INCH-POUND MS27039F 15 NOVEMBER 1995 SUPERSEDING MS27039E 24 JANUARY 1995 MILITARY SPECIFICATION SHEET SCREW, MACHINE - PAN HEAD, STRUCTURAL, CROSS RECESSED This Specification is approved for use by all Departments and Agencies of the Department of Defense. The requirements for acquiring the product described herein shall consist of this specification sheet .
conflict between the text of this document and the references cited herein, the text of this document will take precedence. 6. Unless otherwise specified, issues of referenced documents are those in effect at the time of solicitation. 7. Caution should be taken during plating process. The contractor shall be responsible for the safe reutilization and disposal of all materials generated by this process in accordance with ASTM A380, section 8.2 and 8.7. 8. Items manufactured to Rev. C and Rev. D may be delivered from suppliers stock until depletion. REQUIREMENTS: 1. Material: Aluminum Alloy 20.
No. | Partie # | Fabricant | Description | Fiche Technique |
---|---|---|---|---|
1 | MS27039 |
Genuine Aircraft Hardware |
Pan Head / Structural Screws / Phillips Drive | |
2 | MS27144C |
ETC |
CONNECTOR | |
3 | MS27183 |
ETC |
Washer | |
4 | MS27183 |
ELITE FASTENERS |
Flat Washer | |
5 | MS27406-xx |
ETC |
(MS Series) Standard Lever Selection Table | |
6 | MS27407-xx |
ETC |
(MS Series) Standard Lever Selection Table | |
7 | MS27467 |
AEC |
I PLUG | |
8 | MS27467 |
ETC |
straight plug | |
9 | MS27467T25B35PD |
AEC |
I PLUG | |
10 | MS27468 |
ETC |
Connect | |
11 | MS27473 |
ETC |
straight plug | |
12 | MS27505xxxx |
AEC |
Back Panel Box Mounting Flange Receptacle |