What it approves
Modify Beechcraft C18 cowl to fit Grumman G-21A.
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 $tatu of arnica Btpartment of '^transportation—federal 2toiation Administration Supplemental ICgpe Certificate SA551SW Pan Air Corporation P. 0. Box 26425 New Orleans, Louisiana 70126 v^wJ^wdeAjjctM^^ Jte.fi/6oijsirwfiwc£u4>6 Aero Bulletin 7A %<H^M wsjMSK?ft^fi& <S'gBiii0i I -<^jA* Bureau of Air Commercei <-%/ / f-I iSleaMlatt&nA/.1 17 ^ ._ ^^ Grunman G21A Modify Beechcraft C-18 cowl to fit Grunman G21A per Pan Air Corporation Drawings EL-0104 dated 5/7/65, EL-0104-1 dated 6/15/65, EL-0104-2 dated 6/15/65.
Compatibility of this modification with other previously approved modifications must be determined by the installer.
FAA Approved Airplane Flight Manual Supplement dated November 30, 1978, is required.
^ May 7, 1965 ^"& ^^««/ November 30, 1978 Revision 1 AUKUSt 31. 1965 -J ate Mtristu/u/ (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 |
|---|---|---|
| Grumman American Aviation Corporation | G-21A (Army OA-9; Navy JRF-1; -2; -3; -4; -5; and -6B) | TC 654 |