barfield 101-01180, Инструкция по эксплуатации

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INSTRUCTION MANUAL
DPS400
56-101-01180-C 1-1
Page
3
November 5, 2003
B. DPS400 Switches and Controls
Note: For DPS400 units incorporating Mod G, Mod D, or for units before Mod D, refer to
previous releases of the DPS400 Instruction manual.
OPEN UNTIL INITIALIZATION
PITOT
VENT
PITOT
POWER
IMPORTANT!
PITOT AND STATIC VENT
VALVES MUST BE FULLY
IS COMPLETED
DPS400
VENT
STATIC
STATIC
PWR
47-400Hz
115/230 VAC
ON
OFF
LEAK TEST
INCREASE
DECREASE
PITOT CONTROL
(KNOTS)
AIRSPEED
REFERENCE ONLY
DIAL INDICATION
INCREASE
DECREASE
P/N
H
B
M/N
G
A
S/N
M L K J
F E D C
MOD
A
G
THE USA
MADE IN
OPT
B C D E F
H J K L M
ALTITUDE
(FEET
STATIC CONTROL
)
REFERENCE ONLY
DIAL INDICATION
RATE CONTROL
LEAK TEST
/
F2 F1 MENU
F4
F3 PUMP
TEST
LEAK
DEC
CONTRAST
INC
DPS400 (Mod P)
Switches and Controls
Figure 5
(1) PITOT CONTROL Controls pitot system pressure to achieve simulated
conditions for airspeeds between 0 Knots to 650 Knots.
(2) PITOT LEAK TEST Isolates the pitot system of the aircraft for leak
VALVE tests.
(3) PITOT VENT Releases applied pitot system pressure to ambient
atmosphere.
(4) STATIC RATE CONTROL/ Isolates the static system of the aircraft for leaks tests,
LEAK TEST VALVE and controls the rate of change of static pressures.
15
3
12
5
10
4
6
14
13
11
7, 8
2
9
1