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 CA081222001Circuit Breaker · unserviceable(CAN) THE FLIGHT CREW REPORTED THE 35 AMP HYDRAULIC PUMP CIRCUIT BREAKER POPPED. THEY ELECTED TO RETURN TO BASE AND USED HYDRAULIC HAND PUMP FOR BRAKE OPS. MX TROUBLESHOT THE SYSTEM, REPLACED 35 AMP CIRCUIT BREAKER, GROUND TESTED THE SYSTEM, AND RETURNED THESDR CA081114008Fastener · loose(CAN) DURING INSP, THERE WAS SEVERAL CHERRY MAX RIVETS FOUND TO BE LOOSE ON THE UNDERSIDE OF THE RT WING BETWEEN STATION 35.15 AND 97.50. THE RIVETS WERE ALL LOCATED ON A TRIPLE ROW OF RIVETS AT THE AFT SPAR. FURTHER INSPECTION REVEALED A TOTAL OF 160 RIVETS NSDR S9BA2008032Gasket · failedLOST NR 2 OIL PRESSURE AND TORQUE PRESSURE OIL ON ENGINE COWLING AND RIGHT FLOAT. FOUND OIL COOLER RETURN LINE GASKET LEAKING. REMOVED AND REPLACED GASKET, SERVICED ENGINE WITH 4 QUARTS OF OIL. LEAK CHECK SATISFACTORY. PROPELLER WAS FEATHERED AND ENGINE WASSDR S9BA2008031Clamp · looseON PREFLIGHT FUEL ODOR NOTICED IN CABIN. FOUND CLAMP AT FWD RT FUEL CELL NIPPLE LOOSE. TIGHTENED CLAMP AND CHECKED FOR LEAKS. NO LEAKS NOTED. REQUEST CHECK FLIGHT TO CHECK FOR FUEL SMELL IN CABIN. CHECK FLIGHT WAS SATISFACTORY.SDR S9BA2008030Relay · faultyON FIRST START, LEFT ENGINE DID NOT SPOOL UP. DURING SECOND ATTEMPT STRONG ELECTRICAL SMELL AND CABIN SMOKE DEVELOPED. START WAS ABORTED. FOUND CABLE TERMINAL END BURNT AT REVERSE CURRENT RELAY (RCR) POST. REPLACED TERMINAL END AND RCR REPLACED WITH NEW. SDR CA081030002Seal · wrong part(CAN) THIS PROBLEM WAS IDENTIFIED WHILE CARRYING OUT ROUTING MX ON AMPHIBIAN FLOAT MAIN WHEELS. THE MFG PARTS BOOK SPECIFIED WHEEL GREASE SEAL THAT WHEN INSTALLED WERE 0.010 TOO SMALL OF A DIAMETER, CAUSING THE SEAL TO FALL OUT OF POSITION. HAVE CONTACTED THSDR S9BA2008029Turbine · damagedRIGHT ENGINE MAKES NOISE WHEN PROP MOVED BY HAND. REMOVED AND REPLACED RIGHT ENGINE AND PROPELLER AS A QEC ASSEMBLY. SPLIT ENGINE AT C-FLANGE AND FOUND POWER TURBINE RUB.SDR CA081017002Csu · malfunctioned(CAN) THE ACFT WAS IN CRUISE FLIGHT WHEN THE TORQUE ON THE RT ENGINE SURGED AND THE PROPELLER BEGAN TO FEATHER. AS THE POWER WAS BROUGHT BACK THE PROPELLER STOPPED FEATHERING. A PRECAUTIONARY ENGINE SHUTDOWN WAS PERFORMED AND THE ACFT RETURNED TO BASE WITHOUT SDR S9BA2008028Counterweight · looseLEFT PROPELLER BLADE NR 3 COUNTER WEIGHT LOOSE. BOTH MOUNTING BOLTS WERE INSTALLED WITH LOCKING PINS. REMOVED AND