STC SA3195WE

Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA3195WE This certificate issued to: John K. McGuyer Certifies that the change in the type design for the following product with the limitutions and conditions herefor as specifed heren mels the airorthiness requirements f hurt 3t f the Civil Air ‹CAR-3 effective May 15, 1956 thru Amend. 3-2 and Par. 3.304 and 3.705 Regulations: of Amend. 3-7 effective May 3, 1962.

Original Product -Type bertificate Number: 2A13 Make: PIPER Model: PA-28-235, N9127W, Serial No. 28-10744 Description of Type Design Change:

Installation of Lycoming 0-540-AB5 engine, Hartzell HC-C2YK-1BF/F8477-4 propeller and associated powerplant components in accordance with John McGuyer Installation Instructions No. JM-II4576 dated April 5, 1976.

John McGuyer FAA Approved Airplane Flight Manual Supplement dated May 12, 1976 is required with this installation.

LimilalunandOnditin Data not suitable for reproduction of installation in other aircraft; therefore, they are satisfactory for Piper PA-28-235, N9127W, Serial No.

28-10744 only. No additional modifications of this type are to be approved solely by reference to this Supplemental Type Certificate or to the data submitted therefor.

A copy of this certificate, STC Addendum No. SA3195WE and John McGuyer Installation Instructions No. J-II4576 are required to be maintained as part of the modified aircraft permanent records.

28-10744 Supplemental Type Certificate ADDENDUM NO. SA3195WE The conditions and limitations of Type Certificate Data Sheet No. 2A13 apply except as follows:

This Addendum, which is part of Supplemental Type Certificate No. SA3195WE, prescribes conditions and limitations under which the product for which the STC was issued meets the airworthiness requirements of the Civil Air Regulations.

A copy of this Addendum shall be maintained as part of the modified aircraft permanent records.

I - Model PA-28-235 (Normal Category, Landplane only) as modified by STC SA3195WE.

Engine: Lycoming 0-540-A4B5 Engine Limits: For all operations - 235 HP (2575 RPM) Fuel: 100/130 Minimum Octane Aviation Gasoline Propeller: Hartzell HC-C2YK-1BF/F8477-4 Diameter: Maximum - 80" Minimum - 79" Pitch Settings: Low - 14.0° High - 32.0° Powerplant Instruments:

Serial Numbers Eligible:

Certification Basis:

Required Equipment:

Manifold Pressure Gage:

Red Line: 27.3" Hg.

No. 28-10744 only See Page 1.

In addition to the equipment applicable and required by Type Certificate Data Sheet 2A13, the equipment specified by John McGuyer Installation Instructions No. JM-II4576 dated April 5, 1976 must be installed as a result of the incorporation of this STC.

47 PAGE 3 OF 4 PAGES FAA AC 73-2651

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Shect) Number: SA3195WE Make: May 12; 1976 PIPER PA-20-232: N912 W Serial No. 28-10744 Supplemental Type Certificate ADDENDUM NO. SA3195WE (Continued) Required Equipment John McGuyer FAA Approved Airplane Flight Manual (Continued) : Supplement dated May 12, 1976.

NOTE 1. Current Weight and Balance Report including list of equipment included in certificated empty weight and Approved Loading Schedule must be in the aircraft.

NOTE 2. The following placards must be displayed in clear view of the pilot:

1. In full view of the pilot:

THIS AIRPLANE MUST BE OPERATED IN COMPLIANCE

WITH THE PROVISIONS OF JOHN MCGUYER FAA APPROVED AIRPIANE FLIGHT MANUAL SUPPLIMENT DATED MAY 12, 1976."

2. At the Master Switch:

"DO NOT TURN ALTERNATOR OFF IN FLIGHT, EXCEPT IN EMERGENCY."

3. Adjacent to each Wing Fuel Filler Cap:

'FUEL - 100/130 MINIMUM OCTANE. MAXIMUM CAPACITY - 25 GAL. CAPACITY TO BOTTOM OF FILLER NECK INDICATOR - 18 GAL."

4. Adjacent to each Tip Fuel Filler Cap:

'FUEL - 100/130 MINIMUM OCTANE. MAXIMUM CAPACITY - 17 GAL."

- END -

FAA FORM 6110-2-1 (10-69) PAGE 4 OF 4 PAGES © FAA AC73-2651