STC SA2171NM

Supplemental type certificate · Precise Flight Inc

Holder
Precise Flight Inc · United States
Status
Current · Amended
Status date
March 10, 2005
Applied
August 5, 1983
Product
Aircraft · Single-Engine
Certification basis
Part 3, Part 21
Data sheet
TCDS2A13

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 5, 2025.

What it approves

Installation of Precise Flight speedbrake system.

What the certificate saysPartly OCR

Some pages are 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: SA2171NM This certificate issued to: Precise Flight, Inc.

63354 Powell Butte Rd.

Bend, OR 97701

(This STC is a duplicate original to replace the original which was lost. Issued 3/10/05)

Part 3 of the Civil Air Regulations.

Original Product Type Certificate Number: 2A13 Make: Piper Model: PA-28-201T, PA-28R-201T and PA-28RT-201T

Description of Type Design Change: 1) Installation of Precise Flight Speedbrake in accordance with Precise Flight, Inc. Speedbrake Installation Manual Report No. 121, or later FAA approved revisions.

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 this model on which other previously approved modifications are incorporated unless it is determined that the relationship 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, Addendum, and Airplane Flight Manual Supplement, dated June 16, 1983, or later FAA approved revisions, 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: August 5, 1983 Date Reissued: September 7, 2004 Date of Issuance: November 17, 1983 Date amended: May 24, 1984; February 20, 1987, September 7, 2004;

March 10, 2005

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

Number: SA2171NM

Precise Flight, Inc.

Reissued: September 3, 2004 Amended: May 24, 1984, February 20, 1987, September 7, 2004; March 10, 2005

Supplemental Type Certificate ADDENDUM NO. SA2171NM

The conditions and limitations of the original Type Certificate No. 2A13 apply except as follows:

This Addendum, which is part of Supplemental Type Certificate No. SA2171NM, prescribes the conditions and limitations under which the STC was issued meets the airworthiness requirements of the Civil Air Regulations.

Supplemental Type Certificate HOLDER: Precise Flight, Inc.

1. PIPER PA-28-201T AND PA28RT-201T (NORMAL CATEGORY) AS MODIFIED BY STC SA2171NM

Equipment: Piper Owner’s Manual or Pilot’s Operating Handbook and AFMS for the Speedbrake System must be maintained in the airplane at all times.

Note 1: Current weight and balance report including list of equipment in the certified empty weight must be in the aircraft.

Note 2: In addition to the placards and Markings required by Type Certificate Data Sheet 2A13, Note 2, apply the following:

(a) The following placard is to be located at the circuit breaker panel and on the engine control console near the safety toggle switch when applicable:

SPEED BRAKE

(b) The following placard is to be on the horn of the pilot’s control wheel near the Speedbrake control horn switch:

SPEED BRAKE PUSH TO DEPLOY

FAA FORM 8110-2- 1 (10-69)

Number: SA2171NM

Precise Flight, Inc.

Reissued: September 3, 2004 Amended: May 24, 1984, February 20, 1987, September 7, 2004; March 10, 2005

Supplemental Type Certificate ADDENDUM NO. SA2171NM

(c) If the standby vacuum system is installed, the following placard is to be in front and in full view of the pilot:

THIS AIRCRAFT IS EQUIPPED WITH PRECISE FLIGHT, INC. STANDBY VACUUM SYSTEM. REFER TO AFM OR PILOT’S OPERATING HANDBOOK FOR OPERATING INSTRUCTIONS.

(d) The following placard is to be placed in front and in full view of the pilot:

SPEEDBRAKE SYSTEM OPEARTING INSTRUCTIONS AND LIMITATIONS – SEE SUPPLEMENT IN OWNER’S MANUAL OR PILOT’S OPERATING HANDBOOK

Note 3: With the described Speedbrake System in stallation, performance will be at least equal to or better than that given in the Owner’s Manual or Pilot’s Operating Handbook for the Piper airplane.

- END -

FAA FORM 8110-2- 1 (10-69)

ADs that name this STC · 0

An AD can apply because an STC is installed, or mention one in its text.

No AD in this release names this STC

Approved models · 3

MakeModelData sheet
The New Piper Aircraft Inc.PA-28-201T2A13
The New Piper Aircraft Inc.PA-28R-201T2A13
The New Piper Aircraft Inc.PA-28RT-201T2A13