1680-01-577-1328 CYLINDER,AIRCRAFT,M Index 1680-01-577-1330 MANIFOLD ASSEMBLY,A

National Stock Number:
1680-01-577-1329

Federal Supply Class:
1680

National Item Identification Number:
015771329

Description:
PISTON,AIRCRAFT,MAT


Manufacturer Information:
7-4644-1381R2JC GLOBAL, INC
7-4644-13B1R2BELL BOEING JOINT PROJECT OFFICE
7-4644-23B1R2BELL BOEING JOINT PROJECT OFFICE
7-4644-197415TRIUMPH ACTUATION SYSTEMS - YAKIMA, LLC


Techincal Specification:
GENERAL CHARACTERISTICS ITEM DESCRIPTIONHEAD DIAMETER: 2.605-2.607" PRE-PLATE; 2.613-2.615" FINISH
OVERALL DIAMETER1.880 INCHES NOMINAL
OVERALL LENGTH18.720 INCHES NOMINAL
MATERIALSTEEL
PART NAME ASSIGNED BY CONTROLLING AGENCYPISTON NOSE LANDING GEAR DRAG STRUT ACTUATOR
SPECIAL FEATURESMATERIAL: ALLOY STEEL PER AMS 6425; PREMIUM QUALITY VAC, ARC REMELT, CLEANLINESS PER AMS 2300; FRACTURE TOUGHNESS TO BE KIC - 100 KSI SQ RT IN MIN, MEASURED PER ASTM-E-399; TENSILE STRENGTH: 220-240KSI; YIELD STRENGTH: 180KSI MINIMUM
SPECIAL TEST FEATURESMAGNETIC PARTICLE INSPECT PER BAC 5424 CLASS A AFTER CHROME PLATE GRINDING; PENETRANT INSPECT CHROME PLATED SURFACES AFTER GRINDING PER BAC 5423, TYHPE I
SPECIFICATION/STANDARD DATA05047-ASME Y14.5M 1994 PROFESSIONAL/INDUSTRIAL ASSOCIATION STANDARD AND 05047-ASME Y14.100 AND SAME-Y STANDARD 8-0001 PROFESSIONAL/INDUSTRIAL ASSOCIATION STANDARD
SUPPLEMENTARY FEATURESHEAT TREAT TO 220-240KSI PER AMS 2759/2 WITH SURFACE CONTAMINATION REQUIREMENTS PER AMS-H-6875 TENSILE TEST PIECES REQUIRED FOR EACH HEAT TREAT LOT; HARDNESS TEST PER ASTM E18 ROCKWELL HARDNESS C 46-48 ON PISTON HEAD PRIOR TO POST HEAT TREAT MATERIAL REMOVAL BUFF OUT RAISED EDGES AFTER TEST
SURFACE TREATMENTCADMIUM AND CHROMIUM


Click here to Register for Free 30-day Trial