What it approves
Installation of alternate Hartzell Propellers and Governors
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.
Number SA00326BO
FAA Form 8110-2 (8/13) Page 1 of 3 This certificate issued to:
Aerodyme Corporation 274 Valley Road South Burlington, VT 05403 Part 23 of the Federal; Aviation Regulations.
Original Product - Type Certificate Number: A12SO Make: Commander Model: 114, 114A, 114B
Installation of alternate Hartzell Propellers and Governors in accordance with Aerodyme Corporation Master Document List (MDL), Document number AMDL326-01, Rev 01, dated February 08, 2014, or later FAA approved revision.
1. This modification is to be maintained in accordance with Aerodyme Corporation Hartzell Propeller and Hartzel Propeller Governor (if installed) Instructions for Continued Airworthiness, document number AD1626-02, revision 02, dated February 8, 2016, or later accepted revision and must be made available to the operator at the time of installation.
(continued on Page 3 of 3)
Date of Application: June 13, 2012 Date reissued:
Date of Issuance: October 5, 2013 Date amended: April 6, 2016
Signature Gaetano Sciortino
Acting Manager, Boston Aircraft Certification Office Title
SUPPLEMENTAL TYPE CERTIFICATE, FAA FORM 8110-2 (CONTINUED)
FAA Form 8110-2 (8/13) Page 2 of 3
TRANSFER
ENDORSEMENT
To (Name of transferee)
(Address of transferee)
(Number and street)
(City, State, and ZIP Code)
From (Name of grantor)
(Address of grantor)
(Number and street)
(City, State, and ZIP Code)
Number SA00326BO April 6, 2016
FAA Form 8110-2 (8/13) Page 3 of 3
Limitations and Conditions: (continued from Page 1 of 3)
2. This approval should not be extended to other aircraft of this model on which other previously approved modifications are incorporated unless it is determined by the installer that the interrelationship between this change and any of those other previously approved modifications will produce no adverse effect upon the airworthiness of that airplane.
Certification Basis:
Based on 14 CFR § 21.115 and § 21.101, and the FAA policy for design changes that are identified as not significant in FAA Order 8110.48, the certification basis for the Commander 114/114A/114B aircraft is as follows:
a. The type certification basis for parts not changed or not affected by the change is shown on TCDS A12SO.
b. The modification certification basis for parts changed or affected by the change since the reference application date, June 13, 2012, is based upon part 23 as amended by Amendment 23-62 as follows:
Regulations at the latest amendment 23-0 through 23-62
23.33, 23.45, 23.49, 23.51, 23.53, 23.63, 23.65, 23.69, 23.71, 23.75, 23.141, 23.143, 23.145,
23.147, 23.153, 23.155, 23.157, 23.161, 23.171, 23.173, 23.175, 23.177, 23.181, 23.201,
23.203, 23.207, 23.231, 23.233, 23.251, 23.253, 23.301, 23.307, 23.337, 23.341, 23.347,
23.349, 23.361, 23.363, 23.371, 23.391, 23.901, 23.905, 23.907, 23.925, 23.943, 23.1041,
23.1043, 23.1047, 23.1529.
Regulations at an intermediate amendment None Regulations at the amendment level in TCDS A12SO None ------------------------------------------------------------END-------------------------------------------------------
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.
Approved models · 3
Every issue · 2
DRS keeps each issue of an STC as its own record, with its own certificate and attachments.
| Date | Status | Files |
|---|---|---|
| April 6, 2016 | Amended, current | Certificate |
| October 5, 2012 | Issued, earlier issue | Certificate |