N964FD

Service difficulty reports · 184

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 = 'N964FD' 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 FDEA201205251971Crease Beam · damagedRT CREASE BEAM ANGLE BETWEEN STA 940-980 RBL 64 HAS TWO AREAS OF DAMAGE. BLENDED AREA IAW SRM 51-10-02 CHECKED LIMITS. ORIGINAL MATERIAL .063 REWORK .040 MATERIAL LOSS .023 CREASE BEAM FOUND TO BE OUT OF LIMITS IAW SRM 53-60-13, DETAIL VIII, FIG 101. R & R May 25, 2012 · N964FD · Boeing 757200 · Fuselage Main, StructureSDR FDEA201205251968Skin · misrepairedEXTERNAL FUSELAGE SKIN AT BS 1380-1400, BETWEEN S27R - S30R. DOES NOT COMPLY WITH SRM. ACCOMPLISHED EA F-5330-160580. MAJOR REPAIR.May 25, 2012 · N964FD · Boeing 757200 · Fuselage Main, Plate/SkinSDR FDEA201205251967Frame · dentedFRAME AT BS 660, BETWEEN S24R AND S25R HAS DENT IN UPPER FLANGE, FOUND TO BE OUT OF LIMITS IAW SRM 53-30-07, FIG 101, SH 1. REMOVED AND INSTALLED NEW FRAME IAW SRM 51-40-02 AND DWG 143N1024. MAJOR REPAIR.May 25, 2012 · N964FD · Boeing 757200 · Fuselage Main, FrameSDR FDEA201205241962Crease Beam · corrodedCREASE BEAM INNER CORD AT STA 1628 RT IS CORRODED. R & R CREASE BEAM IAW SRM 51-40-02 AND DWG 146N5590-57. MAJOR REPAIR.May 24, 2012 · N964FD · Boeing 757200 · Fuselage Main, StructureSDR FDEA201205241961Crease Beam · corrodedCREASE BEAM INNER CORD STA 1628 LT IS CORRODED. BLENDED AREA IAW-SRM-51-10-02, CHECKED LIMITS, ORIG MATERIAL 0.079, MATERIAL LOSS 0.070, MATERIAL REMAINING 0.009, CREASE BEAM FOUND TO BE OUT OF LIMITS IAW-SRM-53-60-13, FIG 101, DETAIL VIII. R & R CREASE BEAMay 24, 2012 · N964FD · Boeing 757200 · Fuselage Main, StructureSDR FDEA201205181878Frame · dentedFRAME DENTED, BS 1400 S25L. R & R FRAME IAW SRM 51-40-02 AND DWG 146N1011. MAJOR REPAIR.May 18, 2012 · N964FD · Boeing 757200 · Fuselage Main, FrameSDR FDEA201205181884Frame · corrodedCABIN FRAME SUPPORT HAS 4 ATTACH BOLTS CORRODED AT STA 1260, STR 2R. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07, FIG 101, DETAIL II, SECTION AA ALLOWABLE DAMAGE 2. REPAIRED FRAME SECTION FROM STRG 3RH TO 6LH IAW SRM 53-00-07, REPAIR 3 CATEGORY "B" MAJOR REPAMay 18, 2012 · N964FD · Boeing 757200 · Fuselage Miscellaneous StructureSDR FDEA201205181882Frame · corrodedBS 1300, S26R, CORROSION ON FWD SIDE OF FRAME AFT BAGGAGE COMPARTMENT. REMOVED CORROSION IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07, FIG 101, DETAIL II. R & R FRAME IAW SRM 51-40-02 AND DWG 146N1006. MAJOR REPAIR.May 18, 2012 · N964FD · Boeing 757200 · Fuselage Main, FrameSDR FDEA201205181881Frame · damagedAFTER REMOVAL OF TRANSITION PANEL FOUND DAMAGE ON FRAME BS 1340 STR 28L AFT CARGO BAY. FOUND DAMAGE TO BE .026 DEEP ORIGINAL MATERIAL .071 MATERIAL REMAINING .045 OUT OF LIMITS IAW SRM 53-00-07, FIG 101 ALLOWABLE DAMAGE 2. NO DAMAGE ALLOWED IN FLANGE OF FRAMMay 18, 2012 · N964FD · Boeing 757200 · Fuselage Main, FrameSDR FDEA201205171825Seat Track · gougedMAIN DECK SEAT TRACK GOUGED AT FS 700 TO 780 RBL 45.50. