1560-01-473-5854

Find complete technical information, availability, and procurement data for: 1560-01-473-5854

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1560-01-473-5854
Federal Supply Group
Aerospace Craft and Structural Components
Federal Supply Classification
1560 Airframe Structural Components
National Stock Number
1560-01-473-5854
Item Name Code
51576
Assigment Date
04/11/2000 (26 years ago)

A rigid item of various shapes permanently attached to a structure of an aircraft, designed to provide access for inspection, service, replacement of components and/or adjustments. It is designed to be attached by means of hinges or similar device. It may include self-closing features and have a quick release or other type latching to permit access with a minimum of effort. It may include an observation window. Excludes:cover, access; cover access, aircraft; door, access; door, aircraft and all doors not specficially designed to provide access for the purposes listed above.

sh-2g(a) seasprite helicopter end item identification, aluminum alloy 2024 material, handle for opening, lifting, closing, or the like and sealing capability features provided, door assembly-oil access, crown panel extension part name assigned by controlling agency, length 8.000 in. nominal; width 6.890 in. nominal; thickness 0.032 in. nominal; assembly includes a door, latch, two hinges, three types of rivets (as required), four seals, and two stiffeners; door is formed to contour and stiffeners are formed to door; remove pins provided with two hinges p/n ms20257p2-150 and replace with two pins p/n ms20253p2-275; adhesive mmm-a-1617, type ii, used to bond seals to door; door location is sta 142.50 to sta 149.25 and rbl 5.60 to rbl 12.67 special features

Product Characteristics

Below you’ll find the complete technical specifications and performance data for this part, including material details and compliance information.

End Item Identification
sh-2g(a) seasprite helicopter
Features Provided
handle for opening, lifting, closing, or the like and sealing capability
Part Name Assigned By Controlling Agency
door assembly-oil access, crown panel extension
Special Features
length 8.000 in. nominal; width 6.890 in. nominal; thickness 0.032 in. nominal; assembly includes a door, latch, two hinges, three types of rivets (as required), four seals, and two stiffeners; door is formed to contour and stiffeners are formed to door; remove pins provided with two hinges p/n ms20257p2-150 and replace with two pins p/n ms20253p2-275; adhesive mmm-a-1617, type ii, used to bond seals to door; door location is sta 142.50 to sta 149.25 and rbl 5.60 to rbl 12.67
Material
aluminum alloy 2024
Material Document And Classification
qq-a-250/5 fed spec single material response

Related Parts

This NSN group includes multiple components designed to meet specific performance and operational standards. Each listing provides detailed specs, functionality data, and replacement compatibility information:

Part Number Name
K836789-001 Aircraft Access Door

FAQs

Find helpful answers about installation, operation, maintenance, compliance, and troubleshooting.

What is the FSCG of the NSN 1560-01-473-5854?
The FSCG of the NSN 1560-01-473-5854 is 1560
Does the NSN 1560-01-473-5854 have a Schedule B code assigned?
Yes, the Schedule B code is 8807909060
Does NSN 1560-01-473-5854 require demilitarization?
"commerce control list items (ccli) - mut to the point of scrap required outside the united states. Inside the united states, mut is required when the demil integrity code (ic) is "3" and mut is not required when the demic is "6" (note 8)"
Does NSN 1560-01-473-5854 contain precious materials?
Item does not contain precious metal.
Does NSN 1560-01-473-5854 contain hazardous materials?
Indicates there is no information in the hmirs. The nsn is in a fsc in table ii of fed std 313 and a msds may be required by the user. The requirement for a msds is dependent on a hazard determination of the supplier or the intended end use of item.
When the NSN 1560-01-473-5854 was assigned to the Federal Catalog?
It was assigned 26 years ago, on Tue, Apr 11, 2000

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