JASC 7210
Service difficulty reports · 873
Reports filed under 7210 · Turbine Engine Reduction Gear, 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 = '7210' 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 = '7210' 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 CA070227003Gearbox · making metal(CAN) SHORTLY AFTER TAKEOFF THE ENGINE CHIP LIGHT ILLUMINATED. THE PILOT RETURNED TO BASE. THE REDUCTION GEARBOX CHIP DETECTOR WAS INSPECTED AND A FERROUS METAL FLAKE WAS FOUND ON THE DETECTOR, NO CONTAMINATION WAS FOUND IN ANY SCREENS OR THE MAIN OIL FILTER. SDR CA070227015Gearbox · making metal(CAN) ENGINE NR 1 CHIP DETECTOR CAUTION LIGHT ILLUMINATED WHILE IN CRUISE FLIGHT AND PILOT RETURNED TO BASE. REDUCTION GEARBOX NR 1 SIDE CHIP DETECTOR FOUND WITH SMALL AMOUNT OF METAL. CHIP DETECTOR WAS CLEANED AND AIRCRAFT FLEW ANOTHER 2 HOURS BEFORE SECOND CSDR TAMF20070001OGearbox · leakingDURING CLIMB ON FLIGHT # 861 (MDE-SCL) LT ENGINE OIL QTY DECREASED TO ZERO AND OIL PRESS DECREASED FROM 64 TO 15 PSI. ENGINE WAS REDUCED TO IDLE AND OIL PRESS REMAINED IN 15 PSI. AIRCRAFT WAS RETURNED TO MDE AND LANDED IN NORMAL CONDITION. DURING MAINTENANCE SDR AALA20061262Gearbox · failedRIGHT ENGINE OIL PRESSURE WENT TO ZERO DURING CLIMB AT 24000 FEET. THE ENGINE SHUT DOWN. OIL QUANTITY AND TEMPERATURE NORMAL. SINGLE ENGINE TIME 18 MINUTES. RETURNED TO UIO AND LANDED WITHOUT INCIDENT. REPLACED RIGHT ENGINE DUE TO GEARBOX FAILURE. SYSTEMSDR 2006UALA02127Shaft · brokenNR 3 ENG FLAMEOUT. WHEN THE AGB COVER WAS REMOVED, THE TOWERSHAFT & TOWERSHAFT RETAINING RING FELL OUT. IT WAS CONCLUDED THAT THE TOWERSHAFT RETAINING RING WAS ONLY PARTIALLY ENGAGED IN THE TOWERSHAFT'S MATING GROOVE AT INSTALLATION. IN TIME, THIS ALLOWED SDR YTRR111853Gearbox · making metalDURING CRUISE FLIGHT, ENGINE CHIP LIGHT ILLUMINATED ACCOMPANIED BY HOWLING SOUND FROM ENGINE AREA. ONE MINUTE LATER, FADEC SYSTEM FAILED. PILOT AUTOROTATED INTO WATER.SDR CA061220005Bolt · sheared(CAN) IN CRUISE FLIGHT, ENGINE OIL PRESSURE WAS SEEN TO FLUCTUATE AND THEN DECAY TO ZERO. THE ENGINE WAS SHUTDOWN IN FLIGHT. SUBSEQUENT INVESTIGATION REVEALED A SHEARED 1ST STAGE REDUCTION GEAR BOX CARRIER BOLT. (TC NR 20061220005)SDR 2006FA0001004Restrictor Valve · failedFOLLOWING O/H AND INSTALLATION OF ENGINE ON AC AN IN-FLIGHT CHECK OF THE NTS SYSTEM WAS PERFORMED IAW MM INSTRUCTIONS. UPON ACTUATION OF THE STOP SWITCH BY THE PILOT FOR THE LT ENGINE THE AC YAWED NOSE LT APPROXIMATELY 20 TO 25 DEGREES. ALSO, THE ENGINE RPM SDR DSC4L6255Bearing · failedENGINE RECEIVED FOR REPORTED METAL IN OIL. UPON DISASSEMBLY, FOUND BEARING PN: 18118 (FAA-PMA REPLACEMENT PN: 3103585-1) INSTALLED IN ACCESSORY GEAR ASSY PN: 3103598-1 HAD FAILED, CAUSING MULTIPLE ACCESSORY GEAR DAMAGE AND METAL CONTAMINATION IN GEARBOX / OISDR CA061103005Shaft · damaged(CAN) THE ENGINE FLAMED-OUT IN CRUISE AND THE AIRCRAFT DIVERTED TO POINT OF