Limitations Flashcards
1
Q
Max Ramp Weight
A
48,300lbs
2
Q
MTOW
A
48,200lbs
3
Q
MLW
A
38,000lbs
4
Q
Max ZFW
A
32,000lbs
5
Q
Min flight weight
A
26,000lbs
6
Q
Min operating empty weight
A
22,150lbs
7
Q
Max ambient temp approved for take off
A
ISA +35
8
Q
Min ambient temp approved for take off
A
-40 C/-40F
9
Q
Tactile check of wing leading edge required when
A
OAT 5 or less
Wing fuel temp is 0 or less
Atmospheric conditions have been conducive to frost
10
Q
Cowl anti ice required when
A
10c or less
11
Q
Wing anti ice required when
A
5c or less
12
Q
Max slope
A
2% up or down
13
Q
Max tailwind for takeoff or landing
A
10kts
14
Q
N1 red line
A
98.6%
15
Q
Max continuous thrust ITT
A
900 degrees
16
Q
Max continuous ITT with APR
A
928 degrees
17
Q
N2 red line
A
99.3%
18
Q
Oil temp red line
A
163 degrees
19
Q
Oil temp green band
A
-40 to 154 degrees
20
Q
Oil pressure red line
A
0-25psi
21
Q
Oil pressure green band
A
26-115psi
22
Q
Limitation to operating above FL400
A
One pack must be operating
23
Q
N2 split should not be greater than
A
2%
24
Q
If the aircraft is cold soaked, the aircraft must be motored for how long
A
60 seconds
25
Continuous ignition required when
TO/LDG on contaminated runway
Crosswind greater than 10kts
Flight through moderate rain or turbulence
In the vicinity of TS
26
Max motoring on first engine start
90 seconds
27
Max motoring on 2nd and subsequent engine start
30 seconds
28
Time off required if engine is motored beyond limit
5 minutes
29
Engine start: fuel to idle when ITT
120 on ground
90 in flight
30
Engine relight windmilling 21-10
IAS 300-348 N2 12 -55%
31
Engine relight windmilling 10-8
IAS 300-348 N2 10 -55%
32
Engine relight windmilling 8-0
IAS 300 N2 10 -55%
33
Engine relight starter assisted 21-15
IAS 200-300 N2 0 -55%
34
Engine relight starter assisted 15-0
IAS 140-300 N2 0 -55%
35
Fuel imbalance
400 taxi, take off, landing
800 in flight
36
Main tank quantity
9,720lbs
37
Aux tank quantity
7,168lbs
38
Tail tank quantity
3,112lbs
39
Gravity quantity
15,780lbs
40
Fuel percentage reduction with gravity refuel
7%
41
Aux - tail ratio
2.65%
42
500lbs permitted in aux provided there is at least what quantity in the mains
1500lbs + none in the tail
43
Aux must be at least what ratio to tail quantity if the tank is equal to or greater than 1200lbs
2.75%
44
Aux must be at least what ratio to tail quantity if the tank is less than 1200lbs
2.2%
45
Fuel dump limitations
Zero flap, no lightening
46
Max engine time without servicing oil
16 hrs
47
Oil level should be checked at what time interval after shutdown
15 mins - 2 hrs
48
Max oil refill without dry motoring
2 qt
49
Flaps 20 speed
231 kts
50
Flaps 30 speed
197 kts
51
Flaps 45 speed
189 kts
52
Max landing gear operating speed
197 kts
53
Max landing gear extended speed
250 KIAS/0.7M
54
Landing gear cannot be operated above what alt
FL200
55
Tire limit speed
182 kts
56
Wet ADG limitation speed
250 kts
57
TURB penetration speed
280KIAS/0.75M
58
Load factor flaps up
-1 to 2.5G
59
Load factor flaps down
0 to 2G
60
Max differential pressure
9.2psi
61
Max negative differential pressure
-0.5psi
62
Take off, taxi and landing pressure must not exceed
0.2psi
63
Min Autopilot height on takeoff
320 ft
64
Min Autopilot height precision approach (less than 3.5)
80 ft
65
Min Autopilot height precision approach (3.5 - 4.5)
160 ft
66
Limitation on 10th stage if cowl/wing anti ice is required for take off
10th stage must be closed
67
AC System loads 0-FL20
30kva
68
AC System loads FL20-35
30kva
69
AC System loads FL35-41
25kva
70
AC System loads for APU 0-FL20
30kva
71
Max load for TRU’s
100amps
72
Flap use enroute limitation
Cannot be used
73
Flap use limitation
Prohibited above 15,500ft
74
Spoiler use limitation
Cannot be used below 300ft
75
Spoiler limitation
Must not be extended in flight at air speeds below the recommended approach speed +10
76
Reversers limitation
Below 60kts, reverse thrust must be reduced to 60% N1 or less
77
FMS must be receiving suitable nav from what
1 x VOR/DME or
2 x DME’s or
1 x IRS or
GPS
78
Airplane operation must not be predicated upon performance data ETE/ETA and fuel remaining
True
79
Flight plans must be what to conduct an FMS approach operation
Identical
80
FMS instrument approaches are prohibited unless approach is
Annunciated on the PFD
81
VNAV prohibited during
QFE ops
82
VNAV prohibited between what points of a V-MDA approach
FAF to missed approach point
83
VFLC prohibited when using
MACH
84
Maximum operating altitude for 150 series APU
20
85
Maximum altitude and IAS for guaranteed 150 series APU start
20/ 141-290kts
86
Maximum inflight bleed air extraction altitude for 150 series APU
15
87
Start % - fuel and ignition in for 150 series APU
5%
88
Start % - starter cutout for 150 series APU
35-45%
89
Start % - ignition deactivated for 150 series APU
99%
90
Hung start for 150 series APU
Less than 30% in 60 seconds
91
Is in flight use of 100/150 APU permitted?
100 - if IDG’s fail
150 - yes
92
Overspeed auto shutdown of APU 100/150
100 - 110%
150 - 107%
93
In flight engine start guarantee for 100/150 series APU
100 - 2 engine out 10,000ft
150 - 2 engine out 15,000ft
94
Does the APU have dual powered ECU’s
100 - no
150 - yes
95
Max EGT for APU use (steady ops)
731 degrees
96
APU Start cycles using battery power on ground or normal in flight start
3 x 30 seconds of cranking
20 minutes off
2 further attempts each 30 seconds
97
APU start cycles using ground power
2 x 15 seconds continuous cranking
20 minutes off
2 further attempts at 15 seconds
98
If you cannot start the APU after reaching the limit of attempts, how long must you then wait
35 minutes
99
Max APU EGT for starting
974 degrees
100
Hydraulic accumulator pressure should be what during preflight?
1500psi
101
Normal hydraulic pressure is?
3000psi
102
Hydraulic pressure turns amber when pressure falls below?
1800psi
103
OXY LO PRESS EICAS message when?
Less than 800psi
104
OXY HP disk will rupture when pressure exceeds?
2800psi
105
The other disk will rupture if the LP module pressure exceeds?
90psi
106
Maximum operating altitude
FL410
107
Takeoff Rotation Rate
Maximum 3 degrees/ second
108
Maximum number of occupants
19 passengers,
3 crew
109
Fuel Jettison
Only with flaps at 0.
Jettisoning of fuel in known lighting conditions is prohibited.
110
Oil Consumption
6.4 ounces per hour / 0.05 gallons per hour
111
Oil Level
Maximum duration without engine oil servicing is 16 hours
112
Oil level should be checked...
between 15 minutes to 2 hours after engine shutdown.
Maximum refill allowable is 2 qts without dry motoring the engine
