時(shí)間：2015-01-22 15:18來源：藍(lán)天飛行翻譯公司 作者：民航翻譯 點(diǎn)擊：次
|
To view this page ensure that Adobe Flash Player version 9.0.124 or greater is installed. (2) It has sufficient portable PBE to protect the eyes, nose and mouth of all required cabin crew members and to provide breathing gas for a period of not less than 15 minutes. (b) [AOC] The oxygen supply for PBE may be provided by the required supplemental oxygen system. (c) [AOC] The PBE intended for flight crew use shall be conveniently located on the flight deck and be easily accessible for immediate use by each required flight crew member at their assigned duty station. (d) [AOC] The PBE intended for cabin crew use shall be installed adjacent to each required cabin crew member duty station. (e) [AOC] Easily accessible portable PBE shall be provided and located at or adjacent to the required hand fire extinguishers except that, where the fire extinguisher is located inside a cargo compartment, the PBE shall be stowed outside but adjacent to the entrance to that compartment. (f) [AOC] The PBE while in use shall not prevent required communication. 14 CFR: 121.337 JAR-OPS 1: 1.780 7.9.1.15 FIRST AID OXYGEN DISPENSING UNITS (a) [AOC] No AOC holder may conduct a passenger carrying operation in a pressurised aeroplane at altitudes above 25,000 feet, when a cabin crew member is required to be carried, unless it is equipped with— (1) Undiluted first-aid oxygen for passengers who, for physiological reasons, may require oxygen following a cabin depressurisation; and (2) A sufficient number of dispensing units, but in no case less than two, with a means for cabin crew to use the supply. (b) [AOC] The amount of first-aid oxygen required in paragraph (a) for a particular operation and route shall be determined on the basis of— (1) Flight duration after cabin depressurisation at cabin altitudes of more than 8,000 feet; (2) An average flow rate of at least 3 litres Standard Temperature Pressure Dry (STPD)/minute/person; and (3) At least 2% of the passengers carried, but in no case for less than one person. (c) The amount of first-aid oxygen required for a particular operation shall be determined on the basis of cabin pressure altitudes and flight duration, consistent with the operating procedures established for each operation and route. (d) The oxygen equipment provided shall be capable of generating a mass flow to each user of at least four litres per minute, STPD. Means may be provided to decrease the flow to not less than two litres per minutes, STPD, at any altitude. 14 CFR: 121.333(e)(3), 135.91 JAR-OPS 1: 1.760 7.9.1.16 MEGAPHONES (a) [AOC] Each person operating a passenger-carrying aeroplane shall have a portable battery-powered megaphone or megaphones readily accessible to the crew members assigned to direct emergency evacuation. (b) [AOC] The number and location of megaphones required in paragraph (a) shall be determined as follows: (1) On aeroplanes with a seating capacity of more than 60 and less than 100 passengers, one megaphone shall be located at the most rearward location in the passenger cabin where it would be readily accessible to a normal cabin crew member seat; and (2) On aeroplanes with a seating capacity of more than 99 passengers, two megaphones in the passenger cabin on each aeroplane one installed at the forward end and the other at the most rearward location where it would be readily accessible to a normal cabin crew member seat. (3) For aeroplanes with more than one passenger deck, in all cases when the total passenger seating configuration of a deck is more than 60, at least one megaphone is required on the deck. Note: The Authority may grant an exemption from the requirements of paragraph (b) if the Authority finds that a different location would be more useful for evacuation of persons during an emergency. 14 CFR: 91.513(f); 121.309(f) JAR-OPS 1: 1.810 7.9.1.17 INDIVIDUAL FLOTATION DEVICES (a) Landplanes. (1) [AAC] Landplanes shall carry the equipment prescribed in paragraph 2: (i) When flying en-route over water beyond gliding distance from the shore; (ii) When flying over water at a distance of more than 93 km (50 NM) away from the shore for aircraft capable of maintaining safe altitude after the failure of one engine for two-engine aircraft and the failure of two engines for three or four-engine aircraft.; or (iii) When taking off or landing at an aerodrome where the (Authority) has determined the takeoff or approach path is so disposed over water that in the event of a mishap there would be the likelihood of a ditching. (2) [AAC] One life-jacket or equivalent flotation device equipped with a means of electric illumination shall be carried for each person on board, stowed in a position easily accessible from the seat or berth of the person for whose use it is provided. (b) Seaplanes. (1) [AAC] For all flights, seaplanes shall be equipped with the equipment prescribed in paragraph 2. ICAO Annex 6: Part 1: 6.5.1(a), 6.5.2.1, 6.5.2.2, 6.5.3.2 ICAO Annex 6, Part II, Section II: 2.4.4.3.1; 2.4.4.3.2 ICAO Annex 6, Part III, Section III: 3.6.2.1 ICAO Doc. 9388: 2.4.1.12, 14 CFR: 121.339(a), 121.340(b) JAR-OPS 1: 1.825, 1.830, 1.835(c) 7.9.1.18 LIFE RAFTS (a) [AAC] In addition to the equipment prescribed in § 7. 