# STC SA10953SC - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Textron Aviation Inc, United States - Description: Installation of the Honeywell Cabin Pressure Outflow and Safety Valves in accordance with Hawker Beechcraft Services, Inc. STC Master Data List No. RAS230600900, Revision 1.0, dated 06/05/2009 or later FAA approved revision. - Applied: January 19, 2007 - Status date: December 12, 2016 - Product: Aircraft, Single-Engine - Certification basis: Part 3, Part 21, Part 23, Part 25, Part 27, Part 29, Part 34, Part 36 - Data sheets: [TCDS 3A20](https://openairdocs.org/tcds/3A20), [TCDS A24CE](https://openairdocs.org/tcds/A24CE) - Certificate PDF: https://openairdocs.org/files/sha256/18/e8/18e8fa40bb1e62443755943b6c995a06b69fac601071cb1ca4c1a51c8b45709d - Approved model list and other attachments: [SA10953SC AML.pdf](https://openairdocs.org/files/sha256/dc/d2/dcd2259de860c666b0e9d26a883c71a9f7b87ac0b9453b81550fa19321bcc327) - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/576BE9CA0052E07E86258148006BD538.0001 - DRS record last changed: December 5, 2025 - Page: https://openairdocs.org/stc/SA10953SC ## ADs that name it (0) None. ## Approved models (9) - Hawker Beechcraft Corporation B200 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Hawker Beechcraft Corporation B200C ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Hawker Beechcraft Corporation B200CGT ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Hawker Beechcraft Corporation B200GT ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Hawker Beechcraft Corporation B300 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Hawker Beechcraft Corporation B300C (C-12W) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Hawker Beechcraft Corporation C90A ([TCDS 3A20](https://openairdocs.org/tcds/3A20)) - Hawker Beechcraft Corporation C90GT ([TCDS 3A20](https://openairdocs.org/tcds/3A20)) - Hawker Beechcraft Corporation C90GTi ([TCDS 3A20](https://openairdocs.org/tcds/3A20)) ## 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 (5/14) Page 1 of Part of the Signature Title Textron Aviation Inc. One Cessna Boulevard Wichita, KS 67215 * 2 SA10953SC * Regulations. See attached FAA Approved Model List (AML), Document No. HBSAPD90008, Revision IR, or later approved revisions for the Certification Basis. *See attached FAA Approved Model List (AML), Document No. HBSAPD90008, Rev IR, or later FAA approved revision for list of approved airplane models, applicable installation data requirements and specific limitations. Installation of the Honeywell Cabin Pressure Outflow and Safety Valves in accordance with Hawker Beechcraft Services, Inc. STC Master Data List No. RAS230600900, Revision 1.0, dated 06/05/2009 or later FAA approved revision. The installer must determine whether this design change is compatible with previously approved modifications. 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. Operator must be furnished with Instructions for Continued Airworthiness Document No. RAS230600914, Rev IR or later FAA accepted revision. October 5, 2010; December 12, 2016 January 19, 2007 September 14, 2009 Mark Fuller STC ODA administrator ODA-100129-CE FAA Form 8110-2 (5/14) Page 2 of To (Name and address of transferee) From (Name and address of grantor) ### SA10953SC AML.pdf Document No. HBSAPD90008 Revision 2.0 Hawker Beechcraft Corporation FAA APPROVED MODEL LIST FOR: Cabin Pressure Outflow and Safety Valves 103648-16, 103648-17, 103648-18, and 103648-19 Honeywell Aerospace STC Number SA10953SC APPROVED BY ____________________________________ S. Frances Cox, Manager Special Certification Office, ASW-190 Federal Aviation Administration Fort Worth, Texas 76137 DATE OF APPROVAL _______________________________ Hawker Beechcraft Corporation FAA Approved Model List (AML) 9709 E. Central Honeywell Cabin Pre ssure Outflow and Safety Valves Wichita, KS 67206 STC # SA10953SC Document No. HBSAPD90008 Page i Revision 2.0 **LOG OF REVISIONS** REV PAGES DESCRIPTION FAA APPROVAL