# STC SA01790SE

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: AeroMech Incorporated, United States
- Description: Group approval for Reduced Vertical Separation Minimum (RVSM)
- Applied: August 15, 2007
- Status date: September 20, 2007
- Product: Aircraft, Single-Engine
- Certification basis: Part 21, Part 23
- Data sheets: [TCDS A24CE](https://openairdocs.org/tcds/A24CE)
- Certificate PDF: https://openairdocs.org/files/sha256/02/0b/020bde7de5d0c8674ffdd86a5d01c89ee3fda3070fca390473e8086d619c3bb4
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/3B7A9FBFA4552E008625770B00551E7B.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA01790SE

## ADs that name it (0)

None.

## Approved models (12)

- Hawker Beechcraft Corporation 200 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation 200C ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation 300 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation 300LW ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation B200 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation B200C ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation B200C (C-12F) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation B200C (C-12R) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation B200C (UC-12F) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation B200C (UC-12M) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation B300 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation B300C (C-12W) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))

## 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 SA01790SE

This certificate, issued to AeroMech Incorporated 1616 Hewitt Avenue, Suite 312 Everett, WA 98201 Part 23 of the Federal Aviation Regulations.

Original Product⎯Type Certificate Number: A24CE (Revision 95) Make: Hawker Beechcraft Model: 200, 200C B200, B200C, 300, 300LW, B300, B300C

Description of the Type Design Change: Group approval for Reduced Vertical Separation Minimum (RVSM) in accordance with AeroMech Document No. AMI-QD-KAIR-0709, Rev. “NEW,” dated September 10, 2007, or later FAA approved revisions.

Limitations and Conditions: For Class 1 Airframes, Instructions for Initial and Continued Airworthiness, Document AMI-IICA-KAIR-0713, Rev. “New,” dated September 10, 2007, or later approved revision, is a required part of this STC.

The Airplane Flight Manual Supplement for the Class 1 airframes, AeroMech Document AMI-AFMS-KAIR-0718, Rev. “Original”, FAA Approved September 20, 2007, (or latest FAA-approved revision), is required on-board for operation of the aircraft.

Descriptive data pertaining to this design change are considered inadequate for duplication on other products.

This approval is limited to the Hawker Beechcraft Models 200, 200C, B200, B200C, 300, 300LW, B300, B300C aircraft only.

A copy of this certificate and FAA approved flight manual supplement must be maintained as part of the permanent records of the aircraft. If the holder agrees to permit another person to use this certificate, the holder shall give the other person written evidence of the permission.

Date of application: August 15, 2007 Date reissued:

Date of issuance: September 20, 2007 Date amended:

(Signature)

Acting Manager, Seattle Aircraft Certification Office (Title)

## Every issue (1)

- September 20, 2007: Issued, Current. [certificate](https://openairdocs.org/files/sha256/02/0b/020bde7de5d0c8674ffdd86a5d01c89ee3fda3070fca390473e8086d619c3bb4)

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