(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: 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
SUBTASK AMM-34-10-00-071-921-002
.
11. Outside Air Temperature Test
SUBTASK AMM-34-10-00-071-701-008
* * * ALL
A. Do an Outside Air Temperature Test as follows:
(1) Power up the aircraft by setting the SYS BATT and START BATT switches to ON
and the BUS TIE switch to AUTO.
(2) Scroll to the ICE synoptic page on the MFD by using the lower left/right softkey.
(3) Expected results are that left and right OATs are within ± 5°C of the measured
outside temperature. Left and Right PFDs are within ± 2°C of MFD OAT temperature.
(4) Power down the aircraft by setting the SYS BATT and START BATT switches to OFF
and the BUS TIE switch to OPEN.
12. Job Close-Up
SUBTASK AMM-34-10-00-071-921-002
* * * ALL
A. If no other tests are required with the Weight On Wheels (WOW) box or Aircraft
Maintenance Computer (AMC), select WOnW.
(1) Re-set the following ECBs:
•
ECB - WEATHER RADAR (L FWD Bus)
•
ECB - DEICE MANIFOLD HTR (R AFT Bus)
•
ECB - L PITOT HEAT (L FWD Bus) or ECB - L PITOT HEAT (BATT Bus)
•
ECB - R PITOT HEAT (R FWD Bus)
•
ECB - L STATIC HEAT (BATT Bus)
EA500 Aircraft Maintenance Manual — 06-117751
Temporary Revision No. 34-21
EFFECTIVITY: NOTED
34-10-00
Page 531
Sep 30/20
© 2020 Eclipse Aerospace, Inc.
