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Newbie 2
15th Mar 2007, 10:38
Hi everyone,

Currently doing my initial multi endorsement paper on PA44. When doing a walk around noted that it appeared to have to stall warning devices on the left wing, is this correct? Also noted appeared to be placed at two different angles to the leading edge.

Does anyone have any thoughts on what they might be and why the differing angles?

:ugh:

Appreciate any help

Peter Fanelli
15th Mar 2007, 17:49
The Grumman Cougar does also.
If I recall correctly in both cases one is for the clean configuration and the other if for a full flap config.
Or it might be the second is for ANY flaps config, it was a long time ago :)

Bling-Blot
16th Mar 2007, 00:21
Newbie2
The 2 Stall warning detectors on the leading edge of the PA44 are indeed for different airframe configurations. The inboard one is for flaps 25 or 40. The outboard detector is for the other flap positions.

You cannot check them on the ground, a squat switch in the system prevents them being activated on the ground.

Hope this helps!

Cheers
BB