N709AL
Service difficulty reports not matched to an aircraft · 30
They name N709AL, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. 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 = 'N709AL' AND registry_match IS NULL 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 = 'N709AL' AND registry_match IS NULL 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 ALGA052320137420Longeron · corrodedLONGERON CORRODED BEYOND LIMITS.SDR ALGA052320137418Conduit · corrodedCORROSSION ON CONDUIT FOUND DURING CLEAN UP.SDR ALGA2012110729113Governor · looseNR 2 ENGINE FAILED POWER CHECK. TIGHTENED NR 2 GOVERNOR AND RESEATED NR 2 HEATER VALVE. SUBSEQUENT POWER CHECK AT +2.SDR ALGA2012012372124Support · corrodedSUPPORT PITTING CORROSION BEYOND LIMITS.SDR ALGA062011709ALEngine · power lossON APPROACH NR 2 ENGINE LOST POWER AND WENT HOT, THEY TRIED TO MAKE A GO AROUND. THEY HAD TO LAND DUE TO THE A/C MAKING NOISES. ACFT LANDED SAFELY.SDR ALGA030310709ALConnector · shortedIN CRUISE FLIGHT, NR 2 ENGINE FIRE T-HANDLE ILLUMINATED WITH AUDIBLE TONE. MX REPLACED NR 2 ENGINE FLAME DETECTOR AND CONNECTOR.SDR ALG2006F00023Downlock Sensor · out of adjustLANDING GEAR UNLOCKED LIGHT ILLUMINATED WHEN THE GEAR WAS EXTENDED. MAITENANCE ADJUSTED THE DOWN LOCK PROXIMITY SENSOR FOR THE RT MAIN LANDING GEAR. (K)SDR ALG2006F00025Warning Light · illuminatedWHILE ON APPROACH TO LANDING, LANDING GEAR WAS PLACED IN THE DOWN POSITION. SYSTEMS INDICATED THE LANDING GEAR WAS NOT SECURE. RETURNED TO BASE AND NOTIFIED MAINTENANCE. (K)SDR ALG2003F00104Pump · failedAIRCRAFT RUNNING ON THE PLATFORM. THE NR 2 HYDRAULIC FAILED WHILE THE AIRCRAFT WAS ON THE PLATFORM, MAINTENANCE WAS NOTIFIED. THE MECHANIC REMOVED AND REPLACED THE NR 2 HYDRAULIC PUMP DUE TO A SHEERED SHAFT, GROUND RUN WAS PERFORMED AND AIRCRAFT WAS RETURNEDSDR ALG2003F00101Relay · failedON PRE-FLIGHT, THE FIRE EXTINGUISHER SYSTEM FAILED. MAINTENANCE WAS INFORMED AND THE MECHANIC REMOVED AND REPLACED THE K2 RELAY IN THE NR 1 RELAY IN THE OVERHEAD PANEL IAW MM. THE AIRCRAFT WAS RETURNED TO SERVICE.(K)SDR ALG2003F00075Oil Cooler · malfunctionedSHORTLY AFTER TAKE OFF, DURING CLIMB OUT NR 2 ENGINE OIL TEMP EXCEDED REDLINE. AIRCRAFT RETURNED TO CREOLE, TEMPERATURE REACHED 115 DEGREES FOR 10 MINUTES, THE MECHANIC CHECKED CHIP PLUGS AND REPLACED THE ENGINE OIL, THERMOSTAT AND OIL COOLER AND HE CHECKED TSDR ALG2001F00015Landing Gear · malfunctionedAFTER TAKEOFF, THE LANDING GEAR FAILED TO RETRACT. PERFORMED FUNCTION CHECK OF THE LANDING GEAR AND COULD NOT DUPLICATE. THE LANDING GEAR WAS EXTENDED AND RETRACTED APPROXIMATELY 13 TIMES AND FUNCTIONED NORMALLY.SDR ALG2001F00014Gear · corrodedUPON REMOVAL FROM BOX AND VISUAL INSPECTION, FOUND CORROSION PITTING ON GEAR SURFACE, GEAR TEETH, AND BEARING JOURNAL. C/W BLACK OXIDE PROCEDURE AT FACTORY BEFORE RELEASING PART.SDR 2001F00601Pinion Gear · spalledUPON INSPECTION OF GEARBOX PARTS, LIGHTS