# STC SA00153SE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: LifePort LLC, United States
- Description: Installation of emergency medical stretcher, oxygen, and electrical systems.
- Applied: October 22, 1994
- Status date: May 10, 2019
- Product: Aircraft, Small Airplane
- Certification basis: Part 21, Part 23
- Data sheets: [TCDS A27CE](https://openairdocs.org/tcds/A27CE)
- Certificate PDF: https://openairdocs.org/files/sha256/fb/ce/fbce8e15b8fbe46b3bacb3923db192a546f79e66ba7bf728f1bdef5d3131f5a1
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/0B1292A5C42896EC862585D000425EA4.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA00153SE

## ADs that name it (0)

None.

## Approved models (2)

- The Cessna Aircraft Company 501 ([TCDS A27CE](https://openairdocs.org/tcds/A27CE))
- The Cessna Aircraft Company 551 ([TCDS A27CE](https://openairdocs.org/tcds/A27CE))

## 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 SA00153SE

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

Part 23 of the Federal Air Regulations.

Original ProductType Certificate Number: A27CE Make: Cessna Model: 501 and 551 Description of the Type Design Change: Installation of emergency medical stretcher, oxygen, and electrical systems in accordance with LifePort, Inc. Master Drawing List No. 520-5000, initial release, dated October 26, 1994, or later FAA approved revision.

NOTE: This installation includes provisions for mounting equipment in the cabin interior (via equipment sleds and arches). Equipment mounted on these provisions, which is not specified in t he above drawing package, requires separate FAA approval.

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 11, dated November 18, 1994, or later FAA approved revision, must be maintained as part of the permanent records for 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 22, 1994 Date reissued: May 10, 2019 Date of issuance: November 18, 1994 Date amended:

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/fb/ce/fbce8e15b8fbe46b3bacb3923db192a546f79e66ba7bf728f1bdef5d3131f5a1)
- November 18, 1994: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/c5/6d/c56d6a0ca439b4b336a4ec2cfb96d276104a243aa5edc6e77a7c91c1272fd7f1)

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