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RYAN E175 GROUND SCHOOL > E175 Limitations > Flashcards

E175 Limitations Flashcards

1
Q

Start Cycles Flight

A 
1 - 120/10sec
2 - 120/10 sec
3 - 120/5 min
4 - 120/5 min
5 - 120/5 min
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2
Q

Max pressure differential above 37,000ft

A

8.4 psi

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3
Q

Vmin RAT for pwr

A

130 kts

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4
Q

Vfe 3

A

200 kts

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5
Q

TRU

A

Convert 115v AC to 28v DC

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6
Q

Engine dry motoring cycles

A

1st cycle: 90 sec ON 5 min OFF

2nd-5th cycles: 30 sec ON 5 min OFF

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7
Q

Min Spoiler Speed

A

180 kts

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8
Q

ROLL (YAW) TRIM RUNAWAY

A

AP/TRIM DISC BUTTON - PRESS & HOLD

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9
Q

Max Takeoff and Landing Altitude

A

10,000

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10
Q

PTU

A

Assists gear up/down

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11
Q

V wiper ops max

A

250 (SW)

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12
Q

CABIN ALTITUDE HI

A

O2 Mask - Don 100%

Crew Communications - Establish

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13
Q

Airspeed ADSP and TAT valid

A

60 kts

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14
Q

Max static crosswind for takeoff

A

25 kts in new FOIB

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15
Q

Max Single Pack Operations

A

31,000 ft

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16
Q

Min Temp T/O & Lnd

A

-40C

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17
Q

Go Around full flaps

A

Flaps 4

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18
Q

V Window

A

160 kts

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19
Q

Max Operating Altitude

A

41,000ft

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20
Q

Max Altitude flaps/slats extended

A

20,000 ft

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21
Q

Full Flaps

A

165 kts

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22
Q

Vle

A

250 kts

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23
Q

V RAT DEPLOY MAX

A

Vmo/Mmo

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24
Q

Max Tailwind

A

15 kts

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25
Autopilot Minimum Use Height
50 ft
26
Vlo ext
250 kts
27
Autopilot Minimum Use Height Non Percision
MDA
28
Smoke/Fire/Fumes
Oxygen Masks . . .DON 100% | Crew Communication. . .ESTABLISH
29
Max X-Wind - Compact Snow (RCC-4) BA=Good to Med.
20 kts
30
RAT
150 kts min to spin up 8sec 130 min sustain Powers AC ESS Bus
31
CAT II Approach Flap Setting?
Flaps 5
32
Max x-wind ice RCC-2
12 kts
33
Max Zero Fuel Weight
69,886 lbs
34
APU running unattended
5 min
35
Min runway width
100 ft
36
Jammed Control Column - Pitch
ELEVATOR DISCONNECT HANDLE - PULL
37
BATT 1 (2) OVERTEMP
Associated Battery - OFF
38
APU start temp
-54C to ISA +35
39
Start Cycles Ground
``` 1 - 90/10sec 2 - 90/10 sec 3 - 90/5 min 4 - 90/5 min 5 - 90/5 min ```
40
Max X-wind Standing water/slush/Wet snow/Dry snow
18 kts
41
Vfe 5
180 kts
42
Max Runway Slope
+/- 2%
43
HBIT
60 sec All hyd systems pressurized Interrupt: move flight controls
44
APU Starter Limits
Attempts 1-2 - 60 Sec On - 60 Sec Off | Attempt 3 - 60 Sec On - 5 Min Off
45
APU max alt for bleed air use
15,000 ft
46
Min Fuel
2250 lb
47
BATT 1 (2) OVERTEMP
Associated Battery - OFF
48
Emergency Fuel
1500 lb
49
Vmo (10,000-Mach Trans)
320 kts
50
Pitch Trim Runaway
AP/TRIM DISC BUTTON - PRESS & HOLD | Pitch trim sys 1&2 cutout buttons - push in
51
Max Temp T/O & Lnd
ISA +35C (52C)
52
DC System
24v charges 28v | SLAB
53
Take-Off DATASET MENU
Visible moisture <1700 or <1sm vis ENG 5-10C ALL <4C
54
Vmo (SL-8000ft)
300 kts
55
Max pressure differential (overpressure)
8.8 psi
56
Min battery voltage
22.5V
57
Vfe 4
180 kts
58
Max Landing Weight
74,957 lbs
59
Aircraft Length
103ft 11in
60
Engine start oil pressure limits
Min 25psi
61
