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2、REMOVE BURRS AND BREAK SHARP EDCES. FOR DESIGN FEA= PURPOSES,THIS STANMRD TARES PRECEDENCE OVER BEFERENCE DOCuME(“S SHALL BE OF THE ISSUE IN EFFECT ON DATE OF NVITATION Hp BID. THIS IS A DESIGN STANDARD. NOT TO BE SED AS A PART NUMBER. M3TiiOD OF ATiAC“T OF CONNECTION TO AIRCRAFT STRwrpuRE OPTIONAL.
3、 INSTALUTION MVST BE SEAIED To HAIKPAIN HIESSURE CONNECTION MVST BE ACCESSIBLE AND HAVE TiiE lUQU“D MNIMM CIEARANCE ZN aPm TO PERMIT BEMOVAI CAP AND CONNECTION OF COWARTMEW IEAIUQ?, lEST EQIFHEW A CAP WITH SEALING GASKET SHALL BE PBOVIDED AND ATIIACHEDM THE AIBCRAFT FLMIBIE CHAIN. XCWNE EFEBENCE Vmr
4、 A =IN. a OF * PROVISIOS OF THIS STANMRD ARE TE SUBJECT OF I“AT1ONAL STANMRDITdMa 17/33 AND STANAG 3315.WHEN MENTAL CUSTODIANS WILL INFORM &BIR BEspecTIvE DEPARTMENTAL STANDARDIZATXM OFPICE Sb TK4T APPROPRIATE ACTION MY BE TAKEN BEsm TBE InIBRNATIONAL AGBEKNEaI -. REVISION OR CANCELUTION OF THIS STA- Is PPOPOSED TLIE DEPART- m REVISED AND REDRAWN Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-
