曝光台 注意防骗
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END
G. TCAS System Failure
Indication: TCAS FAIL caution message on PFD and/or MFD.
(1) Radio tuning unit, TCAS page,
AUTO/STBY line select key ..................................Press to select STBY mode.
Check TCAS OFF indicated
on MFDs/PFDs.
END
ABNORMAL PROCEDURES
Aural/Visual Warning System
05−18−2
REV 71, Oct 31/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. AURAL/VISUAL WARNING SYSTEM (CONT'D)
H. TCAS Resolution Advisory Failure
Indication: TCAS RA FAIL caution message on PFD.
TCAS RA FAIL message displayed on both PFD:
Yes
(1) Radio tuning unit, TCAS
page, AUTO/STBY line
select key.......................................................Press to select TA ONLY mode.
Check TA ONLY indicated on
MFDs/PFDs.
− END −
No
TCAS RA FAIL caution message on one PFD.
(1) Pilot with functional RA-display would be required to carry out any subsequent
avoidance maneuvers.
END
I. TCAS Traffic Advisory Failure
Indication: TCAS TA FAIL caution message on MFD.
TCAS TA FAIL message displayed on both MFDs:
Yes
(1) No further action required. Assume loss of TA data on
both MFDs.
RA data remains available.
− END −
No
TCAS TA FAIL message displayed on one MFD:
(1) Other MFD............................................................... Use to obtain TA data.
END
J. TCAS Traffic Display Failure
Indication: TD FAIL caution message on MFD.
(1) No further action required. Assume loss of TA data on
both MFDs.
RA data remains available.
END
ABNORMAL PROCEDURES
Aural/Visual Warning System
05−18−3
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
ABNORMAL PROCEDURES
Aural/Visual Warning System
05−18−4
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
THIS PAGE INTENTIONALLY LEFT BLANK
GENERAL
Introduction 06−01−1
Conversion Data 06−01−2
Temperature Conversion 06−01−2
Wind Component 06−01−4
Calibration 06−01−6
Airspeed Position Error Correction – Primary Flight Display 06−01−6
Altitude Position Error Correction – Primary Flight Display 06−01−8
Airspeed Position Error Correction – Standby Airspeed Indicator (Flaps Up) 06−01−10
Altitude Position Error Correction – Standby Altimeter (Flaps Up) 06−01−12
Airspeed Position Error Correction – Standby Airspeed Indicator (Flaps 20°,
30°, 45°) 06−01−14
Altitude Position Error Correction – Standby Altimeter (Flaps 20°, 30°, 45°) 06−01−16
Flight Capabilities 06−01−18
Reference Stall Speed – Flaps 0°/Landing Gear Up 06−01−18
Reference Stall Speed – Flaps 20°/Landing Gear Up 06−01−20
Reference Stall Speed – Flaps 30°/Landing Gear Up 06−01−22
Reference Stall Speed – Flaps 45°/Landing Gear Down 06−01−24
Maneuvering Capabilities 06−01−26
Performance Conditions and Configurations 06−01−28
Minimum Control Speed, Air (VMCA) 06−01−28
Minimum Control Speed, Ground (VMCG) 06−01−28
Minimum Control Speed, Landing (VMCL) 06−01−28
Demonstrated Crosswind (Take-Off and Landing) 06−01−28
Maximum Tailwind (Take-Off and Landing) 06−01−29
Configurations and Thrusts 06−01−29
THRUST SETTINGS
Thrust Settings 06−02−1
General 06−02−1
Thrust Setting Charts 06−02−2
PERFORMANCE
Table of Contents
06−00−1
REV 66, Feb 01/07
CHAPTER 6 - PERFORMANCE
06−00−1
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
TABLE OF CONTENTS
Page
TABLE OF CONTENTS
THRUST SETTINGS
Normal Take-Off Thrust 06−02−3
Single Engine Climb Thrust (APR Rating) 06−02−10
Maximum Continuous Thrust, Single Engine Climb 06−02−17
TAKE-OFF PERFORMANCE
Introduction 06−03−1
Maximum Allowable Take-Off Weight 06−03−1
Take-Off Weight Limited By Climb Requirements – Flaps 20° 06−03−2
Take-Off Weight Limited By Brake Energy – Flaps 20° 06−03−6
Take-Off Weight Limited by Maximum Tire Speed 06−03−8
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庞巴迪挑战者604飞机飞行手册CL604 Airplane Flight Manual 2(30)
