A
757
MAINTENANCE MANUAL
(b)
Set the rudder pedal to the position as shown in the table that follows:
(c)
Make sure the tester display shows the correct value as listed in the table.
~..................................................... | TEST | POSITION | TESTER DISPLAY | ....................................................... | RUDDER | LEFT FULLY FORWARD | 0367 to 0655 | | PEDAL .......................................... | | RIGHT FULLY FORWARD | 7140 to 7401 | 2............….....................…..................1
(d)
Set the rudder position back to the neutral position.
Z. Flap Handle Position Test
S 735-755-002
(1) Do the flap handle test that follows:
(a)
Make sure these circuit breakers on the overhead circuit breaker panel, P11, are close: 1) 11G12, FLAP/SLAT ELEC UNIT-1 PWR 2) 11G13, FLAP/SLAT ELEC UNIT-1 CONT 3) 11G14, FLAP/SLAT ELEC UNIT-1 SENSOR
(b)
On the tester, set the SUBFRAME to 3 and the WORD to 14.
(c)
Set the flap handle position, and make sure the tester display shows the value as shown in the table that follows:
~............................................. | FLAP HANDLE POSITION | TESTER DISPLAY | ............................................... | UP | 0000 to 2211 | ............................................... | 15 | 4426 to 5156 | 2........................…....................1
GUN 001-008, 010, 101 POST-EO B531006; ú 31-31-00
GUN 051, 102-999 ú CONFIG 2 ú 06 Page 523 ú May 28/02
A
757
MAINTENANCE MANUAL
(d) Set the flap handle to the UP position.
S 735-746-002
(2) Leading Edge Slat Position Test
(a)
Make sure the leading edge slat system is operational
(AMM 27-81-00).
(b)
Set the SUBFRAME and WORD for each parameter condition as shown in the table that follows.
(c)
Make sure the tester display shows the correct data for each postion.
~................................................................ | | TESTER SETUP | TESTER DISPLAY | | L.E. SLATS/CONDITION ........................................... | | SUBFRAME | WORD |BIT (DISCRETE)| VALUE | .................................................................. | FULL EXTEND | 0 | 03 | 1 | 1 | .................................................................. | NOT FULLY EXTEND | | | | 0 | .................................................................. | PART EXTEND | 0 | 11 | 1 | 1 | .................................................................. | NOT PART EXTEND | | | | 0 | .................................................................. | RETRACTED | 0 | 19 | 1 | 1 | .................................................................. | NOT RETRACTED | | | | 0 | .................................................................. | FAIL *[1] | 0 | 27 | 1 | 1 | .................................................................. | NOT FAIL | | | | 0 | 2......................…..........….......…..............….......1 *[1] Uncommanded motion (UCM) or Asymmetry. Refer to 27-81-00 to make the slat condition of the UCM. To created the UCM
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：757 AMM 飞机维护手册 仪表 CHAPTER 31 - INSTRUMENTS 1(92)
