N766AT
Service difficulty reports not matched to an aircraft · 27
They name N766AT, 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 = 'N766AT' 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 = 'N766AT' 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 DHL2003783013O-Ring · brokenAFTER ENGINE START LOST ALL OIL QUANTITY FOLLOWED OIL PRESSURE ON ENGINE NR 1. COMPLETED LOW OIL PRESSURE ABNORMAL AND SHUT DOWN ENGINE NR 1 AT 35 PSI. FOUND O-RING ON OIL FILTER BROKEN. REMOVED AND REPLACED O-RING AND FILTER. OPS CHECKED NORMAL IAW M/M 79SDR DHL2003783011Seat Belt · damagedUNABLE TO UNLOCK SECOND OFFICERS SHOULDER HARNESS FROM RETRACTED POSITION. REMOVED AND REPLACED S/O SHOULDER HARNESS BELT REEL IAW M/M 25-10-0. OPS CHECKED GOOD.SDR DHL2003783010Wire · shortedENGINE NR 3 DETECTOR CIRCUIT GROUND FAULT LIGHTS ILLUMINATED AT P6 CIRCUIT BREAKER PANEL. DEFERRED PER DHL MEL 26-9-1 CAT-C. ASSIGNED CONTROL 12957. PLACARD INSTALLED. REF DMI 12957 ENGINE NR 3 DETECTOR GROUND CIRCUIT FAULT LIGHT ILLUMINATED. FOUND POOR ISDR DHL2003783009Fire Detector · malfunctionedENGINE NR 3 DETECTOR CIRCUIT GROUND LIGHT IS ILLUMINATED ON CIRCUIT BREAKER PANEL. REPLACED LOWER DETECTOR ELEMENT SUPPORT CLAMP DUE TO WORN SYSTEM. TESTED IAW M/M 20-11-00, OPS NORMAL. GROUND FAULT LIGHT IS OFF.SDR DHL2003783008Fire Loop · shortedDURING CLIMBOUT OF CVG, NR 3 DETECTOR CIRCUIT GROUND LIGHT ILLUMINATED INTERMITTENTLY THEN REMAINED ON. FOUND LOOP CONTACTING LOWER ENGINE COWL. RE-SECURED LOOP. OPS CHECKED NORMAL IAW M/M 26-21-0.SDR DHL2003783007Warning Horn · malfunctionedON PREFLIGHT CHECK, NO HORN DURING ENGINE OR WHEEL WELL FIRE TEST. REMOVED AND REPLACED AURAL WARNING DEVICE (BOX ASSEMBLY) & OPS TESTED NORMAL PER M/M 26-11-0.SDR DHL2003783006Fire Loop · groundedFOLLOWING LANDING, THE NR 3 DETECTOR CIRCUIT GROUND ON THE P6 3 V-PANEL ILLUMINATED. FOUND LOOP TOUCHING SUPPORT BRACKET. RE-SECURED LOOP. OPS CHECKED GOOD PER 26-21-0.SDR DHL2003783005Fire Loop · out of positionENGINE NR 3 ENGINE DETECTION DETECTOR CIRCUIT GROUND LIGHT ILLUMINATED. DEFERRED PER DHL MEL 26-9 CAT-C NR 12894. REF DMI 12894; ENGINE NR 3 ENGINE DETECTION DETECTOR CIRCUIT GROUND LIGHT ILLUMINATED. REPOSITIONED FIRE DETECTION LOOP NR 3 ENGINE FOR CLEARASDR DHL2003783004Module · failedUPON GEAR RETRACTION RIGHT GEAR RED LIGHT REMAINED ILLUMINATED. CHECKED ABNORMAL PROCEDURE DISCUSSED WITH MAINTENANCE, PROCEDED DIRECTLY TO KCVG. LANDED AT KCVG NORMALLY. WITH RED RIGHT GEAR LIGHT ILLUMINATED DOOR LIGHTS WERE OUT AND RIGHT GREEN GEAR DOWN LIGHSDR DHL2003783002Gasper Fan · odorGASPER FAN POPS CIRCUIT BREAKER AND HAS ELECTRICAL ODOR. REPLACED GASPER FAN IAW MM 21-23-1. OPS CHECKED GOOD.SDR DHL2003783001Fire Loop · out of adjustNR 3 FIRE DETECTOR INOPERATIVE LIGHT ILLUMINATED INDICATING A SHORT IN THE RESPECTIVE ENGINE'S FIRE DETECTION CIRCUITRY. INSPECTED LOOP AND ADJUSTED SLIGHTLY IAW BMM CHAPTER 26-11-01, OPS CHECKED GOOD ON GROUND.SDR 20010207SG003Bracket · brokenDURING PREFLIGHT, FOUND THE L1 DOOR RETAINING BRACKET FOR THE GIRT BAR BROKEN. REPLACED BRACKET. (M)SDR 20000619AP002Hydraulic Line · leakingMDW-PHL - DURING CRUISE, THE B SYSTEM WAS LOST WITH BOTH LIGHTS ON, QTY WENT OT ZERO. LANDED WITHOUT INCIDENT, A/C WAS TOWED TO GATE. REPLACED THE B-1 HYDRAULIC PRESSURE LINE, THE B-2 PUMP AND THE PRESSURE AND CASE DRAIN FILTER TO THE B SYSTEM. LEAK CHECKEDSDR 20000412AP003Pin · looseFLL - FLT 572, AFTER ENGINE SHUTDOWN FIRE BELL SOUNDED WITH NO FIRE LIGHT INDICATION. BELL COULD NOT BE SILENCED AS PER ABNORMAL CHECK LIST WITH EITHER OVERHEAD OR GLARESHIELD CUT OUTS. CLEANED AND RESEATED NR 1 ENGINE LOWER LOOP. CLEANED AND RESEATED STUB SDR 20000412AP004Seal · wornDURING CRUISE, L-1 DOOR IS VERY NOISY. REPLACED L1 DOOR SEAL PER MM 52-11-711. (M)SDR 99ZZZM415Motor · leakingFLIGHT 8035 - ATL-MUN - DURING CLIMB-OUT, SYSTEM 'A' PRESSURE STARTED SURGING WITH HYDRAULIC QUANTITY WENT OT ZERO AT APPROXIMATELY FL240. DIVERTED TO MCO. FOUND FLAP HYDRAULIC MOTOR IN RIGHT WHEEL WELL LEAKING. REPLACED FLAP MOTOR IAW MM 27-51-62, OPS CHECSDR 99ZZZM414Switch · inoperativeDURING APPROACH, THE NR 4 LEADING EDGE FLAP WOULD NOT EXTEND ACCORDING TO F/C ANNUNCIATOR. REPLACED LEADING EDGE FLAP SWITCH TO THE NR 4 POSITION PER 27-82-01, GROUND OPS CHECKED GOOD. (M)SDR 99ZZZM413Control Cable · brokenDURING PREFLIGHT, THE LEFT INBOARD TRAILING EDGE CABLE ASSY WAS FOUND BROKEN. REPLACED LEFT INBOARD TRAILING EDGE FLAP CABLE ASSY IAW MM 27-51-5, OPS CHECKED NORMAL. (M)SDR 99ZZZM271Controller · failedAT FL220, CABIN BEGAN TO CLIMB AT 1500 FPM, CREW DONNED OXYGEN MASKS. EMEREGNCY DECLARED AND DIVERTED TO ORD, WITHOUT FURTHER INCIDENT. REMOVED AND REPLACED CABIN PRESSURE CONTROLLER, CHECKED SYSTEM AND GOOD. (M)SDR 98ZZZX1963Wire · shortedFORWARD PANEL WARNING LIGHTS ILLUMINATED AS IF STICKING OR STUCK IN TEST MODE. CIRCUIT BREAKER RECYCLING INEFFECTIVE IN CLEARING LIGHTS. FOUND TERMINAL SHORTED TO GROUND ON FIRST OFFICER'S COMPASS TRANSFER LIGHT. REPAIRED AND SECURED PER SWPM 20-10-13. OK SDR 98ZZZM188Retract Mech · out of adjustFLT 511 - AT MDW, DURING TAKEOFF, AIRCRAFT REQUIRED 2 UNITS LEFT RUDDER TRIM. WHEN FLAPS UP, WENT TO 1 UNIT RIGHT TRIM. WHEN EXTENDING FLAPS TO 2, A/C IMMEDIATELY ROLLED LEFT AND REQUIRED 2 UNITS LEFT TRIM. ADJUSTED AND INSPECTED FLAPS.SDR 98ZZZM189Indicator · malfunctionedFLT 540 - AT MCO, DURING TAXI AFTER LANDING, THE FLAPS WERE RETRACTED AND THE OUTBOARD FLAPS INDICATED UP. WHILE THE INBOARD FLAPS INDICATED DOWN. REMOVED AND REPLACED INBOARD FLAP INDICATOR.SDR 98ZZZM190Indicator · failedFLT 7053 - AT HOW, DURING TAXI, TURNED BACK TO GATE DURING TAXI OUT INBOARD FLAP GAUGE INDICATED 15 DEGREE FLAPS THEN MOVED TO 0 DEGREES. FLAPS REMAINED AT 15 DEGREES SETTING. REMOVED AND REPLACED INBOARD FLAP INDICATOR.SDR 98ZZZM191Retract Mech · malfunctionedFLT 5039 - AT ATL, DURING DESCENT SPLIT FLAPS ON APPROACH TO ATL. INBOARD FLAPS DID NOT MOVE FROM 0 DEGREES. USED ALTERNATE FLAP SYSTEM TO EXTEND FLAPS. INSPECT FLAPS (INBD) AND RUN FLAPS SEVERAL TIMES. NO DEFECTS NOTED. (M)SDR 95ZZZM218Switch · failedMDW - SMOKE AND ELECTRICAL SMELL IN THE COCKPIT BELOW 10,000 FEET INTO MDW, COMING FROM OVERHEAD PANEL. FOUND RT RUNWAY TURNOFF SWITCH BAD SECURED WIRES. COLLAR CIRCUIT BREAKER SWITCH WAS REPLACED 5-10-95 SYSTEM OPS CEHCK GOOD. (M)SDR 95ZZZX5185Diffuser · crackedIND - NR 3 ENGINE HAS A CRACK IN THE OUTER DIFFUSER DUCT. NR 3 ENGINE WAS REMOVED AND REPLACED.SDR 95ZZZW327Uplock Switch · malfunctionSTL - FLT 491 - AFTER TAKEOFF UPON GEAR RETRACTION HAD NOSE GEAR UNSAFE INDICATION. RECYCLED GEAR, NO HELP. RAN ABNORMAL PROCEDURES, INDICATION REMAINED. REPLACED NOSE LANDING GEAR UPLOCK SWITCH. PIN WAS STUCK IN GROUND POSITION, PERFORMED REMOVAL/INSTALLA
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