N801AY

Service difficulty reports · 106

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 = 'N801AY' 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.

SDR REXA201000317Bulkhead · crackedFS 202.75 PRESSURE BULKHEAD IS CRACKED AT BRAKE CABLE PASS-THRU HOLE. REPAIRED 202.75 PRESSURE BULKHEAD IAW REO 601R-53-11-563 AND BSC STANDARD REPAIR 601R-53-0101A.Dec 18, 2010 · N801AY · Cndair CL6002B19 · Fuselage Main, BulkheadSDR REXA201000316Pressure Panel · damagedFOUND DOUBLE DRILLED HOLE IN PRESSURE FLOOR AT FS 523.00 AT RBL 27.00. PERFORMED A MAJOR REPAIR TO DAMAGED HOLE ON PRESSURE FLOOR AT FS 523.00 RBL 27.00 IAW BOMBARDIER SERVICES CORPORATION ENGINEERING ORDER NO: 601R-53-20026.Dec 18, 2010 · N801AY · Cndair CL6002B19 · Fuselage Main, BulkheadSDR REXA201000280Skin · dentedA SINGLE INDENTATION WAS FOUND ON THE RT WING OTBD GROUND SPOILER UPPER SURFACE. THE DAMAGE IS RECORDED AS 0.049 INCH DIAMETER AND A MAXIMUM DEPTH OF 0.006 INCH AND IS LOCATED 3.7 INCHES AFT OF THE L/E AND 7.68 INCHES FROM THE OTBD EDGE. TEMPORARY REPAIR IAW SNov 29, 2010 · N801AY · Cndair CL6002B19 · SpoilersSDR REXA201000157Step · puncturedPUNCTURE IN THE PASSENGER STEP SURFACE WAS FOUND ON THE SECOND STEP FROM THE TOP (WITH DOOR IN OPEN POSITION). THE PENETRATION MEASURES APPROX 0.50 INCH DIAMETER AND IS LOCATED AT THE INBD EDGE OF THE STEP 4.75 INCHES FWD OF THE AFT EDGE. A VISUAL CHECK FROM TSep 23, 2010 · N801AY · Cndair CL6002B19 · Passenger/Crew DoorsSDR REXA201000047Wire Harness · faultyWOW INPUT CAUTION MSG CYCLED FIVE TIMES ON AND OFF AFTER GEAR RETRACTION. REMOVED AND REPLACED NLG ELECTRICAL HARNESS IAW AMM 32-61-25. OPS CHECK NORMAL, OK FOR SERVICE.Apr 10, 2010 · N801AY · Cndair CL6002B19 · Landing Gear System WiringSDR REX2005F00016Control System · failed(REF NR: 05-087) FLAPS FAILED ON APPROACH, QRH FOLLOWED UNEVENTFUL LANDING. RESET FLAPS AND PLACED SYSTEM ON 72 HOUR WATCH IAW AD 98-20-01. (K)Jul 15, 2005 · N801AY · Cndair CL6002B19 · Trailing Edge Flap Control System
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