What it approves
Installation of weight on top rib of vertical fin
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.
United States of amtrica Bepartment of transportation— federal 2tt>iation administration Supplemental 'Cgpe Certificate Project H5261SW-DS SH4446SW TAD- 212 Agusta Aviation Corporation One West Loop South Suite 600 Houston, Texas 77027 JfaJufi&sCtedj:^^
21.29/3^^*' Federal Aviation *-/t&2Mt&&Wl&.
H7EU Agusta A109A Installation of weight on top rift of vertical fin according to Drawing 109-4200-67, Rev. B, dated 8/13/81, or later FAA approved revision.
Compatibility of this modification with other previously approved modifications must be determined by the installer.
<J%^^*!7<<^&i*2^_*fc7Z<2^^4<^^W£>^x^^ S$drriim4&foa£>v-J^£ 1 Q 1 Qft 1 AugUSt 18, 1981 ^Signature) Don P. Watson Chief, Engineering and Manufacturing Branch
FAA FOUM 8110-2 (10-68)
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.
Approved models · 1
| Make | Model | Data sheet |
|---|---|---|
| Agusta S.p.A. | A109A | H7EU |