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 = '177RG' 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 = '177RG' 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 CA040607001Wire · broken(CAN) PILOT EXPERIENCED NO GEAR DOWN AND LOCK INDICATION LIGHT AFTER GEAR HAD COMPLETED CYCLE. AFTER AN UN-EVENTFUL LANDING AND INSPECTION, FOUND NOSE GEAR DOWNLOCK SWITCH WIRE WAS BROKEN AT BASE OF SWITCH.SDR 2004FA0000346Rub Strip · missingDURING ANNUAL INSPECTION LANDING GEAR RETRACTION TEST WAS PERFORMED AND THE NOSE GEAR DOORS WOULD NOT FULLY CLOSE. INVESTIGATION FOUND THE TEFLON RUB STRIP ON THE NOSE LANDING GEAR DOOR ACTUATOR MISSING.SDR CA031023003Bearing · broken(CAN) ON APPROACH FOR LANDING PILOT SELECTED GEAR DOWN ANDHEARD A LOUD BANG FROM BEHIND HIM RECIEVING NO GREEN DOWN LIGHT THE PILOT ABORTED HIS LANDING. HE CIRCLED THE AIRPORT AND TRIED NUMEROUS TIMES TO GET HIS GEAR DOWN. FINALLY HE SELECTED GEAR DOWN AND DIDSDR CA031022011Bearing · broken(CAN) PILOT WAS COMING INTO LAND SELECTED GEAR DOWN. HEARD LOUD BANG FROM REAR OF A/C AND GOT NO GREEN DOWN LIGHT INDICATION. ABORTED APPROACH & TRIED SEVERAL TIMES TO GET GEAR DOWN, NO SUCCESS. PUT GEAR HANDLE DOWN & DID FLY-BY. TOWER REPORTED HE HAD NOSE GEASDR 2003FA0001039Bearing · meltedNR 2 CYLINDER CONNECTING ROD FAILED AT THE CRANKSHAFT DUE TO OIL STARVATION AOF THE CONNECTING ROD BEARING. POSSIBLE OIL QUICK DRAIN VALVE OPENED IN FLIGHT AND DEPLETED ENGINE OIL SUPPLY.SDR 2003FA0000951Stall Warning · malfunctionedSTALL WARNING SYSTEM FUNCTION TEST AT ANNUAL INSPECTION WAS CORRECT. SYSTEM WOULD NOT OPERATE WHEN PITOT HEAT WAS SWITCHED ON. REMOVED STALL SWITCH AND CLEANED CORROSION FROM GROUND. BOTH STALL WARNING AND PITOT HEAT WOULD OPERATE CORRECTLY THEN. PREVIOUSLSDR CA030604001Valve · broken(CAN) PILOT REPORTED HEARING A BANG DURING CLIMB, FOLLOWING BY PARTIAL POWER LOSS AND VIBRATION WAS FELT. AN EMERGENCY WAS DECLARED AND AIRCRAFT RETURN FOR AN UNEVENTFUL LANDING. INITIAL INVESTIGATION REVEALED NR 3 CYLINDER HAS A VALVE HEAD SEPARATED AND IS SDR 2003FA0000581Gps · failedGPS SCREEN WENT TOTALLY BLANK. UNIT STILL RECEIVING AND TRANSMITTING COMMUNICATION DATA. SCREEN FAILED 2-3 MINUTES AFTER POWER UP. REPORTED THAT HIGH VOLTAGE TRANSFORMER FAILED UNDER IFR FLIGHT COULD BE FATAL.SDR 2003FA0000465Bellcrank · failedNOSE GEAR FAILED TO EXTEND ON LANDING SUBSTANTIAL DAMAGE OCCURRED. JACKED AIRCRAFT, CYCLED GEAR TO UP POSITION WITH AFT LG DOORS DISCONNECTED. ON EXTENTION, NOSE GEAR FAILED ONCE AGAIN. MECHANICAL UPLOCK FAILED TO RELEASE. SUSPECT OUT OF ADJUSTMENT.SDR 0300719927Line · rupturedINBOUND