AC 90-14A: Altitude - Temperature Effect on Aircraft Performance

United States. Department of Transportation. Federal Aviation Administration

doi:10.21949/1515005

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AC 90-14A: Altitude - Temperature Effect on Aircraft Performance

1968-01-26
By United States. Department of Transportation. Federal Aviation Administration

[PDF-216.79 KB]

English

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Details:

Alternative Title:

Advisory Circulars from 1968
Corporate Creators:

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

[+]

Air Pilots Air Transportation Automation Guidelines
Publication/ Report Number:

AC 90-14A
DOI:

https://doi.org/10.21949/1515005
Resource Type:

Manual
Right Statement:

Public Domain
Geographical Coverage:

United States
Corporate Publisher:

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

This circular introduces the Denalt Performance Computer and reemphasizes the hazardous effects density altitude can have on aircraft performance.
Format:

PDF
Collection(s):

FAA Advisory Circulars
Main Document Checksum:

[+]

urn:sha256:c2f65442c53ea36599d1391614592814bc4741186372b0446afe4c8c37b2e403
Download URL:

https://rosap.ntl.bts.gov/view/dot/72080/dot_72080_DS1.pdf
File Type:

No Additional Files

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AC 90-14A: Altitude - Temperature Effect on Aircraft Performance

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