Boeing DHC-6-300
Service difficulty reports · 655
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 = 'DHC6300' 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 aircraft_model_key = 'DHC6300' 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 CA020508010Door · failed(CAN) DURING TAKEOFF ROLL THE CABIN AIRSTAIR DOOR OPENED. AIRCRAFT RETURNED TO THE TERMINAL AND PAX DISEMBARKED. THE AIRSTAIR DOOR INSPECTED AND THE TOP FORWARD LATCH PIN WAS FOUND IN THE RETRACTED POSITION. IT IS STILL NOT CLEAR WHAT CAUSED THE REAR PIN TO RESDR CA020225004Engine · corroded(CAN) - DETERIORATION INTERNALLY- CORROSION THROUGHOUT ENGINE - WHITE POWDERSDR CA020225003Engine · deteriorated(CAN) - DETERIORATION INTERNALLY- COATING DETERIORATED ON SMALL EXIT DUCT WHICH CAUSED DAMAGE TO TURBINE BLADES.- CORROSION THROUGHOUT ENGINE (UNEXPLAINABLE) INSIDE AND OUT - WHITE POWDER.SDR CA060208008Longeron · fractured(CAN) ON TAKE-OFF THE ENGINE TORQUE INDICATION OBSERVERED DROPPING OFF, ABORTED TAKE-OFF. OBSERVED LEFT ENGINE SAGGING IN THE COWLING. (TC# 20060208008)SDR CA020129003Blade · cracked(CAN) WHILE CARRYING OUT A POST LEASE INSPECTION ON THE AIRCRAFT BOTH ENGINES ARE SPLIT AT THE "C" FLANGE FOR HOT SECTION INSPECTION. DURING THE RIGHT H.S.I. THE ENGINEER NOTICED "LINES" ON SOME OF THE C.T. BLADES. NINE BLADES SEEM TO BE CRACKED. SEVEN BLADES SDR AUS20011365Audio Panel · failed(AUS) AUDIO PANEL FAILED. SUSPECT INTERNAL TRANSFORMER BURNT.SDR AUS20011446Block · failed(AUS) RH MAIN LANDING GEAR COMPRESSION BLOCKS FAILED. DAMAGE CAUSED TOTHE FUSELAGE LOCATED INBOARD OF THE RH MLG.SDR CA011218002Throttle Cable · failed(CAN) DURIING A ROUTINE EMMA CHECK 46, THE LT ENGINE THROTTLE CABLE TURNBUCKLE END WAS FOUND FRACTURED AND WAS ONLY HELD TOGETHER BY LOCKWIRING. CABLE REPLACED.SDR CA011030002Frame · cracked(CAN) CRACK FOUND IN SIDE FRAME AT RT. STATION 218.125 RUNNING ON AN ANGLE FROM TOP OF FRAME. NOTE PART IS POST MOD 6/1462 AS DIRECTED BY CF-78-17R1. DHC SB 6/371 REV.B.PLEASE SEE PHOTOS.SDR CA011016001Screen · broken(CAN) DURING MAINTENACE TO CHANGE A GROUND BLOWER THE EXPANSION CHAMBER WAS REMOVED TO GAIN ACCESS TO THE BLOWER. A RATTLE WAS NOTICED INSIDE THE CHAMBER . INVESTATION REVEALED THE INTERNAL SCREEN HAD SEPERATED FROM THE FILTER SCREEN. THIS CONDITION COULD POSSDR CA020508008Csu · failed(CAN) IN CRUISE AT 3,500 FT THE RT ENGINE PROP RPM REDUCED TO 40 PERCENT WITH TORQUE ON RT ENGINE INCREASING. WE REDUCED POWER. PROP RPM CONTINUED TO REDUCE TO 20 PERCENT. POWER WAS REDUCED FURTHER TO IDLE. NO BETA INDICATION. I CALLED FOR THE PROPELLER FEATHESDR CA011128008Cell · deformed(CAN) SMOKE WAS VISIBLE IN THE BAGGAGE COMPARTMENT WHEN OPENED ON THE RAMP. ONE CELL WITHIN THE BATTERY WAS FOUND TO BE DEFORMED FROM HEAT.SDR AUS20010720Fcu · faulty(AUS) FUEL CONTROL UNIT FAULTY. INVESTIGATION