FLIGHT ENVIRONMENT DATA - ADJUSTMENT/TEST
AMM-34-10-00-071-801
1. General
A. This task gives procedures to do an adjustment/test of the flight environment data
components.
NOTE: This test procedure complies with the requirements of 14 CFR Part 43 Appendix
E.
(1) Unless indicated differently, the adjustment/test procedures are the same for both left
and right sides.
(2) Included are procedures for use of both the Barfield Pitot/Static Tester (Barfield,
DPS450) and the Barfield Pitot/Static Tester (Barfield, DPS500).
(3) After a replacement of the left and right Pitot/AOA probes, static ports, Air Data
Computers (ADCs), Standby Pitot/Static probe and Outside Air Temperature (OAT)
probes, do the test for each component shown in the table below.
Component to be Tested
Left and right ADCs
Left and right Pitot/AOA
probes
Left and right Static ports
EFFECTIVITY: NOTED
EA500 Aircraft Maintenance Manual — 06-117751
Table 501. Component Test Matrix
Pitot and Static System Leak Test
AMM-34-10-00-071-701-001, Pitot and Static Verification Test
SUBTASK AMM-34-10-00-071-701-005
Test
SUBTASK AMM-34-10-00-071-701-004
AMM-24-00-00-071-801 – Electrical Power - Adjustment/Test,
SUBTASK AMM-24-00-00-071-701-005, Left and Right ADC
Test.
If software only is replaced, perform the following: Pitot
and Static Verification Test
AMM-34-10-00-071-701-005.
Pitot and Static System Leak Test
AMM-34-10-00-071-701-001, Angle of Attack Test
AMM-34-10-00-071-701-004
Pitot and Static Anti-Ice System - Adjustment/Test.
If software only is replaced, perform the following: Pitot
and Static System Leak Test
AMM-34-10-00-071-701-001, and Angle of Attack Test
SUBTASK
AMM-34-10-00-071-701-004.
Pitot and Static System Leak Test
AMM-34-10-00-071-701-001
Pitot and Static Anti-Ice System - Adjustment/Test.
© 2020 Eclipse Aerospace, Inc.
Temporary Revision No. 34-21
Test
SUBTASK
and Angle of Attack
and
SUBTASK
SUBTASK
SUBTASK
and
AMM-30-30-00-071-801 –
SUBTASK
SUBTASK
and
AMM-30-30-00-071-801 –
34-10-00
Page 501
Sep 30/20
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