Short Bros SD3-30
Service difficulty reports · 126
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 = 'SD330' 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 = 'SD330' 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 DATA200700012Engine · shutdownALL ENGINE INDICATIONS APPEARED NORMAL. RIGHT LOW FUEL PRESSURE ANNUNCIATOR CAME ON. ABOUT 5-10 SECONDS LATER, RIGHT ENGINE QUIT. ENGINE FAILURE CHECKLIST WAS CARRIED OUT, ENGINE SECURED AND AIRCRAFT DIVERTED TO VAN NUYS.SDR HSYA20071102Fcu · inoperativeDURING CLIMB OUT THE CREW REPORTED THE LT ENGINE LOST POWER. THE LT ENGINE PROP RPM DROPPED TO 1200 AND THE BLUE FINE PITCH LIGHT BEGAN FLASHING ALONG WITH A DROP IN TORQUE. THE CREW ELECTED TO RETURN TO DEPARTURE AND LANDED WITH OUT INCIDENT. MX FOUND THE LTSDR DATA200700008Seal · blew outRIGHT ENGINE CAUGHT FIRE DURING ENGINE START. AIRCRAFT WAS ON THE GROUND BEFORE FLIGHT. EVIDENCE OF ENGINE OIL ON PROP BLADES AND FUSELAGE. REPLACED SEALS TO PRESSURE OIL TRANSFER TUBE TO POWER SECTION MODULE. NO FIRE DAMAGE WAS NOTED ON ENGINE OR AIRCRAFTSDR HSYA20070601Proximity Switch · out of adjustFLT 120-DURING APPROACH, CREW REPORTED RT MLG UNLOCK INDICATION AFTER SELECTING GEAR HANDLE TO THE DOWN POSITION. THE AIRCRAFT WAS DIVERTED, ATC DECLARED AN EMERGENCY AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MX FOUND THE RT MLG DOWNLOCK PROXIMITY SWITCH OUT OSDR DATA200700004Bolt · looseDURING INSPECTION OF AD 2006-22-12 TWO PROPELLER BOLTS WERE FOUND LOOSE. REPLACED PROPELLER BOLTS AND PROPELLER ASSEMBLY.SDR DATA200700001Audio Panel · intermittentNUMBER 2 VHF RADIO INOP. NUMBER 1 VHF RADIO INTERMITTENT. CLEANED F/O AUDIO SELECT PANEL CONNECTORS.SDR DAT2006F00007Gas Generator · poppedREPAIR STATION REPORTED THE ENGINE ASSEMBLY WAS TESTED TO VERIFY THE COMPLAINT OF COMPRESSOR STALLING. DURING THE ENGINE RUN UP, OIL WAS OBSERVED IN THE BLEED VALVE AREA. THE AGB AND OIL FILTER HOUSING WAS REMOVED AND FOUND A MISSING PACKING ON THE OIL FILTESDR DAT2006F00005Bolt · damagedDURING THE COMPLIANCE OF AD (SB A203A) ON LT PROPELLER, THE MECHANIC FOUND (1) LOOSE BOLT. AS REQUIRED BY AD, THIS PROPELLER WAS REMOVED IAW THE SD3-30 MM. AFTER REMOVAL OF THE PROPELLER THE PROPELLER AND ENGINE FLANGES WERE INSPECTED AND NO DAMAGE OF FRETTISDR DAT2006F00006Engine · malfunctionedDURING THE TAKEOFF ROLL THE FLIGHT CREW HEARD THE RT ENGINE POPPING WITH FLASHES OF LIGHT WITH A RAPID DECREASE IN TORQUE. THE TAKEOFF ROLL WAS ABORTED AND AC TAXIED CLEAR OF THE RUNWAY. A MECHANIC WAS DISPATCHED. ENGINE ASSY WAS REMOVED AND REPLACED WITH ASDR DAT2006F00003Transmitter · inoperativeDURING THE FLIGHT BACK, THE FLIGHT CREW NOTICED THE LT ENGINE HAD LOW OIL PRESSURE. UPON GOING THROUGH THE EMERGENCY PROCEDURES THE LT ENGINE WAS SHUTDOWN. THE FLIGHT CONTINUED WITH THE RT ENGINE. NO EMERGENCY WAS DECLARED. A SAFE LANDING RESULTED TO THE CSDR