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FAA AC 20-95 : 0

Superseded

Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

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superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

FATIGUE EVALUATION OF ROTORCRAFT STRUCTURE

Available format(s)

Hardcopy , PDF

Superseded date

02-12-2003

Language(s)

English

SECTION 1 INTRODUCTION
  1 BACKGROUND
SECTION 2 FLIGHT STRAIN MEASUREMENT PROGRAM
  2 General
  3 Instrumentation
  4 Parts to be strain-gaged
  5 Flight regimes and conditions to be investigated
SECTION 3 FREQUENCY OF LOADING
  6 Type of operation
  7 Loading spectrum
SECTION 4 FATIGUE STRENGTH EVALUATION
  8 General
  9 Analytical method
  10 Testing methods
  11 Combination replacement time and fail-safe evaluation
  12 Extension of replacement time
SECTION 5 FAIL-SAFE STRENGTH EVALUATION
  13 General
  14 Identification of critical portions of primary structure
  15 Extent of fail-safe damage
  16 Determination of probable failure locations
  17 Fail-safe demonstration
  18 Inspection
TABLE 1 PERCENT OF OCCURRENCE
FIGURES 1 Power On - Rotor R.P.M. Airspeed Envelope
        2 Power Off - Rotor R.P.M. Airspeed Envelope
        3 Oscillatory off - Rotor R.P.M. Airspeed Envelope
        4 Stress vs. Number of Cycles

Gives an acceptable means of compliance with the provisions of Federal Aviation regulations, Section 27-.571 and 29.571 dealing with the fatigue evaluation of rotorcraft structure.

DocumentType
Standard
Pages
20
PublisherName
Federal Aviation Administration
Status
Superseded
SupersededBy

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US$40.00
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