E175 Limitations/Memory Items Flashcards
1
Q
Aircraft length
A
103’ 11” (104’)
2
Q
Aircraft width
A
93’ 11” (94’) (Wingspan)
3
Q
Aircraft height
A
32’ 4” (33’)
4
Q
Max PAX
A
76 (12 First/64 Coach)
5
Q
Max cargo weights
A
FWD 3307 lbs
AFT 2535 lbs
6
Q
Maximum ramp weight
A
85,800 lbs
7
Q
Maximum takeoff weight (structural)
A
85,500 lbs
8
Q
Maximum landing weight (structural)
A
74,900 lbs
9
Q
Maximum zero fuel weight
A
69,800 lbs
10
Q
Minimum crew
A
2 pilots (left/right seat)
11
Q
Aircraft operations
A
Day/night
VFR/IFR
Icing conditions
CAT I/CAT II
RVSM
Extended Overwater Operation (when EOW equipped)
12
Q
Max cabin differential overpressure (safety valve)
A
8.8 PSI
13
Q
Max cabin differential pressure above FL 370
A
8.4 PSI
14
Q
Max cabin differential pressure for T/O and landing
A
0.2 PSI
15
Q
Max cabin Negative differential pressure
A
-0.5 PSI
16
Q
Max altitude depressurized
A
10,000’ or MEA whichever is higher
17
Q
Max altitude for single pack operation
A
31,000’
18
Q
Mmo (above FL280)
A
.82M
19
Q
Vmo (above 10,000’ to FL280)
A
320 KIAS
20
Q
Vmo (below 10,000’) (FAA and structural)
A
250 KIAS FAA regulatory
300 KIAS Structural
21
Q
Va
A
240 KIAS
22
Q
Vle
A
250 KIAS
23
Q
Vlo
A
250 KIAS
24
Q
Vlr
A
250 KIAS
25
Vfe1
230 KIAS
26
Vfe2
215 KIAS
27
Vfe3
200 KIAS
28
Vfe4
180 KIAS
29
Vfe5
180 KIAS
30
Vfefull
165 KIAS
31
Max turbulent airspeed (below 10,000')
250 KIAS
32
Max turbulent airspeed (10,000' and above)
270 KIAS or .76M
33
Max crosswind for takeoff (dry and wet)
Dry 35 kts
Wet 30 kts
34
Max crosswind for takeoff (RWYCC 4)
20 kts
35
Max crosswind for takeoff (RWYCC 3)
15 kts
36
Max crosswind for landing (RWYCC 6)
38 kts
37
Max crosswind for landing (RWYCC 5)
31 kts
38
Max crosswind for landing (RWYCC 4)
20 kts
39
Max crosswind for landing (RWYCC 3)
15 kts
40
Max crosswind for landing (RWYCC 2)
12 kts
41
Max crosswind for landing (RWYCC 1)
8 kts
42
Max crosswind for landing (RWYCC 0)
OPERATIONS PROHIBITED
43
Unless otherwise required by operational restrictions such as CAT II, MEL, or emergency/abnormal procedures, all landings on runways with an RCC less than 5/5/5 must be at what flap setting?
