Page 8 of 28 Sym A
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Dwg. 56201-2
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Scope
1.4
The system meets the requirements of FAA Memo AIR100-14-110-PM01, dated February 5,
2014, regarding the Approval of Non-Required Angle-of-Attack (AoA) Indicator Systems.
These installation instructions become the approved data necessary for the installation of the
SCc.
1.4.1
These installation instructions are FAA Approved Data to be utilized only for the installation of
the AoA system described herein on aircraft certified under 14 CFR Part 23 (or
predecessors). Provided all of the requirements of section 2.0 of this document are met, no
further FAA approval is required for the installation of this AoA system on a Part 23 aircraft.
If the limitations of section 2.0 are not met, further FAA approval may be required.
1.4.2
These installation instructions are only approved for the aircraft models listed: Cessna 172,
182 and 206.
Limitations
1.5
1.5.1
The Safe Flight SCc System is non-required and is to be used only as advisory information to
the pilot. The system cannot replace the certified stall warning system. No performance credit
can be taken from the system, such as reduced approach speeds, reduced takeoff or landing
distances, etc.
1.5.2
The aircraft Pilot Operating Handbook or Aircraft Flight Manual always supersedes this
system’s manual.
1.5.3
SCc cannot be installed in a Commuter or Transport category airplane.
Specifications
1.6
Operational Temperature Range
-45°C to 70°C (DO160G Level B2)
Survival Temperature Range
-55°C to 70°C (DO160G Level B2)
Operating Humidity Range
DO160G Level B (95% max.)
Operating Altitude Range
0 – 25,000 ft. (DO160G Level B2)
Operating Airspeed Range
V
S0
to ~2 x V
S0
Precipitation
No limitations
Icing
Not for use in icing conditions
Deicing Fluids
No limitations
Emissions of RF Energy
DO/160G Category M
Voltage Operating Range
10-32 V
