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C
9
7
-02-3
Primary Flight Computer (PFC) Channels
A
3
2
(M) One may be inoperative deactivated provided:
a)
Operations are limited to three flights before repairs are made, and
b)
Approach minimums do not require its use.
-02-4
PFCS Interface
C
1
0
(M) May be inoperative provided landing gear truck tilt pressure is verified to be normal before each departure.
-02-5
Actuator Pressure Sensors
B
7
6
One flaperon or rudder sensor may be inoperative.
-02-6
Flight Control Hydraulic Shutoff Valve Systems
C
6
3
(M) May be inoperative provided the associated valve is deactivated open.
-02-7
Item Moved
Dispatch relief for this equipment moved to item 27-02-6.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
BOEING B-777
REVISION NO: 15
DATE: 02/11/2009
PAGE:
27-2
1. 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM &
SEQUENCE
NUMBERS
ITEM
4. REMARKS OR EXCEPTIONS
27 FLIGHT CONTROLS
-02-8
Thrust Asymmetry Compensation (TAC) Function (Except
-200LR/GE90-115B and 777F/GE90-115B)
C
1
0
|
|
|
|
-03-1
Flap/Slat Control Lanes
C
2
1
(M) One may be inoperative provided:
a)
Flap lever control position sensor is verified to operate normally, and
b)
Alternate control is verified to operate normally before each departure.
|
|
|
|
-03-2
Flap Secondary Control
C
1
0
(M) May be inoperative provided Slat Secondary Control is verified to operate normally.
|
|
-03-3
Slat Secondary Control
C
1
0
(M) May be inoperative provided Flap Secondary Control is verified to operate normally.
|
|
-11-1
Aileron Trim System
C
1
0
(M)(O) May be inoperative deactivated provided:
a)
Aileron trim system is verified to be centered before departure, and
b)
Autopilot roll modes operate normally.
-11-2
Control Wheel Position Transducers
C
6
5
-11-3
Aileron Power Control Units (PCUs)
|
1)
Passenger (With PRRs 61384-15 and 62200 or Equivalent Installed)
A
4
3
(M) One may be inoperative provided:
a)
Inoperative PCU is deactivated in the bypass mode,
b)
Inoperative PCU blocking mode is verified to operate normally,
c)
Ailerons are verified to operate normally, and
d)
Repairs are made within three flight days.
|
|
|
|
|
|
|
|
|
(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:
27-3
1. 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM &
SEQUENCE
NUMBERS
ITEM
4. REMARKS OR EXCEPTIONS
27 FLIGHT CONTROLS
-11-3
Aileron Power Control Units (PCUs) (Cont’d)
|
2)
777F
A
4
3
(M)(O) One may be inoperative provided:
a)
Inoperative PCU is deactivated in the bypass mode,
b)
Inoperative PCU blocking mode is verified to operate normally,
c)
Ailerons are verified to operate normally,
d)
Appropriate performance adjustments are applied, and
e)
Repairs are made within three flight days.
|
|
|
|
|
|
|
|
|
|
-11-4
Flaperon Power Control Units (PCUs)
|
1)
Passenger (With PRRs 61384-15 and 62200, or Equivalent Installed)
A
4
3
(M) One may be inoperative provided:
a)
Inoperative PCU is deactivated in the bypass mode,
b)
Flaperons are verified to operate normally, and
c)
Repairs are made within three flight days.
|
|
|
|
|
|
|
2)
777F
A
4
3
(M) One may be inoperative provided:
a)
Inoperative PCU is deactivated in the bypass mode,
b)
Flaperons are verified to operate normally, and
c)
Repairs are made within three flight days.
|
|
|
|
|
|
|
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
BOEING B-777
　
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