Brake temp for takeoff
In the green
62
Auto on ACMP flight
Flaps >0 | If EDP fail or Eng fail
63
Auto on ACMP ground
Flaps >0 thrust set T/o or GS>50kts #2 if Eng 1 Start P-brake release (Auto Shutoff 6min p-brake engaged)
64
Mmo
0.82
65
Max Takeoff Weight
85,517 lbs
66
Go Around Flaps 5
Flaps 2
67
ENGINE ABNORMAL START
Affected engine: | START/STOP selector. . .STOP
68
Interrupt Electrical PBIT
AC pwr cycled Normal Mode (disable FMC) Turn on hyd pump
69
APU max alt
33,000 ft
70
Wingspan
93ft 11in
71
Engine start temp
815 C
72
Min Batt voltage mx
21 v
73
Vb (10,000 ft and above)
270/.76M (whichever is lower)
74
APU op temp
-54C to ISA +35
75
Slats/Flaps Enroute Ops
prohibited
76
Vfe 1
230 kts
77
SMOKE EVACUATION
OXYGEN MASKS - DON, EMER CREW COMMUNICATION - ESTABLISH PRESSURIZATION DUMP - PUSH IN
78
Tail Height
32ft 4in
79
Max. ramp weight (lbs)
85,870 lbs
80
Autopilot Minimum Engagement Height
400 ft
81
APU max alt for eng start
21,000 ft
82
Max X-Wind - Dry (RCC-6) BA=Dry
38 kts
83
Electrical PBIT
Good for 50 hrs | 3 min, AC pwr to start
84
Vb <10,00ft
250 kts
85
IDG
AC power 115vAC | 1 each eng
86
Max fuel imbalance
794 lbs
87
Min Fuel Tank Temp
-37C
88
V Tire
195 kts
89
Max pressure differential takeoff and landing
.2 psi
90
Max pressure differential (negative pressure)
-.5 psi
91
Va
240 kts
92
Max pressure differential up to 37,000ft
7.8 psi
93
Max Fuel Capacity
20,935 lb
94
Min runway length
5,400ft reduces to | 5,000ft and SAT level 1-3 <4,000ft MSL
95
Min hyd reservoir temp for eng start
-18C
96
Vfe 2
215 kts
97
APU Max Start Alt
30,000 ft
98
Jammed Control Wheel - Roll
AILERON DISCONNECT HANDLE - PULL
99
Vle (retraction)
250 kts
100
Max X-Wind - Wet (RCC-5) BA=Good
31 kts
101
Batt 1 and 2 power time
10min 2 APU starts
102
Max FWD Cargo Weight
3306
103
Max AFT Cargo Weight
2535
104
Main Landing Gear Distance Between
17' 1"
105
Landing Gear Distance Between Nose and Mains
37' 5"
106
With Battery Power Only, What Is Powered
1. Lighted Compass 2. Cpt's DCU 3. Glare Shield Lights 4. Reversionary Panel 5. Cpt's PFD 6. EICAS 7. IESS 8. Clock 9. FO's MCDU 10. Cpt's CCD 11. Audio Control Panels - Both 12. Dome Light At Half Intensity
107
Take off with ATTCS Off?
Prohibited
108
Fuel: Minimum fuel tank temperature
-37°C
109
Fuel crossfeed operations
Must be off for takeoff
110
APU: limits/restrictions
Wait 30 seconds after EICAS is energized to start. Do not leave the aircraft unattended for more than five minutes with APU running. APU bleed air and high pressure cart air is prohibited at the same time.
111
Windmill Start Max Alt.
25,000'
112
Hydraulic reservoir temperature for engine start, min.
-18C
113
Thrust Reversers (all limits)
Do not attempt a go-around after deployment. Do not move thrust levers into forward thrust range until REV icon is shown in amber or green. Thrust reversers during taxi are prohibited. Thrust reversers for power back are prohibited.
114
Anti-ice system automatic operation temperature limit
No Temp. LImits
115
Wing Anti-ice set on in MCDU turns on at ____
40Kts
116
Anti-ice ENG must be selected on when ___
OAT is between 5°C and 10°C and: Any possibility of encountering visible moisture up to 1700' AFE. When operating on ramps, taxiways, or runways where surface snow, ice, standing water, or slush maybe ingested by the engines, or freeze on Engines, nacelles, or engine sensor probes.
117
Anti-ice ALL on must be selected when ____
OAT is 4C and below and: Any possibility of encountering visible moisture up to 1700' AFE. When operating on ramps, taxiways, or runways where surface snow, ice, standing water, or slush maybe ingested by the engines, or freeze on Engines, nacelles, or engine sensor probes.
118
Anti-ice in flight
System is automatic unless one or both ice detectors are failed, then crew must select anti-ice on when in icing conditions. 10°C TAT with visible moisture.
119
RNAV Approach Minimums
RNAV (GPS) LP minima are not authorized
120
Instruments - TAT, SAT, TAS only valid above __
60 Kts
121
Navigation equipment - standby magnetic compass
While transmitting in VHF 1, the standby magnetic compass is not valid
122
Cat 1 approach : Setting Mins
Barometric altimeter minimums must be used
123
