1
Q
Maximum Ramp Weight
A
29300 lbs 13290 kg
2
Q
Maximum Takeoff Weight
A
29000 lbs 13154 kg (12930 AEG)
3
Q
Maximum Landing Weight
A
28500 lbs 12927 kg (12340 AEG)
4
Q
Maximum Zero Fuel Weight
A
26500 lbs 12020 kg (11660 AEG)
5
Q
Vmo up to FL160
A
250 KIAS
6
Q
Vmo FL250
A
210 KIAS
7
Q
Vleo
A
200 KIAS
8
Q
Vle
A
200 KIAS
9
Q
Vlor
A
150 KIAS
10
Q
Vra
A
190 KIAS (up to FL210)
11
Q
Va
A
180 KIAS
12
Q
Vfe 7 or 15 deg
A
175 KIAS
13
Q
Vfe 20 deg
A
165 KIAS
14
Q
Vfe 35 deg
A
140 KIAS
15
Q
Vmcl Flaps 20 or 35
A
106 KIAS
16
Q
Maximum Operating Altitude
A
25,000 ft
17
Q
A
18
Q
Maximum T.O. and landing altitude
A
8,000 ft
19
Q
Minimum T.O and landing altitude
A
-1,000 ft
20
Q
Maximum OAT T.O.
A
47 deg C
21
Q
Maximum OAT T.O (8000 ft PA)
A
33 deg C
22
Q
Minimum OAT T.O.
A
-55 deg C
23
Q
Runway Slope Takeoff
A
-2% - +1,5%
24
Q
Runway Slope Landing
A
-2% - +2%
25
Maximum Load Limit Flaps UP
+2,75G - -1,0Gg
26
Maximum Load Limit Flaps DOWN
+2,0 - 0G
27
Maximum Tailwind Component
10 Knots
28
Total Useable Fuel
5690 lbs 2500 kg
29
Maximum Fuel Imbalance
200 lbs 100 kg
30
Maximum Refuelling Pressure
50 psi
31
Windshield Wiper LOW Mode
130 KIAS
32
Windshield Wiper HIGH mode
160 KIAS
33
DC Generator Maximum Load
600 amps up to 5 minutes
34
DC Generator Nominal Load
400 amps
35
External Power Maximum Voltage
29,5 VDC
36
External Power Maximum Current
1600 amps for engine start
37
External Power Minimum Current
1200 amps for engine start
38
Main Battery NO BAT Start
57 deg C
39
Main Battery No cross GEN start
61 deg C
40
Main Battery maximum temp for Take-off
64 deg C
41
BAT HOT
71 deg C
42
Main Battery minimum temp for Take-Off
-20 deg C
43
Main Battery minimum temp for eng start
-20 deg C
44
Maximum ITT
940 deg C 5 minutes 950 deg C2 minutes
45
Maximum ITT Transient
965 deg C
46
Maximum ITT Engine Start
965 deg C
Saab 340
flashcards
Decks in class (2)
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