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NOTICE
Weight and balance or operating /1mitat,on changes shall be entered in the r1ppropnate aircraft record. An alteration must be
compatible with all previous alterations to assure cantmu~d conformity with the appl,cable a,rworthiness requ,rements.
8. Description of Work Accomplished
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requtred. attach add,t,onal sheets. ldenr,r; .•,-th a,rcrafl nat1onal1ty and reg,str..11,on mark and date worJ.: completed.,
A.)
Removed the following:
1.)
Piper upper cabin door strut PIN 980162-502 and baggage door
strut PIN 585-231. Units are used to hold doors in open position.
B.)
Installed the following:
1.)
Suspa, Inc. cabin door strut PIN 820162-502-SK.
2.)
Suspa, Inc. baggage door strut PIN 585-231-SK.
3.)
Suspa, Inc. gas cylinders are manufactured to some weight and
outside dimensions as original units supplied by Piper.
4.)
Suspa, Inc. gas cylinders are attached to aircraft and doors in same
configuration as original units.
C.)
No Weight and Balance change.
D.)
Installed I.A.W. FAA Field Approvals dated 9/7/95 (see attached 337's)
................................................................... END ....................................................... .
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Add1t;onal ShP.ets Are Attached
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,'.;.:)VERNME'lT PRINTING OFFICE: 1992-769-012.'60157