G - Electrical systems
p. 48
G.
Electrical systems
4. ACW schematic
ATA 24
NP=0
NP=0
ACW supplied by the External Power
– When the ACW GPU is available (
AVAIL
) but not ON, the GPU supplies only the ACW
Service Bus, if the GND Service Bus switch, on the flight attendant panel, is ON.
– When the ACW GPU is
ON
, the GPU supplies through the BTC, the ACW BUS 1, the ACW
BUS 2 and the ACW SVCE BUS.
– Even if one ACW generator is available, the GPU has always the priority.
ACW
GEN 1
ACW BUS 1
ACW BUS 2
TRU
ACW
GEN 2
SVCE BUS
ACW
GPU
NP=0
NP=0 in hotel mode
NP<20% with prop feathered
ACW in Hotel mode or with the propeller feathered
NOTE:
An ACW Generator is available if the NP is above 66%.
– When the right engine is running in hotel mode, the NP=0.
– When the engines are running but the propeller is feathered, the NP is bellow 20%
In both cases the ACW Busses are not supplied
ACW
GEN 1
ACW BUS 1
ACW BUS 2
TRU
ACW
GEN 2
SVCE BUS
ACW
GPU
NP=0
NP=70.8%
The propeller unfeathered and one ACW GEN on line
On ground, when the propeller is unfeathered, the engine is running on fuel governing mode.
The fuel governing mode, maintain a minimum NP of 70.8%, in order to have the ACW
available (ACW GEN on line at 66%)
The ACW GEN supplies, the ACW BUS 2 and ACW BUS 1 through the BTC, but the SVCE
BUS is shed (one generator is not able to supply all the busses)
CAUTION:
on ground in case of an EEC or PEC fault, the fuel governing mode is lost and the
ACW generator is not available (NP<66%)
ACW
GEN 1
ACW BUS 1
ACW BUS 2
TRU
ACW
GEN 2
SVCE BUS
ACW
GPU
09T2253_ATR_systems42_72PEC_AtoH.indd 48
19/05/10 11:05
Summary of Contents for 42-500
Page 1: ...72 212A 42 500 ...
Page 7: ...A Aircraft general p 6 A Aircraft general p 6 A Aircraft general FCOM 1 00 ...
Page 12: ...A Aircraft general p 11 8 Internal lighting ATA 33 ...
Page 14: ...B Multi Function Computer p 13 B Multi Function Computer FCOM 1 01 ...
Page 16: ...C Centralized crew alerting system p 15 C Centralized crew alerting system FCOM 1 02 ...
Page 22: ...D Air p 21 D Air FCOM 1 03 ...
Page 30: ...E Automatic flight control system p 29 E Automatic flight control system FCOM 1 04 ...
Page 33: ...F Communications FCOM 1 05 p 32 F Communications ...
Page 38: ...G Electrical systems p 37 G Electrical systems FCOM 1 06 ...
Page 52: ...H Emergency equipment p 51 H Emergency equipment FCOM 1 07 ...
Page 57: ...I Fire protection p 56 I Fire protection FCOM 1 08 I Fire protection p 56 ...
Page 60: ...J Flight control p 59 J Flight control FCOM 1 09 ...
Page 65: ...K Flight instruments p 64 K Flight instruments FCOM 1 10 K Flight instruments p 64 ...
Page 74: ...L Fuel system p 73 L Fuel system FCOM 1 11 ...
Page 83: ...M Hydraulic system p 82 M Hydraulic system FCOM 1 12 M Hydraulic system p 82 ...
Page 86: ...N Ice and rain protection p 85 N Ice and rain protection FCOM 1 13 ...
Page 92: ...O Landing gear p 91 O Landing gear FCOM 1 14 ...
Page 95: ...P Navigation system p 94 P Navigation system FCOM 1 15 P Navigation system p 94 ...
Page 98: ...P Navigation system p 97 MODE 4 unsafe terrain clearance MODE 5 below glideslope ...
Page 102: ...Q Power plant p 101 Q Power plant FCOM 1 16 ...
Page 110: ...Annexes p 109 Annexes ...
Page 128: ...p 127 ...