FOUND THE PY RESTRICTOR PARTIALLY BLOCKED BY SUSPECTED PAINT FLAKES.SDR OEZ2001F00000Bleed Valve · contaminatedTHIS ENGINE WAS TESTED AT A REPAIR STATION WITH NO OPERATIONAL DEFECTS FOUND. THE ENGINE WAS REINSTALLED ON THE SAME AIRCRAFT AND TEST FLOWN SUCCESSFULLY. ON 06/21 THE FLIGHT CREW REPORTED UNABLE TO ACHIEVE TAKEOFF POWER AND UNUSUAL SOUND COMING FROM ENGINE.SDR CA020508007Switch · shorted(CAN) AFTER LIFT-OFF NOTICED TORQUE INCREASING & PROP RPM DECREASING ON ENGINE NR 1. VISUAL CHECK FROM LT CONFIRMED THAT ENGINE NR 1 HAD GONE INTO FEATHER. WERE BARELY 200 AGL WHEN OCCURRED. IDENTIFIED & FEATHERED NR 1 ENGINE (POWERLEVER IDLE PROP FEATHERED). SDR CA010629009Servo · failed(CAN) DURING FLIGHT, AILERON CONTROL LOST DUE TO AILERON SERVO SERVO PRIMARY JAMMED. AIRCRAFT RETURNED TO BASE. SERVO WAS REPLACED. AIRCRAFT RETURNED TO SERVICE.SDR CA010622034Seat Belt · damaged(CAN) 10 PAX LAP BELT ASSY'S WERE REPAIRED AND CERTIFIED BY UNAUTHORIZED REPAIR FACILITY. UNKNOWN IF WEBBING MATERIAL AND THREAD MEETS SPECIFICATION. UNKNOWN IF STITCH PATTERN WILL TENSILE TEST TO REQUIRED LIMIT. LAP BELTS WERE RE-WEBBED TO PROPER 1500 LB CINFSDR 20010510AP008Resistor · burnedWINDSHIELD WIPER DROPPING RESISTOR SHORTED TO GROUND THROUGH DEACTIVATED WINDSHIELD WASHER RESISTOR MOUNT. THE WIPER DROPPING RESISTOR LEAD CHAFFED ON THE WINDSHIELD WASHER RESISTOR MOUNTING BRACKET. THIS RESULTED IN SMOKE IN THE COCKPIT DURING DESCENT WHILE USDR CA010515005Rheostat · overheated(CAN) OXYGEN REGULATOR IN COPILOT POSITION WAS REPLACED WITH OVERHAULED UNIT. INTERNAL LIGHTING WIRES FOR THIS UNIT WERE CONNECTED IMPROPERLY (POLARITY REVERSED).AS A RESULT THE RHEOSTAT WHICH CONTROLS LIGHT INTENSITY FOR THE COPILOTS INSTRUMENT LIGHTING WAS SSDR AU010287Governor · faulty(AUS) RT PROPELLER GOVERNOR FAULTY.SDR AU010075Block · failed(AUS) RT MAIN LANDING GEAR COMPRESSION BLOCKS FAILED WITH RESULTANT DAMAGE TO THE FUSELAGE. BLOCKS FAILED DUE TO RT MLG CONTACTING A RIDGE ON THE AIRSTRIP.SDR CA010307006Engine · failed(CAN) WHILE IN LEVEL CRUISE AT 500 AGL THE RT ENGINE FAILED. FIRST OBSERVATION WAS DROPPING OIL PRESSURE, PROPELLER AUTO-FEATHERING AND AIRCRAFT YAWING TO RIGHT. RT ENGINE WAS SECURED AND AIRCRAFT RETURNED TO BASE. UPON EXAMINATION AT BASE, THE POWER TURBINE WSDR 20010215SG002Relay · shortedFLT 9658 - VIJ/SJU - SPARKS NOTICED AT ROW 2EF OVERHEAD PANEL. REMOVED AND REPLACED NR 1 STARTER GENERATOR RELAY. (M)SDR AU010112Fitting · cracked(AUS) VERTICAL STABILISER FORWARD ADAPTER FITTING RIGHT HAND ATTACHMENT LUG CRACKED.SDR CA010212025Tube · cracked(CAN) DURING A SCHEDULED EMMA INSPECTION WHAT APPEARED TO BE A LONGITUDINAL CRACK APPROXIMATELY 6.5 INCHES WAS NOTICED IN THE FORWARD UPPER SCAVENGE OIL TUBE ON THE LEFT ENGINE. FURTHER VISUAL INSPECTION WAS CARRIED OUT USING A 10X MAGNIFYING