DATE IR ALL Initial Release Gary A. Sharon 09/14/2009 1.0 ALL Added Revision to footer. Added aircraft models B200, B200C, B200GT, B200CGT, B300, and B300C to document S. Frances Cox 9/13/2010 2.0 ALL Company Name Change 10/5/2010 Hawker Beechcraft Corporation FAA Approved Model List (AML) 9709 E. Central Honeywell Cabin Pre ssure Outflow and Safety Valves Wichita, KS 67206 STC # SA10953SC Document No. HBSAPD90008 FAA Approved Date: Page ii Revision 2.0 **TABLE OF CONTENTS** **TITLE PAGE** LOG OF REVISIONS … i TABLE OF CONTENTS … ii SECTION I – Introduction: … 1 SECTION II – Certification Basis: … 2 SECTION III – Approved Model List: … 7 Hawker Beechcraft Corporation FAA Approved Model List (AML) 9709 E. Central Honeywell Cabin Pre ssure Outflow and Safety Valves Wichita, KS 67206 STC # SA10953SC Document No. HBSAPD90008 FAA Approved Date: Page 1 of 9 Revision 2.0 SECTION I – Introduction: This document is the FAA Approved Model List (AML) for STC No. ST10953SC for installing the Honeywell 103648-16, 103648-17, 103648-18, and 103648-19 Cabin Pressure Outflow and Safety Valves into eligible aircraft. Revisions to the AML must be coordinated between the STC holder and the responsible ACO, and require FAA approval. IMPORTANT NOTES: This STC is only applicable to the 14 CFR, part 23 Class III, as defined in Advisory Circular AC 23.1309-1C, which are listed in this AML. Installations in 14 CFR, Part 23 Class I, II, and IV, Part 25, Part 27, and Part 29 aircraft are not authorized under this STC. This STC assumes the following equipment is already on each airplane eligible for the proposed modification. The following equipment must be properly linked to meet the intended function for the system, as certified under this AML approval. **NONE** Hawker Beechcraft Corporation FAA Approved Model List (AML) 9709 E. Central Honeywell Cabin Pre ssure Outflow and Safety Valves Wichita, KS 67206 STC # SA10953SC Document No. HBSAPD90008 FAA Approved Date: Page 2 of 9 Revision 2.0 SECTION II – Certification Basis: The certification basis for each model qualified for this modification is detailed below. Aircraft Make Aircraft Model Type Certificate Data Sheet (TCDS) Certification Basis Hawker Beechcraft Corporation C90A 3A20, Rev 67 14 CFR Part 23 Amendments 23-1 through 23-50 and CAR Part 3, amended to May 15, 1956 as specified in TCDS Hawker Beechcraft Corporation C90GT 3A20, Rev 67 14 CFR Part 23 Amendments 23-1 through 23-50 and CAR Part 3, amended to May 15, 1956 as specified in TCDS Hawker Beechcraft Corporation C90GTi 3A20, Rev 67 14 CFR Part 23 Amendments 23-1 through 23-50 and CAR Part 3, amended to May 15, 1956 as specified in TCDS Hawker Beechcraft Corporation B200; B200C; B200GT; B200CGT A24CE, Rev 99 FAR Part 23, effective February 1, 1965, as amended by 23-1 through 23-9, Amendment 23-11, FAR Paragraphs 23.175 and associated FARs 23.143(a), 23.145(d), 23.153, 23.161(c)(3), and 23.173(a) as amended by Amendment 23-14; FAR 23.951(c) and FAR 23.997(d) as amended by Amendment 23-15 (A200CT and B200 series, only); FAR 23.1545(a) as amended by Amendment 23-23 and FAR 23.1325(e) as amended by Amendment 23-20 (B200 Series only); FAR 23.1305(n) as amended by Amendment 23-26; FAA Special Conditions 23-47-CE-5 issued October 30, 1972, Amendment 1 dated December 18, 1973, and Amendment 2 dated January 12, 1979; FAR Paragraphs 25.929 and 25.1419 of FAR Part 25 as amended to December 31, 1972, and FAR 25.831(d) through Amendment 25-41 (For all Model 200 and B200 series aircraft approved for 35,000 feet); SFAR 27 through Amendment 27-4; and FAR Part 36 through Amendment 36-10. For B200 through Serial Number BB-1438 and B200C through Serial Number BL-138 FAR Part 36 through Amendment 36-10. For B200 Serial Numbers BB-1439, BB- 1444 and after, B200C Serial Numbers Hawker Beechcraft Corporation FAA Approved Model List (AML) 9709 E. Central Honeywell Cabin Pre ssure Outflow and Safety Valves Wichita, KS 67206 STC # SA10953SC Document No. HBSAPD90008 FAA Approved Date: