6605-14-553-7127

Aircraft Attitude Computer

6605145537127 145537127 B453AAM

A computer that contains the follow-up servo for pitch and roll information from the platform, and the circuitry for computing vertical attack angles, climb angle, vertical velocity, and ground speed to altitude ratio. View more Aircraft Attitude Computer

6605-14-553-7127 COMPUTER,AIRCRAFT ATTITUDE 6605145537127 145537127

Managed by France
NSN Created on 14 May 2007
Data Last Changed
January 2023
NATO Update Count
1
NATO Data Quality
6605-14-553-7127 COMPUTER,AIRCRAFT ATTITUDE 6605145537127 145537127 1/1
NSN 6605-14-553-7127 (Generic Image) 1/1

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Aircraft Attitude Computer (INC 53058)
6605-01-500-0499 Aircraft Attitude Computer HG2011AC03RNCC: 3 | RNVC: 2 | DAC: 4 12 Aug 2002 6605-14-553-7127

6605-14-553-7127 Demil Restrictions 6605-14-553-7127

DEMIL: | DEMILI: | CRITICALITY: | HMIC: | PMIC: | EDC: | ADPEC:

6605-14-553-7127 is a Aircraft Attitude Computer

6605-14-553-7127 End Users End Users 6605-14-553-7127

Italy (ZR)

6605-14-553-7127 Manufacturers Approved Sources 6605-14-553-7127

Part Number
Manufacturer
Status
B453AAM
F9111 - Thales Avs France Sas (Active)
Primary Buy
RNCC 3 RNVC 2 DAC 2
B453AAM
F6306 - S.F.E.N.A. (Ste Francaise (Replaced)
Original Design
RNCC 3 RNVC 9 DAC 2

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6605-00-915-9319 6605-01-524-9582 6605-01-594-3801 6605-01-622-9362 6605-01-659-9926 6605-01-681-2819 6605-16-004-6073 6605-01-500-0499 6605-01-707-1031 6605-12-379-4247 6605-01-648-1519 6605-14-553-7127