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 = '172RG' 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 = '172RG' 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 2004FA0000725Pivot Assy · crackedIN FLIGHT THE LT LANDING GEAR WOULD NOT COME DOWN. THE PILOT WAS ABLE TO MANUALLY GET THE GEAR DOWN AND LOCKED FOR LANDING. UPON INVESTIGATION IT WAS DISCOVERED THAT THE LT MAIN LANDING GEAR PIVOT ASSEMBLY SHAFT WHERE THE ACTUATOR ATTACHES HAD BROKEN AND WHSDR 2004FA0000637Bushing · splitDURING 100 HR INSPECTION, FOUND BOTH LT AND RT MLG PIVOT BUSHINGS SPLIT AND LEAKING GREASE. THESE BUSHINGS ARE REQUIRED TO BE INSTALLED IAW AD2001-06-06, SB 90-1, SK 172-151. THE SRM HAS NOT BEEN UPDATED TO SHOW ANY DETAIL OF THIS STYLE BUSHING. NO INSPECTISDR 2004FA0000546Actuator · malfunctionedDURING A FLIGHT, THE PILOT REPORTED HEARING A LOUD POP WHEN THE GEAR WAS CYCLED DOWN. UPON INSPECTION OF THE LANDING GEAR, THE LT MLG ACTUATOR WAS FOUND TO BE CRACKED ALL THE WAY ACROSS THE LARGE BORE AT THE FORWARD BOLT HOLE AND THERE WERE TWO OTHER SMALL CRSDR 2004FA0000545Pivot · crackedWHILE REPLACING A BROKEN GEAR ACTUATOR THE PIVOT WAS REMOVED AND INSPECTED. A CRACK WAS FOUND IN THE LOWER RADIUS AT THE BOTTOM OF THE GEAR SPLINES. TO PREVENT THIS PROBLEM IT IS SUGGESTED THAT THE MLG PIVOTS BE REMOVED FROM THE AIRCRAFT AND INSPECTED EVERY SDR 2004FA0000510Alternator · detachedPILOT REPORTED HE THOUGHT ALTERNATOR THREW THE BELT. REMOVED THE COWLING, FOUND ALTERNATOR LYING IN ENGINE COMPARTMENT, WIRING INTACT, COOLING FINS TORN OFF BELT PULLEY, BELT SHREDDD. AN7-40A MOUNTING BOLT NOT FOUND. BELT ADJUSTMENT BRACKET AN5 ATTACH BOLT SDR 2004FA0000567Mount · crackedFOUND AT 100 HOUR INSPECTION. NOSE GEAR ACTUATOR MOUNT, CRACKED AFT OF NOSE GEAR ACTUATOR.SDR 2004FA0000547Rudder Pedal · damagedPILOTS REPORTED AFTER PERFORMING A SIMULATED WING FIRE MANUVER (A STEEP TURN TO THE LEFT) THEY HEARD A LOUD BANG AND THEN LOST CONTROL OF THE RUDDER. THE AIRCRAFT LANDED SAFELY. MAINTENANCE INSPECTED THE RUDDER SYSTEM AND FOUND THE WELD ASSEMBLY GEARS HAD (JSDR 2004FA0000539Mount · brokenNOSE GEAR COLLAPSED DUE TO PART FAILURE ON LANDING ROLL OUT. (NM07200406705)SDR AUS20040412Pipe · corroded(AUS) LANDING GEAR UP PIPE FROM GEAR SELECTOR HANDLE VALVE TO HYDRAULIC POWER PACK CORRODED WITH A SMALL PINHOLE LEAK. A FINE SPRAY OF HYDRAULIC FLUID CONTAMINATED THE REAR OF THE ADF RACK.SDR AUS20040262Gear · disintegrated(AUS) STARTER BENDIX DRIVE GEAR DISINTEGRATED ON START.SDR 2004FA0000120Balance Weight · missingRUDDER BALANCE WEIGHT WAS MISSING FROM IT'S LOCATION. UPON INSP OF RAMP AREA, MISSING WEIGHT ASSY WAS FOUND FROM TAXIWAY. RUDDER TAB, AC WERE DETERMINED TO NOT BE DAMAGED FROM PART DEPARTING ITS LOCATION. WEIGHT ASSY WAS INSP, CAUSE OF PART COMING OFF AC WAS RSDR 2004FA0000079Balance Weight · missingIT WAS NOTED THAT RUDDER BALANCE WEIGHT WAS MISSING FROM LOCATION IN TOP LE OF RUDDER. UPON INSP OF RAMP AREA, IT WAS