B737 NG PTU and LGTU
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Join Date: Feb 2005
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B737 NG PTU and LGTU
With a loss of hydraulic B the PTU uses system A to power the LE devices. Does this just use system A pressure or does it actualy use system A fluid?...(think its just pressure but not sure)
Equaly with loss of system A, System B powers the LGTU to enable normal gear retraction (with a few specific requirements). Does this just once again use the B pressure to raise the gear or does it actualy use B fluid?
Equaly with loss of system A, System B powers the LGTU to enable normal gear retraction (with a few specific requirements). Does this just once again use the B pressure to raise the gear or does it actualy use B fluid?
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For what it's worth, the LGTU doesn't care at all about hyd sys A, only eng 1 N2 (56% springs to mind, but certainly willing to be corrected)
Cheers
Buter
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Buter
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