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Check AVAIL light out.
(b) BLEED AIR, APU LCV
switch/light ...............................................Press out to close load control valve.
Check APU LCV OPEN light
out.
When rpm decreases to below 50% and EGT to below 350°C (662°F):
(c) APU, PWR FUEL switch/light ..................Press out Check the following:
• APU GEN OFF caution
message out.
• APU gauges disappear
from status page after
approximately 60 seconds.
(9) AIR-CONDITIONING, L and R
PACK switch/lights ..........................................Press out to turn off packs.
Check L and R PACK OFF
lights on.
(10) BLEED AIR, 10TH STAGE ISOL
switch/light .......................................................Press out to match isolation valve
position.
Check ISOL OPEN light out.
(11) BLEED AIR, 14TH STAGE
L and R switch/lights .......................................Press out to close left and right valves.
NORMAL PROCEDURES
Terminating
Vol. 1 04−10−1
REV 75, Feb 17/09
▼
CL−604 Operating Manual
PSP 604−6
1. TERMINATING (CONT'D)
A. Securing Check (Cont’d)
(12) BATT MASTER switch .........................................Select to OFF.
(13) MISC LTS switches ..............................................Select to OFF.
(14) Oil master chip detector indicators .......................Check 2
NOTE
When leaving the airplane with no maintenance personnel in
attendance, the doors must be closed.
NORMAL PROCEDURES
Terminating
Vol. 1 04−10−2
REV 74, Nov 07/08
CL−604 Operating Manual
PSP 604−6
INTRODUCTION
General 05−01−1
Landing Distance Factors 05−01−1
POWER PLANT
Power Plant 05−02−1
Reverser Unsafe to Arm 05−02−1
In-Flight Engine Failure/Shutdown 05−02−1
APR Failure 05−02−4
Inadvertent APR Command 05−02−5
Uncommanded Deceleration or Abnormal Engine Oscillation/Fluctuation 05−02−6
N1 Fan Vibration 05−02−7
N2 Core Vibration 05−02−8
Engine Hot Start 05−02−9
Engine DCU Parameter Disagreement 05−02−9
Thrust Lever Inoperative 05−02−10
Fluctuating Engine Oil Pressure 05−02−11
SINGLE ENGINE PROCEDURES
Single Engine Procedures 05−03−1
Engine Failure During Take-Off After Achieving V1 05−03−1
Engine Failure During Approach 05−03−2
Single Engine Procedure 05−03−3
Single Engine Approach and Landing 05−03−4
Single Engine Go-Around 05−03−5
AIR START
Air Start 05−04−1
Windmilling Air Start Procedure 05−04−1
Engine Cross Bleed − Air Start Procedure 05−04−4
ABNORMAL PROCEDURES
Table of Contents
Vol. 1 05−00−1
REV 76, Jul 17/09
CHAPTER 5 - ABNORMAL PROCEDURES
05−00−1
CL−604 Operating Manual
PSP 604−6
TABLE OF CONTENTS
Page
TABLE OF CONTENTS
AIR - CONDITIONING AND PRESSURIZATION
Air-Conditioning and Pressurization 05−05−1
Air-Conditioning Pack High Pressure 05−05−1
Air-Conditioning Pack High Temperature 05−05−2
Automatic Pressurization System Malfunction 05−05−3
Air-Conditioning Pack Pressure/Regulating Valve Failure 05−05−4
Cabin Altitude Too High 05−05−5
Landing Altitude High 05−05−6
Unpressurized Flight Procedure 05−05−6
Manual Cabin Pressurization Control Procedure 05−05−7
Display Overtemperature 05−05−8
Cabin Pressure Acquisition Module Failure 05−05−9
AUTOMATIC FLIGHT CONTROL SYSTEM
Automatic Flight Control System 05−06−1
Autopilot Mistrim 05−06−1
Autopilot Pitch Trim Failure 05−06−2
Double Yaw Damper Failure 05−06−3
Single Flight Director Failed 05−06−4
AUXILIARY POWER UNIT
Auxiliary Power Unit 05−07−1
APU Load Control Valve Fails to Close 05−07−1
APU Low Oil Pressure 05−07−2
APU High Oil Temperature 05−07−3
APU Shut-Off Valve Failed to Close, After APU Shutdown Due to Fire 05−07−4
APU Fuel Shut-Off Valve not in the Selected Position 05−07−4
APU Negative-G Shut-Off Valve Failed to Close After APU Shutdown Due to
Fire 05−07−5
APU Pump Failure 05−07−5
DOORS
Doors 05−08−1
　
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