# STC SA2200SW - Type: Supplemental type certificate - Status: Current, Reissued - Holder: D'Shannon Products Ltd. - Description: Installation of Teledyne Continental IO-520-B, -BA, - BB or IO-550-B engine and applicable McCauley Propeller only as listed on STC. - Status date: March 23, 2009 - Data sheets: 3A15, 3A15, 3A15, 3A15, 3A15, 3A15, 3A15, 3A15, 3A15, 3A15, 3A15, 3A15, 3A15, 3A15, 3A15, 3A15, 3A15, 3A15, 3A15, 3A15, 3A15, 3A15, 3A15, 3A15, A-777, A-777, A-777, A-777, A-777, A-777, A-777 - Certificate PDF: https://openairdocs.org/files/sha256/b3/dd/b3ddbc5d058d899815b957fa63341f2d03b254364632221b1dd22333eaf58c7a - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/714C792048CCCCEB862575990068A28D.0001 - Page: https://openairdocs.org/stc/SA2200SW ## ADs that name it None. ## Approved models (31) - Hawker Beechcraft Corporation 35-33 (TCDS 3A15) - Hawker Beechcraft Corporation 35-A33 (TCDS 3A15) - Hawker Beechcraft Corporation 35-B33 (TCDS 3A15) - Hawker Beechcraft Corporation 35-C33 (TCDS 3A15) - Hawker Beechcraft Corporation 35-C33A (TCDS 3A15) - Hawker Beechcraft Corporation 36 (TCDS 3A15) - Hawker Beechcraft Corporation A35 (TCDS A-777) - Hawker Beechcraft Corporation A36 (TCDS 3A15) - Hawker Beechcraft Corporation B35 (TCDS A-777) - Hawker Beechcraft Corporation C35 (TCDS A-777) - Hawker Beechcraft Corporation D35 (TCDS A-777) - Hawker Beechcraft Corporation E33 (TCDS 3A15) - Hawker Beechcraft Corporation E33A (TCDS 3A15) - Hawker Beechcraft Corporation E33C (TCDS 3A15) - Hawker Beechcraft Corporation E35 (TCDS A-777) - Hawker Beechcraft Corporation F33 (TCDS 3A15) - Hawker Beechcraft Corporation F33A (TCDS 3A15) - Hawker Beechcraft Corporation F33C (TCDS 3A15) - Hawker Beechcraft Corporation F35 (TCDS A-777) - Hawker Beechcraft Corporation G33 (TCDS 3A15) - Hawker Beechcraft Corporation G35 (TCDS A-777) - Hawker Beechcraft Corporation H35 (TCDS 3A15) - Hawker Beechcraft Corporation J35 (TCDS 3A15) - Hawker Beechcraft Corporation K35 (TCDS 3A15) - Hawker Beechcraft Corporation M35 (TCDS 3A15) - Hawker Beechcraft Corporation N35 (TCDS 3A15) - Hawker Beechcraft Corporation P35 (TCDS 3A15) - Hawker Beechcraft Corporation S35 (TCDS 3A15) - Hawker Beechcraft Corporation V35 (TCDS 3A15) - Hawker Beechcraft Corporation V35A (TCDS 3A15) - Hawker Beechcraft Corporation V35B (TCDS 3A15) ## 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. Part 3 of the Civil Air Regulations. (See Aircraft Specification No. A-777 or 3A15, as applicable for complete certification basis). Original Product--Type Certificate Number: A-777, 3A15 Make: Hawker Beechcraft Model: A35, B35, C35, D35, E35, F35, G35, H35, J35, K35, M35, 35-33, N35, 35-A33, 35-B33, P35, S35, 35-C33, 35-C33A, E33, F33, V35, V35A, V35B, E33A, E33C, 36, A36, F33A, F33C, G33. D’Shannon Products, Ltd. 1309 County Road 134 Buffalo, MN 55313 Description of Type Design Change: Teledyne Continental Motor (TCM) Engine/Propeller Models Installation Eligibility Chart: Engin e Maker Engine Model Prop Maker Prop Model Prop Maker Prop Model TCM IO-520 McCauley 2A36C23/84B-0 Ha rtzell PHC-(C,L)3YF-1RF/F8468A(B,K)-6R -B, 2A37C223/90RB-6 PHC-C3YF-1RF/C8468-6R -BA, 3A32C76/82NB-2 HC-C3YF-1/8468A-6R -BB 3A32C406/82NDB-2 PHC-C3YF-1RF/F7691 TCM IO-550 McCauley 3A32C76/82NB-2 Ha rtzell PHC-(C,L)3YF-1RF/F8468A(B,K)-6R -B 3A32C406/82NDB-2 HC-C4YF-1E/F7063()Q D3A32C409/82NDB-2 PHC-C3YF-1RF/F7691 Installation Instructions 71-20-00 dated 10/20/1988, or later FAA Approved Revision. See STC SA01561CH and SA01668CH for Hartzell PHC-(C,L)3YF-1RF/F8068(-2) eligibility. 1. Compatibility of this design change with previously approved modifications must be determined by the installer. 2. 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. 