Limitations Flashcards
(97 cards)
1
Q
TAXI/ RAMP WEIGHT
A
48,300
2
Q
TAKEOFF WEIGHT
A
48,200
3
Q
LANDING WEIGHT
A
38,000
4
Q
Zero Fuel Weight
A
32,000
5
Q
Minimum Flight Weight
A
26,000
6
Q
Maximum Airport Pressure Altitude for T/O and LDG
A
10,000’
7
Q
Maximum Operating Altitude
A
41,000’
8
Q
Maximum OAT for T/O and LDG
A
ISA +35C
9
Q
Minimum OAT for T/O
A
-40C
10
Q
Maximum Runway Slope
A
+/- 2%
11
Q
Maximum Tailwind
A
10 kts
12
Q
Maximum Crosswind to use reverse thrust
A
24 kts
13
Q
Flaps UP load factor
A
-1.0 G to 2.5 G
14
Q
Flaps DOWN load factor
A
0.0 G to 2.0 G
15
Q
Maximum G/P angle < 1500’ TDZE
A
4.49 degrees
(See Supplement 11 Chapter 7 of AFM for G/P angles above 3.5 degrees)
16
Q
Above FL250, at least 1 pilot…
A
Must wear a safety harness
17
Q
Enroute use of flaps or flight with flaps extended is prohibited above what altitude?
A
15,500’
18
Q
VLo
A
197 kts / M .6
19
Q
VLe
A
250 kts / M .7
20
Q
Maximum altitude with gear down
A
20,000’
21
Q
Tire speed limit
A
182 kts
22
Q
Turbulent air penetration speed
A
280 kts / M .75
23
Q
Maximum RVSM cruise speed
A
M .83
24
Q
Maximum N2 split on ground at idle.
A
2%
25
VFe 20 degrees
231 kts
26
VFe 30 degrees
197 kts
27
VFe 45 degrees
189 kts
28
Wing fuel capacity
4,860# each
29
Auxiliary fuel tank capacity
7,168#
30
Tail tank fuel capacity
3,112#
31
Total fuel capacity
20,000#
32
Maximum wing fuel imbalance for taxi, takeoff, and landing
400#
33
Maximum wing fuel imbalance for cruise flight
800#
34
T/O with < 500# fuel in Aux tank permitted provided how much fuel is in each wing tank?
1,500# in each wing tank and tail tank must contain 0.
35
If Aux tank has > 500# fuel, takeoff is permitted when each wing tank is fueled according to the Wing Tank Schedule. What is minimum amount in each wing for a gross weight of up to 42,400?
1,500# in each wing.
36
Minimum fuel for go-around
500# per wing with maximum 10 degrees nose-up pitch attitude.
37
Fuel transfer must be in what position for takeoff?
OFF
38
Can tail tank be used as a C.G. device?
No. Must remain in AUTO mode.
39
2 conditions must be met for jettisoning fuel. What are they?
Flaps 0 degrees and no lightning conditions.
40
Minimum engine fuel temp for takeoff?
5C
41
Minimum altitude to engage autopilot after takeoff
320’ AGL
42
Minimum altitude for autopilot use during visual/non-precision approach
320’ AGL
43
Minimum altitude for autopilot use on precision approach (glide path < or = 3.5 degrees)
80’ AGL
44
Minimum altitude for autopilot use during precision approach (glide path > 3.5 and < 4.5 degrees)
160’ AGL
45
Maximum relief differential pressure
9.2 PSI
46
Maximum negative differential pressure
-0.5 PSI
47
Maximum differential pressure during taxi, takeoff, and landing
0.2 PSI
Aircraft must be depressurized prior to opening doors.
48
If engine cowl and/or wing anti/ice is selected to ON for takeoff or landing, bleed air 10th stage valves must be in what position?
CLOSED
49
Above 40,000’, what must be selected ON for each engine?
1 ACU
or
COWL A/ICE for each engine
50
Maximum engine-driven generator load 0-35,000’?
30 kva
51
Maximum engine-driven generator load > 35,000’?
25 kva
52
Maximum APU generator load 0-20,000’?
30 kva
53
Maximum load on TRU’s?
100 amps
54
During ground operations at ambient temperatures > 40C (104F), operation of electrical/avionics equipment must be limited to how long?
30 minutes
UNLESS: at least 1 air conditioning pack is operating and the passenger door is closed
55
Inflight extension of flight spoilers prohibited below what altitude and below what airspeed?
