# STC ST10958SC - Type: Supplemental type certificate - Status: Current, Amended - Holder: Bizjet International Sales & Support Inc - Description: Installation of a Cabin VIP Interior - Status date: January 3, 2013 - Data sheets: A28NM, A28NM, A28NM, A28NM, A28NM, A28NM, A28NM, A28NM, A28NM, A28NM, A28NM, A28NM - Certificate PDF: https://openairdocs.org/files/sha256/70/af/70af7a03e560443024c68d434802ef9a2f201e84798c20b40973da01fa873a9a - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/209F3E0B6371723486257AF50070E2B4.0001 - Page: https://openairdocs.org/stc/ST10958SC ## ADs that name it None. ## Approved models (12) - Airbus A318-111 (TCDS A28NM) - Airbus A318-112 (TCDS A28NM) - Airbus A318-121 (TCDS A28NM) - Airbus A318-122 (TCDS A28NM) - Airbus A319-111 (TCDS A28NM) - Airbus A319-112 (TCDS A28NM) - Airbus A319-113 (TCDS A28NM) - Airbus A319-114 (TCDS A28NM) - Airbus A319-115 (TCDS A28NM) - Airbus A319-131 (TCDS A28NM) - Airbus A319-132 (TCDS A28NM) - Airbus A319-133 (TCDS A28NM) ## 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 Number: ST10958SC This certificate issued to BIZJET International Sales & Support 3515 North Sheridan Road Tulsa, OK 74115 Part 25 of the Federal Aviation Regulations. Original Product Type Certificate Number : A28NM Make : Airbus Model : A318 Series; A319 Series Description of Type Design Change: Installation of a Cabin VIP Interior in accordance with master Data List (MDL) document number 1110000010, Revision R, dated December 31, 2012 or later Federal Aviation Administration (FAA) approved revision. FAA approved Airplane Flight Manual Supplement (AFMS) document number 1110021090, Revision IR, dated December 18, 2009 or later FAA approved revision is required for the -001 configuration on Airbus A318 Series aircraft. FAA approved AFMS (See continuation sheet 3 of 3) 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. Supplemental Type Certificate (STC) ST10964SC, provisions for executive power system, must be installed with MDL document number 1110000010-001 only. Date of application: October 06, 2008 Date reissued: Date of issuance: December 23, 2009 Date amended: July 12, 2010; March 20, 2012; July 26, 2012; January 3, 2013 (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) Number ST10958SC Date of Issuance: December 23, 2009 Date Amended: January 3, 2013 Description of Type Design Change (Continued): document number 1160021090, Revision A, dated May 12, 2011 or later FAA approved revision is required for the -002, -003, -005 and -007 configurations on Airbus A318 series aircraft. FAA approved AFMS document number 1190021090, Revision IR, dated August 19, 2011 or later FAA approved revision is required for the -004 configuration on Airbus A319 Series aircraft. FAA approved AFMS document number 1275021090, Revision IR, dated February 12, 2012 or later FAA approved revision is required for the -006 configuration on Airbus A318 Series aircraft. FAA approved AFMS document number 1310021090, revision IR, dated August 24, 2012 or later FAA approved revision is required for the -008 configuration on Airbus A319 Series aircraft. Certification Basis: The certification basis for this installation is per type certificate data sheet A28NM, plus the following: Regulations that meet amendment 25-72: 25.29, 25.803, 25.809(a)(b)(c), 25.1581 Regulations that meet amendment 25-74: 25.854(a) Regulations that meet amendment 25-83: 25.853 Regulations that meet amendment 25.88: 25.811(a)(b)(c )(d)(e)(f)(g), 25.812 (a)(b1)(c)(d)(e)(f)(i)(l)(l), 25.813(a)(b)(c)(d)(f) Regulations that meet amendment 25-91: 25.561(c) Regulations that meet amendment 25-93: 25.858 Regulations that meet amendment 25-94: 25.807(c) Regulations that meet amendment 25-105: 25.1583(h), 25.1585(a) Regulations that meet amendment 25-111: 25.856(a) Regulations that meet amendment 25-123: 25.869(a)(1)(2) Regulations that meet amendment 26-0: 26.11(c) --END-- ## Every issue (4) - January 3, 2013: Amended, Current. [certificate](https://openairdocs.org/files/sha256/70/af/70af7a03e560443024c68d434802ef9a2f201e84798c20b40973da01fa873a9a) - July 26, 2012: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/d3/88/d38847795e6d20bf7c0428025de1020ead02cd98561bf5468c3c76632f013f7b) - March 20, 2012: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/e2/70/e27081a9174718e06ce790f95c242e71866bb2ae7559de35d5b5ef7dcc1d6698) - December 23, 2009: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/64/d6/64d64122ac6964e2313273f74e36b6702d830a3ad9fa1bee402809b7d44d2df7) --- 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.