DOCUMENT No.:
REVISION: 1.2
DATE: 2014/11/10
DC-MAM-001-X-C-2
Page 194
PROCEDURE (REMOVAL)
The procedures described below are general. Reference must be made to the applicable equipment
/ system documentation with regard to the connection and disconnection of mechanical cables,
electrical wires, signal wires and fluid piping. The following documents have relevance:
Rotax 914 UL installation manual, maintenance manuals
and operator’s manual.
AP3 series and AP4 series constant speed propeller operator’s manual.
MGL RDAC and EFIS documentation.
Retain any bolts, clamps, spacers, screws and washers (with the exception of lock-washers) for
reassembly.
1. Support the tail of the aircraft adequately before removing the engine.
2. Remove the propeller (refer to paragraph 5.3.4) if the intention is to remove the engine without
the propeller attached.
3. Remove the top and bottom cowls (refer to paragraph 5.1.1).
4. Undo the clamps (1) retaining the oil reservoir to the firewall bracket. Removing the oil reservoir
with the engine (i.e. not disconnecting the piping) has the advantage that the oil system remains
closed and negates the need for refilling. Alternatively the piping (2) to the oil reservoir can be
disconnected, leaving the oil reservoir behind on the firewall.
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Summary of Contents for Sling 4
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