Enhanced ground proximity warning system (EGPWS) limitations
Navigation is not to be predicated on the use of the terrain awareness system. Landing at an airport that is not in the database, EGPWS functions should be inhibited. Use of EGPWS functions must be inhibited when GPS data is unavailable or inoperative. Press the ground proximity terrain inhibit button to inhibit predictive EGPWS functions.
124
Autopilot must be used above __
20,000'
125
Use of flight director
The flight director is used and updated at all times. When the flight director is not synchronized with the actual aircraft maneuver it must be updated or turned off. Turning off flight director will not turn off autopilot.
126
Auto-throttle use
Preferable to override the Auto-throttles than turn them off
127
IESS initialization
The aircraft must not be moved until IESS is initialized, usually within 90 seconds after power up. Verify only screens 2 and 3 are available.
128
Electrical PBIT
Takes three minutes after electrical power up. Interrupted by.... any hydraulic pump turned on. flight control mode panel switches cycled. A/C power supply interrupted.
129
Hydraulic PBIT
All three hydraulic systems must be pressurized for at least 1 minute and reservoir temperature greater than 10°C. Interrupted by moving any flight control surface --One minute, one thing--
130
Hydraulic System Warm-Up. Must be done when reservoir temperatures are below __?
-18°C
131
Air data smart probe heater
Must be turned on during the first flight of the day with temperatures below -18°C, or when Smart probes are frozen. Turn off during after start checklist.
132
Ram air fault nuisance message
If ram air fault message remains for more than one minute after power up: - Pack one and pack two: push out - Wait five seconds - Pack one and pack two: push in
133
Walk Around: Turbine exhaust area
After engine shutdown, the scavenge system is no longer a effective. A small amount of oil may leak through the oil sump drain and pool in the engine Chevron nozzle. Oil puddle must not exceed 4 inches.
134
Walk Around: Brake Wear Indicators
Parking brake must be selected on and sufficient hydraulic pressure.
135
Hoar frost layer permitted underneath wing surfaces
Up to 1/8 of an inch, 3 mm, is allowed
136
Crew oxygen levels
``` Green = 3 Crewmembers Cyan = 2 Crewmembers Amber = no dispatch ```
137
Before start check list BELOW the line can be read___
Once ready to taxi signal has been received from the flight attendants and cockpit door has been closed and locked
138
Auto-brakes during pushback
When pushback speed is higher than 5 Kts auto-brakes may disarm
139
Engine start actions
At 7% N2 ignition, at 20% N2 fuel flow, positive oil pressure, ignition out at 50% N2. N1 target value on EICAS must be equal or greater than but not greater than 0.5% of the computed calculation value. SOPM 4-3.5
140
IDG's during cold weather operations
May take five minutes for IDG's to stabilize
141
Oil pressure during cold weather operations
Oil pressure may remain below minimum levels for two minutes, then engine must be shut down and oil heated to at least -20°C
142
IDG faults
IDG 1/2 OIL Caution displayed on EICAS and amber LED illuminates on overhead panel when either: IDG oil pressure drops below 140 psi +/- 25 PSI, IDG oil temperature reaches 335°F +/- 10°F Automatic disconnection is achieved at 366°F IDG oil temperature, or by manually selecting IDG disconnect position for one second.
143
IDG and APU generator ratings
40 kVA, 115 VAC, 400 Hz, three-phase
144
RAT USE and Operations
Deploys whenever AC power sources are not powering easy buses. After eight seconds it supplies power to the AC essential bus. During the eight second period batteries are used as backups to power the DC essential buses and standby AC bus. RAT's electrical power drives the AC motor driven pump 3A. Minimum of 130 Kts maximum of VMO/MMO 150 Kts need to "latch" the contact No altitude restriction
145
TRU's (transformer rectifier units)
Three on the aircraft rated at 300A. TRU 1 , TRU 2, TRU essential. They convert 115 VAC power from the AC buses into 28 VDC power If one fails, the buses will automatically be powered by the remaining TRU's
146
Aircraft batteries
