E175 Limitations Flashcards
1
Q
Aircraft Length
A
103’ 11”
2
Q
Aircraft Width
A
93’ 11”
3
Q
Aircraft Height
A
32’ 4”
4
Q
Max PAX
A
76
5
Q
First class seats
A
12
6
Q
Coach seats
A
64
7
Q
Cargo FWD compartment weight limit
A
3,307 lbs.
8
Q
Cargo AFT compartment weight limit
A
2,535 lbs.
9
Q
Aircraft Weight: MRW
A
85,870 lbs.
(85,800)
10
Q
Aircraft Weight: MTOW
A
85,517 lbs.
(85,500)
11
Q
Aircraft Weight: MLW
A
74,957 lbs.
(74,900)
12
Q
Aircraft Weight: MZFW
A
69,886 lbs.
(69,800)
13
Q
Minimum Crew
A
Left seat pilot & Right seat pilot
14
Q
Aircraft Operations
A
- Day & Night
- VFR & IFR
- Icing Conditions
- CAT I & CAT II
- RVSM
- Extended Overwater Operation (EOW equipped)
15
Q
Max Cabin Differential Overpressure:
A
8.8 psi
16
Q
Max Cabin Differential Pressure (Above FL370):
A
8.4 psi
17
Q
Max Cabin Differential for Takeoff & Landing
A
0.2 psi
18
Q
Max Cabin Differential Negative Pressure
A
-0.5 psi
19
Q
Max Altitude Depressurized
A
10,000’ or MEA whichever is higher
20
Q
Mmo (Above FL280)
A
0.82
21
Q
Vmo (Above 10,000’ to FL280)
A
320 KIAS
22
Q
Vmo (Below 10,000’)
A
FAA - 250 KIAS
Structural - 300 KIAS
23
Q
Va
A
240 KIAS
24
Q
Vle
A
250 KIAS
25
Vlo
250 KIAS
26
Vlr
250 KIAS
27
Vfe1
230 KIAS
28
Vfe2
215 KIAS
29
Vfe3
200 KIAS
30
Vfe4
180 KIAS
31
Vfe5
180 KIAS
32
Vfefull
165 KIAS
33
Max Turbulent Airspeed (Below 10,000’)
250 KIAS
34
Max Turbulent Airspeed (10,000’ and Above)
270 KIAS or .76 Mach (whichever is higher)
35
Max Crosswind for Takeoff (Dry)
35 kts
36
Max Crosswind for Takeoff (Wet)
30 kts
37
Max Tailwind
10 kts
38
Max DV Window Operation
160 KIAS
39
Max Tire Speed
195 KIAS
40
Max Windshield Wiper Speed
250 KIAS
41
Max Operating Altitude
41,000’
42
Max Altitude with Flaps Extended
20,000’
43
Max Takeoff & Landing (alt)
10,000’
44
Min Takeoff & Landing (alt)
-1,000’
45
Min Takeoff & Landing Temperature (SAT)
-40°C
46
Max Takeoff & Landing Temperature (SAT)
52°C
47
Max altitude display difference in flight for RVSM
180’
48
In the event of a landing below \_\_\_\_\_°C, …
-40°C, the Airplane may not takeoff without further maintenance inspection.
49
APU (brand)
Sundstrand APS 2300
50
APU First & Second Start Attempts
START/ON then 60 sec. OFF
51
APU Third Start Attempt
START/ON then 5 min. OFF
52
APU Minimum Operation Temperature
-54°C
53
APU Maximum Operation Temperature
ISA + 35°C
54
APU EGT (Start)
1032°C
55
APU EGT (Continuous)
717°C
56
APU: No time limit in amber on the ground/inflight from ____ to \_\_\_\_
662°C to 717°C
57
APU Max Operation Altitude (Electrical)
33,000’
58
APU Max Start Altitude
30,000’
59
APU Max Operation Altitude (Eng. Start Assist)
21,000’
60
APU Max Operation Altitude (ECS Bleed)
15,000’
61
APU Max Rotor Speed
108%
62
AP Minimum Engagement Altitude on Takeoff or Go Around
Above 400’
63
AP minimum Engaged Altitude during Landing
Above 50’
64
Engine (Model)
GE CF34-8E5
65
Engine: N1 RPM Max
99.5%
66
Engine: N2 RPM Max
99.4%
67
Engine: Max Start ITT
815°C
68
Engine: Max Normal T/O ITT
965°C (2 min.)
