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民航规章 CIVIL AVIATION REGULATIONS 2

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(1) Meet the applicable minimum performance requirements of the Authority; and
(2) Not contain Halon 1211, Halon 1301, or Halon 2402.
Note 1:  The substances listed in (a)(2) above of Halon 1211, Halon 1301, and Halon 2402 are listed Annex A, Group II of the Montreal Protocol on Substances that Deplete the Ozone Layer, 8th Edition, 2009, which is listed in ICAO Annex 6, Part I: 6.2.2.1; ICAO Annex 6, Part II, Section II: 2.4.2.3, and ICAO Annex 6, Part III, Section III: 4.1.3.2.
Note 2:  Information concerning extinguishing agents is contained in the UNEP Halons Options Committee Technical Note Number 1 – New Technology Halon Alternatives and FAA Report Number DOT/FAA/AR-99-63, Options to the Use of Halons for Aircraft Fire Suppression Systems.
ICAO Annex 6, Part I: 6.2.2(b); 6.2.2.1
ICAO Annex 6, Part II, Section II: 2.4.2.2(b); 2.4.2.3
ICAO Annex 6, Part III, Section II: 4.2.2(b)
ICAO Annex 6, Part III, Section III: 4.1.3.1(b); 4.1.3.2
ICAO Annex 8, Part II, Chapter 1: 1.2.5
14 CFR: 91.513(c)(2);121.309(c), 135.155
JAR-OPS 1: 1.790
JAR OPS 3: 3.790
7.9.1.7 LAVATORY FIRE EXTINGUISHER
(a) [AAC] No person may operate an aircraft unless each lavatory in the aircraft is equipped with a built-in fire extinguisher for each disposal receptacle for towels, paper, or waste located within the lavatory.
(b) [AAC] Built-in lavatory fire extinguishers shall be designed to discharge automatically into each disposal receptacle upon occurrence of a fire in the receptacle.
(c) [AAC] Any agent used in a built-in fire extinguisher for each lavatory disposal receptacle for towels, or waste in an aircraft for which the individual certificate of airworthiness is first issued on or after 31 December 2011 shall:
(1) Meet the applicable minimum performance requirements of the Authority; and
(2) Not contain Halon 1211, Halon 1301, or Halon 2402.
Note 1:  The substances listed in (a)(2) above of Halon 1211, Halon 1301, and Halon 2402 are listed Annex A, Group II of the Montreal Protocol on Substances that Deplete the Ozone Layer, 8th Edition, 2009, which is listed in ICAO Annex 6, Part I: 6.2.2.1; ICAO Annex 6, Part II, Section II: 2.4.2.3, and ICAO Annex 6, Part III, Section III: 4.1.3.2.
Note 2:  Information concerning extinguishing agents is contained in the UNEP Halons Options Committee Technical Note No1 – New Technology Halon Alternatives and FAA Report no. Dot/FAA/AR-99-63, Options to the Use of Halons for Aircraft Fire Suppression Systems.
ICAO Annex 6, Part I: 6.2.2.1
ICAO Annex 6, Part II, Section II: 2.4.2.3
ICAO Annex 6, Part III, Section III: 4.1.3.2
ICAO Annex 8, Part II, Chapter 1: 1.2.5
14 CFR: 25.854; 121.308(b)
7.9.1.8 LAVATORY SMOKE DETECTOR
(a) [AOC] No person may operate a passenger-carrying transport category aeroplane unless each lavatory in the aeroplane is equipped with a smoke detector system or equivalent that provides—
(1) A warning light in the cockpit; or
(2) A warning light or audio warning in the passenger cabin which would be readily detected by a cabin crew member, taking into consideration the positioning of cabin crew members throughout the passenger compartment during various phases of flight.
14 CFR: 25.854; 121.308(a)
7.9.1.9 CRASH AXE
(a) [AAC] No person shall operate an  aeroplane certificated with a take-off mass of 5 700 kg or more unless it is equipped with a crash axe appropriate for effective use in that type of aeroplane, stored in a place not visible to passengers on the aeroplane.
14 CFR: 91.513(e); 121.309, 135.177
JAR-OPS 1: 1.795
7.9.1.10 MARKING OF BREAK-IN POINTS
(a) [AAC] If areas of the fuselage suitable for break-in by rescue crews in an emergency are marked on an aeroplane, such areas shall be marked as shown below, and the colour of the markings shall be red or yellow and, if necessary, they shall be outlined in white to contrast with the background.
(b)  If the corner markings are more than 2 m apart, intermediate lines 9 cm x 3 cm shall be inserted so that there is no more than 2 m between adjacent markings.
ICAO Annex 6, Part I: 6.2.4.1; 6.2.4.2
ICAO Annex 6, Part II, Section II: 2.4.2.2(b)
ICAO Annex 6, Part III, Section II: 4.2.4
ICAO Annex 6, Part III, Section III: 4.1.4.1; 4.1.4.2
14 CFR: 121.310(g)
JAR-OPS 1: 1.800
JAR OPS 3: 3.800
7.9.1.11 FIRST-AID KIT AND UNIVERSAL PRECAUTION KIT
(a) First Aid Kits.
(1) No person may operate the following aircraft unless it is it is equipped with an accessible, approved first-aid kit(s):
(i) [AAC - Aeroplane] Aeroplanes with a maximum certificated take-off weight of over 5 700 kg;
(ii) [AOC] - All AOC holders.
