STC SA3348NM

Supplemental type certificate · Thompson Aero Products

Holder
Thompson Aero Products · United States
Status
Current · Issued
Status date
April 10, 1986
Applied
October 25, 1984
Product
Aircraft · Single-Engine
Certification basis
Part 21
Data sheet
TCDS3A21

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 6, 2025.

What it approves

Fabrication and installation of external hinged-plate spoilers and dive brakes.

What the certificate saysOCR

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: SA3348NM This certificate issued to: Thompson Aero Products Part 3 of the CIVIl Air Regulations Original Product - Type berlificate Number.

ЗА21 CESSNA 210G, T210G, 210H, T210H, 210J, T210J, 210K, T210K, 210L, T210L, 210M, T210M, 210N, T210N, P210N Fabrication and Installation of external hinged-plate spoilers and dive brakes in accordance with FAA sealed Thompson Aero Products Production Drawing List Number DRC-210, Revision "E", dated April 10, 1986, or later FAA approved revision.

Limitations and Conditions: The approval of this change in type design applies only to those basic Cessna Models referenced above. This approval should not be extended to other airplanes of this model on which other previously approved modifications are incorporated unless it is determined by the installer that the modifications will introduce no adverse effect on the airworthiness of that aircraft. Airplanes equipped with this modification must be operated in accordance with either the FAA approved Supplemental Airplane Flight Manual or Airplane Flight Manual Supplement, whichever is (see continuation sheet) A copy of this Certificate and the Continuation Sheet Number SA3348NM shall be maintained as a part of the permanent records of the modified aircraft.

NOTE: The Auxiliary Vacuum System (AVS) is considered optional equipment for airplanes powered with normally aspirated engines and essential for proper DRC operation when installed on turbocharged T210/P210 models.

- END - 47 PAGE 3 OF 3 PAGES

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 · 15

MakeModelData sheet
The Cessna Aircraft Company210G3A21
The Cessna Aircraft Company210H3A21
The Cessna Aircraft Company210J3A21
The Cessna Aircraft Company210K3A21
The Cessna Aircraft Company210L3A21
The Cessna Aircraft Company210M3A21
The Cessna Aircraft Company210N3A21
The Cessna Aircraft CompanyP210N3A21
The Cessna Aircraft CompanyT210G3A21
The Cessna Aircraft CompanyT210H3A21
The Cessna Aircraft CompanyT210J3A21
The Cessna Aircraft CompanyT210K3A21
The Cessna Aircraft CompanyT210L3A21
The Cessna Aircraft CompanyT210M3A21
The Cessna Aircraft CompanyT210N3A21