Part detail
Shroud Segment Turb
1284M82G05NSN2840-01-200-6464CAGE57613
Shroud Segment Turb
Detailed description
1284M82G05 procurement notes
Shroud Segment Turb
Specifications
Reference data
Multi-line procurement
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Compliance
- AS9120:2025· Aerospace QMS
- ISO 9001:2015· Quality Management
- FAA AC 00-56B· Voluntary Industry Distributor Accreditation
- U.S. ONLY· Fulfillment
NSN Information for Part Number 1284M82G05 with NSN 2840-01-200-6464, 2840012006464
Characteristics Data of NSN 2840-01-200-6464, 2840012006464
| MRC | Criteria | Characteristic |
|---|---|---|
| ABHP | OVERALL LENGTH | 12.233 INCHES NOMINAL |
| ABMK | OVERALL WIDTH | 1.890 INCHES NOMINAL |
| AGAV | END ITEM IDENTIFICATION | F110 ACFT ENGINE |
| CRTL | CRITICALITY CODE JUSTIFICATION | AGAV |
| CZBJ | ENGINE SECTION LOCATION | COMPRESSOR |
| CZCJ | STAGE NUMBER | 2 |
| FEAT | SPECIAL FEATURES | OUTER RADIUS 2ND END 11.908 IN.; INNER RADIUS 1ST END 11.393 IN.; INNER RADIUS 2ND END 11.14 IN.; FORMED SHAPE 45 DEG. 57 MIN. 27 SEC.; 11 HOLES 0.3535 IN. DIA. COUNTERBORE 0.520 IN. DIA. W/2 CUTTER RUN OUTS PER EA HOLE |
| MATT | III MATERIAL | ALUMINUM ALLOY 2618 OVERALL |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | AMS4132 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| SFTT | SURFACE TREATMENT | ANODIZE OVERALL |