(11) Set the Barfield Pitot/Static Tester DPS450 static pressure to 40,613 feet and set the
airspeed to 159.2 knots as follows:
(a) Press ALT Ps to select the ALT control aim, enter 40613 and press ENTER.
Press SPEED Qc, enter 159.2 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.
(12) Record the left PFD altimeter and airspeed.
•
Expected results are 41,000 ± 40 feet, 160 ± 2.5 knots, and 0.575 ± 0.008 Mach.
(13) Set the Barfield Pitot/Static Tester DPS450 static pressure to 29,698 feet and
increase the airspeed to 199.3 knots as follows:
(a) Press ALT Ps to select the ALT control aim, enter 29698 and press Enter. Press
SPEED Qc, enter 199.3 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.
(14) Record the left PFD altitude and airspeed.
•
Expected results are 30,000 ± 40 feet, 200 ± 2.7 knots and 0.557 ± 0.006 Mach.
(15) Set the Barfield Pitot/Static Tester DPS450 static pressure to 19,706 feet and
increase the airspeed to 237.6 knots as follows:
(a) Press ALT Ps to select the ALT control aim, enter 19706 and press Enter. Press
SPEED Qc, enter 237.6 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.
(16) Record the left PFD altitude and airspeed.
•
Expected results are 20,000± 40 feet, 240 ± 3 knots and 0.535 ± 0.006 Mach.
(17) Set the Barfield Pitot/Static Tester DPS450 static pressure to 9,872 feet set the
airspeed to 195.9 knots as follows:
(a) Press ALT Ps to select the ALT control aim, enter 9872” and press Enter. Press
SPEED Qc, enter 195.9 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.
(18) Record the left PFD altitude and airspeed.
•
Expected results are 10,000± 33 feet and 200 ± 2.7 knots.
(19) Set the Barfield Pitot/Static Tester DPS450 static pressure to 6,008 feet and set the
airspeed to 66.1 knots as follows:
(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 altimeter and airspeed.
•
Expected results are 6,000 ± 25 feet and 65 ± 2 knots.
(21) Press GROUND to go to atmospheric pressure. Press F1 to select Yes to confirm.
EA500 Aircraft Maintenance Manual — 06-117751
Temporary Revision No. 34-21
EFFECTIVITY: NOTED
34-10-00
Page 521
Sep 30/20
© 2020 Eclipse Aerospace, Inc.
