Limitations Flashcards
(95 cards)
1
Q
Types of Operations
A
- VFR
- IFR
- Icing conditions
- CAT I
- CAT II
- RVSM
- EOW; E175 when properly equipped
SOP 3-2
2
Q
Max ramp weight
A
82,364
SOP 3-3
3
Q
Max Takeoff weight
A
82,011
SOP 3-3
4
Q
Max landing weight
A
72,310
SOP 3-3
5
Q
Max zero fuel weight
A
65,256
66,446 for N646RW and above
SOP 3-3
6
Q
Min crew
A
pilot and copilot
SOP 3-4
7
Q
Max t/o and landing tailwind
A
10 knots
SOP 3-4
8
Q
Max runway slope
A
+/- 2.0 %
SOP 3-4
9
Q
Runway surface type
A
Paved
SOP 3-4
10
Q
Flaps up maneuvering G load
A
-1.0G to +2.5G
SOP 3-4
11
Q
Flaps down maneuvering G load
A
0.0G to +2.0G
SOP 3-4
12
Q
Max operating altitude
A
41,000 ft
SOP 3-4
13
Q
Max T/O and landing altitude
A
8,000 ft
SOP 3-4
14
Q
Max ambient temp t/o and landing
A
+52C
SOP 3-4
15
Q
TAS, TAT and SAT valid above speed
A
60 knots
SOP 3-13
16
Q
Mag compass not valid when…
A
Transmitting on VHF #1
SOP 3-13
17
Q
All CAT I approaches must use…
A
BARO altimeter mins
SOP 3-13
18
Q
Back course ILS prohibited when…
A
On IESS
SOP 3-13
19
Q
A/P min engagement height for takeoff
A
400 ft
SOP 3-18
20
Q
A/P min height for approach on coupled ILS
A
50 ft
SOP 3-18
21
Q
Max operating airspeed
A
VMO
tbd
22
Q
Max operating mach number
A
.82M (MMO)
tbd
23
Q
Max A/S for RAT operation
A
VMO/MMO
tbd
24
Q
Turbulent air A/S below 10,000ft
A
250KIAS
SOP 3-6
25
Turbulent air A/S above 10,000 ft
270KIAS
.76M
SOP 3-6
26
Max tire ground speed
195 knots
SOP 3-6
27
Max windshield wiper operation speed
250 KIAS
SOP 3-9
28
Max gear extension/extended/retraction speed
250 KIAS
SOP 3-6
29
Design maneuvering speed
240 KIAS
SOP 3-8
30
VFE1 (structural/republic)
230 KIAS
To extend the life of the flaps, the flaps should be extended as much as possible below max flap extension speed, but in no case below green dot
SOP 3-6
31
VFE2 (structural/republic)
215 KIAS
To extend the life of the flaps, the flaps should be extended as much as possible below max flap extension speed, but in no case below green dot
SOP 3-6
32
VFE3 (structural/republic)
200 KIAS
To extend the life of the flaps, the flaps should be extended as much as possible below max flap extension speed, but in no case below green dot
SOP 3-6
33
VFE4 (structural/republic)
180 KIAS
To extend the life of the flaps, the flaps should be extended as much as possible below max flap extension speed, but in no case below green dot
SOP 3-6
34
VFE5 (structural/republic)
180 KIAS
To extend the life of the flaps, the flaps should be extended as much as possible below max flap extension speed, but in no case below green dot
SOP 3-6
35
VFE full (structural/republic)
165 KIAS
To extend the life of the flaps, the flaps should be extended as much as possible below max flap extension speed, but in no case below green dot
SOP 3-6
36
Max operating speed SL-8,000ft
300 KIAS
SOP 3-7
37
Max operating speed 8K-10K
300-320 KIAS
SOP 3-7
38
Max operating speed 10K-FL290
320 KIAS
SOP 3-7
39
Max operating speed FL290-FL410
.82M
SOP 3-7
40
Definition of icing conditions
When SAT on ground or TAT in flight is:
1. 10C or below; and
2. Visible moisture is present in any form, such as clouds, fog with vis
41
Engine and wing anti-ice system operation on ground
During taxi and takeoff the MCDU DATASET MENU must be set to ALL when SAT is 10C or below and icing conditions exist or are anticipated
SOP 3-9
42
Engine and wing anti-ice systems operations in flight
The engine and wing anti-ice systems operate automatically in case of ice encounter when the ICE PROTECTION Mode Selector is in AUTO. If either one or both ice detectors are failed, the crew must set the mode selector to ON when icing conditions exist or are anticipated at or below 10°C TAT with visible moisture.
