# STC ST10396SC - Type: Supplemental type certificate - Status: Current, Issued - Holder: Boeing Company - Description: Installation of Phase II Global Air Traffic Management (GATM) System (Honeywell Communication Management System with Aircraft Communication Addressing and Reporting System, VHF Data Link System, Cockpit Thermal Printer, Selcal Decoder System, and Update the Flight Interphone System) for models 747-E4A and 747-E4B. - Status date: August 23, 2005 - Data sheets: A20WE - Certificate PDF: https://openairdocs.org/files/sha256/fa/68/fa68376dddeeff11299e183398fb9c2e210fbef83f150f5443c416f2a6e8249c - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/67A40654FE89A0198625707400621E6F.0001 - Page: https://openairdocs.org/stc/ST10396SC ## ADs that name it None. ## Approved models (1) - The Boeing Company 747-100 Series (TCDS A20WE) ## 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 No. ST6751SC-T KSC FAA Form 8110-2(10-68) Page 1 of 2 Number ST10396SC This Certificate issued to Boeing Wichita Maintenance & Mod. Center 3801 S. Oliver Building 200X, M/S K86-74 Wichita, KS 67210 Part 25 of the Federal Aviation Regulations. Original Product Type Certificate Number : A20WE Make : The Boeing Company Model : 747-E4A, 747-E4B Description of Type Design Change: sin accordance with Boeing Master Drawing List D226-38759-1, Revision G, dated April 22, 2005, or later FAA approved revision. Airplane Flight Manual Supplement D226-38931-1, dated April 21, 2005, or later FAA approved revision, is required. Date of application : June 18, 2001 Date of issuance : August 23, 2005 Date reissued : ( Signature) Fred Stellar Acting Manager, Special Certification Office Southwest Region (Title) FAA Form 8110-2-1(10-69) Page 2 of 2 Number ST10396SC Date of Issuance: August 23, 2005 1. This approval should not be incorporated in any aircra ft of this model on which other approved modifications are incorporated, unless it is determined that the interrelationship between this change and any of those previously incorporated approved modifications will not introduce any adverse effect upon the airworthiness of the aircraft. 2. If the holder agrees to permit another pe rson to use this Certificate to alter the product, the holder shall give the other person written evidence of that permission. 3. Other military modifications may have been installed on th e aircraft which are not part of this Supplemental Type Certificate. These installations do not conform to FAA Approved type design, but may have been accepted by the military Airworthiness Authority for operation by the United States Department of Defense. These installations are shown on FAA Form 8130-2, Conformity Certificate – Military Aircraft, dated April 26, 2005 or later. All non-conformances to FAA approved type design must be removed, or FAA approved, prior to returning the aircraft to civil registration with a standard airworthiness certificate. 4. This approval is limited to Boeing Mode l 747-E4B, Serial Numbers 20682, 20683, and 20684. 5. Prior installations are required of th e following Supplemental Type Certificates: a. STC ST00259WI, INMARSAT b. STC ST09661SC, FMS; EFIS; GPS c. STC ST09504SC, VHF Com Upgrade d. STC ST09662SC, TCAS; TA/VSI; IFF Mode S e. STC ST09663SC, TAWS Certification Basis: The Certification Basis for this installation is per Type Certificate Data Sheet No. A20WE, Revision 35. Voluntary compliance has been found relative to the following regulations: a. Amendment 25-23, effective April 8, 1970 [25.301(a)(b)(c); 25.303; 25.471; 25.607; 25.611] b. Amendment 25-38, effective December 20, 1976 [25.1385] c. Amendment 25-41, effective July 18, 1977 [25.1309] d. Amendment 25-42, effective January 16, 1978 [25.1353(a)(b)] e. Amendment 25-46, effective October 30, 1978 [25.603; 25.605, 25.777(a)(b)(c); 25.789(a)] f. Amendment 25-51, effective February 4, 1980 [25.787] g. Amendment 25-54, effective September 11, 1988 [25.365(a)(d); 25.561; 25.571; 25.1529] h. Amendment 25-72, effective August 20, 1990 [25.21( a)(d); 25.29; 25.307(a); 25.613(a)(b)(c)(d); 25.869(a4); 25.1351; 25.1581(a)(b)(d)] i. Amendment 25-80, effective April 28, 1994 [25.1316] j. Amendment 25-86, effective February 9, 1996 [25.305(a)(b)] k. Amendment 25-91, effective July 29, 1997 [25.561(a)(b3)(c)] l. Amendment 25-102, effective June 6, 2001 [25.981] m. Amendment 25-105, effective J une 26, 2001 [25.1583(c1); 25.1585(a)] -end- ## Every issue (1) - August 23, 2005: Issued, Current. [certificate](https://openairdocs.org/files/sha256/fa/68/fa68376dddeeff11299e183398fb9c2e210fbef83f150f5443c416f2a6e8249c) --- 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.