Limitations Flashcards

1
Q

Maximum landing weight?

A

74,957 lbs

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2
Q

Max Takeoff and Landing Tailwind Component

A

10 knots

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3
Q

Max Operating Altitude

A

41,000 feet

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4
Q

Max Operating Altitude

A

41,000

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5
Q

Max Flap Extension Altitude

A

20,000 feet

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6
Q

Max Operating Airspeed

A

Vmo

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7
Q

Max Operating Mach Number

A

Mmo (.82M)

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8
Q

Types of Operations

A
VFR
IFR
NIGHT
ICING
CATI
CAT II
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9
Q

Turbulent airspeed below 10,000 feet?

A

250KIAS

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10
Q

Turbulent airspeed at or above 10,000 feet

A

270 KIAS

.76M

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11
Q

Max ramp weigh?

A

85,870

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12
Q

Max takeoff weight?

A

85,517

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13
Q

Max landing weight?

A

74,957

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14
Q

Max zero fuel weight?

A

69,886

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15
Q

Flap maneuvering load acceleration limits:

A

Flaps up -1.0 G to +2.5G

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16
Q

Flap maneuvering load acceleration limits:

Flaps down

12345 and full

A

-0 G to +2.0 G

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17
Q

Takeoff and landing max and min

A

8000’

-1000’

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18
Q

Max ambient air temperature for takeoff and landing

A

52 deg C

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19
Q

Max flap extension altitude?

A

20,000’

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20
Q

Maximum latitude for stationary alignment ?

A

78.25 N to 78.25 S

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21
Q

Min ambient temperature approved for takeoff?

A

-40 deg C (SAT)

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22
Q

Minimum Ambient Temperature for operation?

A

-54 deg C

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23
Q

Min ambient temp for operation?

A

-54 deg C (SAT)

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24
Q

Maximum windshield wiper operation speed?

A

253 KIAS

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25
Maximum gear speed?
EXTENTION (VLOE). 250 KIAS EXTENDED (VLE). 250 KIAS RETRACTION (VLOR). 250KIAS
26
Flaps 1
230 KIAS
27
Flaps 2
215 KIAS
28
Flaps 3
200 KIAS
29
Flaps 4
180 KIAS
30
Flaps 5
180 KIAS
31
Flaps full
165 KIAS
32
Max operating speed up to 8000'
300 KIAS
33
Flaps full
165
34
Max operating speed 8000' to 10,000
300 to 320 KIAS (increases linearly)
35
10,000 ' to FL290
320 KIAS (VMO)
36
FL290 to FL410 max operating speed?
.82M
37
Definition of icing conditions
Whenever the outside air temperature (OAT) on the ground or for takeoff, or Total Air Temperature (TAT) inflight, is 10 deg C or below and visible moisture in any form is present (such as clouds, fog with visibility of one mile or less, rain, snow, sleet and ice crystals).
38
Maximum Fuel Capacity (total)
20,935 lbs (10,392.5 lb or 1535.5 U.S. Gal per tank)
39
Unusable Quantity per tank
75 lbs/US Gal per tank
40
Max fuel imbalance ?
794
41
Minimum fuel tank temperature?
-40 deg C
42
Crossfeed operations must be ?
Off during takeoff and landing
43
Max differential pressure up to 37000'?
7.8 psi
44
Max differential pressure above 37,000'?
8.34 psi
45
Max differential overpressure?
8.77 psi
46
Maximum differential negative pressure
-0.5 psi
47
Maximum differential pressure for takeoff and landing
0.2 psi
48
Max altitude for single pack operation
FL 310
49
Do not take off with brake temperatures in the
Amber
50
Thrust Reversers:
Ground use only Not authorized while taxiing Full stop landings Do not attempt go-around after deployment Power back is prohibited Min REV thrust with the Translating Cowl open below 60 KIAS Idle thrust with the Translating Cowl closed @ 30kts
51
AUTOPILOT | Minimum Engagement height on takeoff ?
``` 1000 feet (Mesa) 400 feet (aircraft) ```
52
Autopilot minimum use height for coupled ILS approach?
50 feet
53
What type of engine is on the E175?
CF34-8E5
54
How long is takeoff thrust time limited to? | CF34-8E5
10 minutes
55
N1
99.5%
56
N2 Minimum
58.6%
57
N2 Maximum
99.4%
58
ITT start
815 deg C
59
Max takeoff and go around | After first 2 minutes
990 deg C | From 2 minutes to 10 min
60
Max takeoff and go around (2 minutes)
1006 deg C During the first 2 minutes
61
ITT max continuous 960 deg C
Oil pressure minimum
62
Oil pressure minimum
25 PSI
63
Oil pressure maximum
95 PSI
64
Oil temperature continuous
155 deg C
65
Oil temperature transient
163 deg C | Transient operation above 155 deg C limited to 15 minutes
66
EICAS markings
Red. --- max and minimum limitations Amber --- caution range Green --- normal operating range
67
FLEX reduction:
Must not exceed 25% of the full takeoff thrust
68
When is FLEX prohibited?
On contaminated runways
69
ATTCS must be on for
All takeoffs and landings