# STC SA2106NM

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Precise Flight Inc, United States
- Description: Installation of Precise Flight Speedbrake System.
- Applied: February 16, 1983
- Status date: November 7, 2003
- Product: Aircraft, Single-Engine
- Certification basis: Part 21
- Data sheets: [TCDS 5A6](https://openairdocs.org/tcds/5A6), [TCDS 3A13](https://openairdocs.org/tcds/3A13), [TCDS 3A24](https://openairdocs.org/tcds/3A24), [TCDS A4CE](https://openairdocs.org/tcds/A4CE), [TCDS A16CE](https://openairdocs.org/tcds/A16CE), [TCDS 3A21](https://openairdocs.org/tcds/3A21)
- Certificate PDF: https://openairdocs.org/files/sha256/9a/3f/9a3f94fb3c6ee5d3a2634f9fdcc707bbdfbf2347260c2ca0a0fda67acfff4ada
- Approved model list and other attachments: [MEL SA2106NM.pdf](https://openairdocs.org/files/sha256/8d/09/8d09d2e11cddf8993f24fa6c82160a0551be6d4bc77f4d7c55d082beec21b36b)
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/A2D80FC9E6A7D71786256DF9004EA7BF.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA2106NM

## ADs that name it (0)

None.

## Approved models (9)

- Cessna Aircraft Company 180 ([TCDS 5A6](https://openairdocs.org/tcds/5A6))
- Cessna Aircraft Company 182 ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 185 ([TCDS 3A24](https://openairdocs.org/tcds/3A24))
- Cessna Aircraft Company 206 ([TCDS A4CE](https://openairdocs.org/tcds/A4CE))
- Cessna Aircraft Company 207 ([TCDS A16CE](https://openairdocs.org/tcds/A16CE))
- Cessna Aircraft Company 210-5 (205) ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company 210E ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company 210F ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company T210F ([TCDS 3A21](https://openairdocs.org/tcds/3A21))

## 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 SA2106NM This certificate, issued to Precise Flight, Inc.

63354 Powell Butte Road Bend, OR 97701 Part * of the * Regulations.

Original ProductType Certificate Number: *See attached Master Eligibility List (MEL) Make: No. SA2106NM for list of approved airplane Model: models and applicable airworthiness regulations.

Description of the Type Design Change: Installation of Precise Flight Speedbrake System in accordance with Precise Flight, Inc. Speedbrake System (SBS) Installation Manual, Report No. 111, dated May 27, 1983, 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 these models 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, Continuation Sheet, MEL No. SA2106NM, and Precise Flight, Inc. Airplane Flight Manual Supplement 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: February 16, 1983 Date reissued:

Date of issuance: May 27, 1983 Date amended: 5/24/84; 10/25/85; 11/7/03

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

Number SA2106NM Precise Flight, Inc.

Reissued:

Amended: 5/24/84; 10/25/85; 11/7/03

Limitations and Conditions (cont’d): The conditions and limitations of the original Type Certificate as reflected in the Master Eligibility List (MEL) apply except as follows:

This addendum, which is part of Supplemental Type Certificate No. SA2106NM, prescribes the conditions and limitations under which the STC was issued and meets the airworthiness requirements of the Civil Air Regulations.

CESSNA MODELS 180, 182, 185, 210-5 (205), 206, 207, 210E, 210F and T210F, 4PCLM (NORMAL CATEGORY) AS MODIFIED BY STC SA2106NM.

EQUIPMENT: Cessna Owner’s Manual or Pilot’s Operating Handbook and AFMS for the Speedbrake System (SBS) 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 Sheets as referenced in the MEL, apply the following:

a. The following placard is to be located at the circuit breaker panel:

**SPEEDBRAKE**

b. The following placard is to be on the left horn of the pilot’s control wheel near the speedbrake control switch:

**SPEEDBRAKE PUSH**

**TO DEPLOY**

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.

**FAA FORM 8110-2- 1 (10-69) PAGE 3 OF 4 PAGES**

Number SA2106NM Precise Flight, Inc.

Reissued:

Amended: 5/24/84; 10/25/85; 11/7/03

Limitations and Conditions(cont’d):

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

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

e. The following placard is to be placed in front and in full view of the Cessna Models 210E, 210F and T210F:

**OPERATION LIMITATIONS**

**SPEEDBRAKES SHALL NOT BE ACTIVATED ABOVE 185 KIAS**

NOTE 3: With the described Speedbrake System (SBS) installation, performance will be at least equal to or better than that given in the Owner’s Manual or Pilot’s Operating Handbook for the Cessna airplane.

- END -

**FAA FORM 8110-2- 1 (10-69) PAGE 4 OF 4 PAGES**

### MEL SA2106NM.pdf

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

MEL AMENDMEN DATE 9/16/85 May 27, 1983 AFM SUPPLEMENT NUMBER/ DATE 5/27/83 5/27/83 5/27/83 5/27/83 5/27/83 5/27/83 5/27/83 REV.

SHT. INC. MASTER ELIGIBILITY LIST NUMBER SA2106NM FOR PRECISE FLIGHT SPEEDBRAKE SYSTEM FAA SEALED CERTIFICATION DRAWING/ BAS1S DRAWING LIST FOR ALTERATION NUMBER 180-208-040 Part 3 of Civil Air Regulations & T.C. 180-208-040 Part 3 of Civil Air Regulations & T.C.. Part 3 of Civil Air' 180-208-040 Regulations & T.C. 180-208-040 Part 3 of Civil Air Regulations & T.C. 180-208-040 Part 3 of Civil Air Regulations & T.C. 180-208-040 Part 23 of Federal Aviation Regulations and T.C. A16CE 180-208-040 Part 3 of Civil Air Regulations and T.C.

PRECISE #5A6 3A13 3124 3A21 A4CE 3A21.

ORIGINAL TYPE CERTIFICATE NUMBER 5A6, 3A13 3A24 3A21 A4CE A16CE 3A21 AIRCRAFT MODEL 210-5(205) 180 182 185 206 207 210E 210F T210F

**AIRCRAFT MAKE CESSNA ITEM 1. 5. 7.**

## Every issue (1)

- November 7, 2003: Amended, Current. [certificate](https://openairdocs.org/files/sha256/9a/3f/9a3f94fb3c6ee5d3a2634f9fdcc707bbdfbf2347260c2ca0a0fda67acfff4ada), [MEL SA2106NM.pdf](https://openairdocs.org/files/sha256/8d/09/8d09d2e11cddf8993f24fa6c82160a0551be6d4bc77f4d7c55d082beec21b36b)

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