曝光臺 注意防騙 網曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

the heat away. The temperature of the
pressure vessel air supply is regulated by a
valve, which varies the amount of pylon ram
air flowing over the heat exchangers.
The cooled, pressurized bleed air enters the
pressure vessel through a set of valves. Pressure
regulating shutoff valves (PRSOVs) ensure
that a constant bleed-air pressure is maintained
regardless of engine power settings. Flow control
valves adjust flow to compensate for single-
engine operation. The inboard bleed air
from both engines supply temperature-controlled
bleed air directly to the pressure vessel.
Pressure vessel air supply is discussed in
more detail in Chapter 11—“Air Conditioning.”
The pressure vessel air supply exhausts overboard
through nominal leakage in the cabin and
through controlled venting by outflow valves
in the aft cabin pressure bulkhead. The outflow
valves are controlled by the pressurization system
to maintain adequate cabin pressure at all
altitudes. The pressurization system is explained
in detail in Chapter 12—
“Pressurization.”
COMPRESSED NITROGEN
BOTTLES
Separate bottles of pressurized nitrogen supply
emergency pneumatic power for emergency
landing gear extension and emergency braking.
Landing Gear Emergency
Extension (Blow-Down)
An independent emergency pneumatic system
uses pressurized nitrogen in a bottle for
emergency landing gear extension (blowdown).
The high-pressure nitrogen bottle is attached
to the right forward bulkhead inside the
nose baggage compartment. Emergency gear
extension is pilot-activated with the AUXILIARY
GEAR CONTROL handle. This system
is explained in Chapter 14—“Landing Gear
and Brakes.”
Emergency Brakes
An independent emergency pneumatic system
uses pressurized nitrogen in a bottle for
emergency braking. The high-pressure nitrogen
bottle is attached to the right forward
bulkhead inside the nose baggage compartment.
Emergency braking is pilot-activated
with the EMERGENCY BRAKE handle. This
system is explained in Chapter 14—“Landing
Gear and Brakes.”
CITATION MUSTANG OPERATING MANUAL
9-4 510OM-00
CHAPTER 10
ICE AND RAIN PROTECTION
CONTENTS
Page
INTRODUCTION................................................................................................................. 10-1
GENERAL ............................................................................................................................ 10-1
ENGINE INLETS ................................................................................................................. 10-3
Description.................................................................................................................... 10-3
Components ................................................................................................................... 10-3
Controls and Indications................................................................................................ 10-5
Operation ....................................................................................................................... 10-5
SURFACE DEICE (WING AND STABILIZERS)............................................................... 10-5
Description.................................................................................................................... 10-5
Components ................................................................................................................... 10-6
Controls and Indications................................................................................................ 10-7
Operation ....................................................................................................................... 10-7
WINDSHIELD ICE AND RAIN PROTECTION ................................................................ 10-8
Description and Components......................................................................................... 10-8
Controls and Indications................................................................................................ 10-9
Operation ..................................................................................................................... 10-11
SENSOR ANTI-ICE SYSTEMS ........................................................................................ 10-11
Description and Components ...................................................................................... 10-11
Controls and Indications.............................................................................................. 10-11
Operation ..................................................................................................................... 10-11
　
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：Cessna塞斯納公務機飛行手冊(50)