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Other procedures do not require use of APU, and
b)
Flight remains within 180 minutes of landing at a suitable airport.
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|
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-94-2
APU OIL PRESS Indication
C
1
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:
52-1
1. 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM &
SEQUENCE
NUMBERS
ITEM
4. REMARKS OR EXCEPTIONS
52 DOORS
-00-1
Door Synoptic Display
C
1
0
-11-1
Main Entry Doors or Slide/Rafts
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1)
Passenger
A
-
-
(M)(O) One door or slide/raft may be inoperative or slide/raft missing provided:
a)
All other passenger entry doors are fully operational,
b)
Affected door is not used for passenger loading,
c)
A conspicuous barrier strap or rope and a placard stating that the door is inoperative shall be placed across the inoperative door,
d)
Emergency exit sign and floor proximity lights associated with the inoperative exit must be covered to obscure the sign and lights,
e)
Passengers must be advised to not use affected door,
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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:
52-2
1. 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM &
SEQUENCE
NUMBERS
ITEM
4. REMARKS OR EXCEPTIONS
52 DOORS
-11-1
Main Entry Doors or Slide/Rafts (Cont’d)
|
1)
Passenger (cont’d)
f)
All passenger seats halfway to the next exit in each direction from the inoperative door or slide/raft, across the entire width of the airplane, shall be blocked off with conspicuous tapes or ropes that contrast with the airplane interior before loading passengers. Only the seats in these areas shall be blocked; main passenger aisles, cross aisles and exit areas must not be blocked. (For an inoperative forward door or side/raft, the blocked seating area shall extend from the forward cabin end, rearward to a line halfway between the inoperative forward door and the next set of doors aft of the inoperative one. For an inoperative rear door or slide/raft, the blocked seating area shall extend forward from the aft cabin end to a line halfway between the inoperative door and the next set of doors forward of the inoperative one),
g)
Conspicuous signs and placards shall be placed in appropriate locations to indicate seats are not to be occupied by passengers,
h)
Seated capacity must not exceed rated capacity of remaining pairs of exits,
i)
For extended overwater operations, occupancy shall not exceed the normal rated capacity of the slide/rafts, or the remaining slide/rafts, or the rated overload capacity of the slide/rafts remaining after loss of one additional slide/raft of greatest capacity, whichever is least,
(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:
52-3
1. 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM &
SEQUENCE
NUMBERS
ITEM
4. REMARKS OR EXCEPTIONS
52 DOORS
-11-1
Main Entry Doors or Slide/Rafts (Cont’d)
|
1)
Passenger (Cont’d)
j)
Blocked seating layouts and evacuation procedures must be developed and approved by the FAA certificate holding office for inclusion in the operator’s manual, and
k)
Repairs are made within one flight day.
NOTE 1: Flight attendants may be stationed in the vicinity of each door within blocked areas.
NOTE 2: Weight and Balance Manifest must be revised as necessary to ensure proper loading limits are observed.
NOTE 3: A door with an inoperative EPAS must be considered inoperative.
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2)
777F
C
2
1
One door or slide/raft may be inoperative or slide/raft missing.
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-11-2
Main Entry Doors Pressure Stop Assemblies
C
-
-
(M)(O) One forward or aft stop per door (total of 8 stops per –200 airplane, or 10 stops per –300 airplane, or 2 stops per 777F) may be missing or inoperative provided:
a)
There are no visible defects on remaining stops for the affected door(s),
b)
Both cabin altitude auto controllers operate normally,
c)
For inoperative or missing pressure stops 1, 2, 7 and 8, limit maximum cabin differential pressure to 2.5 psi, and
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