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Summary
DescriptionAbsolute and Service Ceilings.jpg
English: At the absolute ceiling,
there is no excess of power and only one speed allows steady,
level flight. The service ceiling is the altitude at
which the aircraft is unable to climb at a rate greater than 100
feet per minute (fpm)
Date
Source
Pilot's Handbook of Aeronautical Knowledge, FFA-H-8083-25B, https://www.faa.gov/regulations_policies/handbooks_manuals/aviation/phak/
Author
U.S. Dept. of Transportation, FAA
Licensing
Public domainPublic domainfalsefalse
This work is in the public domain in the United States because it is a work prepared by an officer or employee of the United States Government as part of that person’s official duties under the terms of Title 17, Chapter 1, Section 105 of the US Code.
Note: This only applies to original works of the Federal Government and not to the work of any individual U.S. state, territory, commonwealth, county, municipality, or any other subdivision. This template also does not apply to postage stamp designs published by the United States Postal Service since 1978. (See § 313.6(C)(1) of Compendium of U.S. Copyright Office Practices). It also does not apply to certain US coins; see The US Mint Terms of Use.
This file has been identified as being free of known restrictions under copyright law, including all related and neighboring rights.
https://creativecommons.org/publicdomain/mark/1.0/PDMCreative Commons Public Domain Mark 1.0falsefalse
Captions
Coefficients of Drag and Lift vs AOA, with Best Angle of Climb and Best Rate of Climb airspeeds
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media type
image/jpeg
checksum
7b80cd4f5801a549d3a56cbb9ed12fc01ad6f683
determination method: SHA-1
data size
116,861 byte
height
615 pixel
width
630 pixel
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17:05, 7 February 2021
630 × 615 (114 KB)
Pi3.124
Uploaded a work by U.S. Dept. of Transportation, FAA from Pilot's Handbook of Aeronautical Knowledge, FFA-H-8083-25B, https://www.faa.gov/regulations_policies/handbooks_manuals/aviation/phak/ with UploadWizard
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