| ANGLE | 90.0 DEGREES NOMINAL |
| CRITICALITY CODE JUSTIFICATION | FEAT |
| FIRST LEG LENGTH | 3.187 INCHES NOMINAL |
| HEAT TREATMENT | ANNEALED |
| OVERALL WIDTH | 1.125 INCHES NOMINAL |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | JAW,CLAMPING SEALING STRIP ANCHOR |
| MATERIAL | STEEL COMP 6150 |
| SECOND LEG LENGTH | 0.875 INCHES NOMINAL |
| SECOND LEG THICKNESS | 0.375 INCHES NOMINAL |
| SPECIFICATION/STANDARD DATA | 05047-ASME Y14.5M-1982 PROFESSIONAL/INDUSTRIAL ASSOCIATION STANDARD AND 05047-ASME B46.1 PROFESSIONAL/INDUSTRIAL ASSOCIATION STANDARD AND 96906-MIL-STD-130 GOVERNMENT STANDARD |
| SPECIAL FEATURES | THE ITEM SPECIFIED BY DRAWING 11-30635 WILL BE USED AS A PART OF A SYSTEM SUPPORTING THE LAUNCH AND OR RECOVERY OF AIRCRAFT AND IS ESSENTIAL TO SYSTEM PERFORMANCE OR OPERATION OR THE PRESERVATION OF LIFE OR SAFETY OF OPERATING PERSONNEL; ITEM HAS BEEN DESIGNATED AS CRITICAL APPLICATION ITEM (CAI); ANY DEVIATION FROM DRAWING WITHOUT WRITTEN APPROVAL FROM THE NAVAL AIR SYSTEMS COMMAND (NAVIAR), SUPPORT EQUIPMENT AND AIRCRAFT LANCH AND RECOVERY EQUIPMENT (SE AND ALRE) DEPARTMENT, IS STRICTLY PROHIBITED |
| SUPPLEMENTARY FEATURES | MATERIAL TO BE I/A/W SPEC ASTM A322,GRADE STEEL 6150 ANNEALED OR SAE AMS 4350M; HEAT TREAT I/A/W AMS 2759/1 SO THAT FINISHED PART HAS A HARDNESS OF HRC 41 TO 45;EACH FINISHED PART SHALL BE 100% MAGNETIC PARTICLE INSPECTED I/A/W ASTM E1444/E1444M PERFORMED BY BOTH CIRCULAR AND LONGITUDINAL METHOD;THE WET PROCESS SHALL BE USED; PARTS MUST MEET REQUIREMENTS OF MIL-STD-2035 EXCEPT NO INDICATIONS GREATER THAN .062" ARE ACCEPTABLE |