N930FD

Service difficulty reports · 176

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 = 'N930FD' 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 FDEA201006192074Frame · corrodedMAIN CABIN FRAME 1600 OTBD CHORD ANGLE HAS CORROSION AT STR 17R. REMOVED CORROSION IAW SRM 51-10-02. FOUND OUT OF LIMITS IAW SRM 53-60-13, FIG 101, DETAIL 3, P.103. FABRICATED ANGLE AND FAIL-SAFE. LOCATED, DRILLED, TREATED AND PRIMED ALL REPAIR PARTS IAW Jun 19, 2010 · N930FD · Boeing 7572Y0 · Fuselage Main, FrameSDR FDEA201006182061Frame · corrodedNR 2 ENG STRUT FAIRING PANEL 443AR FRAME HAS CORROSION. COMPLIED WITH EA F-5450-141157 PART 1, STEPS 1-7. A MINOR REPAIR.Jun 18, 2010 · N930FD · Boeing 7572Y0 · Nacelle/Pylon, Frame/Spar/RibSDR FDEA201006172042Floorbeam · corrodedFLOORBEAM BL0 AND STA 324 GOUGED. DAMAGED FLOORBEAM FOUND OUT OF LIMITS WITH ORGINAL MATERIAL .110 LOSS.024 MATERIAL REMAINING .086, L-.050 W-2" AS PER SRM 53-00-51 PG.103 DETAIL 3 & FLOOR SUPPORT ORGINIAL MATERIAL .050 MATERIAL LOSS .009 REMAINING MATERIJun 17, 2010 · N930FD · Boeing 7572Y0 · Fuselage Main, Floor BeamSDR FDEA201006172045Seat Track · damagedMAIN DECK SEAT TRACK LBL 45.5 STA 440 TO 644.5 GOUGED IN SEVERAL AREAS. REMOVED GOUGES AND FOUND PART TO BE OUT OF LIMITS IAW SRM 53-00-52, FIG 101 DET 1, PG 102. ORIGINAL MATERIAL IS .230, REMAINING MATERIAL .195, A REMOVAL OF .035. FABRICATED SEAT TRACKJun 17, 2010 · N930FD · Boeing 7572Y0 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201006152018Floorbeam · misinstalledSECTION 43, SEAT TRACK AT RBL 58.22 BETWEEN STA 620, 640 AND 660 UNABLE TO LOCATE SEAT TRACK EXISTING FASTENER HOLES ON THE FLOORBEAM ARE NOT POSITIONED AS DEPICTED IN THE DWG 657N3321, SHEET 12, REV B. ON ACCESSING AREA, FOUND EXISTING GOUGES ON BS 660 FLOJun 15, 2010 · N930FD · Boeing 7572Y0 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201006142003Shear Web · corrodedMAIN DECK FLOOR, RT, SHEAR WEB, BS 1360-1380, LOWER SURFACE HAS CORROSION.Jun 14, 2010 · N930FD · Boeing 757200 · Fuselage Miscellaneous StructureSDR FDEA201006111964Floorbeam · gougedSTA 1240 FLOORBEAM SCRATCHED AND GOUGED FROM RBL 25 TO LBL 60. BLENDED AREA IAW SRM 51-10-02,ORIGINAL MAT =.125 IN AFTER BLEND = 090 IN WHICH IS OUT OF LIMITS IAW SRM 53-00-51. REMOVED AND REPLACED FLOOR BEAM. LOCATED AND DRILLED NEW FLOORBEAM IAW SRM 51-4Jun 11, 2010 · N930FD · Boeing 7572Y0 · Fuselage Main, Floor BeamSDR FDEA201006111968Floorbeam · corrodedSTA. 740 FLOORBEAM RBL 46 TO RBL 60 UPPER FLANGE CORRODED.Jun 11, 2010 · N930FD · Boeing 7572Y0 · Fuselage Main, Floor BeamSDR FDEA201006111967Floorbeam · gougedSTA. 