Full Limitations Flashcards
(209 cards)
1
Q
Maximum Crosswind Component for Takeoff and Landing
A
27
2
Q
Maximum crosswind component for landing from a Category II approach
A
15
3
Q
Maximum headwind component for landing from a category II approach
A
16
4
Q
Maximum tailwind component for takeoff and landing (INCLUDES GUSTS)
A
10
5
Q
Maximum Operating Altitude
A
41,000’
6
Q
Except in an emergency, takeoff or landing will not be attempted whenever peak wind value exceeds
A
50 knots
7
Q
Maximum altitude for single pack operation
A
31,000’
8
Q
Turbulence penetration speed
A
280 or .75M, whichever is lower
9
Q
Maximum gear extension speed
A
220
10
Q
Maximum gear extended speed
A
220
11
Q
Maximum gear retraction speed
A
200
12
Q
Maximum speed for windshield wiper operation
A
220
13
Q
Vfo/Vfe Flaps 1
A
230
14
Q
Vfo/Vle Flaps 8
A
230
15
Q
Vfo/Vfe Flaps 20
A
220
16
Q
Vfe/Vlo Flaps 30
A
185
17
Q
Vfe/Vlo Flaps 45
A
170
18
Q
The APU starter motor duty cycle is limited to not more than ______ starts/start attempts in _____ hour with a ______ minute delay between cranking attempts
A
3; 1; 2
19
Q
Maximum APU starting Altitude
A
37,000
20
Q
Maximum APU operating altitude
A
41,000’
21
Q
Maximum altitude for APU Bleed Air for Air Conditioning
A
25,000’
22
Q
With the APU door not closed or the door position is unknown the airspeed limitation is ______ or the APU ________.
A
220, must remain in operation
23
Q
Maximum AC Electrical load on the engine or APU driven Generator
A
40 Kva
24
Q
Maximum DC Electrical Load on each TRU
A
120 amps
25
Maximum time on the ground with only DC power available
5 minutes
26
During all starts, do not exceed ______ N1 for _______ after start, or until all operating indications are in the normal range, whichever is longer.
75%; 2 minutes
27
Operate engines at or near idle for _____ minutes prior to shutdown
2 minutes
28
Maximum Time at TOGA power on 2 engines
5 minutes
29
Maximum ITT for engine start on the ground \_\_\_\_\_\_\_.
120 before attempting start; 815 during the start
30
Maximum ITT for engine start in flight
90 before starting; 927 while starting
31
Minimum oil pressure at idle
25 psi
32
Minimum oil pressure at takeoff power
45 psi
33
After cold start, engine must remain at _______ until oil pressure returns to normal range
Idle
34
Continuous engine ignition must be used during the following:
1. Takeoff AND landing on contaminated runway 2. Takeoff with high crosswind components (15 knots or greater) 3. Flight through moderate or heavier intensity rain 4. Flight through moderate or heavier turbulence 5. Flight in the vicinity of thunderstorms
35
Starter cranking limits:
90sec - 10sec 90sec - 10sec 90sec - 5min
36
During landing, maximum reverse thrust is prohibited below \_\_\_\_\_\_, and reverse idle should be achieved by \_\_\_\_\_\_\_.