DEPARTURE. SUBSEQUENT INSPECTION REVEALED METAL DEBRIS ON THE ENGINE CHIP DETECTOR AND DAMAGE TO THE TOWERSHAFT. MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISSDR 2006FA0000959Gearbox · making metalFOUND PTO , PTO BALL BEARING AND TORQUEMETER SPALLED. FOUND CHIPS ON CHIP PLUGS. DISASSEMBLED GEAR BOX AND FOUND PTO GEAR, TORQUEMETER GEAR AND PTO BALL BEARING SPALLED. REPLACED GEARBOX. (K)SDR CA060920001Gearbox · making metal(CAN) DEPARTING THE CREW OBSERVED A CHIP LIGHT INDICATION ON NR 2 RGB. THE ENGINE WAS SHUT-DOWN AND THE AIRCRAFT RETURNED TO POINT OF DEPARTURE WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND CONTAMINATION ON THE RGB PLUG BELIEVED TO BE FROM THE STARTER SEAL. THESDR SX4A200609002Planetary Gear · brokenGEARBOX FAILURE ON NR 1 ENGINE JUST AFTER TAKE OFF, INDICATED BY CHIP DETECTOR LIGHT.SDR SX4A0609002Planetary Gear · brokenGEARBOX FAILURE ON NR 1 ENGINE JUST AFTER TAKE OFF, INDICATED BY CHIP DETECTOR LIGHT.SDR SX4A0609001Planetary Gear · brokenGEAR BOX FAILURE ON NR1 ENGINE JUST AFTER TAKE OFF, INDICATED BY CHIP DETECTOR LIGHT.SDR C2XA06RI004Bevel Gear · fracturedDURING CLIMB, ENG NR 1 IN FLT SHUTDOWN. ACFT DIVERTED TO IAD. MX FOUND METAL DEBRIS ON CHIP DETECTOR. MX R & R ENGINE. OPS CHECKS PERFORMED SUCCESSFULLY. ACFT APPROVED TO RETURN TO FLT. REMOVED ENG FOR INVEST & REPAIR. DFDR DATA REVIEWED & INDICATED N2 STEADSDR CA061106001Shaft · fractured(CAN) THE ENGINE SUFFERED AN IN FLIGHT SHUTDOWN AS A RESULT OF A FRACTURED TOWER SHAFT. (TC NR 20061106001)SDR MAC070602Warning Light · illuminatedTHE LT ENGINE GEARBOX LOW OIL PRESSURE LIGHT ILLUMINATED IN FLIGHT 7 MIN AFTER T/O.SDR CA060731002Planetary Gear · making metal(CAN) METAL CONTAMINATION WAS FOUND ON THE CHIP DETECTOR. METAL ORIGINATED FROM RGB AND WAS THE RESULT OF SIGNIFICANT MATERIAL LOSS BETWEEN THE 1ST STAGE SUN GEAR AND THE 1ST STAGE PLANETARY GEARS. THIS IS OUR 2ND SUCH CASE WITH TIME CONTINUED GEARS. (TC NR 2SDR TIMR200600001Gearbox · corrodedOIL PRESSURE ANNUNCIATOR ILLUMINATED, GAUGE INDICATED OIL PRESSURE WAS LOW. PILOT ELECTED TO SHUTDOWN ENGINE. INVESTIGATION REVEALED CORROSION INTERNALLY IN THE REAR RGB CASE HAD CREATED AN OIL LEAK RESULTING IN EXCESSIVE OIL LOSS FOR THE ENGINE.SDR CA061006016Planetary Gear · worn(CAN) DURING CLIMB, ENGINE POWER FLUCTUATED ACCOMPANIED BY AN INCREASE IN ITT TEMPERATURE AND LOW OIL PRESSURE. THE ENGINE WAS SHUTDOWN IN FLIGHT. SUBSEQUENT INVESTIGATION REVEALED FIRST STAGE PLANETARY GEAR DISTRESS. (TC NR 20061006016)SDR CA060605007Shaft · broken(CAN) THREADED END BROKEN OFF DURING ASSY. (ENGINE POWER OUTPUT ADAPTOR SHAFT) (TC NR 20060605007)SDR CA060704002Gearbox · spalled(CAN) THE ENGINE CHIP DETECTOR WARNING ANNUNCIATED IN FLIGHT. THE ENGINE WAS SHUT DOWN AND THE AIRCRAFT DIVERTED TO AN ALTERNATE AIRPORT. SUBSEQUENT INSPECTION REVEALED SPALLING OF THE FIRST STAGE REDUCTION GEARBOX GEARING. (TC# 20060704002)SDR 