Component to be Tested Test
Standby Pitot/Static probe Standby Pitot/Static Probe System Leak Test SUBTASK
AMM-34-10-00-071-701-002, Standby Pitot/Static Probe
Verification Test (Effectivity Noted) SUBTASK
AMM-34-10-00-071-701-006 or SUBTASK
AMM-34-10-00-071-701-007 and AMM-30-30-00-071-801 –
Pitot and Static Anti-Ice System - Adjustment/Test.
If software only is replaced, perform the following: Standby
Pitot/Static Probe Verification Test (Effectivity Noted)
SUBTASK AMM-34-10-00-071-701-006 or SUBTASK
AMM-34-10-00-071-701-007.
Right and left OAT probes Outside Air Temperature Test SUBTASK
AMM-34-10-00-071-701-008.
2. Equipment and Materials
Table 502. Special Tools and Equipment
Name and Part Number
Barfield Pitot/Static Tester (Barfield, DPS450) or Barfield Pitot/Static Tester (Barfield, DPS500)
or Equivalent Tester.
Air Data Accessories Kit (NavAids P/N ADA500MD-945) (or) Air Data Accessories Kit ; (Nav
Aids PN ADA500945) (Note: If using ADA500–945, covering pitot probes with tape is required)
Stop Watch (Inotek, EH365528) or Equivalent (Note: Calibrated with 1 second resolution)
Weight-on-Wheels (WOW) Box (EAI, 87-117390-1001) or Avio Maintenance Computer (AMC)
(EAI 20-120576-1001 or 20-121926-1001), SW version “1.5.71 or higher” for Pre-Avio NG
aircraft and “2.2.02 or higher” for Avio NG aircraft (for Weight off Wheels simulation)
Vinyl Tape (To cover drain hole on Pitot probes)
Ground Power Unit (GPU). AllStar 450 or AllStar G.S.E. or Hobart GPU-400 or Hobart GPU-
600 or Bycan PS-28100 (Note: 28.0 ± 0.5 VDC)
EA500 Aircraft Maintenance Manual — 06-117751
Temporary Revision No. 34-21
EFFECTIVITY: NOTED
34-10-00
Page 502
Sep 30/20
© 2020 Eclipse Aerospace, Inc.
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