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

doi:10.21949/1514756

i

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

1966-03-16
By United States. Department of Transportation. Federal Aviation Administration

File Language:

English

Details

Alternative Title:

Advisory Circulars from 1966
Corporate Creators:

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

Air Pilots Air Transportation Aviation Certification Guidelines
Publication/ Report Number:

AC 61-22A
DOI:

https://doi.org/10.21949/1514756
Resource Type:

Manual
Right Statement:

Public Domain
Geographical Coverage:

United States
Corporate Publisher:

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

This circular rescinds the limitation introduced by Advisory Circular No. 61-22 for pilot certificates issued on the basis of flight training and tests in airplanes equipped with gyroscopic stability/ control augmentation systems.
Format:

PDF
Collection(s):

FAA Advisory Circulars
Main Document Checksum:

urn:sha256:e90c92267d95b4bf355c9222b202d93dba47a181de9c0cf4bec240566a60b8be
Download URL:

https://rosap.ntl.bts.gov/view/dot/71501/dot_71501_DS1.pdf
File Type:

[PDF - 49.61 KB ]

File Language:

English

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