Limits Flashcards
1
Q
Max engine ground start TGT?
Time limit?
A
700
Momentary
2
Q
Max engine air start relighting TGT?
Time limit?
A
850
Momentary
3
Q
Max engine takeoff LP
HP
TGT
Time limit
A
101.1
99.6
900
5 mins. Two engine, 10 mins. Single engine
4
Q
Max continuous LP
HP
TGT
Time limit
A
101
98.9
860
Unrestricted
5
Q
Max engine over speed LP
HP
TGT
TIME LIMIT
A
101.5
99.8
905
20 seconds
6
Q
Max reverse thrust LP
TIME LIMIT
A
70
30 seconds
7
Q
Max Zero fuel weight
A
54,500
8
Q
Max ramp weight
A
91,400
9
Q
Max takeoff weight
A
91,000
10
Q
Max landing weight
A
75,300
11
Q
Fuel imbalance for takeoff
A
1,000 lbs
12
Q
Fuel imbalance in-flight
A
2,000 lbs
13
Q
Max fuel
A
41,300 lbs
14
Q
Aircraft length
A
96’ 5”
15
Q
Aircraft wingspan
A
93’ 6”
16
Q
Aircraft height
A
25’ 11”
17
Q
Aircraft nosewheel to MLG
A
45’
18
Q
MLG width
A
14’ 4”
19
Q
Elevator width
A
35’ 2”
20
Q
When HMG is in operation, speed brakes may be used provided operation is ?
A
Slow operation, approx 3 seconds for full range movement
21
Q
Do not operate HMG when normal AC power is available, except?
A
For L or R ESS DC bus failure
22
Q
Max cabin diff for taxi/takeoff/landing
A
0.3 PSID
23
Q
Max cabin pressure diff
A
10.48 PSID
24
Q
When aircraft is static on the ground, stabilized engine operation in the keep out zone of what LP RPM, is prohibited.
Any accel-decel through this band must not exceed 10 seconds.
A
66 to 80% RPM
25
Max ZFW
54,500 lbs
26
Max ramp weight
91,400 lbs
27
Max takeoff
91,000 lbs
28
Max landing
75,300
29
Max fuel imbalance for takeoff
1,000 lbs
30
Max fuel imbalance in-flight
2,000 lbs
31
Max fuel load
41,300 lbs
32
Max TGT prio to ground start
150 deg. C
33
When the HMG is in operation, speed brakes may be used provided operation is ? (Approx. ? seconds for full range movement
Slow, 3 seconds
34
Max cabin pressure diff
10.48 PSID
35
Max cabin press diff taxi/takeoff/land
0.3 PSID
36
Keep out zone
66-80% while static, on the ground. Any accel/decel must not exceed 10 seconds.
37
Takeoff in ? Control mode is prohibited
Alt
38
X-wind above 20 knots, accel to takeoff power, fan speed limited to
66%
20 knots
39
Add ? Feet to required field length for slam takeoff
600’
40
X-wind >20 kts, forward speed >20 kts, a ? Acceleration is required.
Slam
41
Max x-wind for takeoff & land
28 knots
42
Once takeoff had commenced, use of tiller >? Knots, is not recommended
60 knots
43
Max x-wind for engine start
30 knots
44
Max tailwind for engine start
20 knots
45
Weather radar, ? Feet from refueling ops
300’
46
Min crew
2 pilots
47
Max pax
19
48
Max occupants
22
49
Slope
+2% uphill
-2% downhill
50
Max eng oil temp
160 deg C
51
Min eng oil temp for start
-30 deg C
52
Min eng oil temp for takeoff power
20 deg C
53
Min Eng oil press for T/O (<72.3 HP)
35 PSI <72.3 HP
54
Min oil press for T/O (>90 Hp)
45 PSI >90 HP
55
Eng oil press continue flight (<72.3 HP)
25 PSI <72.3 HP
56
Eng oil press continue flight (>90 HP)
35 psi >90HP
57
Engine starter duty limits
3, three minute attempts, 15 seconds between each then 15 minutes off
58
The starter may be reengaged at HP RPM speeds up to starter cut out of
42% HP RPM
59
All operable fuel boost pumps must be selected “?” for ??? phases of flight unless fuel balancing is in progress
On for all
60
Engines will suction feed at or below ? feet
20,000’
61
Use of T/R’s for power back is/is not approved?
Is not
62
Minimum fuel tank temp
-37 deg C
63
Max fuel tank temp
+54 deg C
64
10 deg flaps speed
250 knots/.60 mt
65
20 deg flaps speed
220kcas/.60mt
66
39 deg flaps speed
170 kcas/.60 mt
67
Use of speed brakes is/is not allowed with gear down and/or full flaps?
Is not
68
Ground spoilers may be inop if ? Is operative! 20 deg flaps are used, and wing anti-ice systems are not used. See MEL
Anti-skid
69
If a touch-and-go landing is to be performed, the ground spoiler switch must be ? and manual spoiler landing distances must be taken into account.