GLASS. SUBSEQUENTSDR 20010112SG055Filter · looseDURING CRUISE FLIGHT FROM GCN-LAS, FLIGHT CREW REPORTED HYDRAULIC PRESSURE FELL TO ZERO AND EMERGENCY PUMP DID NOT WORK EITHER. AN EMERGENCY WAS DECLARED TO ATC AND A SUCCESSFUL LANDING WAS MADE. COMPANY MAINTENANCE PERSONNEL FOUND HYDRAULIC FLUID LEAKING ATSDR CA001031028Link · cracked(CAN) CRACK INDICATION ON THE LINK ARM FOUND DURING OVERHAUL INSPECTION.SDR AU001326Vane · damaged(AUS) LT ENGINE POWER TURBINE VANE ASSEMBLY BROKEN AND POWER TURBINEDISC DISLODGED.SDR CA001018020Control Rod · cracked(CAN) DURING INSPECTION THE SERVO TAB LINK FOR THE AILERON WAS FOUND CRACKED AT THE UPPER END. THE CRACK EXTENDED FROM THE WITNESS HOLE TO THE END OF THE ROD. FOR REFERENCE SEE DEHAVILLAND IPC 27-10-00, FIG.5 (SHEET 1 OF 1), ITEM 90. THE ROD WAS REPLACED AND TSDR CA001020022Control Unit · malfunctioned(CAN) PIC REPORTED TO YVP FSS (22:40 H LCL) THAT THE NOSE WHEEL STEERING TILLER WAS STUCK IN RT POSITION. THE AIRCRAFT LANDED WITHOUT INCIDENT.NOSE WHEEL STEERING SYSTEM INSPECTED WITH AIRCRAFT ON JACKS; CABLE TENSION VERIFIED, HYDRAULIC SYSTEM CHECKED, ACTUATSDR CA000928005Stall Bar · debonded(CAN) DURING A SCHEDULED MAINTENANCE CHECK,, THE RT STALL BAR WAS FOUND TO BE PARTIALLY UNGLUED. THE STALL BAR WAS REMOVED, CLEANED AND REBONDED AS PER DHC MAINTENANCE INSTRUCTIONS.SDR AU000647Seal · failed(AUS) BLEED AIR PIPE CONNECTOR PERISEAL DETERIORATED AND LEAKING. (X)SDR AU000617Windshield · cracked(AUS) AIRCRAFT WAS PARKED (AWAITING DEPARTURE) BEHIND ANOTHER AIRCRAFT WHEN THE PILOT OF THE LEAD AIRCRAFT PERFORMED AN ENGINE POWER CHECK. STONES WERE THROWN UP AND CRACKED THE RIGHT WINDSHIELD. (X)SDR AU000616Skin · wrinkled(AUS) NOSE LANDING GEAR IMPACTED TWO EARTH MOUNDS ON LANDING. GROUND INVESTIGATION FOUND SKIN RIPPLES AND LOOSE RIVETS IN THE LOWER FUSELAGE AREA AT STN 60. TWO LOWER STRINGER ANGLES WERE ALSO FOUND TO BE CRACKED. (X)SDR AU000615Terminal · faulty(AUS) DURING CRUISE, THE ENGINE T5 INDICATOR FLUCTUATED BETWEEN 500 DEGREES CELSIUS AND 630 DEGREES CELSIUS. INVESTIGATION FOUND A DEFECTIVE WIRING JOINT AT THE ENGINE TERMINAL. (X)SDR CA010111021Oil Cooler · leaking(CAN) IT WAS OBSERVED BY THE ENGINEER THAT THE LEFT ENGINE COWLING AFT OF THE OIL COOLER AIR EXHAUST WAS COVER WITH OIL. THE OIL COOLER WAS PRESSURE TESTED, HOWEVER, A VISUAL LEAK WAS NOT DETECTABLE. THE OIL COOLER WAS REPLACED AND THE OIL ON THE COWLING HAS NSDR 20001113SH019Switch · defectiveSECOND RADIO SWITCH FROM LEFT STARTED SMOKING. NOW INOPERATIVE AND SPONGY FIRST SWITCH. REMOVED AND REPLACED CIRCUIT BREAKER SWITCHES WITH 2 RELAYS AND 2 SWITCHES IAW 337 DATED 8-3-00. (X)SDR AU000557Strut · corroded(AUS) LEFT WING STRUT CORRODED IN AN AREA LOCATED APPROXIMATELY 355.6 MM (14 INCHES) OUTBOARD FROM THE LOWER ATTACHMENT FITTING ON THE AFT WEB. FOUND