Eclipse EA500 Maintenance Manual page 29

(a) Press ALT Ps to select the ALT control aim, enter 6008 and press Enter. Press
SPEED Qc, enter 66.1 and 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.
(20) Record the left PFD altitude and airspeed.
• Expected results are 6,000 ± 25 feet and 65 ± 2 knots.
(21) Press GROUND to go to atmospheric pressure. Press F1 (Go to Ground).
(a) After the Barfield Pitot/Static Tester DPS500 displays shows SAFE AT GROUND
prompt, press CLEAR/QUIT.
(22) Select WOnW on the WOW test box.
(23) Make sure that the Pitot and Static heat ECB's are collared.
(24) 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
9. Standby Pitot/Static Probe Verification Test
SUBTASK AMM-34-10-00-071-701-006
* * * 000001-000262, 000262 and 000267 PRE 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 or AMC to the aircraft and make sure that the ECB's are
collared. Refer to
(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 PFD baro to 29.92 by using the BARO SET
knob on the ACP.
• Make sure the baro setting matches on the left and right PFD.
(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 MFD.
• Expected Results: 40,000 ± 105 feet, 190 ± 2.7 knots, and 0.667 ± 0.011 Mach.
EFFECTIVITY: NOTED
EA500 Aircraft Maintenance Manual — 06-117751
SUBTASK AMM-34-10-00-071-921-002.
SUBTASK AMM-34-10-00-071-921-001.
© 2020 Eclipse Aerospace, Inc.
Temporary Revision No. 34-21
34-10-00
Page 525
Sep 30/20