Systems Study Guide Flashcards
(102 cards)
0
Q
Maximum Takeoff Weight (MTOW)
A
89,000/82,011
89/82
1
Q
Maximum Ramp Weight (MRW) (175/170)
A
89,352lbs/82,363
89.5/82.5
2
Q
Maximum Landing Weight (MLW)
A
75,177 / 72,311
75.2/72.3
3
Q
Maximum Zero Fuel Weight (MZFW)
A
70,547 / 66,447
4
Q
Cargo Weight Limits - E175
A
Forward Bin: 3,306
Aft Bin: 2,535
5
Q
Cargo Weight Limits - E170
A
Forward Bin: 3,020
Aft Bin: 2,271
12
Q
Max Runway Slope
A
+/- 2%
13
Q
Runway Surface Type
A
Paved
14
Q
Flaps Maneuvering Load Acceleration Limits, Flaps Up
A
-1.0G to +2.5G
15
Q
Flaps Maneuvering Load Acceleration Limits, Flaps 1, 2, 3, 4, 5, Full
A
0G to +2.0G
16
Q
Maximum Operating Altitude
A
41,000 feet
17
Q
Maximum Takeoff and Landing Altitude
A
8,000 feet
18
Q
Minimum Takeoff and Landing Altitude
A
-1,000 feet
19
Q
Max Temperature for Takeoff and Landing
A
ISA +35
20
Q
Min Temperature Approved for Takeoff
A
M40 C (SAT)
21
Q
Max Flap Extension Altitude
A
20,000 feet
22
Q
Hydraulic Warm Up Needed When…
A
<M18 hydraulic temp
23
Q
Crosswind Limits - Dry
A
28kts sustained, 38kts gusts (28G38)
24
Q
Crosswind Limits - Wet
A
28kts
25
Q
Crosswind Limits - Static Takeoff
A
25kts
26
Q
Crosswind Limits - Compact Snow
A
20kts
27
Q
Crosswind Limits - Standing Water /Slush
A
18kts
28
Q
Crosswind Limits - Wet Ice
A
12kts
29
Q
Maximum Operating Speed - Vmo
A
320kts
30
Maximum Operating Mach Number - Mmo
.82M
31
Minimum RAT Speed
130kts
32
Maximum Turbulent Airspeed - Below 10,000 feet
250kts
33
Maximum Turbulent Airspeed - At or Above 10,000 feet
270kts / 0.76M
34
Maximum Tire Limit Ground Speed
195kts
35
Maximum Windshield Wiper Operation Speed
250KIAS
36
Maximum Gear Speed - Extension (Vloe), Extended (Vle) AND Retraction (Vlor)
250 KIAS
37
Flap Limitations - Flaps 1
230 KIAS
38
Flap Limitations - Flaps 2
215 KIAS
39
Flap Limitations - Flaps 3
200 KIAS
40
Flap Limitations - Flaps 4
180 KIAS
41
Flap Limitations - Flaps 5
180 KIAS
42
Flap Limitations - Flaps FULL
165 KIAS
43
Max Fuel Capacity (Total)
20,785 lbs. (3,071 gallons!)
44
Minimum Fuel Tank Temperature
M40C
45
Maximum Fuel Imbalance
794 lbs
46
Crossfeed Operations (Must be off when...)
During takeoff and landing
47
Maximum Differential Pressure (up to 37,000 feet)
7.8 PSI
48
Maximum Differential Pressure (above 37,000 feet)
8.3 PSI
49
Maximum Differential Overpressure
8.7 PSI
50
Maximum Differential Negative Pressure
-0.5 PSI
51
Max Differential Pressure for Takeoff and Landing
0.2 PSI
52
Maximum Altitude for Single Pack Operation
31,000 feet
53
Thrust Reverser Limitations - engines must be idle by:
60 KIAS
54
Thrust Reverser Limitations - Engines Must Be Out Of Reverse By:
30 KIAS
55
Cockpit Crew Oxygen:
| 3 Crewmembers, 2 Crewmembers, No Dispatch
3=Green, 2=Cyan, No Dispatch= Amber
56
Autopilot Limitations: Minimum Engagement Height
Acceleration Altitude
57
Autopilot Limitations: Minimum En Route Height
500' AGL
58
Autopilot Limitations: Minimum Height to Engage on Go-Around
400' AGL
59
Autopilot Limitations: Minimum Height for a Precision Approach
70' AGL
60
Autopilot Limitations: Minimum Height for a Non-Precision Approach
MDA
61
Autopilot Limitations: Special Instrument Approach
As specified in the procedure
62
Crosswind Limits - Max Tail Wind
10kts
63
CAT II - Max Headwind
25kts
64
CAT II - Max Crosswind
12kts
65
CAT II - Max Tailwind
10kts
66
Max Taxi Speed - Straight Dry/Wet
30kts
67
Max Taxi Speed - Straight Contaminated
15kts
68
ITT Max Start Temp
815C
69
For takeoff, ATTCS must be:
On
70
Engine warm-up and cool down period:
2 minutes
71
Powerback Operations are:
Prohibited!
72
Engine Starter Duty Limits - Ground
1-2: 90 seconds on, 10 seconds off
3-5: 90 seconds on, 5 minutes off
*After five sequential motorings, the cycle may be repeated following a 15 minute cool down.
