# STC SA10071SC

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Sabreliner Aviation LLC
- Description: Installation of General Electric engine with Avia propeller
- Status date: March 3, 2020
- Data sheets: 3A20, 3A20, 3A20, 3A20, 3A20
- Certificate PDF: https://openairdocs.org/files/sha256/37/a3/37a3b64b113a943ed18e537a8cea74da86bbffcdb2e44854b2300845352643b3
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/341F9257D48797988625853600558773.0001
- Page: https://openairdocs.org/stc/SA10071SC

## ADs that name it

None.

## Approved models (5)

- Beechcraft Corporation 65-90 (TCDS 3A20)
- Beechcraft Corporation 65-A90 (TCDS 3A20)
- Beechcraft Corporation B90 (TCDS 3A20)
- Beechcraft Corporation C90 (TCDS 3A20)
- Beechcraft Corporation E90 (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 This certificate issued to:

Part of the Original Product – Type Certificate Number: Make:

By Direction of the Administrator Signature Title SA10071SC Sabreliner Aviation, LLC 6 Trautman Industrial Drive Sainte Genevieve, MO 63670 3 Civil Air Regulations.

Beechcraft Corporation 65-90, 65-A90, B90, C90, E90 3 3A20

1. Installation of General Electric M601E-11 engine for 65-90, 65-A90, B90 and C90, with Avia 5-blade propeller model V510, in accordance with LoneStar Propjets Drawing List No. DLKA90, Rev. G, dated 7/15/2003, or later FAA Approved revision.

2. Installation of General Electric M601E-11A or M601E-11AS engine for C90 and E90, with Avia V510 Propeller, in accordance with LoneStar Propjets Installation Manual No. 90-200, Rev. G, dated 6/11/2013, or later FAA Approved Revision.

1. For 65-90, 65-A90, B90 and C90 with General Electric M601E-11 engine, FAA approved Flight Manual Supplement, dated 10/4/2002, or later FAA approved revision is required.

2. For C90 with General Electric M601E-11AS engine, follow STC SA10219SC for Instruction for Continued Airworthiness and FAA approved Flight Manual Supplement.

(See Continuation Sheet page 3) 12/19/2001 5/11/2011, 5/24/2011, 12/30/2014, 3/3/2020 10/4/2002 9/20/2011, 10/23/2012, 5/29/2013, 3/13/2014 Grant Youngdahl Program Manager Wichita ACO Branch

FAA Form 8110-2 (5/14) Page 2 of

To (Name and address of transferee) From (Name and address of grantor) Extent of Authority (if licensing agreement):

SA10071SC 3

FAA Form 8110-2 (5/14) Page 3 of

Description of Type Design Changes (Continued):

3. Installation of General Electric M601E-11AS engine for C90 must also install STC SA10219SC.

4. Installation of General Electric H80 engine for C90 and E90, with Avia V510 Propeller and optional Maximum Takeoff Gross Weight (MTOGW) change in accordance with Lonestar Propjets Installation Manual No. 90-200, Rev. G, dated 6/11/2013 or later FAA approved revision.

3. For C90 and E90 with General Electric M601E-11A and H80 engines, including MTOGW change option, the LoneStar Propjets Flight Manual Supplement No. 90-100, Rev. F, dated 2/21/2014, and LoneStar Propjets Instructions for Continued Airworthiness, No. 90-E5, Rev. E, dated 9/12/2012, or later FAA approved revisions are required.

4. For C90 and E90 with General Electric M601E-11A and H80 engines and MTOGW change option, the installation of lower aft fuselage strakes per STC SA4010NM is required.

5. Compatibility of this design change with previously approved modifications must be determined by the installer.

6. 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 ------ SA10071SC 3

## Every issue (6)

- March 3, 2020: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/37/a3/37a3b64b113a943ed18e537a8cea74da86bbffcdb2e44854b2300845352643b3)
- December 30, 2014: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/d7/72/d772828414d1170890aaf591287f9d8ff244a2505ac30a73d7dc42b32fbb2fa4)
- March 13, 2014: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/b4/c3/b4c329a29ebb2b426883bd794bb615acf0ffc1fe1dacc396f7f5d6cc049fe407)
- May 29, 2013: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/61/59/615932fb68672f74510a718be2e50523e72c11c310457828a3fe0dd5126edc56)
- October 23, 2012: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/90/a6/90a61817f7566f82af7dfa4ddaf52c6ff76cb0658866093050d4c75743b66e55)
- May 24, 2011: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/79/06/7906f9f3a383fdb7847868a0b3dd63386b71cc8a30f388cbd87caddbc350e03d)

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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.