UAV-1003947-001, AV-30-C, Installation Manual
13
Rev E
7 Certification
This installation manual provides mechanical and electrical information
necessary to install the AV-30-C. The content of this manual assumes use
by competent and qualified personnel using standard maintenance
procedures in accordance with Title 14 of the Code of Federal Regulation
(CFR) and other related accepted procedures.
The certification basis for the AV-30-C is 14 CFR Part 23, Amendment 23-
61. Installation is approved as a Level A system and is robust to High
Intensity Radiated Field (HIRF) and lightning levels applicable for both
metallic and non-metallic aircraft.
The AV-30-C is approved for primary Attitude, Slip and Direction of
Flight.
All other functionality is supplemental in nature and may not satisfy
regulatory requirements for required instrumentation.
The installer must ensure that all installation limitations as defined
in this document are observed.
The internal battery capacity has been tested and verified to provide 30
minutes of operational capacity (with reserve), and meets the requirements
defined in CFR 23.1311(a)(5) and 23.1353(h), allowing independent
operation from the primary electrical power system.
See §10.3 Internal Battery Operation for additional battery operational
characteristics.
For aircraft capable of acrobatic flight, the AoA indication may
become unreliable for operation in inverted flight and maneuvers
exceeding ±8 G.
