HK 36 TC with Rotax 912 S3
Flight Manual
Mass & Balance
Doc. No. 3.01.12-E
Rev. 1
06 Oct 2003
Page 6 - 4
6.4
BASIC EMPTY MASS AND MOMENT
The empty mass CG limitations are defined in the Airplane Maintenance Manual,
Section 4.
These limitations guarantee that solo-pilots with a mass (weight) of at least 70 kg
(154 lb) will not overstep the maximum rearward CG when flying with a full tank and no
baggage.
The CG will not exceed the maximum forward position if not more than 220 kg (485 lb)
of useful load on the seats and 10 kg (22 lb) of fuel for a half hour flight are aboard.
6.5
MASS OF ALL NON-LIFTING PARTS
The maximum mass (weight) of all non-lifting parts is 610 kg (1345 lb). A list of all
non-lifting parts is included in the Airplane Maintenance Manual, Paragraph 4.6.
NOTE
Due to the design of the HK 36 TC, the maximum mass
(weight) of all non-lifting parts will not be exceeded as long
as the maximum flight mass (max. gross weight) of 770 kg
(1698 lb) is complied with.
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