Batteries are charged by any AC source through the TRU's During an electrical emergency, batteries supply essential loads for 10 minutes Battery over temp is triggered if battery temperature reaches 70°C for at least two seconds
147
DC GPU
Used during the APU starting cycle if battery number two is below -20° C or is not available. Suitable DC GPU should be at least 24 VDC and no more than 32 VDC, can be checked on the synoptic page
148
SPDA'S (secondary power distribution assemblies)
An electrical load management unit which receives power from the ICC AC/DC electrical buses and distributes it to the aircraft systems. Two in each plane, number one is in the forward electronics bay and number two is in the center electronics bay. Incorporate electronic circuit breakers to protect load distribution
149
What is on the AC essential bus
4 things: - AC fuel pump 2A - ACMP HYD 3A - SF-ACE 1 FLAP ch 1 AC feed - SF-ACE 2 SLAT ch 1 AC feed
150
Electrical priority for power
On side, inside, outside, Cross side
151
Engine vibration indications
Green: normal operating range 0 to 3.9 Amber: cautionary operating range 4.0 to 5.0 Amber dashed: invalid information or value
152
Air data smart probes (ADSP)
Comprised of: Multi function probes, Air data computer. Work with TAT to sense and transmit static pressure, total pressure, angle of attack and total air temperature to the air data system Angle of attack is calculated based on an interface between the static pressure of the smart probes
153
Taxi Speeds - Dry
Straight - 30 Kts max Turn - 10 Kts max
154
Taxi Speeds - Wet
Straight - 10 Kts max Turn - 5 Kts max
155
Lavatory Waste - Size, Full mark
Size - 95 liters MAX Full - (Service Light) @ 75% (71.25 liters)
156
Potable Water Amount
70 liters MAX
157
Brake Locked Wheel Protection
Active anytime on ground and wheel speeds greater than 30 kts. Compares wheel speeds, anytime they differ by 33% or more the brake control module releases either opposite outboard or opposite inboard brake pressure until both wheels equalize. The 33% tolerance is to allow for steering with differential breaking.
158
Cabin High Altitude
9,700'
159
Engine Out Distance for Takeoff Alt.
300nm
160
MINTO | Min. Takeoff Fuel
Fuel to fly from A to B + 45min. reserve + furthest Alternate + Holding fuel
161
RLSF | Release Fuel
MINTO + Contingency Fuel + Taxi Fuel
162
Fuel Gauges Turn Amber? Red?
2640 total = 1320lbs /side Fuel Low Level @ 660lbs. Either Tank
163
Things That Cause A Red Light For The Tug Driver
1. Parking Brake On 2. Toe Brakes depressed 3. Steering Engaged 4. External Disconnect Switch Not On
164
T.O. Config Is Checking
1. Parking Break 2. Spoilers 3. Flaps 4. Trim "Please Stop For Takeoff"
165
Fab 4 For After Stall/Wake/Uncontrolled Maneuver
1. FLCH 2. HDG 3. A/P 4. A/T
166
When does Auto Throttle take over?
At 50° TLA
167
Climb/Cruise/Descent Deviation and Callouts - SPEED
Target speed +/- 10 KIAS or .02 Mach
168
Climb/Cruise/Descent Deviation and Callouts - BANK
Bank angle in excess of 30°
169
Climb/Cruise/Descent Deviation and Callouts - HEADING
Heading differs from bugged +/- 10°
170
Climb/Cruise/Descent Deviation and Callouts - COURSE
Course differs from the established course by 1/4 deflection
171
Climb/Cruise/Descent Deviation and Callouts - PITCH
Pitch angle above or below typical angles, may result in a profile deviation
172
Climb/Cruise/Descent Deviation and Callouts - VERTICAL SPEED
Vertical speed too high or low, may result in a profile deviation
173
Climb/Cruise/Descent Deviation and Callouts - Call the failure
Any autopilot or flight director malfunction
174
Contaminated Runway
A runway is considered contaminated when more than 25% of the runway surface area (whether in isolated areas or not) within the reported length and width being used, is covered by more than 1/8", 3MM, of standing water or it's equivalent in slush, wet snow, dry snow or any depth of ice or compacted snow.
175
Stabilized Approach Windows By 1,500' AGL/RA or the FAF, whichever occurs later...
- Landing gear down | - Airspeed no greater than 180 KIAS
176
Stabilized Approach Windows At 1,000' AGL/RA
- Final landing configuration - Airspeed with in +15 and minus 5 KTS of target airspeed - On the lateral and vertical profiles/minor bracketing