1320 FLOORBEAM BL "0" TO LBL 60 GOUGED AND CORRODED. REMOVED GOUGED & CORROSION AREA IAW SRM 51-10-01, ORIG MAT THICKNESS 0.125", AFTER REWORK 0.106", MEASURED AREA L=60.00", X W=2.00", X DEPTH 0.019", FOUND OUT OF LIMITS IAW SRM 53-00-51, PAGE 101, FIGJun 11, 2010 · N930FD · Boeing 7572Y0 · Fuselage Main, Floor BeamSDR FDEA201006111965Floorbeam · gougedSTA. 1600 FLOORBEAM SCRATCHED AND GOUGED FROM BL "0" TO RBL 60.Jun 11, 2010 · N930FD · Boeing 7572Y0 · Fuselage Main, Floor BeamSDR FDEA201006111963Seat Track · damagedEXISTING SEATTRACK HAS SCALLOPS PREVIOUSLY REMOVED AT STA 1635-1640 AT RBL 45.50" WHICH WILL INTERFERE WITH INSTALLATION OF CARGO HANDLING SYS. REMOVED SEAT TRACK SECTION AT RBL 45.5, BS 1540-1640. FABRICATED NEW SEAT TRACK SECTION, TREATED/PRIMED, APPLIED TOJun 11, 2010 · N930FD · Boeing 7572Y0 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201006111962Seat Track · damagedEXISTING SEAT TRACK HAS SCALLOPS PREVIOUSLY REMOVED STA 1635-1640 AT LBL 45.50" WHICH WILL INTERFERE WITH INSTALLATION OF CARGO HANDLING SYS. REMOVED SEAT TRACK BS 1540-1640, LBL 45.5, IAW SRM 51-40-02. REMOVED WEB, BS 1620-1640 PET SRM 51-40-02. FABRICATEJun 11, 2010 · N930FD · Boeing 7572Y0 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201006111961Floorbeam · corrodedSTA 700, FLOORBEAM, RBL 55 UPPER FLANGE CORRODED.Jun 11, 2010 · N930FD · Boeing 7572Y0 · Fuselage Main, Floor BeamSDR FDEA201006081955Floorbeam · corrodedSTA 700 FLOORBEAM, RBL 55 UPPER FLANGE CORRODED. REMOVED CORROSION IAW SRM 51-10-02. ORIG MATERIAL 0.130 AFTER REWORK 0.107. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51 FIG 101 DETAIL III. R & R FLOORBEAM AT STA 700, LBL 63 TO RBL 63 IAW SRM 51-40-02 AND DWG Jun 8, 2010 · N930FD · Boeing 7572Y0 · Fuselage Main, Floor BeamSDR FDEA201006082041Floor Support · corrodedMAIN DECK FLOOR RT SHEAR WEB OTBD SUPPORT ANGLE HAS CORROSION AROUND FASTENERS AT STA 1600-1620. REMOVED ANGLE SUPPORT OUT OF LIMITS IAW SRM 51-40-02 CHECKED LIMITS ORIG MAT .090 LOSS .025. REMAINING .065 IAW SRM 53-60-13 LOCATED 7 DRILLED NEW ANGLE SUPPOJun 8, 2010 · N930FD · Boeing 7572Y0 · Fuselage Miscellaneous StructureSDR FDEA201006082040Seat Track · corrodedSEAT TRACK STA 1180-1280, RBL 25 HAS GOUGES, CORROSION, AND WORN PAINT.Jun 8, 2010 · N930FD · Boeing 7572Y0 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201006082039Floorbeam · corrodedSTA 740, FLOORBEAM, RBL 46 TO RBL 60 UPPER FLANGE CORRODED. REMOVED CORROSION, EVALUATED FOUND OUT OF LIMITS, MAT THICKNESS 0.125", MAT BLENDED .018", REMAINING MAT .107", IAW SRM 53-00-51, FIG 101, PG 101, DETAIL III, REMOVED FLOORBEAM IAW SRM 51-40-02, LJun 8, 2010 · N930FD · Boeing 7572Y0 · Fuselage Main, Floor BeamSDR FDEA201006082038Floor Support · corrodedMAIN DECK FLOOR LT SHEAR WEB INBD SUPPORT ANGLE HAS CORROSION AROUND FASTENER