VansAirForceForums  
Home > VansAirForceForums

- POSTING RULES
- Donate yearly (please).
- Advertise in here!

- Today's Posts | Insert Pics


Go Back   VAF Forums > Main > Safety
Register FAQ Members List Calendar Today's Posts

Closed Thread
 
Thread Tools Search this Thread Display Modes
  #41  
Old 01-17-2009, 08:14 AM
pierre smith's Avatar
pierre smith pierre smith is offline
 
Join Date: Jan 2005
Location: Louisville, Ga
Posts: 7,840
Default A question for you Airline drivers..

...Since both engines went TU, what drives the hydraulics for control of the airplane? Batteries or APU?

Thanks,
__________________
Pierre Smith
RV-10, 510 TT
RV6A (Sojourner) 180 HP, Catto 3 Bl (502Hrs), gone...and already missed
Air Tractor AT 502B PT 6-15 Sold
Air Tractor 402 PT-6-20 Sold
EAA Flight Advisor/CFI/Tech Counselor
Louisville, Ga

It's never skill or craftsmanship that completes airplanes, it's the will to do so,
Patrick Kenny, EAA 275132


Dues gladly paid!
  #42  
Old 01-17-2009, 08:19 AM
jsharkey's Avatar
jsharkey jsharkey is offline
 
Join Date: Nov 2006
Location: Bennington, Vermont USA
Posts: 1,301
Default Possibly an Air Driven Generator

...a small windmill that drops out of the fuselage and spins in the breeze to generate enough power to keep essential controls working.
  #43  
Old 01-17-2009, 08:40 AM
airguy's Avatar
airguy airguy is offline
 
Join Date: Oct 2006
Location: Garden City, Tx
Posts: 5,118
Default

I was in the LAX terminal waiting for a flight while all this was unfolding, and I heard a couple pilots talking about systems and procedures on the A320. They SOUNDED like they knew what they were talking about....dunno....both these guys were corporate pilots with ATP experience.

Anyhow, the gist of the conversation was that coming out of that airspace, the crew would have still had the APU running at that point in time for hydraulic and electrical.
__________________
Greg Niehues - SEL, IFR, Repairman Cert.
Garden City, TX VAF 2020 dues paid
N16GN flying 700 hrs and counting; IO360, SDS, WWRV200, Dynon HDX, 430W
Built an off-plan RV9A with too much fuel and too much HP. Should drop dead any minute now.
  #44  
Old 01-17-2009, 10:03 AM
Bubblehead's Avatar
Bubblehead Bubblehead is offline
 
Join Date: Jul 2007
Location: Keller, TX
Posts: 1,553
Default USN Award for pilot

As a former USN guy, I have decided that given the aquatic nature of this incident the Navy should give the pilot a special award.

I have not decided yet whether it should be US Naval Aviator's wings or Submariner's Dolphins!
__________________
RV-8 180 hp IO-360 N247TD with 10" SkyView!

VAF Donations Made 8/2019 and 12/2019
"Cum omni alio deficiente, ludere mortuis."
(When all else fails, play dead.)
  #45  
Old 01-17-2009, 10:49 AM
rvbuilder2002's Avatar
rvbuilder2002 rvbuilder2002 is offline
 
Join Date: Jul 2005
Location: Hubbard Oregon
Posts: 9,026
Default

Quote:
Originally Posted by wrongway john View Post

We prop folks should be thankful for our shreaders, which should make them mince meat before they hit our windshields.

wj
It is not really relative to this thread, but a propeller does nothing to protect us from birds. Particularly at high speed. In the 360 deg space covered by the propeller the blade cord only covers a very small portion of it. With the relatively slow RPM the propeller turns, a bird can easily get through without being hit.
__________________
Opinions, information and comments are my own unless stated otherwise. They do not necessarily represent the direction/opinions of my employer.

Scott McDaniels
Van's Aircraft Engineering Prototype Shop Manager
Hubbard, Oregon
RV-6A (aka "Junkyard Special ")
  #46  
Old 01-17-2009, 11:49 AM
David-aviator David-aviator is offline
 
Join Date: Feb 2005
Location: Chesterfield, Missouri
Posts: 4,514
Default

Quote:
Originally Posted by pierre smith View Post
...Since both engines went TU, what drives the hydraulics for control of the airplane? Batteries or APU?

Thanks,
The later Boeings have a RAT....ram air turbine. The 707 was total manual control with cool aerodynamic balance chambers at each surface. The 727 was hydraulic with manual reversion.

The Douglas 9's and MD80's have manual controls with several thousand miles of cables. The rudder has a hydraulic boost package.

