N992FD

Service difficulty reports · 113

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 = 'N992FD' 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.

SDR FDEA201105241965Seat Track · gougedMAIN CABIN COMPARTMENT STA 1170, LBL 45 SEAT TRACK GOUGED. R & R SEAT TRACK IAW SRM 51-40-01, 51-40-02, AND 51-40-05. MAJOR REPAIR.May 24, 2011 · N992FD · Boeing 757232 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201105241964Seat Track · corrodedMAIN CABIN STA 1120, LBL 25 SEAT TRACK CORRODED. BLENDED AREAS OF CORROSION WITH MATERIAL LOSS OF .070. CLEAN UP MAX ALLOWED IS .040". AREA FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, FIG 101, DETAIL 4. R & R SEAT TRACK IAW SRM 51-10-02, 51-40-02, 51-40-05May 24, 2011 · N992FD · Boeing 757232 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201105211925Floorbeam · gougedSTA 1200, FLOORBEAM UPPER FLANGE GOUGED BL 0 TO LBL 64. FOUND OUT OF LIMITS IAW SRM 53-00-51 DETAIL III. REPAIRED FLOORBEAM AT STA 1200 LBL 19.5 IAW SRM 53-00-51 DETAIL 1, AND REPAIR 3. BLENDED GOUGES; L=2.5, W=1.0, D=.002, ORIGINAL MATERIAL WAS .125, FOUMay 21, 2011 · N992FD · Boeing 757232 · Fuselage Main, Floor BeamSDR FDEA201105201916Floorbeam · damagedMAIN DECK FLOORBEAM UPPER T-CHORD HAS 2 EA ELONGATED FASTENER HOLES BETWEEN RBL 45 AND RBL 63 AT STA 460. FOUND TO BE OUT OF LIMITS .250 MAX DIA. AFTER .310 IAW SRM 53-00-51 FIG 101. REPAIRED FLOORBEAM AT STA 460 RBL 33- 63 IAW SRM 53-00-51 FIG 201. CATMay 20, 2011 · N992FD · Boeing 757232 · Fuselage Main, Floor BeamSDR FDEA201105201915Floorbeam · damagedMAIN DECK FLOORBEAM UPPER TEE FITTING HAS 2 EA. ELONGATED FASTENER HOLES AT STA 480 BETWEEN RBL 45 TO RBL 63. FOUND OUT OF LIMITS PER SRM 53-00-51, FIG.101. REMOVED AND INSTALLED ANGLES, BS 480, RBL 50, PER SRM 51-40-02, FOR ACCESS. REMOVED DAMAGED TEE FITMay 20, 2011 · N992FD · Boeing 757232 · Fuselage Main, Floor BeamSDR FDEA201105201901Seat Track · brokenLBL 24 SEAT TRACK SCALLOP BROKEN AT BS 1200. TRANSFERED FROM N00741, REMOVED SEAT TRACK FS 1180-1320 LBL 24 IAW SRM 51-40-02, FABBED NEW SEAT TRACK FROM BAC1520- 792, BATCH 1904663, LOCATED AND DRILLED IAW SRM 51-10-02 AND 51-10-55, TREATED, PRIMED AND TOPMay 20, 2011 · N992FD · Boeing 757232 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201105201910Frame · corrodedAFT CARGO FRAME BS 1400 HAS CORROSION UNDER DOOR SILL AREA. CORROSION FOUND OUT OF LIMITS IAW 53-00-07, PG 104, FIG 101, DET V, RECEIVED NEW FRAME & SPLICE. R & R FRAME IAW SRM 51-40-02 & DWG 146N1028. MAJOR REPAIR.May 20, 2011 · N992FD · Boeing 757232 · Fuselage Main, FrameSDR FDEA201105201900Seat Track · corrodedMAIN CABIN STA 900 RBL 45 SEAT TRACK CORRODED. BLENDED CORROSION . ORIGINAL MATERIAL .230, MATERIAL REMOVED .050. MATERIAL REMAINING .180 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52 DETAIL I FIG 101. R & R SEAT TRACK AT STA 900, RBL 45 IAW SRM 51-40-02, PG 8.May 20, 2011 · N992FD · Boeing 757232 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201105191875Seat Track · gougedMAIN CABIN SEAT TRACK CROWN HAS GOUGE AT STA 877 RBL 45 REMOVED AND REPLACED SEAT TRACK STA 760- 879 RBL 45 IAW 51-10-02, PN BAC1520-792, BATCH 1904663. SEAT TRACK WAS FOUND TO BE OUT OF LIMITS PER SRM 53-00-52, FIG.101, DETAIL 1; ORIGINAL MATERIAL .145", AMay 19, 2011 · N992FD · Boeing 757232 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201105191876Seat Track · corrodedCABIN SEAT TRACK STA 760-879 LBL 24, CORRODED. REMOVED AND REPLACED SEAT TRACK AT STA 760 - 879 LBL 24 IAW SRM 51-40-02 P/N BAC1520-792 BATCH 1904663, FABRICATED WITH SEAT TRACK WAS FOUND OUT OF LIMITS IAW 53-00-52 FIG 101 DETAIL I. ORG MATERIAL .188 AFTERMay 19, 2011 · N992FD · Boeing 757232 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201105171853Floorbeam · corrodedSTA. 365, FLOORBEAM CORRODED BL-0 - 24L. REMOVED CORROSION AT STA 365 LBL 6 ORGINAL MAT .125 MATERIAL REMOVED .060 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51 FIG 101 DETAIL III. FABERICATED FLOORBEAM IAW SRM 53-10-51 FIG 101 DETAIL II PART MARKED IAW GMM 7-0May 17, 2011 · N992FD · Boeing 757232 · Fuselage Main, Floor BeamSDR FDEA201105171859Floorbeam · corrodedFLOOR BEAM AT STA. 345, LBL10 CORRODED. REMOVED; .040", FOUND TO BE OUT OF LIMITS PER SRM 53-00-51, DETAIL 3. REMOVED FLOORBEAM PER SRM 51-40-02. FABRICATED NEW FLOORBEAM PER SRM 53-10-51 & INSTALLED PER SRM 51-40-02. MAJOR REPAIRMay 17, 2011 · N992FD · Boeing 757232 · Fuselage Main, Floor BeamSDR FDEA201105121831Floorbeam · corrodedSTA. 377 FLOORBEAM CORRODED BL 24 - 45 L. REMOVED CORROSION IAW SRM 51-10-02. AREA OUT OF LIMITS IAW SRM 53-00-51 FIGURE 101 DETAIL III. ORIG. MAT. .125 AFTER REWORK .107 MAT. LOSS EXCEED MAX. ALLOWED. REMOVED FLOORBEAM IAW SRM 51-40-02. FABRICATED NEW FLOOMay 12, 2011 · N992FD · Boeing 757232 · Fuselage Main, Floor Beam
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