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TE.DOA.00830-005© European Union Aviation Safety Agency. All rights reserved. ISO9001 Certified. Proprietary document. Copies are not controlled.Confirm revision status through the EASA-Internet/Intranet. An agency of the European Union Page 1 of 1 APPROVAL CERTIFICATE EASA.21J.357 Pursuant to Regulations (EU) 2018/1139 and (EU) 748/2012 and subject to the conditions specified below, the Agency hereby certifies PILATUS AIRCRAFT LTD. Ennetbürgerstrasse 101 CH-6370 Stans Switzerland as a DESIGN ORGANISATION approved according to Part 21, Section A, Subpart J. CONDITIONS : 1. The approval is limited to that specified in the enclosed Terms of Approval, and 2. This approval requires compliance with the procedures specified in the Design Organisation Handbook, reference EZ-DOA-00-1001, in the latest revision, and 3. This approval is valid whilst the approved Design Organisation remains in compliance with Part 21, Section A, Subpart J. 4. Subject to compliance with the foregoing conditions, this approval shall remain valid until surrendered or revoked. For the European Union Aviation Safety Agency, Date of issue: 20/03/2020 Hans LUNDSTRÖM Senior DOA Team Leader Ref. Ares(2020)1791504 - 27/03/2020

Transcript of W/> dh^ /Z Z &d >d X...W P í } ( í WWZKs > Zd/&/ d ^ X î í: X ï ñ ó W µ µ v } Z P µ o ] }...

Page 1: W/> dh^ /Z Z &d >d X...W P í } ( í WWZKs > Zd/&/ d ^ X î í: X ï ñ ó W µ µ v } Z P µ o ] } v ~ h î ì í ô l í í ï õ v ~ h ó ð ô l î ì í î v µ i } Z } v ] ]

TE.DOA.00830-005© European Union Aviation Safety Agency. All rights reserved. ISO9001 Certified. Proprietary document. Copies are not controlled.Confirm revision status through the EASA-Internet/Intranet.

An agency of the European Union

Page 1 of 1

APPROVAL CERTIFICATE

EASA.21J.357

Pursuant to Regulations (EU) 2018/1139 and (EU) 748/2012 and subject to the conditions specified below, the Agency hereby

certifies

PILATUS AIRCRAFT LTD. Ennetbürgerstrasse 101

CH-6370 Stans Switzerland

as a DESIGN ORGANISATION

approved according to Part 21, Section A, Subpart J.

CONDITIONS : 1. The approval is limited to that specified in the enclosed Terms of Approval, and 2. This approval requires compliance with the procedures specified in the Design Organisation

Handbook, reference EZ-DOA-00-1001, in the latest revision, and 3. This approval is valid whilst the approved Design Organisation remains in compliance with

Part 21, Section A, Subpart J. 4. Subject to compliance with the foregoing conditions, this approval shall remain valid until

surrendered or revoked. For the European Union Aviation Safety Agency, Date of issue: 20/03/2020

Hans LUNDSTRÖM Senior DOA Team Leader

Ref. Ares(2020)1791504 - 27/03/2020

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Terms of Approval 21J.357 Pilatus Aircraft Ltd

Issue 11, 20/03/2020

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Terms of Approval

Design Organisation Approval Certificate EASA.21J.357

1 Scope This Design Organisation Approval is applicable for the scope defined in Annex A and Annex B for design work with regard to the airworthiness, operational suitability and environmental characteristics of the products.

2 Privileges a) (Reserved)

b) (Reserved)

c) The holder of this design organisation approval shall be entitled, within the scope of this terms of

approval, and under the relevant procedures of the design assurance system: 1. to classify changes to a type-certificate or to a supplemental type-certificate and repair designs as

“major” or “minor”; 2. to approve minor changes to a type-certificate or to a supplemental type-certificate and minor

repair designs; 3. (Reserved); 4. (Reserved); 5. to approve certain major repair designs under Part 21, Section A, Subpart M to products or auxiliary

power units (APUs); 6. to approve for certain aircraft the flight conditions under which a permit to fly can be issued in

accordance with point 21.A.710(a)(2), except for permits to fly to be issued for the purpose of point 21.A.701(a)(15);

