What it approves
Installation of the Mechanical Provisions for the Garmin G600 Flight Display 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.
Part 23 of the Federal Aviation Regulations.
Description of Type Design Change: Installation of the Mechanical Provisions for the Garmin G600 Flight Display System on Pilatus PC-12, PC-12/45, PC-12/47 and associated hardware in accordance with Master Drawing List 2-117127-001 Revision B dated January 2, 2013 or later FAA approved drawing revisions.
Limitations and Conditions: This approval should not be extended to other aircraft of this model on which other previously approved modifications are incorporated, unless it is determine by the installer that the interrelationship between this change and any other previously approved modifications will produce no adverse effect upon the airworthiness of that airplane. If the 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.
Pilatus Business Aircraft 11755 Airport Way Broomfield, CO 80021 A78EU Make : Pilatus PC-12, PC-12/45, PC-12/47 Model :
Date of application: May 5, 2012
Date of issuance: February 6, 2013
Date reissued: June 4, 2013
(Signature)
Melvin D. Taylor Manager, Atlanta Aircraft Certification Office
(Title)
FAA FORM 8110-2-1(10-69) PAGE 2 of 2 PAGES
Number SA03992AT Instructions for Continued Airworthiness (ICA), EMTEQ Engineering Document No. 2-117127-903, Rev.
IR, dated June 20, 2012, or later FAA accepted revision must be made available to the operator at the time of installation.
Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for Pilatus PC-12, PC-12/45, PC-12/47 aircrafts is as follows:
a. The type certification basis Pilatus PC-12, PC-12/45, PC-12/47 airplanes is shown on TCDS A78EU for parts not changed or not affected by the change.
b. The certification basis for parts changed or affected by the change since the reference date of application, May 5, 2012 is based upon Part 23 as amended by Amendment 23-63. Based on 14 CFR §§ 21.115 and
21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for this modification was determined to be:
Regulations at the latest amendment 23-0 through 23-63
23.23(a), 23.301(a)(b), 23.303, 23.305(a), 23.307(a), 23.573(b), 23.601, 23.603(a)(b), 23.605(a), 23.607,
23.609(a), 23.611, 23.613(a)(b)(c)(d), 23.625(a), 23.627, 23.867(b), 23.1529, 23.1541(b)
Regulations at an intermediate amendment
Regulations at the amendment level in TCDS A78EU
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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 |
|---|---|---|
| June 4, 2013 | Reissued, current | Certificate |
| February 6, 2013 | Issued, earlier issue | Certificate |