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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SEHW_ATA28_FuelSystem.pdf
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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: | Mr Perpustakaan Poltekbang Surabaya |
| 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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