7. to issue a permit to fly in accordance with point 21.A.711(b) for an aircraft it has designed or modified, or for which it has approved, in accordance with point 21.A.263(c)(6), the flight conditions under which the permit to fly can be issued, and where the holder of this design organisation approval itself: (i) controls the configuration of the aircraft, and (ii) attests conformity with the design conditions approved for the flight;

Ref. Ares(2020)1791504 - 27/03/2020

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Terms of Approval 21J.357 Pilatus Aircraft Ltd

Issue 11, 20/03/2020

TE.DOA.00831-007 © European Union Aviation Safety Agency. All rights reserved. ISO9001 Certified. Proprietary document. Copies are not controlled. Confirm revision status through the EASA-Internet/Intranet.

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3 Obligations The holder of this design organisation approval shall, within the scope of this terms of approval: a) maintain the handbook required under point 21.A.243 in conformity with the design assurance system; b) ensure that this handbook or the relevant procedures included by cross-reference are used as a basic

working document within the organisation; c) determine that the design of products, or changes or repairs thereto comply with the applicable

specifications and requirements and have no unsafe features; d) provide the Agency with statements and associated documentation confirming compliance with point

(c), except for approval processes carried out in accordance with point 21.A.263(c); e) provide to the Agency data and information related to the actions required under point 21.A.3B; f) under the privilege of paragraph 2(c)(6), determine the flight conditions under which a permit to fly can

be issued; g) under the privilege of paragraph 2(c)(7), establish compliance with points (b) and (e) of point 21.A.711

before issuing a permit to fly to an aircraft; h) designate data and information issued under the authority of the approved design organisation within

the scope of its terms of approval as established by the Agency with the following statement: “The technical content of this document is approved under the authority of the DOA ref. EASA. 21J.357”.

Date of issue: 20/03/2020 Hans LUNDSTRÖM Senior DOA Team Leader

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Terms of Approval 21J.357 Pilatus Aircraft Ltd

Issue 11, 20/03/2020

TE.DOA.00831-007 © European Union Aviation Safety Agency. All rights reserved. ISO9001 Certified. Proprietary document. Copies are not controlled. Confirm revision status through the EASA-Internet/Intranet.

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Annex A

Scope of work

Legend:

Title for category of product Within scope Title for design scope Outside scope Title for design area

TC STC

maj

or c

hang

es

min

or c

hang

es

maj

or re

pair

s

min

or re

pairs

fligh

t con

ditio

ns

perm

it to

fly

(Powered) sailplaneAll scope (TCH)

All areas 1 1 1 1 1 1 1Structures (non-TCH activity)

Control surfaces / Moveables 1 1Empennage 1 1Engine mounts 1 1Fuselage 1 1Landing gears 1 1Support for external equipment 1 1Wings 1 1

Small aeroplaneAll scope (TCH)

All areas 1 1 1 1 1 1 1Structures (non-TCH activity)

Control surfaces / Moveables 1 1Empennage 1 1Engine mounts 1 1Fuselage 1 1Landing gears 1 1Support for external equipment 1 1Wings 1 1

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Terms of Approval 21J.357 Pilatus Aircraft Ltd

Issue 11, 20/03/2020

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List of products

Limitations

Product Design Activity Types(Powered) sailplane TC B4-PC11()

Small aeroplane TC

PC-12()PC-6()PC-24()

Limitations common to all products and activities

21J.3571. Development of Operational Suitability Data excludes the OSD constituents CCD and MCSD. 2. The privilege under paragraph 2(c)(5) is limited to the approval of the design of major repairs to products for which the DOA holds the type-certificate or the

Product Limitations particular to each product

(Powered) sailplaneFor non-TCH ac vity: NoneFor TCH ac vity: None

Small aeroplaneFor non-TCH ac vity: NoneFor TCH ac vity: None

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Terms of Approval 21J.357 Pilatus Aircraft Ltd

Issue 11, 20/03/2020

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Annex B [Not applicable]


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