1
Q
Va
A
181
2
Q
Vfe approach
A
200
3
Q
Vfe landing
A
157
4
Q
Vlo extension
A
181
5
Q
Vlo retraction
A
163
6
Q
Vle
A
181
7
Q
Vmca (red line)
A
86
8
Q
Vno
A
259
9
Q
Vyse (blue line)
A
121
10
Q
Vxse
A
115
11
Q
Total usable fuel
A
544
12
Q
Each main tank
A
193
13
Q
Each aux tank
A
79
14
Q
Max ramp weight
A
12,590
14,090
15
Q
Max takeoff weight
A
12,500
14,000
16
Q
Max landing weight
A
12,500
13,500
17
Q
Max zero fuel weight
A
11,000 for both
18
Q
Max baggage comp weight
A
550
19
Q
Max altitude
A
35,000
20
Q
Emergency descent
A
181
21
Q
Max glide
A
135
22
Q
Vx
A
100
23
Q
Vy
A
125
24
Q
Turbulent air
A
170
25
Engine
PT6A 850 SHP reverse flow, free turbine, turboprop
26
ITT
Interstage Turbine Temperature
27
Engine oil two functions
1. Cooling
2. Lubricating engine
28
Props
Full feathering, reversing
29
Electrical system
28 volt 250 amp
30
Pitot-Static instrument’s
Airspeed
Altimeter
VSI
31
Vacuum instruments
Attitude indicator
Heading indicator
Turn coordinator
32
Climb Speeds: Sea level to 10,000
160
33
Climb Speed: 10,000 to 20,000
140
34
Climb Speed: 20,000 to 25,000
130
35
Climb Speed: 25,000 to 35,000
120
King Air 200
flashcards
Decks in class (1)
# Cards