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, FIG 101, DETAIL I. REMOVED AND INSTALLED NEW SEAT TRACK IAW SRM 51-40-02 AND DWG 143N5085. MAJOR REPAIR.May 17, 2012 · N964FD · Boeing 7572B7 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201205161818Floorbeam · damagedFLOORBEAM UPPER TEE BS 1640 LBL 58 TO RBL 58 HAS SEVERAL AREAS OF DAMAGE. FLOORBEAM REPLACED IAW SDR 12-2016, NO FURTHER ACTION.May 16, 2012 · N964FD · Boeing 757200 · Fuselage Main, Floor BeamSDR FDEA201205121806Skin · corrodedUPPER WING CENTER BOX UPPER EXTERNAL SKIN UNDER STUB BEAM AT BS 940, RBL 63, CORRODED. REMOVED CORROSION, FOUND OUT OF LIMITS IAW SRM 57-10-01, FIG 101, TABLE 1, NOTE A. COMPLIED WITH EA F-5710-159946. MAJOR REPAIR.May 12, 2012 · N964FD · Boeing 757200 · Fuselage Main, Plate/SkinSDR FDEA201205121805Skin · corrodedRT UPPER CENTER WING BOX EXTERNAL SKIN AT BS 960, RBL 64 CORRODED. REMOVED CORROSION, FOUND OUT OF LIMITS IAW SRM 57-10-01, FIG 101, TABLE 1, NOTE A. COMPLIED WITH EA F-5730-160574. MAJOR REPAIR.May 12, 2012 · N964FD · Boeing 757200 · Fuselage Main, Plate/SkinSDR FDEA201205121804Skin · corrodedCORROSION ON CENTER WING BOX UPPER SKIN, UPPER SURFACE AT BS 940, LBL 63. REMOVED CORROSION, FOUND OUT OF LIMITS IAW SRM 57-10-01, FIG 101, TABLE 1 NOTE A. REPAIRED IAW NR 4774935 AND EA 757-5710-16-F3831. MAJOR REPAIR.May 12, 2012 · N964FD · Boeing 757200 · Fuselage Main, Plate/SkinSDR FDEA201205111800Floorbeam · corrodedFLOORBEAM BS 1681 UPPER CAP CORRODED BL 0 TO RBL 62. BLENDED AREA, ORIGINAL MATERIAL 0.156, AFTER REWORK 0.124, MATERIAL LOSS 0.032 FLOORBEAM FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51, DETAIL II, FIG 101. R & R FLOORBEAM IAW SRM 51-40-02 AND DWG 146N5111. May 11, 2012 · N964FD · Boeing 757200 · Fuselage Main, Floor BeamSDR FDEA201205111799Frame · dentedBS 1260, STR 26L HAS A DENT IN FRAME AFT BAGGAGE. R & R FRAME STA 1260 S-25L TO S-25R IAW SRM 51-40-02 AND DWG 146N1004. MAJOR REPAIR.May 11, 2012 · N964FD · Boeing 757200 · Fuselage Main, FrameSDR FDEA201205111797Skin · corrodedCABIN SKIN HAS CORROSION AROUND DOME NUTS BS 1500-1520, STRINGER 1-2L.May 11, 2012 · N964FD · Boeing 757200 · Fuselage Main, Plate/SkinSDR FDEA201205021712Skin · gougedFUSELAGE