# STC SA1691GL - Type: Supplemental type certificate - Status: Current, Reissued - Holder: D'Shannon Products Ltd. - Description: Installation of McCauley Propeller Model 3A34C423/90DFA-10 in accordance with D Shannon Drawing No. 533420, Revision C, dated October 26, 1991, or later FAA Approved revision. - Status date: June 17, 2011 - Data sheets: 3A15, 3A15, 3A15, 3A15, 3A15, 3A15, 3A15, 3A15, 3A15, 3A15, 3A15, 3A15, 3A15, 3A15 - Certificate PDF: https://openairdocs.org/files/sha256/93/64/936482fcffc48b9126644594e237023b561e5df04e4e2031b4810bf2b9a7d1b2 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/C854D067EAEF892B8625792C00573273.0001 - Page: https://openairdocs.org/stc/SA1691GL ## ADs that name it None. ## Approved models (14) - 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 E33 (TCDS 3A15) - Hawker Beechcraft Corporation F33 (TCDS 3A15) - Hawker Beechcraft Corporation G33 (TCDS 3A15) - 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) ## 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 8110-2-1(10-69) PAGE 1 of 3 PAGES Number SA1691GL This certificate issued to Part 3 of the Civil Air Regulations. ( See Type Certificate Data Sheet 3A15 for complete certification basis) Installation of McCauley Propeller Model 3A34C423/90DFA-10 in accordan ce with D’Shannon Drawing No. 533420, Revision C, dated October 26, 1991, or later FAA Approved revision. 1. 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 any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of that aircraft. 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 established by the Administrator of the Federal Aviation Administration. D’Shannon Products, Ltd. 1309 County Road 134 Buffalo, MN 55313 3A15 Make : Beech Model : E33, F33, G33, 35-33, 35-A33, 35-B33, 35-C33, H35, J35, K35, M35, N35, P35 Date reissued : March 15, 2011, June 17, 2011 By direction of the Administrator Original Signed By: Timothy Smyth ( Signature) Timothy Smyth Manager, Propulsion Branch Chicago Aircraft Certification Office ( Title) Date of application: October 26, 1991 Date of issuance : January 14, 1992 Date of Issuance: January 14, 1992 Limitations and Conditions: (Continued from Page 1 of 3) 2. FAA-Approved Airplane Flight Manual Supplement for Beech Model Aircraft H35; N35, P35, or G33; J35, K35, or M35; and 35-33, 35-A33, 35-B33, 35-C33, E33, F33, all dated December 26, 1991 or later FAA-Approved revisions are required.3. Aircraft specifications are the same listed on Type Certificate Data Sheet No. 3A15, except as follows: Propeller and Propeller Limits McCauley 3A34C423 hub with 90DFA-10 blades Diameter: 80 to 78 inches Teledyne Takeoff & Propeller Continental Maximum Pitch Setting Beech Motors Combustion Continuous (at 30’ station) Aircraft Engine Damper Ratio HP RPM Low High ( ± 0 . 2 °) (±0.5 °) 35-33, -A33, -B33 IO-470-J, -K 1-5, 1-6 7:1 225 2600 8.8° 29.0° 35-C33 IO-470-K 1-5, 1-6 7:1 225 2600 8.8° 29.0° E33, F33 IO-470-K 1-5, 1-6 7:1 225 2600 8.8° 29.0° G33, N35, P35 IO-470-N 4-6 8.6:1 260 2625 11.8° 29.0° J35, K35, M35 IO-470-C 4-6 8:1 250 2600 11.0° 29.0° H35 O-470-G 1-6.5, 1-9 8.1 240 2600 10.0° 29.0° 3. 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. …END… ## Every issue (2) - June 17, 2011: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/93/64/936482fcffc48b9126644594e237023b561e5df04e4e2031b4810bf2b9a7d1b2) - March 15, 2011: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/b3/d3/b3d3c3caf55034e17c76096ef5805eda9278352d502cc607ba1b096356cc3911) --- 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.