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Converted with kit
NS402S with ROTAX 912 S3 and
HOFFMANN HO-V352F/170FQ+10
LOADING EXAMPLE
1.
Basic Empty Weight (Use the data
pertaining to your airplane as it is pres-
ently equipped. Includes unusable fuel
and full oil)
2.
Usable fuel (SPG. 0,72 kg /ltr.)
•
Standard tanks (85,2 ltr. max.)
•
Long range tanks (132,5 ltr. max.)
(reduced fuel as limited by maximum weight )
3.
Pilot and passenger (Sta. 84 to 104
cm)
4.
Baggage area 1 (or passenger on child
seat) (Sta. 127 to 193 cm, max. 54 kg)
5.
Baggage area (2) (Sta. 193 to 239 cm)
6.
TOTAL WEIGHT AND MOMENT
7.
Locate this point (65.3 cmkg/1000 at 725.7 kg) on the Center of Gravity Moment
Envelope, and since this point falls within the envelope, the loading is acceptable.
Fig. 7c - 3 – Sample loading problem
Airplane Flight
Manual Cessna F150L
Example airplane
Weight
kg
496.7
61.2
154.2
13.6
725.7
(example)
Moment/1000
Weight
cmkg
41.3
6.5
15.3
2.2
65.3
Nr. 160
7-5c
Page:
Revision 1
Your airplane
Moment/1000
kg
Cmkg
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