Page 3 of 9 Revision 2.0 BL-139 and after, A200CT Serial Numbers FE-25 and after, FAR Part 36 through Amendment 36-20. Compliance with ice protection has been demonstrated in accordance with FAR 25.1419 when ice protection equipment is installed in accordance with the airplane equipment list. Effective April 20, 1993, Electronic Flight Instrument Systems shall meet the requirements of FAR 23.1322 as amended by Amendment 23-17; 23.1301 and 23.1305 as amended by Amendment 23.20; 23.1309, 23.1311, and 23.1321 as amended through Amendment 23-41 and Special Condition 23-ACE-68. Effective January 20, 1994, FAR 23.1457 as amended by Amendment 23-35.. In addition, FAR 135, Appendix A, effective December 1, 1978 (B200 High Density Configuration; See NOTE 11) Equivalent Safety Findings: FAR 23.621 (BB-2 through BB-1042 only); 23.997(d) (All models except A200CT and B200 series); FAR 23.1443 through Amendment 23-9 - 200 (BB-38, BB-39, BB-42, BB-44, BB-54 and after), 200C, 200CT, 200T, plus any earlier Model 200 modified by Beechcraft kits 101-5007 and 101-5008 in compliance with Beech Service Instruction No. 0776- 341. Model UC-12F (BU-1 through BU- 12). Not applicable to B200 Series. Application for Type Certificate dated January 11, 1971. Type Certificate No. A24CE issued December 14, 1973, obtained by manufacturer under delegation option procedures. Additional requirements for Collins Proline 21 Avionics Installation; Special Conditions 23-131-SC, and Equivalent Level of Safety ACE-02-16 for FAR 23.1305c(2), 23.1305(a)(2)(3), and 23.1549(a)(b)(c)(d), for direct reading digital only displays for oil pressure, oil temperature and fuel flow; FAR Hawker Beechcraft Corporation FAA Approved Model List (AML) 9709 E. Central Honeywell Cabin Pre ssure Outflow and Safety Valves Wichita, KS 67206 STC # SA10953SC Document No. HBSAPD90008 FAA Approved Date: Page 4 of 9 Revision 2.0 23.1547(e) as amended by Amendment 23-20; FAR 23.603(b) as amended by Amendment 23-23; FAR 23.1309(a), 23.1323(b), 23.1431(b) as amended by Amendment 23-49 as specified in Type Certificate Data Sheet A24CE, Revision 99. For the Models B200 and B200C: 14 CFR Part 23.1529 as amended by Amendment 23-26. Effective Serial Numbers for the B200, BB-1978, BB- 1988 and after and for the B200C, BL- 152 and after. Additional requirements for the Collins IFIS Installation: 23.771(a)(1) as amended by Amendment 23-14; 23.1501 and 23.1541(a)(b) as amended by Amendment 23-21; 23.603, 23.605(a) as amended by Amendment 23-23; 23.1322, 23.1357(c)(d) as amended by Amendment 23-43; 23.305. 23.321, 23.613 as amended by Amendment 23- 45; 23.301, 23.337, 23.571, 23.575, 23.607, 23.611 as amended by Amendment 23-48; 23.1309(b)(c)(e), 23.1311(a)(2)(3), 23.1321(e), 23,1351(e), 23.1351(a)(2)(i), 23.1359(c), 23.1365(a)(d)(e), 23.1431(a) as amended by Amendment 23-49; 23.1555(a), 23.1581(a), 23.1583(h), 23.1585(j) as amended by Amendment 23-50; and 23.777(a)(b) as amended by Amendment 23-51. Effective at Serial Numbers for the B200, BB-1978 and BB- 1988 and after and for the B200C, BL- 152 and after as specified in Type Certificate Data Sheet A24CE, Revision 99. 23.1309(c)(d) as amended by Amendment 23-49 (Electrical Only) Effective at Serial Numbers for the B200, BB-2001 and after and for the B200C, BL-152 and after. For the Models B200GT and B200CGT: Additional requirements for the Models B200GT (S/N BY-1 and after) and B200CGT, (S/N BZ-1 and after): 14 CFR Hawker Beechcraft Corporation FAA Approved Model List (AML) 9709 E. Central Honeywell Cabin Pre ssure Outflow and Safety Valves Wichita, KS 67206 STC # SA10953SC Document No. HBSAPD90008 FAA Approved Date: Page 5 of 9 Revision 2.0 Part 23-1529 as amended by Amendment 23-26; 23.939 as amended by Amendment 23-42; 23.1351(a)(2)(i) as amended by Amendment 23-49. 14 CFR Part 34 through Amendment 34-3; 14 CFR Part 36 through Amendment 36- 20. 