時(shí)間：2015-01-22 15:21來(lái)源：藍(lán)天飛行翻譯公司 作者：民航翻譯 點(diǎn)擊：次
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To view this page ensure that Adobe Flash Player version 9.0.124 or greater is installed. (i) Above the aisle near each over-the-wing passenger emergency exit, or at another ceiling location if it is more practical because of low headroom; (ii) Next to each floor level passenger emergency exit, except that one sign may serve two such exits if they both can be seen readily from that sign; and (iii) On each bulkhead or divider that prevents fore and aft vision along the passenger cabin, to indicate emergency exits beyond and obscured by it, except that if this is not possible, the sign may be placed at another appropriate location. (4) Each passenger emergency exit marking and each locating sign shall be manufactured to meet the interior emergency exit marking requirements under which the aeroplane was type certified, unless the Authority cites different requirements for compliance with this paragraph. Note: No sign may continue to be used if its luminescence (brightness) decreases to below 250 micro lamberts. (5) Sources of general cabin illumination may be common to both the emergency and the main lighting systems if the power supply to the emergency light system is independent of the power supply to the main lighting system. (6) The emergency lighting system shall provide enough general lighting in the passenger cabin so that the average illumination, when measured at 40-inch intervals at seat armrest height, on the centerline of the main passenger aisle, is at least 0.05 foot-candles. (7) Each emergency light shall— (i) Be operable manually both from the flightcrew station and from a point in the passenger compartment that is readily accessible to a normal cabin crew member seat; (ii) Have a means to prevent inadvertent operation of the manual controls; and (iii) When armed or turned on at either station, remain lighted or become lighted upon interruption of the aeroplane’s normal electric power. (iv) Provide the required level of illumination for at least 10 minutes at the critical ambient conditions after emergency landing. (v) Have a cockpit control device that has an "on", "off", and "armed" position. (8) The location of each passenger emergency exit operating handle and instructions for opening the exit shall be shown in accordance with the requirements under which the aeroplane was type certified, unless the Authority cites different requirements for compliance with this paragraph. (9) No operating handle or operating handle cover may continue to be used if its luminescence (brightness) decreases to below 100 micro lamberts. (10) Access to emergency exits shall be provided as follows for each passenger carrying aeroplane: (i) Each passageway between individual passenger areas, or leading to a Type I or Type II emergency exit, shall be unobstructed and at least 20 inches wide. (ii) There shall be enough space next to each Type I or Type II emergency exit to allow a crew member to assist in the evacuation of passengers without reducing the unobstructed width of the passageway below that required in paragraph (j)1 of this section. (iii) There shall be access from the main aisle to each Type III and Type IV exit. The access from the aisle to these exits shall not be obstructed by seats, berths, or other protrusions in a manner that would reduce the effectiveness of the exit. In addition, the access shall meet the emergency exit access requirements under which the aeroplane was type certificated, unless the Authority cites different requirements for compliance with this paragraph. (iv) If it is necessary to pass through a passageway between passenger compartments to reach any required emergency exit from any seat in the passenger cabin, the passageway shall not be obstructed. However, curtains may be used if they allow free entry through the passageway. (v) No door may be installed in any partition between passenger compartments. (vi) If it is necessary to pass through a doorway separating the passenger cabin from other areas to reach any required emergency exit from any passenger seat, the door shall have a means to latch it in open position, and the door shall be latched open during each takeoff and landing. The latching means shall be able to withstand the loads imposed upon it when the door is subjected to the ultimate inertia forces, relative to the surrounding structure, prescribed in the airworthiness standards for type certification in the transport category as cited by the Authority. (11) Each passenger emergency exit and the means of opening that exit from the outside shall be marked on the outside of the aeroplane with a 2-inch coloured band outlining the exit on the side of the fuselage. (12) Each passenger emergency exit marking, including the band, shall be readily distinguishable from the