# STC SA00322DE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Pilatus Business Aircraft, United States
- Description: Modification to the pilot pitot/static system and the installation of a co-pilot pitot/static system and instruments.
- Applied: September 25, 1996
- Status date: March 13, 1998
- Product: Aircraft, Single-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A78EU](https://openairdocs.org/tcds/A78EU)
- Certificate PDF: https://openairdocs.org/files/sha256/27/7a/277ad3c4c0ef348a07bcb2790a7a0edf4a8a837067f48e65fcb56ffdc14b6997
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/EF5EA24061528D9685256CC1007DC8A2.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA00322DE

## ADs that name it (0)

None.

## Approved models (2)

- Pilatus Aircraft Limited PC-12 ([TCDS A78EU](https://openairdocs.org/tcds/A78EU))
- Pilatus Aircraft Limited PC-12/45 ([TCDS A78EU](https://openairdocs.org/tcds/A78EU))

## What the certificate says

This is OCR from the scanned FAA certificate. OCR can misread letters and numbers.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA00322DE This certificate issued to: Pilatus Business Aircraft Part 23 of the Federal Aviation Regulations.

Original Product -Type Certificate Number: A78EU Make: Pilatus Aircraft LTD.

Model: PC-12 and PC-12/45 Description of Type Design Change:

Modification to the Pilot Pitot/Static system and the installation of a Co-pilot Pitot/Static System and Instruments in accordance with Air Methods Corporation Master Drawing List No. 161-9000, Rev. D, FAA Approved October 30, 1997, or later FAA approved revision.

1. FAA approved Airplane Flight Manual Supplement, AFMS 080-0226, dated October 30, 1997, or later FAA approved revision is required.

2. 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.

3. This approval should not be extended to aircraft of this model on which other previously approved modifications are incorporated unless it is determined that the interrelationship 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 Airplane Flight Manual Supplement dated October 30, 1997 or later FAA approved revision, and Instructions for Continued Airworthiness, AMMS 050- 0226, revision (-), dated October 29, 1997 must be maintained as part of the permanent records for the modified aircraft.

Date of Application: September 25, 1996 Date Reissued: March 13, 1998 Date of Issuance: October 30, 1997 Date Amended:

FEDERAL AVIATION By Direction of the Administrator el m Ronald F. May (Dignature) Manager ADMINIST RATION Northwest Mountain Region Denver Aircraft Certification Office (Title)

## Every issue (1)

- March 13, 1998: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/27/7a/277ad3c4c0ef348a07bcb2790a7a0edf4a8a837067f48e65fcb56ffdc14b6997)

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