Dehavilland DHC-2

Service difficulty reports · 120

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 aircraft_model_key = 'DHC2'
  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 CA000301007Spar · deformed(CAN) DURING INSPECTION A SMALL DEFORMATION WAS FOUND ON TOP OF THE WING. FOUND AT DISASSEMBLY OF THE MAIN SPAR AT THE STATION 150.5 TO 164. THE WING PANEL AT THE SPAR WAS REMOVED AND SPAR SECTION REPLACED.Feb 21, 2000 · Dhav DHC2* · Wing SparSDR AU000182Piston · cracked(AUS) PISTON CRACKED FROM GUDGEON PIN HOLE, THROUGH THE RING LANDS TO THE CENTRE OF THE PISTON CROWN.Feb 20, 2000 · Dhav DHC2* · Reciprocating Engine Cylinder SectionSDR AU000130Engine · failed(AUS) ENGINE FAILED IN-FLIGHT.Jan 9, 2000 · Dhav DHC2* · Engine (Turbine/Turboprop)SDR CA991209023Spar Cap · corroded(CAN) DURING A ROUTINE ULTRASONIC INSPECTION AS PER CF83-23, SPAR CAP INSPECTION, A DEFECT WAS DETECTED BEHIND AN INTACT HINGE TANG IN THE UPPER SPAR CAP AREA. UPON FURTHER INVESTIGATION OF THE DEFECTIVE SECTION IT WAS NOTED THE CORROSION HAD ORIGINATED FROM Sep 23, 1999 · Dhav DHC2* · Wing SparSDR AU990803Sump · contaminated(AUS) METAL CONTAMINATION OF ENGINE SUMP.Aug 12, 1999 · Dhav DHC2* · Engine (Reciprocating)SDR 20000714SH005Cylinder · separatedNR 2 CYLINDER HEAD SEPARATED FROM BARREL. AIRCRAFT IN CRUISE, PRECAUTIONARY LANDING MADE WITHOUT INCIDENT. SUBMITTER RECOMMENDED UNTHREADING OF CYLINDER HEAD/BARREL AT OVERHAUL OR MANUFACTURE OF NEW CYLINDER ASSY. (X)Aug 8, 1999 · N2740X · Dhav DHC2* · Reciprocating Engine Cylinder SectionSDR AU990330Cylinder · cracked(AUS) NR 1 CYLINDER HEAD SEPARATED FROM BARREL.Mar 2, 1999 · Dhav DHC2* · Reciprocating Engine Cylinder SectionSDR CA990209003Bulkhead · cracked(CAN) BULKHEAD STA 228 FOUND CRACKED PER AD CF-98-38. CRACKS RUNNING ALONG THE LOWER LEFT CORNER AND MID-WAY UP THE RIGHT SIDE. BOTH CRACKS WERE RUNNING ALONG THE BEND AND STARTED AT THE CUT-OUTS.Feb 2, 1999 · Dhav DHC2* · Fuselage Main, BulkheadSDR 98ZZZX4126Strut · corrodedP/N C2FS3281A AND P/N C2FS3282A STRUT ASSEMBLIES THAT ATTACH TO P/N C2FS3203A TUBULAR FRAME ASSEMBLY WERE DETERMINED UNAIRWORTHY DUE TO CORROSION. BECAUSE OF THE LOCATION OF THESE STRUTS (UNDER THE WINDSCREENS), THEY SHOULD BE INSPECTED WHENEVER THE WINDSCREEOct 24, 1998 · N47241 · Dhav DHC2* · Main Landing Gear Strut/Axle/TruckSDR 98ZZZX4125Strut · corrodedP/N C2FS3281A AND P/N C2FS3282A STRUT ASSEMBLIES THAT ATTACH TO P/N C2FS3203A TUBULAR FRAME ASSEMBLY WERE DETERMINED UNAIRWORTHY DUE TO CORROSION. BECAUSE OF THE LOCATION OF THESE STRUTS (UNDER THE WINDSCREENS), THEY SHOULD BE INSPECTED WHENEVER THE WINDSCREEOct 24, 1998 · N47241 · Dhav DHC2* · Fuselage