B. Ground Tests
(1)
Ground tests provide a means of verifying and amplifying on flight faults to aid in fault isolation. Ground test also provide fault indications when no flight faults were recorded.
(a)
Tests 01 thru 16 are LRU tests oriented towards specific components.
(b)
Tests 30 and 40 are system tests involving the entire autoflight system.
(c)
Tests 51 thru 69 are supporting tests oriented towards specific function involving several components.
(2)
01 FCC (Left, Right, and Center)
(a) Displays any FCC self-test faults and FCC interface faults from the associated system interfaces.
(3)
02 TMC
(a) Displays any TMC self-test faults and TMC interface faults from associated system interfaces.
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(4) 04 MCP
(a) Displays any FCC and TMC self-test faults. Displays FCC and TMC interface faults related to MCP.
NOTE: In later MCP test steps failure of FCC L and FCC C, or
____ FCC R will cause half lighting of lower half of MCP switch/light indicators. Failure of TMC will prevent EPR and SPD switch/lights from lighting.
(b)
Displays the interaction message for checking the MCP
lightswitches.
(c)
Displays interaction messages for checking the on and off position of the captain's flight director switch.
(d)
Displays interaction messages for checking the arm and off position of the autothrottle ARM switch.
(e)
Displays the interaction message for checking the command function of the indicated airspeed/mach select switch.
(f)
Displays the interaction message for checking the command function of heading select switch.
(g)
Displays the interaction message for checking the ON and OFF positions of the first officer's flight director switch.
(h)
GUN 051; displays interaction messages for checking the engaged and disengaged position of the bat handle switches.
(i)
GUN 001-050, 052-999; displays interaction messages for checking the down and up position of the disengage bar.
(j)
Displays interaction messages for checking the command function for each position of the bank limit switch.
(k)
Displays interaction messages for checking the control function of the indicated airpseed/mach display rotary control.
(l)
Displays interaction messages for checking the control function of heading display rotary control.
(m)
Displays interaction messages for checking the control function of the vertical speed display rotary control.
(n)
Displays interaction messages for checking the control functions of the altitude select display rotary control.
(5)
05 TMSP
(a)
Displays TMC self-test faults.
(b)
Displays TMSP-to-TMC interface faults
(c)
Does a TMSP SW/MODE DISPLY test routine which checks the mode display and command function of continuous, climb, and cruise mode switching. Displays an interactive message at end of the test.
(d)
Does a TMSP TEMP SELECT test with interaction messages to check control function of temperature select control display.
(6)
06 ASA
(a)
Displays any FCC self-test faults.
(b)
Displays FCC interface faults related to ASA.
(c)
Checks all ASA displays and their reset function.
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本文链接地址：757 AMM 飞机维护手册 自动飞行 AUTOFLIGHT 1(27)