DURING INSPECTION IAW AD/DHC6/58 AND SB 6-474. (X)SDR AU000566Collar · cracked(AUS) NOSE LANDING GEAR STEERING COLLAR CRACKED IN ATTACHMENT BLOCK RADIUS. FOUND USING VISUAL INSPECTION AND CONFIRMED USING ULTRASONIC INSPECTION.SDR AU000602Longeron · cracked(AUS) A CRACK APPROXIMATELY 44.5 MM (1.75 INCHES) WAS FOUND IN THE RT OUTBOARD ENGINE NACELLE LONGERON, APPROXIMATELY 24 CM (9.5 INCHES) AFT OF THE ENGINE MOUNT FITTING. THE CRACK ORIGINATED FROM BENEATH STRAP P/N C6WM1712-27 WHICH WAS FITTED IAW DHC MOD 6/16SDR CA000621043Gearbox · making metal(CAN) AIRCRAFT RETURNED TO GOOSEBAY AFTER DEPARTURE DUE TO ENGINE PROBLEMS ON CLIMBOUT. ENGINE TORQUE DROPPED OFF FROM POWER SELECTED. CREW SHUTDOWN THE ENGINE AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTION REVEALED METAL IN THE OIL FILTER AND IN SDR AU000400Relay · burned(AUS) GENERATOR CONTROL ASSEMBLY HEAT DAMAGE. LT REVERSE CURRENT RELAY (RCR) SEVERELY HEAT DAMAGED. RT REVERSE CURRENT RELAY HEATDAMAGED.SDR 20000619SH002Diode · shortedGCN/VGT - EN ROUTE, CREW DIVERTED AIRCRAFT TO GCW DUE TO A SMELL OF ELECTRICAL BURNING IN THE COCKPIT. (X)SDR AU000564Longeron · cracked(AUS) ENGINE NACELLE RIGHT OUTBOARD LONGERON CRACKED IN AN AREA APPROXIMATELY 254 MM (10 INCHES) AFT OF THE ENGINE MOUNT FITTING. CRACK LENGTH APPROXIMATELY 57.15 MM (2.25 INCHES). FOUND DURING INSPECTION IAW AD/DHC6/51.4 (DHC6 SB 6/509).SDR CA000606021Control Rod · cracked(CAN) DURING INSPECTION THE SERVO TAB LINK FOR THE AILERON WAS FOUND CRACKED AT THE UPPER END. THE CRACK EXTENDED FROM THE ROD END BEARING RETENTION RIVET HOLE TO THE END OF THE ROD. FOR REFERENCE SEE DEHAVILLAND IPC 27-10-00, FIG. 5 (SHEET 1 OF 1), ITEM 90. SDR 20000721AP001Relay · stuckFLT 9644 - RIGHT ENGINE INDICATED FIRE, FIRE BELL WARNING SOUNDED, PULLED FIRE HANDLE DISCHARGED ENGINE FIRE BOTTLE PER ENGINE FIRE INSTRUCTIONS. DETERMINED GENERATOR RELAY TO HAVE FAILED IN THE ENGAGED MODE, CAUSING THE STARTER/GENERATOR TO REMAIN IN THE STASDR CA000414010Rod End · cracked(CAN) CRACK STARTING UNDER RODEND JAMNUT. APPROX. 1/2 IN LENGTHSDR CA000331008Cooler · leaking(CAN) DURING ROUTINE INSPECTION IT WAS NOTED THAT THE OIL TRANSFER LINE ON THE REAR OF THE OIL COOLER WAS LEAKING UNDER STATIC CONDITIONS. WHEN THE UNIT WAS DRAINED IT WAS ALSO NOTED THAT THE DRAIN PLUG WAS THE INCORRECT TYPE. THE PLUG WAS A BOLT RATHER THANSDR AU000601Door · malfunctioned(AUS) DURING FLIGHT, THE CABIN AIRSTAIR DOOR OPENED. SUBMITER SUSPECTED REAR SEAT PASSENGER MAY HAVE ACCIDENTLY BUMPED THE DOOR HANDLE WITH KNEE.SDR CA000331009Support Bracket · wrong part(CAN) WHILE INSTALLING A NEW STARTER, THE AFT BEARING SUPPORT WAS OF A DIFFERENT TYPE THAN NORMAL. THE BEARING SUPPORT HAD A SHOULDER THAT WOULD NOT PERMIT THE COOLING DUCT TO FIT PROPERLY. UNIT WAS RETURNED FOR REPAIR.
Back to Boeing DHC-6-300