2 quick questions
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2 quick questions
Hi guys,
Was recently asked by a colleague for the answers and I'm stumped.
Why do multi-engine turbines start the number 2 engine first?
What are the fins (vanes or strakes?) on the inside portion of the engine pods on most jet transports?
I suppose I must have fallen asleep during groundschool when these came up.
Was recently asked by a colleague for the answers and I'm stumped.
Why do multi-engine turbines start the number 2 engine first?
What are the fins (vanes or strakes?) on the inside portion of the engine pods on most jet transports?
I suppose I must have fallen asleep during groundschool when these came up.
Per Ardua ad Astraeus
Join Date: Mar 2000
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Wot I wuz told:
Traditionally the battery on multi-engined pistons was on the starboard side hence less voltage drop if you start 2 first.
Fins designed to ensure engine will go under wing if it breaks away rather than over/through.
Stand-by for more 'reasons'.........................
Traditionally the battery on multi-engined pistons was on the starboard side hence less voltage drop if you start 2 first.
Fins designed to ensure engine will go under wing if it breaks away rather than over/through.
Stand-by for more 'reasons'.........................
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Why do multi-engine turbines start the number 2 engine first?
What are the fins (vanes or strakes?) on the inside portion of the engine pods on most jet transports?
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There is no specified mandatory sequence of engine starting.
Individual airline requirements will generally dicate the starting sequence.
Taking in to consideration passenger boarding, elimination or reduce possible hydraulic system pump noise etc
Individual airline requirements will generally dicate the starting sequence.
Taking in to consideration passenger boarding, elimination or reduce possible hydraulic system pump noise etc
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The right side usually is started first, as pax door/jetway is on the left side. In the case of a trijet like the DC10 or L10, usually the center engine is started first as it is closest to the APU pneumatic source.