DAT2006F00001Radar · smokeCLIMBING THROUGH APPROX 4000 FT THE WEATHER RADAR SCREEN STARTED TO FLICKER THEN WENT BLANK. IT WAS ON THE (40 MILE) SETTING. AS I WAS TURNING IT TOWARDS (OFF) THE SCREEN CAME ON AGAIN. IT FLICKERED SOME MORE THEN THERE WAS A SMELL OF SOMETHING BURNING. IMSDR DAT2006F00000Line · chafedON INITIAL TAKEOFF AT APPROXIMATELY 200 FEET AGL BOTH HYDRAULIC LIGHTS CAME ON AND TOTAL SYSTEM PRESSURE WAS ZERO PSI. THE FLIGHT CREW EXECUTED THE CHECKLIST. EVENTUALLY THE RT SIDE PUMP BEGAN WORKING AGAIN. RETURNED AND MADE AN UNEVENTFUL LANDING. SENT RESDR DAT2005F00011Flange · failedDURING THE COMPLIANCE OF AD, SB, FRO THE RT SIDE PROPELLER, THE (8) PROP ATTACH BOLTS, FAILED THE DESCRIBED TORQUE CHECK AS DESCRIBED IN AD (SB). THE PROPELLER WAS REMOVED IAW MM. AFTER THE PROP WAS REMOVED, THE INSPECTION FOUND FRETTING ON THE PROP FLANGE, SDR DAT2005F00012Tire · deflatedTHE LT MAIN WHEEL ASSY DEFLATED DURING TAXI AFTER LANDING. A MECHANIC WAS DISPATCHED AND REMOVED THE DEFLATED LT MAIN WHEEL AND REPLACED WITH A SERVICEABLE MAIN WHEEL ASSY IAW MM. THE AIRCRAFT WAS RETURNED TO SERVICE. (K)SDR DAT2005F00009Wheel · deflatedTHE LT MAIN WHEEL ASSY DEFLATED DURING TAXI AFTER LANDING. MECHANIC WAS DISPATCHED AND REMOVED THE DEFLATED LT MAIN WHEEL AND REPLACED WITH A SERVICEABLE MAIN WHEEL ASSY IAW MM. THE AIRCRAFT WAS RETURNED TO SERVICE. (K)SDR DAT2005F00004Attach Bolt · looseDURING SCHEDULED MAINTENANCE OF COMPLYING WITH AD (PROP TORQUE) ON THE RT PROPELLER IN ACC`S HANGAR, (3) PROP ATTACH BOLTS WERE FOUND LOOSE, BUT NOT BROKEN. AD STATES WHEN LOOSE BOLTS ARE FOUND THE PROPELLER IS TO BE REMOVED AND INSPECTED, THE FLANGE MATING SSDR DAT2005F00002Gas Generator · leakingFLT CREW EXPERIENCED PROBLEMS WITH RT ENG. PRIOR TO CRUISING ALTITUDE, IT WAS NOTICED OIL LIGHT WAS FLICKERING ON AND OFF WHILE OIL PRESS GAUGE WAS OSCILLATING BETWEEN 90 PSI, 135 PSI. THOUGHT IT MIGHT HAVE BEEN ERROR WITH GAUGE. GAUGE CONTINUED WITH ITS OSSDR DAT2005F00001Engine · leakingON FINAL FLT OF DAY, CREW EXPERIENCED PROBLEMS WITH RT ENGINE. PRIOR TO CRUISING ALTITUDE IT WAS NOTICED THE OIL R LIGHT WAS FLICKERING, WHILE OIL PRESSURE GAUGE WAS OSCILLATING BETWEEN 90 PSI AND 135 PSI. GAUGE CONTINUED WITH ITS OSCILLATIONS, BUT THE RANGESDR DAT2005F00000Governor · failedWHILE ON THE RETURN FLIGHT, CREW EXPERIENCED RT ENGINE ABNORMALITIES. THE TORQUE INDICATION EXCEEDED THE RED LINE LIMITATION AND BECAME UNCONTROLLABLE. AT THE SAME TIME, A DRASTIC DECLINE IN PROP RPM (BELOW 900 RPM) WAS NOTED. BOTH INDICATIONS WERE NOT ADJUSDR DAT2004F00008Engine · failedDURING THE TAKEOFF ROLL, A LOUD BANG AND HIGH PITCH WHINE COULD BE HEARD FROM THE RT ENGINE. AC SURGED AND YAWED AND THE POWER LEVERS WERE RETARDED IMMEDIATELY. THE TAKEOFF WAS ABORTED AND THE RT ENGINE WAS SHUTDOWN. THE AC WAS RETURNED TO THE RAMP AT APPROSDR DAT2004F00003Bolt · crackedDURING