Page 14 of 28 Sym B
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Dwg. 56201-2
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FLIGHT CHECK AND ADJUSTMENT
3.0
This procedure may involve flight at near stall conditions. Choose a safe
altitude to enable recovery in the event of a stall. The best results are
found in non-turbulent conditio
ns.
CAUTION
The aircraft’s primary stall warning system calibration must be
verified prior to AoA System calibration.
NOTE
Background
3.1
The Safe Flight SCc System is calibrated using a two-step process: accurate placement of
the Lift Transducer, followed by an in-flight calibration procedure using Landing Approach
and Low Airspeed Awareness data points.
Once the Lift Transducer is installed in the correct location, the system is ready for in-flight
calibration.
Transducer Location Verification Flight
3.2
Using the POH recommended landing approach speed, power setting, and flap extension, fly
a simulated approach (at a safe altitude for possible stall recovery) with the Lift Transducer
installed at its initial location.
If the Indexer Computer displays any of the following indications, the system is ready for the
final in-flight calibration.
Acceptable Indications before In-Flight Calibration
If not, the Lift Transducer needs to be moved on the wing. Land and follow Appendix C for
guidance on how to adjust the Lift Transducer. Then, repeat the verification flight test
procedure.
