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64106-1 — PLATE,STRUCTURAL,AIRCRAFT

✓ Government record, cited
— · MRO · MRO_GENERAL
PRODUCT OVERVIEW

64106-1: PLATE,STRUCTURAL,AIRCRAFT.

The PLATE,STRUCTURAL,AIRCRAFT is a the manufacturer industrial component. Key specifications include overall_width: 3.950 INCHES NOMINAL IN, overall_height: 0.720 INCHES NOMINAL IN, overall_length: 6.600 INCHES NOMINAL IN, end_item_identification: AN/TPQ-37(V)9, part_name_assigned_by_controlling_agency: CIRCUIT CARD ASSEMBLY,RECEIVER,DIGITAL. This part is cataloged in the U.S.

Government catalog under NSN 5325-00-275-4480, indicating validated use in U.S. government and defense logistics supply chains. Available through authorized enterprise resellers and TPM (Third Party Maintenance) channels.

Verify compatibility with your specific system configuration before ordering.

WHERE IT FITS
MRO→ MRO_GENERAL→ 64106-1
NSN: 5325-00-275-4480
NIINs: 002754480, 004065004, 014884200, 014884202, 014884210, 014891063, 014891076, 014891124, 014891139, 015864353
FSC: 5325 — Fastening Devices
CAGE: 53711 — NAVAL SEA SYSTEMS COMMAND (USA)
SPECIFICATIONS
overall_width3.950 INCHES NOMINAL IN
overall_height0.720 INCHES NOMINAL IN
overall_length6.600 INCHES NOMINAL IN
end_item_identificationAN/TPQ-37(V)9
part_name_assigned_by_controlling_agencyCIRCUIT CARD ASSEMBLY,RECEIVER,DIGITAL
NSN5325-00-275-4480
COMPONENT DIAGRAM
BOLT / SCREW — THREAD VERIFICATION REQUIRED Hex HEAD LENGTH: — THREAD: — × — MATERIAL: — PN: 64106-1 · OEM ⚠ VERIFY BEFORE ORDERING Verify thread pitch before ordering — metric (M8×1.25) ≠ imperial (5/16-18). Wrong thread = wrong part. Grade/class stamped on bolt head determines tensile strength ✓ BROKER TIP Grade/class stamped on head determines tensile strength. Grade 8 > Grade 5 > Grade 2. Always confirm head marking matches specification requirement PARTSTABLE TECHNICAL DRAWING — NOT TO SCALE
KEY FEATURES
•
EYELET HEIGHT: 0.203 INCHES NOMINAL IN
•
LARGEST OUTSIDE DIAMETER: 0.313 INCHES NOMINAL IN
•
TURNLOCK EYELET STYLE: EYELET
•
EYELET INSIDE DIAMETER: 0.188 INCHES NOMINAL IN
•
MATERIAL: ALUMINUM ALLOY OVERALL
•
BODY THICKNESS: 0.015 INCHES NOMINAL IN
TECHNICAL CHARACTERISTICS
EYELET HEIGHT0.203 INCHES NOMINAL IN
LARGEST OUTSIDE DIAMETER0.313 INCHES NOMINAL IN
TURNLOCK EYELET STYLEEYELET
EYELET INSIDE DIAMETER0.188 INCHES NOMINAL IN
MATERIALALUMINUM ALLOY OVERALL
BODY THICKNESS0.015 INCHES NOMINAL IN
SUBSTITUTES & CROSS-REFERENCES 10
63-2-16-2Reference document
Same NSN cross-reference
Reference document — Advisory reference — outside the item-of-supply concept
12Z12006-192Same NSN cross-reference
Same NSN cross-reference
Also cataloged under this NSN
1271-3200Reference document
Same NSN cross-reference
Reference document — Secondary reference
GA3-200Reference document
Same NSN cross-reference
Reference document — Secondary reference
107-018-2Reference document
Same NSN cross-reference
Reference document — Secondary reference
1271-3200-AC1Reference document
Same NSN cross-reference
Reference document — Secondary reference
LIFECYCLE
NSN statusCancelled· U.S. Government catalog
No demilitarization required
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FREQUENTLY ASKED QUESTIONS
What is 64106-1?
64106-1 is a PLATE,STRUCTURAL,AIRCRAFT. It is classified as a MRO (MRO_GENERAL).
What parts can replace 64106-1?
There are 10 known substitutes for 64106-1: 63-2-16-2, 12Z12006-192, 1271-3200 and 7 more. Substitute compatibility should be verified for your specific system.
What is the NSN for 64106-1?
64106-1 is cataloged in the U.S. Government catalog under NSN 5325-00-275-4480. This indicates validated use in U.S. government and defense supply chains.
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