What it approves
Addition of Hydro Seal Fluid Additive to the landing gear shock struts.
What the certificate says
From the PDF’s text layer, without the form’s printed wording. Layout and order may differ; the PDF is the record.
Duplicate copy issued on July 23, 2002 Untert £tatu of arertca Btpartmtnt of transportation --Jedera! Station SWministradon Supplemental t^pe Certificate SA2946SW Grsmrllle Lasseter d/b/a Granvllle's Aircraft Strut Sealant 802 E. Grant Morton, Texas 79346 aM 23 A7SO Federal Aviation ..$<M PA-32-260, PA-32-300, PA-32R-300, PA-32RT-300T, PA-32RT-300 . Addition of Hydro Seal Fluid Additive to the landing gear shock struts according to specifications dated 12/26/76, or later FAA approved revision.
Compatibility of this modification with other previously approved modifications must be determined by the installer.
j^^ -!& january 15, 1979 March 2l 1979 August 8, 1980 Revision 1 Origlrl Signed J. J. Shapley (Signafuif) Don P. Watson Chief, Engineering and Manufacturing Branch
This crrtiftcatf may be trtinsjerrtd ^n afcordanct with FAR 21.47.
FAA Fo» 81 10-3 {10-6B|
TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number_ to (Name of transferee) (Address of transferee) and street) (City, State, and ZIP code) from (Name of grantor) (Print or type) (Address of grantor) (Number £ street) {City, State, and ZIP code) Extent of Authority (if licensing agreement):
Signature of grantor (In ink) :
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.