N75429
Service difficulty reports · 55
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 = 'N75429' 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 = 'N75429' 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 CALA2016103100835Battery Pack · inoperativeEMERGENCY LIGHT BATTERY PACK M1674 WILL NOT HOLD A CHARGE. REMOVED AND REPLACED BATTERY PACK AT M1674 IAW AMM 33-51 -06 OPS CHECKED GOOD IAW AMM 33-51-00SDR Z6WR20160621001Panel · delaminatedUPON REMOVAL OF THE 315A2130 BLANKET INSTALLATION, VISUAL AND ULTRASONIC INSPECTION OF THE 315A2101-177 BONDED PANEL ASSEMBLY, CMM 78-31-26, FIG 6, ITEM 40A, REVEALED 6 AREAS OF THERMAL DEGRADATION RESULTING IN DELAMINATION C/T THE-177 BONDED PANEL ASSEMBLY. SDR CALA2015122101009Skin · damagedLEFT LOWER SIDE OF RUDDER AT APPROX 36 INCHES BELOW STATION 60.85, HAS DAMAGE IN MIDDLE OF PANEL. REMOVED DAMAGED AREA & INSTALLED REPAIR IAW SRM 55-40-01 REPAIR 1 & SRM 51-70-05 REPAIR 11, SEALED PRIMED & PAINTED AREA. CALCULATED WEIGHT & BALANCE & UPDATED SDR 39NR2013112162Skin Panel · misrepairedFUSELAGE SKIN PANEL MISDRILLED AT BS 727E STRINGER 2R. REPAIRED FUSELAGE SKIN PANEL AT BODY STATION 727E STRINGER 2R IAW EC/RA 5310-05885.SDR CALA2010021700033Attach Bolt · looseLT ELEVATOR TAB CONTROL ROD ATTACH BOLTS ARE NOT SECURE AT FWD END (NUTS ARE BACKED OFF). REPLACED LT ELEVATOR TAB CONTROL ROD ATTACH BOLT NUTS IAW AMM 27-31-34.
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