In the SRM, the Figure 104... Is from the Allowable Damage pague block. Is from the Repairs block. Is from the identification. Is defined as structure which carriles flight loads? Secondary Structure. Miscelaneus Structure. Primary Structure. Trose fastener that require destroying part or all of the fastener when removing it from the airplane are... Removable Fastener. Permanent Fastener. Structural Fastener. How the changed data is identified? By a Revision Bar (Line) at the Rigth Side of each New or changed page. By a Revision Bar at the Left side of each New or changed page. By a Revision Code at the Left side of each New or changed page. The page block 001-099 is about? Sealant Aplicación. Protective Treatment. Identification. There are two básic formats of the RSM's Out of Production Airplanes are in the... New Format Old Format . The page block 201-999 is about? Fuselage Stations Diagram. Cabin Windows. Repairs. The normal revision time for SRM's is... Every 180 days for in-production airplanes. Every 90 days for in-production airplanes. Every 90 days for out of production airplanes. Which repair meets all regulatory requirements and have no inspections required? Permanent repairs category B. Permanent repairs category A. Time-limeted repairs category C. The RSM boeing meets the especificación. FAA. Air Transport Association Specification number 100. Air Transport Association Specification number 104. The page block 101-199 is about? Fastener Alternatives. Flap Peening. Allowable Damage Limits. Wheen marking repairs side of fuel tack, the commonly used sealant is? BMS 5-95 BMS 5-26 BMS 5-29. The distance from the Center of the fastener hole yo the nearest edge of the part is known as? Revet Pitch. Edge Pitch. Edge Margin. Within the old format SRM's the Allowable Damage data is provided... In page 201 to 299. In the begnning of each Chapter. In each Section. According to tree elements system the Second Element is for? The Page block. The Figure. The Section. Which document gives data on procedures and processes used on the manufacturing of Boeing airplanes... Overhaul Manuel. BMS Boeing Materials Specification. BMS Boeing Process Specification. Most of the metal used in the structurel of the airplane is? Titanium Alloys. Corresion Resistant Stell (CRES). Aluninum Alloy. Those ítems which have no repair figure give are considered to be... Repairable y Replacement. No Repairable and Non repairable. Within Limits.
