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 = 'DHC6' 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 = 'DHC6' 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 CA121011010Circuit Card · shorted(CAN) WHEN CARRYING OUT GROUND TESTS, THE LT PROP WOULD NOT COME OUT OF FEATHER AND WHEN THE NR 2 FWD LOW FUEL PRESSURE INDICATOR LIGHT CAME ON THERE WAS AN UNCOMMANDED FREQUENCY SWAP OF NR 2 COMM. THE PROBLEM FOUND TO BE A SHORT IN THE GENERATOR INPUT/OUTPUTSDR CA121012019Module · malfunctioned(CAN) WHILE THE ACFT WAS IN A CRUISE CONFIGURATION, THE FLIGHT CREW EXPERIENCED A MOMENTARY LOSS OF THE PILOTS AND CO-PILOTS PRIMARY FLIGHT DISPLAYS, PFD IN ADDITION TO THE LOSS OF THE LOWER MULTI-FUNCTION FLIGHT DISPLAY, MFD. AFTER A MOMENTARY LOSS OF APPROXSDR 2012FA0000628Stud · shearedNOSE GEAR ASSEMBLY REMOVED FOR A SCHEDULED INSPECTION. A STUD THAT IS PART OF THE STEERING COLUMN WAS FOUND SHEARED.SDR CA120803003Drive Shaft · sheared(CAN) ACFT LANDING, CREW HAD INDICATION GENERATOR LIGHT ON, PASSENGER INFORMED OF NR 2 ENGINE FUEL LEAKS. FOUND STARTER/GENERATOR OFF THE ENGINE, DAMAGING THE FCU, FUEL PUMP, STARTER/GENERATOR DRIVE AND STARTER/GENERATOR GEAR IN ACCESSORY SECTION OF ENGINE. SDR CA120724005Fitting · mismanufactured(CAN) MFG HAS DETERMINED THAT THE BORE AND THREADS OF THE FITTING HAVE BEEN MACHINED TOO DEEP RESULTING IN THE PART NOT CONFORMING TO THE DWG SPECIFICATION. MFG IS CONTINUING TO INVESTIGATE.SDR GCNA20120427035Switch · shortedUPON LANDING PILOT WAS INFORMED BY PASSENGER THAT TOUR STATION SEAT 6B HAD LOUD POPPING AND SMOKE WAS OBSERVED. MAINTENANCE INSPECTED AND FOUND NO SMOKE BUT ITEM DID SMELL HOT. TOUR STATION REPLACED. INSPECTED REMOVED TOUR STATION AND FOUND VOLUME CONTROL SSDR CA120423009Handle · failed(CAN) THIS DOOR HAND FAILED WHILE CLOSING THE MAIN AIR STAIR DOOR FROM THE OUTSIDE, THE HSG ASSY CRACKED. THE DEFECTIVE DOOR HANDLE WAS REPLACED WITH A NEW UNIT, FUNCTION TESTED AND THE ACFT WAS RETURNED TO SERVICE. THIS FAILURE OF THE DOOR HANDLE WAS REPORTSDR CA120413011Cable · wrong part(CAN) DISCOVERED BARREL FITTING ON TRIM CABLE MENTIONED ABOVE IS TO SMALL. PART IS AN STC PART, WAS MADE IAW STC DATA. THERE WAS AN ERROR ON THE ORIGINAL APPROVAL. INFORMATION FROM OEM MANUAL WAS USED FOR APPROVAL AND THERE WAS A TYPOGRAPHICAL ERROR IN THE OSDR UE5R201203280001Planetary Gear · misalignedIN THE PROCESS OF REPLACING 1ST STAGE SUNGEAR AND PLANET GEAR SET, A DEFECT IN THE BEARING INSTALLED IN ALL 3 PLANET GEARS WAS FOUND. THE BRONZE SLEEVE PORTION