K114 Issue No. 9
6 - 37Druck ADTS 405 User Manual
6
Performance expressed in example aeronautical units
edutitlA
bmilCfoetaR
)COR(
deepsriAdetarbilaC
)SAC(
hcaM
egnahcfoetaR
deepsriAfo
stinU
teefnim/tfstonk-nim/stk
mumixaM
egnaR
)1(
000,501ot0003-000,0010001ot001-79.410002
rodetarbilaC
dradnatS
egnaR
)1(
000,08ot0000,90001ot001-5007
ycaruccA
)2(
0ta3±
000,03ta7±
000,06ta92±
eulavfo%1±
05ta5.0±
055ta70.0±
0001ta50.0±
nahtretteB
500.0
eulavfo%5±
ytilibataepeR
0ta1±
000,03ta2±
000,06ta7±
%5.0±
05ta4.0±
055ta20.0±
0001ta20.0±
100.0
otgnisir
500.0
-
noituloseR
11 1.0100.01.0
NOTES
(1) Altitudes above 80,000 ft and the peak rates of climb are available but subject to the use of a
suitable vacuum pump.
(2) The accuracy figures stated relate to operation over the temperature range 5° to 35°C (+41° to +95°F).
Note: The accuracy figures stated assume Auto-Zero function enabled.