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(IF ANY)
GEAR DISGREE Landing gear position does not match the gear lever
position.
“GEAR DISAGREE”
MLG BAY OVHT High temperature detected in the main landing gear
wheel bins.
“GEAR BAY OVHT”
NOSE DOOR OPEN
Nose doors are open for 10 seconds after the landing
gear is locked in position , or when airspeed is >250
KIAS.
“NOSE DOOR”
PARKING BRAKE The parking brake is set with the aircraft in the takeoff
mode,with N1 greater than 70% rpm.
”CONFIG BRAKES”
A/SKID INBD
A/SKID OUTBD The respective anti-skid channel has failed or is not armed.
INBD BRAKE PRESS
OUTBD BRAKE PRESS The respective brake system pressure is below 1,015 psi.
MLG OVHT FAIL The overheat detection loop in the gear bay is shorted out.
PARK BRAKE SOV The parking brake shutoff valve does not match the commanded position.
PROX SYS Indicates a failure in the PSEU output circuitry (may be accompanied by GND
SPLRS caution message).
STEERING INOP Nosewheel steering has failed.
WOW INPUT The PSEU is unable to determine if the aircraft is airborne or on the ground
(WOW CH 1 & CH 2 disagree).
WOW OUTPUT One or more critical drivers are not in expected state (see following table).
A/SKID IN TEST Anti-skid system is in self-test.
PARKING BRAKE ON The parking brake is activated, aircraft not in takeoff mode (WOW and N1 less
than 70% rpm).
PROX SYS FAULT Indicates a failure in the proximity sensor electronics unit.
WOW OUTPUT FAIL Indicates a weight-on-wheels output fault in a non-critical system (see following
table).
LANDING GEAR/BRAKES
Description
Vol. 2 15−10−22
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
POWER SUPPLY AND CIRCUIT BREAKER SUMMARY
SYSTEM SUB-SYSTEM CB NAME BUS BAR
CB
PANEL
CB
LOCATION
NOTES
Landing Gear
Proximity Sensing
WOW/GEAR/
SPLR 1
DC BUS 1
1
F2
WOW/GEAR/
SPLR 1
DC BATT N2
WOW/GEAR/
SPLR 2
DC BUS 2
2
F2
WOW/GEAR/
SPLR 2
DC BATT N2
Nosewheel Steering NOSE STEER
DC BUS 1 1 F6
DC BUS 2 2 F6
Anti-Skid ANTI SKID
DC BUS 1 1 F7
DC BUS 2 2
F7
Brakes
BRAKE PRESS
IND
G12
LANDING GEAR/BRAKES
Summary
Vol. 2 15−20−1
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
LANDING GEAR/BRAKES
Summary
Vol. 2 15−20−2
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
THIS PAGE INTENTIONALLY LEFT BLANK
DESCRIPTION
General 16−10−1
Exterior Lighting 16−10−1
Description 16−10−1
Components and Operation 16−10−1
Controls and Indicators 16−10−3
Flight Compartment Lighting 16−10−9
Description 16−10−9
Components and Operation 16−10−9
Controls and Indicators 16−10−12
Passenger Compartment (Cabin) Lighting 16−10−15
Description 16−10−15
Components and Operation 16−10−15
Cargo and Service Compartment Lighting 16−10−17
Description 16−10−17
Components and Operation 16−10−17
Emergency Lighting 16−10−19
Description 16−10−19
Components and Operation 16−10−19
Controls and Indicators 16−10−21
EICAS Messages 16−10−22
SUMMARY
Power Supply and Circuit Breaker Summary 16−20−1
LIST OF ILLUSTRATIONS
DESCRIPTION
Figure 16−10−1 Wing Tip Navigation Light 16−10−1
Figure 16−10−2 Exterior Lights − Navigation Lights Location 16−10−3
Figure 16−10−3 Exterior Lights − Anti−Collision Lights and Wing Inspection
Lights Location 16−10−4
Figure 16−10−4 Exterior Lights − Beacon Lights and Logo Lights Location 16−10−5
Figure 16−10−5 Exterior Lights − Landing Lights Location 16−10−6
LIGHTING
Table of Contents
Vol. 2 16−00−1
REV 66, Feb 01/07
CHAPTER 16 - LIGHTING
16−00−1
CL−604 Operating Manual
PSP 604−6
TABLE OF CONTENTS
Page
TABLE OF CONTENTS
LIST OF ILLUSTRATIONS
DESCRIPTION
Figure 16−10−6 Exterior Lights − Landing and Recognition/Taxi Lights
Location 16−10−7
Figure 16−10−7 Exterior Lights − Nose Landing Lights Location 16−10−8
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庞巴迪挑战者604操作手册 Operating Manual 4(53)