TO RIC THE LEFT HYDRAULIC SYSTEM QUANTITY WENT TO ZERO AND PRESSURE WENT TO ZERO. CREW CONTINUED TO DESTINATION AND PERFORMED MANUAL GEAR EXTENSION ON APPROACH. ALL COM PROCEDURES COMPLIED WITH AND THE LANDING WAS UNEVENTFUL. MAINTENANCE INSTALLED GEARSDR 2003FA0000140Attach Fitting · crackedFOUND LT RUDDER STOP RIDING OVER HORN AREA. THIS CAUSED DEFLECTION OF HORN ATTACHMENT AND CRACK. STOP BOLTS NOT HITTING HORN SQUARELY, CAUSING HORN TO RIDE UP OR DOWN UNDER STOP BOLT. ASSURE STOP BOLTS HIT HORN SQUARELY.SDR 2003FA0000038Downlock Switch · shortedFOUND THAT RT MLG DOWNLOCK SWITCH TO BE STUCK IN THE CLOSED POSITION WHICH, WHEN COMBINED WITH THE LT MLG DOWNLOCK SWITCH OPERATING IMPROPERLY, LED TO A LANDING WHERE THE MAIN GEAR COLLAPSED WITH A GREEN DOWN AND LOCKED LIGHT.SDR 2003FA0000037Commutator · wornPUMP OPERATED SLOWLY. SENT FOR OVERHAUL WHICH SHOWED THAT MOTOR BRUSHES WERE WORN AND THE COMMUTATOR WAS WORN IRREGULARLY. LED TO SLOW OPERATION OF THE LANDING GEAR.SDR 11592Hub · crackedCENTER SECTION OF WHEEL FOUND CRACKED BOTH MAIN WHEELS. WHEELS REPLACE WITH NEW CLEVELAND TWO PIECE TYPE WHEELS.SDR 2002FA0001349Magneto · detachedON OCT 12, 2002 AT APPROX. 2030, AIRCRAFT WAS SUBSTANTIALLY DAMAGED WHILE EXECUTING AN ENGINE OUT, GEAR UP, FORCED LANDING, NEAR SOUTH VIENNA, OHIO. PILOT AND PASSENGER WERE SERIOUSLY INJURED. ACCORDING TO THE PILOT, HE WAS CRUISING AT 2500 FT, WHEN HE NOTICEDSDR 2002FA0001204Selector Switch · misinstalledPILOT INEVERTANTLY BUMPED MLG SWITCH ON SHORT FINAL WHILE MOVING THE TRIM WHEEL, CAUSING A GEAR-UP LANDING. THE SAFETY FAILED TO WORK ON MLG SWITCH. UPON INVESTIGATION FOUND THAT THE SWITCH KNOB WHEN SCREWED COMPLETLY ONTO SWITCH CAUSED THE SPRING LOADED SAFETSDR 2002FA0001219Spar · corrodedOBSERVED THE CARRY THRU SPAR CORROSION WHEN LOOKING AT THE AIRCRAFT. THIS ITEM HAD SURFACE CORROSION THAT HAS BLISTERING THAT COULD BE PICKED AT AND MOST OF THE SURFACE AREA HAD WHITE DUSTING AND DISCOLORATION INDICATING CORROSION THAT REQUIRES TREATMENT. CASDR 2002FA0001036Hydraulic Line · separatedHOSE ASSEMBLY SEPARATED AT SWEDGED END/ AT ACTUATOR NO CHAFFING OR OTHER APPARENT WEAR ON HOSE.SDR 2002FA0001034Spring · stretchedDURING LANDING GEAR RETRACTION TEST, NOSE GEAR WOULD NOT FULLY RETRACT. THE BELLCRANK WAS FOUND OVERCENTER, CAUSING THE ROLLER TO MISS THE UPLOCK HOOK AND RESTRICT THE NOSE GEAR TRAVEL. THE SPRING WAS FOUND STRETCHED AND NOT PROVIDING ADEQUATE TENSION. THE SDR 2002FA0000852Door · separatedALTERNATE AIR DOOR CAME LOOSE FROM PLENUM CHAMBER. DOOR WENT INTO FUEL SERVO INLET, CAUSING ENGINE TO QUIT.SDR