Cessna Single Engine High Wing Maintenance Fuel System

TRU, SIMULATION (2017) Cessna Single Engine High Wing Maintenance Fuel System. POLITEKNIK PENERBANGAN SURABAYA, 64.

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Abstract

Fuel flows by gravity from the two wing tanks to a three-position fuel selector valve, labeled BOTH, RIGHT and LEFT, and on to the
fuel reservoir tank. From the fuel reservoir tank, fuel flows through the electrically-driven auxiliary fuel pump, through the fuel shutoff
valve, the fuel strainer, and to the engine-driven fuel pump. From the engine driven fuel pump, fuel flows to the fuel/air control unit on
the bottom of the engine. The fuel/air control unit (fuel servo) meters fuel flow in proportion to induction air flow.

Item Type: Article
Subjects: T Technology > T Technology (General)
T Technology > TA Engineering (General). Civil engineering (General)
Divisions: Politeknik Penerbangan
Depositing User: Users 1 not found.
Date Deposited: 09 Jun 2023 05:26
Last Modified: 09 Jun 2023 05:26
URI: https://repo.poltekbangsby.ac.id/id/eprint/692

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