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.

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.Jan 15, 2006 · N380WL · Boeing 7373G7 · Fuselage Main, Attach FittingsSDR PIDA06004Skin · crackedCRACK IN FUSELAGE SKIN AT BS 380 ABOVE STR 4 RT SKIN LAP JOINT. REPAIRED DAMAGE PER SRM 53-00-01.Jan 12, 2006 · N380WL · Boeing 7373G7 · Fuselage Main, Plate/SkinSDR PIDA06005Skin · crackedCRACK IN FUSELAGE SKIN AT BS 500A ABOVE STR 4 LT SKIN LAP JOINT. REPAIRED DAMAGE PER SRM 53-00-01.Jan 10, 2006 · N380WL · Boeing 7373G7 · Fuselage Main, Plate/SkinSDR 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.Dec 31, 2005 · N380WL · Boeing 7373G7 · Drag Control ActuatorSDR 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.Dec 31, 2005 · N380WL · Boeing 7373G7 · Drag Control ActuatorSDR 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.Dec 23, 2005 · N380WL · Boeing 7373G7 · Autopilot SystemSDR PIDA20050200Control Panel · malfunctionedAUTO PILOT LEVELING OFF 300 FEET ABOVE SELECTED MCP ALTITUDE. REPLACED MODE SELECT PANEL PER MM 22-11-00. OPS CHECKS OK.Dec 21, 2005 · N380WL · Boeing 7373G7 · Autopilot SystemSDR PIDA20050193Lap Joint · crackedDURING "A CHECK, FOUND CRACK ABOVE STR 10 RT SKIN LAP JUST AFT OF BS 440.Nov 22, 2005 · N380WL · Boeing 7373G7 · Fuselage Main, Plate/SkinSDR 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.Nov 22, 2005 · N380WL · Boeing 7373G7 · Fuselage Main, Plate/SkinSDR PIDA20050191Lap Joint · crackedDURING A-CHECK, FOUND CRACK ABOVE STR 10 RT SKIN LAP JUST FORWARD OF BS 520.REPAIRED PER SRM 53-00-01.Nov 22, 2005 · N380WL · Boeing 7373G7 · Fuselage Main, Plate/SkinSDR PIDA20050194Skin · crackedDURING "A" CHECK, FOUND CRACK IN FUSELAGE SKIN JUST BELOW STR 22RT BETWEEN BS 727D AND BS 727E.Nov 22, 2005 · N380WL · Boeing 7373G7 · Fuselage Main, Plate/SkinSDR 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.Oct 24, 2005 · N380WL · Boeing 7373G7 · Auto Throttle SystemSDR 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.Jun 6, 2005 · N380WL · Boeing 7373G7 · Engine (Turbine/Turboprop)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.Mar 7, 2005 · N380WL · Boeing 7373G7 · Visual Omnirange (VOR) SystemSDR 380WL0003Cable · out of rigAUTOTHROTTLE KICKS OFF DURING FLIGHT. RIGGED LEFT THROTTLE FLEX CABLE PER MM 76-11-00. AUTOTHROTTLE CHECKS GOOD.Mar 5, 2005 · N380WL · Boeing 7373G7 · Auto Throttle SystemSDR 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.Aug 20, 2004 · N380WL · Boeing 7373G7 · Auto Throttle System
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