RH62002F00000Alternator · shortedUNUSED RECTIFIER POST BECOME LOOSE AND FELL INTO BOTTOM OF ALTERNATOR CASE. VIBRATION CAUSED LOOSE BOLT TO SHORT STATOR WINDINGS AND INTERMITTENTLY CAUSE DISCHARGE SPIKE IN BUS SYSTEM SPIKE WOULD CAUSE AVIONICS TO TURN OFF AND LOOSE NAVIGATION INFORMATION.SDR 2002FA0000458Support · brokenPILOT REPORTED THAT THE LANDING GEAR PUMP MOTOR CONTINUED TO RUN AFTER THE GEAR WAS PUT IN THE DOWN POSITION AND THAT THE GEAR DOWN LIGHT DID NOT COME ON. THE PILOT MADE AN UNEVENTFUL LANDING AFTER A LOW PASS AND GROUND PERSONNEL VERIFIED THE LANDING GEAR APPSDR 2002FA0000119Axle · crackedDURING FLOURESCENT PENETRANT INSPECTION, FOUND CRACK IN RADIUS OF AXLE SHAFT (AREA 1A )SDR 2001FA0000371Landing Gear · frozenNOSE GEAR IN UP POSITION HAD HYDRAULIC LOCK. KEEPING THE NOSE GEAR IN THE UP POSITION EXTENDED GEAR, MAIN GEAR LOCKED DOWN, NOSE GEAR DID NOT FULLY EXTEND DUE TO HYDRAULIC LOCK IN THE RETURN LINE.SDR 2001FA0000056Actuator · failedDURING CRUISE FLIGHT PILOT REPORTED BUFFET AND LOSS OF GEAR UP INDICATION. PILOT SLOWED TO GEAR SPEED AND DESENDED TO VFR CONDITIONS AND RETURNED TO DEPARTURE AIRPORT. SELECTED GEAR DOWN AND COULD NOT GET GEAR DOWN INDICATION. EMERGENCY EXTENDED GEAR AND OBSDR 20010530CW001Bolt · missingNOSE GEAR COLLAPSED ON LANDING ROLL OUT, DOWN LOCK LINK BOLT(LOWER) WAS FOUND MISSING PN NAS4645A15, NO MEANS OF SAFETY MAY BE USED WITH THIS DESIGN, ONLY LOCTITE CV SEALANT AS STATED IN SERVICE MANUAL. PART HAD 5311 HOURS.SDR 20010613CW023Spar · corrodedDURING THE INSTALLATION OF SHOULDER HARNESS KITS THE HEAD LINER WAS REMOVED. CORROSION WAS PRESENT AT FORE AND AFT UPPER, SPAR CAPS AND SKINS. OWNER WAS ADVISED. FURTHER INSPECTION FOUND CORROSION PRESENT UNDER LEAD SHEETS IN THE SAME AREA. LEFT AND RIGHT SDR 20010604CW001Rib · crackedDURING THE INSTALLATION OF SHOULDER HARNESS KITS, THE HEADLINER WAS REMOVED. CORROSION ON CARRY THRU SPAR FORE AND AFT TOP SPAR CAPS AND SKIN WAS NOTICED. CORROSION WAS ALSO PRESENT AT LEFT AND RIGHT ROOT RIBS. LEFT ROOT RIB HAD SMALL CRACK. NO FURTHER ACTSDR 20001013SH005Seat Track · corrodedINTERGRANULAR CORROSION FOUND ON VERTICAL LEG OF SEAT TRACK STARTING AT LAST SEAT ADJUSTMENT PIN HOLE (APPROX 20.25 INCHES FROM MOST FORWARD HOLE). CORROSION STARTED AT AFT EDGE OF HOLE AND PROGRESSED AFT ONE INCH. SURFACE METAL ON RIGHT SIDE OF VERTICAL LEGSDR 20000828SH031Bolt · shearedLANDING GEAR RIGGING WAS BEING CHECKED. DISCOVERED BOLT SHEARED AT MOUNT ATTACH POINT, MAIN LANDING GEAR SUPPORT ASSEMBLY. REPLACED BOTH BOLTS. AC TT: 6,552.00 HOURS. (X)SDR 20000912SH021Rod End · failedWHEN PILOT SELECTED