EJET - Limitations (AQP) Flashcards

(118 cards)

1
Q

Max Ramp Weight (LR)

A

85,870 lbs

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2
Q

Max Takeoff Weight (LR)

A

85,517 lbs

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3
Q

Max Landing Weight (LR)

A

74,957 lbs

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4
Q

Max Zero Fuel Weight (LR)

A

69,886 lbs

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5
Q

Max Ramp Weight (LL)

A

85,450 lbs

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6
Q

Max Takeoff Weight (LL)

A

85,098 lbs

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7
Q

Max Landing Weight (LL)

A

74,957 lbs

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8
Q

Max Zero Fuel Weight (LL)

A

69,467 lbs

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9
Q

FWD Baggage Compartment Max Load?

A

3,306 lbs

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10
Q

AFT Baggage Compartment Max Load?

A

2,535 lbs

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11
Q

Max Operating Altitude?

A

41,000 feet

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12
Q

Max Operating Speed 8,000-10,000 feet?

A

300-320 knots (increases linearly)

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13
Q

Max Altitude for Takeoff, Landing, Ground start?

A

10,000 feet

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14
Q

Landing below ____ degrees C, may not takeoff again until further maintenance inspection

A
  • 40 degrees C (SAT)
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15
Q

Minimum Takeoff and Landing Altitude

A

-1,000 feet

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16
Q

Min Ambient temperature for operation

A
  • 54 degrees C (SAT)
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17
Q

Max Ambient temperature for takeoff and landing

A

52 degrees C

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18
Q

Maximum Altitude for Flap Extension

A

20,000 feet

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19
Q

Max Landing Gear retraction speed (Vlo - retract)

A

250 kts

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20
Q

Max Landing Gear extension speed (Vlo - extension)?

A

250 kts

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21
Q

Max Landing Gear extended speed (Vle)

A

250 kts

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22
Q

Maximum speed to open the direct vision window?

A

160 kts

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23
Q

Max Operating Speed

A

Vmo/Mmo

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24
Q

Max Operating Speed up to 8,000 feet?

