737NG垂尾升降舵皮托管渗漏测试笔记

机务大神 · 发表于 2022-5-27 18:12:50

AMM27-31-17-790-801

DO NOT INCREASE THE PRESSURE TO MORE THAN 5 PSIG (34.5 KPA) (437 KNOTS
OF COMPUTED AIRSPEED (KCAS)), DURING THE TEST. IF THE PRESSURE IS MORE
THAN 5 PSIG (34.5 KPA) (437 KCAS), IT CAN CAUSE DAMAGE TO THE ELEVATOR
FEEL COMPUTER.
不要将压力增加到超过5psig (34.5 kpa)(437节
计算空速(kcas))。如果压力更大
超过5 psig (34.5 kpa) (437 kcas)，可对电梯造成损坏
感觉压差计算机

0.9正负0.07 下降0.2 2min
4.8正负0.1 下降0.3 2min