N943FD

Service difficulty reports · 119

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 = 'N943FD' 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 FDEA201010134040Floorbeam · corrodedMAIN CARGO COMPARTMENT FLOOR BEAM UPPER CHORD HAS CORROSION ENTIRE LENGTH BS 1660 CHECKED LIMITS STA 1660 FLOORBEAM AT LBL 55. TO RBL 59 L=6.0 W = 2.0 AND D = .038, FOUND TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-00-51, FIG.101, DETAIL 3 . REMOVED AND REPOct 13, 2010 · N943FD · Boeing 7572G5 · Fuselage Main, Floor BeamSDR FDEA201010134041Floorbeam · corrodedMAIN CARGO COMPARTMENT FLOORBEAM UPPER CHORD HAS CORROSION ENTIRE LENGTH BS 1660 CHECKED LIMITS STA 1660 FLOORBEAM AT LBL 55 TO RBL 59. L=6.0 W = 2.0 AND D =.038, FOUND TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-00-51 . R & R STA 1660 FLOORBEAM IAW SRM 51-40-Oct 13, 2010 · N943FD · Boeing 7572G5 · Fuselage Main, Floor BeamSDR FDEA201010134039Seat Track · gougedBS 418-440, LBL 24, SEAT TRACK IS GOUGED. REMOVED GOUGE IAW SRM 51-10-02. AFTER REWORK, FOUND OUT OF LIMITS IAW SRM 53-00- 52, FIG.101, DETAIL 7; L=1.5",W=1.0",D=.019". FABRICATED NEW SEAT TRACK, MATL ID BAC 1520-792, BATCH 1891618. INSTALLED NEW SEAT TRACK Oct 13, 2010 · N943FD · Boeing 7572G5 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201010083976Shear Web · corrodedMAIN CARGO COMPARTMENT SHEAR WEB UPPER SIDE HAS CORROSION AND NUT PLATES CORROED BS 1680 TO BS 1720 BL 0 TO RBL 62. REMOVED CORROSION AT MAIN CARGO COMP . SHEAR WEB UPPER SIDE BS 1680 TO BS 1720 BL 0 TO RBL 62 IAW SRM 51-10-02. BLENED AREA L = 17" W = 1Oct 8, 2010 · N943FD · Boeing 7572G5 · Fuselage Miscellaneous StructureSDR FDEA201010053947Crease Beam · corrodedMAIN DECK LT INBD CREASE BEAM BETWEEN STA.1200-1260 HAS NUT PLATE HOLE CORROSIONS AND SHEARED SCREWS, AS MARKED. REMONED CORROSION IAW SRM 51-10-02 BLENED AREA ORIG MAT .071 L= 4" W=2" D= .020 FOUND OUT OF LIMITS IAW SRM 53-60-13 FIG 101 DET VIII . Oct 5, 2010 · N943FD · Boeing 7572G5 · Fuselage Main, StructureSDR FDEA201010043899Crease Beam · corrodedMAIN CABIN STA 877 LBL 68 CORROSION ON CREASE BEAM REMOVED CORROSION, BLENED AREA L = 2.0" W= 1.5" D=.020 ORGI MAT, .070 REMAINING MAT. .050 OUT OF LIMITS IAW SRM 53-30-13 FIG 101 DET, VIII REPLACED CREASE BEAM STA 760-900 LBL 68 IAW SRM 51-40-02. Oct 4, 2010 · N943FD · Boeing 7572G5 · Fuselage Main, StructureSDR FDEA201010043900Structure · corrodedCORROSION MAIN CABIN STA 1610 WL 200 RBL 68.Oct 4, 2010 · N943FD · Boeing 7572G5 · Fuselage Miscellaneous StructureSDR FDEA201009283774Floorbeam · corrodedMAIN CARGO COMPARTMENT FLOORBEAM UPPER TEE HAS CORROSION BS 377 BLENED AREA IAW SRM 51-10-01. FOUND MUITIABLE AREA OUT OF LIMITS , EXCEEDS MAX OF 10% OF ORIG MAT IAW SRM 53-00-51 FIGURE 101 DETAIL III . REMOVED AND REPLACED UPPER TEE IAW SRM 51-10-01. ISep 28, 2010 · N943FD · Boeing 7572G5 · Fuselage Main, Floor BeamSDR FDEA201009283773Floorbeam · corrodedMAIN CARGO COMPARTMENT FLOORBEAM UPPER TEE HAS CORROSION BS 363.25. BLENDED DAMAGED AREAS IAW SRM 51-10-01. AREAS OUT OF LIMITS IAW SRM 53-00-51, FIG.101, DETAIL 3. R & R UPPER TEE AT RBL 18-60, BS 363.25, IAW SRM 53-00-51, FIG 201, AND SRM 51-40-02. INSTSep 28, 2010 · N943FD · Boeing 7572G5 · Fuselage