D PRESSURE COMPENSATOR. FOR GE GAS GENE
UNIT# 8 AND 9;SERIAL # 296856 AND 296857.
203127737
COMPRESSOR,AIR,558 ACFM,261 PSIA,STG 4
COMPRESSOR,AIR:
COMPRESSION METHOD:
CENTRIFUGAL/ATOMIZING;
CAPACITY:
558 ACFM;
DISCHARGE PRESSURE:
261 PSIA;
MOUNTING:
SKID;
STAGE:
4;
ADDITIONAL DATA:
CENTRIFUGAL ATOMIZING, 550 MM WD X 700
MM LG X 450 MM HT, ASSEMBLY # 806993G07
, SERIAL # ACC97-80594, INLET PRESSURE
ABS: 149 PSIA, 50100 RPM, INLET TEMPERA
TURE: 225 DEG F, SERIAL # ACC96-80449 A
ND ACC95-80196, MAXIMUM WORKING PRESSUR
E: 500 PSIG, MAXIMUM WORKING TEMPERATUR
E: 500 DEG F, FOR ATOMISING AIR SERIAL
# S9880-21636, 9880-21605, 9878-21509 A
ND 9882-21676 USED ONGE GAS TURBINE MOD
EL # MS7001E SERIAL # 296856, 296857.
ATLAS COPCO INCORPORATED:
DWG#417126000
ATLAS COPCO INCORPORATED:
P/N#A88G637411
ATLAS COPCO INCORPORATED:
Model#SCF6-558 ACFM
GENERAL ELECTRIC/DIELEKTROL/LENTRONICS:
P/N#302A1537P005/302A1537P5
ATLAS COPCO INCORPORATED:
DWG#417C126
GENERAL ELECTRIC/DIELEKTROL/LENTRONICS:
P/N#G060700
GENERAL ELECTRIC/DIELEKTROL/LENTRONICS:
P/N#SCF6/302A1537P5
TUBE,CROSSFIRE-COMBUSTION,SSTL,#188D4719G1
TUBE,--:
TYPE:
CROSSFIRE-COMBUSTION;
SIZE:
2 IN ID X 2-1/4 IN OD X 1 FT AND 3-1/2
IN LG;
MATERIAL:
SSTL;
ADDITIONAL DATA:
CROSS FIRING COMBUSTION 7E W SWIRL REV.
C, VC45295, A88G577145 TOTAL OF HOLES 3
0 NUMONIC, FOR COMBUSTION CHAMBER ARRAN
GEMENT SER NO:248901, 248908 TO 248911
282395 TO 282398 ,282483 ,AND 242484 TU
RBINE UNIT NO, 4 -7 AND 13 - 18 . FOR G
E GAS TURBINE-MS7001B AND E
GENERAL ELECTRIC/DIELEKTROL/LENTRONICS:
188D4719G001/188D4719G1
ELEMENT,HTR OL,OIL RELAY,CD C592A,#CR123
ELEMENT,HEATER OVERLOAD:
OPERATION METHOD:
OIL RELAY;
CODE:
C592A;
ADDITIONAL DATA:
OIL RELAY, 12 MM WD X 32 MM LG X 40 MM
HT, 3 PCS PACK, FOR OIL RELAY OF GE GAS
TURBINE MODEL # MS7001.
GENERAL ELECTRIC/DIELEKTROL/LENTRONICS:
P/N#CR123C5.92A
3PCS/PACK
