# STC SA00868LA

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Lifeport Inc, United States
- Description: Installation of patient loading and utility system.
- Applied: January 14, 1999
- Status date: May 10, 2019
- Product: Aircraft, Small Airplane
- Certification basis: Part 21, Part 23
- Data sheets: [TCDS A78EU](https://openairdocs.org/tcds/A78EU)
- Certificate PDF: https://openairdocs.org/files/sha256/ac/6b/ac6b39b257a1dd72c7640bff02bf498bdcce6f1ed6c9bdbd039fa3f69a41e363
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/751611095AAF48EE862585E700527F77.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA00868LA

## ADs that name it (0)

None.

## Approved models (1)

- Pilatus Aircraft Limited PC-12 ([TCDS A78EU](https://openairdocs.org/tcds/A78EU))

## 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 SA00868LA This certificate, issued to LifePort, LLC 1610 Heritage Street Woodland, WA 98674 Part 23* of the Federal Aviation Regulations. *Certification basis is set forth in Type Certificate Data Sheet A78EU.

Original ProductType Certificate Number: A78EU Make: Pilatus Aircraft, Ltd.

Model: Pilatus PC-12

Description of the Type Design Change: Installation of Patient Loading and Utility System in accordance with FAA approved LifePort, Inc. Master Drawing List EGR-591-01, Rev. A, dated October 6, 1999, or later FAA approved revision. FAA approved Airplane Flight Manual Supplement No. EGR -591-11, dated October 6, 1999, or later FAA approved revision, is required as part of this installation.

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 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 pro duct, the holder shall give the other person written evidence of that permission.

Date of application: January 14, 1999 Date reissued: May 10, 2019 Date of issuance: October 12, 1999 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 (1)

- May 10, 2019: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/ac/6b/ac6b39b257a1dd72c7640bff02bf498bdcce6f1ed6c9bdbd039fa3f69a41e363)

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