2995PL1626066 — CONTROL,EXHAUST NOZZLE,TURBINE E

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

2995PL1626066: CONTROL,EXHAUST NOZZLE,TURBINE E.

CONTROL,EXHAUST NOZZLE,TURBINE E. Key specifications include end_item_identification: F100-PW-129 ACFT ENGINE, criticality_code_justification: AGAV, reference_number_differentiating_characteristics: AS DIFFERENTIATED BY SOURCE CONTROL DRAWING. This part is cataloged in the U.S.

Government catalog under NSN 2995-01-433-6462, 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

2995PL1626066

NSN: 2995-01-433-6462
FSC: 2995 — Miscellaneous Engine Accessories, Aircraft
CAGE: 9009H — JEDNOLITY INDEKS MATERIALOWY - UNIFORM MATERIAL INDEX (POL)

SPECIFICATIONS

end_item_identification	F100-PW-129 ACFT ENGINE
criticality_code_justification	AGAV
reference_number_differentiating_characteristics	AS DIFFERENTIATED BY SOURCE CONTROL DRAWING
NSN	2995-01-433-6462

COMPONENT DIAGRAM

KEY FEATURES

•

GENERAL CHARACTERISTICS ITEM DESCRIPTION: CONTROLS/POSITIONS THE EXHAUST NOZZLE IN ORDER TO VARY ENGINE THRUST AND FAN STALL MARGIN; TRANSLATES SIGNALSRECEIVED FROM DEEC INTO MECHANICAL OUTPUT BY INCORPORATING ELECTRO/HYDRAULICSERVOVALVE AND RESOLVER, CONVERTING BLEED AIR PRESSURE TO ROTATIONAL TORQUE THRU AIRMOTOR

•

CRITICALITY CODE JUSTIFICATION: AGAV

•

REFERENCE NUMBER DIFFERENTIATING CHARACTERISTICS: AS DIFFERENTIATED BY SOURCE CONTROL DRAWING

TECHNICAL CHARACTERISTICS

GENERAL CHARACTERISTICS ITEM DESCRIPTION	CONTROLS/POSITIONS THE EXHAUST NOZZLE IN ORDER TO VARY ENGINE THRUST AND FAN STALL MARGIN; TRANSLATES SIGNALSRECEIVED FROM DEEC INTO MECHANICAL OUTPUT BY INCORPORATING ELECTRO/HYDRAULICSERVOVALVE AND RESOLVER, CONVERTING BLEED AIR PRESSURE TO ROTATIONAL TORQUE THRU AIRMOTOR
CRITICALITY CODE JUSTIFICATION	AGAV
SPECIAL FEATURES	ORIGINAL ITEM NAME -- CONVERGENT EXHAUST NOZZLE CONTROL, THIS REDESIGNED NOZZLE CONTROL INCORPORATES ENHANCED TEMPERATURE CAPABILITY TO WITHSTAND HIGHER-THAN-EXPECTED-OPERATING TEMPERATURES THAT WILL EXTEND ITS FUNCTIONAL LIFE
END ITEM IDENTIFICATION	F100-PW-129 ACFT ENGINE
REFERENCE NUMBER DIFFERENTIATING CHARACTERISTICS	AS DIFFERENTIATED BY SOURCE CONTROL DRAWING

SUBSTITUTES & CROSS-REFERENCES 6

2995PL1702849Reference document

Same NSN cross-reference

Reference document — Informative reference only

441944-ISS10Same NSN cross-reference

Same NSN cross-reference

Also cataloged under this NSN

4083219Same NSN cross-reference

Same NSN cross-reference

Also cataloged under this NSN

2995PL1801727Reference document

Same NSN cross-reference

Reference document — Informative reference only

441944Reference document

Same NSN cross-reference

Reference document — Secondary reference

441944-10Same NSN cross-reference

Same NSN cross-reference

Also cataloged under this NSN

LIFECYCLE

NSN statusActive· U.S. Government catalog

Demilitarization required — mutilation + specific procedure

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FREQUENTLY ASKED QUESTIONS

What is 2995PL1626066?

2995PL1626066 is a CONTROL,EXHAUST NOZZLE,TURBINE E.

What parts can replace 2995PL1626066?

There are 6 known substitutes for 2995PL1626066: 2995PL1702849, 441944-ISS10, 4083219 and 3 more. Substitute compatibility should be verified for your specific system.

What is the NSN for 2995PL1626066?

2995PL1626066 is cataloged in the U.S. Government catalog under NSN 2995-01-433-6462. This indicates validated use in U.S. government and defense supply chains.

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2995PL1626066 — CONTROL,EXHAUST NOZZLE,TURBINE E

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