade · misoverhauledPROPELLER VIBRATING AFTER RECENT OVERHAUL. DYNAMIC BALANCING HELPED. FOUND 7 AN 97-3 WASHERS FOR DYNAMIC BALANCE ADDED 6 MORE TO BRING BALANCE TO A 1 IPS. ALSO FOUND 6 STATIC WEIGHTS IN SAME LOCATION. REMOVED PROP FROM AIRCRAFT TO CHECK STATIC BALANCE. COSDR CA000224031Ring · debonded(CAN) PROPELLER LOW OIL INDICATION LIGHT OBSERVED. EVENTUALLY, PROP GOVERNOR CONTROL WAS LOST AND SPEED CONTROL REVERTED TO THE TOPPING GOVERNOR. ON ONE BLADE, THE TEFLON RING DISBONDED ALLOWING THE BLADE DOUGHNUT SEAL TO LEAK.SDR 20000426SH011Erosion Shield · crackedEROSION SHIELD DEBONDED AND CRACKED BLADE NR 2. REMOVED AND REPLACED EROSION SHIELD WITH NEW, STATIC BALANCED PROPELLER IAW PROCEDURE 001 AND HARTZELL CMM. NR 2 BLADE SN 1497, BOOT SN 0255. HYSOL BATCH NR AS9163016 AND 9228-1 (X)SDR 20000329SH008Seal · deterioratedNEW STYLE SEAL APPEARS TO HAVE DETERIORATED AFTER 672.4 HOURS OF SERVICE. RETURNED PARTS TO FACTORY FOR EVALUATION. (X)SDR 2000ZZZX601Blade · crackedPROPELLER BLADE CRACKED IN V SHANK. (ADP)SDR 2000ZZZX573Erosion Shield · damagedREMOVED EROSION SHIELD PAD BOOT FROM NR 1 BLADE, SN 2540, BECAUSE MISSING .1250 INCH BY .50 INCH PIECE OF EROSION SHIELD. INSTALLED NEW EROSION SHIELD AND DE-ICE BOOT WITH EA9330 LOT NR 9228-1 IAW PROCEDURE 001, AND HARTZELL M 135F 61-13-35. BALANCED IAW HARSDR 2000ZZZX574Erosion Shield · crackedREMOVED EROSION SHIELD AND DE-ICE BOOT FROM NR 2 BLADE, S/N 2315, BECAUSE OUT OF LIMITS FOR CRACKS. INSTALLED NEW EROSION SHIELD AND DE-ICE BOOT IAW PROCEDURE 001 AND HARTZELL MM 135F 61-13-35 AND BALANCED IAW 143A 61-10-16. USED HYSOL EA9330 LOT NR 9228-1.SDR 2000ZZZX564Blade · misoverhauledAIRCRAFT WAS IN GEAR UP LANDING IN 1995. PROPELLER WAS OVERHAULED BY KANSAS PROPELLER AND AVIATION. WO NR 1008. SUBMITTER STATED DAMAGE IN PRELOAD SHOULD HAVE BEEN REJECTED IN 1995.SDR CA000128004Blade · debonded(CAN) NICKEL ERROSIONSHEATH WAS FOUND TO BE DISBONDED AT THE HUB END, FACE SIDE OF PROP.SDR AU000128004Blade · disbonded(AU) NICKEL ERROSION SHEATH WAS FOUND TO BE DISBONDED AT THE HUB END, FACE SIDE OF PROPELLER.SDR 2000ZZZX494Shield · debondedEROSION SHIELD DEBONDED, BLADE NR 3 CRACKS, DEBOND AND ONE-HALF IN PIECE MISSING UNDER DEICE BOOT. REPLACED EROSION SHIELD. STATIC BALANCED PROPELLER IAW HARTZELL CMM AND PROCEDURE 001.SDR COMA9910187Blade · damagedFOUND NR 4 BLADE RIGHT PROP HAD TIP DAMAGE. REMOVED AND REPLACED NR 4 BLADE RIGHT PROP.SDR CA991230008Pin · corroded(CAN) DEEP CORROSION PITS, ACTUATING PINS REPLACED.SDR WVBAO1399Seal · leakingDURING INSPECTION OF PROPELLER, RED HUB OIL WAS FOUND LEAKING FROM THE BASES OF ALL 3 BLADES. THE INSIDE OF THE SPINNER AND SPINNER BULKHEAD ALSO HAD A NOTICEABLE AMOUNT OF RED OIL ON THEM. THE PROP WAS WASHED DOWN AND THE ENGINE RAN FOR 5 MINUTES AND SHUT DOSDR WVBAD1499Seal · leakingDURING INSPECTION OF PROPELLER, RED HUB OIL WAS FOUND LEAKING FROM THE BASES OF ALL 3 BLADES. THE INSIDE OF THE SPINNER AND SPINNER BULKHEAD ALSO HAD A NOTICEABLE AMOUNT OF RED OIL ON THEM. THE PROP WAS WASHED DOWN AND THE ENGINE RAN FOR 5 MINUTES AND SHUT DOSDR 99ZZZX4670Shield · crackedEROSION SHIELD CRACKED ON NR 3 BLADE, S/N 1776. REPLACED EROSION SHIELD BLADE NR 3, S/N 1776, TOUCHED UP PAINT, STATIC BALANCED PROPELLER IAW MFG CMM. REPLACED WORN SLIP RING WITH REPLATED, REPLACED BETA RING WITH