Click here to make tpub.com your Home Page

Page Title: Table III. Classification of Defects for Preparation for Delivery
Back | Up | Next

Click here for thousands of PDF manuals

Google


Web
www.tpub.com

Home

   
Information Categories
.... Administration
Advancement
Aerographer
Automotive
Aviation
Construction
Diving
Draftsman
Engineering
Electronics
Food and Cooking
Logistics
Math
Medical
Music
Nuclear Fundamentals
Photography
Religion
   
   

 

Share on Google+Share on FacebookShare on LinkedInShare on TwitterShare on DiggShare on Stumble Upon
Back
Table II. Classification of Defects for Visual Examination of the Adapter
Up
Adapters, Quick-Disconnect, Passenger Seat to Floor
Next
Figure 1. Test Load Diagram



img
MIL-A-21165A
TABLE III
CLASSIFICATION OF DEFECTS FOR PREPARATION FOR DELIVERY
Item
Defects
Exterior and
Missing, incorrect} incomplete, illegible, of
interior markings
improper size, location  } sequence or method of
application; marking not the same on interior
and exterior containers.
Packaging and
Any non-conforming component; any component miss-
packing materials
ing, damaged or otherwise defective.
Workmanship
Inadequate application of components such as in-
complete closure of the unit package, intermediate
package, container flaps, or loose strappings,
etc., bulging or distortion of the container.
,
Number per container is more or less than re-
Exterior and interior
quired; gross or net weight exceeds the require-
weight or content
ment.
4.5.2
Strength tests - Each sample adapter shall be subjected
to the following strength tests and shall meet the requirements of 3.4.1.
4.5* 2.1
Static horizontal loading - Apply a load of 2300 pounds
to a collared adapter parallel to the base of the adapter, as shown in
Figure 1.
4.5.2.2
Static vertical loading - Apply a load of 5475 pounds
to a collared adapter through the longitudinal axis of the adapter, as
shown in Figure 1.
Impact. loading - A force of 5950 pounds resulting from
4.5.2.3
impact loading shall be applied to the adapter at an angle of 22-1/2 degrees
as shown in Figure 1.  The impact loading shall be applied as a half-sine
wave with a base of 0.050 seconds and a peak of 5950 pounds.
Vibration - Each sample adapter shall be fastened and
4*5* 3
vertically tensioned to 200 pounds and vibrated in this condition on a
vibration table at a double amplitude of 1/16 inch at 60 cycles per second
for a period of 6 hours.  The adapter shall meet the requirements of 3.4.2.
The endurance test shall be conducted after the completion of this test.
4.5.4
Endurance - The sample adapter which has been subjected
to the vibration test, shall be subjected to 1000 cycles of engaging and
disengaging,  The adapter shall meet the requirements of 3.4.3.
8

Privacy Statement - Press Release - Copyright Information. - Contact Us

Integrated Publishing, Inc.
9438 US Hwy 19N #311 Port Richey, FL 34668

Phone For Parts Inquiries: (727) 755-3260
Google +