# STC SA10463SC

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Sky International Inc
- Description: Installation of Lycoming Engines Model IO-360-A1D6 engine and an MT Propeller Model MTV-15-B/205-58.
- Status date: December 14, 2005
- Data sheets: A22NM
- Certificate PDF: https://openairdocs.org/files/sha256/6b/3b/6b3bc80ce18bd35911d1c3d42a1b76041d3cd10f561c5b0d38e33c30758955c5
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/8C1897437CC9E115862571F50064D919.0001
- Page: https://openairdocs.org/stc/SA10463SC

## ADs that name it

None.

## Approved models (1)

- Sky International Inc. A-1B (TCDS A22NM)

## 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.

672 S. Washington Afton, WY 83110

Part 23 of the Federal Aviation Regulations.

Original Product Type Certificate Number : A22NM Make : Sky International, Inc.

Model : A-1B Husky

Installation of a Lycoming Engines Model IO-360-A1D6 engine and an MT Propeller Model MTV-15-B/205-58 in accordance with Alamo Aerospace Master Drawing List No. 1100, Rev. B, dated September 1, 2005, or later FAA approved revision and Alamo Aerospace Installation Instructions No. 1101, Rev. B, dated September 1, 2005 or later FAA approved revision. Airplane Flight Manual Supplement, dated September 26, 2005, or later FAA approved revision is required.

Date of application : October 06, 2004

Date of issuance : September 27, 2005 Date reissued : December 14, 2005

( Signature) S. Frances Cox, Manager Special Certification Office, Southwest Region

(Title)

FAA Form 8110-2-1(10-69) Page 2 of 2

Number SA10463SC Date of Issuance: September 27, 2005 Reissuance Date: December 14, 2005

The MT Propeller Model MTV-15-B/205-58 propeller diameter limits are 80.7 to

79.7 inches. The minimum tire size is 8.50 x 6 inch with a minimum tire pressure of 25 psi. The max continuous power is limited to engine RPM of 2650.

Instructions for Continued Airworthiness dated August 12, 2005 is required.

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

- December 14, 2005: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/6b/3b/6b3bc80ce18bd35911d1c3d42a1b76041d3cd10f561c5b0d38e33c30758955c5)
- September 27, 2005: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/ae/ca/aecae5643fdac6bef32a0ca948495815db9b73b2c5d920b575447a90e34c1634)

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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.