NEW.SDR 99ZZZX4669Shield · debondedEROSION SHIELD DEBOND BLADE NR 2. REPLACED EROSION SHIELD BLADE NR 2, S/N 791MA. RE-ASSEMBLED PROPELLER, SET BLADE ANGLE, STATIC BALANCED PROPELLER IAW MFG CMM.SDR CA991229002Blade · cracked(CAN) NICKEL LEADING EDGE SHEATH CRACK PROPAGATED BEYOND ALLOWABLE LIMITS.SDR 2000ZZZM93Blade · looseLEFT PROPELLER BLADE MOVEMENT OUTSIDE ALOOWABLE LIMITS IN HARTZELL SERVICE INSTRUCTIONS. PROPELLER REMOVED AND REPLACED. (M)SDR CA991209040Blade · corroded(CAN) CORROSION FOUND UNDERDEICE BOOTS.SDR 99ZZZX4668Shield · crackedCRACKED EROSION SHIELD BLADE NR 1. REMOVED AND REPLACED EROSION SHIELD ON BLADE NR 1. TOUCHED UP PAINT AND STATIC BALANCED PROPELLER IAW MFG CMM.SDR 99ZZZX4667Shield · debondedEROSION SHIELD DEBOND, OUT OF LIMITS, NR 4 BLADE. REMOVED AND REPLACED EROSION SHIELD IAW PROCESS SPECIFICATION PROCEDURE 001 AS APROVED BY FAA ADMINISTRATOR.SDR AU991013Blade · corroded(AUS) PROPELLER BLADE CONTAINED EXFOLIATION CORROSION. AREA OF CORROSION APPROXIMATELY 6 MM (0.236 INCH) BY 4 MM (0.157 INCH) BY 1 MM (0.039 INCH) DEEP. THE PROPELLER WAS INSTALLED NEW ON THE 7/14/99.SDR AU990992Blade · corroded(AUS) PROPELLER BLADES CONTAINED EXFOLIATION CORROSION.SDR 99ZZZX4690Blade · failedTWO MINUTES AFTER TAKEOFF, NR 2 BLADE SEPARATED 6 INCHES FROM TIP CAUSING SEVERE VIBRATION PUTTING THE AIRCRAFT ALMOST OUT OF CONTROL. TOTAL TIME ON PROPELLER, 1,216.2 HOURS. SUBMITTER RECOMMENDED PROPELLER OVERHAUL AT 1,000 HOURS.SDR CA991004034Spring · broken(CAN) LIGHTNING STRIKE SUSPECT IN CAUSING PART DAMAGE.SDR 99ZZZX3829Shield · debondedEROSION SHIELD DEBONDED NR 3 BLADE. REPLACED EROSION SHIELD, OVERHAULED BLADE, SN 1213. ASSEMBLED PROP SET BLADE ANGLE, REV 14.5 DEGREES, FEATHER AT 79.6 DEGREES, LP AT 18.6 DEGREES, STATIC BALANCED PROP IAW MFG CMM.SDR AU991101Bearing · spalled(AUS) PROPELLER NR 1 BLADE RETAINING BEARING RACE BADLY SPALLED. FURTHER INVESTIGATION FOUND THE RACE WAS ALSO CRACKED.SDR AU990896Blade · cracked(AUS) PROPELLER BLADE CRACKED ON THE CAMBER SIDE OF THE BLADE IN THE MID-SPAN POSITION. THE CRACK RUNS IN A CHORDWISE DIRECTION APPROXIMATELY 381 MM (15 INCHES) FROM THE TIP.SDR 99ZZZX3504Fork · crackedFORWARD EAR OF PITCH CHANGE FORK CRACKED IN INBOARD RADIUS OF PITCH PIN ENGAGEMENT SLOTS. FOUR CRACKS. SUBMITTER STATED RECURRING PROBLEM.SDR 99ZZZX3503Fork · crackedFORWARD EAR OF PITCH CHANGE FORK CRACKED IN INBOARD RADIUS OF PITCH PIN ENGAGEMENT SLOTS. TWO CRACKS.SDR 99ZZZX3831Shield · debondedNR 2 BLADE EROSION SHIELD DEBONDED. DEBONDED BEYOND REPAIRABLE LIMITS. DISASSEMBLED, CLEANED, AND INSPECTED. REMOVED AND REPLACED EROSION SHIELD ON NR 2 BLADE (SN 1100) OVERHAULED BLADE AND RE-ASSEMBLED PROP IAW MFG CMM.SDR 99ZZZX3830Shield · debondedNR 4 BLADE HAS 2 CRACKS IN EROSION SHIELD ABOUT 1.5 INCHES FROM DE-ICE BOOT. DISASSEMBLED, CLEANED, AND INSPECTED. REMOVED AND REPLACED EROSION SHIELD ON NR 4 BLADE (SN 2484) OVERHAULED BLADE, RE-ASSEMBLED PROP, STATIC BALANCED, AND LUBRICATED IAW MFG CMM.SDR 99ZZZX3405Blade · fracturedAPPROXIMATELY 5 INCHES OF ONE PROPELLER BLADE TIP DEPARTED AIRCRAFT IN-FLIGHT. A SUCCESSFUL EMERGENCY LANDING WAS MADE. PROPELLER HAD BEEN RECONDITIONED AFTER PROP STRIKE 883.3 HOURS PREVIOUSLY. THERE IS NO EVIDENCE OF DAMAGE ON THE REMAINING PORTION OF THE
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