# STC ST00129BO - Type: Supplemental type certificate - Status: Current, Amended - Holder: Greenpoint Technologies, United States - Description: Installation of executive interior modifications. Applies to Boeing model 757-2G4. - Applied: April 12, 2000 - Status date: July 31, 2009 - Product: Aircraft, Large Multi-Engine - Certification basis: Part 21, Part 25, Part 26 - Data sheets: [TCDS A2NM](https://openairdocs.org/tcds/A2NM) - Certificate PDF: https://openairdocs.org/files/sha256/94/22/94223b1b4ded83fee0fb42c5efa7fc64d8e50e4434338ffa4142b3b109eaaace - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/2465ED98F2F9492F8625761E00781725.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/ST00129BO ## ADs that name it (0) None. ## Approved models (1) - The Boeing Company 757-200 Series ([TCDS A2NM](https://openairdocs.org/tcds/A2NM)) ## 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 ST00129BO This certificate, issued to: Greenpoint Technologies, Inc. 4600 Carillon Point Kirkland, WA 98033 Part 25 of the Federal Aviation Regulations. Original Product Type Certificate Number: A2NM Make: The Boeing Company Model: 757-2G4 Description of the Type Design Change: Installation of executive interior modifications in accordance with Greenpoint Technologies, Inc. drawing list G7981-DL-01 Revision J dated June 30, 2009 or later Federal Aviation Administration (FAA) approved revisions. Limitations and Conditions: Approval of this change in type design applies to the above model aircraft only. See continuation sheet 3 of 3 for additional limitations. This approval should not be extended to other aircraft of this model on which other previously approved modifications are incorporated unless it is determined that the relationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of the aircraft. A copy of this certificate and Greenpoint Technologies, Inc. Master Drawing List G7981-DL-01 Revision J dated June 30, 2009 or later Federal Aviation Administration (FAA) approved revisions must be maintained as part of the permanent records for the modified aircraft. 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. (Limitations and Conditions continued on page 3 of 3) This certificate and the supporting data which are the basis for approval shall remain in effect until surrendered, suspended, revoked, or a termination date is otherwise established by the Administrator of the Federal Aviation Administration. Date of application: April 12, 2000 Date reissued: March 16, 2000 Date of issuance: December 19, 2000 Date amended: July 31, 2009 By direction of the Administrator Original Signed by Victor W. Wicklund (Signature) Manager, Seattle Aircraft Certification Office (Title) **FAA FORM 8110-2(10-68) P AGE 1 OF 3** United States of America Department of Transportation - Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number ST00129BO Issued to: Greenpoint Technologies Dave of Issuance: December 19, 2000 Dave Amended: July 31, 2009 Note: This continuation sheet is applicable to the STC Amendment as issued on July 31, 2009. The Supplemental Instructions for Continued Airworthiness, Greenpoint Technologies, Inc. document G7981- CA-01 Revision IR, dated May 27, 2009, or later FAA-accepted revision, must be incorporated into the operator’s maintenance program. This modification may not be installed after August 30, 2010 unless (1) previously approved electrical wiring interconnect system (EWIS) instructions for continued airworthiness (ICA) have been evaluated and determined to be adequate for this installation by the FAA, or (2) revised EWIS ICA have been approved by the FAA Oversight Office. (Refer to CFR 26.11). Certification Basis: Based on 14CFR §§ 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for this modification is based upon Part 25 as specified in TCDS A2NM. Regulations at a later amendment level than specified in TCDS A2NM are listed below: § 25.25 Amendment 25-63 § 25.1309(a)(b)(g) Amendment 25-41 § 25.29 Amendment 25-72 § 25.1353(a)(b)(d)(2)(3) Amendment 25-113 § 25.307(a) Amendment 25-72 § 25.1431(a) Amendment 25-113 § 25.571(a)(b) Amendment 25-86 § 25.1529 Amendment 25-54 § 25.613(a)(b)(d) Amendment 25-72 § 25.1583(c)(1)(2) Amendment 25-105 § 25.625 Amendment 25-72 § 26.47 Amendment 26-0 § 25.789(a) Amendment 25-46 § 25.853(a) Amendment 25-116 § 25.869(a)(1)(4) Amendment 25-113 ------------------------------------- END ------------------------------------------- **FAA FORM 8110-2(10-68) P AGE 3 OF 3** ## Every issue (1) - July 31, 2009: Amended, Current. [certificate](https://openairdocs.org/files/sha256/94/22/94223b1b4ded83fee0fb42c5efa7fc64d8e50e4434338ffa4142b3b109eaaace) --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. 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