215316: BLADE,COMPRESSOR,AIRCRAFT GAS TU.
BLADE,COMPRESSOR,AIRCRAFT GAS TU. Key specifications include material: STEEL BLADE, design_type: COMPRESSOR, overall_width: 0.945 INCHES MINIMUM AND 0.955 INCHES MAXIMUM IN, overall_length: 1.953 INCHES MINIMUM AND 1.962 INCHES MAXIMUM IN, hardness_rating: 32.0 ROCKWELL C MINIMUM AND 38.0 ROCKWELL C MAXIMUM BLADE, special_features: FUNCTION. This part is cataloged in the U.S.
Government catalog under NSN 4720-00-622-0696, 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.
| material | STEEL BLADE |
| design_type | COMPRESSOR |
| overall_width | 0.945 INCHES MINIMUM AND 0.955 INCHES MAXIMUM IN |
| overall_length | 1.953 INCHES MINIMUM AND 1.962 INCHES MAXIMUM IN |
| hardness_rating | 32.0 ROCKWELL C MINIMUM AND 38.0 ROCKWELL C MAXIMUM BLADE |
| special_features | FUNCTION |
| material_thickness | 0.493 INCHES MINIMUM AND 0.499 INCHES MAXIMUM IN |
| end_item_identification | TF33 AIRCRAFT ENGINE |
| engine_section_location | COMPRESSOR |
| criticality_code_justification | FEAT |
| material_document_and_classification | AMS5616 ASSN STD SINGLE MATERIAL RESPONSE BLADE |
| NSN | 4720-00-622-0696 |
| MEASURING METHOD AND LENGTH | 28.000 INCHES NOMINAL OVERALL IN |
| TEMP RATING | -40.0 FAHRENHEIT AND 200.0 FAHRENHEIT SINGLE RESPONSE DEGF |
| MINIMUM INSIDE BENDING RADIUS | 1.750 INCHES IN |
| CONNECTION STYLE | SWIVEL, PLAIN SECOND END |
| CONNECTION STYLE | INVERTED FLARE FIRST END |
| END CONNECTION DESIGN | STRAIGHT FIRST END |
| END CONNECTION DESIGN | STRAIGHT SECOND END |
| LAYER COMPOSITION AND LOCATION | 1ST LAYER BRAIDED TEXTILE YARN AND 2ND LAYER BRAIDED TEXTILE YARN AND OUTER LAYER MOLDED RUBBER, SYNTHETIC |
| CONNECTION TYPE | THREADED EXTERNAL PIPE SECOND END |
| CONNECTION TYPE | THREADED EXTERNAL PIPE FIRST END |