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ENGINE FUEL AND CONTROL - ENGINE CONTROL - TRAINING INFORMATION POINT - EEC BITE - EEC TEST 3
EFFECTIVITY
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ENGINE FUEL AND CONTROL - ENGINE CONTROL - TRAINING INFORMATION POINT - EEC BITE - EEC TEST 3
ENGINE FUEL AND CONTROL - ENGINE CONTROL - TRAINING INFORMATION POINT - EEC BITE - EEC TEST 3
EFFECTIVITY
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General
The T/R LEVER INTLK TEST does a test to make sure the EEC
can operate the thrust lever interlock.
NOTE: The CDU screen will show a warning about operation of
the thrust reverser during this test.
You select START TEST on the GROUND TEST T/R LEVER
INTLK TEST page and follow the procedure in 73-21 of the AMM
part II and the steps on the CDU to do the test.
The T/R LEVER INTLK TEST first does a test of channel A then
repeats the test for channel B. When the tests are complete, you
select TEST RESULTS. The EEC shows the faults that were
found or shows the TEST PASSED message. You next select
END TEST or REPEAT TEST. If you select END TEST, the TEST
COMPLETE page shows on the CDU. If one channel of the EEC
does not operate, the TEST COMPLETE page tells you which
channel does not operate.
If you select abort during the test, the test stops and the CDU
shows the test abort page.
ENGINE FUEL AND CONTROL - ENGINE CONTROL - TRAINING INFORMATION POINT - EEC BITE - T/R INTLK 1
EFFECTIVITY
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ENGINE FUEL AND CONTROL - ENGINE CONTROL - TRAINING INFORMATION POINT - EEC BITE - T/R INTLK 1
ENGINE FUEL AND CONTROL - ENGINE CONTROL - TRAINING INFORMATION POINT - EEC BITE - T/R INTLK 1
EFFECTIVITY
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73-21-00-217
General
These are additional CDU screens for the T/R LEVER INTLK
TEST.
ENGINE FUEL AND CONTROL - ENGINE CONTROL - TRAINING INFORMATION POINT - EEC BITE - T/R INTLK 2
EFFECTIVITY
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73-21-00-219
ENGINE FUEL AND CONTROL - ENGINE CONTROL - TRAINING INFORMATION POINT - EEC BITE - T/R INTLK 2
ENGINE FUEL AND CONTROL - ENGINE CONTROL - TRAINING INFORMATION POINT - EEC BITE - T/R INTLK 2
EFFECTIVITY
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CFM56 ENGINES (CFM56-7) 737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
73-21-00-219
General
Here are additional CDU screens for the T/R LEVER INTLK
TEST.
ENGINE FUEL AND CONTROL - ENGINE CONTROL - TRAINING INFORMATION POINT - EEC BITE - T/R INTLK 3
EFFECTIVITY
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73-21-00-221
ENGINE FUEL AND CONTROL - ENGINE CONTROL - TRAINING INFORMATION POINT - EEC BITE - T/R INTLK 3
ENGINE FUEL AND CONTROL - ENGINE CONTROL - TRAINING INFORMATION POINT - EEC BITE - T/R INTLK 3
EFFECTIVITY
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CFM56 ENGINES (CFM56-7) 737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
73-21-00-221
General
The ACTUATOR TEST operates engine actuators to their
minimum and maximum positions with each EEC channel.
NOTE: The CDU screen will show a warning about operation of
the engine during this test.
You select START TEST on the GROUND TEST ACTUATOR
TEST page and follow the procedure in 71-00 of the AMM part II
and the steps on the CDU to do the test.
The ACTUATOR TEST first does a test of channel A then repeats
　
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