Choose the experimental features you want to try

This document is an excerpt from the EUR-Lex website

Document 02011R1332-20160825

Consolidated text: Commission Regulation (EU) No 1332/2011 of 16 December 2011 laying down common airspace usage requirements and operating procedures for airborne collision avoidance (Text with EEA relevance)

ELI: http://data.europa.eu/eli/reg/2011/1332/2016-08-25

02011R1332 — EN — 25.08.2016 — 001.001


This text is meant purely as a documentation tool and has no legal effect. The Union's institutions do not assume any liability for its contents. The authentic versions of the relevant acts, including their preambles, are those published in the Official Journal of the European Union and available in EUR-Lex. Those official texts are directly accessible through the links embedded in this document

►B

COMMISSION REGULATION (EU) No 1332/2011

of 16 December 2011

laying down common airspace usage requirements and operating procedures for airborne collision avoidance

(Text with EEA relevance)

(OJ L 336 20.12.2011, p. 20)

Amended by:

 

 

Official Journal

  No

page

date

►M1

COMMISSION REGULATION (EU) 2016/583 of 15 April 2016

  L 101

7

16.4.2016




▼B

COMMISSION REGULATION (EU) No 1332/2011

of 16 December 2011

laying down common airspace usage requirements and operating procedures for airborne collision avoidance

(Text with EEA relevance)



Article 1

Subject matter and scope

This Regulation lays down common airspace usage requirements and operating procedures for airborne collision avoidance to be fulfilled by:

(a) 

operators of aircraft referred to under Article 4(1)(b) and (c) of Regulation (EC) No 216/2008 undertaking flights into, within or out of the Union; and

(b) 

operators of aircraft referred to under Article 4(1)(d) of Regulation (EC) No 216/2008 undertaking flights within the airspace above the territory to which the Treaty applies as well as in any other airspace where Member States apply Regulation (EC) No 551/2004 of the European Parliament and of the Council ( 1 ).

Article 2

Definitions

For the purposes of this Regulation the following definitions shall apply:

(1) 

‘airborne collision avoidance system (ACAS)’ means an aircraft system based on secondary surveillance radar (SSR) transponder signals which operates independently of ground-based equipment to provide advice to the pilot on potential conflicting aircraft that are equipped with SSR transponders;

(2) 

‘airborne collision avoidance system II (ACAS II)’ means an airborne collision avoidance system which provides vertical resolution advisories in addition to traffic advisories;

(3) 

‘resolution advisory (RA) indication’ means an indication given to the flight crew recommending a manoeuvre intended to provide separation from all threats or a manoeuvre restriction intended to maintain existing separation;

(4) 

‘traffic advisory (TA) indication’ means an indication given to the flight crew that the proximity of another aircraft is a potential threat.

Article 3

Airborne collision avoidance system (ACAS)

1.  
The aeroplanes referred to in Section I of the Annex to this Regulation shall be equipped with and operated in accordance with the rules and procedures as specified in the Annex.
2.  
Member States shall ensure that operation of aeroplanes referred to in Article 1(2)(a) of Regulation (EC) No 216/2008 comply with the rules and procedures specified in the Annex in accordance with the conditions set out in that Article.

▼M1 —————

▼B

Article 5

Entry into force and application

1.  
This Regulation shall enter into force on the 20th day following its publication in the Official Journal of the European Union.

▼M1

2.  
Article 3 shall apply as of 1 March 2012.
3.  
By way of derogation from paragraph 2, in the case of aircraft with an individual certificate of airworthiness issued before 1 March 2012, Article 3 shall apply as of 1 December 2015.

▼B

This Regulation shall be binding in its entirety and directly applicable in all Member States.

▼M1




ANNEX

Airborne collision avoidance systems (ACAS) II

(Part-ACAS)

AUR.ACAS.1005 Performance requirement

(1) The following turbine-powered aeroplanes shall be equipped with collision avoidance logic version 7.1 of ACAS II:

(a) 

aeroplanes with a maximum certificated take-off mass exceeding 5 700 kg;

(b) 

aeroplanes authorised to carry more than 19 passengers.

(2) Aircraft not referred to in point 1 which are equipped on a voluntary basis with ACAS II shall have collision avoidance logic version 7.1.

(3) Point 1 shall not apply to unmanned aircraft systems.

AUR.ACAS.1010 ACAS II training

Operators shall establish ACAS II operational procedures and training programmes so that the flight crew is appropriately trained in the avoidance of collisions and becomes competent in the use of ACAS II equipment.



( 1 )  OJ L 96, 31.3.2004, p. 20.

Top