Quoting Silver1SWA (Reply 20): Here's another example of how things are done differently at different airlines. My friends that have worked at different companies all say they used the bypass pins to push or tow aircraft. At WN, the captain will turn the A-pumps off prior to releasing the breaks for pushback. He communicates to the pushback agent via headset that "the 'A's are off". This allows free movement during pushback giving the driver full steering control. After we disconnect the towbar, as we pull away from the aircraft the captain will turn the A-pumps back on. If the nose-wheel was not left in the perfectly straight position, you will actually see the nose-wheel straighten out.
Sometimes things don't always work out properly though. I was pushing out of a gate one day that required an immediate turn. As I cranked the wheel, POP! The shear pin on the towbar snapped violently (as it is designed to do). I was like "uhhh...towbar just snapped". Captain replies saying, "hmmm...well, apparently the A-pumps didn't turn off". He couldn't get them to turn off. The rest of the push, after replacing the towbar had to go straight back.
I have also had the pumps accidentally turned on (only explanation I can think of) during the push. Haha, I was in the middle of a turn, everything seemed fine and then BAM! There went another towbar pin.
It can be dangerous if procedures are not followed correctly. If a nose-wheel was not in the straight position and the towbar was still connected (this should never be the case), if the pumps are turned on, LOOK OUT! |
First,
WN could still be using procedures originally written for the 737-200, which didn't have a NLG bypass valve. There the pilot had to depressurise hydraulic system A by turning off both the engine driven pump (EDP) and the A sys electrical motor driven pump (EMDP). From the 737 classic on a NLG bypass valve was installed, so that the pumps could stay on, but probably
WN kept the same procedures for their whole fleet to prevent confusions.
Secondly, the EDP is permanently connected to the engine gearbox. There is no way to keep it from turning except by shutting down the related engine (or having the drive shaft shear off at a noth in case the pump jams).
To remove presssure from the EDP, you operate a switch in the cockpit, which will energise a solenoid valve in the pump, which, when opened, will short circuit the pump output line directly to the pump input, so that the pump will just move fluid in a circle, without providing pressure.
This switch and valve are normally to be off (Pump
ON). If you leave it on (Pump OFF) for a longer period of time, without the pump moving fluid, the solenoid can overheat and get damaged.
I think this was the case in your example. The pilot set the A sys EDP switch to off but due to some reason, most probably a fried solenoid, the valve didn't open, so that the pump kept delivering pressure to the A system. In such a case the pilot should have returned to gate and let
MX change the pump, since the shut off function is opart of the emergency functions and AFAIK not deferrable.
Jan