• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-04-01 08:47来源:蓝天飞行翻译 作者:航空
曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 22-31-00
 ALL  ú ú 04 Page 515 ú Nov 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
 (f)
(g)
A
737-300/400/500MAINTENANCE MANUAL
 NOTE:____ 737-500 AND SOME 737-300 AND 737-400 AIRPLANES
 WITH P/N 10-62017-21 AND ON A/T COMPUTERS;
 Line 9 on the CDU will show "START 1,2 ON/OFF"
 and line 11 is not shown.
 f)  Make sure that CDU shows START 1,2 OR ANTI-ICE 1,2 OFF.
 g)  Set the No. 1 ENGINE START switch to FLT.
 h)  AIRPLANES WITHOUT SB 77-1031;
 Make sure that CDU shows START 1,2 OR ANTI-ICE 1,2 ON.
 i)  AIRPLANES WITH SB 77-1031;
 Make sure that CDU shows START 1,2 OR ANTI-ICE 1,2 OFF.
 j)  Set the No. 1 ENGINE START switch to OFF.
 k)  Make sure that CDU shows START 1,2 OR ANTI-ICE 1,2 OFF.
 l)  Do the test again with No. 2 ENGINE START switch.

AIRPLANES WITH A/T COMPUTER P/N 10-62017-1 THRU P/N 10-62017-5;
 Push the NEXT PAGE key on CDU.
 1) Make sure Input Discretes page 4/4 is shown on the CDU.
 2) ENG(ine) CONFIG(uration) - CFM56-XXXX

 a)  Make sure the engine configuration on the CDU shows the correct engines installed on the airplane.
 NOTE: The CDU will show ENG CONFIG INVALID if the
____ program pins for the engines installed on the airplane are not connected correctly.
 3)  F/S BIAS - FAST a) Make sure that CDU shows F/S BIAS FAST.
 4)  AIRPLANES WITH A/T COMPUTER P/N 10-62017-4 AND SUBSEQUENT WHICH HAVE THE OPTION PIN 25 ON THE CONNECTOR D1647A GROUNDED; Do the F/S OPTION - ENABLED/DISABLED
 NOTE: The F/S OPTION-ENABLED/DISABLED does not apply to
____ A/T computer P/N 10-62017-4.
 a)  Make sure the F/S OPTION ENABLED or F/S OPTION DISABLED shown on the CDU agrees with the Fast/Slow option you use on the airplane.
 5)  737-300 AIRPLANES ONLY; MIN SPEED - FAA/CAA a) Make sure that MIN SPEED FAA or MIN SPEED CAA display
 agrees with the wiring configuration on the airplane.AIRPLANES WITH A/T COMPUTER P/N 10-62017-11 AND SUBSEQUENT; Push the NEXT PAGE key on the CDU. 1) Make sure the CDU shows Input Discretes page 4/6. 2) TORQUE SW1 - CLOSED/OPEN
 a) Set the two throttle levers to mid-range and release.
 b) Push the No. 1 throttle lever forward.
 c) Make sure that CDU shows TORQUE SW1 OPEN.
 d) Release the No. 1 throttle lever.

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 22-31-00
 ALL  ú ú 01 Page 516 ú Nov 12/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 e) Make sure that CDU shows TORQUE SW1 CLOSED.
 3)  TORQUE SW2 - CLOSED/OPEN a) Set the two throttle levers to mid-range and release. b) Push the No. 2 throttle lever forward. c) Make sure that CDU shows TORQUE SW2 OPEN. d) Release the No. 2 throttle lever. e) Make sure that CDU shows TORQUE SW2 CLOSED.
 CAUTION: DO NOT TRY TO OPERATE THE THRUST REVERSERS.
_______
 4) THR(ust) REV(erser) 1 - OFF a) Make sure that CDU shows THR REV 1 OFF. 5) THR(ust) REV(erser) 2 - OFF a) Make sure that CDU shows THR REV 2 OFF.
 (h)  AIRPLANES WITH A/T COMPUTER P/N 10-62017-11 AND SUBSEQUENT; Push the NEXT PAGE key on the CDU 1) Make sure the CDU shows Input Discretes page 5/6. 2) DADC L - VALID/INVALID
 a)  Open the No. 1 AIR DATA COMPUTER - AC circuit breaker
 on P18 Panel. b) Make sure that CDU shows DADC L INVALID. c) Close the No. 1 AIR DATA COMPUTER - AC circuit breaker
 on P18 Panel. d) Make sure that CDU shows DADC L VALID.
 3)  LRRA L - VALID/INVALID a) Open the RADIO ALTM-1 circuit breaker on P18 Panel. b) Make sure that CDU shows LRRA L INVALID. c) Close the RADIO ALTM-1 circuit breaker on P18 Panel. d) Make sure that CDU shows LRRA L VALID.
 4)  F/S OPTION - ENABLED/DISABLED
 a)  Make sure that F/S OPTION ENABLED or F/S OPTION DISABLED on the CDU agrees with Fast/Slow option pin which is connected on airplane.
 5)  MIN SPEED - FAA/CAA (On 737-300 Only) a) Make sure the MIN SPEED FAA or MIN SPEED CAA display agrees with the wiring configuration on the airplane.
 
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:737-300 400 500 AMM 飞机维护手册 自动飞行 AUTOFLIGHT 2(160)