177
Stabilized Approach Windows By 500' AGL
- Airspeed indication established within the speed bug | - Thrust setting above idle
178
RNP Airspeed Restrictions - All RF legs IAF to FAF
250 KTS or charted speed (controlling)
179
RNP Airspeed Restrictions - All RF legs FAF to DA
165 KTS (Cat D) or charted speed (controlling)
180
RNP Airspeed Restrictions - All RF legs DA to MAHP (missed approach holding point)
265 KTS or charted speed (controlling)
181
RNP - Terrain Map
Minimum of one pilot must have the terrain map up on MFD.
182
Approach - Temperature Compensation
Approach - Temperature Compensation 1. When Airport 10-7 has blue bar with temperature restriction column. 2. OAT at airport is outside of approach operational temp limits in the remarks section of the IAP 3. When OAT is less than -30•C at any foreign airports. Don't forget to tell ATC you are using temp compensation. Must give corrected altitudes at intermediate altitude segment (initial intercept altitude) and published missed approach hold point.
183
Pressing the TOGA button/s - Speed schedule
Pressing the TOGA button/s - Speed schedule Initially commands Vref + 20 kts Once reaching VNAV Cap alt, a/c accelerates to go-around flap speed schedule.
184
TOGA - Missed Approach sequencing.
TOGA will not sequence the missed approach point until you are two miles prior to FAF.
185
RNP - Procedure to discontinue the approach NEED TO VERIFY THIS
Callout, "Discontinue" Deselect APP and verify LNAV is the new active horizontal mode Set 165 KTS manually Set missed altitude and press FLCH Have PM sequence missed in FMS (LSK L6, Flight Plan page)
186
RNP - Required Flaps setting
Flaps 5 for RNP
187
RNP - Altimeter Settings limit
Remote altimeter settings are not authorized. | PM must perform Altimeter crosscheck at FAF: Limits 100' of each altimeter and 100' of FAF altitude
188
RNP- Single Engine
Is Authorized
189
Flaps Maneuvering Speeds
Provide at least 1.3 g margin over stick shaker which is equivalent to a shaker free bank angle of 40°
190
RNP - Pilot Qualification
Both pilots must have been qualified in the Sim to shoot an RNP approach.
191
Green dot
Provides at least 1.3 G margin over stick shaker speed, adjusted for the current airplane weight. Green dot can be used as the flap maneuvering speed. Flap Ext./Retract (+10 Kts.) L/D Max SE Drift down speed. Emergency Return Speed
192
Cold Weather Preflight required when....
The OAT is 5°C or less The wing fuel temperature 0° or less Atmospheric conditions conducive to icing exist The aircraft has remained overnight and has frozen contaminants adhering to surfaces Any through flight where residual ice from the inbound flight may have accumulated on the airframe surfaces or components Cold soak ice is suspected in the fuel tank area.
193
Unreliable Airspeed - Actions
``` Verbalize indicators PF disconnects auto pilot PF disconnects auto throttles PF determines initial pitch and power for safe flight. PM complete QRH procedure correctly ``` Quick reference..... Clean: 70% N1 and 2° pitch up (2° to5° window for cruise) Flaps extended: 70% N1 and 7° pitch up
194
Unreliable Airspeed - Causes
``` Failure of pitot-static system Failure of AOA probe Failure of air data computer Failure of an IRU Damaged or missing radon's ```
195
Windshear Alerting is active from __ 'to ___'?
10' to 1500' Radio Altitude during takeoff, go around, and landing
196
How do you activate windshear escape after receiving a windshear caution?
Press TOGA to activate windshear escape guidance
197
APU Auto Shutdown in Flight
UFO U Underspeed F Fadec Crit Fault O Overspeed
198
APU Auto Shutdown on ground
``` UFOSHELF Underspeed Fadec Crit. Fault Overspeed Sensor Failure High Oil Temp. EGT Overtemp Low Oil Pressure Fire Detected ```
199
Higher Level Elevator Functions - Elevator
AoA Limiting Thrust Compensation Speed Compensation Speed Brakes Compensation
200
Higher Level Functions - Ailerons
Roll Spoiler Scheduling | Ground Spoiler Auto Deploy
201
Higher Level Functions - Rudder
Rudder Flight Authority | Yaw Damp Turn Coordinator Via AFCS
202
When is flex takeoff prohibited?
Windshear Reported Contaminated Runways When specified by a departure procedure
203
