Emergency Airspeeds (5500 Lbs); One-Engine-Inoperative Procedures; Controllability Vs. Airspeed - Beechcraft Baron G58 Pilot Operating Handbook

Section 3
Emergency Procedures

EMERGENCY AIRSPEEDS (5500 LBS)

One-Engine-Inoperative Best Angle-of-Climb (V
One-Engine-Inoperative Best Rate-of-Climb (V
Air Minimum Control Speed (V
One-Engine-Inoperative Enroute Climb . . . . . . . . . . . . 101 kts
Emergency Descent . . . . . . . . . . . . . . . . . . . . . . . . . . . 152 kts
One-Engine-Inoperative Landing (5400 lbs):
Maneuvering to Final Approach . . . . . . . . . . . . . . . 107 kts
Final Approach (Flaps Down) (30°) . . . . . . . . . . . . . 95 kts
Intentional One-Engine-Inoperative
Speed (V
SSE
Maximum Range Glide . . . . . . . . . . . . . . . . . . . . . . . . . 115 kts
The stall warning horn is inoperative when
the battery and alternator switches are
turned off.

ONE-ENGINE-INOPERATIVE PROCEDURES

CONTROLLABILITY VS. AIRSPEED

Airspeed is the single most important factor in maintaining air-
plane control during single engine operations. The airplane
can be safely maneuvered or trimmed for normal hands-off
operation and sustained in this configuration by the operative
engine AS LONG AS SUFFICIENT AIRSPEED IS MAIN-
TAINED.
3-4
) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 88 kts
) . . . . . . . . . . . . . . . . 84 kts
MCA
Model G58
) . . . 95 kts
XSE
). . . 101 kts
YSE
April, 2008