What it approves
Installation of a Sandel SA4550 Electronic Attitude Display Indicator and a Bendix Vertical Gyro for the copilot use with the existing FGS-70 Flight Director and Autopilot. Airplane Flight Manual Supplement, document number JTECH-FGS70-0102, revision IR, dated February 10, 2011, or later approved FAA revision, is required.
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 a Sandel SA4550 Electronic Attitude Display Indicator and a Bendix Vertical Gyro for the copilot use with the existing FGS-70 Flight Director and Autopilot. Airplane Flight Manual Supplement, document number JTECH-FGS70-0102, revision IR, dated February 10, 2011, or later approved FAA revision, is required.
Limitations and Conditions: This approval is limited to only the installation made in Citation 500 Serial No. 500- 0001 through 500-0274 equipped with FGS-70 AFCS. 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: October 27, 2008
Date of issuance: February 11, 2011
( Signature) S. Frances Cox Manager, Special Certification Office Southwest Region
( Title)
FAA Form 8110-2-1(10-69) Page 2 of 3
FAA Form 8110-2-1(10-69) Page 3 of 3
Number ST11042SC Date of Issuance: February 11, 2011
Certification Basis: Based on 14 CFR §§ 21.115 and 21.101, and FAA policy for significant changes in FAA Order 8110.48, the certification basis for the Citation 500 Copilot Primary Attitude Display System is as follows:
a. The type certification basis for Citation 500 series airplanes is shown on TCDS A22CE for parts not changed or not affected by the change.
b. The certification basis for parts changed or affected by the change since the reference date of applications, October 27, 2008, is based upon part 25 as amended by Amendment 25-129.
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 modification was determined to be:
Regulations at the latest amendment 25-0 through 25-129 14 CFR §§ 25.1, 25.21(a), 25.29, 25.301, 25.303. 25.305(a-c), 25.307(a), 25.561, 25.601, 25.603, 25.605(a), 25.609(a),
25.613(a-c), 25.619, 25.625,25.771(a,e), 25.777(a-c), 25.789(a), 25.869(a4), 25.1303(b4-b5), 25.1307(c), 25.1316,
25.1317, 25.1321(a,b,d,e), 25.1331, 25.1333, 25.1351(a,d), 25.1381, 25.1431(a,c,d), 25.1501, 25.1525, 25.1529,
25.1541, 25.1543(b), 25.1555(a), 25.1581, 25.1585(a,b), 25 Appendix F(25.1), 25 Appendix H(25.1-25.3), 25 Appendix L(25.1).
Regulations at an intermediate amendment 14 CFR § 25.611, Amendment 25-23; 25.981(a,b), Amendment 102; 25.1301, No Amendment; 25.1309, Amendment 25-41; 25.1322, Amendment 25-38; 25.1353(a,b,d), Amendment 25-113; 25.1357(a-e), No Amendment; 25.1583(e), Amendment 25-105; 25.Appendix F, Amendment 25-111; 25.Appendix H(25.4), Amendment 25-102.
Regulations at the amendment level in TCDS A22CE None
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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 |