73
Engine Starter Duty Limits - In Flight
1-2: 120 seconds on, 10 seconds off
3-5: 120 seconds on, 5 minutes off
*After five sequential motorings, the cycle may be repeated following a 15 minute cool down.
74
Engine Starter Duty Limits - Dry Motoring
1: 90 seconds on, 5 minutes off
2-5: 30 seconds on, 5 minutes off
*After five sequential motorings, the cycle may be repeated following a 15 minute cool down.
75
No Flex - Reduced Thrust Takeoff if:
1. Standing water, slush, snow, or ice
2. Anti-skid INOP
3. TLR - No Flex Data
4. Flex prohibited airport (10-7)
5. PIC deems unsafe
76
RVSM requirements
2 - ADS
1 - Autopilot with altitude hold
1 - Altitude alerter
1 - Transponder
77
Air Temperature for Start
-54C to ISA +35C
78
Minimum Battery Voltage to Start the APU
21V
79
Minimum Battery Temperature for APU Start
-20C
80
Max Altitude for APU:
* Generator
* Starting the APU
* Assisted Engine Start
* Bleed Air
* Generator - 33,000'
* Starting the APU - 30,000'
* Assisted Engine Start - 21,000'
* Bleed Air - 15,000'
81
APU Starter Duty Cycle
1: 1 minute on, 1 minute off
| 2-3: 1 minute on, 5 minutes off
82
Icing Conditions on Ground and for Takeoff -
| MCDU TO DATASET MENU - set to ENG when:
1. SAT is 5C to 10C and visible moisture will be encountered up to 1,700' AFE or:
2. Operating on ramps, taxiways, or runways where surface snow, ice, standing water, or slush may be ingested by the engines, or freeze on engine nacelles, or engine sensor probes.
83
Icing Conditions on Ground and for Takeoff -
| MCDU TO DATASET MENU - set to ENG when:
1. SAT is less than 5C and visible moisture will be encountered up to 1,700' AFE or,
2. Operating on ramps, taxiways, or runways where surface snow, ice, standing water, or slush may be ingested by the engines, or freeze on engine nacelles, or engine sensor probes.
84
Icing conditions exist in flight whenever static air temperature (SAT) on the ground (taxi or takeoff), or the Total AirTemperature (TAT) in flight is:
Equal to or less than 10C 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)
85
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 with a TAT of 10C or below with visible moisture.
86
Random Limitations: when the airplane is stopped on the ground,
The taxi and landing lights must be OFF
87
Random Limitations: for takeoff and in flight the taxi nose light must be:
Off.
88
How long should you wait after the GPU switch is pushed in, or the APU power is available before shutting down the engine(s)?
10 seconds
89
Minimum Flight Speed - All Altitudes, exceptions
Except as described in the normal/abnormal/emergency procedures, the airplane may never be operated below the "green dot" speed.
90
Baro altimeter minimums
Must be used for all Cat I approaches
91
VOR flight director mode:
Is prohibited/inhibited. VOR navigation using the FD must be predicated on HDG mode and VHF (green) needles or LNAV mode (magenta).
92
Back course approaches are prohibited using:
IESS
93
Before stopping the APU after engine start:
1. Engine N2 must be stabilized for 5 seconds, OR
| 2. Power transfer is confirmed on the Electrical Synoptic Page
94
Before starting the APU after an engine is shutdown:
1. Wait for the engine to go below 30% N2
95
Minimum distance for a 180 degree turn: (175/170)
175: 59'2"
170: 54'8"
96
MEMORY ITEM: Smoke (fire, fumes, LAV smoke, and cargo smoke)
1. Oxygen Mask - DON, 100% AS REQUIRED
| 2. Crew Communications - ESTABLISH
97
MEMORY ITEM: LOSS OF CABIN PRESSURE (Cabin altitude high)
1. Oxygen mask - DON, 100%
| 2. Crew Communication - ESTABLISH
98
MEMORY ITEM: JAMMED CONTROL COLUMN (Pitch)
1. Elevator Disconnect Handle (CONFIRM) - PRESS & PULL
99
MEMORY ITEM: JAMMED CONTROL WHEEL (ROLL)
1. Aileron Disconnect Handle (CONFIRM) - PRESS & PULL
100
MEMORY ITEM: PITCH TRIM RUNAWAY
1. Autopilot Disconnect Button - PRESS & HOLD
| 2. Pitch Trim Systems 1 & 2 Cut-out Buttons - PRESS IN
101
MEMORY ITEM: ROLL (YAW) TRIM RUNAWAY
1. Autopilot Disconnect Button - PRESS & HOLD
102
MEMORY ITEM: STEERING RUNAWAY
1. Steering Disconnect Switch - PRESS
| 2. Differential Braking and Rudder - USE TO STEER
103
MEMORY ITEM: ENGINE START MALFUNCTION
Affected Engine:
| 1. START / STOP Selector - STOP
104
How many networks make up the electrical system on the airplane? Why?
2 independent networks, to provide redundancy and fault isolation.
105
What happens if a power generating source fails?
Bus ties automatically connect to provide no system degradation.
106
What components power the AC system?
```
2 integrated drive generators (IDG)
Auxiliary Power Unit (APU)
Inverter
Ram Air Turbine (RAT)
AC GPU receptacle
```
107
What components power the DC system?
3 transformer rectifiers
2 NiCAD batteries
1 DC GPU
