Aerospool WT9 Dynamic LSA / Club, Pilot Operating Handbook

Page: 174 / 204

Page 7-40 Initial issue
7.20 Pitot-Static System
The pitot – static system consists of a single pitot probe located under the right wing. The pitot probe includes total
pressure, static pressure and AoA ports. In each line a drain sump is installed under the co-pilot seat to trap water and
moisture that enters the system. The drain sumps should be checked at the annual inspection or in any case when
water in the system is known or suspected.
Pressure distribution to individual instruments in the cockpit is done through flexible plastic hoses (Fig. 7-31).
1. Pitot probe 6. Flight hours counter
2. ADAHRS module 7. Altitude encoder
3. Airspeed indicator 8. Expansion bottle
4. Altimeter 9. Drain sumps
5. Vertical speed indicator - -
Fig. 7-31 Pitot-static system schematic