通航信息_通航_通用航空_General Aviation

ADAA
Validity : S / N 1 - 9999 76 TC (EA) Page 2 OCT 02
 
ENGINE CONTROLS
DESCRIPTION AND OPERATION
1. GENERAL
Engine operation is regulated by several controls located in the cabin on the central pedestal.
The engine control assembly includes :
- power controls - refer to 76-10-00,
- propeller control - refer to 61-20-00.
ABAA
Validity : S / N 1 - 9999
76-00-00 age 1
-00-00
(CA) OCTO 02
 
PAGE INTENTIONALLY LEFT BLANK
ABAA
Validity : S / N 1 - 9999 76-00-00Page 2
(CA) OCT 02
 
POWER CONTROLS
DESCRIPTION AND OPERATION
1. GENERAL
The power control assembly includes :
- throttle control,
- mixture control,
- Alternate Air control,
- pedestal controls.
Each control is actuated using a linkage and sheathed cable device.
2. LOCATION (Figures 1 and 1A)

COMPONENT QTY AREA ACCESS DOOR REFERENCE
Throttle control 1 100 & 250 / 76-10-01
Mixture control 1 100 & 250 / 76-10-03
Pedestal controls / 250 / 76-10-04
Alternate Air control 1 100 & 250 / 76-10-05

3. DESCRIPTION
A. Throttle control
　
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本文链接地址：TB20 MAINTENANCE MANUAL 76 发动机控制 TB20飞机维护手册(2)