. Connect the static
to the top fitting of the Static Port Adaptor (Nav Aids,
SS53515-4-4)
.
(e) Connect the Static Port Adaptor (Nav Aids, SS53515-4-4)
port with the connected fitting to the top port and finger tighten the screws to seat
the seals over the Static ports.
(5) Connect the Barfield Pitot/Static Tester DPS450 to the aircraft using the Air Data
Accessories Kit (NavAids P/N ADA500MD-945) as follows:
NOTE: When installing the pressure test adapters, make sure that the seal is good
by applying a firm force to seat the adapter on the probe.
NOTE: The P22201MD-4 adapter contains a built-in seal that covers the Pitot/AOA
probe drain hole. If using the P22201-3 adapter, the drain hole must be
covered with teflon or vinyl tape.
NOTE: The Pitot/AOA probes with a drain hole near the base of mast, must have the
drain hole covered. Failure to do so will result in a failure of this test.
(a) Connect the Pitot Test Hose Assembly
Pitot/Static Tester DPS450. DO NOT OVERTIGHTEN.
(b) Connect the opposite end of the hose to the NAV Aids P22201MD-4 adapter.
(c) Install the NAV Aids P22201MD-4 adapter to the Pitot/AOA Probe. Make sure
that the internal seal of the adapter covers the pitot probe drain hole. If using the
P22201-3 adapter, make sure that the pitot probe drain hole is covered with tape.
If needed, lubricate with Pitot adaptor lubricating fluid (Part Number LF5050).
NOTE: No other lubricating fluid is permitted. Malfunction of the equipment in
flight is possible.
(d) Connect the Static Port Adaptor (Nav Aids, SS53515-4-4)
port and finger tighten the screws to seat the seals over the static ports.
(e) Connect the Static Test Hose Assembly ; (Nav Aids PN E500-5160) (long hose)
to the Barfield Pitot/Static Tester DPS450 Ps connection
.
(f) Connect the other end of the hose
to the top fitting of the Static Port Adaptor
(Nav Aids, SS53515-4-4)
(6) Use tape to seal the opposite-side static port.
NOTE: Make sure to select a tape that does not leave any adhesive residue on the
Static port when the test is complete.
(7) Select WOffW on the WOW test box.
(8) Set the transponder to STBY on the PFD.
(9) If required, set both the left and right PFD baro to 29.92 by using the BARO SET
knob on the ACP.
•
Make sure that the baro setting matches on the left and right PFD and the
optional Standby Display Unit (SDU) (if installed).
(10) Turn on the Barfield Pitot/Static Tester DPS450.
EA500 Aircraft Maintenance Manual — 06-117751
Temporary Revision No. 34-21
EFFECTIVITY: NOTED
34-10-00
Page 520
Sep 30/20
© 2020 Eclipse Aerospace, Inc.
