(13) If no further maintenance is required, remove all of the Nav Aids test equipment from
the aircraft. Stow all the Air Data Accessories Kit ; (Nav Aids PN ADA500945)
equipment and the Barfield Pitot/Static Tester DPS500.
(14)
Remove the tape from the opposite-side Static port.
5.
Standby Pitot/Static Probe System Leak Test
SUBTASK AMM-34-10-00-071-701-002
* * * ALL
CAUTION: DO NOT PRESSURIZE THE AIRCRAFT DURING TESTING.
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. Complete the Standby Pitot/Static System Leak Test (using the Barfield Pitot/Static
Tester DPS450) as follows:
CAUTION: DO NOT OVER TIGHTEN HOSES. DAMAGE MAY OCCUR TO TEST
EQUIPMENT. HOSES SHOULD BE SNUG.
CAUTION: THE LEAK TEST CAN BE ACCOMPLISHED 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 DPS450 to the aircraft Standby Pitot/Static
probe as follows:
(a)
Attach the Pitot/Static probe adaptor (PS35210-4-4) (6) to the Standby Pitot/
Static probe.
(b) Connect the hose (3) from the Pt connection (2) on the Barfield Pitot/Static
Tester DPS450 to the end fitting on the Pitot/Static probe adaptor (PS35210-4-4)
(6) .
(c) Connect the hose from the Ps (1) connection on the Barfield Pitot/Static Tester
DPS450 to the fitting on the side on the Pitot/Static probe adaptor (PS35210-4-4)
(6) .
NOTE: Cover the probe drain hole with vinyl tape.
(2) Connect the Barfield Pitot/Static Tester DPS500 to the aircraft using the Air Data
Accessories Kit (NavAids P/N ADA500MD-945) as follows:
EA500 Aircraft Maintenance Manual — 06-117751
Temporary Revision No. 34-21
EFFECTIVITY: NOTED
34-10-00
Page 510
Sep 30/20
© 2020 Eclipse Aerospace, Inc.
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