# STC ST11846MC - Type: Supplemental type certificate - Status: Current, Issued - Holder: Gulfstream Aerospace Corporation, United States - Description: Installation of Peregrine Aircraft Modifications - Applied: February 29, 2020 - Status date: December 10, 2024 - Product: Aircraft, Large Airplane - Certification basis: Part 25 - Data sheets: [TCDS A12EA](https://openairdocs.org/tcds/A12EA) - Certificate PDF: https://openairdocs.org/files/sha256/c6/93/c693ae1d7c46a30cd51e9ae3ac4a0a97ef52290f8c66d708ea23eb0e39c676a4 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID172805317020250129143734.0001 - DRS record last changed: December 5, 2025 - Page: https://openairdocs.org/stc/ST11846MC ## ADs that name it (0) None. ## Approved models (1) - Gulfstream Aerospace Corporation GV-SP ([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 TORM STRATOS Supplemental Type Certificate Number: ST11846MC This certificate issued to: Gulfstream Aerospace Corporation 500 Gulfstream Road Savannah, GA 31408 25 of Code of Federal Regulations Original Product A12EA Make: Gulfstream Type Certificate Number: Model: GV-Sp Description of Type Design Change: Installation of the Peregrine Aircraft Modifications in accordance with the following Gulfstream Aerospace Corporation's Master Drawing List SM-GER-0230 revision A, dated December 10, 2024 or later FAA approved revision. (continued on page 3 of 7) Limitations and Conditions: This STC is applicable to all serial numbers for this make-model and certifies the -501, -503, -505, and - 507 configurations. (continued on page 3 of 7) Date of Application: February 29, 2020 Date Reissued: Date of Issuance: December 10, 2024 Date Amended: By Direction of the Administrator V.SO Signature: nanopadol.seniwong@gulfstream.com for Title: Robert Glasscock ODA Lead Administrator, ODA-511131-CE Gulfstream Aerospace Corporation United States of America Department of Transportation Federal Aviation Administration TORM STRATE Supplemental Type Certificate Number: ST11846MC Extent of Authority (if licensing agreement); FEDERAL AVIATION United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: ST11846MC Date of Issuance: December 10, 2024 Description of Type Design Change: (continued): The FAA accepted Instructions for Continued Airworthiness, SM-GER-0272 revision D, dated December 7, 2024, or later FAA accepted revision is required for Gulfstream model GV-SP. The FAA accepted revision must be available to the operator at the time of installation. The FAA accepted EWIS Instructions for Continued Airworthiness, SM-GER-0699 revision A, dated January 11, 2024, or later FAA accepted revision is required for Gulfstream model GV-SP. The FAA accepted revision must be available to the operator at the time of installation. The FAA approved Airplane Flight Manual Supplement (AFMS)G550-Peregrine-AFMS- 2017-02 revision (-), dated December 10, 2024, or later FAA approved revision is required and must be carried in the aircraft on all flights. The FAA accepted Critical Design Configuration Control Limitation (CDCCL), SM-GER- 0752 revision (-), dated August 5, 2024, or later FAA accepted revision is required for Gulfstream model GV-SP. The FAA accepted revision must be available to the operator at the time of installation. Limitations and Conditions: (continued): 1. The installer must determine whether this design change is compatible with previously approved moditications. 