Part Number
Part Number:
NSN:
NIIN:
Item Name:
COMPUTER , FLIGHT DIRECTOR
Definition:
AN AIRBORNE ANALOG COMPUTER USED TO COMBINE SIGNALS FROM VARIOUS NAVIGATIONAL AIDS, GYROSCOPIC CONTROLS, AND LANDING SYSTEMS IN ORDER TO PROVIDE FLIGHT DIRECTOR STEERING SIGNALS TO THE PILOT. EXCLUDES COMPUTER, AIR NAVIGATION; COMPUTER, AZIMUTH; COMPUTER, COURSE-DISTANCE; COMPUTER, DESTINATION PRESET; AND COMPUTER, HEADING.
CAGE Information
| Code | Company |
|---|---|
| 13499 | ROCKWELL COLLINS INC. DBA GOVERNMENT |
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 |
|---|---|---|
| AXQH | INPUT INTELLIGENCE TYPE | HORIZONTAL |
| AXQH | INPUT INTELLIGENCE TYPE | HORIZONTAL |
| AWZJ | POWER SOURCE | EXTERNAL |
| APXH | TERMINAL LOCATION | BACK |
| AEEF | CONNECTOR MANUFACTURER PART NUMBER | 8113-20A41PSP AND 8113-22A55PSPA5 |
| AJAH | UNPACKAGED UNIT HEIGHT | 7.594 INCHES NOMINAL |
| AWJN | UNPACKAGED UNIT WEIGHT | 12.00 POUNDS |
| RDAL | REFERENCE DATA AND LITERATURE | 5F505-7-4, DD FORM 61, & MIL-SPEC |
| AEEE | CONNECTOR MANUFACTURER CODE | 97814 |
| AMPS | CURRENT RATING IN AMPS | ANY ACCEPTABLE |
| AGAV | END ITEM IDENTIFICATION | C-130E, C-141A, & F111 AIRCRAFT |
| TMDN | TYPE/MODEL DESIGNATION | CPU-65/A |
| AAXX | MOUNTING TYPE | RACK |
| AARA | TERMINAL QUANTITY | 2 |
| ACUR | DIRECT CURRENT VOLTAGE RATING IN VOLTS | 28.0 |
| ACUQ | ALTERNATING CURRENT VOLTAGE RATING IN VOLTS | 115.0 |
| AXQK | OUTPUT INTELLIGENCE TYPE | HORIZONTAL |
| AJAG | UNPACKAGED UNIT WIDTH | 5.290 INCHES NOMINAL |
| AXQM | COMPUTATION TYPE | GREAT CIRCLE |
| FTLD | FUNCTIONAL DESCRIPTION | SUPPLIES SIGNALS TO REMOTE FLIGHT DIRECTOR INDICATORS SUCH AS ARU-11/A AND ARU-2B/A ATTITUDE DIRECTOR INDICATORS. CALCULATES SIGNALS FOR EDISPLAY ON THE STTITUDE DIRECTOR TO ENABLE THE PILOT TO PERFORM PROPER CONTROL ACTIONS TO INTERCEPT AND MAINTAIN THE DESIRED COURSE OF THE FLLIGHT PATH FOR THE MAJOR MODES OF VOR, TACAN, DOPLER, DATALINK, ILS. |
| AXQH | INPUT INTELLIGENCE TYPE | ALTITUDE DATA |
| AJAF | UNPACKAGED UNIT LENGTH | 9.467 INCHES NOMINAL |
| FAAZ | PHASE | SINGLE |
| AARB | TERMINAL TYPE | CONNECTOR, RECEPTACLE |
| AXQJ | INTELLIGENCE INPUT METHOD | ELECTRICAL |
| FREQ | FREQUENCY IN HERTZ | 400.0 |