9.1.17 and § 7. 9.1.19 of this Part, lifesaving rafts in sufficient numbers to carry all persons on board shall be installed in: (1) Aeroplanes operated on long range over-water flights, and (2) All other aeroplanes when they are operated over water away from land suitable for making an emergency landing at a distance of more than 185 km (100 NM) in the case of single-engine aeroplanes, and more than 370 km (200 NM) in the case of multi-engine aeroplanes capable of continuing flight with one engine inoperative. Note: Both 14 CFR and JAR OPS 1 set the limit at 30 minutes or 100 NM away from land suitable for making an emergency landing. (3) Class 1 and 2 helicopters when they are operated over water at a distance from land corresponding to more than 10 minutes at normal cruise speed. (4) Class 3 helicopters when they are operated over water beyond autorotational or safe forced landing distance from land. (b) [AOC] An aircraft shall have lifesaving rafts with a sufficient capacity to carry all persons on board in the event of the loss of one raft of the largest capacity. (c) All lifesaving rafts shall be stowed so as to facilitate their ready use in an emergency. (d) Life rafts shall be equipped with the following life sustaining equipment— (1) A electric survivor locator light; (2) A survival kit; (3) A pyrotechnic signaling device; and (4) An ELT (See § 7.9.1.5). (e) [AOC] In helicopters, life rafts which are not deployable by remote control and which have a mass of more than 40 kg shall be equipped with a means of mechanically assisted deployment. Note: The ELT requirement in 7.9.1.18(d)(4) is an FAA requirement and not an ICAO requirement. ICAO Annex 6, Part I: 6.5.3.1 ICAO Annex 6, Part II, Section II: 2.4.4.3.2 ICAO Annex 6, Part III, Section II: 4.5.2.1(b) ICAO Annex 6, Part III, Section III: 4.3.2.1(b) ICAO Doc. 9388: 2.4.2.7, 2.4.2.8 14 CFR: 91.509; 121.339(a); 135.167 JAR-OPS 1: 1.830(b) JAR OPS 3:3.380 7.9.1.19 FLOTATION DEVICE FOR HELICOPTER DITCHING (a) [AAC] All helicopters flying over water at a distance from land corresponding to more than 10 minutes at normal cruise speed in the case of performance Class 1 or 2 helicopters, or flying over water beyond auto-rotational or safe forced landing distance from land in the case of performance Class 3 helicopters, shall be fitted with a permanent or rapidly deployable means of floatation so as to ensure a safe ditching of the helicopter. ICAO Annex 6, Part III, Section II: 4.5.1 ICAO Annex 6, Part III, Section III: 4.3.1 JAR-OPS 3: 3.843 7.10 MISCELLANEOUS SYSTEMS AND EQUIPMENT 7.10.1.1 SEATS, SAFETY BELTS, AND SHOULDER HARNESSES (a) [AAC] Each aircraft used in passenger carrying operations shall be equipped with the following seats, safety belts, and shoulder harnesses that meet the airworthiness requirements for type certification of that aircraft: (1) A seat with safety belt for each person on board over an age to be determined by [STATE]; and a restraining belt for each berth on board the aircraft. (2) A safety harness for each flight crewmember seat. (i) The safety harness for each pilot seat shall incorporate a device, which will automatically restrain the occupant’s torso in the event of rapid deceleration. (ii) The safety harness for each pilot seat, which includes shoulder straps and a seat belt, should incorporate a restraining device to prevent a suddenly incapacitated pilot from interfering with the flight controls. (3) A forward or rearward facing (within 15 degrees of the longitudinal axis of the aeroplane) seat equipped with a safety harness for each cabin crew member station in the passenger compartment. (4) The cabin crew member’s seats shall be located near floor level and other emergency exits as required by the Authority for emergency evacuation. ICAO Annex 6, Part 1: 6.2.2, 6.16.1, 6.16.2, 6.16.3 ICAO Annex 6, Part II, Section II: 2.4.2.2(c);2.4.2.4R ICAO Annex 6, Part II, Section III: 3.6.2.1; 3.6.9.1;3.6.9.2R ICAO Annex 6, Part III, Section II, 4.2.2; 4.12.1; 4.12.2 ICAO Annex 6: Part III, Section III: 4.1.3.1(c); 4.1.3.3R 14 CFR: 23.785; 25,785; 91.521, 121.311 JAR-OPS 1: 1.730 JAR-OPS 3: 3.730 7.10.1.2 PASSENGER AND PILOT COMPARTMENT DOORS –AEROPLANES (a) [AOC] Pilot compartment door — (1) No person may operate a passenger carrying aeroplane of a maximum certificated takeoff mass in excess of 45 500 kg or with a passenger seating capacity greater than 60 unless that aircraft is equipped with an approved flight crew compartment door that is designed to resist penetration by small arms fire and grenade shrapnel, and to resist forcible intrusions by unauthorised persons. |