Don't know anything about the Airbus series except they are advanced electric. There was at least one Airbus accident at an air show where the crew got disconnected from controlling the airplane and it electronically flew into the ground. There was a story early on when the 320's began service in this country .... a crew entered a holding pattern and could not leave....that probably did not happen but it was a good story about automation in those days.

When I fly these days and file a report here I frequently refer to scanning for the enemy. That means birds like geese, turkey vultures, eagles, hawks and of course other airplanes. One has to scan constantly because one minute they are there and then they aren't. I get nervous just looking down long enough to change a radio frequency, the enemy is everywhere and very difficult to see, they are so relatively small. Generally, if an evasive maneuver is necessary, I climb as most of the time a bird will dive. He's probably thinking the airplane is a bigger carnivore and its time to hit the deck, not unlike a jumped fighter in WWII.
__________________
RV-12 Build Helper
RV-7A...Sold #70374
The RV-8...Sold #83261
I'm in, dues paid 2019 This place is worth it!
  #47  
Old 01-17-2009, 12:04 PM
cbo111's Avatar
cbo111 cbo111 is offline
 
Join Date: Feb 2007
Location: Bradenton, fl
Posts: 89
Default

I believe those **** Canadian Geese took out an AF AWACs Boeing 707-320 in Alaska back in the mid-90's. They definitely have more kills against our Air Force than any adversary since Vietnam.
Chuck Olsen
Tehachapi
RV-7A
  #48  
Old 01-17-2009, 12:11 PM
jmbrwn's Avatar
jmbrwn jmbrwn is offline
 
Join Date: Aug 2007
Location: Carrollton, GA
Posts: 313
Default

I flew the A320 for 8 yrs and think it's a very good airplane. Some airlines takeoff with the APU running. My airline does not. With the loss of both engines, the RAT (Ram Air Turbine) could be extended to provide hydraulic power to operate the flight controls. If the APU were not running, the RAT would also provide electrical power. Electrics would only be provided for the essential instruments for flight.
Most accidents involving the Airbus (all aircraft for that matter) are pilot error. As advanced as the aircraft is, it does exactly what you tell it to do.
__________________
Jim Brown
RV6, Christen Eagle II(Sold)
ATP, CFII, A-IGI, A&P/IA
Carrollton, GA
Lyon?s Landing
  #49  
Old 01-17-2009, 12:13 PM
rvbuilder2002's Avatar
rvbuilder2002 rvbuilder2002 is offline
 
Join Date: Jul 2005
Location: Hubbard Oregon
Posts: 9,026
Default

Quote:
Originally Posted by David-aviator View Post

Don't know anything about the Airbus series except they are advanced electric. There was at least one Airbus accident at an air show where the crew got disconnected from controlling the airplane and it electronically flew into the ground.
In this particular case (I don't know about others) the crew did not get disconnected. The flight control computer was designed to prevent the crew from stalling the airplane. They were doing a slow flight (relative) fly by at an airshow...got it behind the power curve, and waited too long to push the power levers up. Because of spool up lag time, etc., the speed continued to decay and regardless of how hard both pilots pulled on the pilot control input devices (I don't know if they can really be called sticks) the computer would not let the AOA increase beyond a programed value.
I believe their was some major software rewrites after that accident.
__________________
Opinions, information and comments are my own unless stated otherwise. They do not necessarily represent the direction/opinions of my employer.

Scott McDaniels
Van's Aircraft Engineering Prototype Shop Manager
Hubbard, Oregon
RV-6A (aka "Junkyard Special ")
  #50  
Old 01-17-2009, 01:35 PM
ajay ajay is offline
 
Join Date: May 2005
Posts: 88
Default Why not LGA or TEB?

Not to negate the pilot and crews fortune and professionalism, but 1549 reached a peak altitude of 3200 ft http://www.usatoday.com/news/nation/...h-hudson_N.htm
and it would have been closer to either return to La Guardia or take the 7000' 19 runway at Teterboro than ditch it where they did. I know everything is 20-20 in hindsight, but it will be interesting to see why these options weren't taken.

ajay
Closed Thread



Posting Rules
You may not post new threads
You may not post replies
You may not post attachments
You may not edit your posts

vB code is On
Smilies are On
[IMG] code is On
HTML code is Off
Forum Jump


All times are GMT -6. The time now is 10:57 AM.


The VAFForums come to you courtesy Delta Romeo, LLC. By viewing and participating in them you agree to build your plane using standardized methods and practices and to fly it safely and in accordance with the laws governing the country you are located in.