SCHEDULED AINT AD86-06-02 (PROP TORQUE) WAS COMPLIED WITH ON THE LT SIDE. ONE PROP ATTACHMENT BOLT, PN B3339 WAS FOUND LOOSE AND ONE BROKEN. ALL EIGHT (8) PROP ATTACHMENT BOLTS (PN B3339) AND WASHERS (PNA20482) WERE REMOVED AND REPLACED WITH NEW ONES SDR DAT2004F00005Indicator · failedRETURNED AFTER TAKEOFF DUE TO LOW PROP RPM ON LT ENGINE. MECHANIC DETERMINED A BAD PROP GAUGE. REMOVED AND REPLACED WITH SERVICEABLE UNIT. OPS CHECK GOOD.SDR DAT2004F00006Line · leakingDURING CLIMB OUT, WHEN GEAR WAS RAISED, FLIGHT CREW HEARD A HIGH PITCH WHINE. IT WAS NOTICED THE HYD L AND HYD R LIGHTS WERE ILLUMINATED ON THE CWP WITH THE CONTENTS GAUGE AT ZERO THUS ALL HYDRAULIC FLUID WAS LOST. EMERGENCY CRUISE AND DESCENT CHECKLISTS WERSDR 2004F00403Line · leakingDURING THE CLIMB-OUT WHEN THE GEAR WAS RAISED, THE FLIGHT CREW HEARD A HIGH PITCH WHINE. IT WAS NOTICED THE HYD L AND HYD R ILGHTS WERE ILLUMINATED ON THE CWP WITH THE CONTENTS GAUGE AT ZERO THUS ALL HYDRAULIC FLUID WAS LOST. THE EMERGENCY, CRUISE AND DESCENSDR DAT2004F00004Bolt · crackedIAW SDR REPLACEMENT OF POWER SECTION AND PROPELLER FOR VIABRATION, ON 09/01/04 (7) OF THE (8) PROP ATTACHMENT BOLTS, PN B3339 WERE FOUND CRACKED. ALL (8) PROP ATTACHMENT BOLTS, PN B3339, AND WASHERS PN A2048-2 WERE REMOVED AND REPLACED WITH NEW ONES PURCHASEDSDR 2004F00322Governor · inoperativeHEARD AN ENGINE NOISE, SOUND CHANGE FROM RT ENGINE & CKD STATUS OF ENGINE & PRIMARY INSTURMENTS. RT ENGINE TORQUE GOING PAST REDLINE & INCREASING. ITT INCREASED SLIGHTLY THEN DROPPED TO 450 & DECREASING. CAPTAIN DECREASED RT ENGINE TORQUE 200 NR'S AT FIRST SDR 2004F00308Uplock Switch · inoperativeWHILE COMING BACK FROM PIA-ASW, MLG WAS LOWERED, DURING APPROACH CHECKS. NLG INDICATION DID NOT GO 'GREEN'. INITIATED MISSED APPROACH & WENT INTO HOLDING PATTERN. FLT CREW CARRIED OUT EMERGENCY CHECKLIST & LOWERED MLG THE EMERGENCY METHOD. DECLARED EMERGENSDR DAT2004F00002Control Valve · failedTHE BRAKES WENT OUT ON THE GROUND. THE FLIGHT CREW LOST CONTROL AND HIT ANOTHER AIRCRAFT. THE RIGHT WING TIP HIT THE RT VERTICAL STABILIZER ON OTHER AC. MECHANICS WERE DISPATCHED, THE RT WING TIP WAS REMOVED AND REPLACED. THE BRAKE CONTROL VALVE WAS ALSO RSDR DAT2004F00000Line · crackedLEAVING 4400 FEET, THE RT ENGINE TORQUE FELL FROM 3200 LBS TO 2000 LBS THEN TO 1500 LBS THEN STABILIZED AT 2000 LBS FOR A WHILE THEN WENT BACK TO 3000 LBS. THE FLIGHT CREW TURNED BACK AND CALLED DEC TO TELL THEM OF THE SITUATION. THE FLIGHT CREW ADVISED THE SDR DAT2004F00007Bolt · crackedDURING THE SCHEDULED MAINTENANCE AD86-06-02 (PROP TORQUE) WAS COMPLIED WITH ON THE RT SIDE. ONE PROP ATTACHMENT BOLT, PN B3339 WAS FOUND CRACKED. ALL (8) PROP ATTACHMENT BOLTS, PN B3339, AND WASHERS PN A2048-2 WERE REMOVED AND REPLACED WITH NEW ONES PURCHASESDR 2004F00214Control Cable · frozenON DESCENT INTO IKK, THE POWER LEVER STUCK, FROZE. THE