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(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
BOEING B-777
REVISION NO: 15
DATE: 02/11/2009
PAGE:
30-4
1. 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM &
SEQUENCE
NUMBERS
ITEM
4. REMARKS OR EXCEPTIONS
30 ICE AND RAIN PROTECTION
-21-1
Engine Anti-Ice Systems (Cont’d)
2)
GE (Cont’d)
C
2
1
(M)(O) For operations at ambient temperature38 degrees C or below, one may be inoperative provided:
a)
Valve is electrically disconnected and verified open,
b)
Engine fan case overheat detection system operates normally,
c)
Associated EAI pressure sensor system operates normally,
d)
Associated EAI card operates normally,
e)
Turbine case cooling air flow systems operate normally,
f)
Appropriate performance adjustments are applied, and
g)
Except for GE90-100 series, EECs are operated in the normal mode.
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A
2
1
(M)(O) For operations at ambient temperature above 38 degrees C, one may be inoperative provided:
a)
Valve is deactivated open using deactivation kit,
b)
Engine fan case overheat detection system operates normally,
c)
Turbine case cooling air flow systems operate normally, and
d)
Appropriate performance adjustments are applied,
e)
Repairs are made within three flight days, and
f)
Except for GE90-100 series, EECs are operated in the normal mode.
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(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
BOEING B-777
REVISION NO: 15
DATE: 02/11/2009
PAGE:
30-5
1. 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM &
SEQUENCE
NUMBERS
ITEM
4. REMARKS OR EXCEPTIONS
30 ICE AND RAIN PROTECTION
-21-1
Engine Anti-Ice Systems (Cont’d)
2)
GE (Cont’d)
A
2
1
(M)(O) For operations at ambient temperature above 38 degrees C, one may be inoperative provided:
a)
Valve is electrically disconnected and verified open,
b)
Engine fan case overheat detection system operates normally,
c)
Associated EAI pressure sensor system operates normally,
d)
Associated EAI card operates normally,
e)
Turbine case cooling air flow systems operate normally,
f)
Appropriate performance adjustments are applied,
g)
Repairs are made within three flight days, and
h)
Except for GE90-100 series, EECs are operated in the normal mode.
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-21-2
Engine Anti-Ice Indications (EAI)
C
2
0
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
BOEING B-777
REVISION NO: 15
DATE: 02/11/2009
PAGE:
30-6
1. 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM &
SEQUENCE
NUMBERS
ITEM
4. REMARKS OR EXCEPTIONS
30 ICE AND RAIN PROTECTION
-31-1
Pitot Probe Heater Systems
1)
Right Pitot Heater
B
1
0
(M) May be inoperative provided:
a)
Right pitot air data module is deactivated,
b)
Left and center pitot air data modules operate normally,
c)
Left and center pitot probe heater systems operate normally,
d)
Left static air data module operates normally,
e)
Standby airspeed indication operates normally,
f)
Right AIR DATA/ATT instrument source switch operates normally,
g)
Approach minimums do not require its use,
h)
SAARU data is verified to be available to the right PFD before each departure, and
i)
Left and center pitot probes are inspected before each departure.
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2)
Left Pitot Heater
B
1
0
(M) May be inoperative provided:
a)
Left pitot air data module is deactivated,
b)
Right and center pitot air data modules operate normally,
c)
Right and center pitot probe heater systems operate normally,
　
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