# STC ST00322SE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: LifePort LLC, United States
- Description: Installation of emergency medical stretcher, oxygen, and electrical systems.
- Applied: October 5, 1995
- Status date: May 10, 2019
- Product: Aircraft, Large Airplane
- Certification basis: Part 21, Part 25
- Data sheets: [TCDS A16SW](https://openairdocs.org/tcds/A16SW)
- Certificate PDF: https://openairdocs.org/files/sha256/44/c0/44c09c66ee30e25e8e291aab5e0c80e2bb0e274eeb4eb2cd0c84a2176c099dc9
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/D1A3EAE058AF5FE1862585EA00647B79.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/ST00322SE

## ADs that name it (0)

None.

## Approved models (1)

- Raytheon Aircraft Company 400A ([TCDS A16SW](https://openairdocs.org/tcds/A16SW))

## 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.

Number ST00322SE

This certificate, issued to LifePort, LLC 1610 Heritage Street Woodland, WA 98674

Part 25 of the Federal Aviation Regulations.

Original ProductType Certificate Number: A16SW Make: Beech Model: 400A, Serial Number RK-24 and up Description of the Type Design Change: Installation of emergency medical stretcher, oxygen, and electrical systems in accordance with LifePort, Inc. Master Drawing List No. 520-4100, Revision L, dated January 29, 1998, or later Federal Aviation Administration (FAA) approved revision. Inspection of the emergency medical oxygen and electrical systems in accordance with section 7.0 of LifePort, Inc. Report No. EGR -387, Revision D, dated February 23, 1998, or later FAA approved revision.

NOTE: The aircraft electrical installation is limited to certain serial number aircraft. See the latest FAA approved revision of Drawing 300-2255 for eligible aircraft.

Limitations and Conditions: 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 model series on which other previously approved modification are incorporated unless the installer determines that the relationship between this change and any other previously incorporated 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 Flight Manual Supplement (FMS) No. 40, Revision A, or later FAA approved revision, must be included in the permanent records of the modified aircraft.

If the holder agree 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: October 5, 1995 Date reissued: May 10, 2019 Date of issuance: March 27, 1996 Date amended: March 2, 1998; June 28, 1999

FAA FORM 8110-2 (5/14) PAGE 1 OF 2 PAGES By direction of the Administrator

(Signature)

Acting Manager, Seattle ACO Branch (Title)

Transfer the ownership of Supplemental Type Certificate Number

to (Name of Transferee)

(Address of Transferee)

(Number and Street)

(City, State, and ZIP Code)

from (Name of Grantor) (Print or Type)

(Address of Grantor)

(Number and Street)

(City, State, and ZIP Code)

Signature of Grantor (In Ink):

U.S. GPO: 1987-763-289

## Every issue (2)

- May 10, 2019: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/44/c0/44c09c66ee30e25e8e291aab5e0c80e2bb0e274eeb4eb2cd0c84a2176c099dc9)
- June 28, 1999: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/77/3e/773e5e30028f380cb37ce791068a6ed3617f125bf7944954895b6e695f21d420)

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