N962FD

Service difficulty reports · 130

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 = 'N962FD' 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 FDEA201203211048Bulkhead · gougedNR 2 PYLON BULKHEAD PP STA 174.3, RT HALF, GOUGED FWD AND AFT SIDE AT UPPER BOLT.Mar 21, 2012 · N962FD · Boeing 7572G5 · Nacelle/Pylon, Bulkhead/FirewallSDR FDEA201203211047Bulkhead · corrodedLEFT PYLON MID BULKHEAD FWD FACE WITH CORROSION. REMOVED CORROSION IAW SRM 51-10-02, FOUND TO BE OUT OF LIMITS IAW SRM 54-50-02, PAGE 105, FIG 101, DETAIL IV. CAT "A" MAJOR REPAIR.Mar 21, 2012 · N962FD · Boeing 7572G5 · Nacelle/Pylon, Bulkhead/FirewallSDR FDEA201203211046Fastener · damagedLEFT PYLON, RT SIDE ACCESS THRU PANEL NR 433LR MID BULKHEAD UPPER SIDE WITH DAMAGED FASTENER. BLENDED IAW EA F-5450-159926.Mar 21, 2012 · N962FD · Boeing 7572G5 · Nacelle/Pylon Miscellaneous StructureSDR FDEA201203160982Seat Track · gougedLBL 45, SEAT TRACK DIRTY AND GOUGED ON INSIDE AND TOP SURFACES BS 1320-1540. REMOVED DAMAGE IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, PAGE 102 AND 103, FIG 101, DETAIL 1. R & R SEAT TRACK IAW SRM 51-40-02 AND DWG 146N5134. MAJOR REPAIMar 16, 2012 · N962FD · Boeing 7572G5 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201203160981Seat Track · corrodedLBL 25, SEAT TRACK CORRODED BS 1610-1640. FOUND OUT OF LIMITS IAW SRM 53-00-52, PAGE 104, FIG 101, DETAIL 7. FABRICATED AND INSTALLED NEW SEAT TRACK IAW SRM 53-60-52, AND DWG 146N5217. MAJOR REPAIR.Mar 16, 2012 · N962FD · Boeing 7572G5 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201203150955Floorbeam · corrodedBS 1360, FLOORBEAM LOWER FLANGE BOTTOM SURFACE CORRODED AT FASTENER HOLES LBL 45 TO RBL 45. R & R FLOORBEAM, AT BS 1360, IAW SRM 51-40-02 AND DWG 146N5009. REMOVED DAMAGE AT BS 1360, LBL 2, 40, 45, AND RBL 20, IAW SRM 51-10-02, FOUND TO BE OUT OF LIMITS IAW SMar 15, 2012 · N962FD · Boeing 7572G5 · Fuselage Main, Floor BeamSDR FDEA201203140939Crease Beam · corrodedMAIN CABIN LEFT BS 395 - 377, S17L CREASE BEAM CORRODED.Mar 14, 2012 · N962FD · Boeing 7572G5 · Fuselage Main, StructureSDR FDEA201203140946Skin · corrodedLT PYLON ACCESS THRU PANEL 433AL HAS CORROSION IN BETWEEN CUT-OUT AND SKIN. REMOVED CORROSION IAW SRM 51-10-02. CHECKED LIMIT OF REMOVAL, REMOVED .017, ORIGINAL .090, REMAINING .063, OUT OF LIMITS IAW SRM 54-50-01, FIG 101, DETAIL V. LOCATED, DRILLED ANMar 14, 2012 · N962FD · Boeing 7572G5 · Nacelle/Pylon, Plate/SkinSDR FDEA201203140945Skin · corrodedLEFT PYLON CORROSION ON PANEL 433GR CUT-OUT. REMOVED CORROSION IAW SRM 51-10-02. MATERIAL LOSS OUT OF LIMITS IAW SRM 54-50-01, FIG 101, DETAIL 5. INSTALLED NEW FWD RT SKIN IAW SRM 51-40-02 AND BAC DWG 311N5002. MAJOR REPAIRMar 14, 2012 · N962FD · Boeing 7572G5 · Nacelle/Pylon, Plate/SkinSDR FDEA201203140944Skin · corrodedNR 2 PYLON LT DOOR 443GL CUT-OUT HAS CORROSION. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 54-50-01, PG 103, FIG 101. REMOVED INBD FWD SKIN IAW SRM 51-40-02. LOCATED,DRILLED AND COUNTERSUNK NEW SKIN IAW SRM 51-40-02 AND DWG 311N5002. INSTALLEDMar 14, 2012 · N962FD · Boeing 7572G5 · Nacelle/Pylon, Plate/SkinSDR FDEA201203140943Skin · corrodedNR 2 PYLON RT PANEL 443 AR CUT OUT HAS CORROSION SPOTS.Mar 14, 2012 · N962FD · Boeing 7572G5 · Nacelle/Pylon, Plate/SkinSDR FDEA201203140940Floorbeam · damagedBS 1540 FLOORBEAM UPPER SURFACE SCRATCHED AND GOUGED BL 0- LBL 60. REMOVED DAMAGE IAW-SRM-51-10-02. CHECKED LIMITS ORIG MAT= .125" AFTER REWORK=.090" FOUND TO BE OUT OF LIMITS IAW-SRM-53-00-51, FIG 101, DETAIL II AND III. REMOVED AND REINSTALLED SHEAR WEBSMar 14, 2012 · N962FD · Boeing 7572G5 · Fuselage Main, Floor BeamSDR FDEA201203130928Skin · corrodedLEFT PYLON, LT SIDE THRU ACCESS PANEL, NR 433BL, CORROSION ON INTERNAL SKIN. REMOVED CORROSION IAW SRM 51-10-02. MATERIAL LOSS .023, ORIGINAL .090, REMAINING .067, OUT OF LIMITS OF SRM 54-50-01, FIG 101, DETAIL V. LOCATED, DRILLED AND COUNTERSUNK NEW SKINMar 13, 2012 · N962FD · Boeing 7572G5 · Nacelle/Pylon, Plate/SkinSDR FDEA201203130927Skin · corrodedNR 2 PYLON LT SKIN HAS CORROSION SPOTS ON P-STA 128-136. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW SRM 54-50-01, FIG 101, DETAIL V. INSTALLED NEW SKIN IAW SRM 51-40-02 AND DWG 311N5002. MAJOR REPAIR.Mar 13, 2012 · N962FD · Boeing 7572G5 · Nacelle/Pylon, Plate/SkinSDR FDEA201203130914Frame · corrodedAFT CARGO BAY, STA 1380 STR 29L-29R, FRAME LOWER CHORD CORRODED. REMOVED CORROSION ORIG MAT .090 AFTER REWORK MAT WAS .061 WITH MATERIAL LOSS OF .029 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07, FIG 101, DETAIL 2. INSTALLED FAILSAFE AND TWO VERTICAL SUPPORTS Mar 13, 2012 · N962FD · Boeing 7572G5 · Fuselage Main, FrameSDR FDEA201203120899Floorbeam · corrodedMAIN DECK FLOORBEAM UPPER TEE CORRODED, BL 0 - RBL 11, BS 377. REPAIRED IAW SRM 51-40-02 AND SRM 53-00-51, AND INSTALLED UPPER TEE AND REPAIR IAW SRM 53-00-51. REPAIR 3, FIG 101. MAJOR REPAIR.Mar 12, 2012 · N962FD · Boeing 7572G5 · Fuselage Main, Floor BeamSDR FDEA201203120896Seat Track · corrodedMAIN CABIN SEAT TRACK RBL 44 BS 1320-1340 CORRODED.Mar 12, 2012 · N962FD · Boeing 7572G5 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201203120898Seat Track · gougedSEAT TRACK GOUGED, RBL 45.5, BS 408.Mar 12, 2012 · N962FD · Boeing 7572G5 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201203120897Seat Track · corrodedSEAT TRACK FLANGE CORRODED, BS 365-377, RBL 45.5. BLENDED CORROSION IAW SRM 51-10-02. ORIG MATERIAL THICKNESS WAS .090 AFTER REWORK .070 TOTAL MATERIAL LOSS WAS .020. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, FIG 101 DETAIL VIII. FABRICATED NEW SEAT TRACMar 12, 2012 · N962FD · Boeing 7572G5 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201203100870Frame · corrodedAFT CARGO BAY BS 1260, STR30 FRAME CORRODED.Mar 10, 2012 · N962FD · Boeing 7572G5 · Fuselage Main, FrameSDR FDEA201203100869Frame · corrodedAFT CARGO BAY STRINGERS 28-29R, FRAME CORRODED.Mar 10, 2012 · N962FD · Boeing 7572G5 · Fuselage Main, FrameSDR FDEA201203100876Crease Beam · corrodedMAIN CABIN LT SIDE BETWEEN BS333.45 TO BS310.5 CREASE BEAM CORRODED. REMOVED CORROSION IAW SRM 51-10-02, MAT LOSS .002, ORIG MAT .071, AFTER BLEND .069, FOUND TO BE WITHIN LIMITS IAW SRM 53-30-13, FIG.101, PAGE 105.Mar 10, 2012 · N962FD · Boeing 7572G5 · Fuselage Main, StructureSDR FDEA201203100875Crease Beam · corrodedMAIN CABIN LT SIDE BS 418-395 CREASE BEAM CORRODED.Mar 10, 2012 · N962FD · Boeing 7572G5 · Fuselage Main, StructureSDR FDEA201203100874Skin · corrodedNR 2 PYLON RT INTERNAL SKIN, PP STA144-153, CORRODED. REMOVED CORROSION IAW SRM 51-10-02. CHECKED LIMITS AND FOUND OUT OF LIMITS IAW SRM 54-50-01, FIG 101, DETAIL IV. REMOVED AND INSTALLED NEW RT SIDE SKIN IAW SRM 51-40-02 AND DWG 311N5002.Mar 10, 2012 · N962FD · Boeing 7572G5 · Nacelle/Pylon, Plate/SkinSDR FDEA201203090853Web · corrodedSHEAR DECK BS 1680-1720, BL 0 - RBL 60 HAS NUMEROUS AREAS OF CORROSION.Mar 9, 2012 · N962FD · Boeing 7572G5 · Fuselage Miscellaneous StructureSDR FDEA201203090846Floorbeam · corrodedCABIN FLOORBEAM BS 365.25, BL 0 - RBL 61, UPPER TEE CORRODED. REMOVED CORROSION, ORIGINAL MATERIAL .125", REMOVED .090", FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51, FIG 101, SHEET 4, DETAIL 3. REPAIRED FLOORBEAM AT BS 365.25, BL 0 - RBL 61, IAW SRM 53-00Mar 9, 2012 · N962FD · Boeing 7572G5 · Fuselage Main, Floor BeamSDR FDEA201203090859Web · corrodedSHEAR DECK UPPER SURFACE BS 1680-1720, BL 0 - LBL 60 HAS NUMEROUS AREAS OF CORROSION. MINOR REPAIR.Mar 9, 2012 · N962FD · Boeing 7572G5 · Fuselage Miscellaneous StructureSDR FDEA201203090860Floorbeam · corrodedMAIN CABIN FLOORBEAM BS 1280, RBL 41 HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-02. FOUND OUT OF LIMITS IAW SRM 53-00-51, FIG 101, PG 104, DETAIL IV. FABRICATED NEW FOORBEAM, IAW SRM 53-60-51, PG 5, FIG 1, DETAIL II, SRM 51-40-02, DWG 146N5005. INSTALLMar 9, 2012 · N962FD · Boeing 7572G5 · Fuselage Main, Floor BeamSDR FDEA201203090855Floorbeam · corrodedMAIN CABIN FLOORBEAM, BS 1320 BETWEEN LBL 25 AND RBL 25 HAS CORROSION. REMOVED DAMAGE IAW SRM 51-10-02. FOUND OUT OF LIMITS IAW SRM 53-00-51, PAGE 104, DETAILS III AND IV. REMOVED FLOORBEAM IAW SRM 51-40-02. FABRICATED NEW FLOORBEAM IAW SRM 53-60-51, PAGE 2Mar 9, 2012 · N962FD · Boeing 7572G5 · Fuselage Main, Floor BeamSDR FDEA201203080826Floorbeam · corrodedBS 1640 FLOORBEAM UPPER SURFACE CORRODED FROM LBL 60 TO RBL 60. REMOVED DAMAGE PER SRM 51-10-02, FOUND OUT OF LIMITS PER SRM 53-00-51, FIG. 1, DETAIL IV, PAGE 104. REPLACED FLOORBEAM PER SRM 53-60-51, PAGE 5, FIG. 1, DETAIL II, SRM 51-40- 02, AND BOEING DRMar 8, 2012 · N962FD · Boeing 7572G5 · Fuselage Main, Floor Beam
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