HOLES STA 1160-1180. REMOVED CORROSION PER SRM 51-10-02. FOUND TO BE OUT OF LIMITS PER SRM 53-40-13, P.104, DETAIL 7; BEFORE: .071", AFTER: .057", LOSS: .014". FABRICATED I/B SUPPJun 8, 2010 · N930FD · Boeing 7572Y0 · Fuselage Miscellaneous StructureSDR FDEA201006081957Support Angle · corrodedMAIN DECK FLOOR RT SHEAR WEB INBOARD SUPPORT ANGLE JOINT SUPPORT FITTING ON FRAME CORRODED STA 1080. REPLACEMENT OF SUPPORT FITTING ACCOMPLISHED (SECONDARY STRUCTURE).Jun 8, 2010 · N930FD · Boeing 757* · Fuselage Miscellaneous StructureSDR FDEA201006082019Floor Support · corrodedMAIN DECK FLOOR RT SHEAR WEB INBD SUPPORT ANGLE SRA 1180 TO 1291 HAS CORROSION AND CHAFE MARKS NEAR FASTENER HOLES. REMOVED FASTENERS IAW SRM 51-40-02. REMOVED CORROSION IAW SRM 51-10-02. CHECKED LIMITS AND FOUND OUT OF LIMITS IAW SRM 53-60-13, FIG 101, DEJun 8, 2010 · N930FD · Boeing 7572Y0 · Fuselage Miscellaneous StructureSDR FDEA201006082016Floorbeam · corrodedSTA 1600 FLOORBEAM SCRATCHES AND GOUGES FROM BL0 TO RBL 60. REMOVED SCRATCHED AND GOUGED AREAS IAW SRM 51-10-02, ORIG MAT .125 AFTER .115", MEASURED AREA L=24:00" X W=2.00", X DEPTH 0.010", FOUND OUT LIMITS IAW SRM 53-00-51, PAGE 103, FIG 101, DETAIL III,Jun 8, 2010 · N930FD · Boeing 7572Y0 · Fuselage Main, Floor BeamSDR FDEA201006081941Crease Beam · corrodedLT CREASE BEAM WEB HAS CORROSION BS 1020 TO 1040 STR 17L.Jun 8, 2010 · N930FD · Boeing 7572Y0 · Fuselage Main, StructureSDR FDEA201006081867Support Angle · corrodedMAIN DECK FLOOR LT SHEAR WEB INBD SUPPORT ANGLE, STA 755 HAS CORROSION.Jun 8, 2010 · N930FD · Boeing 7572Y0 · Fuselage Miscellaneous StructureSDR FDEA201006011778Crease Beam · corrodedRT CREASE BEAM OUTER CHORD STA 378 TO 430 CORRODED AT NUTPLATES AND FASTNER HOLES. REMOVED CORROSION IAW SRM 51-10-02, ON CREASE BEAM INBD CHORD, BS 297-430. FOUND TO BE OUT OF LIMITS IAW SRM 53-30-13, FIG 101, DETAIL 8; BEFORE: .071", AFTER: .057", LOSS: .01Jun 1, 2010 · N930FD · Boeing 7572Y0 · Fuselage Main, StructureSDR FDEA201006011752Floorbeam · corrodedFLOORBEAM UPPER CAP CORRODED STA 377, LBL 60 TO RBL 60. REMOVED CORROSION FROM RBL 16-60, ORIGINAL MATERIAL : .125", REMOVED: .008"; FOUND TO BE WITHIN LIMITS IAW SRM 53-00-51,FIG.101,DETAIL 3. REMOVED CORROSION FROM BS 377, RBL 15-LBL 60, ORIGINAL MATERIAL:Jun 1, 2010 · N930FD · Boeing 7572Y0 · Fuselage Main, Floor BeamSDR FDEA201006011749Crease Beam · corrodedRT CREASE BEAM INNER CHORD STA 820 TO 900 CORRODED. REMOVED CORROSION IAW SRM 51-10-02, FOUND TO BE OUT OF LIMITS IAW SRM 53-30-13, FIG 101, DETAIL 3; BEFORE: .080", AFTER: .061", REMOVED: .019". REMOVED RT CREASE BEAM INNER CHORD, BS 760-900, IAW SRM 51-40-Jun 1, 2010 · N930FD · Boeing 7572Y0 · Fuselage Main, Structure
Back to N930FD