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 MCCA202402150176Cable · brokenELEVATOR TRIM TAB CABLE BROKE AFTER TAKEOFFSDR DATA20181217001Amplifier · failedDURING CRUISE AT 6000 FT FROM SJU TO STT THE LEFT FUEL PRESSURE WARNING ILLUMINATED. RAN MEMORY ITEMS AND ENGINE SHUTDOWN CHECKLIST FROM QRH AND DECLARED AN EMERGENCY. LANDED SAFELY AND NO DAMAGE TO AIRCRAFT. SUBSEQUENT MAINTENANCE TROUBLESHOOTING DETERMINED TSDR DATA2016112301Engine · flamed outDURING FLIGHT, THE AIRCRAFT WAS LEVEL AT 8000 FEET WITH CRUISE CHECKS COMPLETED AND THE SCHEDULED POWER WAS SET. NO ABNORMAL INDICATIONS WERE OBSERVED BY THE CREW DURING CRUISE AND NO MAJOR POWER ADJUSTMENTS WERE MADE ENROUTE. WHILE STILL AT CRUISE POWER JUSSDR DATA2015043001Connector · looseLEFT INVERTER FAILURE IN FLIGHT. FOUND LOOSE CONNECTOR AT INVERTER, ADJUSTED & SECURED CONNECTOR. GND CHECKED GOOD.SDR DATA2015040101Fire Bottle · depletedAFTER TAKEOFF, UPON CLIMB OUT THROUGH 4200 FT IT WAS NOTICED THAT LT FIRE FAULT LIGHT ON CWP ILLUMINATED. CREW CONSULTED QRH & RESET CB WHICH HAD POPPED. IT WAS THEN NOTICED THAT BOTH LT ENG FIRE EXTINGUISHER INDICATORS INDICATED DISCHARGED CONDITION, WHITE.SDR DATA2015011001Transformer · overheatedAFTER CALLING V1, PILOT NOTICED BOTTOM PANEL RADIO LIGHTS GO OUT. UPON COMPLETING CLIMB CHECKLIST, ENTIRE RT SIDE PANEL LIGHTS WENT OUT & AIR CREW SMELLED SMOKE. AN EMER WAS DECLARED. ACFT WAS CLEARED TO LAND, WHICH IT DID WITHOUT INCIDENT & MET BY AIRPORT SDR DATA2014110701Cable · brokenON ROTATION FIRST OFFICER HAD TO USE FULL LT RUDDER PEDAL & WAS UNABLE TO MAKE RUDDER TRIM ADJUSTMENTS. LT ENGINE POWER WAS RETARDED TO COMPENSATE FOR LOSS OF TRIM CONTROL. ACFT RETURNED TO DEPARTURE FIELD WITHOUT ANY FURTHER INCIDENCE. FOUND RUDDER TRIM CASDR HSYA 2013072013Cable · brokenFLT 248, PILOT REPORTED THAT WHILE DESCENDING FROM 8000 TO 3000 FT APPROX 30 NM OF DESTINATION, THE ELEVATOR TRIM FAILED. DECLARED AN EMERGENCY, PILOT REPORTED THAT THE CREW "MUSCLED" THE ACFT WHERE THEY LANDED WITHOUT FURTHER INCIDENT. FOUND TRIM CABLE BSDR HSYA2013041113Governor · failedPILOT REPORTED LT ENGINE WOULD ONLY PRODUCE 1600 LBS OF TORQUE AT MOST. THE TAKEOFF WAS ABORTED AND ACFT RETURNED TO THE PARKING RAMP WITHOUT FURTHER INCIDENT AND MX WAS NOTIFIED. MX TROUBLESHOT ACFT AND PERFORMED THE FOLLOWING MX. TROUBLESHOOT PY LINES ANDSDR HSYA2013012800012Structure · corrodedDURING MX, CORROSION INSPECTION, FOUND CORROSION ON LT WING OTBD SIDE OF NR 1 NACELLE INBD T/E BETWEEN WS 160 & 175. MX REMOVED LT WING UPPER SKIN DOUBLERS AT WS 160 AT APPROX 7.5" FROM L/E SPAR AND APPROX 7.5" FROM THE REAR EDGE SPAR. ON REMOVAL AND FURTHESDR 2013FA0000007Unknown · odorWHILE ENROUTE, THE CREW NOTICED AN ELECTRICAL