NOTICE
Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be
compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements.
8. Description of Work Accomplished'
(If more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.)
COMPONENT TOTAL TIME 270.6 TSO 48.1
Component disassembled and inspected IAW CH67-31-06 HR Textron Component
Maintenance Manual p/n 41000470, Rev 3, dated May 15/96, page 50, para 2A.
Spool/Sleeve By Pass Assembly p/n 41005497-10 and Piston Assembly p/n
RW41000143 replaced at this time. Minor repairs to actuator carried
out IAW Maintenance Manual page 601, para 2A.
Component re-assembled and tested IAW Maintenance Manual Assembly
Instructions beginning page 701, para 1, para 3, para 4, para 5 (5),
( 6) and ( 8).
Final functional test carried out IAW Maintenance Manual Testing
Instructions beginning page 101, para 2.
HR Textron ASB 41000470-67-01 complied with this time.
- - - - - - - - - - - - - - - - -END- - - - - - - - - - - - - - - - -
D Additional Sheets Are Attached
*U.S. GOVERNMENT PRINTING OFFICE: 1992-769-012/60157
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