Main, Floor BeamSDR FDEA201009223645Intercostal · corrodedMAIN CARGO COMPARTMENT INTERCOSTAL HAS CORROSION AROUND HOLES BS 324 TO 340 RBL 25.75. ( ELONGATED HOLES )Sep 22, 2010 · N943FD · Boeing 7572G5 · Fuselage Miscellaneous StructureSDR FDEA201009223639Floor Support · corrodedMAIN CARGO COMPARTMENT FLOOR SUPPORT HAS CORROSION BS 324 TO 325 RBL 43Sep 22, 2010 · N943FD · Boeing 7572G5 · Fuselage Miscellaneous StructureSDR FDEA201009223619Floorbeam · corrodedMAIN CARGO COMPARTMENT FLOORBEAM UPPER CHORD CORRODED AROUND HOLES BS 480. FLOORBEAM WITHIN LIMITS AND CONSIDERED A MINOR REPAIR.Sep 22, 2010 · N943FD · Boeing 7572G5 · Fuselage Main, Floor BeamSDR FDEA201009213603Stringer · corrodedCORROSION FOUND AT STRINGER 3R BETWEEN STA 310.5-324. REMOVED CORROSION IAW SRM 51-10-02. BLENDED AREA L=4",W=1",D=.020". ORIGINAL MATL.050", REMAINING MATL. .030". FOUND OUT OF LIMITS IAW SRM 53-00-03, FIG 101, DETAIL REPAIRED S4R, AT BS 310.5-324, IAW SRM Sep 21, 2010 · N943FD · Boeing 7572G5 · Fuselage Main, Longeron/StringerSDR FDEA201009213599Crease Beam · corrodedMAIN DECK CREASE BEAM, STA 664-776 LBL 60 HAS CORROSION. REMOVED CORROSION ON LT SIDE CREASE BEAM IB CHORD AT STA 664-776 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-30-15, FIG 101, DETAIL IV. ORIG MATERIAL .080 AFTER REWORK .043. R & R CHORD IAW SRM 51-40-02.Sep 21, 2010 · N943FD · Boeing 7572G5 · Fuselage Main, StructureSDR FDEA201009213593Crease Beam · corrodedMAIN CARGO COMPARTMENT CREASE BEAM INBD CHORD CORRODED BS 297 TO BS 324, RBL 62. REMOVED CORROSION AT MAIN CARGO COMPARTMENT CREASE BEAM, BS 297-324, RBL 62, PER SRM 51-10-02. BLENDED AREA; L=18",W=1",D=.049". ORIGINAL MATL .071", MATL. REMAINING; .022". FOSep 21, 2010 · N943FD · Boeing 7572G5 · Fuselage Main, StructureSDR FDEA201009203583Crease Beam · corrodedMAIN CARGO COMPARTMENT CREASE BEAM INBD CHORD HAS CORROSION BS 755 TO BS 900, RBL-62. REMOVED CORROSION ON RT SIDE INBD CREASE BEAM CHORD AND FOUND TO BE OUT OF LIMITS IAW SRM 53-30-13 FIG 101 DETAIL II. REMOVED AND REPLACED CREASE BEAM CHORD IAW SRM 51-40-02Sep 20, 2010 · N943FD · Boeing 7572G5 · Fuselage Main, StructureSDR FDEA201009203571Frame · corrodedMAIN CARGO COMPARTMENT BULKHEAD UPPER CHORD HAS CORROSION BS 324 ENTIRE LENGTH. REMOVED CORROSION UPPER CHORD IAW SRM 51-10-02 . BLENDED AREA L= 44" W=3.0 " D=.039, ORIG MAT .125 REMAINING . 086 OUT OF LIMITS IAW SRM 53-10-08, FIG 101, DET 9. R & R UPPESep 20, 2010 · N943FD · Boeing 7572G5 · Fuselage Main, FrameSDR FDEA201009203560Floorbeam · corrodedMAIN CARGO COMPARTMENT FLOORBEAM UPPER CHORD HAS CHAFED MARK AND CORRODED AROUND HOLES BS 740, RBL 42. REMOVED CORRSION IAW SRM 51-10-02 , CHECKED LIMITS OF BLENDED AREA L=3.01' W= 2.00', D = .015 ORIGINAL MATERIAL .125 , REMAINING. 110, OUT OF LIMITS IAWSep 20, 2010 · N943FD · Boeing 7572G5 · Fuselage Main, Floor BeamSDR FDEA201009203559Floorbeam · corrodedFLOORBEAM UPPER CHORD LOWER SURFACE BS-720 LBL-58 HAS CORROSION. REMOVED CORROSION ON FLOORBEAM UPPER CHORD AT STA 720, LBL 58 IAW SRM 51-10-02. BLEND OUT DIM. =3.5" L2.0" W .019"D, ORIG MATL THICKNESS = .125, FOUND OUT OF LIMITS IAW SRM 53-00-51, FIG 101, DSep 20, 2010 · N943FD · Boeing 7572G5 · Fuselage Main, Floor Beam
Back to N943FD