|
LANDING GEAR Table of Contents Vol. 2 15.00.1
Oct 05/06
CHAPTER 15 - LANDING GEAR
TABLE OF CONTENTS
Page
TABLE OF CONTENTS 15.00.1
DESCRIPTION
General 15.10.1
Landing Gear 15.10.1
Description 15.10.1
Components 15.10.2
Operation 15.10.5
Proximity Sensing Electronic Unit (PSEU) 15.10.10
Description 15.10.10
Operation 15.10.10
Main Wheel Bins and Overheat Detection 15.10.11
Description 15.10.11
Components and Operation 15.10.11
Nose Wheel Steering System 15.10.11
Description 15.10.11
Components and Operation 15.10.12
Wheels and Brakes 15.10.14
Description 15.10.14
Components and Operation 15.10.14
Controls and Indicators 15.10.17
EICAS Messages 15.10.19
SUMMARY
Power Supply and Circuit Breaker Summary 15.20.1
LIST OF ILLUSTRATIONS
DESCRIPTION
Figure 15.10.1 Landing Gear 15.10.1
Figure 15.10.2 Main Landing Gear 15.10.3
Figure 15.10.3 Nose Gear 15.10.5
Figure 15.10.4 Normal Gear Extension 15.10.7
Figure 15.10.5 Alternate Gear Extension 15.10.9
Figure 15.10.6 MLG BAY OVHT TEST Switches 15.10.11
Figure 15.10.7 Steering Tiller 15.10.13
LANDING GEAR Table of Contents Vol. 2 15.00.2
Oct 05/06
Page
LIST OF ILLUSTRATIONS
DESCRIPTION
Figure 15.10.8 Brakes and Lower Main Gear Structure 15.10.15
Figure 15.10.9 HYDRAULIC Synoptic Page (Inboard and Outboard Brake
Pressure) 15.10.15
Figure 15.10.10 PARKING BRAKE Handle 15.10.16
Figure 15.10.11 Landing Gear Panel 15.10.17
Figure 15.10.12 Landing Gear Manual Release 15.10.17
Figure 15.10.13 Landing Gear EICAS Page 15.10.18
LANDING GEAR/BRAKES Description Vol. 2 15.10.1
Oct 05/06
The landing gear for the Challenger 605 is arranged in a standard retractable tricycle configuration. Associated subsystems include:
.
Proximity sensing system;
.
Nose gear doors;
.
Nosewheel steering;
.
Wheel brakes with anti-skid; and
.
Main landing gear overheat detection.
Hydraulic system 3 powers landing gear extension and retraction, nosewheel steering, and brakes.
Landing Gear
| 