PartsTable
Technical Data Sheet
506511 ✓ 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

BLADE,COMPRESSOR,AIRCRAFT GAS TU. Key specifications include material: STEEL BLADE, design_type: COMPRESSOR, overall_width: 1.212 INCHES MINIMUM AND 1.222 INCHES MAXIMUM IN, overall_length: 3.072 INCHES MINIMUM AND 3.081 INCHES MAXIMUM IN, hardness_rating: 32.0 ROCKWELL C MINIMUM AND 38.0 ROCKWELL C MAXIMUM BLADE, special_features: ORIGINAL NAME BLADE,COMPRESSOR ROTOR,TURBINE ENGINE. This product is currently in active production with full OEM support.

This part is cataloged in the Federal Logistics Information System (FLIS) under NSN 2840-00-947-7114, 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
506511
NSN: 2840-00-947-7114
FSC: 2840
CAGE: 77445 — RTX CORPORATION DBA PRATT & WHITNEY DIV PRATT &WHITNEY (USA)
SPECIFICATIONS
materialSTEEL BLADE
design_typeCOMPRESSOR
overall_width1.212 INCHES MINIMUM AND 1.222 INCHES MAXIMUM IN
overall_length3.072 INCHES MINIMUM AND 3.081 INCHES MAXIMUM IN
hardness_rating32.0 ROCKWELL C MINIMUM AND 38.0 ROCKWELL C MAXIMUM BLADE
special_featuresORIGINAL NAME BLADE,COMPRESSOR ROTOR,TURBINE ENGINE
material_thickness0.493 INCHES MINIMUM AND 0.499 INCHES MAXIMUM IN
end_item_identificationENGINE MODEL J57
engine_section_locationCOMPRESSOR
criticality_code_justificationAGAV
material_document_and_classificationAMS5616 ASSN STD SINGLE MATERIAL RESPONSE BLADE
NSN2840-00-947-7114
COMPONENT DIAGRAM
COMPONENT MAIN IC EDGE CONNECTOR No detailed specs available BLADE,COMPRESSOR,AIRCRAFT GAS TU TITLE COMPONENT PN 506511 MFR BLADE,COMPRESSOR,AIRCR
KEY FEATURES
MATERIAL THICKNESS: 0.493 INCHES MINIMUM AND 0.499 INCHES MAXIMUM IN
DESIGN TYPE: COMPRESSOR
MATERIAL DOCUMENT AND CLASSIFICATION: AMS5616 ASSN STD SINGLE MATERIAL RESPONSE BLADE
CRITICALITY CODE JUSTIFICATION: AGAV
HARDNESS RATING: 32.0 ROCKWELL C MINIMUM AND 38.0 ROCKWELL C MAXIMUM BLADE
TECHNICAL CHARACTERISTICS (FLIS)
MATERIAL THICKNESS0.493 INCHES MINIMUM AND 0.499 INCHES MAXIMUM IN
DESIGN TYPECOMPRESSOR
MATERIAL DOCUMENT AND CLASSIFICATIONAMS5616 ASSN STD SINGLE MATERIAL RESPONSE BLADE
CRITICALITY CODE JUSTIFICATIONAGAV
HARDNESS RATING32.0 ROCKWELL C MINIMUM AND 38.0 ROCKWELL C MAXIMUM BLADE
OVERALL WIDTH1.212 INCHES MINIMUM AND 1.222 INCHES MAXIMUM IN
END ITEM IDENTIFICATIONENGINE MODEL J57
OVERALL LENGTH3.072 INCHES MINIMUM AND 3.081 INCHES MAXIMUM IN
ENGINE SECTION LOCATIONCOMPRESSOR
MATERIALSTEEL BLADE
VERIFIED SUBSTITUTES & CROSS-REFERENCES 6
71-1311Interchangeable
interchangeable cross-reference
interchangeable
753011Interchangeable
interchangeable cross-reference
interchangeable
50-6511Interchangeable
interchangeable cross-reference
interchangeable
6981Interchangeable
interchangeable cross-reference
interchangeable
FA-3406Interchangeable
interchangeable cross-reference
interchangeable
A3060816-011Interchangeable
interchangeable cross-reference
interchangeable
LIFECYCLE
StatusACTIVE
AvailabilityOEM and secondary market
RoHS CompliantEAR99Not HAZMAT
Ready to buy 506511?
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 506511?
506511 is a BLADE,COMPRESSOR,AIRCRAFT GAS TU.
What parts can replace 506511?
There are 6 known substitutes for 506511: 71-1311, 753011, 50-6511 and 3 more. Substitute compatibility should be verified for your specific system.
What is the NSN for 506511?
506511 is cataloged in the Federal Logistics Information System (FLIS) under NSN 2840-00-947-7114. This indicates validated use in U.S. government and defense supply chains.
Community Feedback
Comments (0)
No comments yet. Be the first to share what you know.
Leave a Comment
Comments are reviewed before appearing. You will receive an email to verify before your comment appears.

Request a Quote — 506511