SC-POH-1-1-17
SECTION 6
WEIGHT & BALANCE
Revision: -
Date of issue: 2011-09-01
S
S
p
p
o
o
r
r
t
t
C
C
r
r
u
u
i
i
s
s
e
e
r
r
6-3
-
Obtain measurement LN by measuring horizontally and parallel to the
airplane center line, from center of nose wheel axle left sides, to the datum
on the left wing. Repeat on right side and average the measurements.
5.
Using weights from item 3 and measurements from item 4 the airplane
weight and C.G. can be determined.
6.
Basic Empty Weight may be determined by completing appropriate table.
6.3 Operating weights and loading
Weights:
Max. takeoff weight ...........................................................
1,320 lb
Max landing weight ...........................................................
1,320 lb
Max. weight of fuel ............................................................
180 lb
Max. baggage weight in rear fuselage ..............................
40 lb
Max. baggage weight in each wing locker ........................
22 lb
Empty weight (minimum equipment) .................................
760 lb
Crew:
Number of seats ...............................................................
2
Minimum crew
(only
on the left seat)
...............................
1
pilot
Minimum crew weight .......................................................
121 lb
Maximum crew weight on each seat .................................
253 lb
Arms:
Pilot/Passenger ................................................................
27.56 in
Baggage compartment .....................................................
51.58 in
Wing lockers .....................................................................
23.62 in
Fuel tanks .........................................................................
7.09 in
NOTE
Actual Empty weight is shown in Section 9, Supplement No. 02.
NOTE
For the needs of this Handbook the fuel specific weight of 6 lb/US gal was used to
convert volume units into weight units.