23.1309(c)(d) as amended by Amendment 23-49 (Electrical Only) Effective at Serial Numbers for the B200GT, BY-32, BY-36 and after and for the B200CGT, BZ-1 and after Hawker Beechcraft Corporation B300; B300C A24CE, Rev 99 FAR Part 23 effective February 1, 1965, as amended by Amendments 23-1 through 23-34; FAR Part 36 effective December 1, 1969, as amended by Amendment 36-1 through 36-15; SFAR 27 effective February 1, 1974, as amended by Amendments 27-1 through 27-6 and Exemption No. 5077 from compliance with Section 23.207(c). Special Conditions 23-ACE-48A effective August 13, 1990, apply to Electronic Flight Instrument System (EFIS) equipped airplanes. FAR 23 Sections 23.201, 23.203 and 23.205 through amendment 23-45 (S/N FN-1 and up only).as specified in Type Certificate Data Sheet A24CE, Revision 99. Effective January 20, 1994, FAR 23.1457 as amended by Amendment 23.35. Exemption 5599 from compliance with 23.53(c)(1), for use of ground minimum control speed (Vmcg) for determination of takeoff decision speed (V1), (Serials FL-111, FM-9, FN-2 and after, or prior airplanes modified by Beech Kit No. 130- 3004). Compliance with ice protection has been demonstrated in accordance with FAR 23.1419 when ice protection equipment is installed in accordance with the Equipment List. Equivalent Safety Findings: FAR 23.781(b) for shape of the propeller control knob; FAR 23.1305(g) for use of Hawker Beechcraft Corporation FAA Approved Model List (AML) 9709 E. Central Honeywell Cabin Pre ssure Outflow and Safety Valves Wichita, KS 67206 STC # SA10953SC Document No. HBSAPD90008 FAA Approved Date: Page 6 of 9 Revision 2.0 fuel low pressure warning annunciators in lieu of the fuel pressure indicators; FAR 23.1321(d) for the basic "T" instrument panel arrangement. Does Not Apply to Proline 21 Equipped Aircraft. Additional requirements for Collins Proline 21 Avionics Installation; Special Conditions 23-131-SC, and Equivalent Level of Safety ACE-02-17 for FAR 23.1305(c)(2), 23.1305 (a)(2)(3), and 23.1549(a)(b)(c)(d), for direct reading only displays for oil pressure, oil temperature, and fuel flow; FAR 23.301(a) as amended by Amendment 23-42; FAR 23.1322(a)(b)(c)(d)(e), 23.1331(a)(b)(c), 23.1357(a)(b)(c)(d) as amended by Amendment 23-43; FAR23.305(a)(b), 23.397(a)(b), 23.613(a)(b)(c)(d)(e), 23.672(a)(b)(c), 23.1525, 23.1549(a)(b)(c)(d) as amended by Amendment 23-45; FAR 23.561(a)(b), 23.607(a)(b)(c), 23.611 as amended by Amendment 23-48; FAR 23.677(a)(b)(c)(d), 23.867(a)(b), 23.1303 (a)(b)(c)(d)(e)(f), 23.1309(a)(b)(c)(d)(e), 23.1311(a)(b), 23.1321(a)(b)(c)(d)(e), 23.1323(a)(b)(c)(e), 23.1329(a)(b)(d)(e)(f)(g)(h), 23.1351(a)(c), 23.1353(h), 23.1359(c), 23.1365(d)(e), 23.1431(a)(b)(d)(e) as amended by Amendment 23-49; FAR 23.1325(a)(b), 23.1545(a)(b)(c), 23.1583(h), 23.1585(a) as amended by Amendment 23-50; FAR 23.777(a)(b) an amended by Amendment 23-51; 23.1305(a)(c)(e) as amended by Amendment 23-52. Additional requirements for the Collins IFIS Installation: 23.321 as amended by Amendment 23-45; 23.337, 23.574, 23,575 as amended by Amendment 23- 48; 23.1365(a) as amended by Amendment 23-49; 23.1555(a), 23.1581(a), 23.1583(j) as amended by Amendment 23-50; Effective at Serial Numbers for the B300, FL-538 and FL- 544 and after and for the B300C, FM-15 and after Hawker Beechcraft Corporation FAA Approved Model List (AML) 9709 E. Central Honeywell Cabin Pre ssure Outflow and Safety Valves Wichita, KS 67206 STC # SA10953SC Document No. HBSAPD90008 FAA Approved Date: Page 7 of 9 Revision 2.0 SECTION III – Approved Model List: Aircraft Make Aircraft Model Type Certificate Data Sheet (TCDS) Required Approved Data and Added Model Specific Limitations AML Amendment Date Hawker Beechcraft Corporation C90A 3A20, Rev 67 Master Document List: RAS230600900 Instructions for Continued Airworthiness: RAS230600914 Equipment Configuration: Honeywell 103648-16 Cabin Pressure Outflow and Safety Valves Additional Limitations: There are no airworthiness limitations on the replacement Outflow Valve installed by this STC Additional Documents: None Hawker Beechcraft Corporation C90GT 3A20, Rev 67 Master Document