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NSN 6615-01-442-8053, 6615014428053
PROCESSOR,FLIGHT CONTROL

Federal Supply Classification
FSC 6615 - Automatic Pilot Mechanisms and Airborne Gyro Components
National Item Identification Number
NIIN 014428053
Codification Country
United States
Item Name Code
INC 53048
Criticality
(Y) This item does not have a nuclear hardened feature but does have other critical feature(s) 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 6615-01-442-8053

National Stock Number (NSN) 6615-01-442-8053, or NIIN 014428053, (processor,flight control) was assigned March 24, 1997 in the Federal Logistics Information System (FLIS). NIIN 014428053 was cancelled on December 16, 2017, with a cancelled status of "Item is Cancelled - Inactive." There is no known replacement specified for this stock number. This NSN does not replace any other NSNs.

There are 3 manufacturer part numbers associated with this NSN. 2 of those part number(s) are considered obsolete. The manufacturer part numbers were originally supplied by 2 suppliers. Today, 2 suppliers are listed as Active suppliers 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.

This NSN is assigned to Item Name Code (INC) 53048. [A UNIT WHICH ACCEPTS AND PROCESSES INFORMATION FROM FLIGHT INSTRUMENTS AND THE CONTROL MECHANISM OF AN AIRCRAFT TO INITIATE A CHANGE IN THE POSITION OR COURSE OF THE AIRCRAFT.]. This item does not have a nuclear hardened feature but does have other critical feature(s) 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 6615014428053 does not contain precious metals.

This information was last updated on .


Technical Characteristics

DIRECT CURRENT VOLTAGE RATING IN VOLTS
(ACUR) 22.0 AND
FUNCTIONAL DESCRIPTION
(FTLD) USED TO COMPUTE PRIMARY FLIGHT CONTROL, STABILITY AND CONTROL AUGMENTATION AND AUTOMATIC FLIGHT CONTROL FUNCTIONS; PERFORMS ALL CALCULATIONS NECESSARY TO IMPLEMENT FUNCTIONS OF THE STABILITY AND CONTROL AUGMENTATION SYSTEM, AUTOPILOT, AUTOTHROTTLE, FLIGHT DIRECTOR, HEAD UP DISPLAY CONTROL AND GROUND PROXIMITY WARNING SYSTEM
DIRECT CURRENT VOLTAGE RATING IN VOLTS
(ACUR) 22.0 AND 29.5
UNPACKAGED UNIT LENGTH
(AJAF) 16.30 INCHES NOMINAL
INTELLIGENCE INPUT METHOD
(AXQJ) ELECTRICAL
SUPPLEMENTARY FEATURES
(SUPP) MANUFACTURERS NAME: COMPUTER,FLIGHT CONTROL
POWER SOURCE
(AWZJ) EXTERNAL
UNPACKAGED UNIT WIDTH
(AJAG) 10.10 INCHES NOMINAL
CRITICALITY CODE JUSTIFICATION
(CRTL) CBBL
END ITEM IDENTIFICATION
(AGAV) C-17 ACFT
SPECIAL FEATURES
(FEAT) OPERATING TEMP -40 TO 131 DEG F; ALTITUDE UP TO 50,000 FEET; MEMORY 314K; BASIC PROCESSOR UNIT WITHOUT SOFTWARE IS PART NUMBER 103E415G14; PART NUMBER 17B1U6001-555 IS THE BASIC UNIT WITH SOFTWARE VERSION 3.1 INSTALLED
UNPACKAGED UNIT HEIGHT
(AJAH) 7.60 INCHES NOMINAL
FEATURES PROVIDED
(CBBL) ELECTROSTATIC SENSITIVE

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