REPLACED PROPELLER. SENDING PROPELLER TO REPAIR STATION FOR EVALUATION. INSPECTED ALL AIRCRAFT IN FLEET FOR LOOSE PROPELLER WEIGHTS. NONE FOUSDR CA080924010Leg Assy · cracked(CAN) DURING THE 12 MONTH INSPECTION OF THE MLG WHICH CONSISTS OF INSPECTING THE WELDS FOR CRACKS, A CRACK WAS DETECTED ON THE BOTTOM OF THE AFT ATTACH TUBE APPROX 5 INCHES FROM THE AFT GEAR ATTACH FITTING. (TC NR 20080924010)SDR CA080924009Attach Fitting · cracked(CAN) DURING THE 12 MONTH INSP OF THE MLG WHICH CONSISTS OF INSPECTING THE WELDS FOR CRACKS, A CRACK WAS DETECTED ON THE BOTTOM OF THE AFT ATTACH TUBE APPROX 5 INCHES FROM THE AFT GEAR ATTACH FITTING.SDR 2008FA0000696Beta Ring · brokenBETA RING CRACKED, BROKEN. PROPELLER WAS INVOLVED IN PROP STRIKE AT MID STATION OF BLADE NR 2 BY A FOREIGN OBJECT. MALFUNCTION FOUND 3 HOURS FLIGHT TIME AFTER LOCAL REPAIR. (K)SDR 2008FA0000695Rod · brokenBETA ROD CRACKED, BROKEN. PROPELLER WAS INVOLVED IN PROP STRIKE AT MID STATION OF BLADE NR 2 BY A FOREIGN OBJECT. MALFUNCTION FOUND 3 HOURS FLIGHT TIME AFTER LOCAL REPAIR OF BLADE. (K)SDR 2008FA0000615Ring · brokenBETA RING CRACKED, BROKEN. PROPELLER WAS INVOLVED IN PROP STRIKE AT MID STATION OF BLADE NR 2 BY A FOREIGN OBJECT. MALFUNCTION FOUND 3 HOURS FLIGHT TIME AFTER LOCAL REPAIR OF BLADE. (K)SDR 2008FA0000614Rod · brokenBETA ROD CRACKED, BROKEN. PROPELLER WAS INVOLVED IN PROP STRIKE AT MID STATION OF BLADE NR 2 BY A FOREIGN OBJECT. MALFUNCTION FOUND 3 HOURS FLIGHT TIME AFTER LOCAL REPAIR OF BLADE. (K)SDR CA080807005Hinge Fitting · mismanufactured(CAN) THE HINGE ARM ASSY WAS RECEIVED FROM THE OEM WITH THE BONDING STRAP AND TAB INSTALLED ON THE UPPER ARM OF THE ASSY WHICH IF INSTALLED WOULD RESTRICT TRAVEL OF THE ELEVATOR. THE BONDING STRAP IS A FIXED LENGTH AND RIVETED IN PLACE. ADDITIONALLY TO MAKE THSDR S9BA2008027Longeron · crackedLT ENG NACELLE INBOARD LONGERON CRACKED 10.5 INCHES AFT OF THE FWD END. REMOVED AND REPLACED LT ENG INBOARD LONGERON IAW AC 43.13-1B CH 4, RD 6-54-036. (S)SDR S9BA2008026Longeron · crackedRT HAND NACELLE INBOARD LONGERON CRACKED 10 1/2 INCHES AFT OF THE FWD END. REMOVED AND REPLACED RT HAND INBD LONGERON IAW AC 4313-1B CH 4, RD 6-54-036 AND VERIFIED MOD 6/1655 IS INSTALLED PER AD 80-13-12 R1. (A)SDR CA080806009Drive Assy · stripped(CAN) DURING CLIMB OUT AT 800 FEET ALTITUDE THE ACFT SUDDENLY STARTED TO SHAKE VIOLENTLY. THE PILOT ABORTED THE CLIMB, PROCEEDED STRAIGHT AHEAD