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22NA1-62 Nut - Anchor -  Two Lug -  Self-Locking - 6-32 - Nylon Insert

22NA1-62 Nut - Anchor - Two Lug - Self-Locking - 6-32 - Nylon Insert

SKU: 22NA1-62
$6.25

22NA1-62 NUT - ANCHOR, TWO LUG, SELF-LOCKING
PART NUMBER: 22NA1-62
AIRCRAFT: Various
CONDITION: NS
DETAILS: Two lug fixed self-locking anchor nut, 6-32 thread, nylon locking insert, cadmium plated carbon steel

The 22NA1-62 is a two lug fixed anchor nut of the type used throughout WWII and postwar airframes wherever a screw or bolt has to land on a permanent threaded anchor and the back side of the structure cannot be reached. It rivets to the sheet through two rivet holes, one in each lug, and carries a nylon locking insert that supplies prevailing torque so the fastener will not back out under vibration. Typical use is inspection panels, access doors, fairings, cowling attach points, floorboards and equipment shelves.

Specifications

Part Number22NA1-62
Manufacturer SeriesESNA (Elastic Stop Nut Corporation of America)
StyleTwo lug fixed self-locking anchor nut
Mounting ConfigurationTwo lug, plate style
Thread Size6-32
Locking ElementNylon insert
Nut MaterialCarbon steel
Bracket / Base MaterialSteel plate (integral)
FinishCadmium plated
Rivet Holes2 plain (protruding-head) rivet holes
Maximum Temperature250 F
AN / MS / NAS ReferenceAN366F632A / MS21078-06 style
ConditionNS (New Surplus)

Cross Reference and Interchange

Government standard reference: AN366F632A / MS21078-06 style.

ESNA builds this style with either locking insert. 22A1-62 carries the fiber insert and 22NA1-62 carries the nylon insert. The two are dimensionally the same part and are normally interchangeable, so order by whichever number your parts list calls out.

In the ESNA 22 series the 22 prefix denotes cadmium plated carbon steel, A denotes a fiber locking insert and NA denotes a nylon locking insert. The trailing dash number is the thread code, where 62 is 6-32, 82 is 8-32, 02 is 10-32, 048 is 1/4-28, 054 is 5/16-24 and 064 is 3/8-24. A BC suffix indicates 100 degree countersunk rivet holes.

Fitment and Documentation

New surplus original hardware. Sold as-is with no FAA 8130-3 and no traceability. Airworthiness determination is the responsibility of an appropriately rated certificate holder. Confirm the part number against your illustrated parts catalog before installing. If you need help matching a nut plate to an application, an aircraft, or a legacy drawing callout, send us a quick quote request and we will work it with you.

***Photos are for reference only.

Details

22NA1-62 NUT - ANCHOR, TWO LUG, SELF-LOCKING
PART NUMBER: 22NA1-62
AIRCRAFT: Various
CONDITION: NS
DETAILS: Two lug fixed self-locking anchor nut, 6-32 thread, nylon locking insert, cadmium plated carbon steel

The 22NA1-62 is a two lug fixed anchor nut of the type used throughout WWII and postwar airframes wherever a screw or bolt has to land on a permanent threaded anchor and the back side of the structure cannot be reached. It rivets to the sheet through two rivet holes, one in each lug, and carries a nylon locking insert that supplies prevailing torque so the fastener will not back out under vibration. Typical use is inspection panels, access doors, fairings, cowling attach points, floorboards and equipment shelves.

Specifications

Part Number22NA1-62
Manufacturer SeriesESNA (Elastic Stop Nut Corporation of America)
StyleTwo lug fixed self-locking anchor nut
Mounting ConfigurationTwo lug, plate style
Thread Size6-32
Locking ElementNylon insert
Nut MaterialCarbon steel
Bracket / Base MaterialSteel plate (integral)
FinishCadmium plated
Rivet Holes2 plain (protruding-head) rivet holes
Maximum Temperature250 F
AN / MS / NAS ReferenceAN366F632A / MS21078-06 style
ConditionNS (New Surplus)

Cross Reference and Interchange

Government standard reference: AN366F632A / MS21078-06 style.

ESNA builds this style with either locking insert. 22A1-62 carries the fiber insert and 22NA1-62 carries the nylon insert. The two are dimensionally the same part and are normally interchangeable, so order by whichever number your parts list calls out.

In the ESNA 22 series the 22 prefix denotes cadmium plated carbon steel, A denotes a fiber locking insert and NA denotes a nylon locking insert. The trailing dash number is the thread code, where 62 is 6-32, 82 is 8-32, 02 is 10-32, 048 is 1/4-28, 054 is 5/16-24 and 064 is 3/8-24. A BC suffix indicates 100 degree countersunk rivet holes.

Fitment and Documentation

New surplus original hardware. Sold as-is with no FAA 8130-3 and no traceability. Airworthiness determination is the responsibility of an appropriately rated certificate holder. Confirm the part number against your illustrated parts catalog before installing. If you need help matching a nut plate to an application, an aircraft, or a legacy drawing callout, send us a quick quote request and we will work it with you.

***Photos are for reference only.

Warranty Information

All NS parts are sold "as-is". Airworthiness to be determined by an appropriately rated certificate holder. No warranty is implied. AirCorps Depot reserves the right to charge a restocking fee when deemed appropriate.

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