Off
70
Max landing gear altitude
20,000 MSL maximum
71
Normal ops landing gear speed (VLO)
225 kcas/.70 mt
72
Normal ops landing gear extended speed (VLE)
250 kcas/.70mt
73
Landing gear blowdown speed?
Once gear extended?
175kcas
250kcas/.70mt
74
Anti-skid may be inop provided? See MEL
Dry rwy, ground spoilers operative, flaps 20, cowl & wing anti-ice not used.
75
Airspeed limit FL290-320
0.85
76
Airspeed limit FL320-440
0.885
77
Airspeed limit FL440-510
0.86
78
Vmo above 8,000’
340 kcas
79
Vmo below 8,000
300kcas
80
Minimum control airspeed (Vmca)
112kcas
81
Minimum control speed landing (Vmcl)
110kcas
82
Minimum control speed ground (Vmcg)
107kcas at sea level
83
Minimum control speed ground (Vmcg)
.86kcas at 15,000’
84
Vmcg decreases linearly at approx. ? Knot per ? Ft from sea level to 15,000
1 knot per 1,000’
85
Maneuvering speed (Va)
206kcas
86
Turb. Penetration speed (Vb) > 10,000
270kcas/.80mt
87
Turb. Penetration speed (Vb) <10,000’
240kcas
88
Holding speed in icing conditions
160kcas
89
Minimum Mach trim inop.
0.80mt
90
Tire speed limit
195.5 kts
91
Yaw damp inop >10,000’ ft max
260kcas/.80
92
Yaw damp inop. <10,000’ max
250kcas
93
Yaw damps inop. >20,000 ft. minimum
210kcas
94
Yaw damp inop. <20,000’
See chart AOM Vol 1
95
Max airport operating altitude
14,500
96
Max airport with HLFE system fitted
15,000
97
Max operating altitude
51,000
98
Single pack operations
48,000
99
Internal baggage door open
Above 40,000 ft for 5 mins
100
Internal baggage door open with one Pack
One ECS PACK, no entry >45,000 ft
101
Maximum yaw damp inop altitude
45,000
102
APU max operating altitude
45,000’
103
APU guaranteed start altitude
39,000
(May start up to 43,000)
104
APU Electrical load
100% sea level up to 45,000’
105
APU may be used for starter assisted air starts below ? Feet. However, max altitude for an engine air start is ? Feet.
30,000
25,000
106
APU max start TGT
1,050
107
APU max running TGT
732
108
APU max rotor speed
106%
109
Continuous operation of the APU starter when powered by airplane batteries:
? consecutive start attempts followed by a ? hour cooldown
3 consecutive start attempts followed by a 1 hour cooldown
110
Continuous operation of APU starter when powered by external DC cart:
Max of ? start attempts with a ? minute cool down between each attempt. ? hour cool down after 3rd attempt
Successful consecutive starts limited to ? at ? minute intervals per start
Max of 3 start attempts with a 15 minute cool down between each attempt. 1 hour cool down after 3rd attempt.
Successful consecutive starts limited to 6 at 10 minute intervals per start
111
What conditions do we turn on Cowl anti-ice ?
SAT 10 deg. C or below and visible moisture
112
When do we turn on wing anti-ice?
Icing conditions are imminent or immediately upon detection
113
Max engine fuel temp
140 C
114
Fuel temp up to ? for a max of ? minutes is permissible
165 C , 15 mins
115
Minimum engine fuel temp
-40 C
116
Speed brakes are not allowed when landing gear is ? and/or ?
Gear extended and/or full flaps
117
Flaps 0 flight load
-1 to 2.5
118
Flaps 10 or 20 flight load
0 to 2.0 up to max takeoff weight
119
Flaps 39 flight load < 75,300 lbs
0 to 2.0
120
Flaps 39 flight load > 75,300 lbs
0 to 1.5
121
Do not operate HMG when normal ? power is available, except as provided for in L or R ? failure.
AC
ESS DC bus failure
122
With a single nine inop, select ? Only as the TCAS operating
TA only
123
Mach trim inop
.80 MT maximum
124
Autopilot minimum engage height on takeoff
200’ AGL
125
Autopilot minimum disengage height for ILS, MLS, or LPV approach
60’ AGL
126
Autopilot minimum disengage height for MDA/DA from LNAV approach
50’ below MDA/DA
127
Autopilot minimum demonstrated altitude loss for coupled go-around
60’
128
Auto-throttles are available from takeoff to landing except?
Single engine approach
129
Minimum flight crew
Pilot and copilot
130
Maximum passengers
19
131
Max occupants
22
132
Max slope for takeoff and landing
+2% uphill and -2% downhill
133
APU ? Ground ops are prohibited
Ground
134
APU use in flight prohibited except the following
Dual engine failure
Dual generator failure
Single engine failure
Single generator failure
135
The APU may be operated in-flight for the purpose of “bleeds off” takeoff, up to a max of ? Ft
5,000’ AGL
136
Dispatch is ? Premiered with any engine generator inop
Not