List: RAS230600900 Instructions for Continued Airworthiness: RAS230600914 Equipment Configuration: Honeywell 103648-16 Cabin Pressure Outflow and Safety Valves Additional Limitations: There are no airworthiness limitations on the replacement Outflow Valve installed by this STC Additional Documents: None Hawker Beechcraft Corporation C90GTi 3A20, Rev 67 Master Document List: RAS230600900 Instructions for Continued Airworthiness: RAS230600914 Equipment Configuration: Honeywell 103648-16 Cabin Pressure Outflow and Safety Valves Additional Limitations: There are no airworthiness limitations on the replacement Outflow Valve installed by this STC Additional Documents: None Hawker Beechcraft Corporation B200 A24CE, Rev 99 Master Document List: RAS230600900 Instructions for Continued Airworthiness: **RAS230600934** Hawker Beechcraft Corporation FAA Approved Model List (AML) 9709 E. Central Honeywell Cabin Pre ssure Outflow and Safety Valves Wichita, KS 67206 STC # SA10953SC Document No. HBSAPD90008 FAA Approved Date: Page 8 of 9 Revision 2.0 Equipment Configuration: Honeywell 103648-17 Cabin Pressure Outflow and Safety Valves Additional Limitations: There are no airworthiness limitations on the replacement Outflow Valve installed by this STC Additional Documents: None Hawker Beechcraft Corporation B200C A24CE, Rev 99 Master Document List: RAS230600900 Instructions for Continued Airworthiness: RAS230600934 Equipment Configuration: Honeywell 103648-17 Cabin Pressure Outflow and Safety Valves Additional Limitations: There are no airworthiness limitations on the replacement Outflow Valve installed by this STC Additional Documents: None Hawker Beechcraft Corporation B200GT A24CE, Rev 99 Master Document List: RAS230600900 Instructions for Continued Airworthiness: RAS230600934 Equipment Configuration: Honeywell 103648-17 Cabin Pressure Outflow and Safety Valves Additional Limitations: There are no airworthiness limitations on the replacement Outflow Valve installed by this STC Additional Documents: None Hawker Beechcraft Corporation B200CGT A24CE, Rev 99 Master Document List: RAS230600900 Instructions for Continued Airworthiness: RAS230600934 Equipment Configuration: Honeywell 103648-17 Cabin Pressure Outflow and Safety Valves Additional Limitations: There are no airworthiness limitations on the replacement Outflow Valve installed by this STC Additional Documents: None Hawker Beechcraft B300 A24CE, Rev 99 Master Document List: RAS230600900 Instructions for Continued Hawker Beechcraft Corporation FAA Approved Model List (AML) 9709 E. Central Honeywell Cabin Pre ssure Outflow and Safety Valves Wichita, KS 67206 STC # SA10953SC Document No. HBSAPD90008 FAA Approved Date: Page 9 of 9 Revision 2.0 Corporation Airworthiness: RAS230600934 Equipment Configuration: Honeywell 103648-18 Cabin Pressure Outflow and 103648-19 Safety Valves Additional Limitations: There are no airworthiness limitations on the replacement Outflow Valve installed by this STC Additional Documents: None Hawker Beechcraft Corporation B300C A24CE, Rev 99 Master Document List: RAS230600900 Instructions for Continued Airworthiness: RAS230600914 Equipment Configuration: Honeywell 103648-18 Cabin Pressure Outflow and 103648-19 Safety Valves Additional Limitations: There are no airworthiness limitations on the replacement Outflow Valve installed by this STC Additional Documents: None ## Every issue (2) - December 12, 2016: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/18/e8/18e8fa40bb1e62443755943b6c995a06b69fac601071cb1ca4c1a51c8b45709d), [SA10953SC AML.pdf](https://openairdocs.org/files/sha256/dc/d2/dcd2259de860c666b0e9d26a883c71a9f7b87ac0b9453b81550fa19321bcc327) - October 5, 2010: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/ba/95/ba95dc1b35a22b541aa19baf58981769544cc008b5b59a96ace213a01bcb829a), [SA10953SC AML.pdf](https://openairdocs.org/files/sha256/dc/d2/dcd2259de860c666b0e9d26a883c71a9f7b87ac0b9453b81550fa19321bcc327) --- 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.