OF THE BEARINGS HAD ROTATED CAUSING MISALIGNMENT OF BEARING SCALLOPS. THE BRONZE SLEEVE SHOULD NOTSDR UE5R201202020012Planetary Gear · misalignedIN THE PROCESS OF REPLACING 1ST STAGE SUN GEAR AND PLANETARY GEAR SET, A DEFECT IN THE BEARINGS INSTALLED IN ALL 3 PLANET GEARS WAS FOUND. THE BRONZE SLEEVE PORTION OF THE BEARING HAD ROTATED CAUSING MISALIGNMENT OF BEARING SCALLOPS. THE BRONZE SLEEVE SHOULDSDR CA120130014Probe · corroded(CAN) OAT PROBE IS EXHIBITING SIGNS OF CORROSION. MFG IS INVESTIGATING THIS ISSUE WITH THE MFG OF THE PROBE.SDR UE5R201201170001Gear Set · misalignedWHILE REPLACING THE 1ST STAGE SUN GEAR AND PLANET GEAR SET TO COMPLY WITH AD 2011-25-12 AND SB-804 REV B, A DEFECT WAS FOUND IN THE BEARINGS INSTALLED IN THE REMOVED PLANET GEARS. THE BRONZE SLEEVE OF THE BEARINGS HAD ROTATED AND ALSO STARTED TO MOVE OUT OF TSDR CA120118013Control Cable · failed(CAN) FOUND THAT THERE IS POTENTIAL FOR THE AILERON CONTROL CABLE TO CHAFE ON THE WING ROOT RIB FAIRLEAD CAUSING PREMATURE CABLE WEAR.SDR UE5R201201030012Gear Set · misalignedIN THE PROCESS OF REPLACING 1ST STAGE SUNGEAR AND PLANET GEAR SET, A DEFECT IN THE BEARINGS INSTALLED IN ALL 3 PLANET GEARS WERE FOUND. THE BRONZE SLEEVE PORTION OF THE BEARING HAD ROTATED CAUSING MISALIGNMENT OF BEARING SCALLOPS. THE BRONZE SLEEVE SHOULD NOSDR CA111216009Handle · failed(CAN) HANDLE BROKE OFF OF AIRSTAIR DOOR WHEN CLOSING DOOR.SDR CA111124006Latch · loose(CAN) FOUND THE PIVOT PINS OF LATCH, CAN MOVE IN THE ASSEMBLY, THUS MAKING IT POSSIBLE FOR ONE END TO BECOME DISENGAGED FROM THE HOUSING.SDR CA111110007Adapter · damaged(CAN) FOUND A DRILL STRIKE HAS OCCURRED ON THE BOTTOM OF FITTING, PN C6WM1162-3/-4. DURING THE MFG OF NEW WINGS. MFG IS INVESTIGATING TO DETERMINE WHAT FURTHER ACTION IS REQUIRED.SDR CA111025013Strap · mismanufactured(CAN) DURING INSTALLATION OF STRAP, DISCOVERED THAT THE JOGGLE DOES CONFORM TO THE DIMENSIONS AS SPECIFIED BY THE DWG. THIS RESULTS IN INADEQUATE CLEARANCE FOR THE UNDERLYING STRUCTURE. SUBSEQUENTLY, THE JOGGLE WAS REWORKED TO MEET THE CORRECT SPECIFICATIONSSDR CA110808005Tube · corrodedDURING A RECENT FUEL SYS TEST ON ACFT, TUBE ASSY WAS FOUND TO BE LEAKING DUE TO A PIN HOLE SIZED BREACH IN THE FITTING WALL. FURTHER INVESTIGATION REVEALED THE FITTING AND TUBE HAD CORRODED DUE TO ANODIZE RESIDUE THAT MAY NOT HAVE BEEN THOROUGHLY RINSED DURINGSDR CA110715007Structure · misrepairedDETERMINED THAT -3 DIAMETER FASTENERS HAVE BEEN INSTALLED IN THE SIDE STRUCTURE ASSY ON STRINGERS 8, 9, 14, 15 AND 