5340-01-144-2391 CLAMP,LOOP Index 4820-01-144-2393 SEAT,VALVE

National Stock Number:
9535-01-144-2392

Federal Supply Class:
9535

National Item Identification Number:
011442392

Description:
SHEET,METAL

Detail:
A FERROUS OR NONFERROUS PRODUCT WITH CROSS-SECTIONAL DIMENSIONS LIMITED TO THOSE ESTABLISHED IN APPENDIX C, FIIG A131. INCLUDES CORRUGATED AND PERFORATED ITEMS. FOR ITEMS 0.005 INCH OR .125MM THICK AND LESS. SEE FOIL, METAL. FOR SILVER ITEMS SEE SILVER SHEET.


Manufacturer Information:
AMS 489880U583SAE INTERNATIONAL
AMS 49180U583SAE INTERNATIONAL
AMS 49880U583SAE INTERNATIONAL
AMS-T-90460U583SAE INTERNATIONAL
AMS-T-904681343SOCIETY OF AUTOMOTIVE ENGINEERS INC
MIL-T-904681349MILITARY SPECIFICATIONS PROMULGATED BY MILITARY DEPARTMENTS/AGENCIES UNDER AUTHORITY OF DEFENSE STANDARDIZATION MANUAL 4120 3-M
MIL-T-9046,AB-3,CDA,0.063X36X9614153DEFENSE LOGISTICS AGENCY DBA DEFENSE SUPPLY CENTER PHILADELPHIA
MMS-120376301THE BOEING COMPANY


Techincal Specification:
BASIC SHAPE STYLESOLID
CROSS-SECTIONAL THICKNESS0.0630 INCHES NOMINAL
FABRICATION METHODHOT ROLLED
HEAT TREATMENTANNEALED
LENGTH8.000 FEET NOMINAL
MATERIAL DOCUMENT AND CLASSIFICATIONTITANIUM ALLOY, COMP AB-3 ASSN STD SINGLE MATERIAL RESPONSE
MATERIALTITANIUM ALLOY UNS R56620
MINIMUM TENSILE STRENGTH150000 POUNDS PER SQUARE INCH
MINIMUM YIELD STRENGTH145000 POUNDS PER SQUARE INCH
NONDEFINITIVE SPEC/STD DATA6AL-6V-2SN COMPOSITION AND ANNEALED CONDITION
WEIGHT PER UNIT MEASURE35.490 POUNDS PER PIECE
WIDTH36.000 INCHES NOMINAL
SURFACE CONDITIONDESCALED OVERALL


Click here to Register for Free 30-day Trial