N792FD
Service difficulty reports · 62
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 = 'N792FD' 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 = 'N792FD' 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 FDEA201604111184Frame · chafedCABIN STATION 1640, STRINGER 5L - 6L, FRAME INNER FLANGE CHAFED. COMPLIED WITH PART 1 OF EA F 5310-T0324672. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201604081171Stiffener · chafedLEFT WING FRONT SPAR VERTICAL STIFFENER, PN 112N2063-3, FOUND DEEP CHAFING MARK AT FSS 148.9. LT WING FRONT SPAR VERTICAL STIFFENER REPAIR COMPLETED IAW F-5710-T0324436 P1. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201603311125Floorbeam · damagedCABIN STATION 1640, RBL 22.5, FLOORBEAM WEB FOUND FOUR EACH FASTERNER HOLES ELONGATED. FLOORBEAM WAS REPLACED PER DWG 146N5089 SHT 6 REV - & 146N8711 SHT 2 REV R. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201603241026Door Sill · corrodedAFT CARGO COMPARTMENT, STATION 1460 - 1480, AFT CARGO DOOR LOWER SILL WEB CORROSION. R & R WITH NEW FABRICATED LOWER SILL WEB IAW DWG 146N8522 SHT 3 REV E. NEW LOWER SILL WEB FABRICATED IAW DWG 146N8522 SHT 2 REV D REPAIR CLASSIFIED AS MAJOR.SDR FDEA201603231006Skin Panel · chafedRIGHT WING, INBD TE MAIN FLAP, UPPER OTBD PANEL, UPPER SURFACE FOUND CHAFE MARK AT 8" FROM LE, 33" FROM OTBD EDGE. DAMAGE REMOVED, CLEANED & REPAIRED DOUBLER, INSTALLED PER 250 F HOT BONDING IAW SRM 57-53-01-2R DETAIL I REV 117 & SRM 51-70-10-2R PARA 6, 7, SDR FDEA201603220982Stringer · corrodedAFT CARGO COMPARTMENT, STATION 1615, STRINGER 21L, STRINGER CORROSION. STRINGER REMOVED & REPAIR PARTS INSTALLED IAW EA F-5310-T0324239 P1. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201603220981Stringer Splice · corrodedAFT CARGO COMPARTMENT, STATION 1620, STRINGER 18L, STRINGER SPLICE CORROSION OUT OF LIMIT. R & R WITH FABRICATED STRINGER SPLICE IAW EA F-5310-T0324244 P1. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201603170938Stringer Splice · corrodedAFT CARGO COMPARTMENT, STATION 1620, STRINGER 20R, STRINGER SPLICE CORROSION.SDR FDEA201603150927Repair · debondedEXISTING REPAIR WING, THERE IS A REPAIR AT RT WING INBD MAIN FLAP LOWER MIDDLE PANEL. THIS REPAIR REQUIRES EVALUATION IAW EO F-5100-7-5001 A5 PT 1 ATTACHMENT B NO HISTORY. EXISTING REPAIR AT RT WING INBD MAIN FLAP LOWER MIDDLE PANEL WAS EVALUATED & FOUND DSDR FDEA201603150925Frame · corrodedCABIN STATION 1580, STRINGER 9R - 10R, FRAME OTBD FLANGE FOUND CORROSION. CORROSION EVALUATED & FOUND CORROSION MORE THAN 50% THROUGH. FRAME REPAIR CARRIED OUT IAW SRM 53-00-07-2R REV 117. THIS IS A CAT B REPAIR WITH A THRESHOLD OF 10000 FLIGHT CYCLES AFTERSDR FDEA201603130913Door Sill · corrodedCABIN STATION 740 - 755, L2 DOOR CUT OUT LOWER SILL, INNER CHORD FOUND CORROSION. COMPLIED WITH PART 1 OF EA F-5310-T0324494 REV A. THREE EACH FASTENER HOLES ON MED L2 LOWER MAIN SILL INNER CHORD. REPAIR CLASSIFIED AS MAJOR.
SDR FDEA201602240678Skin · damagedLEFT WING, INBD MAIN FLAP UPPER INBD SKIN, EXTERIOR SURFACE FOUND 01 EA DENT & DELAMINATION MARK AT 20.5" FROM TE, 36" FROM INBD EDGE. DAMAGED AREA REMOVED, CLEANED, DRIED & REPAIR DOUBLERS INSTALLED IAW SRM 57-53-01-2R DETAIL I & SRM 51-70-10-2R REPAIR GENER
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