SOP 3-9
43
Max fuel capacity
20,935 lbs
SOP 3-10
44
Unusable fuel quantity per tank
75 lbs
SOP 3-10
45
Min fuel tank temp
-40C
SOP 3-10
46
Max fuel imbalance
790 lbs
SOP 3-10
47
X-Feed operations for t/o and landing
Must be set to OFF
SOP 3-10
48
Max differential pressure up to 37,000ft
7.8 PSI
SOP 3-11
49
Max differential pressure 37,000-41,000 ft
8.3 PSI
SOP 3-11
50
Max differential overpressure
8.7 PSI
SOP 3-11
51
Max differential negative pressure
-0.5 PSI
SOP 3-11
52
Max differential pressure for t/o and landing
0.2 PSI
SOP 3-11
53
Max altitude single pack operation
31,000 ft
SOP 3-11
54
Max flap extension altitude
20,000 ft
SOP 3-12
55
Thrust reverser limitations
a. Ground use only
b. Rejected takeoffs and full stop landings only
c. Do not attempt go-around after deployment
d. Power-back prohibited
e. Must be stowed below 60KIAS
f. After use, do not move TLs to forward range until REV turns amber or green on EICAS
SOP 3-12
56
Max APU rotor speed (%)
108%
SOP 3-23
57
Max APU ITT start
1032C
SOP 3-23
58
Max APU continuous ITT
717C
SOP 3-23
59
Max APU start altitude
30,000ft
SOP 3-23
60
Max APU electrics-only altitude
33,000 ft
SOP 3-23
61
Max APU electric and pneumatics altitude
15,000 ft
SOP 3-23
62
Max APU assist engine start altitude
21,000ft
SOP 3-23
63
Min outside APU operation temp
-62C
SOP 3-23
64
Max outside APU operation temp
ISA +35C
SOP 3-23
65
APU starter duty cycle
2 X (60 on, 60 off) + 60 on, 5 mins off
SOP 3-23
66
Do not takeoff when brake temp is...
In the amber range
67
Max CAT II x-wind
12 knots
SOP 3-19
68
Are manual FD director CAT II approaches authorized?
No
SOP 3-19
69
Max N1 speed
99.5%
SOP 3-20
70
Min N2 speed
58.5%
SOP 3-20
71
Max N2 speed
99.4%
SOP 3-20
72
Max engine start ITT
815C
SOP 3-20
73
Max engine inflight start ITT
815C
SOP 3-20
74
Max NORMAL engine TOGA ITT and time limits
965C for 1st 2 mins, then:
949C for following 3 mins
SOP 3-20
75
Max MAX TOGA ITT and time limits
1006C for 1st 2 mins, then:
990C for following 3 mins
SOP 3-20
76
Max continuous engine ITT
960C
SOP 3-20
77
Engine oil pressure range
25-95PSI
SOP 3-20
78
Max continuous engine oil temp
155C
SOP 3-20
79
Max transient oil temp
163C for up to 15 mins
SOP 3-20
80
EICAS color markings
Red - max and min limitations
Amber - caution range
Green - normal operating range
SOP 3-21
81
Max thrust reduction with FLEX
25%
SOP 3-21
82
When is FLEX prohibited?
On runways contaminated with standing water, slush, snow, or ice and are not allowed on wet runways unless suitable performance accountability is made for the increased stopping distance.
SOP 3-21
83
Engine starter duty cycle on ground
1st and 2nd attempt: 90 sec ON, 10 secs OFF
3rd-5th attempts: 90 secs ON, 5 mins OFF
SOP 3-22
84
Engine start duty cycle in flight
1st and 2nd attempt: 120 secs ON, 10 secs OFF
3rd-5th attempt: 120 secs ON, 5 mins OFF
SOP 3-22
85
Engine start dry motoring duty cycle
1st attempt: 90 secs ON, 5 mins OFF
2nd-5th attempt: 30 secs ON, 5 mins OFF
after 5th attempt: 15 mins OFF
SOP 3-22
86
What are the five factors that can limit takeoff weight?
1. Max takeoff weight (climb limited)
2. Max field length limited takeoff weight
3. Max certified takeoff weight
4. Obstacle clearance, enroute and landing limitations
5. Brake energy limit weights
SOP 3-2
87
What factors determine max landing weight?
1. Max approach and landing weight (runway length plus obstacle, altitude, and temp and including limitations for inoperative equipment)
2. Max landing weight (climb limited)
3. Max certified landing weight
SOP 3-2
88
Forward cargo compartment weigh limit
3,020 lbs
SOP 3-3
89
Aft cargo compartment weight limit
3,307 lbs
SOP 3-3
90
Max recommended crosswind, all conditions
```
Dry - 38 KIAS
Wet - 31 KIAS
Compact snow - 20 KIAS
Standing water/Slush - 18 KIAS
Wet ice - 12 KIAS
```
SOP 3-4
91
Max direct vision window opening speed
160 KIAS
92
Other than speed and altitude, what are the flap operating limitations?
No enroute use, no holding in icing conditions with flaps extended, do not use flaps 4 for approach and landing
93
RVSM Min Equipment Required
- 2 ADS
- 1 Autopilot, engaged, with ALT mode operative
- 1 Altitude Alerter
- 1 Transponder
SOP 3-14
94
Under what conditions is ADS 3 non-RVSM compliant?
In case of loss of sideslip compensation. "ADS3 SLIPCOMP FAIL")
SOP 3-14
95
A ___ cool down must be observed prior to shutting down an engine
2 minute
SOP 3-20
