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钻石20飞机飞行手册 DA 20 Airplane Flight Manual(79)

时间:2011-10-28 13:14来源:蓝天飞行翻译 作者:admin
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9.  
Trim DOWN Light – Illuminates to indicate the need for nose DOWN trim.  When both lights are out, the aircraft is in trim longitudinally.

10.  
Blue (ALT) light illuminates when altitude mode is engaged.

11.  
Flag Window – Red flag visible indicates lack of electrical power to primary turn coordinator unit.

12.  
Autopilot Master ON-OFF Switch – Refer to pre-flight procedures for operating details.

13.  
Remote AP disconnect switch.

14.  
GPSS Heading Switch / Annunciator. Works in conjunction with “HDG” mode. When the GPSS is activated the GPSS converter changes ARINC 429 steering data received from the GPS to heading signals.

 


Figure 1

8. HANDLING, PREVENTATIVE AND CORRECTIVE MAINTENANCE
There is no change in handling, preventative or corrective maintenance with the installation of S-TEC System 30 autopilot (Mod No. 30).

CHAPTER 9

SUPPLEMENT 6
VM1000 Monitoring System

1.
GENERAL ................................................................................................................... S6-2


2.
OPERATING LIMITATIONS ....................................................................................... S6-2


3.
EMERGENCY PROCEDURES................................................................................... S6-2


4.
NORMAL PROCEDURES .......................................................................................... S6-4


5.
PERFORMANCE ........................................................................................................ S6-4


6.
WEIGHT AND BALANCE ........................................................................................... S6-4


7.
DESCRIPTION OF THE AIRPLANE AND ITS SYSTEMS ......................................... S6-4


8.
HANDLING, PREVENTATIVE AND CORRECTIVE MAINTENANCE........................ S6-7

 


1. GENERAL
This supplement addresses the optional installation of the Vision Microsystems VM1000 engine instrument package (Mod 31). Only portions of the flight manual affected by the installation are included in this supplement.
2. OPERATING LIMITATIONS
2.1. Placards
1. Under the buttons of the VM 1000 main display.

3. EMERGENCY PROCEDURES
3.3. Emergency Procedures Checklist
3.3.1. Engine Failures
A. VM 1000 and EC 100 Display Malfunction
1. Instrument Circuit Breaker  PRESS IN or PULL and RESET

NOTE

If indication cannot be restored take care not to shock cool the engine during a descent. Electrical system voltage can be monitored on M803 Clock / OAT / Volt Meter if installed.
4.
Airspeed  Do not exceed 115 KIAS

5.
 
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