Landing Gear Retraction After Practice Manual Extension - Beechcraft Baron G58 Pilot Operating Handbook

Model G58
6. If the electrical system is operative, a positive gear down
indication can be made as follows:
a. LDG GR WARN and LDG GR POS LTS
Circuit Breaker . . . . . . . . . . . . . . . . . . . . . .CHECK IN
b. Landing GEAR DN &
LOCKED Lights. . . . . . . . . .ILLUMINATED (3 green)
c. CHECK that the gear warning horn does not sound
when either throttle is retarded to idle.
7. Handcrank . . . . . . . . . . . . . DISENGAGE, THEN STOW
8. Do not move the Landing Gear Handle or reset the
LANDING GEAR MOTOR Circuit Breaker.
9. The landing gear should be considered UNLOCKED
until the airplane is on jacks and the system has been
cycled and checked.
Do not operate the landing gear electrically
with the handcrank engaged. Damage to
the mechanism could occur.
The manual extension system is designed
to lower the landing gear only. DO NOT
ATTEMPT TO RETRACT THE GEAR
MANUALLY.
LANDING GEAR RETRACTION AFTER PRACTICE
MANUAL EXTENSION
After practice manual extension of the landing gear, the gear
can only be retracted electrically, as follows:
1. Handcrank . . . . . . . . . . . . . . . . . . CONFIRM STOWED
2. LANDING GEAR MOTOR Circuit Breaker . . . . . . . . . IN
3. Landing Gear Handle . . . . . . . . . . . . . . . . . . . . . . . . . UP
April, 2008
Section 3A
Abnormal Procedures
3A-9