What it approves
Operation of airplane on leaded and unleaded automotive gasoline, 91 minimum antiknock index(RON+MON)/2. Intermixing with aviation gasoline also approved. (PA-28-181 SN 28-671 to 28-5859, 28-7105001 to 28-7505261, 28-7690001 to 28-8590001 and up)
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.
984 K Road Minden, NE 68959
CAR 3 of the Regulations.
Original Product Type Certificate Number : 2A13
Make: Piper
Model: See Page 3 of 3 for approved models
Operation of Piper airplanes when using leaded and unleaded automotive gasoline, with a minimum antiknock index (RON+MON)/2 of 91 per ASTM Specification D-439 or D-4814. Intermixing with aviation gasoline also approved.
Data Required:
1. A copy of this certificate
2. Drawing List, 28-TL-2, Rev. (D), dated September 13, 1990, or later FAA Approved revision
3. Drawing List, 28-TL-3, Rev. (H), dated October 16, 1990, or later FAA Approved revision
4. Airplane Flight Manual Supplement No. 2, Rev. (-) dated October 17, 1990, or later FAA Approved revision
1. Limited to those airplanes equipped with engines modified in accordance with STC SE2563CE or SE2587CE.
2. Airplanes equipped with fuel manifold/reservoir are not eligible for this installation.
3. 3/8-inch fuel supply line on the RH fuel tank system which is used for takeoff and landing is required.
4. Compatibility of this design change with previously approved modifications must be determined by the installer.
5. If the STC holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission.
6. Approval of this change in type design applies to the above model airplanes only.
7. A copy of this certificate shall be maintained in the airplane permanent records.
This certificate and the supporting data, which is the basis for approval, shall remain in effect until surrendered, suspended, revoked or a termination date is otherwise established by the Administrator of the Federal Aviation Administration.
Date amended: April 29, 2005
( Signature) Charles D. Riddle Program Manager Wichita Aircraft Certification Office
(Title) Date of application: May 30, 1990
Date of issuance: October 17, 1990
Transfer the ownership of the Supplemental Type Certificate Number to (Name of transferee) (Address of transfer) (Number and street)
(City, State, and Zip code) from (Name of grantor) (Print or type) (Address of grantor) (Number and street)
(City, State, and Zip code) Extent of Authority (if licensing agreement):
Signature of grantor ( In ink):
Item Type Make/Model Airplane Serial Number 1 Piper PA-28-160 Piper PA-28-180 Cherokee 28-671 thru 28-1760 2 Piper PA-28-160 Piper PA-28-180 Cherokee 28-1761 thru 28-5859 28-7105001 thru 28-7505261 3 Piper PA-28-161 Warrior II / Cadet 28-7716002 thru 28-8616057 2816001 thru 2816105 (Except 2816066) 2841001 thru 2841364 (Except 2841351 thru 2841359) 4 12/14 Volt Airplanes Piper PA-181 Archer II 28-7690001 thru 28-8690056 2890001 thru 2890205 5 Piper PA-28-161 Warrior III 2816110 and on 2842001 thru 2842108 2842109 and on 6 24/28 Volt Airplanes Piper PA-28-181 Archer III 2890206 and on 2843001 thru 2843414 2843203 and on
ADs that name this STC · 1
An AD can apply because an STC is installed, or mention one in its text.