NSN 6615-01-522-6398
Part Details | AUTOMATIC PILOT FLIGHT CONTROLLER
6615-01-522-6398 A controller designed to control an aircraft through an automatic pilot in pitch, yaw, roll and coordinated turns.
Alternate Parts: DCK287A37G16, DCK-287/A37G-16, 17B1U6003561, 17B1U6003-561, 6615-01-522-6398, 01-522-6398, 6615015226398, 015226398
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 66 | AUG 05, 2004 | 01-522-6398 | 03365 ( CONTROLLER, FLIGHT, AUTOMATIC PILOT ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 6615-01-522-6398
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| DCK-287/A37G-16 | 07878 | AERONAUTICAL AND SUPPORT EQUIPMENTTYPE/ASETDS/AFLCMC/EZSC |
| 17B1U6003-561 | 88277 | BOEING COMPANY, THEDBA BOEING |
Technical Data | NSN 6615-01-522-6398
| Characteristic | Specifications |
|---|---|
| POWER SOURCE | SELF-CONTAINED |
| MAXIMUM VOLTAGE RATING IN VOLTS | 28.0 DC |
| MAXIMUM WATTAGE RATING IN WATTS | 32.0 |
| INCLOSURE TYPE | ENCASED |
| MAXIMUM OVERALL LENGTH | 8.750 INCHES |
| MAXIMUM OVERALL WIDTH | 16.000 INCHES |
| MAXIMUM OVERALL HEIGHT | 3.500 INCHES |
| SPECIAL FEATURES | ALTERED ITEM DRAWING MADE FROM 17P1E1050-771;SOFTWARE LOAD 103E4171G10 (81F-AA37G16A/C17A-F001-01A |
| CRITICALITY CODE JUSTIFICATION | SUPP |
| END ITEM IDENTIFICATION | C-17A |
| SUPPLEMENTARY FEATURES | ELECTROSTATIC DISCHARGE |
| FUNCTIONAL DESCRIPTION | THE AUTOMATIC FLIGHT CONTROL PANEL PROVIDES THE CAPABILITY FOR THE PILOT TO ENGAGE THE FLIGHT DIRECTOR,AUTOPILOT AND AUTOTHROTTLE AND TO SELECT AND ADJUST MODES OF OPERATION |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | CONTROL-INDICATOR,AUTOMATIC PILOT |