|
National Stock Number(NSN): 6615-01-464-9820 (6615014649820, 014649820)
| NIIN: |
01-464-9820⛔ |
Item Name: |
PROCESSOR,FLIGHT CONTROL |
INC: |
53048
|
| FSC: |
6615
|
Assignment Date: |
May-17-1999 |
CRIT: |
Y |
IIG: |
53048 |
| ISC: |
3 |
Date Standardized: |
Feb-24-2003 |
HMIC: |
N |
DODIC: |
|
| NSC: |
8 |
Cancellation Date: |
Dec-15-2017 |
PMIC: |
A |
FIIG: |
A30800 |
| ESD: |
A |
Schedule B: |
9014.90.0000 |
DEMIL: |
A |
DEMIL INT: |
1 |
| TIIC: |
1 |
Originator: |
TU |
ADPEC: |
0 |
RPDMRC: |
|
| Part Number |
CAGE |
Company |
Status |
RN CC |
RN VC |
DAC |
RN AAC |
RN FC |
RN SC |
RN JC |
SADC |
HCC |
MSDS |
|
17B1U6001-571 |
88277
|
THE BOEING COMPANY |
H |
3 |
2 |
4 |
ZZ |
|
|
|
|
|
|
| MOEC |
SOS |
A A C |
R C |
S L C |
CIIC |
U P Q |
U S C |
Unit Price |
UI |
UICF |
MCD |
Action Date |
C/H |
| DF |
JCD |
Y |
T |
0 |
U |
1 |
L |
$436,696.76 |
EA |
|
--SBA-N |
Feb-01-2008 |
H |
| MOEC |
PC |
Phrase |
QPA |
UOM |
OOU |
JTC |
| DF |
N |
DISPOSAL |
000 |
|
|
|
Technical Characteristics Information
| MRC |
Requirement Statement |
Reply Statement |
| ACUR |
DIRECT CURRENT VOLTAGE RATING IN VOLTS |
28.0 |
| AGAV |
END ITEM IDENTIFICATION |
C-17 ACFT |
| AJAF |
UNPACKAGED UNIT LENGTH |
16.30 INCHES NOMINAL |
| AJAG |
UNPACKAGED UNIT WIDTH |
10.10 INCHES NOMINAL |
| AJAH |
UNPACKAGED UNIT HEIGHT |
7.60 INCHES NOMINAL |
| AWZJ |
POWER SOURCE |
EXTERNAL |
| AXQJ |
INTELLIGENCE INPUT METHOD |
ELECTRICAL |
| CBBL |
FEATURES PROVIDED |
ELECTROSTATIC SENSITIVE |
| CRTL |
CRITICALITY CODE JUSTIFICATION |
CBBL |
| FEAT |
SPECIAL FEATURES |
MFG NAME COMPUTER, FLIGHT CONTROL, OPERATING TEMP -40 TO 131 DEG F; ALTITUDE UP TO 50K FT; MEMORY 314K; BASICPROCESSOR UNIT WITHOUT SOFTWARE IS P/N103E4151G103; P/N 17B1U6001-571 IS THEBASIC UNIT W/SOFTWARE VERSION 6.1 INSTALLELD |
| FTLD |
FUNCTIONAL DESCRIPTION |
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, HEADS UP DISPLAY CONTROL AND GROUND PROXIMITY WARNING SYSTEM |
Replacement & Obsolete Information
| Replaced / Replacement NIIN Information |
|