75knots; 60knots
37
Engine Operating Limits Due to Wind Direction: Within 30 degrees on either direction of the airplane nose-no windspeed limit OR… \>30 degrees in either direction of the airplane nose-between \<5 knots of windspeed
No limitation; TOGA thrust can be applied before brake release
38
Engine Operating Limits Due to Wind Direction: \>30 degrees in either direction of the airplane nose-between 5 and 30 knots of windspeed
Max 75% N1 prior to brake release, then TOGA thrust
39
Engine Operating Limits Due to Wind Direction: \>30 degrees in either direction of the airplane nose-between \>30 knots of windspeed
Apply maximum of idle/taxi thrust before brake release, then TOGA thrust
40
If Static/Standing takeoff data is generated and wind limits prevent a static/standing takeoff winds must be entered in _____ OR for aircraft with ACARS inoperative, Dispatch must _______ winds into TLR data
ACARS; manually insert
41
Enroute use of slats/flaps is
Prohibited
42
Maximum slats and/or flaps extended altitude
15,000’
43
Minimum altitude for flight spoiler deployment
1,000’ AGL
44
Minimum airspeed to extend the flight spoilers is
Recommended reference speed plus 17 KIAS
45
Maximum permissible fuel imbalance between the left and right-wing tanks for TAKEOFF
300 LBS
46
Maximum permissible fuel imbalance between the left and right-wing tanks for ALL OTHER PHASES OF FLIGHT
800 LBS
47
Maximum Fuel Quantity - Pressure Refueling (700/900)
19,594
48
Maximum fuel quantity - Gravity refueling (700)
14,580
49
Maximum fuel quantity - Gravity refueling (900)
14,810
50
Takeoff with a fuel load in excess of _____ lbs. in the center tank is not permitted unless each wing tank is above ______ lbs.
500; 4,400
51
Powered CROSSFLOW and gravity CROSSFLOW must be ______ for takeoff
OFF
52
The minimum fuel quantity for go-around per wing tank (with the airplane level) and assuming a maximum airplane climb attitude of 10 degrees nose up ______ lbs
600
53
Ground Contamination Definition
Runways, ramps or taxiways with surface snow, ice, slush or standing water
54
Visible moisture definition
Visible moisture or precipitation in any form (such as fog with visibility of one mile or less, mist, rain, now, sleet, and ice crystals or clouds inflight)
55
If visible moisture is present below 400’ AGL with OAT ______ or below activate ______ anti-ice. if OAT _______ activate both ______ anti-ice for takeoff.
10; COWL; 5; COWL and WING
56
Icing conditions in flight exist when visible moisture is present, and the TAT \_\_\_\_\_\_, except when the SAT is ____ or below
10C; -40C
57
If icing conditions exist in flight wing and cowl anti-ice is required when the airspeed is below _____ KTS and cowl anti-ice is required when the airspeed is at or above ____ KTS
230; 230
58
If If Ground Contamination or visible moisture is present for takeoff and the OAT is at or below _____ Cowl and wing anti-ice are required
5C
59
If If Ground Contamination or visible moisture is present for takeoff and the OAT is at or below _____ Cowl anti-ice is required
10C
60
In addition to a visual check, a tactile check of the wing leading edge, wing forward upper surface and wing rear upper surface is required during the exterior inspection to determine that the wing is free from frost, ice, snow, or slush when: 1. The OAT is _____ or less, or 2. The bulk fuel temperature is ____ or less, or 3. ___________ 4. Ice and frost may continue to adhere to wing surfaces for some time even at outside air temperatures above \_\_\_\_\_\_\_\_
10C; 0C; The atmospheric conditions have been conducive to frost formation; 10C
61
Do not hold in icing conditions with ________ extended
Slats and/or flaps
62
The Taxi lights must be switched OFF whenever the airplane is stationary in excess of \_\_\_\_\_\_\_\_\_\_\_
10 minutes
63
Equipment Requirements for RVSM
1 Autopilot with Altitude Hold - Needs to be operational 1 Altitude Alerting System - Needs to be operational 2 Altitude Reporting Transponders - 1 must be operational 2 Air Data Computers - 2 must be operational
64
