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Military Standard - Sheet Spring Nut - MS33737-16C

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Military Standard - Sheet Spring Nut - MS33737-16C
Genuine OEM Part

Description: Sheet Spring Nut
Part Number: MS33737-16C
AviAll Fasteners  [ Click Here ]
Alternate Part Numbers: NAS487-21, A8944-632-24J, A8944-632, A8944-632-493


Used for 
mounting of aircraft instruments from the front of the panel. 


Description:

Permit mounting of aircraft instruments from the front of the panel. No change in panel or instrument design required. Non-magnetic (speed nut is brass; the cage is phosphor bronze). Conform to MIL-N-3336. The cage is easily compressed with finger-pressure to allow insertion of legs into clearance holes. When fully inserted and pressure is released, legs spring apart; retain SPEED NUT in screw-receiving position. Turned down corners hold firm against forces of inserting screw and screw-tightening torque. All instrument mounting nuts listed below take a 6-32 machine screw.

The thread size is the same on each nut, but the instrument bezel thickness can be different per gauge. They are ordered by the back bezel thickness. They are inserted from the back, and they have ears pointing out that slide into a groove between the front and back bezel to stay in place.


Item Specification:

Material Thickness :0.040" inches nominal
Mating Member Diameter Accommodated:0.138" Inches nominal
Nut Style:Sheet spring
Panel Thickness:0.375" inches minimum
Nut Mounting Provision:Gripping prongs
Gripping Prong Quantity:2
Gripping Prong Length:0.375" inches minimum
Material:Copper alloy overall
Surface Treatment:Cadmium overall
Surface Treatment Document And Classification:QQ-P-416, ty 2, cl 3 fed spec single treatment response overall


Item Replacement History

• Part Number: MS33737-16C NUT: SHEET SPRING, CU
• Part Number: MS33737-16N/A
• Part Number: NAS487-21USE MS33737-16C=28


**Cessna Model 525 Illustrated Parts Catalog [ Click Here]