2006FA0000476Gear · crackedPILOT REPORTED DURING CRUISE LEVEL FLIGHT FEELING A SUDDEN VIBRATION AND HEARING A SCREAMING NOISE FROM THE LT ENGINE. PILOT THEN NOTICED TORQUE INDICATION ON LT ENGINE INDICATING 120 PERCENT WITH NO YAW INDICATED OR NOTICED BY PILOT. WHILE RETARDING LT POWERSDR 06FDEA1310Engine · failedON CLIMB-OUT TO CRUISE, ALTITUDE PASSING 28000' HEARD A "THUD" AND EXPERIENCED AIRCRAFT YAW TO THE RIGHT. ENGINE INSTRUMENTS INDICATED NR 3 ENGINE FAILURE. SHUT DOWN ENGINE IN ACCORDANCE WITH QRH. FIRE EXTINGUSHING AGENT TO NR 3 ENGINE PER QRH, RETURNED TO SDR 2006FA0000335Sleeve · shiftedOPERATOR ATTEMPTED TO ROTATE THE PROPELLER DURING A PREFLIGHT CHECK AND NOTED PROP SHAFT LOOSENESS AND DRAG. THE ENGINE WAS REMOVED FOR REPAIR. EXAMINATION OF THE 2ND STAGE CARRIER IN THE RGB REVEALED THAT THE SLEEVE USED TO REPAIR THE NR 5 BEARING JOURNAL HADSDR CA060307004Bolt · failed(CAN) THE POWER SECTION OF ENGINE S/N PCE-PS 97533 WAS REMOVED DUE TO SEIZED CONDITION. THE REASON FOR REMOVAL AS DESCRIBED BY THE OPERATOR WAS FAILURE ON START-UP. THE POWER SECTION ROTATION HUNG ON LIGHT UP, RELEASED AND HUNG UP AGAIN. START ABORTED. POWERSDR KBM2006F00097Gearbox · making metalMODULE 5, ENGINE CHIP LIGHT ILLUMINATED, REMOVED AND REPLACED.SDR CA060227012Packing · cutTHE ENGINE LOW OIL PRESSURE WARNING ANNUNCIATED AND THE ENGINE WAS SHUT DOWN IN FLIGHT. SUBSEQUENT INSPECTION REVEALED A CUT O-RING PACKING AT THE PROPELLER CONTROL UNIT ADAPTER INTERFACE TRANSFER TUBE.SDR BAQ2005F00004Pump · unknownPUMP REMOVED IN COMPLIANCE WITH AD 03-21-09. (K)SDR 05FDEA03964Duct · chafedNR 1 ENG HIGH PRESSURE CONTROL VALVE CHAFING INTO 7TH STAGE AIR PRESSURE TURBINE CONTROL LINE. REMOVED 7TH STAGE COOLING TUBE, PER DC10-30 MM 75-22-00-02. REPAIRED DUCT PER EM 72-09-03. REINSTALLED DUCT AND HIGH PRESSURE VALVE. PERFORMED OPS AND LEAK CHECKSDR KBM2005F00331Magnetic Seal · leakingMAGNETIC SEAL, UNIT HAS LEAKS, REMOVED AND REPLACED. (K)SDR 05FDEA03496Case · crackedNR 1 ENGINE IGV CASE CRACKED 3 PLACES ALONG FWD. AND AFT SIDE WELD BEAD. REMOVED NR 1 ENGINE IGV CASE ON WK CARD 7200-2002,N/R00937. REMOVED AND REINSTALLED ENGINE NOSE COWL ,NOSE DOME FOR ACCESS IAW MM 71-10-021-4, MM71-10- 041-4 LEAK AND OPS. CHECKED GOSDR RAIA00509040Gearbox · seizedFLT 5436 - SPI - NR 1 ENGINE SHUTDOWN IN FLIGHT. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE DUE TO INTERMEDIATE GEAR BOX FAILURE.SDR CA051025003Gearbox · contaminatedFOUND A BOLT LOCKTAB IN NR 1 RGB CHIP DETECTOR HOUSING WHEN INVESTIGATING AN ENGINE CHIP LIGHT. ON FURTHER INVESTIGATION A SECOND LOCKTAB WAS FOUND IN THE VICINITY OF THE CHIP DETECTOR HOUSING. POWER SECTION WAS SEPARATED FROM THE C/BOX TO TROUBLESHOOT THE SSDR 2005FA0001363Gear · failedGEAR SET, REQUEST WARRENTY ON GEAR SET TOOTH FAILURE OR PINION. (K)SDR TIM2005F00006Repair · failedA REPAIR BY MFG ON A HOLE IN THE REDUCTION GEARBOX REAR HOUSING FAILED. THE