(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: 30000 ± 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.
(a) Press ALT Ps to select the ALT control aim, enter 5999 and press ENTER. Press
SPEED Qc and enter 64.9 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.
(16) Record the Standby Pitot/Static probe altitude and airspeed from the SDU.
• Expected results are 6,000 ± 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 DPS450 is not in CONTROL MODE, press
LEAK MEASURE/CONTROL.
(b) After the Barfield Pitot/Static Tester DPS450 displays shows SAFE AT GROUND
prompt, power off the Barfield Pitot/Static Tester DPS450.
(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 DPS450.
Also, refer to SUBTASK AMM-34-10-00-071-921-002.
B. Standby Pitot/Static Probe Verification Test with a Barfield Pitot/Static Tester DPS500:
(1) Connect the WOW Box or AMC to the aircraft and make sure that the ECBs are
collared. Refer to SUBTASK AMM-34-10-00-071-921-001.
EA500 Aircraft Maintenance Manual — 06-117751
Temporary Revision No. 34-21
EFFECTIVITY: NOTED
34-10-00
Page 529
Sep 30/20
© 2020 Eclipse Aerospace, Inc.
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