SAFA Ramp Inspections - Code7700

SAFA Ramp Inspection ProceduresGuidance materialInspection Item Std. Cat. Std. ref. Standard’s Text Pre-described Finding PDF code Instructions for completing thedetailed descriptionB09 I 2 A6-I-4.3.8.1 A flight to be operated at flight altitudes at which theatmospheric pressure in personnel compartments will beless than 700 hPa shall not be commenced unlesssufficient stored breathing oxygen is carried to supply:a) all crew members and 10 per cent of the passengersfor any period in excess of 30 minutes that the pressure incompartments occupied by them will be between 700 hPaand 620 hPa; andb) the crew and passengers for any period that theatmospheric pressure in compartments occupied by themwill be less than 620 hPa.A6-I-6.7.1 An aeroplane intended to be operated at flight altitudes atwhich the atmospheric pressure is less than 700 hPa inpersonnel compartments shall be equipped with oxygenstorage and dispensing apparatus capable of storing anddispensing the oxygen supplies required in Annex 6 Part IA8-IIIA-8.3A8-V-6.3A8-IIIB-6.3Chapter 4.3.8.1.Prescribed safety and survival equipment that the crew orpassengers are expected to use or operate at the time ofan emergency shall be reliable, readily accessible andeasily identified, and its method of operation shall beplainly marked.B09 I 3 A6-I-6.7.5 An aeroplane intended to be operated at flight altitudes atwhich the atmospheric pressure is less than 376 hPa, orwhich, if operated at flight altitudes at which theatmospheric pressure is more than 376 hPa, cannotdescend safely within four minutes to a flight altitude atwhich the atmospheric pressure is equal to 620 hPa andfor which the individual certificate of airworthiness is firstissued on or after 9 November 1998, shall be providedwith automatically deployable oxygen equipment to satisfythe requirements of Annex 6 Part I Chapter 4.3.8.2. Thetotal number of oxygen dispensing units shall exceed thenumber of passenger and cabin crew seats by at least 10per cent.B09 I 3 A6-I-6.7.5 An aeroplane intended to be operated at flight altitudes atwhich the atmospheric pressure is less than 376 hPa, orwhich, if operated at flight altitudes at which theatmospheric pressure is more than 376 hPa, cannotdescend safely within four minutes to a flight altitude atOxygen equipmentnot readily accessibleand required for thetype of flightAeroplane notequipped with anautomatic deployableoxygen system(individual CofAissued on or after 9November 1998) andflight planned aboveFL 250Insufficient number ofrequired serviceableautomatic deployableoxygen dispensingunits - individual CofAB09-02 Indicate the particulars of thesituation observedB09-03B09-04 Indicate the particulars of thesituation observedSAFA Coordination Section Page 156 of 217© European Aviation Safety Agency, 2012 V 2.0