N788FD
Service difficulty reports · 60
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 = 'N788FD' 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 = 'N788FD' 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 FDEA201510073108Skin · puncturedLEFT WING INBD FLAP AFT FLAP EXTERNAL SKIN BOTTOM AREA HAS PUNCTURE ADJACENT TO CTR TRACK. REPAIRED ONE EACH PUNCTURE IAW SRM 51-70-17 IAW EA F-5750-T0320393 ISSUED FOR TRACKING. CATEGORY A REPAIR MAJOR REPAIR.SDR FDEA201510013031Skin · dentedFUSELAGE EXTERIOR SKIN HAS AN OUTWARD DENT, BETWEEN BS 1420 - 1440, STRINGER 24L & 25L. NOTED DURING DENT EVALUATION OF NR NOOO48, EVALUATED DENT FOUND A & Y=28.18 OUT OF LIMITS IAW SRM 53-00-01 FIG 101 DET III. REPAIRED DENT STATION 1420 - 1440, STRINGER 24SDR FDEA201509262963Frame · corrodedAFT PIT LT SIDE FRAME IS CORRODED AT STATION 1420, BETWEEN STRINGER 19L & 20L. REMOVED CORROSION IAW SRM 51-10-02, ORIGINAL MATERIAL . 063, REMAINING .052, OUT OF LIMITS IAW SRM 53-00-07 FIG 101 DET II. R & R FRAME STATION 1420, STRINGER 14L - 24L IAW SRM 5SDR FDEA201509252942Skin · dentedFUSELAGE EXT SKIN DENTS, COMBINATION INWARD & OUTWARD, BETWEEN STRINGER 27L & 28L, STATION 1580. DENTS AFTER EVALUATED FOUND OUT OF LIMITS IAW SRM 53-00-01-1A FIG 101 DET III. REPAIRED AREA IAW SRM 53-00-01-2R REPAIR 16. CATEGORY B REPAIR, MAJOR REPAIR.SDR FDEA201509242935Frame · corrodedAFT PIT SIDEWALL LT SIDE FRAME, INNER CHORD CORRODED AT STATION 1420 BETWEEN STRINGER 19L & 18L. R & R FRAME, INNER CHORD AT STATION 1420, STRINGER 18L - 22L IAW SRM 51-40-02 & DWG 146N1012. REMOVED CORROSION, FOUND OUT OF LIMITS IAW SRM 51-10-02, SRM 53-00-SDR FDEA201509242934Frame · corrodedAFT PIT SIDEWALL LT SIDE FRAME, INNER CHORD CORRODED AT STATION 1420, BETWEEN STRINGER 19L & 18L. R & R FRAME INNER CHORD IAW SRM 51-40-02 & DWG 146N1012. REMOVED CORROSION, FOUND OUT OF LIMITS IAW SRM 51-10-02, SRM 53-00-07-1A FIG 101 DET II. CATEGORY A RESDR FDEA201509232928Frame · corrodedAFT CARGO RT FRAME AT STATION 1200, INNER CHORD, TOP SURFACES HAS CORROSIONS, FROM STRINGER 28R - 26R. REMOVED CORROSION IAW SRM 51-10-02. ORIGINAL MATERIAL THICKNESS IS 0.080", AFTER BLEND OUT, NO MATERIAL REMAINING. OUT OF LIMITS IAW SRM 53-00-07-1A FIG 1SDR FDEA201509082817Floorbeam · corrodedFLOORBEAM BS 1681 IS CORRODED ON THE UPPER SURFACE . REMOVED CORROSION IAW SRM 51-10-02 AND FOUND OUT OF LIMITS IAW SRM 53-00-51-1A FIG 101 DETAIL VI , REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-40-02 AND DWG 146N5000 . MAJOR REPAIR.SDR FDEA201508212671Floorbeam · corrodedMAIN DECK FLOORBEAM AT BS 1661 RBL 56, HAS CORROSION AROUND FASTENER HOLE. REMOVED CORROSION IAW SRM 51-10-02. CHECKED LIMITS & FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51-1A FIG 101 DETAIL III. R & R FLOORBEAM IAW SRM 51-40-02 & DWG 146N5090. MAJOR REPAIR.SDR CALA2015030493185Skin · corrodedAFT CARGO CIRCUMFERENTIAL STRAP & FUSELAGE SKIN CORRODED BS 1400, STRINGER 27L - 28L. REMOVED PREVIOUSLY INSTALLED DOUBLER & CIRCUMFERENTIAL STRAP SPLICE SECTION. FABRICATED & INSTALLED 6 STRAIGHT SHANK FREEZE PLUGS, REPAIR DOUBLER, 146N3810-8200 SKIN SPLICE
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