Minimum brake cooling time is \_\_\_\_\_\_\_\_, and all BTMS indicators must be \_\_\_\_\_\_\_\_\_\_\_
15 Minutes; green and not increasing
65
CAT II approaches are prohibited when the braking action is reported as less than \_\_\_\_\_\_\_
MEDIUM (less than 3 CC)
66
Flight must be within _____ minutes of a suitable airport, if cargo is carried in either cargo compartment
60 minutes
67
Operation with the autopilot engaged is prohibited at altitudes below \_\_\_\_\_\_\_
600’ AGL
68
Minimum AP Altitude for visual and non-precision approaches
400’ AGL
69
Minimum AP altitude for precision approaches
80’ AGL
70
Minimum AP altitude for Single Engine Precision approaches or those with vertical guidance on the 900 is _____ feet
110’ AGL
71
Use of SPEED MODE (DES or IAS) with the flight director or autopilot coupled during approach is _____ permitted
NOT
72
Use of VNAV with the flight director or autopilot coupled during climb and approach phases of flight is ______ permitted
NOT
73
Maximum Taxi and Ramp Weight (700)
75,250 LBS
74
Maximum Takeoff Weight (700)
75,000 LBS
75
Maximum Landing Weight (700)
67,000 LBS
76
Maximum Zero Fuel Weight (700)
62,300 LBS
77
Maximum Ramp and Taxi Weight (900)
85,000 LBS
78
Maximum Takeoff Weight (900)
84,500 LBS
79
Maximum Landing Weight (900)
75,100 LBS
80
Maximum Zero Fuel Weight (900)
70,750 LBS
81
Cabin Alt/Emergency Descent
1. Oxygen Masks…… Don and 100%
2. Crew Communications …… ESTABLISH
3. Captain Assumes PF Duties
82
Smoke/Fire/Fumes
1. Oxygen masks (if required) ……….. DON and 100%
2. Crew Communication ………. ESTABLISH
83
Stabilizer Trim Runaway:
1. Control Wheel ………… ASSUME manual control and OVERRIDE runaway
2. STAB TRIM DISC………… Push, hold and release
84
Maximum pressure differentials:
Positive: 8.7
Negative: -0.5
Ground Maneuvering: 0.1
Initial Landing (at touchdown): 1.0
85
When Does Low Pressure air have to be OFF?
Prior to the main cabin door being closed and secure
86
What must we ensure before opening any of the airplane doors?
It is completely depressurized
87
When is the use of EMER DEPRESS switch prohibited?
Above 15,000’
88
Maximum airspeed for windshield wiper operation failed in the non-parked position (Vstuck)
250
89
Maximum cruise Mach in RVSM airspace
0.82M
90
Tire limit ground speed
700: 182KIAS
900: 195KIAS
91
Full application of rudder and aileron controls, as well as maneuvers that involve angles of attack near the stall, must be confined to speeds below \_\_\_\_\_\_.
Va
92
In order to prevent structural failure, we should…
Avoid rapid and large alternating control inputs, especially in combination with large changes in pitch, roll, or yaw (e.g., large side slip angles) as they may cause structural failure at any speed, including below Va
93
When is intentional speed reduction prohibited?
When it’s below the onset of stall warning, as defined by stick shaker operation, Unless a lower speed is specifically authorized for flight tests or training operations
94
Minimum temperature for cold-soaked APU starting on the ground
-40C
95
The APU starter motor duty cycle is limited to what?
Not more than 3 starts/start attempts in 1 hour with a 2 minute delay between cranking attempts
96
Maximum RPM for the APU.
106%
97
APU Maximum EGT for All Conditions
1038
98
All APU Limitations Lowest to Highest Altitude.
21,000' - Highest Altitude for Main Engine Starter using APU Bleed Air (Technically a MES Limitation)
25,000’ - APU Bleed Air Extraction for Packs Maximum Altitude
37,000' - Maximum APU Starting Altitude
41,000' - Maximum APU Operating Altitude
99
The flight deck door must be \_\_\_\_\_\_\_\_\_\_\_, during flight, except to permit \_\_\_\_\_\_\_\_\_\_\_\_\_.
Kept closed and locked; access and egress in accordance with FAA and company procedures for opening, closing, and locking the door.
100
Any time at the flight deck door is opened in flight….
A challenge and response closing and locking verification must be used to verify that the door is closed and locked.
101
Any time a required flight crew member leaves the flight deck, another crew-member must….
