300/350 Limits Flashcards
0
Q
Vmca flaps down
A
- 350
86. 98
1
Q
Min for reverse
A
- 350
40. 40
2
Q
Vmca. flaps up
A
- 350
92. 101
3
Q
V SSE
A
- 350
115. 135
4
Q
V yse
A
- 350
122. 135
5
Q
Vx
A
- 350
122 135
6
Q
Maximum Glide Range
A
- 350
134 135
7
Q
Vy
A
- 350
137. 135
8
Q
Minimum in sustained Icing flight
A
- 350
140. 140
9
Q
VLO. (Retraction)
A
- 350
163. 164
10
Q
Vb. (Turbulence penetration)
A
- 350
170. 170
11
Q
Va (flaps up)
A
- 350
181. 182
12
Q
Vlo. Extension
A
- 350
181. 182
13
Q
Vfe (approach)
A
- 350
200. 202
14
Q
Max Windshield Deicing
A
- 350
226. 226
15
Q
Vmo (below 24000 ft)
A
- 350
259. 245
16
Q
Mmo
A
- 350
.58. .58
17
Q
Torque Limits
A
0-100 Norm op range
- Max transient (20 sec)
- Max TQ Abv 1700
- Transient 7 minutes (350)
18
Q
Turbine Tach (N1) speed limits
A
- Min low idle
- Max
- Max transient
19
Q
ITT Limits
A
- Max low idle
- Max reverse
- Rec Cruise climb
- Max Cruise
- Transient. (20 sec)
- Max transient starting
20
Q
Oil temp limits
A
-40 to. 110. Starting, low idle 0 to. 99 Normal 110. Maximum 99. To. 110. Max transient (10 min) 55. Rec for fuel heater op
21
Q
Oil PSI limits
A
- Minimum low idle
60-90. Caution range
90-136. Normal operating
200 Max starting
22
Q
Pneumatic pressure limits
A
12-20 psi. Normal Op range
20 psi. Max
23
Q
DC Power limits
A
75 Pct. Max (62 - 70 n1)
100 Pct. Max (< 34000)
95 Pct. Max (> 34000)
27.5-29. Norm VDC
24
Props (N2 RPM) limits
```
1050. Minimum idle
1450-1700. Normal Op range
1650. Max Reverse
1700. Max
1870. Transient
400-1050. Avoid during ground op
```
25
Weight Limits
300. 350.
```
15100 16600. Max ramp weight
15000. 16400. Max TO weight
14000. 15675. Max Land weight
11500. 13000. Max zero fuel
550 lbs Max baggage compmnt wt.
one person Max on airstair door
```
26
Rudder boost
Must be operative for all flights
27
Yaw damp system
18500 (300). 19000 (350) Max alt inop (Dual strakes)
| Greater than or above must be on except for takeoff and landing
Check REL
28
Brake Deice limitations
Don't use:
1 Above. 15 degrees C
2 More than 10 min w/wheels
retracted
29
Fuel system limits
```
300 lbs maximum imbalance
265 lbs Min each main for takeoff
10 hrs Max with fuel pressure light
539 (300) 775 (ER) gal Max usable
Fuel quantity.
If fuel in Aux.'s mains must be full
(Main and aux full before filling
```
30
Gear cycle limits
1. 6 cycles at one cycle every 5 min
| 2. 15 minutes rest after 6 cycles
31
Starter limitations
30 seconds on 5 min off
30 seconds on 5 min off
30 seconds on 30 min
32
Prop deice ammeter limits
26-32 amps normal range
33
Cabin altimeter and differential limits
0. - 6.6 PSI