PIM 417-O
PITOT-STATIC LEAK TESTER TYPE D51600
Issue 5
November 2009
Page 3
SPECIFICATION
1. PHYSICAL DIMENSIONS
Overall Dimensions:
192.3 mm x 110 mm x 210 mm
Front Panel:
147.4 mm x 77 mm
Weight:
2.3 kg, maximum
Output Port:
push-to-fit pipe
2. POWER SUPPLY
Battery Voltage:
10 x 1.5 V d.c.
Battery Current:
600 mA maximum, 300 mA typical,
> 1.2 Ah recommended
3. OPERATIONAL LIMITS
A.
Pitot
Range (wrt Atmosphere):
0 to 430 knots
0 to 10 inHg
0 to 340 mbar
Normal Rate of Change:
47 mbar / minute
Rapid Rate of Change:
114 mbar / minute
Power Fail Rate of Change:
80 mbar / minute (<47 knots/min
@ 400 knots in 1 litre)
B.
Static
Range (wrt Atmosphere):
0 to -430 knots
0 to -10 inHg
0 to -340 mbar
0 to +10000 feet
Normal Rate of Change:
56 mbar / minute (1670 ft/min @ 0 ft;
2500 ft/min @ 15000 ft)
Normal Rate Operating in Feet:
1670 feet / minute
Rapid Rate of Change:
136 mbar / minute ) 3600 ft/min
@ 0 ft; 6000 ft/min @ 15000 ft)
Rapid Rate Operating in Feet:
4000 feet / minute
Power Fail Rate of Change:
< 70 mbar / minute (<2500 ft/min
@ 10000 ft above sea level in 1 litre)
4. INPUT
Ambient Vent Source:
-1500 feet (1069 mbar) to
150000 feet (572 mbar)
Pneumatic Pressure from the Aircraft
NOTE:
Vacuum performance is reduced above 4500 feet
5. OUTPUT
Pneumatic Load:
5 litres, maximum
(Volume of the Aircraft)