ACA 8KCAB 2003, Руководство по летной эксплуатации

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FAA APPROVED
Page 18 of 19
AIRPLANE FLIGHT MANUAL - MODEL 8KCAB Revision: H
Issued:
2.1.21 Noise Characteristics
The noise level for this airplane
measured in accordance with FAR 36,
Appendix G at full throttle, 2700 RPM.
All Propellers:
76.79 dBA
No determination has been made by the Federal Aviation Administration that the
noise levels of this airplane are or should be acceptable or unacceptable for
operation at, into, or out of, any airport
2.2 Emergency Procedures
2.2.1 Engine Restart
Caution: If propeller ceases to turn, diving will not cause windmilling.
Fuel starvation may occur after a series of inverted maneuvers since the header
tank may have had insufficient time to refill. (See section 1.2.6)
Check:
1) Assume ERECT Flight Attitude
2) Throttle – ¾ Forward
3) Mixture – Full Forward
4) Propeller – Full Forward
5) Fuel Valve – On
6) Emergency Fuel Pump – On
7) Magnetos – On
8) Master –On
9) Starter – Engage if Windmill RPM is Insufficient
2.2.2 Alternate Air
If induction ice is indicated (gradual decrease in manifold pressure), use full
alternate air until all ice is dissipated.
2.2.3 Fuel Pressure Loss
For fuel pressure loss or fluctuation, turn “ON” the Emergency Fuel Pump.
2.2.4 Engine Fire (Ground)
1) Mixture - idle cut-off.
2) Fuel valve off.
3) Master & magneto switches - OFF.
4) Cabin heater off.
5) Extinguish with fire extinguisher.