N915FD

Service difficulty reports · 213

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 = 'N915FD' 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 FDEA200808073308Crease Beam · corrodedMAIN CABIN, CREASE BEAM INBD CHORD BS 395-BS 418 LBL 65 HAS CORROSION ALSO SEE BS 331 AT FASTENER HOLE FOR CORROSION. REMOVED CORROSION IAW SRM 51-10-02. L=VARIOUS AREAS TOTAL 6.5 INCHES, W=1.5 INCH, D=0.035 INCH. FOUND TO BE OUT OF LIMITS NO SRM REFERENCE. Aug 7, 2008 · N915FD · Boeing 757236 · Fuselage Main, KeelSDR FDEA200808073307Crease Beam · corrodedMAIN CABIN, CREASE BEAM INBD CHORD BS 395-BS 418 LBL 65 HAS CORROSION ALSO SEE BS 331 AT FASTENER HOLE FOR CORROSION. REMOVED CORROSION IAW SRM 51-10-02. L=VARIOUS AREAS TOTAL 6.5 INCHES, W=1.5 INCHES, D=0.035 INCH. FOUND TO BE OUT OF LIMITS NO SRM REFERENCAug 7, 2008 · N915FD · Boeing 757236 · Fuselage Main, StructureSDR FDEA200808073306Floor Support · corrodedMAIN CABIN FIXED FLOOR STRUCTURE BETWEEN STA 1681.8-1720 HAS SEVERAL AREAS OF CORROSION. BLEND CORROSION IAW SRM 51-10-02, AREAS FOUND TO BE OUT OF LIMITS IAW SRM 53-60-51. FABRICATED REPAIR DOUBLERS IAW SRM 53-60-51 FRON 2024-T3 .063 BATCH NR 0001466849. IAug 7, 2008 · N915FD · Boeing 757236 · Fuselage Miscellaneous StructureSDR 08FDEA03308Crease Beam · corrodedMAIN CABIN, CREASE BEAM INBD CHORD BS 395-BS 418 LBL 65 HAS CORROSION ALSO SEE BS 331 AT FASTENER HOLE FOR CORROSION. REMOVED CORROSION IAW SRM 51-10-02, L=VARIOUS AREAS TOTAL 6.5'', W=1.5'', D=0.035. FOUND TO BE OUT OF LIMITS NO SRM REFERENCE. REMOVED CREAAug 7, 2008 · N915FD · Boeing 757236 · Fuselage Main, StructureSDR 08FDEA03307Crease Beam · corrodedMAIN CABIN, CREASE BEAM INBD CHORD BS 395-BS 418 LBL 65 HAS CORROSION ALSO SEE BS 331 AT FASTENER HOLE FOR CORROSION. REMOVED CORROSION IAW SRM 51-10-02, L=VARIOUS AREAS TOTAL 6.5'', W=1.5'', D=0.035. FOUND TO BE OUT OF LIMITS NO SRM REFERENCE. REMOVED CREAAug 7, 2008 · N915FD · Boeing 757236 · Fuselage Main, StructureSDR 08FDEA03306Web · corrodedMAIN CABIN FIXED FLOOR STRUCTURE BETWEEN STA 1681.8-1720 HAS SEVERAL AREAS OF CORROSION. BLEND CORROSION IAW SRM 51-10-02, AREAS FOUND TO BE OUT OF LIMITS IAW SRM 53-60-51 PG FIG. FABRICATED REPAIR DOUBLERS IAW SRM 53-60-51. INSTALLED REPAIR DOUBLERS IAW SRAug 7, 2008 · N915FD · Boeing 757236 · Fuselage Miscellaneous StructureSDR 08FDEA02875Seat Track · damagedSTA 1046, LBL 47, LUG SCALLOP IS MISSING ON SEAT TRACK. REMOVED SEAT TRACK SECTION IAW SRM 53-00-52. FABRICATED NEW ON MAE TRAV NR T8/750424. INSTALLED NEW SEAT TRACK REPAIR PARTS IAW SRM 51-40-02, AND 53-00-52.Jul 14, 2008 · N915FD · Boeing 757236 · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA02874Crease Beam · corrodedMAIN CABIN CREASE BEAM CHORD BS 680 -740, RBL 66 HAS CORROSION. REMOVED CORROSION AND FOUND OUT OF LIMITS. REMOVED CREASE BEAM, RECEIVED NEW PART NR 143N8328U54 IAW SRM 53-30-13. INSTALLED NEW CREASE BEAM PART IAW SRM 51-40-02, AND 51-10-02, FS 680-740, RJul 14, 2008 · N915FD · Boeing 757236 · Fuselage Main, StructureSDR 08FDEA02690Floorbeam · corrodedMAIN CABIN FLOOR STA 365 RBL 58 FLOORBEAM CORROSION. REMOVED DAMAGE, FABRICATED ANGLES MAE TRAV T8/748437. FABRICATED T-CHORDS MAE TRAV T8/748430, IAW SRM 53-00-51. INSTALLED REPAIR PARTS STA 365 RBL 34-70 IAW SRM 53-00-51 FIG 201. REPAIR 3. MAJOR REPAIJul 3, 2008 · N915FD · Boeing 757236 · Fuselage Main, Floor BeamSDR 08FDEA02463Floorbeam · corrodedMAIN CABIN BS 418, BL0 TO LBL 15, FLOORBEAM HAS AREAS OF CORROSION AROUND FASTENER HOLES. CLEANED AREA AND CHECKED LIMITS IAW SRM 51-10-3 AND 53-00-51, DETAIL 3. FLOORBEAM OUT OF LIMITS PER SRM 53-00-51, DETAIL 3; ORIGINAL MATERIAL THICKNESS .125 INCH, AFTJun 25, 2008 · N915FD · Boeing 757236 · Fuselage Main, Floor BeamSDR 08FDEA02432Floorbeam · corrodedMAIN CABIN FLOORBEAM STA 1640 RBL 47-51 HAS CORROSION BLENDED AREA IAW SRM 51-10-02, ORIG MAT. .125 AFTER 0.90 FOUND OUT LIMITS, IAW SRM 53-00-51 PAGE 103, CUT OUT DAMAGED AREA STA 1640 BET RBL36.5 TO RBL 68.5, IAW SRM 53-00-51 PAGE 201. RECEIVED REPAIR PARTSJun 24, 2008 · N915FD · Boeing 757236 · Fuselage Main, Floor BeamSDR 08FDEA02431Floorbeam · corrodedSTA 377.7, BL0 TO LBL 45 HAS CORROSION AROUND NUT PLATE HOLES. REMOVED DAMAGED AREA, LBL 13 TO LBL 70, BS 377.7 IAW SRM 53-00-51, FIG 201, REPAIR NR 3. FABRICATED T-CHORD AND SHIM IAW SRM 53-00-51, REPAIR NR 3. FABRICATED STRAP NR 4 AND NR 5 ON TRAVELER NR Jun 24, 2008 · N915FD · Boeing 757236 · Fuselage Main, Floor BeamSDR 08FDEA01868Skin · dentedR1 DOOR SKIN DENTED. REMOVED DAMAGE AND INSTALLED A DOUBLER REPAIR ON R1 DOOR SKIN IAW SRM 52-10-01 REPAIR NR 2, FIGURE 202. THIS REPAIR IS CLASSIFIED AS A "MAJOR" REPAIR, CATEGORY A, WITH NO FOLLOW UP TRACKING REQUIRED.May 16, 2008 · N915FD · Boeing 757236 · Cargo/Baggage Doors
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