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.
Table 501. Component Test Matrix
Component to be Tested
Test
Left and right ADCs
Pitot and Static System Leak Test
,
Pitot and Static Verification Test
SUBTASK AMM-34-10-00-071-701-005
and
Angle of Attack
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
.
Left and right Pitot/AOA
probes
Pitot and Static System Leak Test
,
Angle of Attack Test
Pitot and Static Anti-Ice System - Adjustment/Test.
If software only is replaced, perform the following:
Pitot
and Static System Leak Test
, and Angle of Attack Test
SUBTASK AMM-34-10-00-071-701-004
.
Left and right Static ports
Pitot and Static System Leak Test
Pitot and Static Anti-Ice System - Adjustment/Test.
EA500 Aircraft Maintenance Manual — 06-117751
Temporary Revision No. 34-21
EFFECTIVITY: NOTED
34-10-00
Page 501
Sep 30/20
© 2020 Eclipse Aerospace, Inc.
