Limitations Flashcards
1
Q
Max Ramp Weight
A
85,870lb
2
Q
Max Takeoff Weight (MTOW)
A
85,517lb
3
Q
Max Landing Weight (MLW)
A
74,957lb
4
Q
Max Zero Fuel Weight (MZFW)
A
69,886lb
5
Q
Max Cargo Weight (FWD)
A
3,307lb
6
Q
Max Cargo Weight (AFT)
A
2,535lb
7
Q
Aircraft Dimensions
A
Length — 103’ 11”
Width (Wingspan) — 93’ 11”
Height — 32’ 4”
8
Q
Cabin Loading
A
Max PAX = 76
12 First / 64 Coach
9
Q
Kinds of Operations (7)
A
- Day and Night
- VFR
- IFR
- Icing Conditions
- Cat I & II
- RVSM
- Extended Overwater Operation (when equipped)
10
Q
Pressure Altitude / Temp where T/O-1 requried
A
At or above 8,000’ PA
Or
At or above ISA +35°C
11
Q
Minimum flight crew
A
Pilot and First Officer
12
Q
Maximum headwind for CAT II
A
25 kts
13
Q
Max crosswind for landing vis < 4000 or 3/4
A
15 kts (E)
14
Q
Max takeoff and landing tailwind component
A
10 kts
15
Q
Max runway slope (uphill, downhill)
A
+ / - 2%
16
Q
Flap manuevering load acceleration limits (up and down)
A
Up: -1.0 to +2.5 G
Down: 0.0 to +2.0 G
17
Q
Max operating altitude
A
41,000’
18
Q
Max takeoff & landing altitude
A
10,000’
19
Q
Max SAT for takeoff, landing, and ground start
A
54°C
20
Q
Max altitude with flaps extended
A
20,000’
21
Q
Max flight operating latitude
A
78° North (E)
78° South (E)
22
Q
Min SAT for takeoff, landing, and ground start
A
-40°C
23
Q
Max crosswind for T/O—Dry runway
A
35 kts (E)
24
Q
Max crosswind for T/O—Wet runway
A
30 kts (E)
25
Max crosswind for T/O—Runway w/ frost
31 kts
26
Max crosswind for T/O—Compacted snow RWYCC 4
20 kts
27
Max crosswind for T/O—standing water / slush / wet snow / dry snow
18 kts
28
Max crosswind for T/O—slippery when wet runway / RWYCC 3
15 kts
29
Max crosswind for T/O—ice
12 kts
30
Max crosswind for landing—RWYCC 6
38 kts
31
Max crosswind for landing—RWYCC 5
Braking Action: Good
31 kts
32
Max crosswind for landing—RWYCC 4
Braking action: Good to Medium
20 kts
33
Max crosswind for landing—RWYCC 3
Braking action: Medium
15 kts
34
Max crosswind for landing—RWYCC 2
Braking action: Medium to Poor
12 kts
35
Max crosswind for landing—RWYCC 1
Braking action: Poor
8 kts
36
Max crosswind for landing—RWYCC 0
Braking action: Nil
Operations Prohibited
37
Vmo (above 10,000’ MSL to FL280)
Max operating airspeed
320 KIAS
38
Mmo (above FL280)
Max operating mach number
.82
39
Max airspeed for RAT (Ram Air Turbine) operation
Vmo / Mmo
40
Turbulent airspeed (below 10,000’ MSL)
250 KIAS
41
Vmo (below 10,000’ MSL)
FAA — 250 KIAS
Structural limitation — 300 KIAS
42
Va
240 KIAS
43
Turbulent airspeed (at or above 10,000’ MSL)
270 KIAS / .76M
| whichever is lower
44
Max airspeeed for windshield wiper operation
250 KIAS
45
Max airspeeed for windshield wiper operation in the non-parked position
320 KIAS
46
Max airspeed to open flight deck window
160 KIAS
47
Vlo (down)
Max gear extension speed
250 KIAS
48
Vlo (up)
Max gear retraction speed
250 KIAS
49
Vle
250 KIAS
50
Vfe 1
230 KIAS
51
Vfe 2
215 KIAS
52
Vfe 3
200 KIAS
53
Vfe 4
180 KIAS
54
Vfe 5
180 KIAS
55
Vfe Full
165 KIAS
56
Max altitude flaps / slats can be extended
20,000’ MSL
57
Approved Fuels
ASTM -- Jet A or A1 (Primary)
Brazilian -- QAV1 (Secondary)
American -- JP8 (Secondary)
58
Max Cabin Differential Overpressure
8.8 psi
59
Max Cabin Differential Pressure (Above FL370)
8.4 psi
60
Max Cabin Differential for T/O & Landing
0.2 psi
61
Max Cabin Differential Negative Pressure
-0.5
62
Max Altitude Depressurized
10,000 or MEA (whichever is higher)
63
Max altitude display difference in flight for RVSM
180 ft
64
What must occur prior to takeoff in the event that the airplane was landed below -40°C?
