I don't know.  From what I have been learning about the 767, it seems they 
need a STANDBY ALTIMETER that has it's source from an area that is not 
subject to the Duct Tape,  somewhere out of the pressurized area, such as aft 
of the pressure dome.  
Then on the other hand,  a little training on how to fly the thing without 
the Flight Director, Auto Pilots, altitude select, altitude hold, Auto 
Throttles, and the rest of the GINGER BREAD would have saved their day.  The 
small amount of training could have been a little briefing on what to do, 
that's about all it would have taken.
From what I have been able to pick up from those who are qualified on the 
767, it seems it is very close to the 747-100/200 series,  which means in the 
same situation as AEROPERU,  if a person uses a power setting which is 
normally used for the maneuvering airspeeds in the terminal area which on the 
747 is to
Stand the power up to the mid position on the quadrant (that is if engine 
instruments are not available).  If the engine instruments are available it 
would be 1.07/1.11 EPR's on the 747 for power and for Pitch Attitude it would 
be a positive five degrees.
I would be interested in knowing what EPR'S it is on the 767 at max. gross 
landing wght. or the position of the power levers.  If a person knows the 
power and the Pitch Attitude for maneuvering it's a very comforting piece of 
knowledge to have stored away for just in case.
--- FLAME v1.1
---------------