Be present in the flight deck to ensure that they are not locked out of the flight deck.
102
Maximum APU electrical load
40Kva
103
Maximum permissible DC electrical System loads:
120 amps
104
During all starts, do not exceed ____ N1 for ______ minutes after start or \_\_\_\_\_\_\_\_
75%; 2; until all operating indications are in the normal range, whichever is longer.
105
Operate engines at or near idle for ______ minutes prior to shutdown.
2
106
Taxi time at a stabilized _________ or below may be credited towards the two-minute cool down period required to operate the engines at prior to shutdown
80% N2.
107
Engines:
1. 700 - General Electric CF 34-8C5B1
2. 900 - General Electric CF 34-8C5
108
Normal takeoff power and maximum power (2 engines) is limited to \_\_\_\_\_\_.
5 minutes
109
APR power (1 engine) is limited to \_\_\_\_\_.
10 minutes.
110
Pilot initiated APR thrust is prohibited \_\_\_\_\_\_\_\_\_.
1. For first 30 minutes after any engine start at altitudes below 7,500’ MSL
2. At all times above 7,500’ MSL
3. does not prohibit the pilot from selecting APR as required for safety of flight.
111
Before Start ITT Temperature Limitations (Ground and Air)
Ground: 120C
Air: 90C
112
Oil pressures (above IDLE) between _________ require oil temperature monitoring.
25 and 45 PSI
113
Oil pressures should show positive value during start and may peak beyond _____ and are displayed as \_\_\_\_\_\_\_.
182 psi; amber dashes
114
Oil pressure may be greater than ______ for a maximum of 10 minutes.
95 psi
115
Minimum oil level for flight
40% min with affected engine not started
116
N2 limitations for starting:
Ground or Assisted Air Start: 0-45%
117
Definition of cold soaked
1. First flight of the day
2. Temperature of -30C or less
3. More than 8 hours
118
What should you do if your airplane is cold soaked?
1. Thrust reversers must be actuated until the deploy and stow cycles are 2 seconds or less
2. verify N1 fan rotation.
119
Minimum Oil Temperature for starting
-40
120
Steady-state idle oil pressure minimum
25 psi
121
Minimum oil pressure for takeoff power
45psi
122
Maximum continuous thrust max oil pressure
95 psi
123
After a cold start the engine must….
Remain at idle until oil pressure returns to normal range
124
Maximum oil consumption
6.4 ounces per hour/0.05 US gallons per hour
125
The starter must not be engaged if indicated N2 RPM exceeds _____ (inflight or on the ground).
45%
126
Air start starter limitations:
1st start: 2 minutes On, 10 Seconds OFF 2nd and on: 1 minute on; 5 minutes OFF
127
An initiation of thrust lever movement from SHUT OFF to IDLE:
ITT must be less than 120C for ground starts ITT must be less than 90C for air starts
128
A dry motoring cycle (thrust levers at SHUT OFF) may be used for engine ground starts and engine air starts as long as:
1st start: 90s on 5m OFF 2nd and subsequent: 30s on 5m OFF
129
What is a dry-motoring cycle?
Thrust levers at SHUT OFF
130
Relight Limitations: Windmilling
25,000 - SL: Speed 250KIAS to Vmo and from 7.2% N2 minimum
131
Relight Limitations: Starter Assisted.
Altitude from 21,000’ to SL: Speed from Vref up to Vmo and from 0-45%N2
132
Engine Relight Limitations: All Engine-Out Rapid Relight
FADEC rapid relight capability has been demonstrated at 200KIAS for up to 15-second fuel interruptions
133
Thrust reversers are approved for _______ and prohibited in \_\_\_\_\_\_\_.
Ground use only; flight
134
Thrust reversers are intended for use during ________ landings.
Full-stop
135
Do not attempt a __________ after deployment of thrust reversers.