SKIN BS 1380, S-25R EDGE OF CARGO DOOR CUTOUT GOUGED. ACCOMPLISHED EA F-5330-160578. MAJOR REPAIR.May 2, 2012 · N964FD · Boeing 757200 · Fuselage Main, Plate/SkinSDR FDEA201204271656Skin · corrodedRT WING ROOT T/E UPPER SURFACE AT REAR SPAR WITH PANEL REMOVED, SUPPORT HAS CORROSION. REPAIRED IAW EA F-5710-159940, STEPS 1-10. MAJOR REPAIR.Apr 27, 2012 · N964FD · Boeing 757200 · Wing, Plate/SkinSDR FDEA201204241558Seat Track · damagedSEAT TRACK BS 440-650 LBL 45, CORRODED AND GOUGED.Apr 24, 2012 · N964FD · Boeing 757* · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201204181482Floorbeam · corrodedFLOORBEAM UPPER TEE AT BS 1660 HAS SEVERAL NICKS, GOUGES, AND CORROSION AROUND NUT PLATE HOLES AND VICINITY OF RBL 58. FLOORBEAM WAS FOUND OUT OF LIMITS IAW SRM 53-00-51, FIG 101, DETAIL II AND III. ORIGINAL MATERIAL .125 AFTER REWORK .060. R & R FLOORBEAM Apr 18, 2012 · N964FD · Boeing 757200 · Fuselage Main, Floor BeamSDR FDEA201204181481Floorbeam · corrodedFLOORBEAM BS 720 BL 0 TO LBL 70 WL 208.1 UPPER TEE CORRODED. FLOORBEAM WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51 FIG 101 DETAIL II AND III. ORIGINAL MATERIAL .125 AFTER REWORK .020. REMOVED AND REPLACED FLOORBEAM IAW DWG 143N5015 SH7 AND SRM 51-40-02.Apr 18, 2012 · N964FD · Boeing 757200 · Fuselage Main, Floor BeamSDR FDEA201204181480Floorbeam · corrodedFLOORBEAM UPPER TEE BS 780 LBL 24 TO RBL 25 CORRODED. FLOORBEAM WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51, FIG 101, DETAIL II AND III. ORIGINAL MATERIAL .125 AFTER REWORK .094. R & R FLOORBEAM IAW DWG 143N5067, SH 1, REV A. MAJOR REPAIR.Apr 18, 2012 · N964FD · Boeing 757200 · Fuselage Main, Floor BeamSDR FDEA201204181479Floorbeam · corrodedFLOORBEAM BS 700 RBL 24 TO LBL 70 WL 208.1 UPPER TEE CORRODED. FLOORBEAM WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51, FIG 101, DETAIL II AND III. ORIGINAL MATERIAL .125 AFTER REWORK .022. R & R FLOORBEAM IAW DWG 143N5014 SH7 AND SRM 51-40-02. MAJOR REPAApr 18, 2012 · N964FD · Boeing 757200 · Fuselage Main, Floor BeamSDR FDEA201204181478Floorbeam · corrodedFLOORBEAM BS 680 LBL 24 TO RBL 27 UPPER TEE CORRODED. FLOORBEAM WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51, FIG 101, DETAIL II AND III. R & R FLOORBEAM IAW DWG 143N5013, SH2, REV C AND SRM 51-40-02. MAJOR REPAIR.Apr 18, 2012 · N964FD · Boeing 757200 · Fuselage Main, Floor BeamSDR FDEA201204171463Floorbeam · corrodedFLOORBEAM UPPER TEE BS 760, RBL 8 TO LBL 24 CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51, FIG 101, DETAIL II AND III. R & R FLOORBEAM IAW DWG 143N5430 SH19 AND DWG 