16 BETWEEN STN 111.8 STN 125.55. DWG C6FS2402 CALLS FOR -4 DIAMETER FASTENERS. INVESTIGATING FURTHER.SDR CA110715006Skin · misrepairedDETERMINED THAT -4 DIAMETER FASTENERS MAY HAVE BEEN INSTALLED IN AS MANY AS 4 RIB TO REAR SPAR JUNCTIONS AT STN 47.5 85.00 ON RECENTLY MFG WING BOX ASSEMBLIES. DWG C6W1002 CALLS FOR -5 DIAMETER FASTENERS IN THESE LOCATIONS. ISSUING A SB TO HAVE IN-SERVICE WISDR CA110603009Arm · chafedAT WS 172.2 THE LT INBD FOREFLAP OTBD HINGE ARM PN CAN RUB ON THE LT OTBD FOREFLAP INBD HINGE ARM WITH FLAPS IN THE FULLY EXTENDED POSITION WHEN A INBD DIRECTION SIDE LOAD IS APPLIED TO THE OTBD FOREFLAP.SDR CA110527007Radio · unserviceableOPERATOR HAS REPORTED THE MULTI MODE DIGITAL RADIO NR 2 AS UNSERVICEABLE. OPERATOR HAS ORDERED A WARRANTY EXCHANGE REPLACEMENT DIRECTLY FROM MFG.SDR CA110527006Wire · damagedDURING A TRAINING FLIGHT, A PUMP 1 FORWARD PRESSURE AMBER (CAUTION LEVEL) CAS MESSAGE APPEARED. SUBSEQUENT INVESTIGATION BY MX REVEALED EVIDENCE OF ELECTRICAL ARCING AND BURNING IN THE FUEL GALLERY. THE WIRE LEADING FROM THE RF (RADIO FREQUENCY) FILTER ON THESDR CA110412010Transponder · failed(CAN) TRANSPONDER NR 1 MODE S TRANSPONDER GENERATING THE CAS MESSAGE : TRANSPONDER 1 FAIL. RESETTING THE CIRCUIT BREAKER CLEARS THE MESSAGE BUT THEN AFTER CYCLING THE POWER FROM EITHER BATTERY OR GENERATORS OR GPU RESETS THE MESSAGE.SDR CA110329011Dau · failed(CAN) MEGGITT SENSING SYSTEMS HAS ISSUED A RECALL LETTER AGAINST P/N 85-302-1, DATA ACQUISITION UNIT. THE SPECIFIC FAILURE MODE WOULD BE THE LOSS OF DATA FROM ONE OR BOTH CHANNELS OF THE DAU, HOWEVER, THE LIKELIHOOD OF BOTH CHANNELS BEING AFFECTED AT THE SAMSDR CA110315016Sensor · false activation(CAN) DURING A TRAINING FLIGHT A CAS WARNING MESSAGE INDICATING AN ENGINE FIRE WAS DISPLAYED. THE ENGINE WAS SHUT DOWN AS A PRECAUTION AND THE A/C RETURNED TO BASE WITH OUT FURTHER INCIDENT. DURING SUBSEQUENT TROUBLE SHOOTING IT WAS DETERMINED THAT WHEN SDR CA110131007Display · malfunctioned(CAN) FOUND A POWER-UP ISSUE WITH THE START UP OF THE KDU-1080 DISPLAY UNITS. THE DISPLAY UNITS (DU`S) THAT ARE AFFECTED BY THIS PROBLEM INTERMITTENTLY FAIL TO BOOT-UP PROPERLY. AN AFFECTED DU WILL DISPLAY A BACK-LIT BLANK SCREEN WITHIN THE FIRST COUPLE SECONSDR CA110110014Dau · malfunctionedTHIS NR 1 DATA ACQUISITION UNITS WAS SENDING INAPPROPRIATE CAS MESSAGES, IE THE FUEL QUANTITY FAIL AMBER CAS MESSAGE APPEARED, THIS UNIT WAS REPLACED WITH A NEW PART AND SYSTEM WAS FUNCTION TESTED AND DEEMED SERVICEABLE.SDR CA100916009Lever · mismarkedCUSTOMER REQUIRED C6FS2665-1, RECEIVED FROM MFG (1)EA C6FS3648-1 MISIDENTIFIED AS C6FS2665-1 FROM WO-76093/1. MFG HAS CONTACTED END USER TO HAVE THE PART RETURNED AND REPLACED.SDR CA100825011Spring Strut · mismanufacturedPN C6CF1257-31, DOES NOT MEET THE DIMENSIONAL SPECIFICATIONS OF THE MFG DWG, THE OUTSIDE DIAMETER IS UNDERSIZED RESULTING IN DECREASED WALL THICKNESS. PN C6CF1257-31 IS A SUBORDINATE PART OF ASSY, PN C6CF1257-1. QTY 4 EA OF PN C6CF1257-1 WERE SOLD. MFG HAS SDR CA100706009Retainer · mismanufacturedPN C6W1130-39, SEAL, RETAINER, WING FENCE HAS BEEN MFG USING INCORRECT MATERIAL. INVESTIGATING TO DETERMINE IF FURTHER ACTION IS REQUIRED.SDR CA100705002Bungee · brokenDURING INSTALLATION BUNGEE CORD BROKE. HAD 2 REPORTS FROM 2 DIFFERENT CUSTOMERS FROM 1 BATCH OF PARTS. 20 PARTS IN TOTAL MADE UNDER THIS BATCH. NO REPORTS OF FAILURES FROM OTHER BATCHES. 7 PARTS WITH ONE CUSTOMER, THE REMAINING 11 REMOVED FROM STOCK. NO RSDR CA100621008Relay · failedDURING POST MX GROUND RUNS, LT GEN SWITCH WAS SELECTED OFF. IT WAS IMMEDIATELY NOTICED THAT THE RT ENGINE BEGAN TO SLOW DOWN WITH A RISE IN TEMPERATURE. BOTH ENGINES WERE SHUTDOWN AND ELECTRICAL POWER TURNED OFF. INVESTIGATION REVEALED THAT THE NR 1 REVERSE SDR CA100609008Rod · mismanufacturedQTY 4 RODS WERE MFG WITH A FASTENER MISSING, FROM 1 ROD END IAW THE DWG. MFG IS CURRENTLY INVESTIGATING THE CONFIGURATION OF 2 PUSH RODS INSTALLED ON THIS ACFT TO DETERMINE IF FURTHER ACTION IS REQUIRED. 2 ARE BEING RETURNED FOR REWORK.SDR CA100113004Duct · mismanufactured(CAN) DISCOVERED THAT 32 OF THESE DUCTS WERE MANUFACTURED WITH INCORRECT OUTER INSULATING COVER INSTALLED. THE BATCHES INVOLVED ARE: WO-58717/1, WO-59849/1, WO-65452/1, WO-65452/1.1, WO-66588/1, WO-67938/1, WO-74046/1, WO-77354/1. VIKING HAS PULLED EXISTING SDR CA090916003Lever · cracked(CAN) DURING BUILD UP OF THE AICRAFT CONTROL COLUMN, A NEW STEERING LEVER WAS TO BE INSTALLED. INSPECTION OF THE LEVER SHOWED SLIGHT SURFACE DISCONTINUITY AT THE STEERING CABLE BALL RECEIVER LOCATION. CLOSER INSPECTION REVEALED A CRACK RUNNING FROM THE OUTER FSDR CA090902004Indicator · damagedWHEN LIGHTED POINTER ASSY WAS INSPECTED PRIOR TO FLAP POSITION INDICATOR ASSY, TECH NOTED THAT LIGHT ASSY WAS HANGING LOOSE OUTSIDE THE PLASTIC SLIDE AS OPPOSED TO BEING IMBEDDED IN THE PLASTIC SLIDE. ASSEMBLING THE POINTER TO THE INDICATOR SCALE WOULD RENDER SDR CA090817001Stop · mismanufacturedONE INSP OF OUR 2ND PRODUCTION RUN OF THE RUDDER STOPS (P/N TBC6FS1837-3 AND TBC6FS1837-9) IT