Name: FAA AC 91-75 : 2003
Brand: FAA

ATTITUDE INDICATOR

Published date

01-12-2013

Publisher

Federal Aviation Administration

1. PURPOSE
2. RELATED READING MATERIALS
3. BACKGROUND
4. DISCUSSION
5. RATIONALE FOR CHANGE
6. COMPLIANCE REQUIREMENTS
7. RECOMMENDATIONS

Describes a method to substitute an approved attitude indicator for the rate-of-turn indicator mandated by Title 14 of the Code of Federal Regulations (14 CFR) part 91, section 91.205(d)(3). Applicable to part 23-certificated airplanes (or airplanes certificated under earlier equivalent regulations) that weigh less than 12,500 pounds and are operated under part 91.

DocumentType	Standard
PublisherName	Federal Aviation Administration
Status	Current

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SAE AS 396 : 1958	BANK AND PITCH INSTRUMENTS (INDICATING STABILIZED TYPE) (GYROSCOPIC HORIZON, ATTITUDE GYRO)
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