CD39A1541A34 — CABLE,ENGINE RUN UP

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

CD39A1541A34: CABLE,ENGINE RUN UP.

The CABLE,ENGINE RUN UP is a the manufacturer cable assembly designed for reliable internal or external connectivity in enterprise server and storage environments. Key specifications include overall_width: 2.000 INCHES NOMINAL IN, overall_height: 2.000 INCHES NOMINAL IN, overall_length: 20.000 INCHES NOMINAL IN, end_item_identification: F/TF-15A;FMF/TF-15A A, reference_data_and_literature: TO 1F-15C-4-6, general_characteristics_item_description: DESIGN SPEC:MIL-S-8512. This part is cataloged in the U.S.

Government catalog under NSN 4920-01-076-3794, 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

CD39A1541A34

NSN: 4920-01-076-3794
FSC: 4920 — Aircraft Maintenance and Repair Shop Specialized Equipment
CAGE: 76301 — THE BOEING COMPANY DIV DEFENSE (USA)

SPECIFICATIONS

overall_width	2.000 INCHES NOMINAL IN
overall_height	2.000 INCHES NOMINAL IN
overall_length	20.000 INCHES NOMINAL IN
end_item_identification	F/TF-15A;FMF/TF-15A A
reference_data_and_literature	TO 1F-15C-4-6
general_characteristics_item_description	DESIGN SPEC:MIL-S-8512
NSN	4920-01-076-3794

COMPONENT DIAGRAM

KEY FEATURES

•

GENERAL CHARACTERISTICS ITEM DESCRIPTION: DESIGN SPEC:MIL-S-8512

•

REFERENCE DATA AND LITERATURE: TO 1F-15C-4-6

•

FUNCTIONAL DESCRIPTION: USED TO PREVENT THE AIR INLET CONTROLLER SIGNALS FROM BEING TRANSMITTED TO THE FIRST RAMP ACTUATORS DURING ENGINE RUN UPS WHEN THE AIRCRAFT IS INSTALLED IN A NOISE SUPPRESSOR SYSTEM

TYPICAL APPLICATIONS

Server Internal Cabling
Data Center Cable Infrastructure
SAS/SATA Drive Connectivity

TECHNICAL CHARACTERISTICS

OVERALL HEIGHT	2.000 INCHES NOMINAL IN
GENERAL CHARACTERISTICS ITEM DESCRIPTION	DESIGN SPEC:MIL-S-8512
REFERENCE DATA AND LITERATURE	TO 1F-15C-4-6
OVERALL LENGTH	20.000 INCHES NOMINAL IN
OVERALL WIDTH	2.000 INCHES NOMINAL IN
FUNCTIONAL DESCRIPTION	USED TO PREVENT THE AIR INLET CONTROLLER SIGNALS FROM BEING TRANSMITTED TO THE FIRST RAMP ACTUATORS DURING ENGINE RUN UPS WHEN THE AIRCRAFT IS INSTALLED IN A NOISE SUPPRESSOR SYSTEM
END ITEM IDENTIFICATION	F/TF-15A;FMF/TF-15A A

OTHER ITEMS IN FSC 4920 — Aircraft Maintenance and Repair Shop Specialized Equipment

Items in the same Federal Supply class. No interchangeability or substitution relationship is implied.

4920-00-000-0190 4920-00-001-1405 4920-00-001-1716 4920-00-001-1744 4920-00-001-1745 4920-00-001-1746 4920-00-001-1747 4920-00-001-1748

SUBSTITUTES & CROSS-REFERENCES

No substitute or cross-reference records for this part.

LIFECYCLE

NSN statusActive· U.S. Government catalog

Acquisition advice: Terminal item — no further procurement; issued until stock is exhaustedNo demilitarization required

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FREQUENTLY ASKED QUESTIONS

What is CD39A1541A34?

CD39A1541A34 is a CABLE,ENGINE RUN UP.

What is the NSN for CD39A1541A34?

CD39A1541A34 is cataloged in the U.S. Government catalog under NSN 4920-01-076-3794. This indicates validated use in U.S. government and defense supply chains.

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CD39A1541A34 — CABLE,ENGINE RUN UP

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