Pratt & Whitney JT3D series

Service difficulty reports · 70

Newest first. General aviation reporting is voluntary.

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 engine_model_key = 'JT3D'
  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 ABXA030216Frame · corrodedAFT CARGO BS 1010, BETWEEN LONGERON 35 LEFT AND 35 RT, FUSELAGE FRAME CORRODED ON UPPER CAP, UPPER AND LOWER SURFACES. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS, REMOVED (1 EA) FRAME CAP, (6 EA) GUSSETS, CUT OUT DAMAGED AREA, FABRICATED REPAIR ANGLE, FILLERJul 16, 2002 · N816AX · Doug DC863F · Fuselage Main, FrameSDR ABXA030218Structure · crackedFORWARD SERVICE DOOR UPPER FORWARD CORNER HAD A CRACK IN OUTER SKIN. CUT OUT CRACKED AREA, FABRICATED DOUBLER, TRIPLER, FILLER, AND INSTALLED EACH IAW SRM 53-2-0, 51-1-8, 51-1-21, 51-1-20D, 51-3-0 AND 51-1-14.Jul 16, 2002 · N816AX · Doug DC863F · Fuselage Main, Attach FittingsSDR ABXA030224Shear Tie · corrodedAFT LOWER CARGO, SHEARTIE CORRODED AT STA. 1200, LONGERON 28 - 29 LEFT. REMOVED CORROSION, OUT OF LIMITS. REMOVED FITTING AND FABRICATED SPLICE, INSTALLED NEW FITTING IAW DC-8 SRM 51-1-8, 53-2-0, AND 51-1-20D.Jul 15, 2002 · N816AX · Doug DC863F · Fuselage Main, StructureSDR COOSDR02051Frame · corrodedAFT CARGO COMPONENT STA 1600 BETWEEN LONG 34 LEFT AND 34 RIGHT FRAME, CORRODED.Apr 1, 2002 · N950R · Doug DC863 · Fuselage Main, FrameSDR COOSDR02050Floorbeam · corrodedMAIN CARGO COMPONENT, STA 1680, Z0, +X7 INCHES AND X 15 INCHES, FLOOR BEAM UPPER CHORD CORRODED.Apr 1, 2002 · N950R · Doug DC863 · Fuselage Main, Floor BeamSDR COOSDR02012Floorbeam · crackedMAIN CARGO COMPARTMENT. Y STA 1580, Z0, +49.0 AND +X56.0, FLOORBEAM UPPER CHORD WITH CRACK.Mar 8, 2002 · N950R · Doug DC863 · Fuselage Main, Floor BeamSDR COOSDR02013Longeron · corrodedFORWARD CARGO COMPT. Y STA 570.0, LONGERON 31R WITH CORROSION.Mar 1, 2002 · N950R · Doug DC863 · Fuselage Main, Longeron/StringerSDR COOSDR02011Floorbeam · corrodedMAIN CARGO COMPARTMENT Y STA 1680, Z0, -X10, FLOOR BEAM WITH CORROSION.Mar 1, 2002 · N950R · Doug DC863 · Fuselage Main, Floor BeamSDR COOSDR020009Frame · crackedNOSE SECTION, WHEEL WELL FRAME CRACKED AT STA Y 19,000, -X 23,000.Mar 1, 2002 · N950R · Doug DC863 · Fuselage Main, FrameSDR COOSDR020008Frame · crackedNOSE SECTION - WHEEL WELL FRAME CRACKED AT STA Y = 19,000 =X 23,000.Mar 1, 2002 · N950R · Doug DC863 · Fuselage Main, FrameSDR COOSDR02005Skin · dentedRIGHT WING, INBOARD AILERON-CONTROL TAB (PN 5642831502, SN 60023311) LOWER AND UPPER SKIN WITH DENT.Mar 1, 2002 · N950R · Doug DC863 · AileronsSDR COOSDR020006Doubler · corrodedLEFT LOWER WING EXTERNAL (BEAVER TAIL) DOUBLER WITH CORROSION.Mar 1, 2002 · N950R · Doug DC863 · Wing Miscellaneous StructureSDR COOSDR020007Doubler · corrodedRIGHT LOWER WING EXTERNAL (BEAVER TAIL) DOUBLER WITH CORROSION.Mar 1, 2002 · N950R · Doug DC863 · Wing Miscellaneous StructureSDR COOSDR02010Fitting · corrodedNET SUPPORT FITTING (PN 5711283516) CORRODED LOCATED AT AFT CARGO COMPARTMENT STA 1145 LONG 31R.Mar 1, 2002 · N950R · Doug DC863 · Fuselage Main, Attach FittingsSDR COOSDR020001Floorbeam · crackedFRAME TO FLOORBEARM STRUT, CRACKED.Mar 1, 2002 · N950R · Doug DC863 · Fuselage Main, Floor BeamSDR 20010403CW001Wire · brokenAFTER TAKEOFF, PILOT NOTICED ODD SMELL, FOLLOWED BY SMOKE. HE DECLARED AN EMERGENCY AND RETURNED TO AIRPORT WITHOUT INCIDENT. TROUBLE SHOT SYSTEM, FOUND OLD DEAD END GALLEY WIRE LAYING ON RES R4-35. REMOVED OLD WIRE. CHECKED WIRING TO SWITCHES 51-403, 51-3Jan 10, 2001 · N959R · Doug DC863F · Light System WiringSDR 99ZZZX559Gearshaft · crackedCHROME PLATE REMOVED FROM SEAL FACE (INDEX 27) AND BASE METAL FOUND TO BE CRACKED IN SEVERAL PLACES. FMPI FOUND THE PROBLEM. CAUSE UNKNOWN.Apr 8, 1998 · Turbine Engine Accessory DriveSDR ZIAA97011Bleed Valve · malfunctionedDAY - DURING TAKEOFF ROLL WITH POWER SET, LARGE BANG AND FIREBALL WAS OBSERVED ON RIGHT SIDE OF THE AIRCRAFT. RETURNED TO RAMP. INSPECTED NR 3 AND NR 4 ENGINES FOR DAMAGE. NONE FOUND. COULD NOT DUPLICATE ON GROUND RUN. SUBMITTER STATES, SUSPECT MOMENTARY Jan 23, 1997 · N799AL · Doug DC862 · Compressor Bleed ValveSDR BUFA9521Oil Line · looseMROC-MIA - NR 1 ENGINE LOW OIL PRESSURE LIGHT CAME ON 15 MILES TO MIA. AT FLIGHT IDLE, OIL PRESSURE INDICATOR READ LOW RED LINE. PRECAUTIONARY ENGINE SHUT DOWN PROCEDURE COMPLETED BEFORE LANDING MIAMI. NO EMERGENCY DECLARED, LANDING UNEVENTFUL. FOUND LOOSESep 21, 1995 · N915BV · Doug DC861 · Turbine Engine Oil SystemSDR 95ZZZZ266Engine · failedMIA - IN CLIMB, THE NR 1 ENGINE EGT INCREASED AND EXPERIENCED ENGINE VIBRATION. SHUTDOWN NR 1 ENGINE AND RETURNED AND LANDED AT MIA WITHOUT INCIDENT. INSPECTION REVEALED METAL IN THE TAIL PIPE. REPLACED NR 1 ENGINE.May 23, 1995 · N427FB · Doug DC8F54 · Engine (Turbine/Turboprop)
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