What it approves
Installation of SANDEL SA4550 Primary Attitude Display, SN4500 Primary Navigation Displays and associated equipment into a Cessna 500 aircraft to obtain WAAS approval for a GARMIN GNS-400W/500W Global Navigation System with an FGS-70 Automatic Flight Control System. Equipment Installations
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.
Part 25 of the Federal Aviation Regulations.
Description of Type Design Change: Installation of SANDEL SA4550 Primary Attitude Display, SN4500 Primary Navigation Displays and associated equipment into a Cessna 500 aircraft to obtain WAAS approval for a GARMIN GNS-400W/500W Global Navigation System with an FGS-70 Automatic Flight Control System. Equipment Installations are in accordance with Master Document List JTECH-FGS70-0001, Revision B, dated March 2, 2009 or later FAA approved revision.
Limitations and Conditions: The installer must determine whether this design change is compatible with previously approved modifications. If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission.
JETTECH, LLC 10116 Maypole Court Oklahoma City, OK 73159 A22CE Make : Cessna Aircraft Company Model : 500 Date of application : February 22, 2008
Date of issuance : May 26, 2009
( Signature) Gary A. Sharon Acting Manager, Special Certification Office Southwest Region
( Title)
FAA Form 8110-2-1(10-69) Page 2 of 4
FAA Form 8110-2-1(10-69) Page 3 of 4
Number ST10945SC Date of Issuance: May 26, 2009
Description of Type Design Change (Continued):
Airplane Flight Manual Supplement JTECH-FGS70-0002, Revision IR, dated May 26, 2009 is required for the SA4550 Primary Attitude Display only.
Airplane Flight Manual Supplement JTECH-FGS70-0002A, Revision IR, dated May 26, 2009 is required for the SN4500 Primary Navigation Displays only.
Airplane Flight Manual Supplement JTECH-FGS70-0002B, Revision IR, dated May 26, 2009 is required for the SA4550 Primary Attitude Display, SN4500 Primary Navigation Displays and associated equipment to obtain WAAS approval for a GARMIN GNS-400W/500W series Global Navigation System with an FGS-70 Automatic Flight Control System.
Certification Basis: Compliance with the following requirements, in addition to the requirements shown on Type Certificate Data Sheet A22CE, Revision 64 has been shown:
25.21(a), (b-g), Amendment 25-121
25.29, Amendment 25-72
25.301, Amendment 25-23
25.303, Amendment 25-23
25.305 (a-c), (e&f) Amendment 25-86
25.307 (a), Amendment 25-72
25.561, Amendment 25-91
25.603, Amendment 25-46
25.605 (a), Amendment 25-46
25.611, Amendment 25-23
25.613 (a-c), Amendment 25-112
25.619, Amendment 25-23
25.625, Amendment 25-72
25.777 (a-c), Amendment 25-46
25.789 (a), Amendment 25-46
25.869(a), (4), Amendment 25-113
25.981(a, b), Amendment 25-102
25.1117, Amendment 25-122
25.1303 (b4, b5, b6), Amendment 25-90
25.1307 (b, c, d, e), Amendment 25-72
25.1309, Amendment 25-41
25.1316, Amendment 25-80
25.1317, Amendment 25-122
25.1321(a, b, d, e), Amendment 25-41
25.1322, Amendment 25-38
25.1329 (i), Amendment 25-46
25.1331, Amendment 25-41 Number ST10945SC
FAA Form 8110-2-1(10-69) Page 4 of 4
Date of Issuance: May 26, 2009
Certification Basis (Continued):
25.1333, Amendment 25-41
25.1335, Amendment 25-41
25.1351 (a, d), Amendment 25-72
25.1353 (a, b, d), Amendment 25-113
25.1357(a b, c, d. e),
25.1381, Amendment 25-72
25.1431 (a, c, d), Amendment 25-113
25.1501, Amendment 25-42
25.1529, Amendment 25-54
25.1543 (b), Amendment 25-72
25.1581, Amendment 25-72
25.1583 (a&b, e), Amendment 25-105
25.1529, Amendment 25-54
Also Part 25 Appendices Appendix H (25.4), 25.1529, Amendment 25-102 Appendix L, Amendment 25-122
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 |
|---|---|---|
| Cessna Aircraft Company | 500 | A22CE |