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 Advisory Callouts inoperative:
A. The Flight Crew shall adopt Callouts for Radio ALtimeter Readings 2500’, 100’, 50’, 30’, and 10’ to compensate the lack of Advisory Callouts by GPWS.
 Windshear Mode inoperative:
A. The Flight Crew shall keep up close monitoring of Airspeed and Vertical Speed for deviations that indicate wind shear during takeoff, approach and landing.
 

NUMBER INSTALLED
2 NUMBER REQUIRED FOR DISPATCH
REMARKS OR EXCEPTIONS
1 One may be inoperative.

 
EICAS STATUS MESSAGES
None
PLACARD
As appropriate
 
 
B757 - 200 MINIMUM EQUIPMENT LIST

 

NUMBER INSTALLED
2
2 NUMBER REQUIRED FOR DISPATCH
REMARKS OR EXCEPTIONS
1 One ATC transponder and/or Automatic Altitude Reporting Function may be inoperative.
0 May be inoperative provided ATC authorization
is granted for routes where ATC Transponder and/or Automatic Altitude Reporting is
required.
2 1 Either one must be operative for RVSM operations.
 
EICAS STATUS MESSAGES
None
PLACARD
As appropriate
 
EICAS STATUS MESSAGES
None
PLACARD
As appropriate
 
NUMBER INSTALLED

 NUMBER REQUIRED FOR DISPATCH
REMARKS OR EXCEPTIONS
2 0 May be inoperative provided navigation and/or
approach procedures do not require its use.

 
EICAS STATUS MESSAGES
None
PLACARD
As appropriate
 

NUMBER INSTALLED
- NUMBER REQUIRED FOR DISPATCH
REMARKS OR EXCEPTIONS
0 (O) May be inoperative provided alternate procedures according to Operational Procedures are used.

 
NOTE: The Global Positioning System function may be implemented by using either a dedicated GPS receiver or a GPS module within the Mult-Mode Receiver (MMR). This MEL item is intended to provide relief for the GPS function, regardless of how the function is implemented.
EICAS STATUS MESSAGES
None
PLACARD
As appropriate
OPERATIONS (O)
The Flight Crew shall verify that ANP is equal or greater than RNP along the route with remaining navigational aids and that FMC is not using GPS Signals for navigational guidance.
 
REPAIR INTERVAL

ITEM
34-61-1 Flight Management
Computer Systems (FMCS) (Including MCDU)
 Navigation Databases
 FMC Annunciator Light C
C
C
C
C
 

 
NOTE: For those airplanes with the advanced stall warning computer and speed tape display, dispatch with a "WARN ELEX" status message is allowed provided the P51 WEU BITE module displays only fault code D7 (FMC invalid). This should be checked prior to each departure. For those airplanes that do not have both the advanced stall warning computer and speed tape display, dispatch is not allowed with a "WARN ELEX" status message.
　
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