NSN 6610-01-338-5338
Part Details | POSITION TRANSMITTER
6610-01-338-5338
Alternate Parts: 17B6F1113503, 17B6F1113-503, 6703A000103, 6703A0001-03, 6610-01-338-5338, 01-338-5338, 6610013385338, 013385338
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 66 | MAY 04, 1991 | 01-338-5338 | 13367 ( TRANSMITTER, POSITION ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 6610-01-338-5338
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 17B6F1113-503 | 88277 | BOEING COMPANY, THEDBA BOEING |
| 6703A0001-03 | 17472 | EATON CORPORATIONDIV FUEL & MOTION CONTROL SYSTEMS |
Technical Data | NSN 6610-01-338-5338
| Characteristic | Specifications |
|---|---|
| OVERALL LENGTH | 5.070 INCHES MINIMUM AND 5.190 INCHES MAXIMUM |
| OVERALL WIDTH | 3.540 INCHES NOMINAL |
| OVERALL HEIGHT | 3.610 INCHES NOMINAL |
| MOUNTING METHOD | FLANGE |
| MOUNTING POINT QUANTITY | 4 |
| ELECTRICAL CONNECTION QUANTITY | A1$$A2 |
| CONTACT QUANTITY | A12$$A15 |
| CONTACT TYPE | PIN |
| ELECTRICAL CONNECTION CONTROLLING AGENCY | MILITARY SPECIFICATION |
| ELECTRICAL CONNECTION IDENTIFYING NUMBER | M83723/83W132127 & 83W14157 |
| MECHANICAL CONNECTION QUANTITY | 1 |
| MECHANICAL CONNECTION TYPE | DP ANY ACCEPTABLE |
| CURRENT TYPE | AC |
| VOLTAGE IN VOLTS | 26.0 |
| FREQUENCY IN HERTZ | 400.0 |
| PHASE | SINGLE |
| ACTUATION METHOD | ROTARY SHAFT |
| SUPPLEMENTARY FEATURES | NOMINAL SYNCRO PERFORMANCE AT 25 DEG C: 26VRMS,400HZ;NOMINAL RVDT PERFOMANCE AT 25 DEG C:INPUT VOLTAGE-7.07VRMS,3100HZ |
| FUNCTIONAL DESCRIPTION | USED TO TRANSMIT THE HORIZONAL STABILIZER & FLAPS POSITION |
| RELATIONSHIP TO SIMILAR EQUIPMENT | NOT INTERCHANGEABLE WITH 6610-01-339-5254 & 6610-01-450-3998 |
| REFERENCE DATA AND LITERATURE | 1C-17A-4-27 (SHEET 45-00) FIG 87 INDEX 3 |
| END ITEM IDENTIFICATION | C-17 AIRCRAFT; RIGHT HAND STABILIZER |