GEAR DOWN, HE HEARD A POP/BANG UNDER THE FLOOR AND THE MAIN GEAR FAILED TO EXTEND. ACFT WAS LANDED GEAR UP WITH MINIMAL AIRFRAME DAMAGE. INVEST REVEALED MAIN GEAR ACTUATOR ROD END BEARING PN S2049-6FG HAD FAILED AND SPLIT APART AT THE SPHSDR 20000613SH013Bracket · crackedTHREE OF FOUR BALANCE WEIGHT SUPPORT BRACKETS WERE CRACKED ALONG THE BEND RADIUS. CRACKS WERE 1.25 INCHES, 1.50 INCHES, AND 1.75 INCHES ON EACH. THIS WAS NOTICED DURING STABILIZER BEARING REPLACEMENT WITH THE STABLIZER OFF THE AIRCRAFT. SUBMITTER RECOMMENDESDR 20000613SH012Bracket · crackedTHREE OF FOUR BALANCE WEIGHT SUPPORT BRACKETS WERE CRACKED ALONG THE BEND RADIUS. CRACKS WERE 1.25 INCHES, 1.50 INCHES, AND 1.75 INCHES ON EACH. THIS WAS NOTICED DURING STABILIZER BEARING REPLACEMENT WITH THE STABLIZER OFF THE AIRCRAFT. SUBMITTER RECOMMENDESDR 20000613SH011Bracket · crackedTHREE OF FOUR BALANCE WEIGHT SUPPORT BRACKETS WERE CRACKED ALONG THE BEND RADIUS. CRACKS WERE 1.25 INCHES, 1.50 INCHES, AND 1.75 INCHES ON EACH. THIS WAS NOTICED DURING STABILIZER BEARING REPLACEMENT WITH THE STABLIZER OFF THE AIRCRAFT. SUBMITTER RECOMMENDESDR 20000531SH003Elt · failedELT UNIT RECEIVED FROM MANUFACTURER AS AN EXCHANGE UNIT. ELT FAILED TEST AFTER REINSTALLATION. NO SWEEPS COULD BE HEARD ON 121.5. AN OCCASIONAL SHORT ''CHIRP'' COULD BE HEARD, BUT NO SWEEPS. (X)SDR 20000330SH009Plunger · malfunctionedWHEN THE GEAR WAS RETRACTED, THE SOLENOID PLUNGER EXTENSION WAS NOT PULLING THE DOWNLOCK MECHANISM COMPLETELY OPEN. WHEN THE GEAR WAS THEN EXTENDED AND THE GEAR HIT THE DOWNLOCK MECHANISM, IT WOULD DRIVE IT OVERCENTER BACKWARDS. REPLACING WORN PARTS FIXED THSDR 20000531SH004Elt · failedELT FAILED TEST PER FAR 91.207. NO SWEEPS COULD BE HEARD ON 121.5. UNIT WAS REPAIRED FOR SAME PROBLEM 11 MONTHS EARLIER ON 1-19-99. (X)SDR 99ZZZX4098Hose · failedHOSE BLEW APART AT FITTING WHILE IN-FLIGHT. SHOWED NO OUTWARD SIGNS OF FAILURE. LOSS OF ALL HYDRAULIC FLUID. SUBMITTER SUGGESTED MANDATORY REPLACEMENT TIME OF HOSES BE ESTABLISHED BY MANUFACTURER.SDR 99ZZZX3409Elt · failedDURING INSPECTION IAW FAR 91.207, THE UNIT COULD NOT BE ACTIVATED BY MEANS OF THE 'G' SHOCK SWITCH.SDR 99ZZZX3740Engine · leakingAPPROXIMATELY ONE HOUR OPERATION AFTER COMING OUT OF MAINTENANCE WHICH INCLUDED OIL AND OIL FILTER CHANGE AND REINSTALLING AN OVERHAULED PROP AND PROP GOVERNOR, THE ENGINE OIL PRESSURE DROPPED, ENGINE OIL PRESSURE DROPPED, ENGINE OIL EXITED, AND THE ENGINE SEISDR 99ZZZX2652Resistor · burnedDURING ANNUAL INSP, SMOKE NOTICED COMING OUT OF RADIO STACK. INVEST SHOWED THE S2041-50-1.6 RESISTOR FOR THE CIGARETTE LIGHTER