Safety; Repeating Symbols; Safety Information - Rotax 447 UL SCDI Installation Manual

1) Safety

Although the mere reading of such an instruction does not eliminate a hazard, the understand-
ing and application of the information will promote correct use.
The information and components-/system descriptions contained in this Maintenance Manual
are correct at the time of publication. ROTAX
improvement of its products without imposing upon itself any obligation to install them on its
products previously manufactured.
ROTAX reserves the right at any time to discontinue or change specifications, designs,
®
features, models or equipment without incurring obligation.
The figures in this Maintenance Manual show the typical construction. They may not
represent in full detail or the exact shape of the parts which have the same or similar function.
Specifications are given in the SI metric system with the USA equivalent in parenthesis.
Where precise accuracy is not required, some conversions are rounded off for easier use.
1.1)

Repeating symbols

This Manual uses the following symbols to emphasize particular information. These
indications are important and must be respected.
▲ WARNING:
■ ATTENTION: Denotes an instruction which, if not followed, may severely
◆ NOTE:
1.2)

Safety information

▲ WARNING:
▲ WARNING:
▲ WARNING:
Effectivity: 447 UL SCDI, 503 UL DCDI, 582 UL DCDI /mod. 99
AIRCRAFT ENGINES
INSTALLATION MANUAL
, however, maintains a policy of continuous
®
Identifies an instruction which, if not followed, may cause
serious injury including the possibility of death.
damage the engine or other component.
Indicates supplementary information which may be needed to
fully complete or understand an instruction.
This engine, by its design, is subject to sudden stoppage. Engine
stoppage can result in forced landings, no power landings or crash
landings. Such crash landings can lead to serious bodily injury or
death.
Never fly the aircraft equipped with this engine at locations, air-
speeds, altitudes, of other circumstances from which a successful
no-power landing cannot be made, after sudden engine stoppage.
Aircraft equipped with this engine must only fly in DAYLIGHT VFR
conditions.
This is not a certificated aircraft engine. It has not received any
safety or durability testing, and conforms to no aircraft standards.
It is for use in experimental, uncertificated aircraft and vehicles only
in which an engine failure will not compromise safety.
User assumes all risk of use, and acknowledges by his use that he
knows this engine is subject to sudden stoppage.
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Initial issue, May 01/99