ALLOWS THE SECOND STAGE TURBINE ROTOR ASSEMBLY TO BE MOVED WITHOUT DAMAGE TO THE TURBINE BLADES
FCLS
FUNCTIONAL CLASSIFICATION
HH-1.1
FTLD
FUNCTIONAL DESCRIPTION
ALLOWS THE SECOND STAGE TURBINE ROTOR ASSEMBLY TO BE MOVED WITHOUT DAMAGE TO THE TURBINE BLADES
ALBY
USAGE DESIGN
AIRCRAFT ENGINE
ABHP
OVERALL LENGTH
34.600 INCHES NOMINAL
MATT
MATERIAL
ALUMINUM ALLOY
AMSZ
WARNING STREAMER
NOT INCLUDED
FCLS
III FUNCTIONAL CLASSIFICATION
HH-1.1
FEAT
SPECIAL FEATURES
"C/O A SPLIT, CIRCULAR RING WHOSE INSIDE DIAMETER IS MACHINED INTO A ""U""CHANNEL, LINED WITH NEOPRENE. THE CHANNEL FITS OVER AND PROTECTS THE TURBINEBLADES FROM DAMAGE. A FIXED HINGE JOINS THE TWO HALVES AT ONE END. A HAND KNOB ASSY CLOSES THE RING AT THE OTHER END. TWO TRUNNION SPOOLS ARE LOCATED ONEACH HALF-RING."