FAILURE ALLOWED OIL TO LEAK IN TO THE COMBUSTION SECTION OF THE ENGINE. (K)SDR SWAA052386Gearbox · making metalDURING SCHEDULED A1 CHECK, FOUND METAL CHIPS IN NR 2 ENGINE FWD OIL MAGNETIC CHIP DETECTOR. REMOVED AND REPLACED NR 2 TRANSFER GEARBOX ASSY PER MM.SDR 2005FA0000988Module · making metalPILOT REPORTED ENGINE CHIP LIGHT ON HIS WAY TO HANGAR. MECHANIC DID THE INSPECTIONS IAW MFG MM AND FOUND A SMALL SINGLE FLAKE ON THE ELECTRIC MAG PLUG WHICH MONITORS THE REAR BEARING OIL RETURN LINE. MECHANIC ALSO THEN FOUND MULTIPLE FLAKES OF PLATEING ON THSDR CA050725003Carrier Assy · cracked(CAN) DURING ENGINE TREND RECORDING BY THE FLIGHT CREW IT WAS NOTICED THAT THE LH ENGINE OIL PRESSURE INDICTION HAD DECREASED 15 PSI WITHIN A WEEK OF OPERATION. UPON ARRIVAL MAINTENACE WAS ADVISED AND ELECTED TO REMOVE THE ENGINE FOR INSPECTION. UPON INSPECTIOSDR DLM88050371Gearbox · crackedNR 2 ENGINE INFLT SHUTDOWN DUE TO LOSS OF ENGINE OIL AND PRESSURE. FOUND OIL LEAK AT OIL FILTER CAP. GEARBOX CRACK AT STUD HOLDING CAP - NDS ENG CHANGE.SDR CA050719001Gearbox · failedTHE PILOT OBSERVED LOW/ERRATIC OIL PRESSURE AND TORQUE INDICATIONS AND EXECUTED A PRECAUTIONARY LANDING. A LARGE OIL LEAK WAS FOUND FROM THE EXHAUST STACK (GEARBOX VENT) AND COMPRESSOR VENT ORIFICE. THE ENGINE GEARBOX WAS FOUND TO HAVE MORE OIL THAN NORMAL ISDR AU510002167Bull Gear · brokenCHIP LIGHT ON IN FLIGHT. STRIP INSPECTION FOUND THAT THE ENGINE BULL GEAR HAD BROKEN TEETH.SDR KBM2005F00219Gear · making metalM05 REDUCTION GEAR, SUSPECTED OF CAUSING CHIP LIGHT. (K)SDR CA050725006Housing · corroded(CAN) DURING CRUISE, ENGINE OIL PRESSURE DECREASED AND THE ENGINE WAS SHUT DOWN IN FLIGHT. SUBSEQUENT INSPECTION REVEALED CORROSION OF THE REDUCTION GEARBOX HOUSING AT THE PCU TRANSFER TUBE LOCATION.SDR CA050609015Reduction Gb · making metal(CAN) DURING ROUTINE MAINTENANCE INSPECTION , NR 2 ENGINE RGB CHIP DETECTOR FOUND FLAGGED. WHEN REMOVING CHIP DETECTOR FOR INSPECTION , AUTO SHUTOFF DID NOT ACTIVATE AS LARGE METAL CHIP FOUND HOLDING CHIP DETECTOR BASE VALVE OPEN. CHIP POSSIBLY GEAR MATERIAL.SDR KBM2005F00052Chip Detector · defectiveENGINE CHIP LIGHT ON. REMOVED AND REPLACED ENGINE HORIZONTAL CHIP DETECTOR. (M)SDR UIEA200500055Gearbox · seizedDURING CRUISE ENGINE NR 2 FUEL FLOW BEGAN FLUCTUATING FOR 30 SECONDS, THEN THE ENGINE SHUTDOWN WITH THE FOLLOWING INDICATIONS. N1=26.1 PERCENT, EGT 0.0, N2 0.0, OIL PRESSURE 0.0, OIL QUANTITY 3.7 GALLONS, AND FUEL FLOW WAS 1.095. ENGINE WAS WINDMILLING 3 HOUSDR PCSA05041401Housing · strippedFLT 8414 ON APPROACH TO MIA CREW REPORTED NR 1 ENGINE LOST OIL, ENG. NR 1 WAS SHUTDOWN AS A PRECAUTION. A/C LANDED AT INTENDED DESTINATION WITHOUT FURTHER INCIDENT. MX INSPECTION OF THE NR 1 ENGINE FOUND OIL FILTER & GEARBOX CHIP DETECTORS HAD NO METAL, INSPECSDR AU510001454Gearbox · making metal(AUS) COMBINING GEARBOX METAL CONTAMINATION. (CASA# 510001454)
Back to JASC 7210