# STC ST11147SC - Type: Supplemental type certificate - Status: Current, Issued - Holder: COMTECH Aviation Services Inc. - Description: Installation of interior components - Status date: August 12, 2013 - Data sheets: A43NM, A43NM, A43NM - Certificate PDF: https://openairdocs.org/files/sha256/eb/a2/eba2811c33105ad50ededb16d5eed42350008d73d06a002e32b9e8218466d7dc - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/A43952C202D8936D86257BCC0048CD28.0001 - Page: https://openairdocs.org/stc/ST11147SC ## ADs that name it None. ## Approved models (3) - Airbus A340-311 (TCDS A43NM) - Airbus A340-312 (TCDS A43NM) - Airbus A340-313 (TCDS A43NM) ## What the certificate says Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can differ. The PDF is the record. United States of America Department of Transportation - Federal Aviation Administration Supplemental Type Certificate Project Number ST09536SC-T JPC N umber: ST11147SC This certificate issued to Comtech Aviation Services, Inc. 401 Marseille Drive Hurst, Texas 76054 Part 25 of the Federal Aviation R egulations. Original Product Type Certific ate N umber : A43NM M ake : AIRBUS M odel : A340-300 Series: Models: A340-311, -312, -313 Description of Type Design Change: Installation of interior components in accordance with Comtech Aviation Services, Inc. Drawing List CTDL01009, Revision C, dated June 12, 2013, or later Federal Aviation Administration (FAA) approved revisions. Airplane Flight Manual Supplement document number CTAFMS01009, Revision NC, dated August 12, 2013 or later FAA approved revisions. Instructions for Continued Airworthiness (ICA) document number CTICA01009, Revision D, dated April 30, 2012 or later FAA approved revisions. 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. Date of application: May 31, 2011 Date reissued: Date of issuance: August 12, 2013 Date amended: B y direction of the A dministrator (Signature) S. Frances Cox Manager, Special Certification Office Southwest Region (Title) FAA FORM 8110-2-1(10-69) PAGE 2 of 3 PAGES 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) Signature of grantor (In ink): FAA FORM 8110-2-1(10-69) PAGE 3 of 3 PAGES United States of America Department of Transportation - Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) N umber ST11147SC Date of Issuance: August 12, 2013 Certification B asis: Based on 14 CFR §§21.115 and 21.101(b)(1), and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for AIRBUS A340-300 Series aircraft with the installation of a cabin interior is as follows: The type certificate basis for AIRBUS A340-300 Series airplanes is shown on TCDS A43NM for parts not changed or not affected by this change. The type certification basis for parts changed or affected by this change since the reference date of application, May 31, 2011, is based upon part 25 as stated by amendment levels below for each section. Based on 14 CFR §§21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis was determined to be: as shown in TCDS A43NM. Regulations at a later amendment than specified in A43NM 25.791(a)(b) Amdt. 25-72; 25.851(a)(1) Amdt. 25-74; 25.853 (a)(c) Amdt. 25-116; 25.869 (a)(4) Amdt. 25-113; 25.899 Amdt. 25-123; 25-981 (a)(b) Amdt. 25-125; 25.1301 (a)(1)(2)(3)(4) Amdt. 25-123; 25.1309 (a)(b)(d)(e) Amdt. 25-123; 25.1310 Amdt. 25-123; 25.1351 (a)(d) Amdt. 25-72; 25.1357 (a)(b)(c) Amdt. 25.123; 25.1360 Amdt. 25.123; 25.1423 (c) Amdt. 25-115; 25.1431 (a)(c)(d) Amdt. 25-113; 25.1581 Amdt. 25-72; 25-1583 (h) Amdt. 25-130; 25.1729 Amdt. 25-123 26.11 (c) Amdt. 26-10; and 26.47 Amdt. 26-1 --END-- ## Every issue (1) - August 12, 2013: Issued, Current. [certificate](https://openairdocs.org/files/sha256/eb/a2/eba2811c33105ad50ededb16d5eed42350008d73d06a002e32b9e8218466d7dc) --- From OpenAirDocs.org, an independent open copy of FAA data. Only the Federal Register edition on govinfo.gov is the official legal text of an AD.