N153GA
Service difficulty reports · 30
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
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 n_number = 'N153GA' AND registry_match = 'registration' 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 n_number = 'N153GA' AND registry_match = 'registration' 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 TIMA202207130008Engine · shutdownPS NORMAL THROUGH 10,000 FT. CLIMBING THROUGH ABOUT 10500 FT THE PILOT NOTICED THE RH TORQUE GAUGE BEGIN TO FALL, THEN THE RH OIL PRESSURE LIGHT CAME ON. PILOT FELT A YAW, WAITED ABOUT THIRTY SECONDS TO CONFIRM FAILURE, SECURED THE ENGINE AND RETURNED BACK TO SDR TIMA20211220002Unknown · unknownGOT SMOKE/HAZE IN THE COCKPIT ONCE LEVELED IN CRUISE. TURNED BACK TO BIL AND SHUT OFF THE BLEED VALVES. ONCE BLEED VALVES WERE OFF THE COCKPIT CLEARED. LANDED AND TAXIED WITH NO ISSUES.SDR TIMA20161213019Windshield · crackedTHE PILOT’S SIDE WINDSHIELD CRACKED DURING FLIGHT. THERE WAS A 3 INCH WIDE BAND OF SHATTERING OF THE OUTER LAYER THAT RAN FROM THE TOP TO THE BOTTOM OF THE WINDSHIELD ON THE INBOARD EDGE NEXT TO THE CENTER POST.SDR TIMA20130830009Skin · corrodedCORROSION FOUND ON BELLY OF ACFT UNDER ADF ANTENNA BS 183.25. REPAIRED.SDR KGBR507Y201105250Skin Panel · crackedCRACK IN SKIN PANEL .5 INCH FWD OF THE TRAILING EDGE, 4.5 INCHES TO 10.5 INCHES FROM THE INBOARD EDGE OF THE FLAP. ALSO ARE 2 CRACKS IN THE AREA OF THE INBOARD ATTACH BRACKET AREA AT THE OUTBOARD ACCESS HOLE, 13 INCHES OUTBOARD OF THE INBOARD EDGE, EACH AT APSDR TIMA2010000011Seat Track · corrodedLEFT SIDE SEAT RAIL CORRODED.SDR TIM2005F00000Blade · brokenAIRCRAFT DEPARTED AT CRUISE. THE LT ENGINE HAD AN EXPLOSIVE NOISE AND THE LT ENGINE SEIZED. PRE-INSPECTION OF ENGINE INDICATES LOSS OF CT BLADE. (K)SDR 2005FA0000006Blade · brokenAIRCRAFT DEPARTED, AT CRUISE, THE LT ENGINE HAD AN EXPLOSIVE NOISE AND THE LEFT ENGINE SEIZED. PRE INSPECTION OF ENGINE INDICATES LOSS OF CT BLADE. (K)SDR 2005FA0000005Cable · brokenON CLIMBOUT THE AIRSTAIR DOOR OPENED. AC RETURNED, WHEN AIRSTAIR DOOR OPENED IN FLIGHT, DOOR DAMPER BROKE AND SUPPORT CHAINS BROKE. CHAIN HIT PROPELLER AND CAUSED NOTICEABLE DAMAGE. DOOR ANNUNCIATOR LIGHT WAS NOT ILLUMINATED SO NO INDICATION OF ANY PROBLEMSDR TIM2001F00010Bulkhead · crackedTHE RIGHT ENGINE COWLING BULKHEAD AT STATION 238.18 THAT THE LOWER FRONT ENGINE COWLING ATTACHES TO WAS CRACKED ON THE RIGHT LOWER SIDE. THIS LOCATION IS WERE ONE OF THE FOUR BOLTS SECURE THE LOWER COWL TO THE BULKHEAD. (PICTURES INCLUDED)SDR 2001F00624Shaft · damagedINSPECTION OF THE FLAP CABLES AS OUTLINED IN BEECH S/B 27-3397 PER AD 2001-18-07 REVEALED THE CABLES DIAGONAL WRAP TO BE UNWINDING. CONTINUED INSPECTION REVEALED THAT THREE OF THE FOUR CABLES TO BE UNWINDING. THE CABLES WERE INSTALLED IN THE CORRECT FASHION.SDR 2001F00622Shaft · damagedINSPECTION OF THE FLAP CABLES AS OUTLINED IN BEECH S/B 27-3397 PER AD 2001-18-07 REVEALED THE CABLES DIAGONAL WRAP TO BE UNWINDING. CONTINUED INSPECTION REVEALED THAT THREE OF THE FOUR CABLES TO BE UNWINDING. THE CABLES WERE INSTALLED IN THE CORRECT FASHION.SDR 2001F00621Shaft · damagedINSPECTION OF THE FLAP CABLES AS OUTLINED IN BEECH S/B 27-3397 PER AD 2001-18-07 REVEALED THE CABLES DIAGONAL WRAP TO BE UNWINDING. CONTINUED INSPECTION REVEALED THAT THREE OF THE FOUR CABLES TO BE