3. The following FAA Approved Flight Manual Supplements are required: Date reissued: 9/13/84; 1/31/86; 3/5/88; 3/23/09 Date amended: 8/10/81; 2/20/85; 9/21/90; 9/21/92; 11/20/92; 5/18/95; 10/20/95; 12/22/95; 6/12/96; 5/8/97; 5/31/01; 1/3/05 By direction of the Administrator Original Signed BY: Thaddeus D Krolicki, Jr. (Signature) Thaddeus D. Krolicki, Jr. Manager, Propulsion Branch Chicago Aircraft Certification Office (Title) Date of application: 8/23/74 Date of issuance: 9/5/75 FAA FORM 8110-2-1(10-69) PAGE 3 of 3 PAGES Number SA2200SW LIMITATIONS AND CONDITIONS (Continued) Date amended: 1/3/2005 Date reissued: 3/23/2009 Flight Manual Supplement, date Aircraft Model Hawker Beechcraft 6/23/1975 A35, B35 (IO-520-B, -BA, -BB) 9/5/1975 A35, B35, C35, D35, E35, F35, G35, H35, J35, K35, M35 (IO-520-B, -BA, -BB) 8/10/1981 A35, B35, C35, D35, E35, F35, G35, H35, J35, K35, M35, 35-33, 35-A33, 35-B33, 35-C33, E33, F33 (IO-520-B, -BA, -BB) McCauley C23 and C76 only. 12/19/1984 E-33A/TCM IO-550B (285 hp) C409 McCauley Only 2/20/1985 A35, B35, C35, D35, E35, F35, G35, H35, J35, K35, M35, N35, P35, 35-33, 35-A33, 35-B33, 35-C33, E33, F33, S35, V35, V35A, V35B, E33A, E33C, F33A, F33C, A36, 36/TCM IO-550-B (285 hp) C409 McCauley only Flight Manual Supplement, date Engine Maker/Model Power Prop. Maker Prop. Model 5/24/1989 TCM/IO-550-B 285 hp McCauley 3A32C76/82NB-2 3A32C406/82NDB-2 D3A32C409/82BDB-2 8/28/1990 TCM/IO-520-B, 285 hp McCauley 2A36C23/84B-0 -BA, -BB 3A32C76/82NB-2 3A32C406/82NDB-2 TCM/IO-550-B 300 hp McCauley 3A32C76/82NB-2 3A32C406/82NDB-2 D3A32C409/82NDB-2 9/18/92 TCM/IO-520-B, 285 hp McCauley 2A37C223/90RB-6 -BA, -BB Hartzell PHC-(C,L)3YF-1RF/F8468A(B,K)-6R PHC-C3YF-1RF/C8468-6R HC-C3YF-1/8468A-6R 11/20/92 TCM/IO-550-B 285 hp/ Hartze ll PHC-(C,L)3YF-1RF/F8468A(B,K)-6R 300 hp 7/27/95 TCM/IO-550-B 285 hp/ Hartzell HC-C4YF-1E/F7063()Q 300 hp 12/22/95 TCM/IO-520-B, -BA, -BB 285 hp Hartzell PHC-C3YF-1RF/F7691 TCM/IO-550-B 285 hp/ Hartzell PHC-C3YF-1RF/F7691 300 hp 4. Installation of Teledyne Continental IO-550-B aircraft engine must be derated to 285 H.P. on the applicable aircraft model unless engine mounts 35-910027-1, 35-910027-7, 35-910027-9, 35-910027-11, 35-910027-3, and 35-910027-5 are installed. 5. Aircraft equipped with canted front engine mounts No. 35-910027-11, 35-910027-9, and rear engine mounts No. 35-910027-5, 35-910027-3 or front engine mounts No. 35-910027-7, 35-910027-1 and rear engine mounts No. 35-910027-5, 35-910027-3 are eligible for optional D’Shannon Products Cooling Air Baffle Kit for indicated models when installed in accordance with D'Shannon Installation Instructions Document #DSP-IM95-1, rev. 6, dated April 16, 2002, and Drawing List BDS-DW-200A-01, revision 1, dated February 14, 1995, or later FAA approved revision. 6. Aircraft equipped with strai ght engine mounts No. 35-910018-1, 35-910018-2, and 35-910019(2), or 35-910018-3, 35-910018- 4, 35-910019-1, and 35-910019-3, are eligible for optional D’Shannon Products Cooling Air Baffle Kit for indicated models when installed in accordance with D'Shannon Installation Instructions Document #DSP-IM96-1, rev. 5, dated September 24, 2003, and Drawing List DW-200A-03, revision 3, dated February 11, 1997, or later FAA approved revision. 7. STC SA542WE engine cowl flap assembly is optional for Beech Models 35-33, 35-A33, 35-B33, 33-C33, E33, F33. Nose bowl air intake modifications called out on drawing 68B001 and 54-10-00 are optional on all 33 and 35 models. ...END... ## Every issue (1) - March 23, 2009: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/b3/dd/b3ddbc5d058d899815b957fa63341f2d03b254364632221b1dd22333eaf58c7a) --- From OpenAirDocs.org, an independent open copy of FAA data. 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