(7)
Close the core cowl panels (AMM 71-11-06/201). S 415-156-N00
(8)
Close the fan cowl panels (AMM 71-11-04/201). S 445-157-N00
(9)
Do the activation procedure for the thrust reversers (AMM 78-31-00/201).
S 975-090-N00 CAUTION: TO PREVENT ERRORS WHEN YOU USE THE CHECKOUT TARGET, DO NOT USE
_______ THE AIRPLANE INDICATION OF THE TOTAL AIR TEMPERATURE FOR THE AMBIENT AIR TEMPERATURE. MAKE SURE TO GET THE LOCAL BAROMETRIC PRESSURE (NOT CORRECTED TO SEA LEVEL) FROM THE CONTROL TOWER.
DO NOT USE A MERCURY THERMOMETER ON THE AIRPLANE. IF THE THERMOMETER BREAKS, THE MERCURY CAN CAUSE DAMAGE TO EQUIPMENT.
(10)
Find the ambient air temperature [outside air temperature (OAT)] with the thermometer.
S 975-091-N00
(11)
Make a record of the barometric pressure, OAT and specific humidity.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
71-00-00
ALL ú ú N04 Page 551 ú Oct 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / PW4000 SERIES /747-400 / ENGINES/MAINTENANCE MANUAL ////////////////////////
TEST NO. 9 - PERFORMANCE TEST
_____________________________
S 975-022-N00
(12) Find these trim targets from the table for the Engine Checkout target (Ref 71-00-01/201) and write the data:
NOTE: Make sure you write the target values, the tolerances and the
____
permitted ranges (minimum/maximum).
(a)
MIN IDLE (%N2)
(b)
MIN PB (PSIA)
(c)
APP IDLE (%N2)
(d)
N1 @1.25 EPR (%N1)
S 975-024-N00
(13) Find the range (minimum/maximum) of the %N1 INCREASE from the table for the FADEC MODE SELECTION CHECK (Ref Table 502) and write the data.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
71-00-00
ALL ú ú N03 Page 552 ú Jun 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
TEST NO. 9 - PERFORMANCE TEST
_____________________________
~................................................ | TABLE 502 | | FADEC MODE SELECTION CHECK | .................................................. | | N1 INCREASE | | OAT | FROM SETTING TARGET | | ............................... | °F (°C) | MINIMUM | MAXIMUM | ..................................................
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:747-400 AMM 飞机维护手册 动力装置 POWER PLANT 1(68)