What it approves
Install Dual Collins FD-108 flight director system replacing Collins ID -105 Flight Director System having dual instrumentation with single steering computer
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.
ftirittd States of america Bepartmcnt of transportation— Jp'ederal 3toiation administration Supplemental t^uje Certificate BA4208W Braniff Airways, Inc. Pmipot vi64osw-SP. 0. BOX 35001 rrojecT, AJ.OHUDW o Dallas, Texas 75235 .1!^^^^1^^ 4b ^^iv CiVll Air iSltau£a/tvnfr.
4A21 and 4A28 : Boeing : 707-227, 720-027, 707-1388 Install dual coning JD-108 Flight Director System replacing Collins ID -105 Flight Director System having dual instrumentation with single steering computer according to Braniff Airways Engineering Change Release 15-6U dated 7/28/6U with Addenda 1 dated 8/6/6U, 2 dated 9/1/6U and 3 dated 9/3/6>j or replacing Bendix 300 Series according to EA Ho. 8-31-21, Rev. 1 dated 6/24/69, EA Ho. 8-31-218, Rev. 1 dated 6/2W69, SA Ho. 8-3^-6l, Rev. 1 dated 6/2U/69, EA Ho. 8-34-81 Section A dated 12/19/69, EA Ho. 8-3^-81 Section B dated 3/26/70.
1. FAA Approved Airplane Flight Manual Supplemental Revision Ho. 19 dated 10/20/64 required for Boeing 707-227"
2. FAA Approved Airplane Flight Manual Supplemental Revision Ho. 6 dated 9/16/64 required for Boeing 720-027*3. FAA Approved Airplane Flight Manual Supplemental Revision Ho. 1 dated 6/26/69 required for Boeing 707-138B.4. This equipment has not been evaluated for Category II performance.
ri& /w. August 13* 1964 £/•<,&.*,*&«,</: June 26, 1969 Revision 116, 1964 ^/a£e-atn*tu/t</:
(Signature) len V. Welsh Chief. Engineering and Manufacturing Branch(Title) ___
FAA Fout 81 10-2 (10-68)
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.