Beechcraft Baron G58 Pilot Operating Handbook page 296

Section 6
Wt and Bal/Equip List
WEIGHT AND BALANCE LOADING FORM
Serial No.: ______________
LINE
1. BASIC EMPTY WEIGHT
2. Pilot and Front Seat Passenger
3. 3rd and/or 4th Seat Passengers
4. 5th and/or 6th Seat Passengers
5. Baggage - Nose Compartment
6. Baggage - Between Spars
7. Baggage - Aft of Rear Spar
8. Baggage - Aft Compartment
9. Other -
10. ZERO FUEL WEIGHT
11. Fuel Load
12. RAMP WEIGHT
(DO NOT EXCEED 5524 LB)
13. *Less Fuel for Start, Taxi and Run-Up
14. TAKE-OFF WEIGHT
(DO NOT EXCEED 5500 LB)
15. Fuel Load from Line 11.
16. Less Fuel to Destination including Start,
Taxi and Run-up from Line 13.
17. Fuel Remaining - Moment/100 from
Usable Fuel Table
18. Zero Fuel Weight from Line 10.
19. Add Fuel Remaining from Line 17.
20. LANDING WEIGHT
(DO NOT EXCEED 5400 LB)
* Fuel for start, taxi and run-up is typically 24 lb with a Moment/100 of
20 lb-in., which may operationally vary.
6-18
Date: ___________
ITEM
Model G58
WEIGHT ARM
(lb) (in.)
152.0
15.0
108.0
150.0
180.0
December, 2009
MOMENT
100
(lb-in.)