What it approves
Installation of a Lycoming IO-360-A1B6 and a Hartzell HC-M2YR-1B/7666A-2 propeller and associated baffling changes
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: SA14854M This certificate issued to: Larry J. Martinez Punt 3 of the CIVIl Air Regulations:
Original Product -Type bertificate Number: 2A13 Make: Piper Model: PA 28-180 Description of Type Design Change: Installation of a Lycoming 10-360-A1B6 and a Hartzell HC-M2YR-1B/7666A-2 propeller and associated baffling changes in accordance with Larry J. Martinez Photographs 1 through 3.
Limitations and Conditions: Data pertaining to this modification are considered inadequate for duplication in other aircraft. This approval is limited to the installation in Piper PA 28-180, Serial Number 28-7305227, only. A copy of this Certificate, Addendum SA1485NM, and FAA Approved Airplane Flight Manual Supplement, shall be maintained as part of the permanent records for the modified aircraft.
March 15, 1982 Sale unended:
ÇEDERAL AVIATION •By difestion of the ildus Navell Medeson (Signature) TOMINIST AT ON Chief, Seattle Area Aircraft /Certification Office (Title)
47.
FAA FOR 8110-2 (10-68)
United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) March 15, 1982 Number: SA1485NM Supplemental Type Certificate ADDENDUM NO. SA1485NM The conditions and limitations of Type Certificate Data Sheet Number A213 apply except where superseded by the following:
Supplemental Type Certificate Data Sheet, which is part of STC SA1485NM 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: LARRY J. MARTINEZ PIPER PA 28-180 ARCHER, 4PCLM (NORMAL CATEGORY) AND 2PCLM (UTILITY CATEGORY) AS MODIFIED BY STC SA1405NM.
Engine: Lycoming 10-360-A1B6 Engine Limits: 200 hp. at 2700 rpm S.L.
Fuel: 100/130 octane aviation gasoline.
Propeller: Hartzell HC-M2YR-1B/7666A-2 Propeller Limits: 180 hp: @ 2900 rpm All else is the same as Data Sheet 2A13.
- END -
IA FORM 8110-2-1 (10-69) PAGE 3 OF 3 PAGES C FAA AC 73-2651
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-28-180 | 2A13 |