< 300’ AGL
< approach speed plus 10 kts
56
Continuous engine ignition is required when?
T/O and LDG on contaminated runway
T/O and LDG with high crosswind component
Flight through moderate or heavier intensity rain
Flight through moderate or heavier intensity turbulence
Flight in vicinity of thunderstorms
57
Maximum contaminant depths for takeoff?
Standing water 0.25 in
Slush 0.25 in
Wet snow 0.5 in
Dry snow 1.2 in
58
Maximum contaminant depths for landing?
Standing water 0.5 in
Slush 0.5 in
Wet Snow 1.0 in
Dry snow 2.4 in
59
Taxi lights must be selected OFF when the aircraft is?
Stationary
60
Left and right landing lights must be selected OFF when the aircraft is?
Stationary
The left and right landing lights must not be used on the ground, except for the takeoff roll and landing
61
APU max EGT (start)
974C
62
APU max continuous EGT
731C
63
APU max RPM
110% (auto shutdown at 107%)
64
APU minimum temp for start
-40C
65
APU max altitude for start
20,000’
66
Maximum indicated airspeed for inflight APU start and operation
290 kts
67
APU max altitude for bleed air usage
15,000’
68
Max altitude to use APU for inflight engine start (double-engine failure only)
15,000’
69
If both engines started with APU, what is the maximum N2 for the operating engine?
70%
70
Selection of the APU PWR FUEL switch/light activates:
APU ECU is powered, and after 3-second BITE test, the APU EGT and RPM are displayed on the EICAS page
APU fuel pump energizes
Opens APU fuel shutoff valve
Opens negative-G shut off valve
71
APU Battery rating
24V / 43 ampere-hour
72
Minimum APU battery voltage for APU start
22 volts
73
APU start cycles using aircraft batteries
Attempt 1, 2, 3
Max time 30 seconds ON
Followed by 20 minutes cooling
Attempt 4, 5
Max time 30 seconds ON
Followed by 35 minutes cooling
*3 attempts in 1 hour (AOM 12.8.1)
74
APU start cycles using ground power
Attempt 1, 2
Max time 15 seconds ON
Followed by 20 minutes OFF
Attempt 3, 4
Max time 15 seconds ON
Followed by 35 minutes OFF
*3 attempts in 1 hour (AOM 12.8.1)
75
APU hung start
Not greater than 30% RPM within 60 seconds
76
Normal takeoff maximum ITT and time limits
884 for 5 minutes
900 2 minutes out of 5 total transient
77
Maximum takeoff (APR operating) ITT and time limits
899 for 5 minutes
928 for 2 minutes out of 5 total transient
78
Minimum engine oil pressure for takeoff
45 psi
79
Maximum transient engine oil pressure after cold start
156 psi
(130 psi at idle, 10 minutes max)
80
Normal engine starter cycle
3 consecutive start attempts of 60 seconds each. 5 minutes cooling required prior to additional start attempts.
81
Engine dry motoring limits
First dry motor 90 seconds followed by 5 minutes cooling.
Second and subsequent dry motors 30 seconds followed by 5 minutes cooling.
82
Continuous engine ignition required
Takeoff/landing on contaminated runway
Takeoff in high crosswind
Moderate or heavier intensity rain
Moderate or heavier intensity turbulence
In vicinity of thunderstorms
83
Maximum crosswind dry or wet runway?
24 knots
84
Maximum crosswind contaminated runway fair/medium braking action?
15 knots
85
Maximum crosswind contaminated runway braking action poor?
10 knots
86
45-minute IFR Reserve Fuel
2019#
87
Minimum Release Fuel
4000#
88
Hot Spare Fuel
8500#
89
Emergency Release Fuel
1500#
90
Minimum Dry Runway Length
4500’
91
Minimum Runway Width
75’
92
Baggage Compartment Max Weight
900#
93
Minimum Altitude for use of Flight Spoilers
300’ AGL
94
Minimum Pavement Width for 180-degree turn
61 feet
95
Maximum fuel imbalance between left & right main tanks during gravity refueling
2500 lbs.
96
When is the use of KA SAT GND TX/KA BAND GND TX feature prohibited?
1. During deice operations
2. 100 feet or less from a building higher than the aircraft
97
Fuel quantity required for parking aircraft in inclement weather?
6500-8500#