Go-around
136
Takeoff with any _____________ displayed is prohibited except as described in MEL 78-30-01
Thrust reverser lights ON, icons, or EICAS thrust reverser messages
137
During preflight check of the thrust reversers with the Airplane stationary, reverse thrust must be limited to \_\_\_\_\_\_\_\_.
Reverse idle
138
\_\_\_\_\_\_\_\_ using thrust reversers is prohibited
Backing-up
139
Dispatch with ______ on runway ______________ is prohibited.
1 thrust reverser deferred; contaminated with ice
140
If static/standing takeoff data is generated and wind limits prevent a Static/standing takeoff:
1. Must must be entered in ACARS 2. IF ACARS inoperative, dispatch must manually insert winds into TLR data.
141
In order to do a FLEX takeoff ______ must be operative
Anti-skid
142
When is a FLEX thrust takeoff prohibited:
1. Contaminated runways
2. Airplane has been de-iced
3. Anti-ice is on
4. Warnings of windshear or downdrafts have been forecast
5. An engine that cannot achieve full-rated thrust 6. A special departure procedure specifies full thrust for takeoff
6. When Anti-skid is inop
143
Maximum permissible fuel imbalance between left and right wing tanks:
1. Takeoff: 300lbs 2. All other phases of flight: 800lbs 3. Refuel/Defuel: 2,500lbs
144
Fuel remaining in a tank when the appropriate fuel quantity reads _______ is \_\_\_\_\_\_.
Zero; not usable.
145
Fuel quantities for the limitations are based on:
6.75 lbs/per US gal.
146
\_\_\_\_\_\_ must be on OFF for takeoff
Powered CROSSFLOW and gravity CROSSFLOW.
147
Minimum fuel quantity for go-around per wing tank (with the airplane level) and assuming a maximum airplane climb attitude of 10 degrees nose up:
600 lbs
148
Takeoff with engine fuel temperature below _____ is prohibited
5 degrees.
149
Takeoff with bulk fuel temperature indications below ______ using Jet A is prohibited.
-40C
150
When using JET A type fuel with ambient temperature of ______ or below, the bulk fuel temperature prior to flight must be verified to be above \_\_\_\_\_\_.
-30; -29C…. So it needs to be -28 or warmer
151
If the wing anti-ice system is selected ON for take off…
The cowl anti-ice system must also be on.
152
When type IV anti-icing fluids have been applied, what must be done differently with the CRJ's Anti-icing Systems?
Wing anti-ice system must only be selected and confirmed on just prior to thrust increase for takeoff.
153
Wing and/or cowl anti-ice selection inflight is prohibited with the ______ as a bleed source in ______ mode.
APU; Manual
154
What can adversely affect stall speeds, stall characteristics, and the protection from the stall protection system and lead to loss of control on takeoff?
Small amount of frost, ice, snow, or slush on the wing leading edges and froward upper wing surface
155
Takeoff is prohibited with frost, ice, snow, or slush adhering to any \_\_\_\_\_\_
Critical surface: 1. Wings 2. Horizontal stabilizer 3. Vertical stabilizer 4. Control surfaces 5. Engine inlets
156
Other than \_\_\_\_\_\_\_\_\_, the upper fuselage must also be de-iced anytime the _______ require de-icing.
Frost; wing and tail surfaces
157
Take-off is permitted with frost adhering to:
1. The upper surface of the fuselage 2. The underside of the wing, (maximum 1/8 inch) caused by cold soaked fuel.
158
Frost on the upper fuselage surface is not considered critical if \_\_\_\_\_. Frost in excess of this \_\_\_\_\_\_.
It is possible to distinguish surface features (markings and lines); must be removed from the fuselage
159
Single Engine Taxi is prohibited when ramps or taxiways are \_\_\_\_\_\_\_\_\_\_.
Contaminated with snow, slush, or ice, or when snow or other freezing/frozen precipitation is present
160
When and why should operating thrust reversers during taxi operations be avoided?
Taxiway is wet or contaminated and to prevent wing contamination from reverse jet blast.
