What it approves
Installation of the Bendix/King KGP 860 GA-EGPWS as a Class B TAWS.
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.
23500 W. 105th Street Olathe, KS 66061
certifies that the change in the type desi gn for the followin g product with the limitation s and conditions therefor as sp ecified hereon meets the airworthi ness requirements of Part 23* of the Federal Aviation Regulations
Original Product- -Type Certificate Number : A24CE Raytheon Make :
200, B200 & 300 Model :
Description of Type DesignChange:
Installation of the Bendix/King KGP 860 GA-EGPWS as a Class B TAWS.
REQUIRED DATA: 1. Master Drawing List 159-08300-0001, Revision A, dated 7-11-2003; 2. Airplane Flight Manual Supplem ent 006-10314-0000, Revision -, dated 8-21-2003. Later FAA approved revisions to the above listed data are incorporated without further revision to this Supplemental Type Certificate.
1. The installation should not be incorporated in any aircraft unless it is determ ined that the interrelationship between this installation and any previously approved configuration will not introduce any adverse effect upon the airworthiness of the aircraft.
2. If the holder agrees to perm it another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission.
This certificate and the supporting data which is the basis for a pproval shall remain in effect until surrendered, suspended, r evoked or a termination date is otherwise established by the Administrator of the Federal Aviation Administration.
( Signature) Robert G. Murray DAS Administrator, DAS-500863-CE
(Title) Date of application : 6-16-2003
Date of issuance : 8-21-2003
INSTRUCTIONS: The transfer endorsem ent below m ay be used to notify the appropriate FAA Regional Office of the transfer of the 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 (Name of transferee) (Address of transferee) (Number and street)
(City, State, and ZIP code) from (Name of grantor) (Print or type) (Address of grantor) (Number and street)
(City, State, and ZIP code) Extent of Authority (if licensing agreement):
Signature of grantor (In ink):
,U.S.G.P.O: 1989-662-030
FAA FORM 8110-2-1(10-69) PAGE 3 of 3 PAGES
Number SA01190WI-D *Certification Basis:
Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for this change is as follows:
a. The certification basis for parts not changed or not affected by this change is shown on TCDS A24CE.
b. The certification basis for parts changed or affected by this change since the date of application is determined to be:
Regulations at the latest amendment Section Section Amdt. Amdt.
23.301 All 23-48
23.303 23-0
23.305 23-45
23.307 23-0
23.365 23-0
23.561 e 23-48
23.571 a 23-48
23.603 All 23-23
23.605 a 23-23
23.607 b 23-48
23.609 All 23-0
23.613 All 23-45
23.627 23-0
23.1301 All 23-20
23.1309 a(1)(3), b 23-49
23.1321 a, c, e 23-49
23.1322 All 23-43
23.1331 a 23-43
23.1351 a, b 23-49 23-1357 All 23-43
23.1365 a, b, d, e 23-49
23.1367 23-0
23.1381 23-0
23.1431 a, b, e 23-49
23.1501 23-21
23.1529 23-26
23.1541 a2, b 23-21 Regulations at an intermediate amendment none Regulations at the amendment level shown on TCDS none
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.