LOW PRESSURE TURBINE (LPT) SECTION - ADJUSTMENT/TEST
1. General
A. This procedure is only used if the Trim Balance Procedure in the Fan and Low Pressure
Compressor Section - Adjustment Test (PAGEBLOCK 72-31-00/201) does not satisfactorily balance
the engine.
TASK 72-52-00-705-060-G00
2. LPT Trim Balance Procedure
A. General
(1) The terms and symbols used in this procedure are specified as follows:
(a) Vibration Amplitude (U) - The engine imbalance as measured by the No. 1 bearing
accelerometer and shown on the trim balance analyzer, in units of mils.
(b) Phase angle (A) - The phase angle of the engine imbalance as shown on the trim
balance analyzer in units of degrees.
(c) Weight (W1, W2, W3, etc.) - A balance correction weight in gram-inches. It is a balance
clip (or clips) which are installed on the low pressure turbine (LPT) blades.
(d) R - The resultant imbalance (in units of mils) because of the correction weight (W).
B. References
Reference Title
71-00-00 P/B 201 POWER PLANT (OPERATING PROCEDURES) -
MAINTENANCE PRACTICES
71-11-04 P/B 201 FAN COWL PANELS - MAINTENANCE PRACTICES
(OPEN/CLOSE)
71-11-06 P/B 201 CORE COWL PANELS - MAINTENANCE PRACTICES
(OPENING/CLOSING)
72-00-00 P/B 601 ENGINE - INSPECTION/CHECK
78-31-00 P/B 201 THRUST REVERSER SYSTEM - MAINTENANCE PRACTICES
C. Tools/Equipment
NOTE: When more than one tool part number is listed under the same "Reference" number, the
tools shown are alternates to each other within the same airplane series. Tool part numbers
that are replaced or non-procurable are preceded by "Opt:", which stands for Optional.
Reference Description
COM-3932 System - Portable Engine Balancing
767-200
Part #: PBS-4100 Supplier: 26741
SPL-5659 Kit - Fan Trim Balance
767-200
Part #: 2C14963G06 Supplier: 06083
Part #: PBS-4100 Supplier: 26741
SPL-13247 Tool - LPT Balance Clip Installation
767-200
Part #: 2C14798G02 Supplier: 06083
STD-600
Mirror - Inspection
767
AIRCRAFT MAINTENANCE MANUAL
CF6-80A SERIES ENGINES
72-52-00
NoC
Page 501
D633T1B7 Dec 22/2016
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