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<< Lancair Builders' Mail List >>
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In a message dated 2/20/2002 12:04:36 AM Pacific Standard Time,
dfs155@earthlink.net writes:
<<<...From the forces resulting from a prop strike/sudden stoppage, the crank
can
suffer a crack if not outright failure...>>>
Dan:
Sage advice, but perhaps wasted.
Do you think a guy who does taxiway departures is going to be influenced by
the experience-developed procedures regarding sudden stoppages contained in
such publications as Lycoming Service Bulletin 533-A, Continental Service
Bulletin 96-11, Woodward (prop governors) Service Bulletin 33574B, McCauley
(prop governors) Service Bulletin SB 215B, or the Slick (magnetos) Overhaul
Manual?
For anyone interested, a prop strike has the potential to severely damage NOT
ONLY the prop and crankshaft/propshaft, but ALSO all accessories,
accessory-drives, and recip parts in the engine. Lycoming, Continental, and
others define a "propeller strike" as follows (from Lyc SB-533-A):
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(a) Any incident, whether or not the engine is operating,
that requires repair to the propeller other than minor
dressing of the blades;
(b) Any incident during engine operation in which the
propeller impacts a solid object which causes a drop
in RPM and also requires structural repair of the
propeller (incidents requiring only paint touch-up
are not included). This is not restricted to propeller
strikes against the ground, and although the propeller
may continue to rotate, damage to the engine may
result, possibly progressing to engine failure.
(c) A sudden RPM drop while impacting water,
tall grass, or similar non-solid medium, where propeller
damage is not normally incurred.
The above definitions encompass any propeller strike
occurring at taxi speeds and during touch-and-go operations,
involving propeller tip ground contact. In addition, they
also include situations where an aircraft is stationary
and the landing gear collapses causing one or more
blades to be bent or substantially damaged, or where
a hangar door (or other object) strikes the propeller
blade. These cases should be handled as a sudden
engine stoppage because of potentially severe side
loadings on the propshaft flange, front bearing, and seal.
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Complete disassembly and inspection (per ASTM E-1444 or E-1417) of engine and
accessories is required by all the abovementioned publications. Some will
argue it's overkill; I would respond that if you believe it's overkill, you
are deeply involved in wishful thinking (as opposed to rational thought).
Yes, many post-strike inspections find no damage. But when actual damage is
discovered, it has the high potential of being fatal.
For more info on prop strikes
(and info on the forced landing of a Lancair-4P), visit:
http://www.epi-eng.com/Propeller_Damage.htm
Jack Kane
EPI, Inc.
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