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Technical Data Sheet
1MA160D05-10322 ✓ Verified by PartsTable
· COMPONENT
WHAT YOU NEED TO KNOW
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PRODUCT OVERVIEW

SUPPORT,STRUCTURAL COMPONENT,AIR. Key specifications include length: 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM FT, material: ALUMINUM ALLOY 7075, leg_thickness: 0.125 INCHES NOMINAL IN, heat_treatment: T-73511 SOLUTION HEAT TREATED, overall_height: 1.750 INCHES NOMINAL IN, first_tip_style: SQUARE W/ INNER AND OUTER CORNER RADII. This product is currently in active production with full OEM support.

This part is cataloged in the Federal Logistics Information System (FLIS) under NSN 9540-01-189-8617, 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
1MA160D05-10322
NSN: 9540-01-189-8617
FSC: 9540
CAGE: 76301 — THE BOEING COMPANY DIV DEFENSE (USA)
SPECIFICATIONS
length10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM FT
materialALUMINUM ALLOY 7075
leg_thickness0.125 INCHES NOMINAL IN
heat_treatmentT-73511 SOLUTION HEAT TREATED
overall_height1.750 INCHES NOMINAL IN
first_tip_styleSQUARE W/ INNER AND OUTER CORNER RADII
top_flange_width3.625 INCHES NOMINAL IN
basic_shape_styleT SHAPE
fabrication_methodEXTRUDED
left_top_inside_angle90.0 DEGREES NOMINAL
first_tip_inner_radius0.031 INCHES NOMINAL IN
first_tip_outer_radius0.031 INCHES NOMINAL IN
NSN9540-01-189-8617
COMPONENT DIAGRAM
COMPONENT MAIN IC EDGE CONNECTOR No detailed specs available SUPPORT,STRUCTURAL COMPONENT,AIR TITLE COMPONENT PN 1MA160D05-10322 MFR SUPPORT,STRUCTURAL COM
KEY FEATURES
FABRICATION METHOD: EXTRUDED
FIRST TIP STYLE: SQUARE W/ INNER AND OUTER CORNER RADII
HEAT TREATMENT: T-73511 SOLUTION HEAT TREATED
FIRST TIP OUTER RADIUS: 0.031 INCHES NOMINAL IN
MATERIAL: ALUMINUM ALLOY 7075
RIGHT TOP INSIDE ANGLE: 90.0 DEGREES NOMINAL
RIGHT SIDE TOP FLANGE THICKNESS: 0.125 INCHES NOMINAL IN
SECOND TIP RELATIONSHIP TO FIRST TIP: IDENTICAL
TECHNICAL CHARACTERISTICS (FLIS)
FABRICATION METHODEXTRUDED
FIRST TIP STYLESQUARE W/ INNER AND OUTER CORNER RADII
HEAT TREATMENTT-73511 SOLUTION HEAT TREATED
FIRST TIP OUTER RADIUS0.031 INCHES NOMINAL IN
MATERIALALUMINUM ALLOY 7075
RIGHT TOP INSIDE ANGLE90.0 DEGREES NOMINAL
RIGHT SIDE TOP FLANGE THICKNESS0.125 INCHES NOMINAL IN
SECOND TIP RELATIONSHIP TO FIRST TIPIDENTICAL
NONDEFINITIVE SPEC/STD DATAT73511 TEMPER
MATERIAL DOCUMENT AND CLASSIFICATIONAMS-Q-A-200/11 FED SPEC SINGLE MATERIAL RESPONSE
VERIFIED SUBSTITUTES & CROSS-REFERENCES 24
331104Interchangeable
interchangeable cross-reference
interchangeable
GC810HM5Interchangeable
interchangeable cross-reference
interchangeable
G33JC107Interchangeable
interchangeable cross-reference
interchangeable
CW51066Interchangeable
interchangeable cross-reference
interchangeable
D173360Interchangeable
interchangeable cross-reference
interchangeable
BPL51387ISS2Interchangeable
interchangeable cross-reference
interchangeable
LIFECYCLE
StatusACTIVE
AvailabilityOEM and secondary market
RoHS CompliantEAR99Not HAZMAT
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FREQUENTLY ASKED QUESTIONS
What is 1MA160D05-10322?
1MA160D05-10322 is a SUPPORT,STRUCTURAL COMPONENT,AIR.
What parts can replace 1MA160D05-10322?
There are 24 known substitutes for 1MA160D05-10322: 331104, GC810HM5, G33JC107 and 21 more. Substitute compatibility should be verified for your specific system.
What is the NSN for 1MA160D05-10322?
1MA160D05-10322 is cataloged in the Federal Logistics Information System (FLIS) under NSN 9540-01-189-8617. This indicates validated use in U.S. government and defense supply chains.
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