600 ASSEMBLY
SECTION
600 ASSEMBLY
SECTION
Page 29
Problem
状 况
Cause
原因
Solution
对策
Blade
Tracking
双 桨 平衡
Tracking is Off
双桨
Pitch linkage rods are not
even length.
PITCH
连杆长 度 调整不 均 匀.
A
djust
l
ength
o
f
p
itch
l
inkage
r
ods
(
A
) .
调整连杆
(
A
)
长度.
Hover
停 悬
If the problem is still there even after tried above, stop flying and contact with your seller.
在 做完以 上 调整后,仍 然 无法改 善 情况 时 ，应立 即 停止飞 行 并联络 你 的经销 商 。
Headspeed too
low or high.
主 旋翼转 速 偏低
或者偏 高.
Excessive pitch high or low.
主旋 翼的
PITCH
偏高 或 过低.
Adjust pitch linkAge rods(A) to reduce
pitch by 4 to 5 degrees.Hovering
headspeed should be around 1900RPM.
调整 连杆
(
A
)
调低
Pitch
约+
4～5
度
(
停悬时 主 旋翼需 为 约
190 0 RPM
).
Hovering Throttle curve is
too low or high.
停 悬 点油门 曲 线过低 或 过高.
Increase throttle curve at hovering
point on transmitter(around 65%).
调 停 悬点油 门 曲线
(
约
65%
).
Oscillation
during
flight
飞行 抖 动
Helicopter Oscillation.
机身 抖 动.
Main shaft instal no vertical,
Main shaft bear mount screws
need to Cross tighten.
主轴安装不垂直,主轴轴承座螺
丝需要交叉拧紧.
Please refer to page 15.
15
页
请参照说明注第
.
Foward/aft oscillation
when elevator is applied.
升 降舵打 舵 动作时,机 体
前后 抖 动.
Helicopter front bobbles
(nods) during foward flight.
直线飞行时,机头点头.
Elevator gyro gain too high.
升 降舵陀 螺 感度偏 高,产生
追 踪现象.
Turn the ELE gaina dial on 3GX
counterclockwise,10degrees at a time
until oscillation is eliminated.
逆时针调 整
3GX
上的升 降舵感 度调整旋钮,
以每次调整 约
10
度方 式,调整 至适 当 位置
.
Worn servo,or slack in control
links.
伺服器老化控制结构有虚位.
Replace servo,ball link,or linkage balls.
更换伺服器,连杆头,球头.
Left/right oscillation when
aileron is applied.
副翼打舵动作时,机体左右
抖动.
Elevator input causes
helicopter to drift
.
升降舵动作漂移.
Aileron gyro gain too high.
副翼陀螺感度偏高产生追踪
现象.
Turn the AIL gain dial on 3GX
counterclockwise,10degrees at a time
until oscillation is eliminated.
逆时针调 整
3GX
上 的副翼 感度调整 旋钮,
以每次 调整约
1 0
度方 式,调 整至适当位 置
.
Helicopter head up during
fast flight.
快速飞行时直升机机头
会上扬.
Helicopter
Head Up
直升机 机
头会上 扬
Gyro pitch gain too low.
俯仰
(
Pitch
)
感度不足.
Increase the pitch gain.
请调高俯仰
(Pitch
)感度.
Elevator trim not centered.
十字盘升降舵中立点不对.
Check if helicopter is tilting backwards
during hover.
请测试悬停时,直升机中立点是否朝后.
Rudder
Response
尾 舵 反应
Drifting of tall occurs during
hovering, or delay of rudder
response when centering
rudder stick.
停悬时尾翼向某一边偏移,
或拨动方向舵并回复到中
立点时,尾翼产生延迟,无
法停顿在所控制位置上.
Rudder neutral
pointimproperly set.
尾中立点设定不当.
Rudder gyro gain too low.
尾舵陀螺仪感度偏低.
Reset rudder neutral point.
重设尾中立点.
Increase rudder gyro gain.
增加尾舵陀螺仪感度.
Tail oscillates
(hunting,or wags)at hover
or full throttle.
停悬或全油门时尾翼左右
来回摇摆.
Rudder gyro gain too high.
尾舵陀螺仪感度偏高.
Reduce rudder gyro gain.
降低尾舵陀螺仪感度.