BURNING ODOR IN THE COCKPIT. A PRECATIONARY LANDING WAS MADE TO INVESTIGATE. MX INSPECTED BEHIND ALL CIRCUT BREAKER PANELS,UNDER THE FLOOR,AND IN BOTH BATTERY BOXES WITH NO INDICATION OF OVERHEATING OR BURNING OFSDR DATA2012000006Downlock Switch · out of adjustON APPROACH, CREW SELECTED LANDING GEAR DOWN. RIGHT MAIN SHOWED UNSAFE. CREW ABORTED APPROACH AND PERFORMED QRH PROCEDURES TO ATTEMPT TO REMEDY THE PROBLEM. CREW WERE UNABLE TO GET A GREEN INDICATION FOR THE RIGHT MAIN. CREW DECLARED AN EMERGENCY AND LANDESDR DATA201200000501Indication Sys · faultyON APPROACH, CREW SELECTED LANDING GEAR DOWN. RT MLG SHOWED UNSAFE. CREW ABORTED APPROACH AND PERFORMED QRH PROCEDURES TO ATTEMPT TO REMEDY THE PROBLEM. CREW WERE UNABLE TO GET A GREEN INDICATION FOR THE RIGHT MAIN. CREW DECLARED AN EMERGENCY AND LANDED WISDR HSYA2012100512Engine · failedAFTER LEVELING OFF AT 9,000 FT, CREW OBSERVED A FLAME COME OUT OF NR 1 ENGINE, FOLLOWED BY THE GENERATOR LIGHT ILLUMINATING, AND ENGINE SPOOLING DOWN. FOLLOWED EMERGENCY CHECKLIST AND SHUTDOWN NR 1 ENGINE IN-FLIGHT. ATTEMPTED TO RESTART NR 1 ENGINE PER EMERGENSDR HSYA201272512Downlock · contaminatedFOUND LT DOWNLOCK MECHANISM WOULD NOT RETRACT BECAUSE OF EXCESSIVE GREASE. CLEANED EXCESSIVE GREASE FROM DOWNLOCK MECHANISM PISTON AND PERFORM LANDING GEAR OPERATIONAL CHECKS. LANDING GEAR FULLY CYCLED UP AND DOWN EIGHT TIMES - MX PERFORMED IAW CMM 32-11-01SDR HSYA2012072512Landing Gear · malfunctionedPILOT REPORTED THAT AFTER TAKEOFF AND UPON RETRACTION OF THE LANDING GEAR, THE RT NOSE GEAR INDICATED UP AND LOCKED AND THE LT MAIN GEAR INDICATED DOWN AND LOCKED. PILOT ELECTED TO RETURN TO DEPARTURE. GEAR WAS SELECTED DOWN AND 3 DOWN AND LOCKED LIGHTS ILLUMSDR DATA2012053000003Display · failedAFTER TAKEOFF CREW NOTED SMOKE IN THE COCKPIT. CONTINUED CLIMB, DECLARED EMERGENCY AND DIVERTED TO ALTERNATE. MAINTENANCE DETERMINED SMOKE TO BE DUE TO FAILURE OF THE RADAR DISPLAY UNIT.SDR HSYA2012050412Bolt · failedDURING TAXI, RT POWER LEVER HAD SEVERE VIBRATION. RETURNED TO RAMP. INSPECTED NR 2 ENG & PROP. FOUND 3 PROP BOLTS FRACTURED AND/OR SHEARED. ACFT GROUNDED. PERFORMED ENGINE VIBRATION INSPECTION CHECK IAW MM 5-51-13. NR 2 ENG REDUCTION GEARBOX PROP MOUNTSDR MCCA2012F00001Wire · damagedPILOT SELECTED GEAR DOWN AND NEVER GOT A GREEN DOWN AND LOCKED INDICATION FOR THE NOSE GEAR. ALL OTHER INDICATIONS SUGGESTED THAT GEAR WAS DOWN AND LOCKED. ACFT MADE AN UNEVENTFUL LANDING. TROUBLESHOOTING BY MX FOUND WIRE ON LANDING GEAR ACTUATOR WAS STARTISDR HSYA2011100811Actuator · failedAFTER DEPARTURE, LEFT MLG DID NOT APPEAR TO CYCLE FROM GREEN TO NORMAL UP INDICATION. PILOT ADVISED RESELECTED LANDING GEAR LEVER TO DOWN IAW ABNORMAL CHECKLIST AND GEAR SHOWED 