Limitations Flashcards
(92 cards)
1
Q
Max ramp weight
A
35200lb
2
Q
Max Take off weight
A
35000 lb
3
Q
Max Landing weight
A
33900
4
Q
Max Zero fuel weight
A
31700
5
Q
Load factor limits
A
Flap up : +2.5g / -1g
Flaps down: +2g / 0g
6
Q
Max operating Altitude
A
25,000 ft
7
Q
Max altitude for T/O and Landing
A
10,000
8
Q
Max runway slope T/O and Landing
A
+2% uphil
-2% downhill
9
Q
Max Tail wind component ( With sup 3)
A
10kt (20Kt)
10
Q
Max ambiant air temperature limit
A
48,9 or ISA +35 wichever is lower
11
Q
Min ambient temperature
A
-54 C
12
Q
Approved T/O Flaps setting
A
5 / 15
13
Q
Max Altitude with landing gear and/or flaps extended
A
15,000
14
Q
Vmo 0-14000
A
242 kt
15
Q
Vmo 15,000’
A
239 kt
16
Q
Vmo 20’000
A
223 kt
17
Q
Vmo 25’000
A
207 kt
18
Q
Vfe Flaps 5
A
148 kt
19
Q
Vfe Flaps 15
A
148 kt
20
Q
Vfe Flaps 35
A
130 kt
21
Q
Va
A
163 kt
22
Q
Vlo
A
158 kt
23
Q
Vle
A
172 kt
24
Q
Rough air airspeed
A
180 kt
25
Alt Landing gear extension
140 kt
26
Max tire GS
139 kt
27
Max propeller unfeathering
165 kt
28
Starter cranking limits
1 minute - 2 min off
1 minute - 2 min off
1 minute - 30 minutes off
29
Min voltage for GPU or APU engine start
24 V
30
Min Voltage for Battery start
22 V
31
Minimum NH ground operations
60%
32
Max torque with prop feathered
50%
33
Propeller restricted range
Continuous ops between 500-780 is prohibited
34
Propeller Ground limitation
Extended ops in excess of 780 must be carried out with airplane facing wind
35
Min oil temperature for unfeathering or power above idle
0 degres
36
Min oil temp for engine inlet splitter ice protection
Temp below -45 could result in ice build up
37
Pre heat engine prior to start
-40 or below
38
Complete Engine shut down
Oil pressure below 40 PSI
39
Max T/O max Torque
105%
40
Max T/O max ITT
816 deg
41
Max T/O max NH
100%
42
Max T/O max NP
1212RPM
43
Max T/O Oil pressure
55-65
44
Max T/O Oil temp
45-115
45
Normal T/O max torque
92%
46
Normal T/O max ITT
785 deg
47
Normal T/O max NH
100 %
48
Normal T/O max NP
1212 RPM
49
Normal T/O Oil pressure PSI
55 to 65 PSI
50
Normal T/O Oil temp
45-115 deg
51
Max continuous max Torque
90%
52
Max continuous max ITT
800 deg
53
Max continuous max NH
100%
54
Max continuous max NP
1212 RPM
55
Max continuous Oil pressure
55 to 65 PSI
56
Max continuous Oil temperature
45-115 deg
57
Starting max ITT
950 deg
Between 816-850 max 20 seconds
Between 850-950 max 5 seconds
58
Starting max Oil pressure
200 PSI
59
Starting oil temperature
Min -40 to start
60
Transcient max Torque
125%
61
Transcient max ITT
850 deg
62
Transcient max NH
102%
63
Transcient max NP
1320 RPM
64
Transcient max oil temp
125 deg max
65
Maximum Reverse max Torque
90%
66
Maximum Reverse max ITT
785 deg
67
Maximum Reverse max NH
100%
68
Maximum Reverse max NP
1212 RPM
69
Maximum Reverse Oil pressure
55-65 PSI
70
Maximum Reverse Oil temp
45-115 deg
71
Max usuable fuel
5678 lb
72
Approved fuel
Jet A, Jet A1, Jet B, JP-4
73
Fuel heater outlet temperature
11-57 deg
74
Max fuel imballance
600 lb
75
Electrical load DC Gen on ground
0.7
76
Electrical load DC Gen in flight
1.0
77
Electrical load TRU gnd and flt
1.0
78
Electrical load AC Gen per phase GND
Below 10 deg : 1.0
| 10 deg and above : 0.33
79
Electrical load AC Gen per phase FLT
1.0
80
Inverters ground and flight
1.0
81
Normal cabin ∆P
5.5 PSI (+/- 0.3)
82
Maximum cabin ∆P
5.95 PSI
83
Maximum Taxi, T/O and landing ∆P
0.5 PSI
84
Maximum cabin altitude pressurized
8000 ft
85
Lenght
73 ft 01 in
86
Width
85 ft
87
Height
24 ft 05 in
88
Propeller Diameter
13 ft
89
Propeller tip to ground
3 ft 01in
90
Hstab Width
26 ft
91
Normal 180 radius
60 ft
92
Maximum structural design weight
21400
