STC ST00138MC

Supplemental type certificate · Sierra Nevada Corporation

Holder
Sierra Nevada Corporation · United States
Status
Current · Issued
Status date
September 2, 2016
Applied
May 11, 2016
Product
Aircraft · Large Airplane
Certification basis
Part 21, Part 25
Data sheet
TCDSA45NM

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 5, 2025.

What it approves

Installation of a cargo door latch capability from inside the aircraft.

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.

Vniteti States of Jlmerica ©epartment of <Transportation P edera( }l viation }ld"ministration Suppfementa(r[ype Certificate

1.fum6er: ST00138MC 'ITiis certificate issueti to: Sierra Nevada Corporation 11551 E. Arapahoe Road Centennial, CO 80112 certifies tliat tlie cfianne in tlie type aesign for tlie foffowino proauct witli tfie {imitations anti contfitions tfierefore as specifiealiereon meets tlie airwortliiness requirements of Cl'art .E__of tlie Chapter 14 Code of Federal Regulations Original Product - Type Certificate Number:

A45NM Description of Type Design Change:

Make: 328 Support Services GmbH Model:

Dornier Model 328-100 Installation of a cargo door latch capability from inside the aircraft. Required data includes:

1) Sierra Nevada Corporation (SNC), Master Data List (MDL) 0703-00-9311, Revision A, dated September 2, 2016, FAA approved September 2, 2016, or later FAA approved revisions.

(Continued on page 3) Limitation s and Condition s:

1) Compatibility of this design change with previously approved modifications must be determined by the installer.

2) 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 .

(Continued on page 3) 'ITiis certificate anti tlie supporting aata wliicli is tfie 6asis for approva( sliaff remain in effect unti( surrentfered', suspentfed', anti revo~ti or a tennination tiate is otlierwise esta6lisliea 6y tlie }ltiministrator of tlie Petferaf Jlviation JLd'tninistration.

Date of Application: 05/11/2016 Date Reissued:

Date of Issuance: 09/02/2016 Date Amended :

cBy CDirection of tlie JLtiministrator S•M"re ~ ~ 'litfe William Eckler ODA administrator, ODA-833355-CE The STC's supporting documentation {drawings , instructions , specifications , flight manual supplements , etc.) is the property of the STC holder . {Ref. 14 CFR 21 .120).

FAA Form 8110·2 (5/14) Page 1of4

Vnitetf States of }f.merica (])epartment of <Transportation P eclera[ Jl viation }laministration Supp Cementa{ CJ'ype Certificate (Continuation Sheet) :Num6er: ST00138MC Description ofType Design Change (continued from page 1):

2) Sierra Nevada Corporation (SNC) Instructions for Continued Airworthiness (ICA) 0703-00-9305, Rev A, dated June 22, 2016, or later FAA approved revision.

Limitations and Conditions (continued from page 1):

3) Approval of this change in type design applies to 328 Support Services GmbH, Dornier 328-100 Mod 20 aircraft only as defined in TCDS A45NM.

4) A copy of this certificate and the ICA shall be maintained in the airplane permanent records.

47. (Ref. 14 CFR 21 .120).

FAA Form 8110-2 (5/14) Page 3 of 4

Vnitea States of .ftmerica (])epartment of rrransportation Peaera[ }lviation }laministration Suppfementa{Type Cenificate (Continuation Sheet) Jfum6er: ST00138MC Certification Basis:

Based on 14 CFR §21.115 and§ 21.101, and the FAA policy for significant changes in FAAOrder8110-48, the certification basis for the Dornier Model 328-100 cargo door latch installation is as follows:

a. The type certificate basis for 328 Support Services GmbH, Dornier Model 328-100 is shown on A45NM 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 the application, 05/11 /2016, is based upon 14 CFR Part 25 as amended by Amendment 25-1through25-64 and additional selected rules at later amendments as listed on the TCDS. Based on 14 CFR 21.115 and 21.101, and the FAA policy for significant changes in the FAA Order 8110.48, the certification basis for this modification was determined to be:

Regulations at the latest amendment 25-0 through 25-141:

25.853(a) [Arndt. 25-116] Regulations at the amendment level in the TCDS A45NM:

25.301 [Arndt. 25-23], 25.303 [Arndt. 25-23], 25.305(a}(b} [Arndt. 25-54], 25.307(a) [Arndt. 25-54], 25.601 [Arndt. 25-0], 25.603 [Arndt. 25-46], 25.605(a) [Arndt. 25-46], 25.607(a)(b) [Arndt. 25-23], 25.609 [Arndt. 25-0], 25.611 [Arndt. 25-23], 25.613 [Arndt.

25-46], 25.625(a)(b)(c) [Arndt. 25-23], 25.783(b)(g) [Arndt. 25-54], 25.791 (e) [Arndt. 25-72], 25.1301 (a)(b)(c)(d) [Arndt. 25-0],

25.1309(a)(b)(c) [Arndt. 25-41 ], 25.1529 [Arndt. 25-54] Regulations a~ an intermediate amendment:

None ---------------------------------------END----- This certificate may be transferred or made available to third persons by licensing agreements in accordance with 14 CFR 21 .47. Possession of this Supplementa l Type Certificate (STC) document by persons other than the STC holder does not constitute rights to the design data nor to alter an aircraft. aircraft engine, or propeller . .

FAA Form 8110-2 (5/14) Page 4 of 4

ADs that name this STC · 0

An AD can apply because an STC is installed, or mention one in its text.

No AD in this release names this STC

Approved models · 1

MakeModelData sheet
328 Support Services GmbH328-100A45NM