1
1
2
2
3
3
4
4
5
5
6
6
7
7
8
8
D D
C C
B B
A A
EA 300/LT
EFD 1000 PFD
7, 5A
AVIONIC-BUS
AIRCRAFT POWER
AI RC R AFT G ROU ND
AI RC R AFT G ROU ND
EFD-1000 DISPLAY
PFD
1
2
4
5
EA-9D102 .46
21.04.10 HW
A/C GND
AI RCRAFT G ROUND
AIRCRAFT POWER
6
3
7
AIRCRAFT POWER
30
31
32
33
34
RSM_C
RSM_D
RSM_E
36
RSM_G
CONFIG_B
CONFIG_C
CONFIG_A
CONFIG_D
RSM_A
RSM_B
41
42
43
44
35RSM_F
#18
#18
DIGITAL_OUT
Die Gültigkeitszuord nung
von Version zu
dem jeweil igen Fertigungsauftrag
zu entnehmen.
Zuordnun g lin ks / rechts w ird mit
*/* in allen Feldern angeg eben.
04
03
02
01
Ver. Bezeichnung
Nr. : Änderun g/Mod . Nr. : Datum Name
Letzte Bearbeitung:
Datum Name
Bearb.:
Gepr.:
Maßstab
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Ob erfläc hensch utz
Projektion
Freimaßtoleran z
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Sch ut zvermerk na ch DIN 34 beach te n.
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auf
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Gepr.:
Flugzeug baureihe
ist der Bauakte b zw.
1A3 1
#24
#24
#24
#24
#24
#24
CONFIG_B
CONFIG_D
CONFIG_A
CONFIG_C
1
2
3
4
CONFIG_S
5
1
2
3
4
5
RSM_C
RSM_D
RSM_E
7
RSM_G
RSM_A
RSM_B
6
RSM_F
CONFIGURATION MODULE PFD
REMOTE SENSOR PFD
DD44 F1 00 00
P1
Hirose SR30-10PF-7P(71)
P3
Molex 5 0-57-90 45
P2
blk
brn
org
red
blk
brn
org
red
41 2- 0 004-00 1
#24
#24
#24
#24
#24
#24
#24
#24
#24
#24
#24
#24
#24
#24
max 12'
910-00001-001
920-00004-00x
910-00003-001
#18
16
17
18
19
429 GPS RX1 A
429 GPS RX1 B
429 VL OC RX2A
429 VL OC RX2B
429 GPS/VLOC TXB
429 GPS/VLOC TXA 26
27
ws
bl
ws
bl
ws
bl
#24
#24
#24
16
17
429 GPS RX1A
429 GPS RX1B
RS232_RX4
RS232_TX2
11
14
RS232_RX5
RS232_TX2
14
12
D-SU B 44S
AIRFRAME GROUND
CHASS IS STUD
#24
ws
bl
24
25
429 TAS RX5A
429 TAS RX5B
ws
bl #2 4
24
25
429 TAS RX5A
429 TAS RX5B
P1
EFIS-MFD
EFD-500/1000 MFD
#24
#24
#24
#24
ws
bl
ws
bl
ws
bl
ws
bl
#24
ws
bl
OPTIONEN
EA3D0955
0204 03 BenennungNr01 Teilekennzeichen ZF Werkstoff Abmessungen Menge Gew ichtEinheit MaWi-Nr.
1
2
3
4
CONFIGURATION MODULE (PFD-PIL)
1
1
910-00003-001
5
REMOTE SENSOR MODULE1
1
1
920-00004-001
EFD 1000 (DISPLAY)
910-00001-001
CIRCUIT BREAKER 7,5A
116-00022-002CONNEC TOR S UBD 44S
7277-2-7,5
6
7
8
CONNEC TOR R SM CIRC ULAR
1
1
MIL-C-27500 -18TG 1
9
WIRE AWG18 SHIELDX
116-00020-001
CONNEC TOR 5S WITH CABLE
412-00004-001
X
mtr
WIRE AWG18
MIL-W-22759/16-18
3
2
7
1
5 8
4
10
6
mtr
10X
mtr
WIRE AWG24
12
ARINC 429 IN 1 B
32 ARINC 429 IN 1 A
35
30
28
ARINC 429 Out 2 A
ARINC 429 Out 2 B
P1
TRANSPOND ER
GTX-330/328
#24
#24
ws
bl
ws
bl
46
47
24
23
50
51
ARINC 429 IN 2 A
ARINC 429 IN 2 B
VO R/ ILS ARINC 429 OUT A
ARINC 429 OUT 1 A
ARINC 429 OUT 1 B
VO R/ ILS ARINC 429 OUT B
ARINC 429 In 1 A
ARINC 429 In 1 B
48
49
COM/NAV/GPS SYSTEM
GNS-430 W
P4001 P4006
#24
#24
ws
bl
ws
bl
ws
bl
ws
bl
ws
bl
ws
bl
ws
bl
ws
bl
ws
bl
ws
bl
Opti on EFD-5 00/1 000 MFD EA-9D1 02.47
Opti on TRAN SPONDER GT X-330/ 328
EA-9D1 02.54Opti on COM/NAV/ GPS GNS-430W
EA-93 102.21
46
47
50
51
48
49
GNC-420W
P4001
Option 01 = PFD "Pilot" installation (no HSI)
2
Option 02 = PDF "Pro" installation (including HSI)
3
2 CONFIGURATION MODULE (PFD-PRO)1
920-00004-002
1
1
1
1
1
1
X
X
X
1
1
additional MFD installation is optional
2
optional PFD "Pro" requires GNS-430W or GTN-650/GTN-750 to be installed. PDF "Pilot" requires GNC-420W or GTN-635 to be installed.
3
optional PFD installation requires GTX-330; GTX-328 or GTX-33 to be installed
9
11X
mtr
SHI ELDX
MIL-W-22759/16-24
11
12XGROUND WIRE
EA-86201.1
X
10
29
24
23
47
66
GTN-650/750
P1001 P1004
32
35
30
28
P3301
GTX-33
10
29
47
66
GTN-63 5
P4001
EA-9D102.63 & EA-9E102.63Option COM/NAV/GPS GTN-650/750
Opti on TRAN SPONDER GT X-33 EA-9D102 .64
15RS232_TX3
RS232 IN 3
25
RS232 IN 2
24
PFD
A
05.09.1 2 HWAÄM-300-12-01
24
19
18
429 VL OC RX2B
429 VL OC RX2A
#24 ws
bl
ws
bl
ws
bl
ws
bl
25
EA-9D1 02.48Option COM/GPS GNC-420W
EA-9D102.62 & EA-9E102.62Opti on COM/GPS GTN-63 5
32112
00776
FE4011
20.10.1 2 HW
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