Beechcraft Baron 58 - Emergency Static Air Source; Emergency Exits

Section III
Emergency Procedures
BEECHCRAFT Baron 58
Serial TH 773 and After
Verification of suspected obstruction is possible by
switching to the emergency system and noting a sudden
sustained change in rate of climb. This
may be accompanied
by
abnormal indicated airspeed and altitude changes
beyond normal calibration differences.
Whenever any obstruction exists in the Normal Static Air
System or the Emergency Static Air System is desired for
use:
1. Emergency Static
Air Source - Switch to ON
EMERGENCY.
(lower sidewall adjacent to pilot)
2. For Airspeed Calibration and
Altimeter Corrections,
refer to the PERFORMANCE section.
CAUTION
The emergency static air valve should remain in
the OFF
NORMAL position when system is not
needed.
EMERGENCY EXITS
Emergency exits, provided by the openable window on each
side of the cabin, may be used
for egress in addition to the
cabin door and the utility door.
NOTE
For access past the 3rd and/or 4th seats, rotate
the red handle, located on the
lower inboard
side of
the seat back. and fold the seat back
over.
3-16
Revised: March 1983