CURRENTECH
214-693-
REVISION: B
2.8.4
The P2 connector is utilized for unit power, ground, switch logic, and annunciator logic inputs
and outputs. The electrical contacts will accommodate 20 or 24 AWG wire.
Crimp tooling required is M22520/2
(Daniels Mfg.). Refer to "
Refer to "
specific connections for the P
The +28VDC input
Power for the unit should be
galley bus.
The power ground
close as practical to the unit connector.
The Fault
load and may be utilized for annunciation or relay switching.
The Fault
control annunciator
color and Green
cockpit mounted status annunciators ensure that appropriate isolation techniques are
employed.
CURRENTECH
-6751
REVISION: B
2.8.4 P2 PINOUT
2 connector is utilized for unit power, ground, switch logic, and annunciator logic inputs
and outputs. The electrical contacts will accommodate 20 or 24 AWG wire.
Crimp tooling required is M22520/2
(Daniels Mfg.). Refer to "
Refer to "Table 5 Connector J
connections for the P
The +28VDC input (pin 1)
Power for the unit should be
galley bus.
ower ground (pin 2) and signal ground (pin 11)
close as practical to the unit connector.
The Fault Hi (pin 5) and Norm Hi (pin
load and may be utilized for annunciation or relay switching.
Fault GND (pin 4)
control annunciator monitoring
color and Green for the Norm annunciator color.
cockpit mounted status annunciators ensure that appropriate isolation techniques are
employed. The annunc
Figure
2 PINOUT DESCRIPTIONS
2 connector is utilized for unit power, ground, switch logic, and annunciator logic inputs
and outputs. The electrical contacts will accommodate 20 or 24 AWG wire.
Crimp tooling required is M22520/2
(Daniels Mfg.). Refer to "Figure 4
Connector J2 Pin Function List
connections for the P2 connector
(pin 1) must be circuit breaker protected by a 1 amp rated circuit breaker.
Power for the unit should be supplied by a non
(pin 2) and signal ground (pin 11)
close as practical to the unit connector.
Hi (pin 5) and Norm Hi (pin
load and may be utilized for annunciation or relay switching.
GND (pin 4) and Norm GND
monitoring circuits.
the Norm annunciator color.
cockpit mounted status annunciators ensure that appropriate isolation techniques are
The annunciators may be mounted in the cockpit for flight crew monitoring of
**Mating face view of pin
P1 Connector
Figure 3 AGFCI Unit
DESCRIPTIONS
2 connector is utilized for unit power, ground, switch logic, and annunciator logic inputs
and outputs. The electrical contacts will accommodate 20 or 24 AWG wire.
Crimp tooling required is M22520/2-01 Crimp Tool (Daniels Mfg.) with M2252
4 AGFCI Unit J
2 Pin Function List
2 connector.
must be circuit breaker protected by a 1 amp rated circuit breaker.
supplied by a non
(pin 2) and signal ground (pin 11)
close as practical to the unit connector.
Hi (pin 5) and Norm Hi (pin 6) +28VDC
load and may be utilized for annunciation or relay switching.
and Norm GND (pin 3)
circuits. Typical installations use
the Norm annunciator color.
cockpit mounted status annunciators ensure that appropriate isolation techniques are
iators may be mounted in the cockpit for flight crew monitoring of
**Mating face view of pin
P1 Connector Wire Side Layout Is Opposite
AGFCI Unit J1 Connector Layout
DESCRIPTIONS
2 connector is utilized for unit power, ground, switch logic, and annunciator logic inputs
and outputs. The electrical contacts will accommodate 20 or 24 AWG wire.
01 Crimp Tool (Daniels Mfg.) with M2252
AGFCI Unit J2 Connector Layout
2 Pin Function List, and "Figure
must be circuit breaker protected by a 1 amp rated circuit breaker.
supplied by a non-essential aircraft bus or a non
(pin 2) and signal ground (pin 11) should be connected to airframe ground as
6) +28VDC outputs are
load and may be utilized for annunciation or relay switching.
(pin 3) outputs are Ground/Open logics
Typical installations use
the Norm annunciator color. In the case of interfacing these outputs with
cockpit mounted status annunciators ensure that appropriate isolation techniques are
iators may be mounted in the cockpit for flight crew monitoring of
**Mating face view of pin layout** Aircraft
Wire Side Layout Is Opposite
1 Connector Layout
2 connector is utilized for unit power, ground, switch logic, and annunciator logic inputs
and outputs. The electrical contacts will accommodate 20 or 24 AWG wire.
01 Crimp Tool (Daniels Mfg.) with M2252
2 Connector Layout" for details.
Figure 5 Interconnect D
must be circuit breaker protected by a 1 amp rated circuit breaker.
essential aircraft bus or a non
should be connected to airframe ground as
outputs are rated at 400 m
load and may be utilized for annunciation or relay switching.
outputs are Ground/Open logics
Typical installations use White
In the case of interfacing these outputs with
cockpit mounted status annunciators ensure that appropriate isolation techniques are
iators may be mounted in the cockpit for flight crew monitoring of
layout** Aircraft
Wire Side Layout Is Opposite
1 Connector Layout
2 connector is utilized for unit power, ground, switch logic, and annunciator logic inputs
and outputs. The electrical contacts will accommodate 20 or 24 AWG wire.
01 Crimp Tool (Daniels Mfg.) with M22520/
" for details.
Interconnect Diagram
must be circuit breaker protected by a 1 amp rated circuit breaker.
essential aircraft bus or a non-essential cabin or
should be connected to airframe ground as
rated at 400 milliamp
outputs are Ground/Open logics that are used to
White as the Fault annunciator
In the case of interfacing these outputs with
cockpit mounted status annunciators ensure that appropriate isolation techniques are
iators may be mounted in the cockpit for flight crew monitoring of
layout** Aircraft
Wire Side Layout Is Opposite
AGFCI
2 connector is utilized for unit power, ground, switch logic, and annunciator logic inputs
0/2-08 Positioner
iagram" for
must be circuit breaker protected by a 1 amp rated circuit breaker.
essential cabin or
should be connected to airframe ground as
mp maximum
that are used to
as the Fault annunciator
In the case of interfacing these outputs with
cockpit mounted status annunciators ensure that appropriate isolation techniques are
iators may be mounted in the cockpit for flight crew monitoring of
AGFCI
9
2 connector is utilized for unit power, ground, switch logic, and annunciator logic inputs
Positioner
must be circuit breaker protected by a 1 amp rated circuit breaker.
essential cabin or
should be connected to airframe ground as
maximum
that are used to
as the Fault annunciator
In the case of interfacing these outputs with
