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Originally posted by R_Mackey
Perhaps you've heard the old saying, "I've forgotten more than you've learned"? Perhaps not...
Originally posted by R_Mackey
Thanks for taking the time to look it up and referencing it properly!
Originally posted by R_Mackey
... I personally have no problem admitting when I'm wrong.
Originally posted by turbofan
Now that we're done with the semantics (hopefully) and construction basics
of aneroid devices, I'd be happy if someone would concede the '50 foot error'
nonsense of static port intergration to the vent of a pressure altimeter.
Originally posted by turbofan
I debate my own topics thank you.
Originally posted by turbofan
YOu can continue to go off topic with "R_Mackey" all you please, but perhaps via U2U, or another thread would be more acceptable.
Originally posted by turbofan
As for the length of static tube altering the pressure in the PA device:
Do you continue to stand by your previous statement, or would you like to rethink your position?
Originally posted by turbofan
... but perhaps via U2U ...
Originally posted by iSunTzu
Tree hit by a 483 KIAS Flight 77.
[atsimg]http://files.abovetopsecret.com/images/member/dee8f0261cd4.jpg[/atsimg]
Originally posted by tomk52To be exact, I didn't say the length "altered the static pressure". I said the length & diameter (& several other factors) introduced errors into the PA reading.
And I'm comfortable with that statement.
Do you claim that this statement is wrong?
Originally posted by tomk52
Not quite.
By adding piping "and stuff", the ERROR in the reading goes up by 50'.
Since the "and stuff" includes a bunch of stuff that is outside of the control of the altimeter manufacturer, including:
1. the length & diameter of the piping
2. the number of other systems that are accessing (read "changing") the static pressure
Originally posted by turbofan
Speaking of experts, there are quite a few of them at P4T that have
mile long resumes flying and dealing with the very systems and data
some of you are trying to wrap your head around.
I wonder why their verified work experience is always shunted by the
GL camp, and their names constantly attacked?
Originally posted by 911filesFirst, I am not a GL camper. But to answer your question, the 'experts' at P4T that I am aware of tend to view all evidence through the '911 was an inside job' prism. That is called bias, and most over there cannot look at the data without attempting to fit it into a particular theory.
Science works in the exact opposite manner.
Originally posted by tomk52
my social skills.... are non-existent.
Originally posted by turbofan
Originally posted by tomk52
Not quite.
By adding piping "and stuff", the ERROR in the reading goes up by 50'.
Since the "and stuff" includes a bunch of stuff that is outside of the control of the altimeter manufacturer, including:
1. the length & diameter of the piping
2. the number of other systems that are accessing (read "changing") the static pressure
Remainder truncated
Correction: you said the reading goes UP by 50 feet.
Patiently awaiting your clarifciation on this point alone.
Originally posted by tomk52Do you not understand the difference between "the reading" and "the error in a reading"? Even when I emphasize the difference by using BOLD CAPITAL LETTERS?
Reheat was explaining to you the difference between the FAA specs for the bench top altimeter and the installed altimeter system. There is an additional error allowance of 50'. (±70' vs ±20', IIRC)
The additional 50' error tolerance in the FAA specification is simply recognition of all the various sources of error that are lumped into the catch basket called "position error".
Can you name the FIVE types of errors associated with altimeters? That would be a good place to start. Tom
Originally posted by turbofan
You get ONE chance to get it right. THis will prove to everyone here
whether or not Reheat, or TomK can backup their talk.
Originally posted by R_Mackey
Based on data, the aircraft was traveling .70-.72 Mach. Mmo for a 757 is .86M. Well within the envelope of the aircraft with respect to compressibility issues which could affect the static system.
Originally posted by ImAPepper
I find this a bit disturbing, since you ... have failed to back up anything.
Step up and prove all the evidence false.
Originally posted by turbofan
Well then Reheat is wrong - again. I've already outlined and proven that
the FAA specification is a MINIMUM REQUIREMENT FOR INSTRUMENTS USED
IN PASSENGER CATEGORY AIRCRAFT.
Do you understand this?
FAA sets a spec. of +/- 75 feet for Pressure Altitude at a certain altitude.
Devices certified for the aircraft must MEET, or EXCEED this tolerance.
Originally posted by turbofan
The FAA specification has absolutely NOTHING to do with bench test vs.
installed system. NOTHING.
Originally posted by turbofan
Wrong! See above. See page 14. It is NOT an additional, "50 feet to allow
for various sources". It's +/- 75 feet to allow for various sources of error.
Period. Not to be debated.
Can you name the FIVE types of errors associated with altimeters? That would be a good place to start. Tom
Originally posted by turbofan
No I cannot. I do not work with altimeters. It's irrelevant to this discussion.
Originally posted by turbofan
If you feel the need to overstep the FAA and FAR regulations, please
show your sources and work.
Originally posted by turbofan
It's quite pathetic that we've already proven a list of theories from the
GL camp incorrect and now you're frontline spreading this disinformation.
It's quite pathetic that you're attempting to skew the information listed
on FAA.gov for all to clearly see.
Originally posted by turbofan
It's quite clear nobody here has a clue of how the PA system functions,
nor the connections.
Originally posted by Reheat
Originally posted by turbofan
The FAA specification has absolutely NOTHING to do with bench test vs.
installed system. NOTHING.
Prove it Einstein.
Says the googleologist without a clue. Isn't this what we've been saying from day one to refute your bench test tolerance of +- 20'?
It's obvious that you don't work with them. How did you get so smart?