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NSN 6615-01-110-6322, 6615011106322
Cancelled -> Replaced by 6615012689235

Federal Supply Classification
FSC 6615 - Automatic Pilot Mechanisms and Airborne Gyro Components
National Item Identification Number
NIIN 011106322
Codification Country
United States
Item Name Code
INC 03365
Criticality
(X) This item does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application.
Hazardous Material Indicator Code
(N) There is no data in the HMIRS and the NSN is in an FSC not generally suspected of containing hazardous materials.
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DLMS® Summary

National Stock Number 6615-01-110-6322

National Stock Number (NSN) 6615-01-110-6322, or NIIN 011106322, (controller,flight,automatic pilo) was assigned April 3, 1981 in the Federal Logistics Information System (FLIS). This NIIN is Available for Manual Assignment. This NSN replaces 2 stock numbers: 6615012689235, 6615012430319.

There are 4 manufacturer part numbers associated with this NSN. One of those part number(s) are considered obsolete. The manufacturer part numbers were originally supplied by one supplier. Today, one supplier is listed as an Active supplier for this NSN. Of the active suppliers, only one supplier is deemed design controlled or valid supply parts.

This part number has not been procured by the US Government in over 5 years.

Based on a planned procurement review by the Primary Inventory Control Activity (PICA) on Jul 22, 1998, this NSN's acquisition method was noted as: Acquire directly from the actual manufacturer, whether or not the prime contractor is the actual manufacturer. The Government physically does not have in its possession sufficient, accurate, or legible data to purchase this part from other than current source(s). (NOTE: This code is applicable only to parts under immediate buy requirements and only as long as the deficiency is under review for resolution and appropriate recoding.) Valid AMCs: 1, 2, 3, 4 and 5.

This NSN is assigned to Item Name Code (INC) 03365. [A CONTROLLER DESIGNED TO CONTROL AN AIRCRAFT THROUGH AN AUTOMATIC PILOT IN PITCH, YAW, ROLL AND COORDINATED TURNS.]. This item does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. There is no data in the HMIRS and the NSN is in an FSC not generally suspected of containing hazardous materials. NSN 6615011106322 does not contain precious metals.

This NSN is associated to Schedule B 9014900000: parts & accessories for direction finding compasses and other navigational instruments and appliances. The Schedule B End Use is listed as marine engines, parts. NAICS classification category 334511: search, detection, navigation, guidance, aeronautical, and nautical system and instrument manufacturing.

This information was last updated on .


Technical Characteristics

UNABLE TO DECODE
(ADTV) UNABLE TO DECODE
CASE MATERIAL
(ADTV) ALUMINUM
END ITEM IDENTIFICATION
(AGAV) MODULAR GUIDED BOMB GBU-15(V)1/B AND 2/B
CASE MATERIAL
(CWJK) ALUMINUM
CURRENT RATING IN AMPS
(AMPS) 0.2 AND 0.7
FREQUENCY IN HERTZ
(FREQ) 400.0
FUNCTIONAL DESCRIPTION
(FTLD) RELAYS COMMANDS RECVD FROM THE ACFT DIRECTLY OR INDIRECTLY THROUGH THE REMOTE CONTROL SUBSYSTEM DATA LINK TO THE TARGET DETECTING DEVICE FOR DETECTING, DESIGNATING AND TRACKING TARGETS; ALSO PROCESSES GUIDANCE AND INERTIAL STABILIZATION SIGNALS RECVD FROM THE MIDCOURSE GUIDANCE DEVICE, TARGET DETECTING DEVICE AND INERTIAL SENSORS INTO POSITION COMMANDS FOR THE FLIGHT CONTROL SURFACE ACTUATORS IN ORDER TO CONTROL THE FLIGHT PATH OF THE GBU-15(V)
MAXIMUM OVERALL HEIGHT
(CHQR) 4.200 INCHES
MAXIMUM OVERALL LENGTH
(CHQP) 9.800 INCHES
MAXIMUM OVERALL WIDTH
(CHQQ) 4.200 INCHES
MAXIMUM VOLTAGE RATING IN VOLTS
(AFXE) 115.0 AC AND 28.0 DC
PHASE
(FAAZ) SINGLE
POWER SOURCE
(ATJK) EXTERNAL
SPECIAL FEATURES
(FEAT) GUIDED BOMB AUTOMATIC PILOT; HAS ANALOG INPUTS FOR PITCH AND YAW, MIDCOURSE GUIDANCE DEVICE, INTERTIAL SENSORS, LINE OF SIGHT RATE COMMANDS; ANALOG OUTPUTS FOR FLIGHT CONTROL SYSTE; DISVRETE INPUTS AND OUTPUTS FOR ACFT COMMAMNDS, DATA LINK COMMANDS, IDENTIFIERS, TIME DELAY, WEAPON COMMANDS, WEAPON READY STATUS; DESIGNED FOR AIRBORNE GUIDED BOMB INSTALLATION; INSTALLED IN THE COMMON CONTROL MODULE BY MEANS OF 4 SOCKET HEAD CAP SCREWS; A SINGLE 158 CONTACT CONNECTOR ATTACHES TO THE COMMON CONTROL MODULE WIRING HARNESS

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