3 DOWN AND LOCKED INDICATION. ACFT DECLARED AN EMERGENCY AND CONTROL TOWER REPORTSDR DATA2011000003Downlock Switch · misriggedRIGHT MLG UNLOCKED INDICATION ON APPROACH. DECLARED EMERGENCY AND PERFORMED FLY-BY TO VERIFY GEAR DOWN. LANDED SAFELY. DETERMINED TO BE AN INDICATION PROBLEM. GEAR WAS DEFERRED PER MEL AND PINS INSTALLED TO LOCK GEAR DOWN. RIGHT DOWNLOCK MICROSWITCH WAS DSDR 2011FA0000584Indication Sys · malfunctionedRT MLG UNLOCKED INDICATION ON APPROACH. DECLARED EMERGENCY AND PERFORMED FLY-BY TO VERIFY GEAR DOWN. LANDED SAFELY. DETERMINED TO BE INDICATION PROBLEM. GEAR DEFERRED IAW MEL AND PINS INSTALLED TO LOCK GEAR.SDR HSYA2011082511Lamp · burned outON APPROACH, THE PILOT PUT THE LANDING GEAR HANDLE DOWN FOR LANDING AND THE RT MAIN GEAR INDICATOR FAILED TO ILLUMINATE. THE CREW EXECUTED A GO AROUND AND REQUESTED VECTORS IN ORDER TO ACCOMPLISH ABNORMAL CHECKLIST (DID NOT DECLARE AN EMERGENCY). AFTER A SUCSDR HSYA20100721102Skin · corrodedLT AND RT CEILING STA 584.93 HAS SKIN CORROSION, APPROX SIZE (5" X 9"). LT UPPER SIDE WALL STA 514 HAS SKIN CORROSION. REMOVED CORROSION, TREATED AREA AND INSTALLED 5.25" X 7.25" FABRICATED DOUBLER FROM 2024T3 .032. CLEANED ALODINED AND PRIMED, INSTALLED ISDR HSYA20100721101Strap · corrodedDURING 4800/9600 HOUR STRUCTURAL INSP THE FOLLOWING ITEMS WERE FOUND. RT FWD TENSION STRAP AT STA 238.17 HAS CORROSION DAMAGE. REMOVED CORROSION,TREATED AREA AND INSTALLED DOUBLER FABRICATED FROM 2024 T351 .190- SIZE (26" X 4"). REPAIRED IAW ENGINEERING REPORTSDR HSYA2010072110Window Frame · corrodedDURING 4800/9600 HOUR STRUCTURAL INSP THE FOLLOWING ITEM WAS FOUND. RT LOWER WINDOW FRAME RAIL-STA 30 HAS CORROSION DAMAGE. REMOVED CORROSION, TREATED AREA AND INSTALLED DOUBLER FABRICATED FROM 2024 T3 .063-SIZE (7" X 4"). REPAIRED IAW ENGINEERING REPORT NR 84SDR HSYA20100720101Skin · corrodedDURING 4800/9600 HOUR STRUCTURAL INSP, THE FOLLOWING ITEMS WERE FOUND. CORROSION DAMAGE ON FUSELAGE SKIN FOUND AT STA 213.2-FUEL TANK RT OF CENTERLINE. REMOVED CORROSION, TREATED AREA AND INSTALLED DOUBLER FABRICATED FROM 2024 T3 .032 - 6" X 9" IN SIZE AT STA SDR HSYA2010072010Skin · corrodedDURING 4800/9600 HOUR STRUCTURAL INSP, FOUND CORROSION ON FUSELAGE SKIN FOUND AT STA 146.2-FUEL TANK RT OF CENTERLINE. REMOVED CORROSION, TREATED AREA AND INSTALLED DOUBLER FABRICATED FROM 2024T3 .032 -10" X 6" IN SIZE AT STA 146.2 - (7) INCHES RT OF CENTERLINSDR HSYA2010071910Seat Track · corrodedLT FWD SEAT TRACK CORRODED AT STA 117.6 REQUIRES A 11 INCH SPLICE REPAIR- (REF SRM 53-00-00 PAGES 62 &64). LT FWD SEAT TRACK CORRODED AT STA 187.2 AND STATION 213.2 - REQUIRES A 36 INCH SPLICE REPAIR- (REF SRM 53-00-00 PAGES 62 & 64). LEFT AFT SEAT TRACK CORROSDR