Beechcraft Baron G58 Pilot Operating Handbook page 290

Section 6
Wt and Bal/Equip List
CREW FS 75.0
TO FS 82.0
AFT FACING PASS
FS 111.0 TO FS 115.0
PASS. FS 152.0
NOTES:
1
2
3
4
Notes
1. The floor structure load limit is 50 pounds per square foot
between the front and rear spars, and 100 pounds per square
foot aft of the rear spar.
2. Any combination of the 3rd, 4th, 5th and 6th seats may be
removed by the Owner/Operator or Pilot-in-Command, with the
appropriate Log Book approved entry and Weight and Balance
Record change. Refer to the Equipment List for seat weights
and arms.
3. All Maximum Baggage Weights include baggage, cargo and
installed equipment, if applicable. All baggage and cargo must
be secured with an approved retention system.
6-12
(PILOT)
(3RD
SEAT
PASS.)
(5TH
SEAT
PASS.)
Maximum Baggage Weight is 300 pounds.
Maximum Baggage Weight is 200 pounds between
Front and Rear Spars with aft facing or removed 3rd
and 4th seats. This location is not approved for
baggage when the 3rd and 4th seats are facing
forward.
Maximum Baggage Weight is 400 pounds aft of the
Rear Spar, with 5th and 6th seats removed, or 200
pounds with only the 5th or 6th seat removed.
Maximum Baggage Weight is 120 pounds.
FS -10.0
BAGGAGE FS 15.0
1
FS 39.0
(FRONT
SEAT
PASS.)
BAGGAGE
2
FS 108.0
(4TH
FWD FACING PASS
SEAT
PASS.)
FS 115.0 TO FS 120.0
BAGGAGE
3
FS 150.0
(6TH
SEAT
PASS.)
BAGGAGE
4
FS 180.0
Model G58
TH06C
053923AA.AI
December, 2009