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Druck ADTS 505 User Manual
3 - 17
K0260 Issue No. 8
3
3.7.2 Testing the Aircraft Pitot System
CAUTIONS:
1
O
BSERVE
ALL
SAFETY
PRECAUTIONS
DETAILED
IN
THE
A
IRCRAFT
M
AINTENANCE
M
ANUAL
.
2
W
HEN
USING
P
T
(
PITOT
ONLY
),
MAKE
SURE
THAT
THE
DIFFERENTIAL
PRESSURE
(Q
C
)
STAYS
WITHIN
THE
LIMITS
OF
THE
ASI.
1.
Remove the Pitot and static blanking caps and switch ON.
2.
Connect the ADTS 505 to the Aircraft Pitot System.
3.
Press
SPEED/Qc
and make sure the display shows Qc Leak Measure.
Note:
To monitor the rate of change press RATE after pressing SPEED/Qc. The control rate of change
for airspeed is fixed at 300 kts/min.
4.
If necessary, select Units in the Main Menu, press F1 [ft, kts, ft/min]. Press
CLEAR/QUIT
to go back
to the Main Menu.
5.
If necessary change the limits in the Main Menu, press F6 [More], F1 [Limits]. After setting the limits,
press repeatedly
CLEAR/QUIT
to go back to the Main Menu.
6.
Press
LEAK MEASURE/CONTROL
to select control mode and, using the numeric keys, set the control
aim. Press
ENTER
, the airspeed changes to the control aim the rate of change slows as it gets near
the control aim and does not "overshoot" the aim value.
7.
Enter another aim or use the nudge facility to change the aim value. At the end of testing, press
GROUND
to return to zero pressure.
8.
On completion of testing, select
GROUND
and wait for the `Safe at Ground' message to be displayed,
see 3.7.8., refit the pitot and static blanking caps.
Содержание Druck ADTS 505
Страница 1: ...GE Measurement Control Druck ADTS 505 Air Data Test Set User Manual K0260 ...
Страница 14: ...xii K0260 Issue No 8 Druck ADTS 505 User Manual ...
Страница 54: ...3 26 Operation K0260 Issue No 8 ...
Страница 55: ...Druck ADTS 505 User Manual 3 27 K0260 Issue No 8 3 ...
Страница 56: ...3 28 Operation K0260 Issue No 8 ...
Страница 66: ...5 4 Testing and Fault Finding K0260 Issue No 8 FIGURE 5 1 FAULT FINDING CHART ...
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Страница 124: ...6 44 Reference and Specification K0260 Issue No 8 Intentionally left blank ...