949°C (3 min.) [Total: 5 min.]
69
Engine: Max T/O & G/A ITT
1006°C (2 min)
990°C (3 min.) [Total: 5 min.]
70
Engine: Max Continuous ITT
960°C
71
Engine: Min Oil Pressure
25 psi
72
Engine: Max Oil Pressure
95 psi
73
Engine: Continuous Oil Temperature (Max)
155°C
74
Engine: Transient Oil Temperature (Max)
163°C (15 min. limit)
75
Engine: Thrust (T/O-1)
13,000 lbs.
76
Engine: Thrust (T/O-1) (OEI ATTCS)
14,200 lbs.
77
Engine: Thrust (T/O-2)
11,800 lbs.
78
Engine: Thrust (T/O-2) (OEI ATTCS)
13,000 lbs.
79
Fuel (Brazilian)
QAV1
80
Fuel (ATSM)
Jet A or A1
81
Fuel (MIL-T)
JP8
82
Maximum Fuel Capacity
20,934 lbs. (10,467 per tank)
83
Maximum Useable Fuel Quantity
20,784 lbs. (10,392 per tank)
84
Unusable Fuel Quantity
150 lbs. (75 per tank)
85
Maximum Fuel Imbalance
794 lbs.
86
Adopted Fuel Density
6.77 lbs./US Gal.
87
Minimum Fuel Tank Temperature
-37°C
88
Crossfeed Operation Limitation
Crossfeed Knob must be OFF for Takeoff and Landing
89
Starter: 1st Dry Motor
Max 90 sec. (5 min. Cool-Down)
90
Starter: 2nd to 5th Dry Motor
Max 30sec. (5 min. Cool-Down)
91
Starter: After 5 sequential Dry Motors, the cycle may be repeated following a ____ min. Cool-Down period.
15 min.
92
Starter: 1st & 2nd Start (Grd)
90 sec. (With 10 sec. Cool-down)
93
Starter: 1st & 2nd Start (Flt)
120 sec. (With 10 sec.Cool-down)
94
Starter: 3rd to 5th Start (Grd)
90 sec (with 5 min. Cool-down)
95
Starter: 3rd to 5th Start (Flt)
120 sec. (With 5 min. Cool-down)
96
Flaps Up Min Speed
210
97
Flaps 1 Min Speed
180
98
Flaps 2 Min Speed
160
99
Flaps 3 Min Speed
150
100
Flaps 4/5 Min Speed
140
101
Flaps Full Min Speed
Vapp
102
Engine: N2 RPM Min.
58.5%
103
Wing/Engine Strikes During Landing. Angle:
18º at touchdown
16° with gear struts compressed
104
Max Crosswind Landing (Code 6)
38
105
Max Crosswind Landing (Code 5)
31
106
Max Crosswind Landing (Code 4)
20
107
Max Crosswind Landing (Code 3)
15
108
Max Crosswind Landing (Code 2)
12
109
Max Crosswind Landing (Code 1)
8
110
Max Crosswind Takeoff (Dry)
35
111
Max Crosswind Takeoff (Wet)
30
112
Max Crosswind Takeoff (Compacted Snow)
20
113
Max Crosswind Takeoff (Standing Water)
18
114
Max Crosswind Takeoff (Slush)
18
115
Max Crosswind Takeoff (Wet Snow)
18
116
Max Crosswind Takeoff (Dry Snow)
18
117
Max Crosswind Takeoff (Ice)
12
118
Max Crosswind for Landing in Vis less than 4000 or 3/4
15