A

300 knots

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25
Max Operating Speed from 10,000 feet to FL 290?
320 knots (Vmo)
26
Max Operating Speed FL 290-410?
0.82 mach (Mmo)
27
Max Operating mach?
Mmo (0.82 mach)
28
What is Vfe - 1?
230 kts
29
What is Vfe - 2?
215 knots
30
What is Vfe - 3?
200 Knots
31
What is Vfe - 4?
180 Knots
32
What is Vfe - 5?
180 Knots
33
What if Vfe - FULL?
165 Knots
34
Maximum Tire Ground Speed?
195 knots
35
Maximum Takeoff and Landing Tailwind?
10 knots
36
Maximum recommended takeoff crosswind for - DRY RUNWAY?
38 Knots
37
Maximum recommended takeoff crosswind for - WET RUNWAY?
31 Knots
38
Maximum recommended takeoff crosswind for - COMPACTED SNOW?
20 Knots
39
Maximum recommended takeoff crosswind with STANDING WATER/SLUSH/WET SNOW/DRY SNOW?
18 knots
40
Maximum recommended takeoff crosswind with ICE (including WET ICE)?
12 knots
41
Max recommended crosswind for static takeoff?
25 knots
42
What is the maximum recommended crosswind landing for DRY runway?
38 knots
43
What is the maximum recommended crosswind speed for landing with GOOD runway - 5/5/5 code?
31 knots
44
What is the maximum recommended crosswind landing speed for condition 4/4/4 - compacted snow?
20 knots
45
What is the maximum recommended crosswind speed for landing with code 3/3/3 - wet runway?
15 knots
46
What is the maximum recommended crosswind speed for landing with code 2/2/2 - wet/slush more than 1/8th inch depth?
12 knots
47
What is the maximum recommended crosswind speed for landing with code 1/1/1 - ICE?
8 knots
48
What is the maximum recommended crosswind for landing with code 0/0/0 braking action NIL?
No operations allowed
49
Flap maneuvering load acceleration limits for flaps up/flaps down
Flaps Up = -1.0g to 2.5g | Flaps Down = 0.0g to 2.0g
50
Max runway slope
+/- 2%
51
What is the approved runway surface type?
Paved
52
Max Fuel Capacity?
20,935 lbs | Per tank 10,392.5 lbs per tank or 1,535.5 gallons
53
Unusable Fuel Quantity per tank?
75 lbs (11 gallons)
54
Maximum permitted fuel imbalance between tanks?
794 lbs (roundest to nearest 800 lbs)
55
Minimum Fuel Tank Temperature
-37 degrees C
56
Limitation on takeoff and cross feed operation “Crossfeed Operations must be ___ for takeoff and landing”
OFF
57
What is the make and model of the APU for the E-175?
Sundstrand APS 2300
58
Min Temperature for APU start?
-54 degrees C
59
Max altitude for APU START (in-flight)?
30,000 feet
60
Max altitude for APU Operation?
33,000 feet
61
Max Altitude for APU (Electrical Load), if used for electrics?
33,000 feet
62
Max altitude for APU operation if used for Bleed Air?
15,000 feet
63
Max altitude for APU when used to assist for engine starting?
21,000 feet
64
Max Rotor Speed of the APU?
108%
65
Max Continuous EGT for APU?
717 degrees C
66
Max EGT for APU Start?
1,032 degrees C
67
APU Starter Cooling Period * Attempts 1, 2* * Attempts 3*
*Attempts 1, 2* 1 min ON, 1 min OFF *Attempts 3* 1 min ON, 5 min OFF
68
Max N1 with brakes applied?
60%
69
What kind of engine does the E175 have?
General Electric CF34-8E5
70
What is the time limit for takeoff thrust on the CF34-8E5 engine?
10 minutes
71
What is the max N1 speed?
99.5%
72
What is the Minimum N2 speed?
58.5%
73
What is the maximum N2 speed?
99.4%
74
What is max ITT for engine start (engine start limitation)?
815 degrees C (limited to 10 minutes)
75
Max takeoff and go around ITT?
990 degrees C (Can be exceeded up to 1,006 degrees C for 2 minutes) *Time limited to 5 minutes with all engines operative, 10 minutes with single engine*
76
Max continuous ITT
960 degrees C
77
Minimum Oil Pressure?
25 PSI
78
What is maximum oil pressure?
95 PSI
79
Maximum Continuous Engine Oil Temperature?
155 degrees C
80
What is the Maximum Engine Oil Transient Temperature?
163 degrees C (above 155 degrees, limited to 15 minutes)
81
Dry Motoring Duty Cycle Limits: * Attempt 1* * Attempt 2-5*
Attempt 1: 90 Seconds ON, 5 Minutes OFF Attempt 2-5: 30 Seconds ON, 5 Minutes OFF *NOTE* After 5 sequential motorings, cycle may be repeated following a 15 minute cool down
82
Engine Starter Duty Cycle Limits, Ground vs. In-Flight? * Attempt 1 and 2* * Attempt 3-5*
Attempts 1-2: 90 Seconds ON, 10 Seconds OFF Attempts 3-5: 90 Seconds ON, 5 Minutes OFF *IN-FLIGHT* BOTH are 120 Seconds ON
83
FLEX Limitations
1. FLEX reduction must not exceed 25% of the full takeoff thrust 2. FLEX is prohibited on contaminated runways 3. ATTCS (Automatic Takeoff Thrust Control System) must be ON for both takeoffs and landings
84
Maximum Differential Pressure?
8.4 PSI
85
Maximum Differential Overpressure?
8.8 PSI
86
Maximum Differential Negative Pressure
- 0.5 PSI
87
Maximum Differential Pressure for Takeoff and Landing?
0.2 PSI
88
Max Altitude for Single Pack Operations?
31,000 feet
89
On ground between ___ and ___ the TO DATA SET MENU on the MCDU must be set to ___ when 1. ) If there is a possibility when encountering visible moisture up to 1,700 AFE 2. ) When operating on ramps, taxiways, runways where surface snow, ice standing water or slush may get into the engine nacelles ingested or freeze on engines nacelles and probes
5 degrees C and 10 degrees C | ENG
90
On ground when OAT is below ___ the TO DATA SET MENU on the MCDU must be set to ___ when 1. ) If there is a possibility when encountering visible moisture up to 1,700 AFE 2. ) When operating on ramps, taxiways, runways where surface snow, ice standing water or slush may get into the engine nacelles or freeze on the engine nacelles and probes
5 degrees C, ALL
91
Engine/Wing Anti-Ice system operates automatically in ice encounters when the ___ selector is in the ___ position If either one or both ice detectors fail crew must select the ___ selector to the ___ position
MODE, AUTO | MODE, ON
92
Definition of Icing Conditions?
When on the ground or for Takeoff the temperature (OAT) is 10 degrees C, or inflight TAT is 10 degrees C or lower With visible moisture present with visibility of less than 1 mile
93
Maximum Airspeed for Windshield Wiper Operation?
253 Knots
94
Autopilot Minimum Engagement Height (Takeoff) *PER MESA CFM*
1,000 feet AGL
95
Autopilot Minimum Use Height (Coupled ILS Approach)
50 feet AGL
96
When is TAS, TAT, SAT information valid?
Only above 60 Knots
97
What is the limitation pertaining to transmitting with VHF 1?
Standby magnetic compass indication is not valid
98
What is the limitation pertaining to LOC BACK Course approaches?
LOC back course approaches are not authorized with use of the IESS (Integrated Electronic Standby System)
99
Max Latitude for stationary alignment
78.25 degrees North to 78.25 degrees South
100
In flight, if one or both ice detectors fail, the crew must do what…?
The crew must select the MODE selector to ON - When icing conditions exist or anticipated below 10 degrees C (TAT) with visible moisture
101
CAT II approach and landing must be performed with flaps ___
5
102
CAT II demonstrated headwind?
25 knots
103
CAT II demonstrated tailwind
10 knots
104
CAT II demonstrated crosswind
12 knots
105
What is the max difference for routes in degrees between published charts and FMS?
Up to 3 degrees is acceptable
106
Temperature Compensation Baro-Nav operation
1. ) Must be coordinated with ATC | 2. ) Must be used for operation outside the temperature limits published on the approach procedure
107
What Equipment is required for RVSM? (Oral Question)
Autopilot Altitude Alerting System Altitude Reporting Transponder (x1, one must be operational) Air Data Computers (x2, both must be operational)
108
Max airspeed for RAT Operation?
Vmo/Mmo
109
Brake temperature limitation for takeoff… | Do not takeoff with brake temperatures in ____
Amber, do not takeoff with brake temps in amber
110
Max Turbulent Airspeed
Below 10,000 feet: 250 Knots Above 10,000 feet: 270 Knots/.76 Mach whichever is slower
111
What is the height of the E175?
32’4”
112
What is the length of the E175?
103’11”
113
What is the wingspan of the E175?
93' 11"
114
What is the distance you need to make a 180 degree turn in E175?
59' 2”
115
With FD inoperative what pitch angle would you use for flaps 1?
11 degrees
116
With FD inoperative what pitch angle would you use for flaps 2?
10 degrees
117
With FD inoperative what pitch angle would you use for flaps 3?
N/A
118
With FD inoperative what pitch angle would you use for flaps 4?
12 degrees