(2) The contents of first-aid kits to be carried shall comply with IS: 7.9.1.11.
(3) Each aircraft shall carry first-aid kits in accordance with at least the following schedule:
Number of Passenger Seats Number of
First-Aid Kits
0-100 1
101-200 2
201-300 3
301-400 4
401-500 5
More than 500 6
(4) The location of first aid kits should be:
(i) Distributed evenly throughout the aircraft;
(ii) Readily accessible to cabin crew members, if cabin crew members are required for flight; and
(iii) Located near the aircraft exits should their use be required outside the aircraft in an emergency situation.
(b) Universal Precaution Kit.
(1) No person shall operate an aircraft that requires a cabin crew member unless it is equipped with at least one universal precaution kit.
(2) The contents of universal precaution kits to be carried shall comply with IS: 7.9.1.11.
(3) Each aircraft shall carry universal precaution kits in accordance with the following:
(i) Two kits; and
(ii) Additional kits, as determined by the Authority, at times of increased public health risk, such as during an outbreak of a serious communicable disease having pandemic potential.
ICAO Annex 6, Part I: 6.2.2(a); Attachment B: 2.1; 2.2
ICAO Annex 6, Part II, Section III: 3.6.2.1(b)
ICAO Annex 6, Part III, Section II: 4.2.2(a)
ICAO Annex 6, Part III, Section III: 4.1.3.1(a)
ICAO Doc.  9388: 2.4.1.7
14 CFR: 121.803(c)(1); 121 Appendix A; 135.177
JAR-OPS 1: 1.745
JAR OPS 3: 3.745
7.9.1.12 EMERGENCY MEDICAL KIT - AEROPLANES
(a) [AOC] No person may operate a passenger flight in an aeroplane with 30 seats or more unless the aeroplane is equipped with an approved emergency medical kit for treatment of injuries or medical emergencies that might occur during flight time or in minor accidents.
(b) [AOC] The contents of emergency medical kits to be carried shall comply with IS: 7.9.1.12.
(c) [AOC] The medical kit shall be stored in a secure location.
ICAO Annex 6, Part I: 6.2.2(a)
14 CFR: 121.803(c)(2)(3); 121, Appendix A; 135.177
JAR-OPS 1: 1.755
7.9.1.13 OXYGEN STORAGE AND DISPENSING APPARATUS
(a) [AAC] All aircraft intended to be operated at altitudes requiring the use of supplemental oxygen shall be equipped with adequate oxygen storage and dispensing apparatus.
(b) [AAC] The oxygen apparatus, the minimum rate of oxygen flow, and the supply of oxygen shall meet applicable airworthiness standards for type certification in the transport category as specified by the Authority.
(c) [AAC] No person may operate an aircraft at altitudes above 10,000 feet unless it is equipped with oxygen masks, located so as to be within the immediate reach of flightcrew members while at their assigned duty station.
(d) [AAC] No person may operate a pressurised aeroplane at altitudes above 25,000 feet unless:
(1) Flightcrew member oxygen masks are available at the flight duty station and are of a quick donning type;
(2) Sufficient spare outlets and masks and/or sufficient portable oxygen units with masks are distributed evenly throughout the cabin to ensure immediate availability of oxygen to each required cabin crew member regardless of his location at the time of cabin pressurisation failure
(e) [AAC] An oxygen-dispensing unit connected to oxygen supply terminals is installed so as to be immediately available to each occupant, wherever seated.  The total number of dispensing units and outlets shall exceed the number of seats by at least 10%.  The extra units are to be evenly distributed throughout the cabin.
(f) [AAC] The amount of supplemental oxygen for sustenance required for a particular operation shall be determined on the basis of flight altitudes and flight duration, consistent with the operating procedures established for each operation in the Operations Manual and with the routes to be flown, and with the emergency procedures specified in the Operations Manual.
(g) [AAC]  The process to determine the amount of supplemental oxygen needed for non-pressurised and pressurised aircraft is contained in IS: 7.9.1.13.
ICAO Annex 6, Part I: 4.3.8; 4.3.8.1; 4.3.8.2; 4.4.5.2, 4.4.6, 6.7; 6.7.1, 6.7.2; 6.7.3; 6.7.4R; 6.7.5; 6.7.6R
ICAO Annex 6, Part II, Section II: 2.4.6.1; 2.4.6.2
ICAO Annex 6, Part II, Section III: 3.6.3.6.2; 3.6.3.6.3, Attachment 2A
ICAO Annex 6, Part III, Section II: 2.3.8; 2.3.8.1; 2.3.8.2; 4.8.1; 4.8.2; 4.8.3; 4.8.4R
ICAO Annex 6, Part III, Section III: 2.9; 2.9.1; 2.9.2; 4.5.1; 4.5.2R
ICAO Doc.  9388: 2.4.1.15, 2.4.1.16(a)
14 CFR: 91.211;121.327-329, 135.157
JAR-OPS 1: 1.770, 1.775
JAR OPS 3: 3.775
7.9.1.14 PROTECTIVE BREATHING EQUIPMENT
(a) [AOC] No AOC holder may operate an aeroplane with a maximum certified takeoff mass exceeding 5700 kg. or having a maximum approved seating configuration of more than 19 seats unless—
(1) It has PBE to protect the eyes, nose and mouth of each flight crew member while on flight deck duty and to provide oxygen for a period of not less than 15 minutes; and
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