What it approves
Removal of main landing gear doors, door actuators and switches, and installation of skin fairings, bulkhead, stiffeners and hydraulic line caps.
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.
flnited States of America Btpartmtnt of transportation— jfedtral Htoiation administration Supplemental ICgpe Certificate SA3722SW Proj. No. 190-537 MS-192 Valley Aero Inc.
Rt. 2, Box 407 Weslaco, Texas 78596 .<^ 3 ^'j&fy Civil Air 3A21^T*«.J.
Ooctgria 21QJ ana T210J Removal of main landing gear doors, door actuators and switches, and installation of skin fairings, bulkhead, stiffeners and hydraulic line caps in accordance with Valley Aero, Inc., STC Project No. SA 190-537 drawing list dated Novattoer 3, 1986, or later EAA revision.
The compatibility of this modification with other previously approved modifications is the responsibility of the installer.
;^ev<v?^ September 16, 1986 January 26, 1987 L. B.
Manager, Aircraft CJertification Division, Southwest Region (Title)
This certificate may be transferred in accordance with FAR 21 .47.
FAAFoiw 81 10-2 (10-68)
INSTRUCTIONS: The transfer endowment below may be used to notify the appropriate FAA Regional Office of the tranifer of thU Supplemental Type Certificate.
The FAA will reissue the certificate in the name of the transferee and forward it to him.
TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number to (Mame of transferee)———————————————————-——————— (Address of transferee) ———————,Ata*rW*.
(Address of grantor) Extent of Authority (if licensing agreement):
Signature of grantor (In ink):
y.Statt.fnJ^IP from (Name of grantor) (Print or type) ———————————— (Citf. Sun.
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.