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MS20001P |
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| Part Number | MS20001P |
| Manufacturer | ETC |
| Description | INCH-POUND MS20001P 21 May 2012 SUPERSEDING MS20001N 16 November 2010 DETAIL SPECIFICATION SHEET HINGE, BUTT STRUCTURAL, EXTRUDED This specification sheet is approved for use by all Departments and A... |
| Features |
shall not be cumulative. (b) Dimension K must never exceed a full loop or tang, and both ends must be equal within .020 inch.
INTERCHANGEABILITY RELATIONSHIP, see table II. MS20001 hinges are not universally interchangeable with AN252 hinges. TABLE II. Interchangeability. Inactive and cancelled AN252-1 AN252-2 AN252-4 AN252-6 AN252-8 AN252-10 Universally interchangeable ------------MS20001-2 MS20001-4 MS20001-6 MS20001-8 MS20001-10
2
MS20001P REQUIREMENTS: 1. Material Aluminum alloy 2024-T3511 per SAE-AMS-QQ-A-200/3, ASTM-B221, ASTMB241/B241M or aluminum 7075-T73511 per SAE-AMS-QQ-A-200/11... |
| Document |
 MS20001P Data Sheet
PDF 77.21KB |
Similar Datasheet
| No. | Parte # | Fabricante | Descripción | Hoja de Datos |
|---|---|---|---|---|
| 1 | MS20001 |
Genuine Aircraft |
Hinge / Butt / Structural / Extruded |
|
| 2 | MS20001 |
AVIAQUIP |
STRUCTURAL EXTRUDED HINGE |
|
| 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 |
|
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