# STC ST00221BO - Type: Supplemental type certificate - Status: Current, Amended - Holder: BAE SYSTEMS Information and Electronic Systems Integration Inc., United States - Description: Installation of a BAE Systems IRCM. - Applied: October 6, 2004 - Status date: February 4, 2019 - Product: Aircraft, Large Multi-Engine - Certification basis: Part 21, Part 25, Part 26 - Data sheets: [TCDS A1SO](https://openairdocs.org/tcds/A1SO) - Certificate PDF: https://openairdocs.org/files/sha256/6e/48/6e48cf413f63b53672af5433c9ffb4650ed71de12745ea75acfa434d41cca5e0 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/40A2F71CE87D37B3862584D40069884F.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/ST00221BO ## ADs that name it (0) None. ## Approved models (1) - Lockheed Martin Corporation 382G ([TCDS A1SO](https://openairdocs.org/tcds/A1SO)) ## 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. Number ST00221BO FAA Form 8110-2 (5/14) Page 1 of 4 This certificate issued to: BAE Systems Information and Electronic Systems Integration Inc. 65 Split Brook Road Nashua, NH 03061 Part 25 of the Federal; Aviation Regulations. Original Product - Type Certificate Number: A1SO Make: Lockheed Martin Corporation Model: 382G Installation of a BAE Systems Infrared Countermeasure (IRCM) Set 8350550G12 in accordance with BAE Systems Master Document List (MDL) 94117-8458635, Revision M, dated December 21, 2018, or later FAA approved revision. 1. This STC is for government use only. 2. IRCM Set 8350550G12 replaces and makes obsolete IRCM Set 8350550G6 (also known as AN/ALQ-212(V)6), of which none are installed or procurable as verified by BAE Systems. (continued on Page 3 of 5) Date of Application: October 06, 2004 Date reissued: Date of Issuance: October 28, 2005 Date amended: May 07, 2010; August 30, 2010; January 27, 2012; March 19, 2012; February 04, 2019 Anthony Pigott for Signature Kevin Dickert Manager, Boston ACO Branch Title FAA Form 8110-2 (5/14) Page 2 of 4 To (Name and address of transferee) Name: Address (Number and Street, City, State, and ZIP Code): From (Name and address of grantor) Name: Address (Number and Street, City, State, and ZIP Code): (Continuation Sheet) Number ST00221BO FAA Form 8110-2 (5/14) Page 3 of 4 Limitations and Conditions: (continued from Page 1 of 4) 3. Operation must be in accordance with Pro Star Aviation Aircraft Flight Manual Supplement (AFMS), Document number 20568-FMS-21, Revision B, FAA approved on August 03, 2015, or later FAA approved revision. The AFMS must be carried in th e aircraft during all flights. 4. Maintenance must be in accordance with Instructions for Continued Airworthiness (ICA): BAE Systems ICA, Document number 94117-B49939, Revision A, dated December 14, 2018, or later FAA accepted revision. Airworthiness Limitations Section 15 is FAA approved. BAE Systems Electrical Wiring Interconnection Systems (EWIS) ICA, Document number 94117- A67561, Revision B, dated November 11, 2018, and FAA approved on February 04, 2019, or later FAA approved revision. These ICAs must be made available to the operator at the time of installation. 5. FAA Certification of this installation was limited to the evaluation of the electronic countermeasures equipment’s effects on the safe operation of the aircraft, and does not connote FAA endorsement of the effectiveness of the equipment in countering a MANPADS threat. In addition, the FAA has not evaluated the safety of the IR laser for use on the ground or in the air. Operation of the IR laser, to include appropriate laser safety training for flight crew and maintenance personnel, should be in accordance with the intent of American National Standards Institute (ANSI) Standards Z136.1, Safe use of Lasers, and Z136.6, Use of Lasers Outdoor. The IR jam deflector door was not evaluated by the FAA for its ability to protect the IR jam head from foreign object damage. 6. Compatibility of this design with previously approved modifications must be determined by the installer. (Continuation Sheet) Number ST00221BO FAA Form 8110-2 (5/14) Page 4 of 4 Certification Basis: Based on 14 CFR § 21.115 and § 21.101, and the FAA policy for design changes that are identified as not significant in FAA Order 8110.48, the certification basis for the Lockheed Martin Corporation 382G is as follows: a. The type certification basis for parts not changed or not affected by the change is shown on TCDS A1SO. b. The modification certification basis for parts changed or affected by the change since: (1) the amendment application date March 07, 2011, corresponding to the reference amendment date January 27, 2012, is based upon part 25 as amended by Amendment 25- 132 and (2) the amendment application date June 07, 2010, corresponding to the reference amendment date August 30, 2010, is based upon part 26 as amended by Amendment 26-4 as follows: Regulations at the latest amendment 25-0 through 25-132 25.29, 25.143, 25.251, 25.301 - 307, 25.365, 25.561, 25.601 - 609, 25.613, 25.625, 25.853, 25.869, 25.1351, 25.1381, 25.1431, 25.1501, 25.1529, 25.1581, 25.1585, 25.1713, Appendix H25.1 - H25.5 Regulations at the latest amendment 26-0 through 26-4 26.11(c)(d)(5), 26.47(c)(e)(3) Regulations at an intermediate amendment 25.143 at 25-108, 25.177 at 25-108, 25.571 at 25.96, 25.611 at 25-23, 25.773 at 25-108, 25.1301 at 25-0, 25.1309 at 25-41, 25.1322 at 25-38, 25.1353 at 25-113, 25.1357 at 25-0, 25.1583 at 25-105 Regulations at the amendment level in TCDS A1SO None ------------------------------------------------------------END------------------------------------------------------- ## Every issue (7) - February 4, 2019: Amended, Current. [certificate](https://openairdocs.org/files/sha256/6e/48/6e48cf413f63b53672af5433c9ffb4650ed71de12745ea75acfa434d41cca5e0) - March 19, 2012: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/57/d2/57d2896ad6dc866af5bd12762dbf84c4f2b3f682631ae7e1935c79f406dd73b1) - January 27, 2012: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/d2/b5/d2b5a466b08b008c29a6b78b69d5020b0da2d7382c493bb7f200abdea1b27e99) - August 30, 2010: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/09/26/09260a97a47cf06eecc9504c7780a79de84088a3584d5abc4878c2a846cb8da5) - May 7, 2010: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/72/2d/722da7c16a70bd932a5825ebdf2557be0be2de1a02806c758d37475561fb6111) - November 14, 2005: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/86/e2/86e2db666bc67ad131979fc8e0b152f1f7fd76d1e87905be2a00420a493440f0) - October 28, 2005: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/1b/dc/1bdcc4b71ea6cb60c38410b4a0dd00358d348d889f026d33c4bb057f40faf0d9) --- 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.