What it approves
Installation of a Lycoming O-360-A3A engine, a McCauley 1A200/DFA-8243 (Seaplane) propeller, cowling, air inlet filter assembly, baffling, and Edo 248-2440 floats (with aileron/rudder interconnect)
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: SA1015N4 This certificate issued to: James L. Hawk Certifies that the change in the type design for the fillewing product with the limitations and conditiond therefer as specifed heren meets the airunthiness requirements 1f Purt 3 of the CIVIL AiT Fregulations:
Original Product - Sype Bertificate Lumber: 1A6 Make: Piper Mired: PA-22-160 Vescription f-Sype Saign Change: Installation of a Lycoming 0-360-ABA engine, a McCauley 1A200/DFA-8243 (Seaplane) propeller, cowling, air inlet filter assembly, baffling, and Edo 248-2440 floats (with aileron/rudder interconnect) in accordance Limilatina andfenditiona Data pertaining to this modification are considered inadequate for duplication in other aircraft. This approval is limited to the installation in Piper PA-22-160, Serial Number 22-6653 only. A copy of this Certificate and Addendum No. SA1015NW shall be maintained as part of the permanent records for the modified aircraft,
Date of Application: July 18, 1980 I ute missued:
Date of Issuance: August 15, 1980 Date Amended:
FEDERAL AVIATION $ the Administrater D. L. Rugger TO MINISTRATION Chief, Engineering and Manufacturing Branch (Title) 47 FAA FORM 8110-2 (10-68)
United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) August 15, 1980 Number SA1015NW Supplemental Type Certificate ADDENDUM NO. SA1015NW The conditions and limitations of Type Certificate Data Sheet Number 1A6 apply except where superseded by the following:
Supplemental Type Certificate Data Sheet, which is part of STC SA1015NW, prescribes the conditions and limitations under which the product for which the STC was issued meets the airworthiness requirements of the Civil Air Regulations.
Supplemental Type Certificate HOLDER: James L. Hawk PA-22-160 4PCSM (NORMAL CATEGORY ONLY) AS MODIFIED BY SIC SA1015NW Engine: Lycoming 0-360-A3A Fuel: 91/96 minimum grade aviation gasoline Engine Limits: For all operations 2700 rpm (180 Hp) Propeller and Propeller Limits: McCauley 1A200/DFA-8243 Diameter: 82" maximum; 78" minimum Powerplant Instrument Markings: Tachometer:
2700 rpm (red line) maximum Oil Temperature Gauge:
245°F (red line) maximum Oil Pressure Gauge:
25 psi (red line) minimum 100 psi (red line) maximum 60 to 90 psi (green arc) normal operating range Fuel Pressure Gauge:
5 psi (red line) minimum 8 psi (red line) maximum 3 to 5 psi (green arc) normal operating range
FAA FORM 8110-2-1 (10-69) PAGE 3OF 4 PAGES FAA AC 73-2651
August 15, 1980 STC Addendum No. SA1015NW C. G. Range: Seaplane (normal category) :
(15.0) to (20.0) at 2000 pounds
(12.0) to (20.0) at 1800 pounds
(10.0) to (20.0) at 1500 pounds or less
STRAIGHT LINE VARIATION BETWEEN POINTS GIVEN Maximum Weight: 2000 pounds Required Equipment: None Serial Number Eligible: 22-6653
- END - Page 4 of 4 Pages
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.
Approved models · 1
| Make | Model | Data sheet |
|---|---|---|
| Piper Aircraft Inc. | PA-22-160 | 1A6 |