FOR 4 MILES TO A LANDING STRIP AND LANDED SAFELY WITH NO INJURIES TO PERSONS ON BOARD. UPON INVESTIGATION AS TO THE SDR S9BA2008025Bellcrank · wornDURING AD 89-24-06 FOUND ELEVATOR BELL CRANK WORN. REMOVED AND REPLACED ELEVATOR BELL CRANK. NO OTHER DEFECTS NOTED. (S)SDR CA080704002Rod · worn(CAN) DURING AN INSPECTION ON ACFT, IT WAS DISCOVERED THAT THE LT INBD CHORD-WISE FLAP ROD WAS RUBBING AGAINST THE SPAN-WISE ROD. ONCE THEY WERE REMOVED FROM THE ACFT, IT WAS NOTED THAT THE SPAN-WISE ROD HAD A GROOVE WORN IN IT FROM THE OTHER ROD. A NEW SPAN-WSDR 2008FA0000520Jackscrew · damagedFOUND SCREW-DRIVE INTERNAL THREADS STRIPPED AND SAFETY SPLIT, PIN MISSING. PILOT HAD DIFFICULTY CONTROLLING ELEVATOR. PART HAD 196.2 IN SERVICE, SINCE REPAIR. RECOMMENDED TO INSPECT LT ELEVATOR TRIM TAB FOR EXCESSIVE PLAY IAW MM AS PART OF PREFLIGHT AND EVESDR S9BA2008024Blade · wornUNUSUAL NOISE NOTED IN COMPRESSOR SECTION (NR 2 ENG) UPON START UP. REMOVED ENGINE FROM SERVICE, ENGINE RETURNED TO ENGINE SHOP, FOUND 1ST STAGE BLADE RUB. ENGINE PENDING REPAIR. (K)SDR S9B2008F00001Compressor · noisyUNUSUAL NOISE NOTED IN COMPRESSOR SECTION NR 2 ENGINE, UPON START UP, REMOVED ENGINE FROM SERVICE WILL CLOSE SDR WHEN SOURCE OF NOISE IS FOUND AND CORRECTED. (K)SDR CA080612004Line · mismanufactured(CAN) A NEW FUEL TUBE ASSY WAS TO BE INSTALLED BETWEEN FUEL CELL NR 5 AND NR 8 AS PART OF THE MOTIVE FLOW SYS. THE INSTALLER FOUND THE TUBE ASSY TO BE ONE INCH TOO LONG FOR THE LOCATION.SDR CA080612003Line · mismanufactured(CAN) A NEW FUEL TUBE ASSY WAS TO BE INSTALLED BETWEEN FUEL CELL NR 4 AND NR 6. THE INSTALLER FOUND THE TUBE ASSEMBLY TO BE .7500 INCHES TOO SHORT FOR THE LOCATION.SDR S9BA2008022Float · leaking"OPEN" LEFT FLOAT BAY NR 6 LEAKING. REMOVED AND REPLACED FLOAT. WILL UPDATE AFTER FLOAT INSPECTION, EMERGENCY MEASURE EXECUTED NO. AIRCRAFT GROUNDED. FLIGHT NA.SDR S9BA2008021Mount · failedRT SPINNER NOTED MISALIGNED. REMOVED AND REPLACED TOP ENGINE MOUNT INSPECTED ALL RIGGING AND WIRING. EMERGENCY MEASURES EXECUTED, RETURNED TO DOCK. AIRCRAFT GROUNDED, RETURNED TO SERVICE NEXT DAY. FLIGHT NR 189SDR S9BA20080020Adapter · cracked(CLOSE) LT AFT HORIZONTAL WEB ADAPTER CRACKED FOUND DURING SB 454 PART A