HSYA201002272Web · crackedDURING 4800/9600 HOUR STRUCTURAL INSP OF ACFT THE FOLLOWING ITEM WAS FOUND. WEB CRACK AT LT AFT AIR STAIR ENTRANCE. REMOVED DAMAGED WEB AND FABRICATED WEB FROM 2024 T3 .050 AND INSTALLED -WORKED COMPLETED IAW SRM 51-70-00.SDR HSYA20100227Angle · crackedDURING 4800/9600 HR STRUCTURAL INSP OF ACFT FOUND FOLLOWING ITEM. CRACK AT LT AFT DOOR FWD THRESEHOLD. REMOVED DAMAGED PARTS AND FABRICATED NEW PARTS (2) EACH ANGLES FROM 2024 T3 .032 AND (2) EACH CHANNELS FROM 2024 T3 .040. WORKED COMPLETED IAW SRM 51-70-00.SDR HSYA201002253Fitting · crackedDURING 4800/9600 HOUR STRUCTURAL INSP OF ACFT THE FOLLOWING ITEM WAS FOUND. CRACKED CLIP ON FRAME 146.2 AT RT OF CTR LINE. REMOVED CRACKED CLIP FROM FRAME 146.2. DUPLICATED SERVICEABLE CLIP FROM 2024 T3 .040 IAW SRM 51-70-00.SDR HSYA20100225Skin · corrodedDURING 4800/9600 HR STRUCTURAL INSP OF ACFT, THE FOLLOWING CORROSION WAS FOUND AND REPAIRED. CORROSION THROUGH SKIN AT FRAME/FUSELAGE STA 289.92-RT OF CENTERLINE EXTERIOR BOTTOM. REPAIRED BY REMOVING/TREATING CORROSION AND INSTALLING DOUBLER 2024 T3 .040 APPROSDR HSYA2010022310Longeron · crackedDURING 4800/9600 HOUR STRUCTURAL INSP, DISCOVERED LONGERON AT FUSELAGE STA 127 LT SIDE CRACKED APPROX 3 INCHES. REMOVED DAMAGED LONGERON FRAME AT FUSELAGE STA 127 LT SIDE. NEW PART FABRICATED AND REPAIR INSTALLED IAW REPORT NR 8173-1.SDR HSYA20100221Fuel Tank · corrodedDURING 4800/9600 HR STRUCTURAL INSP OF ACFT, THE FOLLOWING CORROSION WAS FOUND AND REPAIRED. CORROSION ON UPPER SKIN AFT FUEL TANK. REPAIRED AFT UPPER FUEL TANK SKIN BETWEEN STA 289.92 AND 340.46. INSTALLED 4 DOUBLERS, MADE FROM 2024 T3 .040- APPROX SIZES (6.5SDR HSYA20100220Bracket · crackedDURING 4800/9600 HOUR STRUCTURAL INSP THE FOLLOWING ITEMS WERE FOUND. ANGLE BRACKET CRACKED AT LT CTR WING OTBD AFT SPAR. REMOVED ANGLE BRACKET AND DUPLICATED BRACKET FROM 2024 T3 .050 AND INSTALLED IAW SRM 51-40-00 AND 51-70-00. ANGLE BRACKET CRACKED AT RT CTSDR HSYA2010021810Channel · crackedDURING 4800 AND 9600 HOUR STRUCTURAL INSP OF THE ACFT. INSP REVEALED 2 LOWER LT STUB WING HAT CHANNELS/RE-INFORCING STRAPS THAT WERE CRACKED.SDR HSYA2009100209Fcu · damagedNR 2 (RT) ENGINE FAILED AFTER LANDING. FUEL LEAKING FROM COWLING. TROUBLESHOOT NR 2 ENG AND FOUND FUEL CONTROL UNIT REAR PLUG O-RING DAMAGED. REMOVED AND REPLACED NR 2 ENGINE FUEL CONTROL UNIT IAW MM 73-20-00. LEAK AND OPS CHECKS GOOD. GROUND PERFORMANCE SDR 2009F00059Indicator · smokeDURING LEVEL OFF AT 5000 FT, CREW SMELLED AND OBSERVED SMOKE COMING FROM THE CAPTAIN'S SIDE GLARESHIELD. MX DETERMINED THE SMOKE CAME FROM THE CAPTAIN'S DME INDICATOR.SDR DATA200900001Hydraulic Line · rupturedIMMEDIATELY AFTER THE GEAR WAS SELECTED UP, BOTH THE HYDRAULIC LIGHTS