UAV-1004045-001 AV-30-C ICA
12
Revision A
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
applicable.
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
.
