SEE 
SEE 
PERF/APU PAGE(BOTTOM DISPLAY)
APU DISPLAYS
APU PARAMETERS
APU AUTO EVENT MESSAGE(EXAMPLE) 
APU SENSORS
VARIOUS
APU: PARAMETER VALUES AND INDICATIONS ARE
EGT 640FOR ILLUSTRATION PURPOSES ONLY. 
RPM 87
0.25EICAS COMPUTER IS SOURCE FOR FUNCTION IDENTIFIERS. IDENTIFIERS ARE LIGHT BLUE IN COLOR, 
OIL Q DIGITAL READOUTS ARE WHITE IN COLOR. 
APU OIL QTYENGINE PARAMETERS ARE SAME AS ON FIG. 3.GUN 051
EICAS Displays - PERF/APU Page 
LIMITS - EGT (0 TO 900`C)
RPM (0 TO 120% RPM) 
-
OIL Q (0 TO 1.00 %FULL)
-4
INDICATES CONDITION THAT CAUSED APUAUTO EVENT 
Figure 5C 
D07703
A 
757 
MAINTENANCE MANUAL
ú
 31-41-00
 ALL  ú ú 08 Page 20 ú Jan 28/02
SEE
(AIRPLANES WITH EICAS COMPUTERS -108 AND SUBSEQUENT)
ENG EXCD PAGE(BOTTOM DISPLAY)
SEE
(AIRPLANES WITH -107 EICAS COMPUTERS)
ENG EXCD PAGE(BOTTOM DISPLAY)
EICAS COMPUTER IS SOURCE FOR FUNCTION IDENTIFIERS. IDENTIFIERS ARE LIGHT BLUE IN COLOR;
READOUTS ARE WHITE IN COLOR.
SEE TEXT FOR EXPLANATION.
PARAMETER VALUES AND INDICATIONS ARE FOR ILLUSTRATION PURPOSES ONLY.
1 SYMBOL NAME SOURCEPRIME REMARKS
ENGINE EXCEEDANCE DISPLAYS
EICAS INDICATES ENGINE
ENG EXCD PAGE IDENTIFIER COMPUTER EXCEEDANCE PAGEEICAS SHOWS MAXIMUM VALUE OF N1, EGT
N1 EXCEEDANCE
121.7 :06 N1 REDCOMPUTER 
START, EGT, N2, AND N3 FOR LEFTAND RIGHT ENGINES. ALSO SHOWS
762 :12 EGT STARTEGT START EXCEEDANCE 
TOTAL ACCUMULATED TIME (IN MINUTESAND SECONDS) THAT EACH PARAMETEREGT RED 8651:02
WAS IN EXCEEDANCE RANGE.
EGT EXCEEDANCE 
N2 RED 114.9 :03 
N2 EXCEEDANCE
N3 RED 107.4 :05 
N3 EXCEEDANCEMAX L EGTSTARTSTART LIMIT EICAS 
SHOWS PROFILE OF START LIMITEXCEEDANCE PROFILE 
 
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