What it approves
Installation of Engine Oil Cooler System
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.
N umber SA00753DE This certificate, issued to : KNR-INC 2150 County Rd. 111 Evanston, WY 82931 certifies that the change in the ty pe design for the followi ng product with the limitations and conditions therefor as specified hereon meets the airworthiness requirements of P art 23 of the Federal Aviation R egulations.
Original Product T ype Certificate N umber: 1A6 M ake: Piper Aircraft, Inc M odel : PA-22-150 Description of the Type Design Change :
Installation of Engine Oil Cooler System in accordance with Document Number PP-260-MDL, Master Data List, Piper PA22, Oil Cooler System, Revision B, dated December 13, 2012, or later FAA approved revision.
1. Instructions for Continued Airworthiness, Oil Cooler Modification: Piper PA-22-150, Document Number PP- 261-ICA, Revision “-“, dated October 13, 2013, or later FAA accepted revision is required.
(Continued on Page 2)
Date of application: July 18, 2011 Date reissued: September 22, 2014
Date of issuance: January 3, 2013 Date amended:
B y direction of the A dministrator
(Signature) Gregory K. Johnson Northwest Mountain Region Manager(Acting) Denver Aircraft Certification Office (Title)
N umber SA00753DE
Limitations and C onditions (continued):
2. The installer must determine whether this design change is compatible with previously approved modifications.
3. A copy of this STC must be included in the permanent records of the modified aircraft.
4. If the holder agrees to permit another person to use this certificate to alter the product, the holder must give the other person written evidence of that permission.
Certification B asis:
The type certification basis for the Piper Aircraft, Inc., PA-22-150 series aircraft is shown on TCDS 1A6 for parts not changed or affected by this Supplemental Type Certificate.
The certification basis for parts changed or affected by the change since the reference date of application, July 18, 2011, is based upon Part 23 as amended by Amendment 23-61. The certification basis for this modification is as follows:
23.1(a),(b) Amendment 23-34 23.1017(a) Amendment 23-14
23.301(a),(b),(c) Amendment 23-48 23.1023 Amendment 23-0
23.303 Amendment 23-0 23.1041 Amendment 23-51
23.305 Amendment 23-45 23.1043(a)(1)(2)(3)(5),(b),(c),(d) Amendment 23-51
23.307(a) Amendment 23-0 23.1091(a),(b)(3), Amendment 23-51
23.601 Amendment 23-0 23.1093(a) Amendment 23-51
23.603 Amendment 23-23 23.1101 Amendment 23-43
23.605(a) Amendment 23-23 23.1183(a) Amendment 23-51
23.607(b) Amendment 23-48 23.1193(a),(b),(c) Amendment 23-43
23.609 Amendment 23-0 23.1301(a),(b),(c),(d) Amendment 23-20
23.611 Amendment 23-48 23.1309(a)(1)(2), (b)(1)(2)(3)(4),(f) Amendment 23-49
23.613(a),(b),(d) Amendment 23-45 23.1521(a),(b)(5),(c)(4) Amendment 23-50
23.901(a),(b),(c),(e) Amendment 23-53 23.1529 Amendment 23-26
23.1011(a),(b) Amendment 23-43 -END-
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-22-150 | 1A6 |