Schweizer SGS 2-33A
Service difficulty reports · 18
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 = 'SGS233A' 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 = 'SGS233A' 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 CA190614014Hinge · worn(CAN) AN INSPECTION OF THE RUDDER TOOK PLACE AFTER FIRST WAS FOUND. THE RIVETS THAT ATTACH HINGE TO RUDDER SPAR FOUND LOOSE. SERVICEABLE RUDDER INSTALLED. (TC# 20190614014)SDR CA190614013Hinge · worn(CAN) THE LOWER RUDDER HINGE ATTACHMENT RIVETS WORKED LOOSE WHICH ATTACH HINGE TO RUDDER . THIS WAS FOUND DURING 100 HOUR INSPECTION. THIS IS AN ORIGINAL PART SINCE NEW. SERVICEABLE RUDDER INSTALLED. (TC# 20190614013)SDR CA150513006Doubler · cracked(CAN) DURING ANNUAL INSPECTION, A CRACK WAS DISCOVERED RADIATING FROM THE BEND LINE RELIEF HOLE ON THE HINGE DOUBLER, PN 33501-40. ON THE LT OTBD AILERON, INBD HINGE, A NEW DOUBLER WAS INSTALLED & THE AILERON RETURNED TO SERVICE.SDR CA110504006Spar · misrepairedDURING INSPECTINO, PAINT WAS REMOVED FROM WING AND A LARGE AMOUNT OF FILLER WAS DISCOVERED NEAR THE WING TIP. UPON REMOVAL OF THE FILLER AN UNDOCUMENTED PATCH WAS DISCOVERED. UPON FURTHER INVESTIGATION IT WAS DISCOVERED THAT THE TIP RIB PN 33408-4 AND THE NESDR CA110504005Rib · misrepaired(CAN) AN UNDOCUMENTED REPAIR WAS FOUND ON THE LEFT HAND WING AT STATION 214.0. UPON REMOVAL OF THE PATCH THE RIB WAS FOUND TO BE BENT OVER. BOTH THE WING SKIN REPAIR AND THE RIB WERE NOT COMPLETED AS PER ANY APPROVED OR ACCEPTED DATA, AND WERE NOT RECORDED IN SDR AALA2009061900002Module · inoperativeMIA - EMERGENCY LIGHTS FOR ROWS 9 TO 15 INOPERATIVE. REPLACED MODULE FOR EMERGENCY LIGHTS AT ROWS 9 TO 15.SDR AALA2009061900001Battery Pack · dischargedMIA - EMERGENCY LIGHTS FOR ROWS 9 TO 15 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT ROWS 9 TO 15.SDR CA061201003Spar · cracked(CAN) DURING THE COMPANY 12 YEAR STRUCTURAL INSPECTION AND REPAIR PROGRAM (SIRP), A CRACK WAS FOUND ON THE RUDDER SPAR ON THE OUTER LT EDGE OF THE UPPER HINGE ATTACH POINT. (TC NR 20061201003)SDR CA061201002Spar · cracked(CAN) DURING THE COMPANY 12 YEAR STRUCTURAL INSPECTION AND REPAIR PROGRAM (SIRP), A CRACK WAS FOUND IN ON RUDDER SPAR ON THE OUTER LT EDGE OF THE UPPER HINGE ATTACH POINT. LPI INSPECTION WAS USED TO VERIFY THE CRACK (TC NR 20061201002)SDR CA021210004Shoe · broken(CAN) PIVOT END OF BRAKE SHOE BROKEN.SDR CA020731012Control Cable · frayed(CAN) ELEVATOR CONTROL CABLE FOUND FRAYED AT P/N 22A148-1 FAIRLEAD.SDR CA020731011Control Cable · frayed(CAN) RT ELEVATOR CABLE FOUND FRAYED AT P/N 22A148-1 FAIRLEAD.SDR CA010523032Bellcrank · cracked(CAN) AN INSPECTION WAS CALLED FOR AS INSTRUCTED IN A SPECIAL INSPECTION DND C-12-382-000/NS-016. UPON INSPECTION OF SUBJECT PART, IT WAS DETERMINED THAT THE PART HAD REJECTABLE INDICATIONS. SUBJECT PART WAS SENT FOR REPAIRS AND RETURNED TO SERVICE. FURTHER INSDR CA010523031Bellcrank · cracked(CAN) AN INSPECTION WAS CALLED FOR AS INSTRUCTED IN A SPECIAL INSPECTION DND C-12-382-000/NS-016. UPON INSPECTION OF SUBJECT PART, IT WAS DETERMINED THAT THE PART HAD REJECTABLE INDICATIONS. SUBJECT PART WAS SENT FOR REPAIRS AND ETURNED TO SERVICE. FURTHER INSSDR CA010523030Bellcrank · cracked(CAN) AN INSPECTION WAS CALLED FOR AS INSRUCTED IN A SPECIAL INSPECTION DND C-12-382-000/NS-016. UPON INSPECTION OF SUBJECT PART, IT WAS DETERMINED THAT THE PART HAD REJECTABLE INDICATIONS. SUBJECT PART WAS SENT FOR REPAIRS AND RETURNED TO SERVICE. FURTHER INSSDR CA010314024Control Cable · frayed(CAN) BEARING ASSEMBLY AFT END OF TORQUE TUBE ASSEMBLY, LT MOUNT NUTCONTACTING CABLE. SUSPECT ANGLE BLOCK (FAIRLEAD) AFT END OF TORQUE TUBE ASSEMBLY AMPLIFIED DAMAGE TO CAUSE CABLE WEAR IN EXCESS OF 50 PERCENT. FURTHER INVESTIGATION ONGOING BY SCHWEIZER.SDR CA991103016Bolt · cracked(CAN) NEW WING ATTACHMENT BOLTS NDT'D PRIOR TO INSTALLATION REVEALED THAT 9 OUT OF 24 BOLTS (AN 7-23A) WERE REJECTED. BOLTS ARE MADE OF ROLLED STEEL AND THERE WAS AN INDICATION OF AN INCOMPLETE ROLLING PROCESS. SUBMITTER STATED IT IS UNKNOWN IF THE SEAMS WERSDR CA980406002Tube · cracked(CAN) PRIOR TO RESKINNING, MAGNETIC PARTICLES CHECK OF TUBE REVEALED STRESS CRACKS.
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