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89000004-101
KI 300 Installation Manual
Rev 1
Page 3-3
© Honeywell International Inc. Do not copy without express permission of Honeywell.
Maximum configurable baro correction: 1050 mb / 31.00 inHg
Minimum configurable baro correction: 948 mb / 28.00 inHg
Minimum operational duration on battery: 30 Minutes
Maximum roll rate: 400 degrees / second
Maximum operating G force: 6 G
Battery operation may be inhibited for up to 15 minutes during cold-starts. TSO performance is
met within 10 minutes during cold-starts.
No operational capability on internal battery is possible if the battery is faulted, as shown by a
Red-X over the battery icon.
Battery charging is disabled below approximately 0°C and above 40°C ambient, or when power
input is below approximately 11 volts DC.
If in-Flight alignment is attempted, it must be performed with wings-level non-accelerated flight
conditions.
NOTE
APPROXIMATELY NINE PERCENT OF THE POPULATION HAS SOME SORT OF COLOR VISION DEFICIENCY (WHAT IS
COMMONLY CALLED “COLOR BLINDNESS”). IT SHOULD ALSO BE NOTED THAT THE FAA DOES NOT TEST FOR ALL
POTENTIAL COLOR DEFICIENCIES. (SOURCE TSO-C113a / AS8034)
3.2.7
TSO Deviations
TSO deviations are related to environmental test conditions and software certification basis. In both
cases, the latest versions of RTCA DO-160 (Revision G) and RTCA DO-178 (Revision C) were utilized in lieu
of older guidance.
In certain circumstances, this is a deviation from older TSO and associated MOPS guidance as follows:
TSO’s that reference older versions of DO
-160:
TSO-C2d § c(2)(viii) and corresponding MOPS AS8019 § 5
TSO-C3e § 6 (g) and corresponding MOPS AS8004 § 5
TSO-C8E § 6 (g) and corresponding MOPS AS8016A § 5
TSO’s that directly include a list of environmental specifications:
TSO-C4c § 514.14 and corresponding MOPS AS396B § 3.3, § 3.4, § 3.5, § 4.4, § 7
TSO-C10B § a(2)(ii) and corresponding MOPS AS392C § 3.3, §7
TSO’s that reference older versions of DO
-178:
TSO-C2d § a(3), §a(3)(i), § c(1)(xi), §c(2)(vii)
TSO-C3e § 3(e), § 6(h)
TSO-C113a § 3(e), § 6(g)
