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SAFA Ramp Inspections - Code7700

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<strong>SAFA</strong> <strong>Ramp</strong> Inspection ProceduresGuidance materialInspectionItemStd. Cat. Std. ref. Standard’s Text Pre-described Finding PDFcodeRegistryA03 I 3 A6-I-6.18.2 From 1 January 2005, all turbine-engined aeroplanes of a maximumcertificated take-off mass in excess of 5 700 kg or authorized to carrymore than 19 passengers shall be equipped with an airborne collisionavoidance system (ACAS II).A03 I 2 A2-2.3.1 2.3.1 Responsibility of pilot-in-commandThe pilot-in-command of an aircraft shall, whether manipulatingthe controls or not, be responsible for the operation ofthe aircraft in accordance with the rules of the air, except thatthe pilot-in-command may depart from these rules in circumstancesthat render such departure absolutely necessary in theinterests of safety.A03 I 3 A6-I-4.3.1 A flight shall not be commenced until flight preparation forms havebeen completed certifying that the pilot-in command is satisfied that:b) the instruments and equipment prescribed in Chapter 6, for theparticular type of operation to be undertaken, are installed and aresufficient for the flight.ACAS II N/A or U/S (outsideMEL limits)Aircraft with first CoA issued onor after 1 March 2012 notequipped with ACAS II,software version 7.1GPWS with forward lookingterrain avoidance function notinstalled or unserviceable(outside MEL limits)A6-I-6.15.4 From 1 January 2007, all turbine-engined aeroplanes of a maximumcertificated take-off mass in excess of 5 700 kg or authorized to carrymore than nine passengers shall be equipped with a groundproximity warning system which has a forward looking terrainavoidance function.A6-I-6.15.6 From 1 January 2007, all piston-engined aeroplanes of a maximumcertificated take-off mass in excess of 5 700 kg or authorized to carrymore than nine passengers shall be equipped with a groundproximity warning system which provides the warnings in 6.15.8 a)and c), warning of unsafe terrain clearance and a forward lookingterrain avoidance function.A6-I-6.15.8 A ground proximity warning system shall provide, unless otherwisespecified herein, warnings of the following circumstances:a) excessive descent rate;b) excessive terrain closure rate;c) excessive altitude loss after take-off or go-around;d) unsafe terrain clearance while not in landing configuration:1) gear not locked down;2) flaps not in a landing position; ande) excessive descent below the instrument glide path.A03 I 3 EUR 3.2.1 All aircraft operating above FL 195 in the European Region shall be Radio channel spacing does A03-A03-02A03-03A03-04Instructions forcompleting thedetailed descriptionIndicate theparticulars of thesituation observedIndicate theparticulars of thesituation observedIndicate if no systemat all was found or ifthe forward lookingfunction is missing. Ifunserviceable,specify the reason.<strong>SAFA</strong> Coordination Section Page 43 of 217© European Aviation Safety Agency, 2012 V 2.0

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