AC 20-26 CHANGE 1: Turbine and Compressor Rotors Type Certification Substantiation Procedures

doi:10.21949/1514206

i

AC 20-26 CHANGE 1: Turbine and Compressor Rotors Type Certification Substantiation Procedures

1964-09-18
By United States. Department of Transportation. Federal Aviation Administration

File Language:

English

Details

Alternative Title:

Advisory Circulars from 1964
Corporate Creators:

United States. Department of Transportation. Federal Aviation Administration
Subject/TRT Terms:

Air Pilots Air Transportation Guidelines
Publication/ Report Number:

AC 20-26 CHANGE 1
DOI:

https://doi.org/10.21949/1514206
Resource Type:

Manual
Right Statement:

Public Domain
Geographical Coverage:

United States
Corporate Publisher:

United States. Department of Transportation. Federal Aviation Administration
Abstract:

This circular transmits a revised page. CHANGE. The overspeed r.p.m. figure in paragraph 4c(2)(a) is revised to read 115 percent. Testing a complete engine to 115 percent is considered substantially equivalent to rig testing rotor components separately to 120 percent.
Format:

PDF
Collection(s):

FAA Advisory Circulars
Main Document Checksum:

urn:sha-512:2b0126a7c0c6ccd0b9a68642ebafa40d1123791f01bbfbf8ae8c0506fab12b2f0307f526309a964310294fd6618ceb4e7fd16cfa594a92a48853281b81cfddde
Download URL:

https://rosap.ntl.bts.gov/view/dot/70951/dot_70951_DS1.pdf
File Type:

[PDF - 214.04 KB ]

File Language:

English

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