What it approves
Installation of dual Garmin GTX 330D Mode S Transponders
What the certificate saysOCR
This is OCR from the scanned FAA certificate. OCR can misread letters and numbers.
United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA01512WI-D This certificate issued to: Garmin International, Inc.
1200 East 151$ Street Olathe, KS 66062 Certifies that the change in the type design for the following product with the limitations and condition's therefore as specified hereon meets the airverthiness requirement's of Part 23* of the Federal Aviation Poegulations.
Original Product - Type Certificate Number: A37CE Make: Cessna Model: 208, 208B Description of Type Design Change:
Installation of dual Garmin GTX 330D Mode S Transponders.
Data Required:
Garmin Master Drawing List (MDL) 005-00521-01, Revision 1, Dated November 13, 2008 or later FAA-approved revision.
1. Compatibility of this design change with previously approved modifications must be determined by the installer.
2. Installation of STC SA01712SE is a prior or concurrent requirement.
3. Aircraft equipped with Garmin G1000 Integrated Cockpit System are not eligible for this STC.
4. Aircraft modified by this STC shall be maintained in accordance with the Instructions for Continued Airworthiness identified by the MDL.
5. 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.
suspended, revoked or a ternination date is otherwise established by the Administrator of the Federal Aviation Administration.
Date of Application: June 5, 2008 Date Reissued:
Date of Issuance: November 13, 2008 Date Amended:
FEDERAL AVIATION Robert Murray Lead DAS Administrator TOMINISTRATOS DAS-240087-CE Garmin International, Inc (Title)
Transfer the ownership of Supplement Type Certificate Number To (Name of transferee) (Number and street) (City, State and Bip code) From (Name of granter) Print or type (Address of granter) (Number and street) City, Plate and Zip code) Extent of Authority (if licensing agreement):
Signature of grantor (In Ink):
United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA01512WI-D Date of Issuance: November 13, 2008 *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 the TCDS listed on Page 1 of this Certificate.
b. The certification basis for parts changed or affected by this change since the date of application is determined to be:
Section Amdt. Section Amdt.
23.251 Orig. 23.773(a)(1)(2) 23-45
23.301(a) 23-48 23.777(a)(b) 23-51
23.303 Orig. 23.867 23-49
23.305 23-45 23.1301 23-20
23.307(a) Orig. 23.1309(a)(1)(2)(b)(c)(d)(e) 23-49
23.561(e) 23-48 23.1311(a)(2) 23-49
23.601 Orig. 23.1351(a)(g) 23-49
23.603 23-23 23.1353(h) 23-49
23.605(a) 23-23 23.1357(a)(b)(c)(d) 23-43
23.607(a)(b) 23-48 23.1359 23-49
23.609 Orig. 23.1365(a)(b)(d)(e) 23-49
23.611 23-48 23.1431(a)(b)(e) 23-49
23.613(a)(b)(c) 23-45 23.1529 23-26
23.627 Orig. 23.1555(a)(b) 23-50
23.771(a) 23-14 -END
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.