1MA160D01-10111 — SUPPORT,STRUCTURAL COMPONENT,AIR

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

1MA160D01-10111: SUPPORT,STRUCTURAL COMPONENT,AIR.

SUPPORT,STRUCTURAL COMPONENT,AIR. Key specifications include length: 12.000 FEET NOMINAL FT, material: ALUMINUM ALLOY 7075, leg_thickness: 0.094 INCHES NOMINAL IN, heat_treatment: O-ANNEALED, overall_height: 1.625 INCHES NOMINAL IN, first_tip_style: SQUARE END. This part is cataloged in the U.S.

Government catalog under NSN 9540-01-437-2671, 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

1MA160D01-10111

NSN: 9540-01-437-2671
FSC: 9540 — Structural Shapes, Nonferrous Base Metal
CAGE: 76301 — THE BOEING COMPANY DIV DEFENSE (USA)

SPECIFICATIONS

length	12.000 FEET NOMINAL FT
material	ALUMINUM ALLOY 7075
leg_thickness	0.094 INCHES NOMINAL IN
heat_treatment	O-ANNEALED
overall_height	1.625 INCHES NOMINAL IN
first_tip_style	SQUARE END
top_flange_width	2.500 INCHES NOMINAL IN
basic_shape_style	T SHAPE
fabrication_method	EXTRUDED
left_top_inside_angle	90.0 DEGREES NOMINAL
right_top_inside_angle	90.0 DEGREES NOMINAL
nondefinitive_spec/std_data	7075 ALLOY AND 0 TEMPER
NSN	9540-01-437-2671

COMPONENT DIAGRAM

KEY FEATURES

•

RIGHT SIDE TOP FLANGE THICKNESS: 0.094 INCHES NOMINAL IN

•

LENGTH: 12.000 FEET NOMINAL FT

•

LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES: 1.250 INCHES NOMINAL IN

•

RIGHT TOP INSIDE ANGLE: 90.0 DEGREES NOMINAL

•

LEFT TOP INSIDE ANGLE: 90.0 DEGREES NOMINAL

•

HEAT TREATMENT: O-ANNEALED

•

FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG: 0.125 INCHES NOMINAL IN

TECHNICAL CHARACTERISTICS

OVERALL HEIGHT	1.625 INCHES NOMINAL IN
RIGHT SIDE TOP FLANGE THICKNESS	0.094 INCHES NOMINAL IN
LENGTH	12.000 FEET NOMINAL FT
LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES	1.250 INCHES NOMINAL IN
RIGHT TOP INSIDE ANGLE	90.0 DEGREES NOMINAL
LEFT TOP INSIDE ANGLE	90.0 DEGREES NOMINAL
HEAT TREATMENT	O-ANNEALED
FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG	0.125 INCHES NOMINAL IN
MATERIAL DOCUMENT AND CLASSIFICATION	AMS-QQ-A-200/11 FED SPEC SINGLE MATERIAL RESPONSE
FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG	0.125 INCHES NOMINAL IN

SUBSTITUTES & CROSS-REFERENCES 4

10136-2404/QQ-A-200/11-OReference document

Same NSN cross-reference

Reference document — Secondary reference

AMS-QQ-A-200/11Reference document

Same NSN cross-reference

Reference document — Design control — primary reference

10136-2404Reference document

Same NSN cross-reference

Reference document — Design control — primary reference

QQ-A-200/11Reference document

Same NSN cross-reference

Reference document — Secondary reference

LIFECYCLE

NSN statusActive· U.S. Government catalog

Acquisition advice: Normally procured from the manufacturer (OEM)No demilitarization required

Ready to buy 1MA160D01-10111?

Compare prices from verified sellers on eBay

Buy on eBay →

As an eBay Partner, PartsTable may earn a commission. Your price is not affected.

FREQUENTLY ASKED QUESTIONS

What is 1MA160D01-10111?

1MA160D01-10111 is a SUPPORT,STRUCTURAL COMPONENT,AIR.

What parts can replace 1MA160D01-10111?

There are 4 known substitutes for 1MA160D01-10111: 10136-2404/QQ-A-200/11-O, AMS-QQ-A-200/11, 10136-2404 and 1 more. Substitute compatibility should be verified for your specific system.

What is the NSN for 1MA160D01-10111?

1MA160D01-10111 is cataloged in the U.S. Government catalog under NSN 9540-01-437-2671. This indicates validated use in U.S. government and defense supply chains.

Community Feedback

1MA160D01-10111 — SUPPORT,STRUCTURAL COMPONENT,AIR

Request a Quote — 1MA160D01-10111