| Part Number | MS20001 Datasheet |
|---|---|
| Manufacturer | Genuine Aircraft |
| Overview |
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.
PURPOSES, THIS STANDARD TAKES PRECEDENCE OVER PROCUREMENT DOCUMENTS REFERENCED. ADDITIONAL NOTES: * PROCUREMENT SPECIFICATION: NONE * SUPERSEDES: AN252 all revisions and MS20001K and previous revisions. * THIS INFORMATION FROM MILITARY STANDARD MS20001L PAGE 2 OF 2, REVISED OCTOBER 30, 1989, SOME DE. |
MS20001 Datasheet and Specifications PDF
The MS20001 is a Hinge / Butt / Structural / Extruded.
Key Specifications
| Pins | 20 |
|---|
| Part Number | MS20001 Datasheet |
|---|---|
| Description | STRUCTURAL EXTRUDED HINGE |
| Manufacturer | AVIAQUIP |
| Overview | STRUCTURAL EXTRUDED HINGE STANDARD LENGTH 72 INCHES OTHER LENGTHS AVAILABLE ON REQUEST. MS20001 Dash Number -2 -3 -4 -5 -6 -8 A Ref Width Open 1.062 1.250 1.500 1.750 2.000 2.000 B (Thickness) Max. 2 C3 C4 C5 C6 CRES A Width Open +.016 .750 1.062 1.250 1.500 2.000 B Thickness Alum. Alloy .032 .040 .051 .064 CRES .031 .037 .050 .062 D Loop +.001 -.008 Hole Diameter +.007 -.001 Alum. Alloy .066 P Pitch CRES .066 .093 1.000 Pin Diameter (Ref) Alum. Alloy 3/ .063 CRES 4/ .063 .090 .090 .118 .. |