1
Q
Aircraft Length
A
46’ 8”
2
Q
Aircraft Wingspan
A
57’ 11”
3
Q
Aircraft Height
A
14’ 4”
4
Q
Max Occupancy
A
17 including crew
5
Q
Engine Type and SHP
A
PT6A-60A 1050 SHP
6
Q
Max Ramp Weight
A
15,100 lbs
7
Q
Max Takeoff Weight
A
15,000 lbs
8
Q
Max Landing Weight
A
15,000 lbs
9
Q
Max ZFW
A
12,500 lbs
10
Q
Max Weight in Baggage Area
A
510 lbs with folding seats
550 lbs without folding seats
11
Q
Vxse and Vyse
A
125 KIAS
12
Q
Vmca
A
94 KIAS flaps UP
93 KIAS flaps Approach
13
Q
Emergency Descent Speed
A
184 KIAS
14
Q
Best Glide Speed
A
135 KIAS
15
Q
Va
A
184 KIAS
16
Q
Vfe Approach
A
202 KIAS
17
Q
Vfe Full
A
158 KIAS
18
Q
Vle
A
184 KIAS
19
Q
Vlo Extension
A
184 KIAS
20
Q
Vlo Retraction
A
166 KIAS
21
Q
Vmo
A
263 KIAS, .58 mach
22
Q
Max Demonstrated Crosswind
A
20 KIAS
23
Q
Vx
A
125 KIAS
24
Q
Vy
A
140 KIAS
25
Turbulent Air Penetration Speed
170 KIAS
26
Vsse
110 KIAS
27
Turning Radius
41’ 7”
28
Hydraulic Fluid Type
MIL-5606
29
Battery
24 volt 34 or 36 amp NiCad
30
Main Tires
10 ply 80-92 psi
31
Nose Tire
8 ply 55-60 psi
32
Vso
81 IAS
33
Vs
96 IAS
34
Max Starting ITT
1000 C for 5 seconds
35
Max Idle ITT
750 C
36
Max Takeoff ITT
820 C
37
Max Continuous ITT
820 C
38
Max Cruise Climb ITT
785 C
39
Max Cruise ITT
820 C
40
Max Reverse ITT
760 C
41
Max Transient ITT
850 C for 20 sec
42
Transient Torque Limit
156% for 20 seconds
43
Min N1 at IDLE
62%
44
Max N1
104%
45
Prop RPM at IDLE
1050 rpm
46
Max Prop RPM
1700 rpm, excursions up to 1735 rpm are acceptable for 7 min
47
Max Reverse RPM
1650 rpm
48
Max Transient Prop RPM
1870 rpm
49
Overspeed Governor RPM
1768 rpm
50
Overspeed Governor RPM
1768 rpm
51
Overspeed Governor RPM
1768 rpm
52
Max Starting Oil Press
200 psi
53
Min oil pressure at IDLE
60 psi
54
Normal Oil Pressure Range
90-135 psi
55
Transient Oil Pressure
200 psi
56
Min Oil TEMP for starting
-40 C
57
Min recommended oil temp for takeoff
55 C
58
Normal oil temp range
0-110 C...temps between 99-110 C are limited to 10 min
59
External power limits
28.0-28.4 volts
| 1000 amps momentarily, 300 amps continuous
60
Generator Limits
SL - 34,000 feet = 100% load
| Above 34,000 feet = 95%
61
Max Generator Load 62-70% N1
75%
62
Max Generator Load 70-100% N1
100%
63
Starter limits
30 seconds ON, 5 min OFF, 30 seconds ON, 5 min off, 30 seconds ON, 30 min OFF
64
Limitations using aviation gasoline
150 hours
Prohibited if either standby fuel pump is inop
Crossfeed capability is required above 20,000 feet
65
Usable Fuel (without saddle tanks)
3611 pounds total
1273 pounds in each main
533 pounds in each aux tank
66
Max fuel imbalance
300 pounds
67
Fuel gages in yellow arc
Do not take off if less than 265 pounds in each wing system
68
Aux tank fueling
Do not put any fuel in the aux tanks unless the mains are full
69
Prop manufacturer & diameter
Hartzell, 105”
70
Prop overspeed limits
Flight may be continued with an overspeed up to 1768 rpm as long as torque is limited to 96%
71
Max cabin pressure differential
0 - 6.6 psi
72
Pneumatic pressure gage range
12 - 20 psi, redline is 20 psi
73
Prop de-ice ammeter range
26 - 32 amps
74
Flight Load Limits
Flaps UP = +3.1, -1.24 g
| Flaps DOWN = +2.0. -0.0 g
75
Max Operating Altitude
35,000 feet
76
Max Operating Altitude with YD inop
Above 5,000 feet without strakes
| Above 19,000 feet with Raisbeck STC SA5151NM
B350 Study Materials
flashcards
Decks in class (3)
# Cards
