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T/C, TOC Top Of Climb
T/D, TOD Top Of Descent
T/R Thrust Reverser
TACAN UHF Tactical Air Navigation
Aid
TAS True Airspeed
TAT Total Air Temperature
TCAS Traffic Alert and Collision
Avoidance System
TE Trailing Edge
TEMP Temperature
TGT Target
TO, T/O Take-off
TOL Tolerance
TRB, TURB Turbulence
TRK Track
TRM Trim
TRU Transformer Rectifier Unit
TT2 Engine inlet temperature
U
UNSCHD Unscheduled
USB Upper Side Band
USG United States Gallons
UTIL Utility
V
V Volt
VLOF Lift-Off Speed
VMC Minimum Control Speed with
the Critical Engine
Inoperative
VMO/MMO Maximum Operating Limit
Speed/Mach number
V1 Take-Off Decision Speed
(formerly Denoted as Critical
Engine Failure Speed)
INTRODUCTION
General
01−01−16
REV 77, Oct 20/09
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
5. ABBREVIATIONS (CONT'D)
V2 Take-Off Safety Speed
V2min Minimum Take-Off Safety
Speed
V/S Vertical Speed
V-MDA Vertical Minimum Descent
Altitude
VERT Vertical
VFR Visual Flight Rules
VG Vertical Gyro
VHF Very High Frequency
(30 – 300 mHz)
VIB Vibration
VMC Visual Meteorological
Conditions
VNAV Vertical Navigation
VOL Volume
VOLT Voltage
VOR VHF Omnidirectional Range
Station
VORTAC VOR and TACAN co-located
VSI Vertical Speed Indicator
W
WARN Warning
W/C Wind Component
W/S Wind Shear
W/W Wheel Well
WGT Weight
WHLS Wheels
WIND Window
WOW Weight-On-Wheels
WPT(s) Waypoint(s)
WSHLD Windshield
WX Weather
WXR Weather Radar
X
X Cross Transfer
XFER, XFR Transfer
XFLOW Cross Flow
XMIT Transmit
XPNDR Transponder
XTK Cross Track
XWC Cross Wind Component
Y
YD, Y/D Yaw Damper
Z
ZFW Zero Fuel Weight
INTRODUCTION
General
01−01−17
REV 77, Oct 20/09
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
6. REGISTRY CODES
The following registry codes are utilized throughout the Airplane Flight Manual to identify data
that is only applicable to a particular certification authority:
AR Aviation Registry (Russian)
CAA Civil Aviation Authority (UK)
CAAC Civil Aviation Authority of China
CAAI Civil Aviation Authority of Israel
CTA Centro Tecnico Aerospacial (Brazil)
FAA Federal Aviation Administration (US)
LBA Luftfahrt-Bundesamt (German)
SAAU State Aviation Administration of Ukraine
7. SERVICE BULLETINS
Referenced throughout the manual are airplane serial numbers and Service Bulletins shown in
the following list:
Service Bulletin Title
SB 604–11–001 Increased MTOW to 48,200 LB (21,863 KG).
SB 604–21–002 Air Conditioning Units (ACU), ACUs Inhibit During Either Engine Start
SB 604–21–004 Pressurization Control System, Allow Aircraft Operation at High Field
Elevation
SB 604–21–008 Air Conditioning Units, Replacement of Existing Relays with 5 Second
Delay Relays
SB 604–22–006 Automatic Flight Control System, Introduction of Flight Control Computer to
Decrease Takeoff Pitch Angle
SB 604–23–006 Static Discharger, Installation of Additional Winglet Static Discharger
SB 604–24–002 DC Electrical Load Distribution System, FMS Power Source Change to DC
Battery Bus
SB 604–27–005 Stall Protection System, Dormant Failures in Stall Protection Computer
SB 604–27–009 Elevator Control System, Introduction of Pitch Feel Simulator with
Increased Stick Force in High G Maneuver for CAA Certification
SB A604–27–011 Stall Protection System, Replacement of Out-of-Tolerance AOA
Transducers
SB 604–27–012 Elevator Control System, Introduction of Pitch Feel Simulators with
Increased Stick Force
INTRODUCTION
General
01−01−18
REV 77, Oct 20/09
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
7. SERVICE BULLETINS (CONT'D)
Service Bulletin Title
SB 604–28–006 Fuel Quantity Indicating System, Introduction of New Fuel Quantity Gauging
Computer
SB 604–28–007 Transfer System, Increased Fuel Transfer Rate from Tail Fuel Tank to
Auxiliary Fuel Tank
SB 604–31–015 EICAS and Electronic Flight Display, Introduction of New Software for DCU
and EFD to Correct “C” Chord, Expanded Localizer & FDR Data Validity
中国航空网 www.aero.cn
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庞巴迪挑战者604飞机飞行手册CL604 Airplane Flight Manual 1(40)
