R.A.I. Approval Letter 97/3147/MAE
dated 30 July 1997
The information contained herein supplements the information of
the basic Rotorcraft Flight Manual.
For limitations, procedures and performance data not contained
in this appendix, consult the basic Rotorcraft Flight Manual.
SUPPLEMENTARY FUEL TANKS
The supplementary fuel tanks installation P/N 109-0811-49 provides an
additional 265 liters capacity. It consists of two tank cells (RH cell of 105 liters
and LH cell of 160 liters) installed behind the passenger seat. However the
installation can be arranged as follows:
- Both LH and RH tank cells installed.
- Only RH tank cell installed.
The fuel transfer from the supplementary fuel tank cells to the main fuel cell
is by gravity. The two tank cells are separated by panels; each cell is provided
with a fuel level probe.
RFM A109E
APPENDIX 8
Page1of8
Rev. 11
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