# STC SH588SW - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Scott's Bell 47 Inc - Description: Conversion to single-place cabin, without doors, revised cyclic and collective and throttle controls, rerouted electrical wiring. - Status date: August 7, 2014 - Data sheets: H-1, H-1 - Certificate PDF: https://openairdocs.org/files/sha256/88/56/88563e197812bdf3b288960572220fb95ece875c0967f370fedfca0377bed28b - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/B3298616ED4685E186257DC70066B3FB.0001 - Page: https://openairdocs.org/stc/SH588SW ## ADs that name it None. ## Approved models (2) - Scotts-Bell 47 Inc 47D1 (TCDS H-1) - Scotts-Bell 47 Inc 47G-2 (TCDS H-1) ## 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 6 of the Civil Air R egulations. (See page 3 for complete certification basis). Original Product --Type Certificate N umber : Conversion to single-place cabin, without doors, revised cyclic and collective and throttle controls, rerouted electrical wiring according to Conversion Instructions for Installing Mini Cabin dated June 19, 1968, and K Copters Drawing List FAA Approved on January 6, 1970, and Drawings K5C9, K5C13, K5P-1 dated January 7, 1970, approved January 8,1970, for Bell model 47D1; and according to Conversion Instructions dated December 18, 1970, and Drawing List, Revision B, dated 1/11/71 or later FAA approved revision. This certificate and the supporting data, which is the basis for approval, shall remain in effect until surrendered, suspended, revoked or a termination date is otherwise establ ished by the A dministrator of the F ederal A viation A dministration. Scott’s-Bell 47, Inc. 100 Minnesota Avenue Le Sueur, MN 56058 H-1 M ake : Bell Helicopter Textron M odel : 47D1, 47G-2 Date reissued : 3/4/86; 7/27/87; 4/30/04; 12/15/10; 8/7/14 Date amended : 1/8/70; 1/8/71; 11/22/74 Rev. 3 B y direction of the A dministrator Original Signed By: Gregory J. Michalik for (Signature) Karol Mordasiewicz Manager, Airframe and Administrative Branch Chicago Aircraft Certification Office (Title) Date of application : October 26, 1965 Date of issuance : January 07, 1966 FAA FORM 8110-2-1(10-69) PAGE 2 of 3 PAGES N umber SH588SW FAA FORM 8110-2-1(10-69) PAGE 3 of 3 PAGES Number SH588SW Date of Issuance: January 07, 1966 Date of Reissuance: August 7, 2014 Limitations and Conditions: Limitations and Conditions for Bell Model 47D1: 1. STC SH283SW and Bell 200 horsepower conversion Bell S.I. 150SI and P/N 47-670-030-1 oil cooler installations are required in conjunction with this modification. 2. STC SH752SW required when Lycoming engine is installed. 3. The following FAA Approved Helicopter Flight Manual Supplements are required: a. Dated 1/7/66 for Serial No. T558, Red. No. N6323X. b. Supplement “A” dated 6/28/68 with Franklin 178 h.p. engine. c. Supplement “B” dated 6/28/68 with Franklin 200 h.p. engine. d. Dated 1/31/67 with Lycoming VO-435 A1A, A1B, A1C, or A1D 200 h.p. engine. e. Dated 6/28/68 with Lycoming VO-435 A1A, A1B, A1C, or A1D 178 h.p. engine. f. Dated 1/8/70 with hydraulic boosted flight controls installed according to STC SH397SW. Limitations and Conditions for Bell Model 47G-2: 4. For Bell Model 47G-2 FAA Approved Helicopter Flight Manual Supplement dated 1/8/71 required. 5. Approval is for normal category only for Bell Model 47G-2. 6. The installer must determine whether this design change is compatible with previously approved modification. 7. 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. ------------End----------- ## Every issue (2) - August 7, 2014: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/88/56/88563e197812bdf3b288960572220fb95ece875c0967f370fedfca0377bed28b) - December 15, 2010: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/4f/b5/4fb5baf33eecfe2f56f4b774b3ccfed2958c4cc75442c3f79bc6f3327333fe27) --- From OpenAirDocs.org, an independent open copy of FAA data. Only the Federal Register edition on govinfo.gov is the official legal text of an AD.