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PULL UP display is annunciated on the PFD. When warnings are activated, areas which meet the terrain collision
alert criteria are depicted red. Terrain automatically comes up in MAP mode on MFD at a 10 nm range, if there is a terrain
warning at 30 seconds from impact.
NOTE: When landing at an airport that is not in the database, TERRAIN functions can be inhibited
by selecting the TERRAIN switch OFF. The switch is located on the TAWS
WARN panel.
"TERRAIN "PULL UP!"
TERRAIN"
OFF
TERRAIN
NAVIGATION
Sep 13/2004 Flight Crew Operating Manual Volume 2
REV 1 CSP 100-6 17-01-29
TERRAIN AWARENESS WARNING SYSTEM (TAWS) (Cont)
TERRAIN CLEARANCE FLOOR (TCF)
The TCF function supplements the GPWS function by providing an additional terrain clearance alert envelope
around airports. The TCF criteria determine alert and warning envelopes.
TCF creates an increasing terrain clearance envelope around the intended airport runway directly related to the distance
from the runway. TCF alerts are based on current airplane location, nearest runway center point position and radio altitude,
along with an internal database that includes all worldwide, hard-surfaced runways greater than 3500 feet in length.
Penetration of the alert envelope generates an aural “TOO LOW TERRAIN” and an amber GND PROX is displayed on
the PFD. The aural alert is repeated twice and again thereafter if the radio altitude value decreases by more than 20% from
the altitude at which the initial warning was issued. The amber GND PROX remains displayed until the airplane exits the
alert envelope.
700
AGL
400
AGL
RUNWAY
4 NM 12 NM 15 NM
"TOO LOW TERRAIN"
CFO1701002_007
NAVIGATION
Volume 2 Flight Crew Operating Manual Sep 13/2004
17-01-30 CSP 100-6 REV 1
TERRAIN AWARENESS WARNING SYSTEM (TAWS) (Cont)
ANNUNCIATIONS
All terrain annunciations are displayed on the PFD and MFD.
PFD Display Indicating Terrain Data
1. SOLID RED — Areas of terrain that satisfy the terrain warning alert criteria.
2. SOLID AMBER— Areas of terrain that satisfy the terrain caution alert criteria.
3. GREEN, AMBER, RED DOT PATTERN — Areas of terrain that are significantly close to the aircraft but do not
satisfy warning alert or caution alert criteria.
CFO1701002_025
CAS
CKLST SKIP
FRMT TFC ENTER
A/ICE ELEC FLT HYD
L R
COM1 NAV1 ATC1/TCAS ADF1 HF1 COM3 COM2
118.000 108.00 1200 1799.5 118.000 118.000
118.000 108.00 STBY 190.0 2.0000 118.000 118.000
ABV
TX 2.0000 AM
ECS
25 25
340
UTC
° C
11 : 42
SAT -15
ISA -5 ° C
TAS
GS
250
254
30
MFD
CONTROL
TR / WX / LX
24
W
30
33
N
3
6
DBQ
ALO
TNU
NEBOR
CID
IOW
IA
200
KCID
100
270 / 150
FUEL
TR/WX SUMRY
1
3
FMS1 2
DTK 350
KCID
TTG 15:01
95.0 NM
HDG 340
STAB
NU
ND
6.6
TRIM
AIL
LWD RWD
RUD
GEAR
FLAPS 0
00
M.400
220
260
240
200
180
220
1
9
4200
4
2
1
1
4
APPR LOC2 ALTV FLC GP
APPR VOR2 AP YD VALTV CAP
20
10
20
10
350 16000
35000
4
3
100
00
00
100 00
80
20
2
29.92 IN
93.0 61.0
NI
MACH
HOLD
85.0 MCT
85.0 MCT
N2
OIL PRESS
OIL TEMP
FF PPH
84.7
46
115
7300
84.7
46
115
7300
730 ITT 730
APU RPM
100
APU EGT 250
FUEL QTY LBS
TOTAL 12000
6000 6000
CAB ALT
CAB RATE
7300
1000
REV
L R
GND PROX
UP
UP UP
NAVIGATION
Sep 13/2004 Flight Crew Operating Manual Volume 2
REV 1 CSP 100-6 17-01-31
WEATHER RADAR
DESCRIPTION
The weather radar is an X-band color weather radar system used for atmospheric moisture detection and ground mapping.
The weather radar provides displays of radar-detectable precipitation with in ±60° of the flight path at a selectable range
up to 300 nautical miles. The weather radar also provides ground mapping and incorporates features such as autotilt, ground
clutter suppression, range compensation and path attenuation correction.
The system consists of a receiver transmitter antenna (RTA) and dual controllers. Radar information is normally displayed
　
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