143N5017, SH1, REV A, MAJOR REPAIR.Apr 17, 2012 · N964FD · Boeing 757200 · Fuselage Main, Floor BeamSDR FDEA201204171462Floorbeam · corrodedFLOORBEAM BS 740 LBL 14 UPPER TEE CORRODED. FLOORBEAM FOUND OUT OF LIMITS IAW SRM 53-00-1, FIG 101, DETAIL II AND III. ORIGINAL MATERIAL .125 AFTER REWORK .070. R & R FLOORBEAM IAW SRM 51-40-02 AND DWG 143N5016, SH 5. MAJOR REPAIR.Apr 17, 2012 · N964FD · Boeing 7572G5 · Fuselage Main, Floor BeamSDR FDEA201204161442Floorbeam · corrodedFLOORBEAM, BS 333.45 LBL 45 - LBL 62 WL 208.1 UPPER TEE CORRODED. R & R FLOORBEAM IAW-SRM-51-40-02, CORROSION OUT OF LIMITS IAW-SRM-53-00-51,FIG.101,III, THIS IS A MAJOR REPAIR, CAT."A".Apr 16, 2012 · N964FD · Boeing 757200 · Fuselage Main, Floor BeamSDR FDEA201204161441Floorbeam · corrodedFLOORBEAM BL0 - RBL 62 WL 201.1, UPPER CHORD CORRODED. R & R UPPER TEE IAW SRM 51-40-02 AND DWG 141N5810. MAJOR REPAIR.Apr 16, 2012 · N964FD · Boeing 757200 · Fuselage Main, Floor BeamSDR FDEA201204141428Floorbeam · corrodedFLOORBEAM, BS 377.7, UPPER TEE, LBL 62-RBL 62, CORRODED. BLENDED AREA ORIG MATERIAL .125 AFTER REWORK .087 MATERIAL LOSS .038 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51, FIG 101, DETAIL III, L=3.0 W=2.0 W=.038. R & R FLOORBEAM IAW SRM 51-40-02 AND DWG 141NApr 14, 2012 · N964FD · Boeing 757* · Fuselage Main, Floor BeamSDR FDEA201204141427Floorbeam · corrodedFLOORBEAM BS 395, BL 0-62, UPPER TEE CORRODED. BLENDED IAW SRM 51-10-02, ORIG MATERIAL .125, AFTER REWORK .084, TOTAL MATERIAL LOSS .041, AREA OUT OF LIMITS. REMOVED DAMAGED FLOORBEAM IAW SRM 51-40-02. DRILLED AND LOCATED NEW FLOORBEAM IAW SRM 51-40-05. IApr 14, 2012 · N964FD · Boeing 757* · Fuselage Main, Floor BeamSDR FDEA201204141424Floorbeam · corrodedFLOORBEAM BS 365.25 BL0 TO RBL 61 WL 208.1, UPPER CHORD CORRODED. BLENDED CORROSION IAW SRM 51-10-02 CHECKED LIMITS IAW SRM 53-00-51, FIG 101, FOUND TO OUT OF LIMITS. R & R FLOORBEAM IAW SRM 51-40-02 AN D DWG 141N5112. MAJOR REPAIR.Apr 14, 2012 · N964FD · Boeing 757200 · Fuselage Main, Floor BeamSDR FDEA201204141420Floorbeam · corrodedFLOORBEAM BS 345, LBL 18 - RBL 8, WL 208.1, UPPER TEE CORRODED. R & R FLOORBEAM IAW SRM 51-40-02 AND DWG 141N5111.Apr 14, 2012 · N964FD · Boeing 757* · Fuselage Main, Floor BeamSDR FDEA201204141406Floorbeam · corrodedFLOORBEAM BS 324 LBL 30-RBL 61, WL.208.1, UPPER TEE CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51, FIG 101, DETAIL III. R & R FLOORBEAM UPPER TEE IAW SRM 51-40-02 AND DWG 141N5160. MAJOR REPAIR.Apr 14, 2012 · N964FD · Boeing 757200 · Fuselage Main, Floor Beam
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