N961FD

Service difficulty reports · 80

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 = 'N961FD' 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 FDEA201210303779Strap · corrodedRT APU INLET DOOR FLANGE TO FUSELAGE HAS CORROSION REMOVED CORROSION FROM FWD STRAP IAW SRM 51-10-02 ORIGINAL MATERIAL . 10 REMAINING .060 OUT OF LIMITS IAW SRM 53-00-01, FIG 101, DETAIL II. R & R FWD STRAP STA 1787 S-3R TO S-6R IAW SRM 51-40-02 AND DWG 148NOct 30, 2012 · N961FD · Boeing 7572Y0 · Fuselage Miscellaneous StructureSDR FDEA201210293772Support · corrodedAPU DOOR INLET UPPER SUPPORT BS 1787 - 1825 S3R CORRODED. REMOVED CORROSION AT APU INLET UPPER SUPPORT IAW SRM 51-10-02. BLENDED AREA ORIGINAL MATERIAL .063 MATERIAL REMAINING .023 MATERIAL REMOVED .040 FOUND TO BE OUT OF LIMITS IAW SRM 53-80-15 FIG 101 DETOct 29, 2012 · N961FD · Boeing 7572Y0 · Fuselage Miscellaneous StructureSDR FDEA201210293771Support · corrodedAPU INLET LOWER SUPPORT BS 1787 -1825 S6R CORRODED. REMOVED CORROSION AT APU INLET SUPPORT IAW SRM 51-10-02. BLENDED AREA ORIGINAL MAT .063 MATERIAL REMOVED .040 MATERIAL REMAINING .023 FOUND TO BE OUT OF LIMITS IAW SRM 53-80-15, FIG 101, DETAIL II. R & R Oct 29, 2012 · N961FD · Boeing 7572Y0 · Fuselage Miscellaneous StructureSDR FDEA201210273762Panel · crackedNR 2 SLAT COVE PANEL CRACKED JUST INBD OF OTBD MAIN SLAT TRACK. REMOVED AND REPLACED NR 2 SLAT COVE PANEL IAW SRM 51-40-02 AND DWG 114N4076. MAJOR REPAIR.Oct 27, 2012 · N961FD · Boeing 7572Y0 · Leading Edge DevicesSDR FDEA201210273761Panel · crackedNR 2 SLAT COVE PANEL CRACKED JUST INBD OF INBD MAIN SLAT TRACK. REMOVED AND REPLACED NR 2 SLAT COVE PANEL IAW SRM 51-40-02 AND DWG 114N4076. MAJOR REPAIR.Oct 27, 2012 · N961FD · Boeing 7572Y0 · Leading Edge DevicesSDR FDEA201210253751Panel · corrodedNR 1 SLAT HAS CORROSION AROUND FASTENERS BEHIND OTBD MAIN SLAT COVE PANEL. CLEANED CORROSION IAW SRM-51-10-02, REMOVED .025 FROM ORIGINAL THICKNESS OF .050 AND .025 REMAINING.FOUND TO BE OUT OF LIMITS IAW SRM 57-43-01 FIG.101 DETAIL IV PG.104. LOCATED AND DOct 25, 2012 · N961FD · Boeing 7572Y0 · Leading Edge DevicesSDR FDEA201210243741Web · crackedFOUND WEB, BS 660-680 S17R CRACKED. WEB FOUND TO BE OUT OF LIMITS IAW SRM 53-30-13, FIG 101, DETAIL V, PAGE 103. R & R WEB IAW SRM 51-40-02 AND DWG 143N8322. MAJOR REPAIR.Oct 24, 2012 · N961FD · Boeing 7572Y0 · Fuselage Miscellaneous StructureSDR FDEA201210223707Skin · dentedEXTERNAL FUSELAGE SKIN DENTED BS 660-680 BETWEEN S25 - 26L. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01 FIG 101 DETAIL III. REMOVED DAMAGE IAW SRM 53-00-01 FIG 201 REPAIR 7. NO CRACKS FOUND AROUND DAMAGED AREA, FABRICATED REPAIR PARTS IAW SRM 53-00-01 REPAIR Oct 22, 2012 · N961FD · Boeing 7572Y0 · Fuselage Main, Plate/SkinSDR FDEA201210193698Crease Beam · corrodedCREASE BEAM WEB AT BS 1420-1440 CORRODED. REMOVED CORROSION IAW SRM 51-10-02, WEB FOUND TO BE OUT OF LIMITS IAW SRM 53-60-13, FIG.101, DET III PG.103, A2. REMOVED AND REPLACED WEB IAW SRM 51-40-02 & DWG 146N5590. MAJOR REPAIR.Oct 19, 2012 · N961FD · Boeing 7572Y0 · Fuselage Main, StructureSDR FDEA201210063575Flange · corrodedAPU INTAKE DUCT CUT-OUT AFT FLANGE HAS CORROSION AT BS 1825. REMOVED CORROSION IAW SRM 51-10-02 ORIGINAL MATERIAL .10 REMAINING .060 OUT OF LIMITS IAW SRM 53-00-01, FIG 101, DETAIL II. REPAIRED AFT STRAP IAW SRM 53-80-15, FIG 202, REPAIR NR1, MAJOR REPAIR.Oct 6, 2012 · N961FD · Boeing 7572Y0 · Fuselage Main, Plate/SkinSDR FDEA201209283503Skin · misrepairedSKIN MISREPAIRED AT BS 667 BETWEEN S27R TO S-28R REPAIRED IAW SRM 53-00-01, FIG 201, REPAIR 16. MAJOR REPAIR.Sep 28, 2012 · N961FD · Boeing 7572Y0 · Fuselage Main, Plate/SkinSDR FDEA201209253438Frame · misrepairedFRAME MISREPAIRED AT BS 1280 STR 9-13L. REPAIRED FRAME IAW SRM 53-00-07 FIG 201 PG 202 REPAIR 3.Sep 25, 2012 · N961FD · Boeing 7572Y0 · Fuselage Main, FrameSDR FDEA201209253437Frame · misrepairedFRAME MISREPAIRED AT 1280 STR 9-13R. REPAIRED FRAME IAW SRM 53-00-07 FIG 201 PG 202 DETAIL I REPAIR 3.Sep 25, 2012 · N961FD · Boeing 7572Y0 · Fuselage Main, FrameSDR FDEA201209193359Seat Track · gougedMAIN CABIN AREA BETWEEN BS 700 - 780 LBL 45 SEAT TRACK NICKED, GOUGED, AND SCRATCHED. REPAIR CLASSIFIED AS A MINOR REPAIR.Sep 19, 2012 · N961FD · Boeing 7572Y0 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201209193358Seat Track · gougedMAIN CABIN AREA BETWEEN BS 640- 685 LBL 25 SEAT TRACK WITH NICKS, GOUGE, AND SCRATCHES. REPAIR CLASSIFIED AS A MINOR.Sep 19, 2012 · N961FD · Boeing 7572Y0 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201209113285Frame · dentedCABIN FRAME HAS A DENT BS 377, STR 6R. COMPLIED WITH EA F-5310-162465Sep 11, 2012 · N961FD · Boeing 7572Y0 · Fuselage Main, FrameSDR FDEA201209043223Floorbeam · corrodedCABIN FLOORBEAM HAS CORRISION BS 324, RBL 32 TO RBL 64. REMOVED AND REPLACED FLOORBEAM TEE IAW SRM 51-40-02 AND DWG 141N293. MAJOR REPAIR.Sep 4, 2012 · N961FD · Boeing 7572Y0 · Fuselage Main, Floor BeamSDR FDEA201209013205Floorbeam · corrodedMAIN CABIN FLOORBEAM BS 740, LBL 45 - 60 HAS CORROSION ON UPPER ANGLE. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51 FIG 101 DETAIL III. REPAIRED FLOORBEAM UPPER ANGLE IAW SRM 53-00-51 FIG 201 REPAIR 3. MAJOR REPAIR.Sep 1, 2012 · N961FD · Boeing 7572Y0 · Fuselage Main, Floor BeamSDR FDEA201208143002Crease Beam · corrodedMAIN CABIN AREA BETWEEN BS 1220- 1260, STR 17L CREASE BEAM CORRODED. R & R IAW SRM 51-40-02 AND DWG 146N5590. MAJOR REPAIR.Aug 14, 2012 · N961FD · Boeing 7572Y0 · Fuselage Main, StructureSDR FDEA201208082900Stringer · corrodedSTRINGER 17R , BS 1320-1380 CORRODED.Aug 8, 2012 · N961FD · Boeing 7572Y0 · Fuselage Main, Longeron/StringerSDR FDEA201208082899Floorbeam · corrodedMAIN CABIN SEC 41, AREA AT BS 345, LBL 4 HAS CORROSION ON FLOORBEAM. FLOORBEAM REPAIRED IAW SRM 53-00-01, FIG 201, PG 201, REPAIR 3 AND DWG 141N5160. MAJOR REPAIR.Aug 8, 2012 · N961FD · Boeing 7572Y0 · Fuselage Main, Floor BeamSDR FDEA201208062864Seat Track · damagedSEAT TRACK BS 1540 - 1640 RBL 45, NICKED, GOUGED, AND CORRODED. REMOVED DAMAGE IAW SRM 51-10-02, SEAT TRACK FOUND OUT OF LIMITS IAW SRM 53-00-52. DETAIL VII PG 102, FIG 101 R & R STEAT TRACK IAW SRM 53-00-52 AND DWG 146N5125. MAJOR REPAIR.Aug 6, 2012 · N961FD · Boeing 7572Y0 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201208042841Floorbeam · corrodedFLOORBEAM UPPER TEE, BS 1640 BL 0 - RBL 65, CORRODED. R & R FLOORBEAM IAW DWG 146N5500 SH 1, REV D AND SRM 51-40-02. FLOORBEAM FOUND TO BE OUT OF LIMITS IAW SRM 53-60-51, FIG 101 AND SRM 53-00-51, FIG 101, SH4. MAJOR REPAIR.Aug 4, 2012 · N961FD · Boeing 7572Y0 · Fuselage Main, Floor BeamSDR FDEA201207282732Floorbeam · corrodedCABIN FLOORBEAM HAS CORROSION BS 365, LBL 34- RBL.70. REPAIRED FLOORBEAM UPPER TEE IAW SRM 53-00-51, FIG 201, REPAIR 3. THIS IS A CAT "A" MAJOR REPAIR.Jul 28, 2012 · N961FD · Boeing 7572Y0 · Fuselage Main, Floor BeamSDR FDEA201207252679Web · corrodedSTRINGER 17R WEB LOWER SIDE, BS 1350-1360 CORRODED. FOUND TO BE IN LIMITS.Jul 25, 2012 · N961FD · Boeing 757200 · Fuselage Miscellaneous StructureSDR FDEA201207252678Crease Beam · corrodedSTRINGER 17R CREASE BEAM WEB, BS 1360-1380 CORRODED. REPAIR CONSIDERED MINOR.Jul 25, 2012 · N961FD · Boeing 7572Y0 · Fuselage Main, StructureSDR FDEA201207202626Crease Beam · corrodedMAIN CABIN AREA, STRINGER 17L CREASE BEAM BS 730-760 CORRODED. REMOVED CORROSION IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-30-15, FIG 101, DETAIL IV. R & R IAW SRM 51-40-02 AND DWG 143N8322. MAJOR REPAIR.Jul 20, 2012 · N961FD · Boeing 7572Y0 · Fuselage Main, StructureSDR FDEA201207202625Stringer · corrodedSTRINGER 17R BS 660-760, CORRODED. REMOVED CORROSION IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-30-15, FIG 101, DETAIL IV. INSTALLED STRINGER IAW SRM 51-40-02. MAJOR REPAIR.Jul 20, 2012 · N961FD · Boeing 7572Y0 · Fuselage Main, Longeron/StringerSDR FDEA201207192619Floorbeam · corrodedMAIN CABIN SEC 41, AREA AT BS 377.7 FLOORBEAM CORRODED. BLENDED CORROSION IAW SRM 51-10-02. CHECKED LIMITS IAW SRM 53-00-51, FIG 101, DETAIL III, D=.029 W=.6 L=1.3 ORIGINAL MATERIAL THICKNESS, .150 AFTER BLEND .121 FOUND TO BE OUT OF LIMITS. REMOVED FLOORBEAMJul 19, 2012 · N961FD · Boeing 7572Y0 · Fuselage Main, Floor BeamSDR FDEA201207032458Crease Beam · corrodedAT BS 1440 INNER CREASE BEAM CORRODED ON RT SIDE.Jul 3, 2012 · N961FD · Boeing 7572Y0 · Fuselage Main, Structure
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