clunk1001
23rd Oct 2012, 08:34
Hi,
Hopefully someone can shed some light on this relatively trivial query.
The PA34 Seneca II has electric fuel pumps (with HI and LO setting), the POH makes reference to the auxiliary pumps as a backup to the engine driven pumps, also in relation to vapour suppression and as part of the cold weather start procedure.
Other Piper aircraft POHs (at least the ones I've flown e.g. PA28 Arrow II) are much more specific and state that the Auxiliary pump should be ON during takeoff and landing and changing tanks.
I've noticed that some schools teaching IR/MEP do not use Electric Pumps during takeoff, and some do.
I cannot understand why you wouldn't have the Pumps on LO for takeoff. A failure of an engine driven pump right after rotation on a short strip (below vyse, no more runway) is going to be very messy. And I can't understand why the POH doesn't include any mention to this practice specifically.
Can anyone shed any light on :
(a) why you would not have the electric pumps on LO during take-off,
(b) why the PA34 POH is far less specific about the operation of the Electric Pumps than other Piper aircraft POHs?
Thanks
Clunk
Hopefully someone can shed some light on this relatively trivial query.
The PA34 Seneca II has electric fuel pumps (with HI and LO setting), the POH makes reference to the auxiliary pumps as a backup to the engine driven pumps, also in relation to vapour suppression and as part of the cold weather start procedure.
Other Piper aircraft POHs (at least the ones I've flown e.g. PA28 Arrow II) are much more specific and state that the Auxiliary pump should be ON during takeoff and landing and changing tanks.
I've noticed that some schools teaching IR/MEP do not use Electric Pumps during takeoff, and some do.
I cannot understand why you wouldn't have the Pumps on LO for takeoff. A failure of an engine driven pump right after rotation on a short strip (below vyse, no more runway) is going to be very messy. And I can't understand why the POH doesn't include any mention to this practice specifically.
Can anyone shed any light on :
(a) why you would not have the electric pumps on LO during take-off,
(b) why the PA34 POH is far less specific about the operation of the Electric Pumps than other Piper aircraft POHs?
Thanks
Clunk