Development of a Supplemental Inspection Document for the Fairchild SA226 and SA227 Aircraft, Part 2, Volume II

Abstract

This report (consisting of volume I and volume II) is the second phase of a three-phase program sponsored by the Federal Aviation Administration to develop a supplemental inspection document for the Fairchild SA226 and SA227 aircraft. In this report, the results of material characterization and testing are presented. Crack growth analysis of all the critical structural elements using NASGRO is performed and the results documented.

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Document Details

Document Type
Technical Report
Publication Date
Oct 01, 1999
Accession Number
ADA372525

Entities

People

  • W. Dwyer

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aircrafts
  • Computer Programs
  • Damage Tolerance
  • Digital Data
  • Fatigue Tests (Mechanics)
  • Fuselages
  • Gusts
  • Materials
  • Measurement
  • Mechanics
  • Modulus Of Elasticity
  • Spars
  • Tensile Strength
  • Tensile Testing
  • Test And Evaluation
  • Test Equipment
  • Test Methods

Readers

  • Business Analytics
  • Environmental Remediation and Restoration.
  • Structural Health Monitoring of Composite Structures.