Beechcraft Baron 58 - Page 66

Section II
Limitations
BEECHCRAFTBaron 58
Serial TH
773 and After
On Left Sidewall of Utility Compartment or Aft Bulkhead
(with utility door removal kit):
BAGGAGE COMPARTMENTS
LOAD IN ACCORDANCE WITH
WEIGHT
AND BALANCE DATA
o
MAXIMUM STRUCTURAL CAPACITY
MAIN COMPARTMENT· 400 POUNDS
AFT COMPARTMENT· 120 POUNDS
o
WHEN' UTILITY DOORS ARE REMOVED THE FOLLOWING
RESTRICTIONS APPLY TO
CABIN AREA:
1. NO SMOKING
2. ALL LOOSE OBJECTS MUST BE SECURED
3. PERSONNEL
NOT SECURED IN SEATS BY SAFETY
BELTS
MUST WEAR PARACHUTES
On Floating Panel when Utility Doors are Removed:
WHEN UTILITY DOORS ARE
REMOVED AIR SPEED IS NOT TO
EXCEED
174 KNOTS
In Plain View When Nose Baggage Compartment Door Is
Open:
o
BAGGAGE COMPARTMENT
LOAD IN ACCORDANCE WITH
AIRPLANE FLIGHT MANUAL
o
2-22
MAXIMUM STRUCTURAL CAPACITY - 300 POUNDS
August, 1984