161
In addition to a visual check, a tactile check of the \_\_\_\_\_\_\_\_\_. Is required during the _________ to determine that the wing is free from frost, ice, snow, or slush when:
Wing forward upper and rear upper surface; exterior inspection. 1. OAT is 10C or less 2. Bulk fuel is 0C or less 3. Atmospheric conditions have been conducive to frost formation
162
Taxi lights must be switched OFF whenever the airplane is stationary in excess of _____ minutes.
10
163
What must be observed between a landing or rejected takeoff and a subsequent takeoff?
Brake cooling times. In order to ensure sufficient brake energy is available.
164
Category II approaches are prohibited with RCC codes (Braking Action Codes) less than: \_\_\_\_\_\_\_\_\_.
“Medium”
165
Crosswind component under _____ braking action is not limited by \_\_\_\_\_.
Good (5); Gusts.
166
CC Code Wind Limits:
5: 10kt TW; 27kt CW (Not including gusts)
4: 10kt TW; 27kt CW (Including gusts)
3: 5kt TW; 15kt CW (Including gusts)
2: 5kt TW; 10kt CW (Including gusts)
1: 0kt TW; 10kt CW (Including gusts
167
For dispatch to an airport use _____ winds.
Steady-state
168
Inflight internet system is to be used only \_\_\_\_\_\_\_\_\_\_\_\_\_.
In the passenger cabin.
169
Live animals shall not be transported \_\_\_\_\_\_\_\_\_\_
In the forward cargo compartment.
170
Autopilot use lowest authorized altitude (700) PAR/ILS approaches.
80’ AGL unless: GPA 3.5-4.0 and airport elevation is less than or equal to 4,000’: 120’ AGL GPA 3.5-4.0 and airport elevation greater than 4,000’: AP use PROHIBITED GPA greater than 4.0: AP use is PROHIBITED
171
Autopilot use lowest authorized altitude (900) PAR/ILS approaches.
80’ AGL GPA greater than 3.5, AP use is PROHIBITED.
172
In the 900, the minimum height for autopilot use OEI is?
110’ AGL
173
Category II approaches ______ with the autopilot.
Must be flown.
174
If an engine failure occurs during a climb while in “ALTS CAP” or just before “ALTS CAP” \_\_\_\_\_\_\_\_.
The airspeed may drop significantly below the safe operating speed. Crew intervention may be required to maintain safe operating speed.
175
Use of ISI localizer and BC information is prohibited \_\_\_\_\_\_\_.
During LOC BC approaches.
176
Before takeoff, the difference between the published field elevation and the altimeter display should not exceed \_\_\_\_\_.
75’
177
In flight: primary and stand-by altimeters should be cross-checked \_\_\_\_\_\_\_.
At least every hour.
178
If there is a difference greater than \_\_\_\_\_\_\_’ the altimeter system should \_\_\_\_\_\_\_\_/
200’, be reported to ATC as being defective.
179
Airplane navigation must not be predicated upon \_\_\_\_\_\_.
Use of the terrain display.
180
To avoid giving unwanted alerts, the terrain awareness alerting and display functions must be inhibited \_\_\_\_\_\_\_\_.
On takeoff, approach, or landing within 15NM of an airport not included in the EGPWS airport database.
181
The terrain database, terrain displays, and alerting system do not \_\_\_\_\_\_\_\_\_\_\_.
Account for man-made obstructions, except for all KNOWN man-made obstructions in Canada, the US and Mexico
182
When would the EGPWS fail to alert when a terrain threat exists?
If GPS is inoperative during ambient surface temperatures below ISA, non-standard temperature lapse rates, or if incorrect barometric settings are set on the altimeter.
183
How would you identify if GPS is inoperative?
LOSS OF INTEGRITY GNSS NOT AVAILABLE; GNSS-FMS DISAGREE messages on the FMS CDU
184
FMS Prohibited Approaches:
RNAV (RNP), ILS, LOC, LOC/BC, LDA, and SDF
185
FMS ________ information is advisory only
Thrust, range, fuel management and VNAV system information.
