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Technical Data Sheet
1MA160D05-10218 ✓ Verified by PartsTable
· COMPONENT
WHAT YOU NEED TO KNOW
Verify manufacturer and server generation compatibility Check if Option PN or Spare PN — same part, different channel
Confirm exact part number — similar PNs may be different parts
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: 0.063 INCHES NOMINAL IN, heat_treatment: T-73511 SOLUTION HEAT TREATED, overall_height: 2.120 INCHES NOMINAL IN, first_tip_style: SQUARE END. This product is currently in active production with full OEM support.

This part is cataloged in the Federal Logistics Information System (FLIS) under NSN 9540-01-176-4067, 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
1MA160D05-10218
NSN: 9540-01-176-4067
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_thickness0.063 INCHES NOMINAL IN
heat_treatmentT-73511 SOLUTION HEAT TREATED
overall_height2.120 INCHES NOMINAL IN
first_tip_styleSQUARE END
top_flange_width2.120 INCHES NOMINAL IN
basic_shape_styleT SHAPE
fabrication_methodEXTRUDED
left_top_inside_angle90.0 DEGREES NOMINAL
right_top_inside_angle90.0 DEGREES NOMINAL
weight_per_unit_measure0.324 POUNDS PER LINEAR FOOT LBS
NSN9540-01-176-4067
COMPONENT DIAGRAM
COMPONENT MAIN IC EDGE CONNECTOR No detailed specs available SUPPORT,STRUCTURAL COMPONENT,AIR TITLE COMPONENT PN 1MA160D05-10218 MFR SUPPORT,STRUCTURAL COM
KEY FEATURES
RIGHT SIDE TOP FLANGE THICKNESS: 0.063 INCHES NOMINAL IN
FABRICATION METHOD: EXTRUDED
FIRST TIP STYLE: SQUARE END
SECOND TIP RELATIONSHIP TO FIRST TIP: IDENTICAL
LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES: 1.060 INCHES NOMINAL IN
LEFT TOP INSIDE ANGLE: 90.0 DEGREES NOMINAL
MATERIAL: ALUMINUM ALLOY 7075
LEG THICKNESS: 0.063 INCHES NOMINAL IN
TECHNICAL CHARACTERISTICS (FLIS)
RIGHT SIDE TOP FLANGE THICKNESS0.063 INCHES NOMINAL IN
FABRICATION METHODEXTRUDED
FIRST TIP STYLESQUARE END
SECOND TIP RELATIONSHIP TO FIRST TIPIDENTICAL
LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES1.060 INCHES NOMINAL IN
LEFT TOP INSIDE ANGLE90.0 DEGREES NOMINAL
MATERIALALUMINUM ALLOY 7075
LEG THICKNESS0.063 INCHES NOMINAL IN
RIGHT TOP INSIDE ANGLE90.0 DEGREES NOMINAL
FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG0.125 INCHES NOMINAL IN
VERIFIED SUBSTITUTES & CROSS-REFERENCES 9
1M5164Interchangeable
interchangeable cross-reference
interchangeable
AMS-QQ-A-200/11Interchangeable
interchangeable cross-reference
interchangeable
60-4254Interchangeable
interchangeable cross-reference
interchangeable
26241Interchangeable
interchangeable cross-reference
interchangeable
MS14372E071Interchangeable
interchangeable cross-reference
interchangeable
MS14375E119Interchangeable
interchangeable cross-reference
interchangeable
LIFECYCLE
StatusACTIVE
AvailabilityOEM and secondary market
RoHS CompliantEAR99Not HAZMAT
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FREQUENTLY ASKED QUESTIONS
What is 1MA160D05-10218?
1MA160D05-10218 is a SUPPORT,STRUCTURAL COMPONENT,AIR.
What parts can replace 1MA160D05-10218?
There are 9 known substitutes for 1MA160D05-10218: 1M5164, AMS-QQ-A-200/11, 60-4254 and 6 more. Substitute compatibility should be verified for your specific system.
What is the NSN for 1MA160D05-10218?
1MA160D05-10218 is cataloged in the Federal Logistics Information System (FLIS) under NSN 9540-01-176-4067. This indicates validated use in U.S. government and defense supply chains.
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