PBE (Hood) Normal Indication? Humidity?
Blue Humidity = Pink
204
Deploying Cargo Fire Bottles | Annunciated vs Non-Annunciated
Push once + +1 for Non- Annunciated +1 for on the ground
205
Pulling the fire handle - Engines
closes Fuel Shutoff Valve Hydraulic Shutoff valve Bleed Air shutoff valve
206
Fire and Smoke Detected in the FWD Cargo Bay
Air circulation fan is turned off Ventilation outflow is close high rate fire bottle armed
207
Pressurization- Recirc Button Auto Mode
Turns on the RECIRC fans when: At least 1 pack is on. Turns the RECIRC fans OFF when: Both PACKs are off Cargo or recirculation bay SMOKE is detected
208
PAX CABIN Knob requires ________
PACK 2 operating
209
PACK in auto mode closes the valve (turns the pack off) automatically when:
Engine Start | Associated bleed duct leak is detected
210
Pressurization- XBLEED Auto
OPENS the XBLEED Valve when bleed air is available on one side and not the other CLOSES the valve automatically when: 1.Bleed leak detected (unless starting engine) 2. A fire extinguishing handle has been pulled
211
External Air Connections
HP High Pressure. Used for Engine start if APU INOP | LP Low Pressure used for cabin heating and cooling (not shown on the synoptics page)
212
APU BLEED Set to Auto:
``` OPENS Automatically when: When APU bleed is available CLOSES Automatically when: APU or left bleed leak is detected Anti Ice system is on Left engine bleed is available (in most cases engine bleed valves have priority over ```
213
Pressurization DUMP BUTTON
When Pressed: 1. OPENING the OFV (outflow valve) to command a 2000fpm cabin climb to 12,400' cabin altitude 2. Commands PACK's off 3. Commands Recirculating fans off
214
How long does the passenger oxygen supply last:
12 Min
215
Fuel Tanks each side
1. Surge Tank Contains fuel vent 2. Main Tank Main fuel storage area 3. Collector Tank: Where AC, DC and Ejector pumps are located
216
DC Fuel Pump:
Located in the right wing Primarily used to supply fuel to APU during start without AC power Can also be used to start Engine 2 without AC power Can be used during and ELECTRICAL EMERGENCY, to start APU and Engine 2
217
AC Standby Buss
Powered through the DC ESS BUS through and inverter when batteries are turned on. Powers Exciter(Igniter) 1 per engine Allows engine start with no AC power
218
Static Air Tempature
Temp. of the air around the plane as if it were standing still
219
Total Air Tempature (TAT)
Temp. of the air experience by the moving plane. includes heating from compression. TAT is used for aircraft icing awareness. Compare to the release for performance awareness.
220
Display Selector Knob selects for which display
MFD
221
ADS Reversion Button
Can selected another Air Data Source. CA PFD defaults to ADS 1 FO PFD defaults to ADS 2 ADS 3 is a dedicated backup. If failure. Default is backup then x-side
222
ADS Reversion Button
Can selected another Air Data Source. (3 on plane) CA PFD defaults to ADS 1 FO PFD defaults to ADS 2 ADS 3 is a dedicated backup. If failure. Default is backup then x-side
223
IRS (inertial reference system)
2 on the plane. | Provides roll pitch and heading information
224
ADS Components
ADSP (Air Data Smart Probes) Total Air Temperature Probes (TAT) Air Data Applications (ADA)
225
Air Data Smart Probes
Composed of: Multi Function Probes Air Data Computer ``` Calculates: Static Pressure Total Pressure AoA Total AIr Temperature ```
226
While the PA button is selected all other transmissions are disables
True
227
DVDR System
Flight Data Recorder and Cockpit Voice Recorder Stores 120 minutes of audio Stores flight data Used for safety trends and after accidents Used for FOQA
228
When will the auto throttles automatically retard upon landing? When will they not?
``` Reduces thrust levers at 30 feet. Requires: Valid Radar Altimeter Landing Gear down AT engaged Altitude below 150 AGL Slat Flap at 5 or full ```
229
Loss of Audio Panel, How do we activate backup radio?
MCDU Radio page 2
230
ATTCS Engages Reserve Thrust:
Thrust levers at TOGA and : 1. N1 Values greater than 15% difference 2. 1 engine failure during takeoff 3. 1 engine failure during go around 4. Windshear

RYAN E175 GROUND SCHOOL (21 decks)

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