N380WL, cancelled Mar 21, 2006
Service difficulty reports · 16
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 = 'N380WL' AND deregistration_id = 'N380WL-2006-03-21' 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 = 'N380WL' AND deregistration_id = 'N380WL-2006-03-21' 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 PIDA06007Attach Angle · crackedUPPER O/B ATTACH ANGLE FOR THE LEFT RAM AIR DUCT IS CRACKED. REPLACED ATTACH ANGLE PER SRM 51-10-02 AND 51-40-00.SDR PIDA06004Skin · crackedCRACK IN FUSELAGE SKIN AT BS 380 ABOVE STR 4 RT SKIN LAP JOINT. REPAIRED DAMAGE PER SRM 53-00-01.SDR PIDA06005Skin · crackedCRACK IN FUSELAGE SKIN AT BS 500A ABOVE STR 4 LT SKIN LAP JOINT. REPAIRED DAMAGE PER SRM 53-00-01.SDR PIDA06002Actuator · brokenLOSS OF -A- SYSTEM HYDRAULIC PRESSURE; QUANTITY ZERO; ISOLATED SYSTEM, PERFORMED MANUAL GEAR EXTENSION & FLAPS 25 LANDING, NO FURTHER INCIDENT. FOUND NR 1 SPOILER ACTUATOR CASTING BROKEN. REPLACED NR 1 SPOILER ACTUATOR PER MM 27-62-94.SDR PIDAS06002Actuator · brokenLOSS OF -A- SYSTEM HYDRAULIC PRESSURE; QUANTITY ZERO; ISOLATED SYSTEM, PERFORMED MANUAL GEAR EXTENSION & FLAPS 25 LANDING, NO FURTHER INCIDENT. FOUND NR 1 SPOILER ACTUATOR CASTING BROKEN. REPLACED NR 1 SPOILER ACTUATOR PER MM 27-62-94.SDR PIDA20050201Autopilot Sys · malfunctionedB-CHANNEL AUTO PILOT CAPTURES PRESELECTED ALTITUDE 300 FEET HIGH ON DESCENT BELOW FLIGHT LEVEL 20,000. A-CHANNEL WORKS FINE. PLACED B-AUTO PILOT ON MEL 22-1.SDR PIDA20050200Control Panel · malfunctionedAUTO PILOT LEVELING OFF 300 FEET ABOVE SELECTED MCP ALTITUDE. REPLACED MODE SELECT PANEL PER MM 22-11-00. OPS CHECKS OK.SDR PIDA20050193Lap Joint · crackedDURING "A CHECK, FOUND CRACK ABOVE STR 10 RT SKIN LAP JUST AFT OF BS 440.SDR PIDA20050192Lap Joint · crackedDURING "A CHECK, FOUND TWO CRACKS ABOVE STR 10 RT SKIN LAP, ONE JUST AFT OF BS 500A AND ONE JUST FORWARD OF BS 500B.SDR PIDA20050191Lap Joint · crackedDURING A-CHECK, FOUND CRACK ABOVE STR 10 RT SKIN LAP JUST FORWARD OF BS 520.REPAIRED PER SRM 53-00-01.SDR PIDA20050194Skin · crackedDURING "A" CHECK, FOUND CRACK IN FUSELAGE SKIN JUST BELOW STR 22RT BETWEEN BS 727D AND BS 727E.SDR PIDA20050182Power Lever · out of adjustLEFT POWER LEVER DID NOT GO TO FLIGHT IDLE WITH LEVEL CHANGE SELECTED, THUS RESULTING IN ASYMMETRICAL THRUST. PERFORMED CABLE LUB PER MM 12-26-00.SDR PIDA20050050Engine · bird ingestionINGESTED BIRD IN RIGHT ENGINE AT ROTATION. VIBRATION INDICATION 4.0 UNITS AT POWER REDUCTION. INSPECTED ENGINE PER MM 71-00-47. UNSHINGLED BLADES NR 20, 21, 22, 23, AND 24. ALL ENGINE PARAMETERS AND VIBRATION CHECKS NORMAL ON ENGINE RUN.SDR 380WL0002Indicator · malfunctionedNR 2 NAV-ILS, FLAGS WHEN IN VOR/ILS/AP MODE. PLACED ON MEL 22-15-7 AND 8. PERFORMED TROUBLE-SHOOTING PROCEDURE FOR VOR/ILS SYSTEM PER MM 34-31-00. NO DEFECTS NOTED. CLEARED MEL.SDR 380WL0003Cable · out of rigAUTOTHROTTLE KICKS OFF DURING FLIGHT. RIGGED LEFT THROTTLE FLEX CABLE PER MM 76-11-00. AUTOTHROTTLE CHECKS GOOD.SDR 380WL0001Computer · malfunctionedAUTO THROTTLE DOES NOT ACHIEVE REQUESTED TAKE OFF THRUST AND DISENGAGES DURING ALL PHASES OF FLIGHT. REPLACED AUTO THROTTLE COMPUTER IAW MM 22-31-10. TEST NORMAL.
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