about 737NG alternate flap extention
Thread Starter
Join Date: May 2012
Location: earth
Age: 36
Posts: 50
Likes: 0
Received 0 Likes
on
0 Posts
about 737NG alternate flap extention
today i flew a simulator lessen , i met a right eigine fire with DC bus 1 off.it took a system b failure to me , when i try to extend flap use the alternate flap switch , nothing happened ,looks like the motor is not move .my question is which bus is assoicate with the alternate flap motor?
Join Date: Apr 2010
Location: Home soon
Posts: 0
Likes: 0
Received 0 Likes
on
0 Posts
The standby hydraulic Electrical motor driven pump is using 115 V AC,3phase 400HZ.
Moving the switch to ARM,will send 28V DC power to energize the stby pump relay.
This relay sends 115 V AC (transfer bus2) power to the standby hydraulic system Electric motor.
Moving the switch to ARM,will send 28V DC power to energize the stby pump relay.
This relay sends 115 V AC (transfer bus2) power to the standby hydraulic system Electric motor.
Last edited by de facto; 11th May 2012 at 13:41.
Join Date: Mar 2001
Location: I wouldn't know.
Posts: 4,499
Likes: 0
Received 0 Likes
on
0 Posts
I think he was asking about the electric motor for the trailing edge devices, not the standby hydraulic for the leading devices.
@sky-738 sorry, can't really help you there as the documentation available to me does not specify which bus powers the alternate flap extension trailing edge motor. Sadly documentation has been dumbed down way too much, try to get hold of an AMM or similar documentation if you can.
@sky-738 sorry, can't really help you there as the documentation available to me does not specify which bus powers the alternate flap extension trailing edge motor. Sadly documentation has been dumbed down way too much, try to get hold of an AMM or similar documentation if you can.