CREW COULD NOT UN-STICK, THEREFORE HAD TO CONDUCT A PRECAUTIONARY ENGIEN SHUTDOWN PRIOR TO LANDING. THE LANDIG WAS UNEVENTFUL AND THE FLIGHT TERMINATED UNTIL REPAIRS COULD BE MADE. A MECHANIC WAS SENT TSDR 2004F00007O-Ring · damagedAIRCRAFT CLIMBED NORMALLY THROUGH 5000 FT WHEN LT OIL LIGHT ON CWP CAME ON. RIGHT AFTER CWP LIGHT CAME ON THE LT OIL PRESSURE GAUGE STARTED SHOWING AN ERRATIC INDICATION. POWER WAS REDUCED ON LT SIDE AND THERE WAS NO CHANGE WITH GAUGE. SHORTLY AFTER THAT CUSDR 2003F00260Bulb · burned outON APPROACH TO SDF, THE LANDING GEAR WAS PUT DOWN, HOWEVER, ONLY THE LT AND NOSE GEAR INDICATED IT WAS DOWN. THE CREW DECIDED TO GO AROUND AND CHECK THE PROBLEM. AFTER THE PROBLEM WAS CHECKED THE CREW DECIDED FOR THE RIGHT MLG WAS DOWN AND THE LIGHT BULB WASSDR 2003F00326Door · damagedDURING THE BEFORE START CHECKLIST, THE MAIN CARGO DOOR MI INDICATED CROSSHATCHED. THE FLIGHT CREW STOPPED THE CHECKLIST AND THE FIRST OFFICER OPENED AND CLOSED THE MAIN CARGO DOOR. THE ALL 7 DOORS MI'S INDICATED SHUT. THE FLIGHT CREW CONTINUED THE CHECKLISTSDR DAT2002F00002Governor · fluctuatesDURING THE SET UP FOR A CRUISE CLIMB CONFIGURATION THE PROP RPM WAS REDUCED TO THE NORMAL 1400 RPM WHEN THE RT PROP KEPT FALLING UNTIL IT STABILIZED AT 750 RPM WITH 4300 POUNDS OF INDICATED TORQUE. AFTER INCREASING AND DECREASING THE RT PROP AND POWER LEVELS SDR DAT2002F00001Blade · brokenLT ENGINE STARTED TO SHAKE AFTER START UP. THE CREW SHUTDOWN THE ENGINE AND EXITED THE AIRCRAFT. MAINTENANCE INSPECTED THE LT ENGINE AND FOUND 2 BROKEN PT BLADES WHICH CAUSED BINDING OF THE POWER SECTION. THE POWER SECTION IS BEING REMOVED AND REPLACED.SDR 2002F01120Engine · malfunctionedOGG - FLT 7672 - OIL PRESSURE FLUCTUATION, LOW OIL PRESSURE WHICH RESULTED IN AN EIFSD, AND A SUBSEQUENT AIR RETURN. INTERNAL COMPONENT FAILURE. UNDETERMINED AT THIS TIME AWAITING TEARDOWN REPORTS FROM OVERHAUL FACILITY. REPLACED POWER SECTION WITH SERVICEASDR 2003F00098Fuel Control · dirtyON FLT 42310, ON THE DESCENT INTO CWA THE FIRST OFFICER PULLED THE POWER BACK AND THE LEFT ENGINE WOULD NOT GO BELOW 2300 LBS OF TORQUE. THE CREW DECIDED TO PRECAUTIONARY SHUTDOWN THE ENGINE ON THE APPROACH INTO CWA. THE CWA ATC WAS NOTIFIED AND AN EMERGENCYSDR AVS2001F00000Tire · separatedAT 100 KTS AS AIRCRAFT WAS BECOMING AIRBORNE, A LOUD BANG FOLLOWED BY A STRONG SHUDDER WAS HEARD AND FELT. AFTER LANDING IT WAS FOUND THAT THE ENTIRE RECAP OFF THE MAIN WHEEL HAD SEPARATED FROM THE TIRE. INSPECTION REVEALED THAT THERE WAS NO BOND BETWEEN THESDR 2001FA0000313Pressure Switch · leakingWHILE SERVICING THE OXYGEN SYSTEM, THE HIGH PRESSURE TRANSDUCER SHAFT SEAL BLEW OUT. THIS PRESSURE SWITCH IS PART OF AN STC MODIFICATION TO CERTIFY THE AIRCRAFT AS A SD3-30, . THIS IS SECOND OCCURANCE OF THIS FAILURE. THE FIRST FAILURE WAS ASSUMED TO BE THASDR 20001130SH002Smoke Detector · malfunctionedSHORTLY AFTER DEPARTURE FROM FWD, THE SMOKE FWD CWP LIGHT ILLUMINATED. THE FIRST OFFICER LOOKED FOR EVIDENCE OF FIRE, NONE WAS FOUND. AN EMERGENCY WAS DECLARED WITH ATC AND THE AIRCRAFT LANDED WITHOUT INCIDENT. FLIGHT CREW DETERMINED THERE WAS AND HAD NEVERSDR 20000731SH006Line · brokenEXPERIENCED LEFT ENGINE FAILURE WHILE LEVELING AT MDA 1,140 FEET FOR THE LOC 15L AT TIMMERMANN. THE PILOT DECLARED AN EMERGENCY WITH MKE ATC. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE EMERGENCY WAS TERMINATED WHILE EXITING THE RUNWAY. MECHANIC FOUND PY LINSDR 20000620SH025Timer · malfunctionedCLE/CVG - EN ROUTE, A PRECAUTIONARY DIVERSION WAS MADE INTO NMV BECAUSE OF A BURNING SMELL IN THE COCKPIT. THE ATC WAS INFORMED, BUT AN EMERGENCY WAS NOT DECLARED. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE FIRE CREW INSPECTED THE AIRCRAFT. A MECHANIC WAS DSDR 20001120SH030Wire · disconnectedHNL - FLT 8676 - PILOT REPORTED COMM FAILURE ALL SYSTEMS. AIR TURNED BACK TO HNL, LANDED WITHOUT INCIDENT. MAINTENANCE DISCOVERED A WIRE DISCONNECTED AND SHORTED AT COPILOT''S MIC SWITCH. RE-SOLDERED WIRE TO TERMINAL. OPERATIONAL CHECKED NR 1 AND NR 2 COMMSDR 20000530SH002Wire · disconnectedHNL - FLT 8676 - PILOT REPORTED COMM FAILURE ALL SYSTEMS . AIRCRAFT TURNED BACK TO HNL AND LANDED WITHOUT INCIDENT. MAINTENANCE DISCOVERED A WIRE DISCONNECTED AND SHORTED AT COPILOT'S MIC SWITCH. RE-SOLDERED WIRE TO TERMINAL. OPERATIONAL CHECKED NR 1 AND NSDR 2000ZZZX628Landing Gear · lack of lubeTHE CREW GOT A GEAR UNSAFE LIGHT (RED) AND DECLARED AN EMERGENCY LANDING INTO BAF. THEY LANDED WITHOUT INCIDENT. A MECHANIC WAS DISPATCHED TO BAF. THE NOSE GEAR WAS MEL'D AND FLEW TO BGR. THE NOSE GEAR WAS CLEANED AND LUBRICATED. A RETRACTION CHECK WAS PERSDR 20000426SH031Skin · corrodedHNL - LOWER FUSELAGE SKIN CORRODED THROUGH CORRUGATED SKIN AT STA 350 - STA 364 AT CENTER LINE ZERO TO 4 LEFT. HIGHLY CORROSIVE OPERATING ENVIRONMENT, AGING AIRCRAFT. REPAIRED WITH INSERTION REPAIR PER THE SD3-30 SRM AND 43.13-1B. DOCUMENTED ON FORM 337. (SDR 2000ZZZX11Nlg · malfunctionedFLYING INTO WILMINGTON, THE CREW EXPERIENCED AN UNSAFE NOSE GEAR INDICATION. CREW TRIED TO HAVE TOWER VERIFY NOSE GEAR POSITION, BUT UNABLE TO. CREW TRIED NUMEROUS TIMES TO VERIFY POSTION BY MEANS OF EMERGENCY CHECKLIST. NONE OF THESE WERE SUCCESSFUL. AN ESDR 99ZZZX4554Control Cable · seizedUPON REACHING CRUISING ALTITUDE FROM PLB, THE THROTTLES ON THE RIGHT SIDE WOULD NOT ADVANCE OR RETARD IN-FLIGHT. THE CAPTAIN SHUT DOWN THE NR 2 ENGINE AND LANDED UNEVENTFULLY IN PLB.SDR 99ZZZX3575Fitting · corrodedFOUND SOME CORROSION OF JACK POINT FITTING BETWEEN SPAR AND SPAR CAP ON LT STUB WING. CONSULTED WITH MANUFACTURER FOR POSSIBLE TREATMENT OF REPLACEMENT. THEY RECOMMENDED CLEANING AND TREATMENT IF NOT MORE THAN 5 INCHES LONG. FITTING WAS REPLACED WITH NEW ON
Back to Short Bros SD3-30