WAS DISCOVED THAT THE URATHANE WAS BONDED BACKWARDS TO THE ALUMINUM BASE. AFTER MAKING THIS FINDING THE FIRST PRODUCTION RUN WAS CHECKED AND THE SAME PROBLEM EXISTEDSDR CA090302010Mount · mismanufactured(CAN) IT WAS DETERMINED THAT DURING THE FORMING STAGE, THE PARTS BEING MFG UNDER WO-32387/1 WERE INCORRECTLY FORMED.SDR CA080722007Bushing · missing(CAN) BUSHINGS MISSING FROM WING PICKUP LUGS ON ORIGINAL FRAMES INSTALLED IN ACFT.SDR CA080714005Bolt · mismanufactured(CAN) TBAL HAD A CUSTOMER REPORT OF THE LOCK WIRE TEARING THROUGH THE LOCK WIRE HOLE DURING INSTALLATION ON 2 OF THE 4 PURCHASED DRAIN VALVE BOLTS. ALL BOLTS IN STOCK WERE PULLED FROM THE SHELF AND EXAMINED. THE BOLTS CONFORMED TO THE TBAL DRAWING. THE BOLTS SDR S9B2008F00000Fuse · burnedAIR CONDITION CABIN FAN INOPERATIVE ON HIGH, MAKES A BURNING SMELL ON LOW. REPLACED 3 BLOWN FUSES WITH NEW. GROUND OPS CHECK, NO ODORS OR DISCREPANCIES NOTED . (K)SDR S9BA200800016Attach Bracket · corrodedDURING CAMP INSPECTION, FOUND CORROSION ON LT AFT (SEA FIN) ATTACHMENT BRACKET. REMOVED AND REPLACED SEA FIN ATTACHMENT BRACKET. EMERGENCY DECLARED? NO, AIRCRAFT GROUNDED, REPAIRED DURING INSPECTION NO.SDR S9BA200800017Spar · corrodedDURING CAMP INSPECTION FOUND CORROSION ON LT AFT STABILIZATION SPARE WHERE THE SEA FIN ATTACHMENT BRACKET IS LOCATED. REMOVED AND REPLACED OUTER HORIZONTAL REAR SPAR IAW AC 43 13 1B CHP. 7. EMERGENCY DECLARED? NO AIRCRAFT GROUNDED? NOT REPAIRED DURING INSPECTISDR S9BA200800014Clevis Pin · missingFLT 170, HEARD A POP IN THE AREA OF THE FLYING WIRE. CLEVIS PIN AT LEFT UPPER FLYING WIRE FOUND MISSING UPON LANDING. REMOVED AND REPLACED FLYING WIRES PN 13A0200-079 UPPER FRONT DRAG FITTING 13A02469-001 AND DRAG WIRE SHIM PN 13A02078-002. EMERGENCY WAS NSDR S9BA20080010Rib · corrodedCPCP INSP, RT WING FWD RIB AT STA.85 CORRODED. REMOVED AND REPLACED RIB WITH NEW PART IAW AC43-14, CHAPTER 4 PARA 4-57.
SDR S9BA20080009Rib · corrodedCPCP INSPECTION, RT WING FWD RIB AT STA 72.5 CORRODED. REMOVED AND REPLACED RIB WITH NEW PART IAW AC43-14, CHAPTER 4 PARA 4-57.SDR S9BA20080006Longeron · corrodedCPCP INSPECTION, LT NACELLE LONGERONS CORRODED. REMOVED AND REPLACED LT AND RT LONGERON IAW SRM 57-30-00 AND AC43-14, CHAPTER 4 PARA 4-57.
SDR S9BA20080003Skin · corrodedCPCP INSPECTION, LT WING CORRUGATION AT WS 65 TO 125 CORRODED. REPAIRED CORRUGATION BETWEEN WS 65 AND 125 IAW SRM 57-30-00 FIG 4 AND RD6-57-077. EMERGENCY MEASURES EXECUTED? NO. AIRCRAFT GROUNDED? YES.
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