SAFA Ramp Inspections - Code7700

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SAFA Ramp Inspection ProceduresGuidance materialInspection Item Std. Cat. Std. ref. Standard’s Text Pre-described Finding PDF code Instructions for completingthe detailed descriptionB07 I 3 A8-IIIA-4.1.7 Ch. 4.1.7 - Emergency landing provisions4.1.7.2 Facilities shall be provided for the rapid evacuation ofthe aeroplane in conditions likely to occur following anemergency landing. Such facilities shall be related to thepassenger and crew capacity of the aeroplane.Emergency exit sign(s)out of order (outside MELlimits).B07-04 Indicate the particulars ofthe situation observedA8-IIIA-8.3A8-V-6.3A8-IIIB-6.34.1.7.3 The interior layout of the cabin and the position andnumber of emergency exits, including the means of locatingand illuminating the escape paths and exits shall be such asto facilitate rapid evacuation of the aeroplane in conditionslikely to occur following an emergency landing.Prescribed safety and survival equipment that the crew orpassengers are expected to use or operate at the time of anemergency shall be reliable, readily accessible and easilyidentified, and its method of operation shall be plainly marked.A8-IIIB-8.4 8.4 EvacuationThe aeroplane shall be equipped with sufficient emergencyexits to allow maximum opportunity for cabin evacuationwithin an appropriate time period. Items to be consideredshall include:a) number of seats and seating configuration;b) number, location and size of exits;c) marking of exits and provision of instructions for use;d) likely blockages of exits;e) operation of exits; andA8-IIIB-4.6.2-4f) positioning and weight of evacuation equipment at exits,e.g. slides and rafts.4.6.2 Facilities shall be provided for the rapid evacuation ofthe aeroplane in conditions likely to occur following anSAFA Coordination Section Page 144 of 217© European Aviation Safety Agency, 2012 V 2.0
SAFA Ramp Inspection ProceduresGuidance materialInspection Item Std. Cat. Std. ref. Standard’s Text Pre-described Finding PDF code Instructions for completingthe detailed descriptionemergency landing. Such facilities shall be related to thepassenger and crew capacity of the aeroplane and shall beshown to be suitable for their intended purpose.4.6.3 The interior layout of the cabin and the position andnumber of emergency exits, including the means of locatingand illuminating the escape paths and exits, shall be such asto facilitate rapid evacuation of the aeroplane in conditionslikely to occur following an emergency landing.4.6.4 On aeroplanes certificated for ditching conditions,provisions shall be made in the design to give maximumpracticable assurance that safe evacuation from theaeroplane of passengers and crew can be executed in caseof ditching.B07 I 3 A8-IIIA-4.1.7 Ch. 4.1.7 - Emergency landing provisions4.1.7.2 Facilities shall be provided for the rapid evacuation ofthe aeroplane in conditions likely to occur following anemergency landing. Such facilities shall be related to thepassenger and crew capacity of the aeroplane.No means for illuminatingthe escape pathsB07-05 Indicate the particulars ofthe situation observedA8-IIIA-8.3A8-V-6.3A8-IIIB-6.34.1.7.3 The interior layout of the cabin and the position andnumber of emergency exits, including the means of locatingand illuminating the escape paths and exits shall be such asto facilitate rapid evacuation of the aeroplane in conditionslikely to occur following an emergency landing.Prescribed safety and survival equipment that the crew orpassengers are expected to use or operate at the time of anemergency shall be reliable, readily accessible and easilyidentified, and its method of operation shall be plainly marked.A8-IIIB-8.5 Emergency lighting shall be provided and shall have thefollowing characteristics:a) independence from main electrical supply;b) automatic activation upon loss of normal power/impact;c) visual indication of the path to emergency exits in smokefilledcabin conditions;d) illumination both inside and outside the aeroplane duringevacuation; ande) no additional hazard in the event of fuel spillage.SAFA Coordination Section Page 145 of 217© European Aviation Safety Agency, 2012 V 2.0
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