Baluminum alloy, qq-a-250/4 2024-t62; primer, epoxy, polyamide, mil-p-23377 or gss 4310, grumman aerospace corp; 2.000 in. Lg; 1.800 in. W; 0.070 in. Material thk; 0.502 in. Min 0.512 in. Max diameter hole
A device of various shapes to be permanently attached to the structure of an aircraft. It is designed to permanently mount and/or support an integral member, or group of members of the airframe in a proper position and bear the stress imposed by the components being supported. It may have mounting provisions, such as slots, holes, and/or attachments to facilitate installation. Excludes items which are primarily designed for dampening shock and/or vibration. Excludes bracket, angle; bracket, double angle; bracket, shelf; bracket, mounting; and bracket (1), structural component, aircraft.
Classification: Other parts, nesoi, for use in other military aircraft, spacecraft and spacecraft launch vehicles (excluding parts of communication satellites)
NSN 5960-01-486-8919
NSN 6240-00-702-1814
NSN 5945-00-235-9110
NSN 6685-01-591-4647
NSN 5945-01-296-5414
NSN 5835-01-045-6371
NSN 6620-00-392-9835
NSN 5930-01-462-2896
NSN 7035-01-560-2623
NSN 5965-01-080-4021
NSN 5945-00-673-1720
NSN 6145-01-062-6917