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AGUSTA A109E - Page 332

AGUSTA A109E
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SECTION 1 - LIMITATIONS
ECS OPERATION
Above 2000 ft pressure altitude (Hp), the ECS shall be OFF during take off
and landing and in flight below 200 ft AGL.
At any altitude the ECS shall be OFF during single engine operation and in all
flight conditions requiring the maximum engine power available.
NOTE
If necessary, the ECS may be used in hovering in ground effect
not above 3 ft wheel height and in hovering out of ground effect
above 200 ft wheels height.
CENTER OF GRAVITY LIMITATIONS
After ECS installation the new empty weight and C.G. location must be
determined.
MISCELLANEOUS LIMITATIONS
During take off and landing with ECS ON, the operations with cargo hook or
external hoist are prohibited.
SECTION 2 - NORMAL PROCEDURES
ENGINE PRE-START CHECK
ECS switch : OFF.
SHUT-OFF #1 switch : OFF.
SHUT-OFF #2 switch : OFF.
RFM A109E
APPENDIX 5
Page 4 of 23 E.A.S.A. Approved
Rev. 44
UNMAINTAINED COPY