AC 61-22: Pilot Flight Tests in Small Airplanes with  Stability/Control Augmentation

doi:10.21949/1514755

i

AC 61-22: Pilot Flight Tests in Small Airplanes with Stability/Control Augmentation

1965-05-21
By United States. Department of Transportation. Federal Aviation Administration

File Language:

English

Details

Alternative Title:

Advisory Circulars from 1965
Corporate Creators:

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

Air Pilots Air Transportation Flight Tests Guidelines
Publication/ Report Number:

AC 61-22
DOI:

https://doi.org/10.21949/1514755
Resource Type:

Manual
Right Statement:

Public Domain
Geographical Coverage:

United States
Corporate Publisher:

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

This circular provides information to the public concerning flight tests conducted in small (12,500 pounds or less maximum authorized takeoff weight) airplanes equipped with gyroscopic stability/control augmentation systems.
Format:

PDF
Collection(s):

FAA Advisory Circulars
Main Document Checksum:

urn:sha-512:506fbe2a5d0bd412a2993b68cd0fc1e29050d1916d091c0ce8c669ce3512d46f88a8c4dc27d76ab9790a74c52ea372541cac0e8e3d445590217d418c62daa070
Download URL:

https://rosap.ntl.bts.gov/view/dot/71500/dot_71500_DS1.pdf
File Type:

[PDF - 67.25 KB ]

File Language:

English

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Details

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