Landing Emergencies; One-Engine-Inoperative Landing - Beechcraft Baron G58 Pilot Operating Handbook

Serials th-2125 and after
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Section 3A
Abnormal Procedures
b. Starter . . . . . . . . . . . . . . . . . . . . . . . . . . . . ENGAGE
c. If engine fails to run, clear engine by allowing it to
windmill with mixture in CUT OFF. When engine fires,
advance mixture to full rich.
8. After Engine Starts . . . . . . . . . . . ADJUST THROTTLE,
9. Fuel Boost Pump. . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
10. Alternator. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
11. Oil Pressure. . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
12. Warm Up Engine (approximately 1500 RPM and 15 in.
Hg)
13. Power . . . . . . . . . . . . . . . . . . . . . . . . . . .AS REQUIRED
14. Trim . . . . . . . . . . . . . . . . . . . . . . . . . . . . .AS REQUIRED

LANDING EMERGENCIES

ONE-ENGINE-INOPERATIVE LANDING

On final approach and when it is certain that the field can be
reached:
1. Landing Gear. . . . . . . . . . . . . . . . . . . . . . . . . . . . DOWN
2. Flaps . . . . . . . . . . . . . . . . . . . . . . . . . APPROACH (15°)
3. Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 107 KTS
4. Power . . . . . . . . . . . . . . . . . . . . . . . . . . .AS REQUIRED
When it is certain there is no possibility of go-around:
5. Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DOWN (30°)
6. Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 95 KTS
7. Execute Normal Landing
3A-4
(to accomplish unfeathering)
PROPELLER and MIXTURE
(when reliable power has been regained)
(to maintain 800 ft/min rate of descent)
Model G58
CONTROLS
April, 2008

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