Maintenance inspection
65
What APU do we have?
Sundstrand APS 2300
66
First & Second APU Start Attempts
START/ON then 60 sec. OFF
67
Third APU Start Attempt
START/ON then 5 min. OFF
68
APU Minimum Operation Temperature
-54°C
69
APU Maximum Operation Temperature
ISA + 35°C
70
APU EGT (Start)
1032°C
71
APU EGT (Continuous)
717°C
72
APU Max Operation Altitude (Electrical)
33,000 ft.
73
APU Max Start Altitude
30,000 ft.
74
APU Max Operation Altitude (Eng. Start Assist)
21,000 ft.
75
APU Max Operation Altitude (ECS Bleed)
15,000 ft.
76
APU Max Rotor Speed
108%
77
When can autopilot be engaged on T/O or go around?
Above 400' AFE
78
When must autopilot be disconnected during landing?
Above 50' AFE
79
Engine Model
GE CF34-8E5
80
N1 RPM Max
99.5%
81
N2 RPM Max
99.4%
82
Max Start ITT
815°C
83
Max Normal T/O ITT
965°C (2 min)
949°C (3 min)
[Total -- 5 min]
84
Max T/O & G/A ITT
1006°C (2 min)
990°C (3 min)
[Total -- 5 min]
85
Max Continuous ITT
960°C
86
Min / Max Oil Pressure
25 psi / 95 psi
87
Continuous Oil Temperature
155°C
88
Transient Oil Temperature
163°C (15 min. limit)
89
Engine Thrust
```
T/O-1 = 13,000 lbs. / OEI ATTCS = 14,200 lbs.
T/O-2 = 11,800 lbs. / OEI ATTCS = 13,000 lbs.
```
90
Maximum Fuel Capacity
20,934 lbs. (10,467 lbs. per tank)
91
Maximum Useable Fuel Quantity
20,784 lbs. (10,392 lbs. per tank)
92
Unusable Fuel Quantity
150 lbs. (75 lbs. per tank)
93
Maximum Fuel Imbalance
794 lbs.
94
Fuel density
6.767 lbs. / US gallon
95
Minimum Fuel Tank Temperature
-37°C
96
Crossfeed Operation
Crossfeed Knob must be OFF for T/O and Landing
97
Dry Motoring Time Limits
1st -- Max 90 sec. ON, followed by 5 min. OFF
2nd through 5th -- Max 30 sec. ON, followed by 5 min. OFF
(After 5 attempts, may be repeated following 15 min. cooldown period)
98
Starter Time Limits
1st and 2nd -- Max 90 sec. (ground) / 120 sec. (flight) ON, following by 10 sec. OFF
3rd through 5th -- Max 90 sec. (ground) / 120 sec. (flight) ON, followed by 5 min. OFF