RECOVERED FROM TAXIWAY. RUDDER TAB AND AC WERE UNDAMAGED FROM IT DEPARTING AC, WEIGHT ASSY WAS INSPECTED TO DETERMINE CAUSE OF DEFECT. SCREW ISDR 2004FA0000314Door · out of rigNG DOOR OB EDGE CAUGHT ON GEAR WELL BUMPERS AND PREVENTED NG DOORS FROM OPENING WHEN GEAR SELECTED DOWN. IT IS CAUSED BY DOORS BEING RIGGED WITH TOO LITTLE CLEARANCE, BUMPERS WEAR THIN AND ALLOW GEAR DOORS TO RAISE ON TOP OF BUMPER AND WEDGE DOORS. NOSE GEASDR 2004FA0000313Door · out of rigNOSE GEAR OB EDGE CAUGHT ON GEAR WELL BUMPERS AND PREVENTED NG DOORS FROM OPENING WHEN GEAR SELECTED DOWN. IT IS CAUSED BY DOORS BEING RIGGED WITH TOO LITTLE CLEARANCE, BUMPER WEAR THIN AND ALLOW GEAR DOORS TO RAISE ON TOP OF BUMPER AND WEDGE DOORS. NOSE GEASDR 2004FA0000312Bumper Block · wornNG DOOR OB EDGE CAUGHT ON GEAR WELL BUMPERS AND PREVENTED NG DOORS FROM OPENING WHEN GEAR SELECTED DOWN. IT IS CAUSED BY DOORS BEING RIGGED WITH TOO LITTLE CLEARANCE, BUMPERS WEAR THIN AND ALLOW GEAR DOORS TO RAISE ON TOP OF BUMPER AND WEDGE DOORS. NOSE GEARSDR 2004FA0000311Bumper Block · wornNG DOOR OB EDGE CAUGHT ON GEAR WELL BUMPERS AND PREVENTED NG DOORS FROM OPENING WHEN GEAR SELECTED DOWN. IT IS CAUSED BY DOORS BEING RIGGED WITH TOO LITTLE CLEARANCE, BUMPERS WEAR THIN AND ALLOW GEAR DOORS TO RAISE ON TOP OF BUMPER AND WEDGE DOORS. NOSE GEARSDR 2004FA0000049Piston · brokenRT MAIN LANDING GEAR ACTUATOR PISTON BROKE IN TWO PIECES ON GEARED PORTION. CAUSING RT GEAR TO FAIL TO LOCK IN DOWN POSITION. RESULT WAS GEAR UP LANDING.SDR AUS20031239Attach Fitting · cracked(AUS) NOSE LANDING GEAR ACTUATOR ATTACHMENT FITTING CRACKED IN TWO PLACES. FITTING HAD BEEN MODIFIED IAW AD/C170/58, SEB93-8 AND SK172-142.SDR 2004FA0000299Governor · malfunctionedWHILE ON CLIMB OUT AT 2500 RPM AND 25 INCHES, ENGINE RPM SUDDENLY WENT TO 3000 AND PILOT WAS UNABLE HAVE ANY EFFECT WITH PROPELLER CONTROL. AIRCRAFT RETURNED TO AIRPORT USING THROTTLE TO CONTROL RPM. ENGINE CONTROLS WERE ALL FOUND TO BE INTACT AND OPERATING SDR CA031028002Tube · melted(CAN) DURING A ROUTINE INSPECTION OF THE AIRFRAME IT WAS FOUND THAT THE SECTION OF PITOT TUBE IN THE WING NEAR THE PITOT TUBE ASSEMBLY WAS FOUND MELTED. THE REASON FOR THIS CONDITION WAS DETERMINED TO BE INTERFERENCE ON THE TUBE BY THE WIRING FROM THE PITOT HESDR 11032003002Bulkhead · crackedCRACKS IN UPPER LEFT BULKHEAD UNDER PILOT'S INBOARD RUDDER PEDAL TORQE TUBE PILLOW BLOCK, ALLOWED ABNORMAL FORWARD/AFT MOVEMENT OF RUDDER PEDAL TORQE TUBE. REPORTED TO MFG BY TELECON.SDR 11032003001Bulkhead · crackedCRACKS IN LOWER LEFT BULKHEAD UNDER PILOT'S INBOARD RUDDER PEDAL TORQUE TUBE PILLOW BLOCK, ALLOWED ABNORMAL FORWARD/AFT MOVEMENT OF RUDDER PEDAL TORQUE TUBE. REPORTED TO MFG BY TELECON. (AL03200407996)SDR 2003FA0000775Actuator · crackedAFTER TAKE OFF TOWER REPORTED RIGHT MAIN GEAR NOT FULLY RETRACTING. AFTER A NONEVENTFULL LANDING I INSPECTED THE MAIN LANDING GEAR ACTUATORS AND FOUND THE RIGHT ACTUATOR TO BE SEVERLY CRACKED AND THE