# STC ST00181SE - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Honeywell International Inc, United States - Description: Installation of Model 4033, 4034 and 4038 Transient Suppression Units - Applied: May 19, 1994 - Status date: January 4, 2022 - Product: Aircraft, Large Airplane - Certification basis: Part 21, Part 25 - Data sheets: [TCDS A35EU](https://openairdocs.org/tcds/A35EU) - Certificate PDF: https://openairdocs.org/files/sha256/af/24/af24ae8ea501fa43b14132b812ab2fbfc44dde51aeba163f15345237ef2ac708 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/250EE372B4C608C7862587DC006599BE.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/ST00181SE ## ADs that name it (0) None. ## Approved models (13) - Airbus SAS A300 B2-1A ([TCDS A35EU](https://openairdocs.org/tcds/A35EU)) - Airbus SAS A300 B2-1C ([TCDS A35EU](https://openairdocs.org/tcds/A35EU)) - Airbus SAS A300 B2-203 ([TCDS A35EU](https://openairdocs.org/tcds/A35EU)) - Airbus SAS A300 B2K-3C ([TCDS A35EU](https://openairdocs.org/tcds/A35EU)) - Airbus SAS A300 B4-103 ([TCDS A35EU](https://openairdocs.org/tcds/A35EU)) - Airbus SAS A300 B4-203 ([TCDS A35EU](https://openairdocs.org/tcds/A35EU)) - Airbus SAS A300 B4-2C ([TCDS A35EU](https://openairdocs.org/tcds/A35EU)) - Airbus SAS A300 B4-601 ([TCDS A35EU](https://openairdocs.org/tcds/A35EU)) - Airbus SAS A300 B4-603 ([TCDS A35EU](https://openairdocs.org/tcds/A35EU)) - Airbus SAS A300 B4-605R ([TCDS A35EU](https://openairdocs.org/tcds/A35EU)) - Airbus SAS A300 B4-620 ([TCDS A35EU](https://openairdocs.org/tcds/A35EU)) - Airbus SAS A300 B4-622 ([TCDS A35EU](https://openairdocs.org/tcds/A35EU)) - Airbus SAS A300 B4-622R ([TCDS A35EU](https://openairdocs.org/tcds/A35EU)) ## 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. FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION Page 1 of ___ ST00181SE Honeywell International Inc. 21111 N 19th Ave Phoenix, Arizona 85027 Part 25 Federal Aviation Regulations A35EU Airbus Industries A300-B2,-B4 Installation of the Mark VII Ground Proximity and Windshear Warning System per Honeywell Top Drawing Number 960-0323, Revision A, dated March 6, 1995 or later FAA approved revisions. The approval of this change in type design applies to the above model aircraft equipped with those engines listed on page 4. The Mark VII system with Ground Proximity only, i.e. without Windshear Warning are approved for all engine types. 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 other previously approved modifications (i.e. hushkits) will introduce no adverse affect upon the airworthiness of the aircraft. A copy of this Certificate and appropriate FAA Approved Flight Manual Supplement must be maintained as part of the permanent records for the modified aircraft. May 19, 1994 January 4, 2022 April 5, 1995 September 27, 2001 For Acting Manager, Seattle ACO Branch 3 FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION Page 2 of ___ ST00181SE 3 Aircraft Model Engine Model Hushkit Compatibilitv Airbus General Electric A300-B2-1A CF6-50A NIA A300-B2-1C CFS-SOC NIA A300-B2K-3C CF6-50C NIA A300-B2-203 CF6-50-C2 NIA A300.B4-2C CF6-50 NIA A300 84-103 CF6-50C, -50C1, -50C2 NIA A300-B4-203 CF6-50C, -50C 11 50C2 NIA United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: End FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION Page ___ of ___ ST00181SE Limitations and Conditions (continued): Installation of the MK VII Warning System is limited to aircraft/engines combinations listed or which have incorporated hushkits listed in Table I. Table I - Hushkit installations not listed which have been shown to meet the requirements of FAA Advisory Circular 25.939-1, or equivalent are also acceptable, if the installer determines that the interrelationship between the MK VII installation and the hushkit installation will introduce no adverse effect upon the airworthiness of the aircraft. The MK VII Warning System has been demonstrated acceptable for use in the following Airbus Industrie airplane/engine/hushkit combinations: ## Every issue (4) - January 4, 2022: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/af/24/af24ae8ea501fa43b14132b812ab2fbfc44dde51aeba163f15345237ef2ac708) - February 14, 2014: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/c1/81/c181548610adce105a82d53a73e3b3a0ed9560e81440fe0ca70833873be2bc77) - December 26, 2013: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/a6/0c/a60c258aee8f606494e0fc5c939e06903a0ff8a75dfe6f1c7c72935ea3bb32aa) - March 29, 2012: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/bf/ae/bfae0e27b02d08f9111ba887b59f9ed1c4b62f5e8b08a7f2f29f5403d786dfee) --- 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.