Limits Flashcards
1
Q
Vmo FL290-FL320
A
0.85M
2
Q
Vmo FL320-FL440
A
0.885M
3
Q
Vmo FL440-FL510
A
0.86M
4
Q
Vmo Above 8,000 ft
A
340 KCAS
5
Q
Vmo Below 8,000 ft
A
300 KCAS
6
Q
Vmca
A
112 KCAS
7
Q
Vmca (Landing)
A
110 KCAS
8
Q
Vmcg (SL)
A
107 KCAS
9
Q
Vmcg (15,000 ft)
A
86 KCAS
10
Q
Vmcg decreases by ____ per 1,000 ft from SL to 15,000 ft
A
~1 KCAS
11
Q
Va (Maneuvering)
A
206 KCAS
12
Q
Vb (Turb Pen) Below 10,000 ft
A
240 KCAS
13
Q
Vb (Turb Pen) Above 10,000 ft
A
270 KCAS / 0.8M
14
Q
Max Tire Speed
A
195.5 KCAS
15
Q
Max Mach Trim Inop speed
A
0.8 M
16
Q
Min Holding speed in Icing
A
160 KCAS
17
Q
Max airport Alt
A
14,500 ft
18
Q
Max airport Alt w/ HFLE
A
15,000 ft
19
Q
Max operating Alt
A
51,000 ft
21
Q
Max single pack operating Alt
A
48,000 ft
21
Q
Baggage door open over 40,000 ft
A
Max 5 min
22
Q
Do not open the baggage door with single pack ops over
A
45,000 ft
23
Q
max alt with no yaw damper
A
45,000 ft
24
Q
Max APU op alt
A
45,000 ft
25
APU guaranteed start up to
39,000 ft
26
APU may start up to
43,000 ft
27
Max APU EGT (start)
1050 deg C
28
Max APU EGT (running)
732 deg C
29
Max APU rotor speed
106% RPM
30
APU Alternator below 45,000 ft
40 kVa
31
Max fuel temp
140 deg C
32
Fuel temp may be up to ___ for ____ min
165 deg C, 15
33
Min fuel temp
-40 deg C
34
Cowl Anti-Ice
SAT 10 deg C or below and visible moisture
35
Wing Anti-Ice
Icing conditions are imminent or immediately upon detection
36
Max Engine Oil temp
160 deg C
37
Min Engine Oil temp (start)
-30 deg C
38
Min Engine Oil Temp (T/O power)
20 deg C
39
Min Engine Oil Px for T/O (below 72.3% HP)
35 psi (T/O), 25 psi (complete flight)
40
Engine must be shut down if Oil Px drops below
25 psi
41
Min Engine Oil Px for T/O (Above 90.0% HP)
45 psi (T/O), 35 psi (complete flight)
42
All operating fuel boost pumps MUST be ___ for all phases of flight unless fuel balancing in progress
ON
43
Max Fuel tank temp
54 deg C
44
Min Fuel tank temp
-37 deg C
45
Use of TR for power back is
NOT APPROVED
46
Starter duty cycle is ___ starts with a max of ___ per start cycle. Delay _____ between start cycles. After 3 start cycles delay use of starter by _____
3, 3 min, 15 sec, 15 min
47
starter my be reengaged at HP RPM speeds up to stater cut out of ____ HP RPM
42% HP RPM
48
Max Speed Flaps 10 deg
250 KCAS / 0.6 Mt
49
Max speed Flaps 20 deg
220 KCAS / 0.6 Mt
50
Max speed Flaps 39 deg
170 KCAS / 0.6 Mt
51
Use of speed brakes is not allowed with
Landing Gear Extended or full flaps
52
Use of flaps in icing is limited to
T/O, Approach, and Landing
53
Ground Spoilers may be inop if
Anti-skid is operational,
20 deg Flaps are used,
Cowl and Wing Anti-Ice systems arent used
54
If a touch and go is to be performed
GRD SPLR must be off and manual spoiler landing distance taken into account
55
Max Alt to extend the landing gear
20,000 ft MSL
56
Max landing gear extension speed
225 KCAS / 0.7 Mt
57
Max gear speed (down and locked)
250 KCAS / 0.7 Mt
58
Max landing gear extension speed (blow down)
175 KCAS
59
Anti-skid my inop if
Runway is dry,
GRD SPLR is operational,
20 deg Flaps,
Cowl and Wing Anti-Ice not used
60
g loading (Flaps up)
-1 to 2.5 g
61
g loading (flaps 10 or 20)
0 - 2.0 g
62
g loading (flaps 39 deg) below 75,300 lbs
0 - 2.0 g
63
g loading (flaps 39 deg) above 75,300 lbs
0 - 1.5 g
64
when HMG is in operation
speed brakes may be used provided 3 seconds for full range of movement
65
Max cabin pressure differential
10.48 PSID
66
Max cabin pressure differentail (T/O, Taxi, Landing)
0.3 PSID
67
Takeoff in Alt Control mode is
Prohibited
68
Max crosswind for engine start
30 Kt
69
Max tailwind for engine start
20 kt
70
Min height to engage auto-pilot
200 ft AGL
71
Single-engine auto-pilot coupled go-around is
NOT ALLOWED
72
Min height to disengage the auto-pilot from an ILS or LPV
60 ft AGL
73
Min height to disengage the auto-pilot from LNAV/VNAV approach
50 ft below DA/MDA
74
Max demonstrated altitude loss for a coupled go-around
60 ft
75
Max slope for takeoff and landing
-2% to 2%
76
Min Flight crew
2 pilots
77
Max passengers
19
78
Max occupants
22
79
Aircraft width
93 ft 6 in
80
Aircraft Height
25 ft 11 in
81
Aircraft Length
96 ft 5 in
82
Max ground starting TGT
700 deg C (Momentary)
83
Max relighting (Airstart) TGT
850 deg C (Momentary)
84
Max Takeoff LP % RPM
101.1%
85
Max Takeoff HP % RPM
99.6%
86
Max Takeoff TGT
900 deg C (5 min 2 Engines, 10 min 1 Engine)
87
Max Continuous LP % RPM
101%
88
Max Continuos HP % RPM
98.9%
89
Max Continuous TGT
860 deg C
90
Max Overspeed LP % RPM
101.5%
91
Max Overspeed HP % RPM
99.8%
92
Max Overspeed TGT
905 deg C (20 sec)
93
Max Reverse LP % RPM
70.0% (30 sec)
94
Zero Fuel Weight
54,500 lbs
95
Max Ramp Weight
91,400 lbs
96
Max Takeoff Weight
91,000 lbs
97
Max Landing Weight
75,300 lbs
98
Max Fuel Imbalance (Takeoff)
1,000 lbs
99
Max Fuel Imbalance (In-flight)
2,000 lbs
100
Max Fuel
41,300 lbs
101
PTU activates
L hydro px < 1500 psi
L hydro Res > 1.5 gal
R hydro temp < 104.4 C
102
Max ALT for air start
25,000 ft
103
Min speed for windmill start
250 KCAS
104
Min Vapp (flaps 20)
125 KCAS
105
Max ALT for suction feed
20,000 ft
106
Pylon Hot illuminates
250 F
107
Aft Equip Hot
250 F
108
L/R EER Hot
150 F
109
Fuel level low
Hopper below 650 lb
110
Maximum speed with the emergency stabilizer trim armed, autopilot engaged and a jammed elevator
270 KCAS / 0.8 Mt
111
Max speed with missing vortex generators
0.85 Mt
112
Max brake temp
650 C
113
Wing anti ice temp
130 F +/- 10