DAMAGED AND SMOKING. SMOKE AND BURN MARKS NOTED ON BOTH SIDES OF GLOVE BOX SIDEWALL WHERE RESISTOR WAS MOUNTED. THE NYLON LOCKING SDR 99ZZZX2380Tube · malfunctionAFTER 15 MINUTES FLIGHT TIME OF 1ST FLT AFTER ANNUAL, PILOT NOTICED PROP OVERSPEEDING AND ENG OIL PRESS DROPPING TO ZERO. PILOT ACCOMPLISHED SUCCESSFUL PARTIAL POWER, DOWNWIND, EMERG LANDING. ENG STOPPED WHEN ACFT HAD CLEARED RUNWAY. ENG COMPT AND BELLY COVSDR 99ZZZX1560Gasket · wrong partDURING 100-HOUR ANNUAL INSPECTION, MAGNETO TYPE BENDIX D2000 SERIES REMOVED FOR CONTACT BREAKER REPLACEMENT AND INTERNAL TIMING CHECK. MAGNETO REFITTING WITH LYCOMING GASKET P/N 62224 INSTEAD OF LW-12681. THE MAGNETO BECAME LOOSE AND BACKED OFF FROM THE ENGISDR 99ZZZX1013Rivets · looseFOUND ALL 4 AFT HIGH SHEAR RIVETS LOOSE, PN NAS1054-8-7 AND NAS1054-6-8 IN THE SUPPORT ASSY. REPLACED WITH OVERSIZED HIGH LOC RIVETS. FOUND DURING ANNUAL INSPECTION.SDR 99ZZZX1012Bearing · corrodedFOUND UPPER TRUNNION BEARING PN S1997-40G12 COMPLETELY RUSTED AND THE BARREL ASSY PN 2043003-4 UPPER BEARING SURFACE WORN WITH .1250 INCH GROOVE. FOUND DURING INSPECTION FOR NOSE WHEEL SHIMMY PROBLEM.SDR 99ZZZX420Engine · misoverhauledMISISNG OIL RESTRICTOR ORFICE AND LOW OIL PRESSURE. FACTORY OVERHAULED ENGINE FROM AVCO-LYCOMING WOULD NOT MAKE PROPER OIL PRESSURE AFTER INSTALLATION. PROPELLER WOULD NOT RESPOND TO PITCH CHANGES. AFTER SENDING PROPELLER AND GOVERNOR TO PROP SHOP, DISCOVERSDR 98ZZZX4568Switch · failedON GEAR RETRACTION, BOTH THE UP AND DOWN LIGHTS WERE ON. PLACED GEAR SELECTOR IN DOWN POSITION AND GEAR STAYED UP. WHEN EMG PUMP GIVEN STROKES, NOSE GEAR STARTED DOWN. THE PUMP THEN CAME ON AND GEARS STARTED TO EXTEND. WHEN THE NOSE GEAR LOCKED DOWN THE PUMSDR 98ZZZX4567Switch · failedON GEAR RETRACTION, BOTH THE UP AND DOWN LIGHTS WERE ON. PLACED GEAR SELECTOR IN DOWN POSITION AND GEAR STAYED UP. WHEN EMG PUMP GIVEN STROKES, NOSE GEAR STARTED DOWN. THE PUMP THEN CAME ON AND GEARS STARTED TO EXTEND. WHEN THE NOSE GEAR LOCKED DOWN THE PUMSDR 98ZZZX4516Air Door · looseOWNER OF AIRCRAFT SAID FUEL FLOW WAS LOW. RAN UP, OPS CHECKED FUEL FLOW AT 14 PSI AT FULL POWER. INSPECTED ACFT AND FOUND TWO BOLTS MISSING FROM THROTTLE CABLE MOUNT ON BOTTOM OF ENGINE AND ALTERNATE AIR DOOR LAYING IN THE AIRBOX ASSY. INSTALLED TWO NEW BOLSDR 98ZZZX4248Bolt · brokenDURING AN ANNUAL INSPECTION, THE NOSE GEAR DRAG BRACE ASSY KNEE JOINT BOLT WAS FOUND SHEARED IN HALF. THIS BOLT IS DRILLED AND ZERKED FOR LUBRICATING. THE BOLT WAS BROKEN AT THE CENTER HOLE WHERE THE GREASE COMES OUT INSIDE THE BRACE BUSHINGS. BOLT WAS REPL
Back to Cessna 177RG