CAME ON THE CENTRAL WARNING PANEL. THE GEAR WAS SELECTED DOWN. THREE RED WAS SHOWN ON THE GEAR INDICATION. AN EMERGENCY WAS DECLARED. THE EMERGENCY GEAR HANDLE WAS PULLED PER THE CHECK LSDR DATA200800012Fuel Sys · out of adjustDURING DESCENT TO DESTINATION AROUND 200AGL LT SIDE FUEL PRESSURE LOW LIGHT ILLUMINATED FOLLOWED BY LT ENG FLAMEOUT.SDR DATA200800011Engine · fireDURING CLIMB, PILOT REPORTS FLAME FROM ENGINE EXHAUST. NO FIRE WARNING OR DAMAGED NOTED ON ACFT. AIR TURNBACK TO DEPARTURE. ACFT LANDED WITHOUT INCIDENT.SDR DATA200800010Engine · surgesPILOT DECLARED A LT ENGINE FIRE WITH NO FIRE SYS ALARM DURING INITIAL CLIMB. FIRE BOTTLES DISCHARGED. FIRE EXTINGUISHED BY ITSELF WHEN ON APPROACH. NO SIGN OF FIRE DAMAGE IN OR AROUND ENGINE. SUSPECT COMPRESSOR SURGE NOTED BY VISIBLE FLAMES FROM EXHAUST STACKSSDR DATA200800000Unknown · unknownFLIGHT CREW STARTED THE RIGHT ENGINE FIRST BECAUSE IT USUALLY STARTS COOLER. THE ITT PEAKED AT 780 DEGREES AND STABILIZED AT 630. THE GS GENERATOR GAUGE WAS SLOW TO RISE. THE PROBLEM OCCURRED NOTICEABLE AT V2, 90KTS, IT WAS AT 830 DEGEES ITT. TAKEOFF WAS CSDR DATA200800004Line · leakingAT 40 NM FROM DEPARTURE AT CRUISE ALTITUDE OBSERVED A GRADUAL DROP IN LEFT ENGINE FUEL FLOW, % NG, TORQUE AND ITT. DROP STABILIZED AT ABOUT 80% NG AND 240 LBS/HR FUEL FLOW. DECISION WAS MADE TO RETURN TO SBA. AT 20 NM OUT FROM SBA LEFT ENGINE BEGAN TO SURGESDR DATA200800002Switch · out of adjustAFTER DEPARTING MYR, THE RED DOOR WARNING LIGHT ON CWP ILLUMINATED AT 600 AGL. AFTER PERFORMING THE LIMITS CHECKLIST THE PILOT TURNED ON THE CABIN LIGHT BECAUSE THE DOOR WARNING LIGHT REQUIRES IMMEDIATE ACTION. THE PILOT NOTICED A SMOKE/FOG BANK IN THE CABINSDR DATA200800003Transceiver · inoperativeAFTER TAKEOFF PILOT NOTICED SMELL OF SMOKE. PILOT ASKED COPILOT TO CONFIRM WHICH HE DID. NO SMOKE INDICATION OCCURRED. COPILOT CHECKED CARGO COMPARTMENT AND NOTICED WHITE SMOKE. SMELL OF SMOKE WAS STILL PRESENT. FLIGHT CREW DECLARED AND EMERGENCY AND RETUSDR DATA200800001Oil Cap · looseDURING CRUISE ABOUT 30 NM OUT MYR, THE RIGHT ENGINE OIL PRESS LIGHT WAS FLICKERING BETWEEN 90-140 PSI ALL THE WHILE DECREASING. WHEN IT DROPPED BELOW 90 PSI THE FLIGHT CREW REDUCED TORQUE TO 2000 PSI AND CONSULTED THE QRH. 46 NM FROM CAE, THE OIL PRESSURE GASDR HSYA20080101Line · rupturedJUST AFTER TAKEOFF, THE CREW REPORTED THAT THE NOSE LANDING GEAR WOULD NOT LOCK IN THE UP POSITION. SHORTLY AFTERWARDS BOTH OF THE HYDRAULIC SYSTEM LOW PRESSURE LIGHTS ILLUMINATED. THE CREW DECLARED AN EMERGENCY AND PERFORMED THE ABNORMAL PROCEDURES LIST FOR HSDR DATA200700011Engine · failedALL 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.
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