LEFT ACTUATOR TO HAVE HAIRLINE CRACKS. A FERRY PERMIT WAS FISDR 2003FA0000902Muffler · crackedWHILE INSPECTING MUFFLER AND SHROUD IAW AD 83-14-04, A CRACK WAS FOUND AROUND A WELD ON THE AFT END OF THE CAN.SDR AUS20030696Housing · cracked(AUS) RT MAIN LANDING GEAR ACTUATOR BODY SEVERELY CRACKED FROM PINION GEAR ACCESS HOLE TO THE OUTER FACE OF THE ACTUATOR. SLIGHT CRACKING WAS ALSO FOUND FROM THE ACCESS HOLE TO THE NEEDLE BEARING HOUSING.SDR AUS20030664Control Cable · broken(AUS) LT FORWARD FLAP CONTROL BROKEN.SDR 2004FA0000083Fitting · crackedFITTING CRACKED ON IB SIDE. DISCOVERED ON 100 HOUR INSPECTION. NO RECOMMENDATION, EXCEPT, CLOSE INSPECTION, ONE TIME INSPECTION ANNUALLY.SDR CA030603005Audio Panel · misinstalled(CAN) CREW REPORTED BOTH VOR SYSTEMS WERE NOT FUNCTIONING COMPLETELY. VOR AUDIO SIGNAL COULD BE PICKED UP AND TO/FROM FLAG WORKED. INDICATOR NEEDLES WOULD NOT DEVIATE FROM CENTER. COMPONENTS FAILED TO DETERMINE SOURCE OF PROBLEM. A/C WAS SENT TO FACILITY WHERESDR 2003FA0000567Housing · crackedPILOT REPORTED HEARING LOUD POP. LT MLG WAS HANGING OUT OF WHEEL WELL. PUTTING GEAR SELECTOR IN DOWN POSITION, RT MAIN AND NLG EXTEND FULLY. LT WAS STILL HANGING LOOSE. ATTEMPT TO PUMP DOWN LT WITH EMERGENCY PUMP WAS UNSUCCESSFUL. A/C WAS PUT INTO HANGAR ASDR 2003FA0000485Actuator · crackedPILOT REPORTED HEARING A LOUD BANG WHEN LAND GEAR WAS RETRACTED. A/C LANDED WITHOUT INCIDENT. INVEST REVEALED MFG PN 1281001-3, RT MAIN GEAR ACTR BODY CRACKED THROUGH (PHOTOS). COMPLIED WITH SEB AT 5741.4 HRS. A/C TT. AD2001-06-06 HAS BEEN COMPLIED WITH. SDR 2003FA0000406Pivot Assy · crackedFOUND CRACK IN RIGHT MAIN GEAR PIVOT ASSEMBLY AT CASTING SEAM. AIRPLANE SAT FOR 8 YEARS ON THE COAST OF FLORIDA. CORROSION WAS A MAJOR FACTOR IN THIS CRACK. PLANE WAS REPAINTED AND CRACK WAS COVERED. PAINT WAS SPLITTING IN AREA. STRIPPED PAINT AND THE CRACK APSDR 2003FA0000484Actuator · crackedDURING A CHECK RIDE, THE PILOT EXAMINER REPORTED A CLUNKING NOISE AS THE GEAR WAS CYCLED. UPON INSPECTION AND REMOVAL OF THE RIGHT MAIN LANDING GEAR ACTUATOR, IT WAS FOUND TO BE CRACKED ALL THE WAY ACROSS THE LARGE BORE AT THE FORWARD BOLT HOLE. THE SECTOR SDR CA030409004Fitting · cracked(CAN) DURING SCHEDULED INSPECTION OF THE AIRCRAFT AND LANDING GEAR IT WAS NOTICED THAT THE FITTING WHICH ACCEPTS THE NOSE GEAR ACTUATOR ASSEMBLY WAS CRACKED. THE TWO CRACKS WERE LOCATED JUST OUTBOARD OF THEACTUATOR MOUNTING BOSSES AND EXTEND BACK FROM THE FORWSDR 2003FA0000266Pivot · crackedDURING A ROUTINE INSPECTION IT WAS NOTICED BY THE TECHNICIAN THAT THERE WAS A LARGE AMOUNT OF VERY THIN GREASE SEEPING OUT FROM AROUND THE MAIN LANDING GEAR ACTUATOR CAPS ON BOTH THE LEFT AND RIGHT SIDES. THE GEAR ACTUATORS AND PIVOTS WERE FOUND TO BE CRACKEDSDR 2003FA0000142Bushing · unsecureDURING 100 HOUR INSPECTION, TECHNICIAN FOUND RT MLG ACTUATOR CAP BUSHING, UNSEATED AND STICKING OUT OF THE ACTUATOR CAP. DURING RETRACT TEST, IT WAS FOUND THAT THE BUSHING