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MS20001 |
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| Part Number | MS20001 |
| Manufacturer | Genuine Aircraft |
| Description | Genuine Aircraft Hardware Co. Hinge, Butt, Structural, Extruded MS20001 TABLE I * CANCELLED - NO SUPERSEDING PART NUMBER ( a ) TOLERANCES FOR DIMENSIONS ON PITCH SHALL NOT BE CUMULATIVE. ( b ) DIME... |
| Features |
nd Drawings are Copyright © by Genuine Aircraft Hardware Co. 2005
Documents in this book for REFERENCE ONLY, not intended for design. Not guaranteed for accuracy.
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Genuine Aircraft Hardware Co.
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REQUIREMENTS: 1. MATERIAL: 2. FINISH: 3. MARKING: ALUMINUM ALLOY 2024-T3511, PER QQ-A-200/3, OR ALUMINUM ALLOY 7075-T3511, PER QQ-A-200/11 (SEE PART NUMBERING). ANODIZED IN ACCORDANCE WITH MIL-A-8625, TYPE II; CHEMICAL SURFACE TREAT IN ACCORDANCE WITH MIL-C-5541; (ENDS OF ALL HINGES SHALL BE FINISHED). INK STAMP MS20001 (DASH NUMBER) REGULAR INTERVALS ALONG LENGTH OF HINGE SO... |
| Document |
 MS20001 Data Sheet
PDF 110.94KB |
| Distributor | Stock | Price | Buy |
|---|
| No. | Parte # | Fabricante | Descripción | Hoja de Datos |
|---|---|---|---|---|
| 1 | MS20001 |
AVIAQUIP |
STRUCTURAL EXTRUDED HINGE |
|
| 2 | MS20001P |
ETC |
Hinge / Butt / Structural / Extruded |
|
| 3 | MS20004 |
Genuine Aircraft |
(MS20004 - MS20008) Diameter / Head Size / Lengths |
|
| 4 | MS20004 |
ETC |
MS20004 - MS20014 |
|
| 5 | MS20005 |
Genuine Aircraft |
(MS20004 - MS20008) Diameter / Head Size / Lengths |
|