SAFA Ramp Inspections - Code7700

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SAFA Ramp Inspection ProceduresGuidance materialInspection Item Std. Cat. Std. ref. Standard’s Text Pre-described Finding PDFcodeinoperative. Where the State of the Operator is notthe State of Registry, the State of the Operator shallensure that the MEL does not affect the aeroplane’scompliance with the airworthiness requirementsapplicable in the State of Registry.B01 M 3 Galley/lavatory wastereceptacle access doorcover inoperative (outsideMEL limits)Instructions forcompleting the detaileddescriptionB01-11 Indicate the particulars ofthe situation observedB01 M 1 Damaged wall panels B01-12 Indicate the particulars ofthe situation observedB01 M 3 (E)TSO-C175SAE AS8056EUROCAE ED-121For new models of carts identified and manufacturedafter 4 November 2005:The brake system shall hold the fully loaded cart, inthe forward and aft orientation, stationary on an 11degree slope carpeted with low-pile carpetrepresentative of that used by the airlines.Obviously defective brakesof service cart(s)B01 M 3 Covers damaged/missingexposing sharp edges and/orcables and wiresB01 M 3 Overhead bins unserviceable(and not identified as such)B01-13 Indicate the particulars ofthe situation observedB01-14 Indicate the particulars ofthe situation observedB01-15 Indicate the particulars ofthe situation observedSAFA Coordination Section Page 126 of 217© European Aviation Safety Agency, 2012 V 2.0
SAFA Ramp Inspection ProceduresGuidance materialInspection Item Inspections Item Title Inspecting InstructionsB02 Cabin Attendant's Station/CrewRest AreaCheck general condition and serviceability of the cabin crew seats.Note: If a cabin crew seat is found unserviceable check against MEL and check if the number of serviceable ones canaccommodate the minimum required number of cabin crew members (information available in the OperationsManual).Note: If a cabin crew seat is found not to retract automatically impeding the rapid evacuation of the aeroplane in anemergency, this finding should be addressed under the item B12 – Access to emergency exit.Check presence and condition of the safety harness and/or belt.Note: Aeroplanes for which the individual CofA was issued on or after 1 January 1981 must be fitted with safety harnessesfor the use of cabin crew members.Check accessibility of life jackets.Check the serviceability of the communication system (Cockpit to Cabin and Cabin to Cabin). In case of unserviceability,check against the MEL.Inspection Item Std. Cat. Std. ref. Standard’s Text Pre-described Finding PDFcodeB02 I 1 A6-I-6.16.1 6.16.1 Aeroplanes for which the individualcertificate of airworthiness is first issued on orafter 1 January 1981Strap or buckle worn ordamagedInstructions forcompleting the detaileddescriptionB02-01 Indicate the particulars ofthe situation observedAll aeroplanes shall be equipped with a forwardor rearward facing (within 15 degrees of thelongitudinal axis of the aeroplane) seat, fitted witha safety harness for the use of each cabin crewmember required to satisfy the intent of 12.1 inrespect of emergency evacuation.B02 I 2 A6-I-6.16.1 6.16.1 Aeroplanes for which the individualcertificate of airworthiness is first issued on orafter 1 January 1981Cabin Crew seat(s) notequipped with safetyharness (only seat belt)B02-02 Indicate the particulars ofthe situation observedAll aeroplanes shall be equipped with a forwardor rearward facing (within 15 degrees of thelongitudinal axis of the aeroplane) seat, fitted witha safety harness for the use of each cabin crewmember required to satisfy the intent of 12.1 inrespect of emergency evacuation.B02 I 2 A6-I-6.5.2 6.5.2.1 Landplanes shall carry the equipmentprescribed in 6.5.2.2:Cabin Crew life jackets(when required) not easilyaccessibleB02-03SAFA Coordination Section Page 127 of 217© European Aviation Safety Agency, 2012 V 2.0
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SAFA Ramp Inspections - Code7700

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