Because this photo has alot of writing on it, and for some reason my scanner only picked up the color portions and made the white transparent, I created a seperate page and retyped the writing so that you could read it. The top portion reads:

Pratt & Whitney
High Pressure Turbopumps
Line Replaceable Units for the Space Shuttle Main Engine

Then there is the picture of the engine.
The next portion is seperated into two columns, I will begin with the left-side column.

Fule Turbopump
Propellant: Liquid Hydrogen
Speed: 36,300 rpm
Discharge Pressure (max): 6,690 psi
Flow: 162 lb/sec (14,700 gpm)
Shaft Horsepower: 73,300 hp
Turbine Inlet Temperature: 1,860°R
Design Life Between Overhaul: 55 Missions/7.5 hr.

And now the right-side column.
Oxidizer Turbopump
Propellent: Liquid Oxygen
Speed: 24,000
Discharge Pressure (max): 7,650 psi
Flow: 1,16 lb/sec (7,400 gpm)
Shaft Horsepower: 26,100 hp
Turbine Inlet Temperature: 1,500°R
Design Life Between Overhaul: 55 Missions/7.5 hr.