FAA AC 91-75 : 2003
Current
The latest, up-to-date edition.
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
|
| FAA AC 23.1311-1 : 2011 | INSTALLATION OF ELECTRONIC DISPLAY IN PART 23 AIRPLANES |
| SAE AS 396 : 1958 | BANK AND PITCH INSTRUMENTS (INDICATING STABILIZED TYPE) (GYROSCOPIC HORIZON, ATTITUDE GYRO) |
| FAA AC 23-17 : 2011 | SYSTEMS AND EQUIPMENT GUIDE FOR CERTIFICATION OF PART 23 AIRPLANES AND AIRSHIPS |
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