MOONEY
M20V ACCLAIM ULTRA
SECTION VI
WEIGHT AND BALANCE
6 - 8
AIRPLANE FLIGHT MANUAL
ORIGINAL ISSUE - 03-16-2017
PROBLEM FORM
A/C Basic Empty Wt. (W.) (from
STEP
ITEM
SAMPLE
PROBLEM
YOUR
PROBLEM
WEIGHT
(Kg)
Lbs
MOMENT
(Kg- cm
/1000)
lb- in
/1000
WEIGHT
(Kg)
Lbs
MOMENT
(Kg- cm
/1000)
lb- in
/1000
1
2
3
4
5
Pilot Seat (#1) *
Co- Pilot Seat (#2) *
Left Rear Seat (#3) or Cargo Area
Right Rear Seat (#4) or Cargo
Baggage (Max. 120 Lbs (54.4 Kg)
@ Sta. 101.5 (257.8 cm)
Hat Rack (Max. 10 Lbs (4.54 Kg)
@ Sta. 126.0 (320 CM)
CONTINUE PROBLEM FORM ON NEXT PAGE
(1009)
2225
(164.7)
363
(77.1)
170
(77.1)
170
(77.1)
170
(114.6)
99.46
(8.52)
7.40
(7.25)
6.29
(14.3)
12.41
(20.59)
17.87
(aft pos)
(2nd. pos)
page 6- 5) (includes Full Oil)
8 Qts (7.57 Li) @ 1.875 Lbs/Qt
(.80 Kg/Li) (Sta. - 20.19) (- 51.3 cm)
(Oil sump assumed FULL for
all flights)
(Max. Usable -
(386.1 Li/266.4 Kg) @ Sta 49.23
(125 cm)
* Obtain the moment/1000 value for each seat position (FWD, MID or AFT)
from loading computation graph.
Area
(77.1)
170
(14.3)
12.41
(45.4)
100
(11.70)
10.15
102.0 Gal/593.6 Lbs.)
Fuel
(Max. Usable -
(378.5 Li/264.0 Kg.) @ Sta 49.23
(125 cm)
100.0 Gal/582.0 Lbs.)
(164.7)
363
(20.59
17.87
Fuel
