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Stefan,
I am sorry that the original message concerning AD 76-07-12 was
corrupted. In essance, the AD speaks to a problem with the ignition
switch. I will attempt to attach the AD one more time.
Again, Best Wishes, Jack
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<P>76-07-12
<BR>
<BR>BENDIX IGNITION SWITCHES
<BR>
<BR>Amendment 39-2575 as amended by Amendment 39-3024
<BR>
<BR>Applies to All aircraft employing magnetos and using Bendix ignition
switches
<BR>listed in the table below except switches identified by four digit
date code (new)
<BR>adjacent to the model number or a white dot (modified) on the support
plate
<BR>adjacent to the Bendix logo.
<BR>
<BR> &nbs
p;
&n
bs
p;
Rotary Action,
<BR> Bendix
Switches
&n
bsp;
Key or Lever Actuated
<BR> Switch
Function
&n
bsp;
Bendix (series) Part Numbers
<BR>
Twist-to-Start
&n
bsp;
10-357XXX, 10-126XXX
<BR> Twist-to-Start/Push-to-Prime
10-357XXX,
10-126XXX
<BR>
Push-to-Start &
nb
sp;
10-357XXX, 10-126XXX, 10-157XXX
<BR>
<BR>Compliance required as indicated:
<BR>
<BR>1. For switches subject to this AD, conduct the following checks
within
the
<BR>next 100 hours' time in service and each 100 hours thereafter to
detect
<BR>possible switch malfunction:
<BR>
<BR>(a) Observing regular ground run-up procedures, allow the engine to
<BR>reach operating temperatures and perform a normal magneto check.
<BR>
<BR>(b) With the engine at normal idle, rotate the switch key or lever
through
<BR>the "OFF" detent to the extreme limit of its travel in the "OFF"
<BR>direction.
<BR>
<BR>(c) If the engine stops firing, this indicates an airworthy switch.
<BR>
<BR>(d) If the engine continues to run with the switch in the extreme
"OFF"
<BR>direction indicating a malfunctioning switch, prior to the next flight
<BR>accomplish Part III outlined in Bendix Service Bulletin No. 583, dated
<BR>April 1976, for Repair and Replacement or use an alternate method
<BR>approved by Chief, Engineering and Manufacturing Branch, Eastern
<BR>Region.
<BR>
<BR>2. The aircraft may be flown in accordance with FAR 21.197 to
a place
<BR>where these modifications can be accomplished.
<BR>
<BR>3. The checks required by this AD may be performed by the pilot.
<BR>
<BR>4. Upon submission by an operator with substantiating data, an FAA
<BR>Maintenance Inspector subject to prior approval of the Chief,
Engineering
<BR>and Manufacturing Branch, FAA Eastern Region may adjust the
<BR>compliance times specified in this AD if the request contains
<BR>substantiating data to justify the increase for the operator:
<BR>
<BR>NOTE
<BR>
<BR>If the engine continues to run when complying with paragraph 1 and
<BR>repair or replacement cannot or will not be accomplished immediately,
<BR>the magneto (primary circuit) should be grounded in accordance with
<BR>Bendix Service Bulletin No. 583, dated April 1976.
<BR>
<BR>Amendment 39-2575 was effective April 14, 1976.
<BR>
<BR>This amendment 39-3024 is effective August 30, 1977.
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