N374NW
Service difficulty reports · 159
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 = 'N374NW' 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.
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 = 'N374NW' AND registry_match = 'registration' 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 DALA1109443274Dummy Rail · corrodedFWD CABIN DUMMY RAIL, Y-189 IS CORRODED AT FRAME 20. BLENDED OUT CORRODED AREA IAW SRM 51-74-00, L=2.0" W=1.0", D=0.051". ORIGINAL MATERIAL THICKNESS 0.080", FOUND TO BE OUTOF LIMITS IAW SRM 53-11-14, FIG 105. REMOVED DAMAGED DUMMY RAIL IAW SRM 51-42-11, INSDR DALA1109433274Floorbeam · corrodedFWD CABIN FLOORBEAM -1292 IS CORRODED BETWEEN FR 16 ANDFR 20. BLENDED OUT CORRODED AREA IAW SRM 51-74-00, L=3.0" W=1.0 D=0.070" ORIGINAL MATERIAL THICKNESS 0.079", FOUND TO BE OUT OF LIMITS IAW SRM 53-11-14, FIG 105. REMOVED FLOORBEAM IAW SRM 51-42-11, INSTSDR DALA1021193274Floor Panel · damagedDURING LINE CHECK FOUND FWD CARGO FLOOR PANEL 131EF WITH SEVERAL SCREWS PULLED THROUGH. REPLACED FLOOR PANEL IAW SRM 53-22-14, PAGE 401.SDR DALA1021183274Floor Panel · damagedDURING LINE CHECK FOUND FWD CARGO FLOOR PANEL 131AF WITH SEVERAL SCREWS PULLED THROUGH. REPLACED FLOOR PANEL IAW SRM 53-22-14 PAGE 401.SDR DALA1010283274Connector · damagedDURING A NON ROUTINE CHECK, MX FOUND ROW 19 EMERGENCY SEAT LIGHT INOPERATIVE. MX FOUND PIN PUSHED BACK IN CONNECTOR, REINSTALLED PIN AND OPS CHECK WAS NORMAL.SDR DALA102563274Wire · brokenTEST OF EMERGENCY LIGHTS FOUND SEAT 4 PATH LIGHT INOP, REPAIRED BROKEN WIRE UNDER SEAT AND CHECKS OK.SDR NWAA073283274Skin · puncturedDURING "H" CHECK, FOUND PUNCTURE IN FORWARD CARGO DOOR INNER SKIN. REPAIRED PER EA 32-210218 SECTION I SECTION II OF EA 32-210218 TO BE ACCOMPLISHED WITHIN 180 DAYS.SDR 0700053274Thermostat · unknownAIR ENGINE NR 1 AND NR 2 BLEEDS FAULTED AT FLIGHT LEVEL 390. STARTED LOSING CABIN PRESSURIZATION, ATC CLEARED AND EXECUTED RAPID DESCENT, DURING WHICH CABIN ALTITUDE WENT TO 12500 FEET. BLEEDS RECOVERED AT 10,000 FEET. MASKS WERE NOT DROPPED, AND AIRCRAFT LSDR 0501483274Outflow Valve · malfunctionedAT CRUISE ALTITUDE OF 37,000 FEET RECEIVED A CAB PR SYS 1 FAULT. MOMENTS LATER RECEIVED CAB PR 1 & 2 FAULT. REQUESTED IMMEDIATE DESCENT WITH ATC. CABIN PRESSURE WAS HOLDING STEADY AT 7,000 FEET. REPORTED TO ATC THAT CABIN PRESSURE WAS HOLDING AND RECEIVED
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