# STC SA00520SE

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Precise Flight Inc, United States
- Description: Installation of Precise Flight Speedbrake System.
- Applied: October 22, 1997
- Status date: January 8, 2008
- Product: Aircraft, Single-Engine
- Certification basis: Part 21, Part 23
- Data sheets: [TCDS A25SO](https://openairdocs.org/tcds/A25SO)
- Certificate PDF: https://openairdocs.org/files/sha256/1a/56/1a56017e509d563498b76f22555c137ae133c234ef47416bcda39045110bbcb3
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/4FA3A8C3DB285968862573DA005514ED.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA00520SE

## ADs that name it (0)

None.

## Approved models (2)

- The New Piper Aircraft Inc. PA-46-310P ([TCDS A25SO](https://openairdocs.org/tcds/A25SO))
- The New Piper Aircraft Inc. PA-46-350P ([TCDS A25SO](https://openairdocs.org/tcds/A25SO))

## 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 SA00520SE This certificate, issued to Precise Flight, Inc.

63354 Powell Butte Road Bend, OR 97701 Part 23 of the Federal Aviation Regulations.

Original Product⎯Type Certificate Number: A25SO Make: Piper Model: PA-46-310P, PA-46-350P; PA-46R-350T

Description of the Type Design Change: Installation of Precise Flight Speedbrake System manufactured in accordance with Precise Flight, Inc. Engineering Drawing List 010S0000, Rev. AE, dated June 18, 2007, or later FAA-approved revision, and installed in accordance with Precise Flight, Inc. Engineering Drawing List 573S0000, Revision J, dated May 17, 2007, or later FAA-approved revision. Maintain in accordance with Instructions for Continued Airworthiness for Piper Malibu Speedbrake 2000, PFI document 573SMAN0001, Rev. B, dated January 8, 2008, or later FAA-approved revision.

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 models on which other previously approved modifications are incorporated unless it is determined that the relationship between this change and any of those 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 a copy of Precise Flight Airplane Flight Manual Supplement (AFMS), PFI document 573SMAN0002, Rev. A., dated January 8, 2008, or later FAA-approved revision, must be maintained as part of the permanent records for the modified aircraft.

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.

Date of application: October 22, 1997 Date reissued: March 10, 2005 Date of issuance: May 10, 1998 Date amended: January 8, 2008

(Signature) Acting Manager, Seattle Aircraft Certification Office (Title)

## Every issue (1)

- January 8, 2008: Amended, Current. [certificate](https://openairdocs.org/files/sha256/1a/56/1a56017e509d563498b76f22555c137ae133c234ef47416bcda39045110bbcb3)

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