Instructions For Continued Airworthiness; Airworthiness Limitations; Test And Service Procedures; Installation, Removal And Trouble Shooting Procedures - uAvionix AV-30-C Instructions For Continued Airworthiness

7 Instructions for Continued Airworthiness

This section provides Instructions for Continued Airworthiness of the AV-
30-C system as installed under AML-STC and satisfies the requirements
for continued airworthiness as defined by 14 CFR Part 23.1529 and Part
23 Appendix G (Amendment 61).

7.1 Airworthiness Limitations

The Airworthiness Limitations section is FAA-approved and specifies
maintenance required under 14 CFR Part 43.16 and 14 CFR Part
91.403 of the Federal Aviation Regulations unless an alternative
program has been FAA-approved.
There are no new (or additional) airworthiness limitations associated
with this equipment and/or installation.
No component-level overhaul is required.

7.2 Test and Service Procedures

Utilize Section 7.8 - Visual Inspection Procedure of this document to
perform visual inspections when required.
Utilize Section 7.9.5 - Altimeter Test and Calibration Procedure of this
document to perform altimeter trimming when required.
Utilize Section 7.10 - Battery Test and Replacement Procedure of this
document to test and replace the battery when required.
The Altitude Trim procedure only applies when the AV-30-C is
configured as an Attitude Indicator. When configured as a Directional
Gyro, altitude is not displayable and therefore trimming is not

7.3 Installation, Removal and Trouble Shooting Procedures

For other non-related instructions including removal, installation and
troubleshooting procedures of the unit, reference AV-30-C Installation
Manual.
UAV-1004045-001 AV-30-C ICA
applicable.
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