Part Number
Part Number:
NSN:
NIIN:
Item Name:
CONTROLLER , AIR INLET , ELECTRONIC
Definition:
A DEVICE WHICH ACCEPTS INPUTS FROM VARIOUS SENSORS AND REGULATES AIR FLOW TO THE ENGINE INTAKES BY OPENING AND CLOSING THE INLET RAMPS IN ORDER TO LET MORE OR LESS AIR IN TO ENSURE EFFICIENT OPERATION.
CAGE Information
| Code | Company |
|---|---|
| 73030 | HAMILTON SUNDSTRAND CORPORATION |
Federal Supply Class
Title
FLIGHT INSTRUMENTS
Inclusions:
INCLUDES AIR SPEED INDICATORS; RATE OF CLIMB INDICATORS; BANK AND TURN INDICATORS; PITOT TUBES; GYRO HORIZON INDICATORS; ATTITUDE GYRO INDICATORS.
Exclusions:
EXCLUDES NAVIGATIONAL INSTRUMENTS (FSC 6605).
Characteristics (Decoded)
| MRC | Requirements Statement | Clear Text Reply |
|---|---|---|
| APXH | TERMINAL LOCATION | BACK |
| APXH | TERMINAL LOCATION | BACK |
| ATJK | POWER SOURCE | EXTERNAL |
| AFXE | MAXIMUM VOLTAGE RATING IN VOLTS | 115.0 AC |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | CONTROLLER,ELECTRONIC AIR INLET |
| FEAT | SPECIAL FEATURES | ONE USED PER ENGINE-2 TOTAL FOR F-15 ACFT |
| TMDN | TYPE/MODEL DESIGNATION | DCU-181/A |
| RDAL | REFERENCE DATA AND LITERATURE | T.O. 5F28-2-4 |
| CCFF | TERMINAL TYPE AND QUANTITY | 2 CONNECTOR, RECEPTACLE |
| FTLD | FUNCTIONAL DESCRIPTION | ACCEPTS INPUTS FROM THE AIRCRAFT PITOT STATIC SYSTEM, ANGLE OF ATTACK, SENSOR, TEMPERATURE SENSOR & DUCT PITOT STATIC SENSOR;IT UTILIZES THESE INPUTS TO GENERATE THE COMMANDS NECESSARY TO CONTROL THE VARIABLE ENGINE INLET GEOMETRY DURING ALL FLIGHT CONDITIONS |
| AGAV | END ITEM IDENTIFICATION | PW200 ENGINE,F15A/B/C/D |
| RTSE | RELATIONSHIP TO SIMILAR EQUIPMENT | RSIMILAR TO 6610-01-223-8179, EACHARE USED ON F-15A/B/C/D, BUT -8179 IS USED W/PW220 ENGINE AND -6625 IS USED WITH PW200 ENGINE;ALSO SIMILAR TO 6610-01-247-1798 & 6610-01-342-9774 EXCEPTTHE -1798 & -9774 ARE F-15E ONLY |
| FAAZ | PHASE | SINGLE |
| FREQ | FREQUENCY IN HERTZ | 400.0 |