Limits Flashcards
(62 cards)
1
Q
Torque Limitations
Normal Operating Range-
A
20-100
2
Q
Torque Limitations
Maximum-
A
100
3
Q
Torque Limitations Max Transient (\_\_ secs)-
A
123 for 5 seconds
4
Q
Torque Limitations
Max w/Prop > 2000 RPM-
A
81
5
Q
Torque Limitations
Max w/Prop < 1600 RPM-
A
49
6
Q
Torque Limitations
Max w/Oil Press < 85 PSI-
A
49
7
Q
Propeller Tachometer (N2) RPM Normal Operating Range-
A
1600-2000
8
Q
Propeller Tachometer (N2) RPM Maximum-
A
2000
9
Q
Propeller Tachometer (N2) RPM Max Transient (\_\_ Secs)-
A
2200 for 5 seconds
10
Q
Propeller Tachometer (N2) RPM Max Reverse (\_\_ min)-
A
1900 for 1 minute
11
Q
Turbine Gas Temperature (TGT) -C
Normal Operating Range-
A
400-800 Celsius
12
Q
Turbine Gas Temperature (TGT) -C
Takeoff and Max Continuous-
A
800 Celsius
13
Q
Turbine Gas Temperature (TGT) -C
Normal Climb/ Cruise-
A
770 Celsius
14
Q
Turbine Gas Temperature (TGT) -C Max Reverse (\_\_\_ Minute)-
A
750 for 1 minute
15
Q
Turbine Gas Temperature (TGT) -C Max Start (\_\_\_ Secs)-
A
1000 Celsius 5 seconds
16
Q
Turbine Gas Temperature (TGT) -C
Max LO Idle-
A
750 Celsius
17
Q
Turbine Tachometer (N1) Speed Takeoff and Max continuous-
A
101.5
18
Q
Turbine Tachometer (N1) Speed Transient (\_\_ Secs)-
A
102.6 for 10 seconds
19
Q
Turbine Tachometer (N1) Speed Max Below -48 Celsius-
A
100.1
20
Q
Turbine Tachometer (N1) Speed LO Idle ( Minimum)
A
56
21
Q
Oil Pressure PSI
Normal below 21,000 feet-
A
100-135
22
Q
Oil Pressure PSI
Caution below 21,000 feet
A
85-100
23
Q
Oil Pressure PSI
Normal Above 21,000 feet
A
85-135
24
Q
Oil Pressure PSI Low Idle (MIN)
A
60
25
Oil Temperature Celsius
| Takeoff and Max Continuous-
0 to 99
26
Oil Temperature Celsius
| Starting-
-40
27
Oil Temperature Celsius
| Low Idle-
-40 to 99
28
Oil Temperature Celsius
| Transient (___ Secs)
99 to 104 for 5 seconds
29
```
Pneumatic Pressure (PSI)
Normal Operating Range-
```
12-20
30
```
Pneumatic Pressure (PSI)
Max-
```
20
31
Starter Limitations-
40 seconds on, 60 seconds off
40 seconds on, 60 seconds off
40 seconds on, then 30 minutes off
32
```
Airspeed Limitations (KIAS)
(Vmo)-
```
Max Allowable- 260
33
```
Airspeed Limitations (KIAS)
(Va)-
```
Max Design Maneuvering- 181
34
```
Airspeed Limitations (KIAS)
(Vb)-
```
Turbulence Penetration- 170
35
```
Airspeed Limitations (KIAS)
(Vf)-
```
Max (flaps APPCH)- 199
36
```
Airspeed Limitations (KIAS)
(Vfe)-
```
Max (flaps FULL)- 157
37
```
Airspeed Limitations (KIAS)
(Vmc)-
```
Min Single Engine Control- 86
38
```
Airspeed Limitations (KIAS)
(Vyse)-
```
Best rate of climb S/E @ 12,500lbs- 121
39
```
Airspeed Limitations (KIAS)
minimum airspeed for sustained icing conditions-
```
140
40
```
Airspeed Limitations (KIAS)
maximum airspeed for effective windshield anti-icing -
```
226
41
Propeller Deicer Ammeter
| Normal Operating Range from-
14-18 Amperes
42
Cabin Altimeter and Differential Pressure
| Normal Range to Max-
0- 6.1
43
Airplane
| Max Ramp weight (LBS)-
14,090
44
Airplane
| Max Gross Take0ff Weight-
14,000
45
Airplane
| Max Landing Weight-
12,500
46
Airplane
| Max Zero Fuel Weight-
11,000
47
Brake Deice System shall not be operated, except to test, at ambient temperatures above ____ Celsius.
15
48
Maintain___ % N1 of higher during simultaneous operation of the brake deice and surface deice.
85
49
Max G loading at 12,500 and below
| Wings UP -/+
-1.27 to +3.17
50
Max G loading at 12,500 and below
| Wings Down -/+
-1.27 to +2.0
51
Fuel Limitations
| No Takeoff Range:
0 to 265 lbs
52
Fuel Limitations
| Max Fuel Imbalance:
1,000 lbs
53
Fuel Limitations
| Max altitude for aircraft operations is ______ feet.
31,000 feet
54
The aircraft shall not be operated when the ambient temperatures are warmer than International Standard Atmosphere (ISA) +___ at SL to 25,000 feet or ISA +____ above 25,000 feet PA.
37 Celsius and 31 Celsius
55
Ice Vanes shall be extended for operations in ambient temperature of ___ or below when flight free of visible moisture cannot be assured.
+5 Celsius
56
Engine ice vanes shall be retracted at ____ and above for flight operations.
+15 Celsius
57
Minimum FAT for operation of deicing boots shall be ___ Celsius.
-40 Celsius
58
Maximum Crosswind Component is ____ kts at 90 degrees.
25 knots
59
The pitot heat is limited to ___ minutes during ground Operations.
15 minutes
60
Hydraulic Landing Gear cycles, a complete retraction and extension are limited to :
1 every 5 minutes for a total of 6 cycles followed by a 15 minute cool-down period.
61
Icing Limitations-
| Typical
1. Unexplained 30 % increase of torque needed to maintain airspeed in level flight
2. A cumulative 2 or more inches of Ice accumulation on the wing.
3. Unexplained decrease of 15 KIAS
4. Unexplained deviation between the pilot and co-pilot airspeed Indicators.
62
Icing Limitations-
| Severe
Use of autopilot is prohibited if any of the visual cues to typical icing condition exist.
