CHAPTER 11. SECURITY
11.1 Aeroplanes used for domestic
Recommendation.— International Standards and Recom-
mended Practices set forth in this chapter should be applied by
all Contracting States for aeroplanes engaged in domestic
11.2 Least-risk bomb location
the type certificate to include a derivative type design is
submitted to the appropriate national authority, consideration
should be given to reinforcing the flight crew compartment
bulkheads, floors and ceilings so as to resist penetration by
small arms fire and grenade shrapnel and to resist forcible
intrusions, if these areas are accessible in flight to passengers
and cabin crew.
Note.— Standards and Recommended Practices concerning
the requirements for the flight crew compartment door in all
commercial passenger-carrying aeroplanes are contained in
Annex 6, Part I, Chapter 13.
For aeroplanes of a maximum certificated take-off mass in
excess of 45 500 kg or with a passenger seating capacity
greater than 60 and for which the application for certification
was submitted on or after 12 March 2000, consideration shall
be given during the design of the aeroplane to the provision of
a least-risk bomb location so as to minimize the effects of a
11.4 Interior design
11.3 Protection of the flight crew compartment
Recommendation.— In all aeroplanes, which are required by
Annex 6, Part I, Chapter 13 to have an approved flight crew
compartment door, and for which an application for amending
For aeroplanes of a maximum certificated take-off mass in
excess of 45 500 kg or with a passenger seating capacity
greater than 60 and for which the application for certification
was submitted on or after 12 March 2000, consideration shall
be given to design features that will deter the easy
concealment of weapons, explosives or other dangerous
objects on board aircraft and that will facilitate search
procedures for such objects.
CHAPTER 11. SECURITY11.1 Aeroplanes used for domesticRecommendation.— International Standards and Recom-mended Practices set forth in this chapter should be applied byall Contracting States for aeroplanes engaged in domestic11.2 Least-risk bomb locationthe type certificate to include a derivative type design issubmitted to the appropriate national authority, considerationshould be given to reinforcing the flight crew compartmentbulkheads, floors and ceilings so as to resist penetration bysmall arms fire and grenade shrapnel and to resist forcibleintrusions, if these areas are accessible in flight to passengersand cabin crew.Note.— Standards and Recommended Practices concerningthe requirements for the flight crew compartment door in allcommercial passenger-carrying aeroplanes are contained inAnnex 6, Part I, Chapter 13.For aeroplanes of a maximum certificated take-off mass inexcess of 45 500 kg or with a passenger seating capacitygreater than 60 and for which the application for certificationwas submitted on or after 12 March 2000, consideration shallbe given during the design of the aeroplane to the provision ofa least-risk bomb location so as to minimize the effects of a11.4 Interior design11.3 Protection of the flight crew compartmentRecommendation.— In all aeroplanes, which are required byAnnex 6, Part I, Chapter 13 to have an approved flight crewcompartment door, and for which an application for amendingFor aeroplanes of a maximum certificated take-off mass inexcess of 45 500 kg or with a passenger seating capacitygreater than 60 and for which the application for certificationwas submitted on or after 12 March 2000, consideration shallbe given to design features that will deter the easyconcealment of weapons, explosives or other dangerousobjects on board aircraft and that will facilitate searchprocedures for such objects.
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