SPALLING AND GALLING ON PINION GEAR TEETH CAUSING LIGHT SPALLING ON T/M GEAR GEARTEETH. (M)SDR 20000502SH008Bearing · failedDURING RETRACTION TEST OF LANDING GEAR, NOSE STRUT PISTON WOULD NOT EXTEND COMPLETELY WITH AIRCRAFT ON JACKS. WHEEL WOULD CENTER 180 DEGREES FROM NORMAL CENTER. (WHEEL AND FORK ASSY WOULD CENTER BACKWARDS). LOWER BEARING, PN 1944E9A, MOUNTING FLANGE BOLT HOSDR 96ZZZX4854Rib · corrodedDURING SCHEDULED MAINTENANCE, FOUND STABILIZER RIB WITH EXCESSIVE CORROSION. COMPONENT P/N 7600006003011.SDR 96ZZZX4853Spar Rib · corrodedDURING SCHEDULED MAINTENANCE, FOUND STABILIZER SPAR RIB WITH EXCESSIVE CORROSION. COMPONENAT P/N 7600006003011.SDR 96ZZZX4852Longeron · corrodedDURING SCHEDULED MAINTENANCE, FOUND LT STABLIZER LONGERON WITH EXCESSIVE CORROSION.SDR 96ZZZX4851Doubler · corrodedDURING SCHEDULED MAINTENANCE, FOUND STABILIZER DOUBLER WITH EXCESSIVE CORROSION. COMPONENT P/N 7600006003011.SDR 96ZZZX4850Tip Cap · corrodedDURING SCHEDULED MAINTENANCE, FOUND STABILIZER INSTALLATION WITH EXCESSIVE CORROSION.SDR 96ZZZX3459Pump · shaft shearedDURING LEVEL FLIGHT, NR 2 HYDRAULIC PRESSURE GAUGE DROPPED TO ZERO, NO NOISE WAS HEARD, AIRSPEED WAS REDUCED TO 80 KNOTS. LANDING GEAR HANDLE WAS MOVED TO THE EXTEND POSITION. GEAR DID NOT EXTEND. EMERGENCY CHECK LIST WAS UTILIZED TO EXTEND GEAR. LANDING GSDR 96ZZZX3458Module · bypass trippedDURING LEVEL FLIGHT, NR 2 HYDRAULIC PRESSURE GAUGE DROPPED TO ZERO, NO NOISE WAS HEARD, AIRSPEED WAS REDUCED TO 80 KNOTS. LANDING GEAR HANDLE WAS MOVED TO THE EXTEND POSITION. GEAR DID NOT EXTEND. EMERGENCY CHECK LIST WAS UTILIZED TO EXTEND GEAR. LANDING GSDR 95ZZZX6894Pto Gear · cracked4-24-95 - RECEIVED GEARBOX FROM A/C N709AL-PTN WITH PTO GEAR CRACKED. CONDITION - FOUND PTO GEAR CRACKED AT FWD END ABOVE SPLINED AREA. SUSPECT OVERTORQUE ON OUTPUT SHAFT.SDR 95ZZZX5476Shaft · wornREMOVED AT ENGINE CHANGE. OIL COOLER BLOWER SHAFT SPLINES WORN EXCESSIVELY.SDR 95ZZZX4419Blade · crackedDURING 500-HOUR INSPECTION, FOUND CRACK IN SPAR ORIGINATING FROM ROOT END BUSHING HOLE. COMPONENT P/N 7600009300013.SDR 95ZZZX4418Blade · crackedDURING 500-HOUR INSPECTION, FOUND CRACK IN SPAR ORIGINATING FROM BUSHING HOLE. COMPONENT P/N 7600009300013.SDR 95ZZZX4100Strut · damagedDURING 1,500 HOUR INSPECTION, FOUND STRUT WITH MECHANICAL DAMAGE. PART UNSERVICEABLE.SDR 95ZZZX3372Mount · crackedDURING 1500 HOUR INSPECTION, FOUND ENGINE MOUNT HAS A SMALL CRACK, NOT SERVICEABLE, DEFECTIVE WELD.SDR 95ZZZX3371Mount · chafedDURING 1500 HOUR INSPECTION, FOUND ENGINE MOUNT CHAFED BEYOND LIMITS, DAMAGED WHEN RIVETS INSTALLED.SDR 95ZZZX2815Shaft · wornDISCOVERED AT ENGINE CHANGE, OIL COOLER BLOWER SPLINES WORN EXCESSIVELY. SUSPECT CAUSE - WHEN INSTALLED ON ENGINE, SPLINES WERE INSTALLED WITH GREASE. THE GREASE BLOCKED ENGINE OIL PASSAGE IN GEARBOX CAUSING LOSS OF LUBRICATION ON WET SPLINES.
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