# STC SA1362SO - Type: Supplemental type certificate - Status: Current, Surrendered - Holder: Page AvJet Corp, United States - Description: Installation of main cabin interior. - Status date: July 9, 2008 - Product: Aircraft, Large Multi-Engine - Certification basis: Part 21 - Data sheets: [TCDS A12EA](https://openairdocs.org/tcds/A12EA) - Certificate PDF: https://openairdocs.org/files/sha256/0a/96/0a96674e7183ee0867d8f218cbfc165a09ee9d2b0480e88698a88707b519ec35 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/B10FA4BF05247731862574B80078720C.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA1362SO ## ADs that name it (0) None. ## Approved models (1) - Gulfstream Aerospace Corporation G-1159A ([TCDS A12EA](https://openairdocs.org/tcds/A12EA)) ## What the certificate says 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 Re-issued on July 9, 2008 to supersede the original STC, which has been lost or misplaced or destroyed Number: SA136250 This certificate issued to: Page AvJet Corp. 9809 Florida Rd Orlando, FL 32812 latio and conditions therefor as specified hereon meets the airworthiness requirements the roderal Aviatio Regulations. Original Product - Type Certificate Number A12EA, Description of Type Design Change: Ipstallation ofpain cabi interior. NOTE 1 - This STC Re-issue is based on the surrender ofthis STC from Page AvJet on July 9, 2008. This "duplicate" produced in accordance with FAA Order 8110.4C paragraph (32)(1)(8) modifies the STC text to address this surrender. As of the surrender date, no new installations of this STC should oøcur without express written authorization from the cognizant Aircraft Certification Office. Future unsafe conditions existing in the product may result in an airworthiness directive requiring correction of the unsafe condition before further flight. The existence of an unsafe condition may result in permanently grounding the aircraft, unless operatef obtais approval for a method of compliance. Contact the Atlanta Aircraft Certification Office for further details. This approval should not be extended to other aircraft of this model on which other previously approved modifications are incorporated, unless it is determined by the installer that the interrelationship between this change and any other previously approved modifications will produce no adverse effect upon the airworthiness of that airplane. If the holder agrees to permit anther person to use this certificate to alter the product, the holder shall give the other person written evidence of that CANN Melvin D. Taylor, Manager Atlanta Aircraft Certification Office TOMINISTRATO (Title) FAA FORM 8110-2-1(10-69) PAGE 1 of 1 PAGES ## Every issue (1) - July 9, 2008: Surrendered, Current. [certificate](https://openairdocs.org/files/sha256/0a/96/0a96674e7183ee0867d8f218cbfc165a09ee9d2b0480e88698a88707b519ec35) --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.