NSN 9905-00-558-5438
Part Details | IDENTIFICATION PLATE
9905-00-558-5438 An item which is rigid or semi-rigid, generally flat and smooth designed to be attached to an item and provides data such as name/nomenclature, weight, tire pressure, dimensional data and the like. See also MARKER,IDENTIFICATION; PLATE,DESIGNATION; PLATE,INSTRUCTION; PLATE SET,IDENTIFICATION; and TAG,MARKER. Excludes LABEL.
Alternate Parts: 0600035, 1002, 1002, 0600035, 1680 L19 011, 9905-00-558-5438, 00-558-5438, 9905005585438, 005585438
Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
---|---|---|---|
99 | JAN 01, 1963 | 00-558-5438 | 00155 ( PLATE, IDENTIFICATION ) |
REFERENCE DRAWINGS & PICTURES
RECTANGULAR

Cross Reference | NSN 9905-00-558-5438
Part Number | Cage Code | Manufacturer |
---|---|---|
0600035 | 71379 | CESSNA AIRCRAFT COMPANYDBA TEXTRON AVIATION |
1002 | 02993 | KIMBALL SYSTEMSDIV OF LITTON INDUSTRIES INC |
1002 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
0600035 | 4J976 | REGAL AIR INC |
1680 L19 011 | 81996 | U S ARMY AVIATION AND MISSILECOMMAND |
Technical Data | NSN 9905-00-558-5438
Characteristic | Specifications |
---|---|
MATERIAL | ALUMINUM ALLOY |
BASIC SHAPE STYLE | RECTANGULAR |
MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250 TO 5, ALLOY ALCLAD 2024 FED SPEC SINGLE MATERIAL RESPONSE |
SURFACE TREATMENT | CHROMATE ZINC |
SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | MIL-P-8585-CANCELLED MIL SPEC SINGLE TREATMENT RESPONSE |
ATTACHMENT METHOD | HOLE |
WIDTH | 0.938 INCHES NOMINAL |
THICKNESS | 0.020 INCHES NOMINAL |
LENGTH | 3.188 INCHES NOMINAL |