186
FMS instrument approaches must not be continued past the ______ if an \_\_\_\_\_\_\_\_\_.
Final approach fix; FMS NO APPR message is displayed on the PFD.
187
In aircraft with a dual FMS installation, if both CDUs and FMCs are operating normally, the system must be operated in ______ mode.
SYNC
188
Use of the FMS ________ is prohibited
Temperature Compensation Function
189
FMS generated altitudes and V-paths are \_\_\_\_\_\_.
Not corrected for non-ISA conditions.
190
Changes to altitudes in the _____________ are prohibited.
Departure and missed approach procedures.
191
Use of descent angles \> 4.5 degrees at high altitude \_\_\_\_\_\_\_\_\_\_\_.
May result in unintended acceleration beyond permitted speeds.
192
The FMS does not provide automatic transition to the \_\_\_\_\_.
ILS
193
Currently PSA does not serve any destination north of _____ latitude.
48N
194
The _______ source coupled to the active ______ must be ___________ during flight in RVSM airspace.
ADC; FCC; the same as that coupled to the ATC transonder.
195
In flight, prior to entering RVSM airspace \_\_\_\_\_\_\_\_\_\_.
All required equipment for operation in RVSM airspace must be operation.
196
Maximum Cruise speed in RVSM airspace.
0.82M.
197
Maximum weight forward cargo compartment (700 and 900)
700 = 1000lbs 900 = 1900lbs
198
Maximum weight in aft cargo compartment 900
3740
199
Pitch trim must be set according to the aircrafts \_\_\_\_\_\_\_. Failure to set the pitch trim appropriate to the computed _______ may result in \_\_\_\_\_\_\_.
Computed C.G; C.G; excessive rotation rate at take-off.
200
What is an excessive rotation rate?
More than 3 degrees per second.
201
Excessive rotation rates or _______ over rotations may lead to high pitch attitudes being attained while near the ground. This can \_\_\_\_\_\_\_\_\_\_\_. Pilots must ___________ then \_\_\_\_\_\_\_.
Over-rotations Reduce stall margins significantly, resulting in stick shaker/pusher activation and potentially loss of control. Rotate smoothly towards the target pitch attitude Transition to speed control.
202
Minimum PSI bleed pressure for Cross Bleed Starts.
42 PSI
203
Immediate action items that do not have steps which must be accomplished from memory:
1. L/R ENG OIL PRESS Msg. Or Oil Pressure Low 2. Aileron System Jammed 3. Rudder System Jammed 4. Elevator System Jammed 5. Uncommanded Yaw Motion 6. Unreliable Airspeed In-Flight
204
Double-engine Failure:
1. CONT IGNITION……..ON 2. Airspeed……………….240 KIAS minimum
205
RVSM is from ______ to \_\_\_\_\_\_\_\_.
FL290 to FL410
206
Maximum temperature for takeoff and landing:
ISA + 40C or OAT of 51C
207
Braking Loss/Asymmetry
1. Wheel brakes………………Release momentarily
2. PM will select ANTI-SKID to OFF
3. Wheel Brakes…………..Re-apply as required
4. Reverse Thrust………….Apply maximum until stopping assured
208
All CRJ 700 and 900 Weight Limits:
700:
Ramp/Taxi - 75,250
Takeoff - 75,000
Landing - 67,000
Zero Fuel - 62,300
900:
Ramp/Taxi - 85,000
Takeoff - 84,500
Landing - 75,100
Zero Fuel - 70,750
209
All Flap and Gear Speeds
GEAR:
Landing Gear Extension: 220
Landing Gear Extended: 220
Landing Gear Retraction: 200
FLAPS:
Flaps 1: 230
Flaps 8: 230
Flaps 20: 220
Flaps 30: 185
Flaps 45: 170
