National Aerospace Standards - Close Tolerance Screw - NAS1153V3A
Genuine OEM Parts
Description: Close Tolerance Screw
Part Number: NAS1153V3A
Product Overview
A screw, machine or screw, cap, socket head whose unthreaded portion is of specified grip length, plated or unplated, and is machined to a tolerance of one thousandth (0.001 in.) (0.025 mm) or less of a specific diameter for items (1.000 in.) (25 mm) or less in diameter. Items over (1.000 in.) (25 mm) in diameter shall have a tolerance of fifteen ten thousandths (0.0015 in.) (0.038 mm) or less. The nominal major diameter of the threads shall be at least one thousandth (0.001 in.) (0.025 mm) below the minimum shank diameter, but not below the minimum major diameter for applicable class of fit, as shown in the screw thread standards, fed std h28 and/or other nationally recognized standards. The head is designed to be held or driven with an inserted driver. It is not designed for rotation by the thumb and fingers. A locking feature may be incorporated in the design of the head or threads.
Used In Following Aircraft
- • Dassault Falcon 2000 all variants
- • Dassault Falcon 7X
- • Dassault Falcon 900 all variants
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Dimensions | |
---|---|
Dimensions (W x H x D) | 0.375'' x 0.464'' x 0.375'' Inches |
Length | 0.464'' Inches |
Weight | 0.001 lbs |
Specifications | |
---|---|
8130-3 Eligible | No |
ATA Chapter | 51 ATA Standard Practices |
Available Conditions | NE |
Cage Code | 80205 |
Country of origin | United States |
ECCN / USML | EAR99 |
FAA Approval Code | STD |
Hazmat Code | Not Applicable |
Hazmat(Y/N) | N |
Material | Aluminum Coated Titanium |
NSN | 5305-01-471-8996 |
Schedule B | 8108.90.8000 |
Thread | 10-32 |
Total Shelf Life (days) | Not Applicable |
Type | Screw |
Units of Measure (UoM) | Each |
Brand | National Aerospace Standard. |
Condition status | Depreciated |