STC SA2807SW

Supplemental type certificate · STC Engineering Co

Holder
STC Engineering Co · United States
Status
Current · Issued
Status date
June 30, 1978
Applied
January 14, 1978
Product
Aircraft · Small Airplane
Certification basis
Part 21
Data sheet
TCDSA3SW

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

What it approves

Installation of P&W R1340-AN2 engine and Hamilton Standard 23D40/AG200-OS propeller.

What the certificate says

From the PDF’s text layer, without the form’s printed wording. Layout and order may differ; the PDF is the record.

iinittd States of aratrica Bcpartment of ^transportation—federal Stoiation administration nipplemental Km Certificate istt&ei£a&&ri&.

SA2807SW Project A3975SW-DS MB-214 S T C Engineering Company 4410 N W 54th Street Oklahoma City, Oklahoma 73112 3f ' A3SW Ayers S--2R Civil Air Installation of Pratt & Whitney R1340-AN2 engine and Hamilton Standard 23D40/AG200-QS propeller according to Drawing List 78100 dated 6/18/78, or later FAA approved revision.

Aircraft must be placarded: Engine Operating Liinist Takeoff only (5 minutes) 600 H.P. 2250 R.P.M. - 36.0" M.P.Maximum Continuous 550 H.P. 2200 R.P.K. - 34.0" M.P. S,L.550 H.P. 2200 R.P.M. - 32.5" M.P. 5000 ft.Straight line variation between points given Compatibility of this modification with other previous approved modificationsmust be determined by the installer.

^ :&}<<7nw January 14, 1978 June 30, 1978 f Signature} Don P. Watson Chief, Engineering and Manufacturing Branch (Title} _^ ~ ~ ~' ~ _

47.

FAA FonMBl 10-2 PO-68)

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 · 1

MakeModelData sheet
Thrush Aircraft Inc.S-2RA3SW