Main, StructureSDR CA981207011Magneto · broken coil(CAN) PILOT RETURNED TO DOCK AFTER RUN-UP INDICATED THE RIGHT HAND MAGNETO WAS DEAD. INVESTIGATION REVEALED THE END OF THE ROTOR WITH CONTACT WITH THE COIL WAS BROKEN OFF AND THE COIL DAMAGED. THE MAGNETO WAS REPLACED.Oct 15, 1998 · Dhav DHC2* · Magneto/DistributorSDR AU981035Skin · damaged(AUS) LEFT WING LEADING EDGE DAMAGED BY CONTACT WITH A YACHT DURING A STORM. AIRCRAFT IS A FLOAT PLANE.Aug 7, 1998 · Dhav DHC2* · Wing, Plate/SkinSDR CA981125083Strut · corroded(CAN) WHILE CHANGING PILOT'S WINDSCREEN, THE FAIRING HOLDING WINDSCREEN WAS REMOVED. CORROSION WAS THEN NOTICED ON BOTH THE RIGHT AND LEFT FUSELAGE STRUT ASSEMBLIES. OTHER P/N C2FS328A.Jul 13, 1998 · Dhav DHC2* · Fuselage Main, StructureSDR CA980706018Fitting · cracked(CAN) STRUT REMOVED TO REPLACE NEW UPPER BUSHINGS. STRUT END SHOWED INDICATION OF SKIN MOVEMENT AT UPPER RIVETS THEN A SCRATCH FOUND ACROSS FACE OF UPPER STRUT END SB 2/41. INSPECTION CARRIED OUT AND A SMALL CRACK WAS FOUND.Jun 19, 1998 · Dhav DHC2* · Wing, Fuselage Attach FittingsSDR 98ZZZX1034Fitting · crackedONLY WHEN SPREADER BAR IS REMOVED CAN THE FLOAT ATTACH FITTINGS BE VIEWED. BOTH FRONT FITTINGS WERE CRACKED THROUGH THE TAPER PIN HOLE. SUBMITTER BELIEVES THE PLATE IN THE SPREADER BAR HAD SOME PLAY AND SOMEONE PUT EXTRA WASHERS AT THE BOTTOM OF THE TAPER PIMar 2, 1998 · N108H · Dhav DHC2* · Wheel/Ski/FloatSDR EY2R9600149Spider · crackedSPIDERS CRACKED IN SPLINES OF HUBOct 1, 1996 · Dhav DHC2* · Propeller Hub SectionSDR 97ZZZX5036Stud · defectiveNR 1 CYLINDER STUD DEFECTIVE. THIS IS A COMMON PROBLEM TO THESE ENGINES. THE BASIC PROBLEM HERE IS HOW THE AD READS. SUBMITTER BELIEVES THERE IS A NEED TO REVISE THE WORDING.Jul 8, 1996 · N38938 · Dhav DHC2* · Reciprocating Engine Power SectionSDR EY2R9600066Clamp · crackedPROP ASSY CLAMP CRACKEDMay 1, 1996 · Dhav DHC2* · Propeller AssemblySDR 95ZZZX1795Spar Doubler · corrodedHORIZONTAL STABILIZER REAR SPAR DOUBLERS EXTENDING FROM STATION ZERO TO 40 ON UPPER AND LOWER FLANGES OF SPAR WERE FOUND CORRODED UNDER ELEVATOR HINGE BRACKETS AND REAR ATTACH FITTING. STEEL BRACKETS RIVETED TO ALUMINUM STRUCTURE ON SEAPLANES ARE SUBJECT TO CApr 4, 1995 · N2740X · Dhav DHC2* · Horizontal Stabilizer, Spar/RibSDR 95ZZZX1794Bulkhead · corrodedAFTER REMOVING HORIZONTAL STABILIZER ATTACH BRACKET, C2FS543A, TO INCORPORATE MOD 2/1338, BULKHEAD FOUND PERFORATED BY CORROSION. DAMAGE WAS NOT APPARENT UNTIL FITTING WAS REMOVED. ALL AREAS ON TAIL WHERE STEEL FITTINGS ARE RIVETED TO ALUMINUM STRUCTURE SHOUApr 4, 1995 · N2740X · Dhav DHC2* · Fuselage Main, Bulkhead
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