UNWINDING. THE CABLES WERE INSTALLED IN THE CORRECT FASHION.SDR TIM2001F00008Motor · shortedAIRCRAFT FILLED WITH SMOKE, CREW MADE AN EMERGENCY LANDING. CHECK OF AIRCRAFT SYSTEMS FOUND THE FORWARD EVAPORATOR MOTOR SHORTED. AIRCRAFT WAS FURTHER INSPECTED FOR DAMAGE, NONE FOUND.SDR 20010507CW019Stringer · corrodedINSPECTION REVEALED A .6 INCH SECTION OF FUSELAGE STRINGER 14L CORRODED AT APPROX F.S. 250 FUSELAGE SKIN WAS NOT DAMAGED.SDR 20010507CW015Bracket · corrodedINSPECTION DISCOVERED SIGNIFICANT CORROSION ON 2 RT ELEVATOR HINGE BRACKETS.SDR 20010507CW014Bracket · corrodedINSPECTION DISCOVERED SIGNIFICANT CORROSION ON 2 RT ELEVATOR HINGE BRACKETS.SDR 20010507CW008Floor Support · corroded4 FLOOR SUPPORT BRACKETS WERE FOUND WITH SIGNIFICANT CORROSION ON THE TOP SURFACE WHERE THEY ARE IN CONTACT WITH THE HONEYCOMB FLOOR PANEL.SDR 20010507CW007Floor Support · corroded4 FLOOR SUPPORT BRACKETS WERE FOUND WITH SIGNIFICANT CORROSION ON THE TOP SURFACE WHERE THEY ARE IN CONTACT WITH THE HONEYCOMB FLOOR PANEL.SDR 20010507CW006Bracket · wornINSPECTION FOUND ALL FLAP TRACK BRACKETS WORN BEYOND ACCEPTABLE LIMITS.SDR 20010507CW005Bracket · wornINSPECTION FOUND ALL FLAP TRACK BRACKETS WORN BEYOND ACCEPTABLE LIMITS.SDR 20001228AP001Fire Loop · shortedFLT 9141 - TPA-RSW - DURING FLIGHT, LEFT ENGINE FIRE INDICATION OCCURRED. PRECAUTIONARY SHUTDOWN AND DISCHARGE OF ENGINE FIRE BOTTLE CARRIED OUT. REMOVED AND REPLACED LEFT ENGINE FORWARD FIRE LOOP DUE TO SHORT. REPLACED LEFT ENGINE FIRE BOTTLE. (M)SDR 20000725AP005Hinge · corrodedDURING SCHEDULED MAINTENANCE, LEFT OUTBOARD ELEVATOR HINGE BRACKET MOUNTED ON THE STABILIZER SHOWED SIGNS OF INTERGRANULAR CORROSION. REMOVED AND REPLACED LEFT ELEVATOR OUTBOARD HINGE. (M)SDR 20000427AP008Engine · failedFLT 9330 - TPA-JAX - WHILE IN DESCENT INTO JACKSONVILLE AT 10,000 FT, A LOUD SQUEALING NOISE WAS HEARD. LEFT ENGINE INDICATED ITT AND TORQUE FLUCTUATIONS. PILOT MADE THE DETERMINATION TO SHUT THE LEFT ENGINE DOWN. REMOVED ENGINE ASSEMBLY AND ROUTED TO PRATTSDR 98ZZZX2870Switch · failedTPA/MIA - FLT 7485 - LANDING GEAR INDICATOR CIRCUIT BOARD TRIPS WHEN GEAR RETRACTS AND WILL NOT RESET UNTIL GEAR IS DOWN AND LOCKED. REMOVED AND REPLACED GEAR UP LIMIT SWITCH. (X)SDR 99ZZZX733Switch · out of ajdustFPO/MIA - FLT 7410 - PILOT REPORT: CANNOT SILENCE WARNING HORN FOR GEAR. ADJUSTED BOTH LEFT AND RIGHT POWER LEVER SWITCHES. (X)SDR 97ZZZM729Relay · shortedFLT 7168 - MCO-FLL, UNABLE TO LOWER GEAR, BREAKER POPPED, HYDRAULIC FLUID LOW LIGHT ILLUMINATED. MANUAL EXTENSION ACCOMPLISHED. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED LANDING GEAR POWER PACK RELAY. GEAR SWINGS ON JACKS SATISFACTORY. (M)SDR 97ZZZM527Switch · intermittentFLT 398 - TCB/FLL - LANDING GEAR LIGHT (INTRANSIT) WOULD NOT GO OFF WHEN LANDING GEAR WAS RETRACTED. NO EMERGENCY DECLARED. AIRCRAFT LANDED WITHOUT INCIDENT. AIRCRAFT FERRIED TO MIA. REPLACED LEFT MAIN LANDING GEAR DOWNLOCK SWITCH. OP ERATIONAL CHECKS SATSDR 97ZZZM150Brakes · inoperativeFLT 437 - TPA-MIA - RIGHT BRAKE INOP, SLIPS. CLEANED AND SERVICED BRAKES. OK FOR SERVICE. (M)SDR 96ZZZX5988Warning Light · malfunctionedEYW/MIA - FLT 403 - PILOT REPORT: WHEELS WARNING LIGHT WILL NOT COME ON IN-FLIGHT. SYSTEM FUNCTIONS PROPERLY WHEN RETARDING POWER LEVERS BACK TO ACTUATE WARNING HORN.
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