EMERGENCY MEASURES EXECUTED. AIRCRAFT GROUNDED, REMOVED AND REPLACED LT AFT WEB ADAPTOR.SDR S9BA20080019Longeron · crackedRT ENGINE, OB NACELLE LONGERON CRACKED. REPLACED WITH FACTORY NEW PART IAW AC43.13-1B SECTION 4 PARA 4-57 FIG 4-6 AND 4-9. (PN C6W1512-S142) NO EMERGENCY MEASURES EXECUTED , AIRCRAFT GROUNDED.SDR S9BA200800018Channel · corrodedDURING CAMP INSPECTION, FOUND LT AILERON OB WEIGHT BALANCE CHANNEL CORRODED. REMOVED AND REPLACED WEIGHT AND BALANCE CHANNEL, AND STATIC BALANCED AILERON IAW SRM 57-50-21 PAGE 3 AND SRM RD6-57-085.SDR 2008FA0000285Pump · failedBOOST PUMP FAILS AT 11,000 TO 12,000 FT OF ALTITUDE. WORKS FINE ON GROUND. (K)SDR S9BA200800015Longeron · damagedDURING SCHEDULED 125HR INSPECTION FOUND: RT ENGINE NACELLE IB LONGERON DAMAGED FORWARD OF LEADING EDGE AT STATION 60.8. REMOVED AND REPLACED RT NACELLE IB LONGERON ASSY IAW AC 43-131B CHP7 EMERGENCY MEASURES EXECUTED: NO AIRCRAFT. GROUNDED: BEING REPAIRED DURSDR S9BA200800013Control Rod · corroded125 HR INSPECTION, EMERGENCY MEASURES EXECUTED, NO, AC GROUNDED. NO CORROSION FOUND ON RT FLAP INTERCONNECT ROD UNDER FLEXIBLE BOOT. ON IB END. REMOVED AND REPLACED CONTROL ROD.SDR CA080220001Rod End · bent(CAN) THE PILOT REPORTED A DEFECT NR 2582A: ABOUT 10 MINUTES AFTER TAKEOFF, THE RT ENGINE NR 2 THROTTLE LEVER WAS STUCK. WORKED THE THROTTLE BACK AND FORTH IN CRUISE 3 - 4 TIMES AND FOUND OK. ON FINAL APPROACH INTO ARRIVAL AIRPORT, THE NR 2 THROTTLE WAS DIFSDR CA080212001Adapter · cracked(CAN) UPON COMPLIANCE WITH SB 6/540 (WING-FRONT SPAR ADAPTER ASSEMBLY (P/N C6WM1027-1) INSPECTION FOR CRACKS) A CRACK WAS FOUND ON THE LT FRONT SPAR ADAPTER. REPLACED LT FRONT SPAR ADAPTER ASSY PN C6WM1027-1 WITH PN C6WM1027-3 IAW SB NR 61542. (TC NR 200802120SDR CA080212004Adapter · cracked(CAN) UPON COMPLIANCE WITH SB 6/540 (WING-FRONT SPAR ADAPTER ASSY (P/N C6WM1027-1) INSP FOR CRACKS) A CRACK WAS FOUND ON THE RT FRONT SPAR ADAPTER. REPLACED RT FRONT SPAR ADAPTER ASSY PN C6WM1027-1 WITH PN C6WM1027-3 IAW SB NO 61542. ALSO REPLACED WEB SUB ASSSDR CA080108007Release Cable · broken(CAN) THE RT POWER CONTROL WAS REPORTED STIFF. AFTER AN INSPECTION ON THIS AREA IT WAS NOTICED THE THE BETA RELEASE CABLE HAD BROKEN AND WAS CAUSING THE POWER CABLE TO BE STIFF. A NEW CABLE WAS PURCHASED AND CABLE WAS CHANGED. (TC NR 20080108007)SDR S9BA200700026Attach Bracket · crackedLT AND RT FORWARD STRUT FITTING CRACKED. REMOVED AND REPLACED LOWER STRUT TO FLOAT FITTINGS.SDR CA071228003Collar · dislodged(CAN) DURING AN ENGINE NR 2 SCHEDULE OIL CHANGE WHILE REMOVING OIL AT THE ACCESSORY GB DRAIN PLUG PORT HOLE, A METALLIC