Eclipse EA500 Maintenance Manual page 34

(2) Set the WOW Box switches to WOnW.
(3) Power up the aircraft by setting the SYS BATT and START BATT switches to ON
and the BUS TIE switch to AUTO.
(4) Select WOffW on the WOW test box.
(5) Set the transponder to STBY on the PFD.
(6) If required, set both the left and right SDU baro to 29.92 by press and HOLD the
MENU button until the Baro reads 29.92 (or use ARROWS to adjust the Baro
reading)..
NOTE: Right SDU is optional.
• Make sure the baro setting matches on the left and right SDU.
(7) Set the static pressure to 39,889 feet and set the airspeed to 197.0 Knots.
(a) Press ALT Ps to select the ALT control aim, enter 39889 and press ENTER.
Press SPEED Qc and enter 197.0 then press ENTER. Wait for at least a 15
second stabilization period after the altitude and airspeed achieve these new air
data parameter set point values to continue.
(8) Record the Standby Pitot/Static probe altitude and airspeed from the SDU.
• Expected Results: 40,000 ± 105 feet and 190 ± 2.7 knots.
(9) Set the static pressure to 29,874 feet and set the airspeed to 247.1 Knots.
(a) Press ALT Ps to select the ALT control aim, enter 29874 and press ENTER.
Press SPEED Qc and enter 247.1 then press ENTER. Wait for at least a 15
second stabilization period after the altitude and airspeed achieve these new air
data parameter set point values to continue.
(10) Record the Standby Pitot/Static probe altitude and airspeed from the SDU.
• Expected Results: 30,000 ± 75 feet and 240 ± 2.7 knots.
(11) Set the static pressure to 19,899 feet and increase airspeed to 247.5 Knots.
(a) Press ALT Ps to select the ALT control aim, enter 19899 and press ENTER.
Press SPEED Qc and enter 247.5 then press ENTER. Wait for at least a 15
second stabilization period after the altitude and airspeed achieve these new air
data parameter set point values to continue.
(12) Record the Standby Pitot/Static probe altitude and airspeed from the SDU.
• Expected Results: 20,000 ± 50 feet and 245 ± 3 knots.
(13) Set the static pressure to 9,998 feet and set the airspeed to 99.9 Knots.
(a) Press ALT Ps to select the ALT control aim, enter 9998 and press ENTER. Press
SPEED Qc and enter 99.9 then press ENTER. Wait for at least a 15 second
stabilization period after the altitude and airspeed achieve these new air data
parameter set point values to continue.
(14) Record the Standby Pitot/Static probe altitude and airspeed from the SDU.
• Expected Results: 10,000 ± 33 feet and 100 ± 3 knots.
(15) Set the static pressure to 5,999 feet and set the airspeed to 64.9 Knots.
EFFECTIVITY: NOTED
EA500 Aircraft Maintenance Manual — 06-117751
© 2020 Eclipse Aerospace, Inc.
Temporary Revision No. 34-21
34-10-00
Page 530
Sep 30/20