Spins - Beechcraft Baron G58 Pilot Operating Handbook

Model G58
2. Rotate exposed red latch handle up (as indicated by
placard) breaking safety wire, and push window out.
Anytime the window has been opened by
breaking the safety wire on the red emer-
gency latch handle, the window must be
reattached and wired by a qualified
mechanic using a single strand of QQ-W-
343, Type S, .020 diameter copper wire
prior to further airplane operation.
For Access Past the 3rd and/or 4th seats:
1. Rotate red handle located on lower inboard side of seat
back.
2. Fold seat back over.

SPINS

Intentional spins are prohibited. If an unintentional spin is
encountered, perform the following procedure IMMEDIATELY
- THE LONGER THE DELAY, THE MORE DIFFICULT
RECOVERY WILL BECOME. Steps 1 through 3 should be
done AGGRESSIVELY and SIMULTANEOUSLY. The full for-
ward position of the control column may be reduced slightly, if
required, to prevent the airplane from exceeding a 90° nose
down (inverted) attitude.
1. Control Column. . . . . . . . . . . . . . . . FULL FORWARD,
2. Full Rudder . . . OPPOSITE THE DIRECTION OF SPIN
3. Power Levers . . . . . . . . . . . . . . . . . . . . . . . . . . . . IDLE
4. Controls . . . NEUTRALIZE WHEN ROTATION STOPS
5. Execute a smooth pullout.
April, 2008
Emergency Procedures
NOTE
AILERONS NEUTRAL
Section 3
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