Eclipse EA500 Maintenance Manual page 11

• After the Waiting and Timing intervals are complete, the Barfield Pitot/Static
Tester DPS450 displays Timed Rates Available.
(16) Check that the maximum ROC is 100 ft/min or less and the maximum Rt CAS is 2
kts/min. or less.
• If the leak rate is not within tolerances, refer to Leak Testing in the Barfield Pitot/
Static Tester DPS450 and Connecting Hoses
AMM-34-10-00-071-701-003). Subtract the Barfield Pitot/Static Tester DPS450
leak check altitude value recorded in Leak Testing in the Barfield Pitot/Static
Tester DPS450 and Connecting Hoses subtask from the value obtained in this
section in order to get a corrected total system leak value.
(17) Press LEAK MEASURE/CONTROL to return to CONTROL MODE.
(18) If no further maintenance is required, remove all of the Nav Aids test equipment from
the aircraft. Stow the Air Data Accessories Kit ; (Nav Aids PN ADA500945)
equipment and Barfield Pitot/Static Tester DPS450.
(19) Remove the tape from the opposite-side Static port.
B. Pitot and Static System Leak Test with Barfield Pitot/Static Tester DPS500:
Procedure is given for the left side and is the same for the right side unless noted.
NOTE: To use the Barfield Pitot/Static Tester DPS500 Remote during this test, connect
the Remote (P/N ADTS405-1728-37M0) and Remote Cord (P/N
ADTS405-1728-28M0) to the Barfield Pitot/Static Tester DPS500 Hand Terminal
Connection.
NOTE: The Pt Hose (p/n ADTS405-1729-62m0) may be used in place of the hose (p/n
E500-7270). The AN6-AN4 adaptor is not needed if using the ADTS405-
1729-62m0 Pt hose.
NOTE: The Ps Hose (p/n ADTS405-1729-61m0) may be used in place of the hose (p/n
E500-5160), The AN6-AN4 connector is not required if using this configuration.
Install a AN5 to AN4 adaptor on the Barfield DPS500 Ps connection.
CAUTION: DO NOT OVER TIGHTEN HOSES. DAMAGE MAY OCCUR TO TEST
EQUIPMENT. HOSES SHOULD BE SNUG.
CAUTION: THE LEAK TEST CAN BE DONE WITH ELECTRICAL POWER OFF.
MAKE SURE THAT IF THE WOW BOX IS CONNECTED, THE
SWITCHES ARE SET TO WONW DURING THIS TEST IF ELECTRICAL
POWER IS USED. WITH WEIGHT OFF WHEELS, THE HEATERS ARE
COMMANDED ON BY THE AIRCRAFT COMPUTER SYSTEM. IF THE
PITOT/STATIC HEAT ECBS ARE NOT COLLARED OFF, HARM TO
PERSONNEL OR AIR DATA TEST EQUIPMENT CAN OCCUR.
NOTE: Refer to step (1) if using the Air Data Accessories Kit ; (Nav Aids PN
ADA500945) or step (2) if using the Air Data Accessories Kit (NavAids P/N
ADA500MD-945).
(1) Connect the Barfield Pitot/Static Tester DPS500 to the aircraft as follows:
(a) Install the Pitot/Angle of Attack (AOA) Probe Adaptor (Nav Aids,
APA94520-4-4-4)
EFFECTIVITY: NOTED
EA500 Aircraft Maintenance Manual — 06-117751
(7) with the label TOP facing up on the Pitot/AOA probe. If
© 2020 Eclipse Aerospace, Inc.
Temporary Revision No. 34-21
(SUBTASK
34-10-00
Sep 30/20
Page 507