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.
ROTOR BRAKE
The Rotor Brake P/N 109-0810-63, consists of a disc type brake, operating
lever, the tubing and fittings required for attachment.
Installation of the rotor brake permits rapid deceleration of the rotor after
engine shut-down.
The rotor brake operation is pointed out by activation of ROTOR BRAKE ON
caution message on EDU 1.
RFM A109E
APPENDIX 1
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