2. If the holder agrees to permit another person to use this certificate to alter a product, the holder must give the other person written evidence of that permission. (continued on page 4 of 7) This FEDERAL AVIATION United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: ST11846MC Date of Issuance: December 10, 2024 Limitations and Conditions: (continued): 3. This STC contains both provision and system approvals. The FAA has not certified the equipment for the provision approvals. Additional FAA approval will be required to install this equipment. The FAA must evaluate the installation to ensure it complies with the applicable airworthiness standards. 4. The following interface document applies to this STC: SM-GER-0123, Peregrine Provisions Limitations. 5. All removed life limited components must be discarded and may not be installed on other GV-SP aircraft. 6. The following changes to the aircraft must be accomplished prior to or concurrently with this STC: A. Gulfstream ASC-026 - Mid Wing Fuel Ejector System, or later approved revision. B. Gulfstream ASC-030A - Additional Electrical Power (-7 configuration), or later approved revision. C. Gulfstream ASC-084D - Enhanced Navigation, or later approved revision. D. Gulfstream ASC105A - Mandates Package (CPDLC/ADS-B Out), or later approved revision. E. Gulfstream ASC-071A - Micro Quick Access Recorder, or later approved revision. F. Gulfstream ASC-128B - Equipment and Furnishings (ATA 25) Flashlights - Replacement, or later approved revision. (continued on page 5 of 7) This FEDERAL AVIATION United States of America Department of Transportation Federal Aviation Administration TORM STRATO Supplemental Type Certificate (Continuation Sheet) Number: ST11846MC Date of Issuance: December 10, 2024 Certification Basis: Gulfstream GV-SP 14 CFR Part 25, effective February 1, 1965, including amendments 25-1 through 25-98, with the following exceptions: a. The type certification basis for Gulfstream GV-SP airplanes is shown on TCDS A12EA for parts not changed or not affected by the change. b. The certification basis for parts changed or affected by the change since the reference date of application, February 29, 2020, is based upon part 25 as amended by Amendment 25-146. Based on 14 CFR 21.115 and 21.101, and the FAA policy for significant changes in FAA order 8110.48A, the certification basis for this modification was determined to be: 14 CFR 25 effective February 1, 1965, including Amendments 25-1 through 25-98, as defined by FAA TCDS A12EA Rev 50 dated July 9, 2019, and amendments 25-99 through 25-146 per G-1 Issue Paper revision 2, dated October 16, 2023. 25.103(a)(b)(c)(d) [25-108], 25.117 [25-0], 25.119(a)(b) [25-108], 25.121(a) (b)(c)(d)[25- 108], 25.123(a)(b) [25-0], 25.143(a)(b)(c)(d)(e)(f)(g) [25-108], 25.145(a) (b)(c)(d) [25- 108], 25.147(a)(c)(d)(f) [25-115], 25.149(a)(b)(c)(d)(e)(f)(h) [25-108], 25.161(a)(b)(c)(d) [25-115], 25.171 [25-7], 25.173(a)(b)(c)(d) [25-7], 25.175(a)(b)(c)(d) [25-115], 25.177(a)(b)(c)(d) [25-135], 25.181(a)(b) [25-108], 25.201(a)(b)(c)(d) [25-108], 25.203 (a)(b)(c) [25-84], 25.207(a) (b)(c)(d)(e)(f) [25-108], 25.231(a)(1) [25-108], 25.233(a)(b) (c) [25-108], 25.237(a) [25-108], 25.251(a)(b)(c)(d)(e) [25-77], 25.253(a) [25-84], 25.255(a)(b)(c)(d)(e)(f) [25-42], 25.301(a)(b)(c) [25-23], 25.303 [25-23], 25.305(a)(b) [25-86], 25.305(c) [25-86], 25.307(a)(d) [25-139], 25.321(a) (b)(c)(d) [25-86], 