surrounding fuselage area by contrast in colour and shall comply with the following: (i) If the reflectance of the darker colour is 15 percent or less, the reflectance of the lighter colour shall be at least 45 percent. (ii) If the reflectance of the darker colour is greater than 15 percent, at least a 30 percent difference between its reflectance and the reflectance of the lighter colour shall be provided. Note: “Reflectance" is the ratio of the luminous flux reflected by a body to the luminous flux it receives. (iii) Exits that are not in the side of the fuselage shall have external means of opening and applicable instructions marked conspicuously in red or, if red is inconspicuous against the background colour, in bright chrome yellow and, when the opening means for such an exit is located on only one side of the fuselage, a conspicuous marking to that effect shall be provided on the other side. (13) Each passenger-carrying aeroplane shall be equipped with exterior lighting that meets the requirements under which that aeroplane was type certificated, unless the Authority cites different requirement for compliance with this paragraph. (14) Each passenger-carrying aeroplane shall be equipped with a slip-resistant escape route that meets the requirements under which that aeroplane was type certificated, unless the Authority cites different requirements for compliance with this paragraph. (15) Each floor level door or exit in the side of the fuselage (other than those leading into a cargo or baggage compartment that is not accessible from the passenger cabin) that is 44 or more inches high and 20 or more inches wide, but not wider than 46 inches, each passenger ventral exit and each tail cone exit, shall meet the requirements of this section for floor level emergency exits. Note: The Authority may grant a deviation from this paragraph if he finds that circumstances make full compliance impractical and that an acceptable level of safety has been achieved. (16) Approved emergency exits in the passenger compartments that are in excess of the minimum number of required emergency exits shall meet all of the applicable provisions of this subsection section and shall be readily accessible. (17) On each large passenger-carrying aeroplane with a ventral exit and tail cone exit shall be— (i) Designed and constructed so that it cannot be opened during flight; and (ii) Marked with a placard readable from a distance of 30 inches and installed at a conspicuous location near the means of opening the exit, stating that the exit has been designed and constructed so that it cannot be opened during flight. (18) Portable lights. No person may operate a passenger carrying aeroplane unless it is equipped with flight stowage provisions accessible from each cabin crew member seat. 14 CFR: 121.310 IS: 7.9.1.11 FIRST- AID KITS AND UNIVERSAL PRECAUTION KITS (a) The required first-aid kits shall include at least the following: (1) Antiseptic swabs (10/pack) (2) Bandage: adhesive strips (3) Bandage: gauze 7.5 cm × 4.5 m (4) Bandage: triangular; safety pins (5) Dressing: burn 10 cm × 10 cm (6) Dressing: compress, sterile 7.5 cm × 12 cm (7) Dressing: gauze, sterile 10.4 cm × 10.4 cm (8) Tape: adhesive 2.5 cm (roll) (9) Steri-strips (or equivalent adhesive strip) (10) Hand cleanser or cleansing towelettes (11) Pad with shield, or tape, for eye (12) Scissors: 10 cm [as allowed by national regulations] (13) Tape: Adhesive, surgical 1.2 cm × 4.6 m (14) Tweezers: splinter (15) Disposable gloves (multiple pairs) (16) Thermometers (non-mercury) (17) Mouth-to-mouth resuscitation mask with one-way valve (18) First-aid manual, current edition (19) Incident record form (20) Mild to moderate analgesic [as allowed by national regulations] (21) Antiemetic [as allowed by national regulations] (22) Nasal decongestant [as allowed by national regulations] (23) Antacid [as allowed by national regulations] (24) Antihistamine [as allowed by national regulations] (b) The required universal precaution kits shall include at least the following: (1) Dry powder that can convert small liquid spill into a sterile granulated gel (2) Germicidal disinfectant for surface cleaning (3) Skin wipes (4) Face/eye mask (separate or combined) (5) Gloves (disposable) (6) Protective apron (7) Large absorbent towel (8) Pick-up scoop with scraper (9) Bio-hazard disposal waste bag (10) Instructions. Note: The carriage of automated external defibrillators (AED) should be determined by operators or the Authority on the basis of a risk assessment taking into account the particular needs of the operation. ICAO Annex 6, Part I: Attachment B ICAO Annex 6, Part III, Attachment C IS: 7.9.1.12 EMERGENCY MEDICAL KIT – AEROPLANES (a) The required medical kit shall include the following equipment: (1) Stethoscope (2) Sphygmomanometer (electronic preferred) |
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