NOW INTERFERED WITH THE BRAKE SWIVEL FITTING. THE CAP WAS REMOVED AND A NEW BUSHING WASDR 2003FA0000141Bushing · unsecureDURING 100HR INSPECTION, TECHNICIAN FOUND THE LT MLG ACTUATOR CAP BUSHING. UNSEATED AND STICKING OUT OF THE ACTUATOR CAP. DURING RETRACT TEST, IT WAS FOUND THAT THE BUSHING NOW INTERFERED WITH THE BRAKE SWIVEL FITTING. THE CAP WAS REMOVED AND A NEW BUSHING SDR AUS20021379Housing · cracked(AUS) LH MAIN LANDING GEAR ACTUATOR HOUSING CRACKED. ACTUATOR RACKSEPARATED FROM SECTOR GEAR.SDR 2003FA0000007Wheel · crackedDISCOVERED CRACK IN THE SEAT FOR THE WHEEL BEARING RACE IN THE NOSE WHEEL HALF DURING ANNUAL INSPECTION. DEFECT APPEARS TO HAVE BEEN CAUSED BY REPEATED INSTALLATION OF THE RACE OVER THE LIFE OF THE WHEELSDR AUS20021266Actuator · cracked(AUS) LH MAIN LANDING GEAR ACTUATOR BODY CRACKED FROM THE BEARING BOSSTO THE INTERNAL DIAMETER OF THE SECTOR GEAR ACCESS HOLE.SDR FPI2002F00013Actuator · crackedLEFT MAIN GEAR ACTUATOR FOUND CRACKED IAW AD.SDR FPI2002F00012Actuator · crackedRIGHT MAIN GEAR ACTUATOR FOUND CRACKED IAW AD.SDR 2002FA0001320Hose · looseTHE OIL RETURN HOSE FROM THE OIL COOLER WORKED ITSELF LOOSE AT THE OIL COOLER FITTING.SDR CMX2002F00000Actuator · brokenACTUATOR BROKEN. THIS BRAKE MAY BE THE RESULT OF A HARD LANDING.SDR CA030122008Cylinder · cracked(CAN) ENGINE RUNNING ROUGH. VISUAL INSPECTION OF ENGINE WAS DONE. FOUND NR 3 CYLINDER CRACKED FROM LOWER SPARK PLUG UP TO UPPER SPARK PLUG ON REAR SIDE. WHEN ENGINE WAS TORN DOWN, IT WAS FOUND THAT A COUNTERWEIGHT BUSHING WAS WORN PAST SERVICE LIMITS. CRANKSHASDR EL62002F00000Housing · brokenPILOT HEARD LOUD BANG IN FLIGHT, ACTUATED GEAR FOR CHECK, NOTED LEFT NOT WORKING. INSPECTION FOUND LEFT MAIN GEAR ACTUATOR HOUSING BROKEN IN HALF AROUND GEAR DRIVE SECTION.SDR 2002FA0000870Air Filter · misinstalledINSPECTED AIRCRAFT FOLLOWING PURCHASE FOR FLIGHT SCHOOL. DISCOVERED INDUCTION AIR FILTER INSTALLED BACKWARDS. HOUSING IS EVEN LABELED FOR AIRFLOW WITH AN ARROW. HOUSING WAS IN BACKWARDS ALSO. WITH ARROW POINTING FORWARD AWAY FROM THE CARB TOWARDS THE INSIDSDR 2002FA0001133Fitting · crackedTHE FUEL STRAINER ON THIS PARTICULAR AIRCRAFT IS NOT MOUNTED RIGIDLY TO THE AIRFRAME. THEREFORE IT IS SUPPORTED BY THE FUEL LINES ATTACHED TO IT. THE VIBRATIONS CAUSED THIS FITTING TO CRACK. MFG MM LATER MODELS USE BRACKET FOR MOUNTING.SDR 2002FA0000566Housing · crackedACCOMPLISHED 500 HR REINSPECTION OF THE LANDING GEAR ACTUATOR HOUSINGS. FOUND THE LEFT AND RIGHT HOUSINGS TO BE CRACKED. THE RIGHT HOUSING WAS REPLACED AT THE INITIAL INSPECTION WITH A USED, SERVICEABLE HOUSING P/N: 9882015-2. REPLACED BOTH HOUSINGS WITH NESDR AUS20020386Actuator · cracked(AUS) RT MLG ACTUATOR CRACKED. FOUND DURING INSPECTION IAW SEB01-2.SDR AUS20020385Pivot · cracked(AUS) BOTH LH AND RH MLG PIVOT ASSEMBLIES SUSPECTED CRACKED. DYECHECKING PIVOTS LATER DID NOT SHOW CLEARLY ANY DEFECTS. INSPECTION CARRIED OUT IAW AD/CESSNA 170/69.
Back to Cessna 172RG