25.331(a) (b)(c) [25-141], 25.333(a) [25-86], 25.335(a)(b)(c)(d) [25-91], 25.337 (a)(b)(c) [25-23], 25.341(a)(b) [25-86], 25.343(a)(b) [25-86], 25.345(a)(b)(2)(d) [25-91], 25.349(a)(b) (continued on page 6 of 7) This FAA Form 8110-2 (03/21) Page_5_of_7 FEDERAL AVIATION United States of America Department of Transportation Federal Aviation Administration TORMISTRATO Supplemental Type Certificate (Continuation Sheet) Number: ST11846MC Date of Issuance: December 10, 2024 Certification Basis (continued): [25-94], 25.351(a)(b)(c)(d) [25-91], 25.363(a)(b) [25-91], 25.365(a)(d)(e) [25-87], 25.367 (a)(b) [25-0], 25.373(a) [25-86], 25.427 (a)(b)(c)(d) [25-86], 25.445(a) [25-86], 25.471(a)(b)(c) [25-23], 25.473(a)(b)(c)(d)(e) [25-103], 25.477 [25-0], 25.479(a)(c)(d) [25-91], 25.481(a)(c) [25-94], 25.483(a)(b) [25-91], 25.485(a)(b) [25-91], 25.489 [25-23], 25.491 [25-91], 25.493(b) (c)(d) [25-97], 25.495 [25-0], 25.499(a) (b)(c)(d)(e) [25-91], 25.519(a)(b 25-81], 25.561(a) (b)(c) [25-91], 25.563 [25-01, 25.571 (a)(b)(c)(e)(1) [25-96], 25.581(a) [25-23], 25.601 [25-0], 25.603(a)(b)(c) [25-46], 25.605(a) [25- 461, 25.60 [25-23], 25.609(a)(b) [25-0], 25.611(a) [25-123], 25.613(a) (b)(c) [25-112], 25.619 [25-23], 25.625(a)(b)(c) [25-72], 25.629(a)(b)(d)(e) [25-77], 25.672(b)(c) [25-23], 25.729(a)(d) [25-75], 25.771 (a) [25-4], 25.773(a) (2) [25-72], 25.783(a) [25-88], 25.789(a) [25-46], 25.801 (b)(c)(d)(e) [25-72], 25.841(a) [25-87], 25.843(a) [25-0], 25.853(a) [25-83], 25.855(d) [25-142], 25.856(a) [25-111], 25.863(a)(b)(c [25-46], 25.867(a) [25-23], 25.899(all) [25-123], 25.954(all) [25-14], 25.963( 25-139], 25.981(a) (3)(d) [25-125], 25.994 [25-139], 25.1093(b)(1) [25-72], 25.1301(a 25-123], 25.1309(a) (b)(c)(d)(e)(f) [25-123], 25.1316(c)(7) [25-80], 25.1322( [25-38], 25.1323 (b)(c)(d)(e)(f)(g) [25-109], 25.1325(e) [25-108], 25.1351(a [25-72], 25.1353(a) [25-123], 25.1381 (a)(b) [25-72], 25.1419(a) [25- 1291, 25.1431 [25-0], 25.1461(a) (b)(c)(d) [25-41], 25.1529 [25-54], 25.1533(a) [25- 92], 25.1541 [25-0], 25.1545 [25-0], 25.1557 (a) [25-72], 25.1563 [25-0], 25.1581(a 125-721, 25.1583( [25-130], 25.1585(a)(b) (d)(e)(f) [25-105], 25.1587(b)(1)(2)(3)(5)(6)(7) [25-108], 25.1703(a)(b)(d) [25-123], 25.1705(a) [25-123], 25.1707 (all) [25-123], 25.1709(a)(b) [25-123], 25.1711(a)(c)(d)(e) [25-123], 25.1713(c) [25-123], 25.1715(a)(b) [25-123], 25.1717 [25-123], 25.1719 [25-123], 25.1721(a) (b)(c) [25-123], 25.1729 [25-123], H25.5(a)(b) [25-123]. (continued on page 7 of 7) This FAA Form 8110-2 (03/21) Page_6_ of _7 FEDERAL AVIATION United States of America Department of Transportation Federal Aviation Administration TORMISTRATO Supplemental Type Certificate (Continuation Sheet) Number: ST11846MC Date of Issuance: December 10, 2024 Certification Basis (continued): 14 CFR 36 effective December 1, 1969, including Amendments 36-1 through 36-30. 36.1(a)(1)(b)(c)(f)(7)(9)(10)(11)(g) [36-30], 36.2(a)(b) [36-24], 36.3 [36-14], 36.5 [36-0], 36.6(a)(b)(c) [36-26], 36.7(a)(b)(f) [36-26], 36.101 [36-24], 36.103(a)(c) [36-26], 36.105 [36-26], 36.1501(a)(b) [36-15], 36.1581(a)(1)(b)(c)(d)(g) [36-25], B36.5(d) [36-26], B36.7(all) [36-24], Special Condition 25-262-SC, dated May 14, 2004, Gulfstream Model GV-SP and GIV- X, High Intensity Radiated Fields (HIRF). ---END-- This FAA Form 8110-2 (03/21) age / of 7 ## Every issue (1) - December 10, 2024: Issued, Current. 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