Quantcast Speed Brake Liminations

 

Click here to make tpub.com your Home Page

Page Title: Speed Brake Liminations
Back | Up | Next

Click here for thousands of PDF manuals

Google


Web
www.tpub.com

Home

   
Information Categories
.... Administration
Advancement
Aerographer
Automotive
Aviation
Construction
Diving
Draftsman
Engineering
Electronics
Food and Cooking
Logistics
Math
Medical
Music
Nuclear Fundamentals
Photography
Religion
   
   

 



STUDENT GUIDE FOR T-1A AIRCRAFT SYSTEMS
CHAPTER FIVE
Speed Brake Indicator Light
A white annunciator on the CP shroud panel illuminates the letters SPD BRAKE EXTEND when
the speed brakes are not retracted.
510. SPEED BRAKE LIMITATIONS
Refer to Speed Brake Limitation, Section V, T.O. 1T-1A-1, for specific limitations of the speed
brakes.
511. LANDING GEAR SYSTEM
The landing gear system is an electrically controlled, hydraulically operated tricycle-type system.
The landing gear system consists of the following subsystems:
1.
Nosewheel steering subsystem
2.
Landing gear subsystem
3.
Brake subsystem
Nosewheel Steering Subsystem
The nosewheel steering subsystem provides aircraft directional control and shimmy dampening
during taxi, takeoff and landing. The system is mechanically controlled by rudder pedal action
and available only when the nose gear is extended.
Landing Gear Subsystem
The landing gear subsystem consists of the following components:
1.
Main landing gear
2.
Main landing gear fuselage and wing doors
3.
Nose landing gear
4.
Nose landing gear doors
5.
Landing gear control unit
6.
Nitrogen bottle
HYDRAULIC POWER SUPPLY & SYSTEMS
5-5


Privacy Statement - Press Release - Copyright Information. - Contact Us

Integrated Publishing, Inc.