Flaps FULL
44
Max tailwind
10 kts
45
Max headwind for CAT II
25 kts
46
Max crosswind for landing (RVR less than 4000 or 3/4 mile)
15 kts
47
Max DV window operation speed
160 KIAS
48
Max tire speed
195 KIAS
49
Max windshield wiper speed
250 KIAS
50
Max operating altitude
41,000'
51
Max altitude with flaps extended
20,000'
52
Max altitude for takeoff and landing
10,000'
53
Minimum altitude for takeoff and landing
- 1,000'
54
Min SAT for takeoff or landing
- 40 deg C
55
Max SAT for takeoff or landing
54 deg C
56
Max altitude display difference in flight for RVSM
180'
57
In the event of a landing below ____ , takeoff not authorized without further maintenance inspection
- 40 deg C
58
APU model
Sundstrand APS 2300
59
APU starter limitations
First and second attempts
Third attempt
START/ON then 60 sec OFF
START/ON then 5 min OFF
60
Minimum starting temperature for APU
- 54 deg C
61
Max APU operation temperature
ISA + 39 deg C (supplemental info applicable at ISA + 35 deg C)
62
Max EGT APU start
1032 deg C
63
Max EGT APU continuous
is there a time limit ground/inflight between 662-717 deg C (amber range)
717 deg C
No time limit between 662-717 deg C (amber range)
64
Max APU rotor speed
108%
65
Max altitude for APU electrical power
33,000'
66
Max altitude for APU start
30,000'
67
Max altitude for ENG start assist with APU
21,000'
68
Max altitude for APU bleed air
15,000'
69
Minimum altitude for autopilot engagement (takeoff/go around)
Above 400'
70
Minimum altitude with autopilot engaged during landing
above 50'
71
Engine model
GE CF34-8E5
72
Max N1 RPM
99.5%
73
Max N2 RPM
99.4%
74
Max start ITT
815 deg C
75
Max normal T/O ITT
965 deg C (2 min)
949 deg C (3 min) [Total 5 min]
76
Max T/O & G/A ITT
1006 deg C (2 min)
990 deg C (3 min) [Total 5 min]
77
Max continuous ITT
960 deg C
78
Min oil pressure
25 PSI
79
Max oil pressure
95 PSI
80
Max continuous oil temp
155 deg C
81
Max transient Oil temp
163 deg C (15 min limit)
82
T/O-1 engine thrust
13,000 lbs
ATTCS 14,200 lbs
83
T/O-2 engine thrust
11,800 lbs
ATTCS 13,000 lbs
84
Fuel types
Jet A or A1
JP8
QAV1 (Brazilian)
85
Max fuel capacity
20,934 lbs (10,467 lbs/tank)
86
Max useable fuel
20,784 lbs (10,392 lbs/tank)
87
Unusable fuel
150 lbs (75 lbs/tank)
88
Max fuel imbalance
794 lbs
89
Minimum fuel temperature
-37 deg C
90
Can you crossfeed fuel during takeoff or landing?
NO
91
1st and 2nd engine start limits
on ground-90 sec START/10 sec cool-down
in flight-120 sec START/10 sec cool-down
92
3rd-5th attempts engine start limits
on ground- 90 sec START/5 min cool-down
in flight-120 sec START/5 min cool-down
93
Dry motoring limits
1st dry motor-Max 90 sec followed by 5 min cool-down
2nd-5th dry motor-Max 30 sec followed by 5 min cool-down
94
After __ sequential dry motoring cycles, the sequence may be repeated following a __ min cool-down period.
5, 15 min
95
CABIN ALTITUDE HI/RAPID Depressurzation
Oxygen masks.....CR.....ON, 100%
96
Jammed Control Column - Pitch
Elevator Disconnect.....CR.....PRESS and PULL
97
Jammed Control Wheel - Roll
Aileron Disconnect.....CR.....PRESS and PULL
98
Pitch Trim Runaway
AP/TRIM Disconnect.....PRESS and HOLD
TRIM PITCH SYS 1 & 2 CUTOUT.....Push IN
99
(Roll or Yaw) Trim Runaway
AP/TRIM Disconnect.....PRESS and HOLD
100
Nosewheel Steering Runaway
Steering Disconnect.....PRESS
101
Aborted Engine Start
Associated Thrust Lever.....IDLE
Associated START/STOP.....STOP
102
Application of reverse thrust is not permitted at airspeeds below __ KIAS during normal operations.
60 KIAS
103
Can you single engine taxi with an inoperative APU?
NO
104
Dry Ice limit
50 lbs in forward compartment only
CAUTION-Not all E170s have forward cargo ventilation fans
dry ice/live animals are prohibited in these aircraft
105
For operations at or above _____’ pressure altitude OR ISA ___ degrees and above, T/O-1 thrust is required.
8,000’
ISA +35
