# STC SA01105SE

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Metzger James R, United States
- Description: Installation of two (2) Hartzell Model HC-B3Z20-2A/10151(B)-8(R), or two (2) HC-93Z20-2C/10151(B)-8(R) propellers on the above model aircraft, per James Metzger s Document JM0001, Revision A, dated January 10, 2000, or later FAA approved revision.
- Applied: June 8, 2000
- Status date: June 24, 2004
- Product: Aircraft, Small Multi-Engine
- Certification basis: Part 3, Part 21
- Data sheets: [TCDS 6A1](https://openairdocs.org/tcds/6A1)
- Certificate PDF: https://openairdocs.org/files/sha256/ba/0d/ba0d7aa8e311a8047139fc3c0ea458b5685778634b3a93db32fc040db407f667
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/00C2086243FA159686256EE500562BCB.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA01105SE

## ADs that name it (0)

None.

## Approved models (2)

- Twin Commander Aircraft Corporation 560-A ([TCDS 6A1](https://openairdocs.org/tcds/6A1))
- Twin Commander Aircraft Corporation 560-E ([TCDS 6A1](https://openairdocs.org/tcds/6A1))

## 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.

United States of America Department of Transportation_Federal Aviation Administration Supplemental Type Certificate Number SA01105SE

This certificate, issued to: James R. Metzger 38205 SW 70th Washougal, WA 98671

Part 3 of the Civil Air Regulations.

Original ProductType Certificate Number: 6A1 Make: Twin Commander Model: 560A with 2 Lycoming GO-480-C1B6, or 2 Lycoming GO-480-G1B6 engines installed, and 560E

Description of the Type Design Change: Installation of two (2) Hartzell Model HC-B3Z20-2A/10151(B)-8(R), or two (2) HC-93Z20-2C/10151(B)-8(R) propellers on the above model aircraft, per James Metzger’s Document JM0001, Revision A, dated January 10, 2000, or later FAA approved revision.

Limitations and Conditions: Second segment climb performance must use the alternate climb power setting given in the Aircraft Flight Manual, which is:

258 BHP-2750 Engine RPM/1765 Prop RPM

Approval of this change in type design applies to the above model aircraft only. This approval should not be extended to other aircraft of these models on which other previously approved modifications are incorporated unless it is determined by the installer that the relationship between this change and any of those other previously approved modifications, including changes in type design, will introduce no adverse effect upon the airworthiness of that aircraft. A copy of this Certificate and FAA approved Aircraft Flight Manual Supplement, dated July 12, 2002, or later FAA approved revision, must be maintained as part of the permanent records for the modified aircraft.

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.

Date of application: June 8, 2000 Date reissued:

Date of issuance July 12, 2002 Date amended: 2/18/00; 6/24/04

(Signature)

Acting Manager, Seattle Aircraft Certification Office (Title)

## Every issue (1)

- June 24, 2004: Amended, Current. [certificate](https://openairdocs.org/files/sha256/ba/0d/ba0d7aa8e311a8047139fc3c0ea458b5685778634b3a93db32fc040db407f667)

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