A320 Ptu -- Stall Margin
Thread Starter
Joined: Jun 2006
Posts: 56
Likes: 0
From: Middle East
Hi,
1. Why Does the Power Transfer Unit PTU runs up for few seconds after ENG start and then goes off in A320??
2. Where can you get a better stall margin .. in higher or lower altitudes ??
Thanks
1. Why Does the Power Transfer Unit PTU runs up for few seconds after ENG start and then goes off in A320??
2. Where can you get a better stall margin .. in higher or lower altitudes ??
Thanks
Joined: May 2007
Posts: 204
Likes: 0
From: Italy
Hi Captain BH,
VS1G increases with increasing altitude, thus the margin will decrease. In normal law however, high AOA prot always keeps that margin at an acceptable level (alpha prot over alpha max).
Best Regard,
fredgrav
VS1G increases with increasing altitude, thus the margin will decrease. In normal law however, high AOA prot always keeps that margin at an acceptable level (alpha prot over alpha max).
Best Regard,
fredgrav
Joined: Oct 2009
Posts: 1,270
Likes: 0
From: UK
Hi,
h3dxb, It's not quite so simple as that - and FCOM doesn't give much guidance.
During the first engine start - the PTU does not run even when there's a pressure difference of 3,000 psi between Green & Yellow systems. This allows quicker start up of the engine by removing unnecessary drag from extra hydraulics. During the second engine start, the PTU is allowed to run - but it stops once the hydraulic pressure on the second engine is within the figure you quoted. So the PTU has now been tested.
MB2002. Affirm. On a previous, very sophisticated aircraft (L1011), I seem to remember we tested the ATMs (air turbine motors with a hydraulic pump) and the PTUs after engine start - and it was all described perfectly in the OPS manuals.
I've noticed in the sim, on the ground and with an engine failed - the PTU does not run when the parking brake is set! Where is that mentioned in FCOM?
h3dxb, It's not quite so simple as that - and FCOM doesn't give much guidance.
During the first engine start - the PTU does not run even when there's a pressure difference of 3,000 psi between Green & Yellow systems. This allows quicker start up of the engine by removing unnecessary drag from extra hydraulics. During the second engine start, the PTU is allowed to run - but it stops once the hydraulic pressure on the second engine is within the figure you quoted. So the PTU has now been tested.
MB2002. Affirm. On a previous, very sophisticated aircraft (L1011), I seem to remember we tested the ATMs (air turbine motors with a hydraulic pump) and the PTUs after engine start - and it was all described perfectly in the OPS manuals.
I've noticed in the sim, on the ground and with an engine failed - the PTU does not run when the parking brake is set! Where is that mentioned in FCOM?
Last edited by rudderrudderrat; 25th February 2010 at 13:43. Reason: tech term




