De Icing Proc while HYD system is depressurized.
Thread Starter
Join Date: Nov 2016
Location: Hong Kong
Posts: 8
De Icing Proc while HYD system is depressurized.
Hi folks,
De Ice proc in parking bay before push. Is there any difference between having aircraft HYD system being pressurized or not during being sprayed? In other words, having HYD system pressurized would reduce the chance of de ice agent entering the opening between flight controls and wings/tail?
Thank you very much for sharing your wisdom online! Stay safe, guys.
De Ice proc in parking bay before push. Is there any difference between having aircraft HYD system being pressurized or not during being sprayed? In other words, having HYD system pressurized would reduce the chance of de ice agent entering the opening between flight controls and wings/tail?
Thank you very much for sharing your wisdom online! Stay safe, guys.
Join Date: Jan 2014
Location: N5109.2W10.5
Posts: 664
Thread Starter
Join Date: Nov 2016
Location: Hong Kong
Posts: 8
Hi Goldenrivett,
I agree. The problem is, de ice agent can freeze up in the air as well. So I was wondering if pressurizing HYD system before being sprayed could have prevented or reduced the chance or amount of de ice agent trapped in the opening. As far as I know, there's no difference. With or without HYD pressure, the size of opening between the flight controls and wings/tail remains the same in my opinion. But I know I don't know everything about my Boeing. Thus I am here to ask for help.
I agree. The problem is, de ice agent can freeze up in the air as well. So I was wondering if pressurizing HYD system before being sprayed could have prevented or reduced the chance or amount of de ice agent trapped in the opening. As far as I know, there's no difference. With or without HYD pressure, the size of opening between the flight controls and wings/tail remains the same in my opinion. But I know I don't know everything about my Boeing. Thus I am here to ask for help.
Join Date: Feb 2002
Location: UK
Age: 55
Posts: 2,927
It used to be a requirement to position the 737 stab LE up before deicing to allow any fluid to drain from the elevator/stab hinge line void area. That is the only reason I know of hydraulics on before deicing.
Join Date: Oct 2013
Location: McHales Island
Age: 65
Posts: 160
okipoki,
On your Boeing, you will find rubber "P" seals installed on fixed structure of various sizes and lengths which are designed to rub against and provide an almost airtight seal between airfoil and structure irrespective if hyd sys is pressurised or not.
Have a closer look on your next walk around and you will see some of them, especially when systems are unpressurised and flight controls are drooping. Hope this helps.
On your Boeing, you will find rubber "P" seals installed on fixed structure of various sizes and lengths which are designed to rub against and provide an almost airtight seal between airfoil and structure irrespective if hyd sys is pressurised or not.
Have a closer look on your next walk around and you will see some of them, especially when systems are unpressurised and flight controls are drooping. Hope this helps.