MS20001 |
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.
Continued...
Genuine Aircraft Hardware Co.
Continued...
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 |
Similar Datasheet
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 | |
6 | MS20005 |
ETC |
MS20004 - MS20014 |