COLLAR HALF (P/N 3008779) FELL OUT. SUSPECTED THAT THIS COLLAR HALF HAD FALLEN OFF THE SCAVENGE OIL PUMP DRIVESHAFT. ENGINE REMOVED FROM AISDR 2007FA0001094Seat Back · brokenBOTH LOWER SEAT BACK BRACES BROKE JUST ABOVE THE WELDS, ABOVE WHERE THE FLANGE BOLTS ON TO THE SEAT BOTTOM. (K)SDR CA080116016Turbine Blades · fractured(CAN) DURING TAKEOFF ROLL, THE ENGINE LOST POWER. TAKEOFF WAS ABORTED AND AC RETURNED TO THE RAMP. INVESTIGATION BY MFG REVEALED FRACTURED COMPRESSOR TURBINE BLADES AND A FRACTURED FUEL BYPASS LINE. (TC NR 20080116016)SDR CA071129001Clevis Pin · missing(CAN) THIS RT ENGINE S/NPCE-50013, WAS IDENTIFIED TO HAVE THE OIL TANK DRAIN PLUG P/N 3004073, MISSING THE LOCKING PIN P/N AS121670. THIS COULD HAD LEAD TO THE COMPLETE LOSS OF ENGINE OIL, RESULTING OF ENGINE SHUTDOWN, IF THE PLUG HAD LOOSEN AND FALLEN AWAY FRSDR CA071115004Bolt · damaged(CAN) ENGINE MOUNT BOLTS THAT DAMAGED THE THREADS UPON REMOVAL. BOLTS WHERE INSTALLED ON 12/22/2005. (2) OF THE (4) TOP MOUNT BOLTS HAVE DAMAGED THREADS AND ARE NOT RE-USABLE. THREADS IN ENGINE CASE REQUIRE CLEAN-UP. (TC 20071115004)SDR CA071115011Plate · cracked(CAN) CRACK INDICATION FOUND IN A CORROSION PIT IN THE AFT ATTACH PLATE WHEN INSPECTING IT IAW SB 454. (TC NR 20071115011)SDR CA071115010Rib · cracked(CAN) RIB FLANGE FOUND CRACKED ON IB SIDE WHERE IT IS RIVETED TO THE TOP SKIN CORRUGATIONS. CRACKING FOUND WHEN INSPECTING RIBS 8-22 IAW MFG STRUCTURAL LIFE LIMITS. (TC NR 20071115010)SDR S9BA200700024Wire · shortedLT GENERATOR WOULD NOT COME ON-LINE AFTER START. FERRIED AC BACK TO BASE SSB. FOUND SHORTED WIRE ON GEN. FIELD RELAY DUE TO LACK OF HEAT SHRINK TUBING ON SOLDERED TERMINAL JOINT.SDR CA071018004Adapter · misinstalled(CAN) WHILE REMOVING ATTACHMENT ADAPTER P/N C6FSM1814-21, IT WAS NOTED THAT THE RIVETS INSTALLED IN THE VERTICAL WEBS TO ADAPTER WERE THE INCORRECT TYPE. THE RIVETS REMOVED FROM THIS ADAPTER PLATE WERE A.D. RIVETS. THE CORRECT RIVET WOULD HAVE BEEN D.D. ADASDR CA071107005Cable · chafed(CAN) WHILE INSPECTING THE CONTROL CABLES IAW TRANSPORT, ALERT (SDA) AL-2007-03, THE ELEVATOR CABLE WAS FOUND CHAFED AT THE PULLEYS AT STA 262.0. THE LOCATION OF THE WEAR ON THE CABLE, IS DIRECTLY OVER THE PULLEYS WHEN THE CONTROL LOCKS ARE IN. (TC NR 200711SDR S9BA200700019Skin · corroded"OPEN" LT WING IB PLANK DOUBLER (STATION 30) CORRODED AT LEADING EDGE.
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