曝光臺(tái) 注意防騙 網(wǎng)曝天貓店富美金盛家居專營(yíng)店坑蒙拐騙欺詐消費(fèi)者

Trim Systems ................................................................................................................. 15-6
Flaps.............................................................................................................................. 15-9
Speedbrakes ................................................................................................................. 15-12
CITATION MUSTANG OPERATING MANUAL
CITATION MUSTANG OPERATING MANUAL
15-ii 510OM-00
INTENTIONALLY LEFT BLANK
510OM-00 15-iii
CITATION MUSTANG OPERATING MANUAL
ILLUSTRATIONS
Figure TItle Page
15-1 Flight Control Surfaces .......................................................................................... 15-2
15-2 Rudder Control System Installation....................................................................... 15-4
15-3 Aileron/Elevator Control Lock .............................................................................. 15-5
15-4 Rudder Lock System (Left Side of Tail Cone) ...................................................... 15-5
15-5 Aileron and Rudder Trim....................................................................................... 15-6
15-6 Trim Display .......................................................................................................... 15-7
15-7 Elevator Trim System............................................................................................. 15-8
15-8 Flaps—LAND Position........................................................................................ 15-10
15-9 Flap System Schematic........................................................................................ 15-10
15-10 Flaps Position Display ......................................................................................... 15-11
15-11 Flaps Position Display—Reversionary Mode ..................................................... 15-11
15-12 Rotary TEST Knob .............................................................................................. 15-12
15-13 Speedbrakes (Extended) ...................................................................................... 15-12
15-14 Throttle Knob Speedbrake Switch (Left Throttle) .............................................. 15-13
CITATION MUSTANG OPERATING MANUAL
15-iv 510OM-00
INTENTIONALLY LEFT BLANK
510OM-00 15-1
CITATION MUSTANG OPERATING MANUAL
INTRODUCTION
This chapter describes the flight controls of the Cessna Model 510 Citation Mustang.
The aircraft has fixed and moveable surfaces that provide stability and control during
flight. The primary flight controls are ailerons, rudder, and elevators. Secondary flight
controls include trim devices, flaps, and speedbrakes. Control locks are also described.
GENERAL
The flight control systems consist of the control
surfaces, trim control surfaces, trim indicating
systems, and the related mechanical
and electrical systems that control the airplane
during flight.
The primary flight controls (elevators,
ailerons, and rudder) directly control aircraft
movement around the three axes of flight
(pitch, roll, and yaw). They are manually actuated
through cables by dual conventional
control yokes and dual sets of rudder pedals
in the cockpit. They can be immobilized by
control locks when on the ground to prevent
damage to the control surfaces and systems
from wind gusts striking the aircraft.
The secondary flight controls include trim,
flaps, and speedbrakes. Trim tabs, electrically
or mechanically adjusted through controls on the
cockpit pedestal or control yoke, assist flight
control on all three axes. Mechanical elevator
trim, adjusted through a cockpit pedestal wheel,
is also provided.
CHAPTER 15
FLIGHT CONTROLS
20
20
20
10
5
5
10 10
5
5
L O C
G
S
Flaps and speedbrakes directly adjust airplane
lift and drag. Both controls are electrically actuated.
Flaps are operated by a handle on the
cockpit pedestal. Speedbrakes are operated by
a switch on the throttle.
All flight control surfaces are shown in
Figure 15-1.
PRIMARY FLIGHT
CONTROLS
DESCRIPTION
The primary flight controls (ailerons, rudder,
and elevators) are manually operated by either
the pilot or the copilot through a conventional
control yoke and rudder pedal arrangement.
Control inputs are transmitted to the control
surfaces through cables, bellcranks, and
pushrods. The rudder pedals also operate the
nosewheel steering and wheel brakes (see
Chapter 14—“Landing Gear and Brakes”). A
flexible mechanical interconnect between the
　
中國(guó)航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：Cessna塞斯納公務(wù)機(jī)飛行手冊(cè)(87)