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AIRCRAFT:
BOEING B-777
REVISION NO: 15
DATE: 02/11/2009
PAGE:
30-1
1. 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM &
SEQUENCE
NUMBERS
ITEM
4. REMARKS OR EXCEPTIONS
30 ICE AND RAIN PROTECTION
-11-1
Wing Anti-Ice Systems
C
2
0
(M) May be inoperative provided:
a)
Associated valve is locked closed,
b)
Wing anti-ice control switch remains OFF, and
c)
Airplane is not operated in known or forecast icing conditions.
-11-2
Wing Anti-Ice Control (Card and Switch)
C
1
0
(M) May be inoperative provided:
a)
Both wing anti-ice valves are locked closed,
b)
Wing anti-ice control switch remains OFF, and
c)
Airplane is not operated in known or forecast icing conditions.
-11-3
Wing Anti-Ice Indications (WAI)
C
2
0
-21-1
Engine Anti-Ice Systems
C
2
1
(M) One may be inoperative provided:
a)
Valve is locked closed,
b)
Associated engine anti-ice control switch remains OFF,
c)
Airplane is not operated in known or forecast icing conditions, and
d)
Flight remains within 120 minutes of landing at a suitable airport.
(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:
30-2
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)
1)
PW and RR
C
2
1
(M)(O) For operations at ambient temperature 38 degrees C or below, one may be inoperative provided:
a)
Valve is deactivated open using deactivation kit,
b)
Engine fan case overheat detection system operates normally, and
c)
Appropriate performance adjustments are applied.
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C
2
1
(M)(O) For operations at ambient temperature 38 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, and
e)
Appropriate performance adjustments are applied.
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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)
Appropriate performance adjustments are applied, and
d)
Repairs are made within three flight days.
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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:
30-3
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)
1)
PW and RR (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)
Appropriate performance adjustments are applied, and
f)
Repairs are made within three flight days.
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2)
GE
C
2
1
(M)(O) For operations at ambient temperature 38 degrees C or below, 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,
d)
Appropriate performance adjustments are applied, and
e)
Except for GE90-100 series, EECs are operated in the normal mode.
　
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