Generator Set, volume 2. These procedures provide
detailed engine and interference removal instructions.
These instructions should be strictly followed due to the
vast differences in removal procedures between a
propulsion GTE and an SSGTG.
You must use the same planning skills and
engineering practices in a GTG engine changeout as you
use in an LM2500 GTE changeout. The same strict
application of safety precautions and following of
technical manual procedures apply to every GTG engine
changeout.
COOPERATION
Ships readiness is the common purpose in the
changeout evolution.
All personnel involved should
share a common commitment in achieving that purpose.
A willingness by each individual to submerge his or her
personal interest in favor of getting the job done is a
necessary prerequisite to cooperation. You may have to
adjust working hours and watch-standing duties to meet
changeout schedule requirements. Personnel may be
assigned to duties they do not want to perform.
Emphasize each individuals importance, willingness,
and contribution to the evolution. Engine changeout is
an opportunist y to display your professional abilities as
a leader and technician
MAINTENANCE TIPS
As a GS supervisor you will be responsible for the
proper completion of most maintenance procedures.
This section will cover some maintenance tips that can
help you to understand the critical relationship between
maintenance performance and the proper operation of
the LM2500. Remember, the contents of this section are
FOR TRAINING PURPOSES ONLY and should in
no way replace the use of the PMS or the manufacturers
maintenance procedures.
PLA RIGGING
If the PLA is replaced for whatever cause, the PLA
rig check (mechanical and electrical) must be
accomplished. If the main fuel control (MFC) rig pin
does not fit properly (too loose, too tight, or cant be
fully inserted), re-rig the PLA. Always comply with the
PLA electrical rig check after you are assured that the
throttle command voltages are properly set (idle and full
throttle).
Mechanical
The key to a successful mechanical rigging is a
proper alignment.
Remember, although the PLA
actuator arm is mechanically linked to the MFC lever
arm, the PLA is electrically driven. The slightest
mechanical restriction (binding) may cause incorrect
PLA movement during engine operation. PLA
movement is most sensitive to a restriction when in
either engine speed or torque, and/or shaft torque
limiting condition. If a possible restriction is suspected,
advance and retard the PLA electrically and check for
any hesitation or jerking during travel. If hesitation
exists, there may be a mechanical restriction.
Electrical
The normal process for this rigging will be checking
dc voltages at idle and full throttle positions. However,
the moment the throttle is moved out of idle, indicated
torque will go to midrange and oscillate. For example,
on the DD-963/DDG-993 class ships, if mid-torque
oscillations are accompanied by an overtorque
indication and a PLA failure indication, then another
problem exists.
Why? When the PLA is at idle, there is a PT5.4 bias
that assures PT5.4 is greater than PT2 for engine start
purposes. During PLA electrical rigging, the bias drops
out when the throttle is advanced.
If PT5.4 is several tenths of a pound less than PT2,
the torque computer goes berserk. But, PLA rigging
may be continued by pressing the BATTLE
OVERRIDE button.
However, suppose you have just been informed that
the PT5.4 transducer requires calibration When the
torque goes berserk as described, immediately dial up
P T5.4 and PT2 on the respective DDIs. PT5.4 will be
lower than PT2, thus requiring the activation of
BATTLE OVERRIDE to continue. This lower reading
tells you the PT5.4 transducer requires calibration.
VSV FEEDBACK CABLE RIGGING
Why is it accomplished? Why is it important?
VSV feedback cable rigging is necessary because
we are timing a pilot valve inside the MFC so the
correct vane angle is obtained for a given CIT/gas
generator speed day. Actually, we are assuring that the
pilot valve is timed to close off high pressure fuel flow
to both the ROD END and the HEAD END pressure
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