What it approves
Modification of fuselage chin fairing to provide service and inspection access doors.
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.
^ntteb ^tates <©f America
•pbpartrtumt nf tEransporiattmt - Jjfeberal ^frtatton <Aommtstrai:t0tt Qlsrttftcate SA5894SW Gulfstream Aerospace Corporation 7440 Aviation Place Dallas, TX 75235 Federal Aviation A2 1EA Canadair CL-600-1A11, CL-600-2A12, CL-600-2B16 Modification of fuselage chin fairing to provide service and inspection access doors in accordance with K-C Aviation Drawing No. 444-0583 dated February 6, 1985, or later FAA approved revision.
Compatibility of this modification with other previously approved modifications must be determined by the installer.
.• February 12, 1985 March 01, 1985 . April 1, 1999 . October 7, 1987 Rev. 1 (Signature) ) S. Ytahice^r Cox, Manager Special Certification Office, Southwest Region (Titk)———————— Any aJteration of t/iis certificate is punishable by a fine o/ not exceeding $1,000, or imprisonment not exceeding 3 years, or both.
1 e FAA Kegion.l Office of the tranifer of ihU Supplemental Type Certificate.
The FAA will reiwuc the certificacc in the name of the transferee and forward il lo h.m.
TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number to (Name of transferee).
(Address of transferee). ( .Vtimter (City. SMe. «*/ ZI from (Name of grantor) (Print or type).
(Address of grantor) 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.