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REVISION NO: 15
DATE: 02/11/2009
PAGE:
27-4
1. 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM &
SEQUENCE
NUMBERS
ITEM
4. REMARKS OR EXCEPTIONS
27 FLIGHT CONTROLS
-21-1
Rudder Trim System
1)
Rudder Trim Control High Rate Function
C
1
0
2)
Rudder MANUAL TRIM CANCEL Switch
C
1
0
-21-2
Rudder Trim Indicator
C
1
0
(O) May be inoperative provided rudder trim is verified centered before each departure.
-31-1
Control Column Position Transducers
C
6
5
-32-1
Stall Warning Systems
C
2
1
1)
Stick Shakers
C
2
1
-41-1
Control Wheel Pitch Trim Switches
C
2
1
-41-2
Alternate Pitch Trim Position Switches
C
6
5
One may be inoperative provided both control wheel pitch trim switches operate normally.
-41-3
Stabilizer Trim Rate Solenoid Valves
C
2
1
-48-1
STAB Position Indicators
C
2
1
(O) One may be inoperative provided it is blanked or covered.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
BOEING B-777
REVISION NO: 15
DATE: 02/11/2009
PAGE:
27-5
1. 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM &
SEQUENCE
NUMBERS
ITEM
4. REMARKS OR EXCEPTIONS
27 FLIGHT CONTROLS
-48-2
Stabilizer Position Transducer Modules
C
3
2
-48-3
***
Nose Gear Pressure Switch
C
1
0
(O) May be inoperative provided stabilizer trim position is verified to be properly set before each departure.
-48-4
***
Nose Gear Pressure Transducer
C
1
0
(O) May be inoperative provided stabilizer trim position is verified to be properly set before each departure.
-51-1
Inboard Flap, Outboard Support Mechanism Springs (No. 3 & No. 6 Supports)
A
4
2
(M) One may be broken or missing on each support provided:
a)
Broken springs are removed,
b)
Remaining spring on each support is verified in place and not broken before each departure, and
c)
Operations are limited to fifteen departures before repairs are made.
-59-1
Flap/Slat Skew Sensors
C
28
14
-61-1
Speedbrake Lever Position Transducers
C
4
3
-61-2
Spoiler Auxiliary Retract Device (SARD) (-300)
A
2
1
One may be inoperative provided:
a)
Associated passenger entry door 3 is considered inoperative, and
b)
Repairs are made within one flight day.
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U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
BOEING B-777
REVISION NO: 15
DATE: 02/11/2009
PAGE:
27-6
1. 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM &
SEQUENCE
NUMBERS
ITEM
4. REMARKS OR EXCEPTIONS
27 FLIGHT CONTROLS
-61-3
Spoiler Power Control Units (PCUs)
|
1)
Passenger (With PRRs 61384-15 and 62200, or Equivalent Installed)
A
14
12
(M)(O) One symmetrical pair (except 4/11) may be inoperative provided:
a)
Symmetrical pair is deactivated in the retracted position,
b)
Remaining spoilers are verified to operate normally,
c)
Appropriate performance adjustments are applied, and
d)
Repairs are made within three flight days.
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2)
777F
A
14
12
(M)(O) One symmetrical pair (except 4/11) may be inoperative provided:
a)
Symmetrical pair is deactivated in the retracted position,
b)
Remaining spoilers are verified to operate normally,
c)
Appropriate performance adjustments are applied, and
d)
Repairs are made within three flight days.
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-62-1
Automatic Speedbrake Function
C
1
0
(M)(O) May be inoperative deactivated provided:
a)
Landing gear truck tilt pressure is verified to be normal before each flight, and
b)
Appropriate performance adjustments are applied.
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U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
BOEING B-777
REVISION NO: 15
　
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