Eclipse EA500 Maintenance Manual page 32

stabilization period after the altitude and airspeed achieve these new air data
parameter set point values to continue.
(16) Record the Standby Pitot/Static probe altitude and airspeed from the MFD.
• Expected Results: 6000 ± 30 feet and 65 ± 4 knots.
(17) Press GROUND to go to atmospheric pressure. Press F1 to select Yes to confirm.
(a) If the Barfield Pitot/Static Tester DPS500 is not in CONTROL MODE, press
LEAK MEASURE/CONTROL.
(b) After the Barfield Pitot/Static Tester DPS500 displays shows SAFE AT GROUND
prompt, power off the Barfield Pitot/Static Tester DPS500.
(18) If no further maintenance is required, remove all of the Nav Aids test equipment from
the aircraft. Stow all air data equipment and the Barfield Pitot/Static Tester DPS500.
Also, refer to
10. Standby Pitot/Static Probe Verification Test - Standby Display Unit (SDU)
SUBTASK AMM-34-10-00-071-701-007
* * * 000001-000262, 000262 and 000267 POST MB 500-31-006
NOTE: If a Barfield Pitot/Static Tester DPS450 is used for this test complete paragraph
A. If a Barfield Pitot/Static Tester DPS500 is used, go to paragraph B.
A. Standby Pitot/Static Probe Verification Test with a Barfield Pitot/Static Tester DPS450:
(1) Connect the WOW Box to the aircraft and make sure that the ECBs are collared.
Refer to SUBTASK
(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 Pitot/Static probe Altitude and Airspeed from the SDU.
• Expected Results: 40,000 ± 105 feet and 190 ± 2.7 knots.
EFFECTIVITY: NOTED
EA500 Aircraft Maintenance Manual — 06-117751
SUBTASK AMM-34-10-00-071-921-002.
AMM-34-10-00-071-921-001.
© 2020 Eclipse Aerospace, Inc.
Temporary Revision No. 34-21
34-10-00
Page 528
Sep 30/20