SOP Chapter 3 Flashcards

Question 1

Q

3-1.1 Kinds of Airplane Operation

Answer

A

Day and night operations
VFR and IFR
Flight in icing conditions
The airplane is certified for ditching when the safety equipment specified by the applicable regulations is installed.
The airplane is certified capable of RVSM operations

Question 2

Q

3-1.1 Kinds of Airplane Operation

RVSM REQUIRED EQUIPMENT LIST

Answer

A

EQUIPMENT: REQUIREMENTS FOR RVSM

AUTOPILOT (1): MUST BE OPERATIONAL

ALTITUDE ALERTING SYSTEM: MUST BE OPERATIONAL ALTITUDE REPORTING TRANSPONDER (2): ONE (1) MUST BE OPERATIONAL

AIR DATA COMPUTERS (2) TWO : (2) MUST BE OPERATIONAL

Question 3

Q

Memory Item - Double Boxed

3-2 STRUCTURAL WEIGHT LIMITATIONS

CRJ700 Structural Weight Limitations

CRJ900 Structural Weight Limitations

CRJ550 Structural Weight Limitations

Answer

A

CRJ 900, 700, 550

Maximum Taxi and Ramp Weight 85,000 lbs==75250==66000

Maximum Takeoff Weight 84,500 lbs==75000===65000

Maximum Landing Weight 75,100 lbs==67000==61==

Maximum Zero Fuel Weight 70,750 lbs==62300==59000

Minimum Flight Weight 45,000 lbs==42000==42000

====================================

Minimum Operating Empty Weight 39,835 lbs (only crj700)

===================================

Note: The maximum takeoff weight (MTOW) and/or maximum landing weight (MLW) may be further limited due to performance consideration(s).

Question 4

Q

The information presented in this chapter (chapter 3 of sop - limitations) contains limitations that have been extracted from the

Answer

A

Aircraft Flight Manual (AFM) and

Flight Crew Operating Manual (FCOM).

The limitations in this chapter are not all inclusive.

Question 5

Q

3-3.1 CRJ700 Center-of-Gravity Limits

Question 6

Q

3-3.2 CRJ550 Center-of-Gravity Limits

Question 7

Q

3-3.3 CRJ900 Center-of-Gravity Limits

Question 8

Q

3-4 ALTITUDE AND TEMPERATURE OPERATING LIMITS

Maximum airport pressure altitude for takeoff and landing

Answer

A

Maximum airport pressure altitude for takeoff and landing is 8,000’

Question 9

Q

3-4 ALTITUDE AND TEMPERATURE OPERATING LIMITS

Maximum operating altitude

Answer

A

Maximum operating altitude is 41,000’

Question 10

Q

3-4 ALTITUDE AND TEMPERATURE OPERATING LIMITS

The maximum ambient air temperature approved for takeoff and landing

Answer

A

The maximum ambient air temperature approved for takeoff and landing is ISA +35°C.

Question 11

Q

3-4 ALTITUDE AND TEMPERATURE OPERATING LIMITS

The minimum ambient temperature approved for takeoff

Answer

A

The minimum ambient temperature approved for takeoff is -40°C (-40°F).

Question 12

Q

Memory Item - Double Boxed

3-5 OPERATION IN ICING CONDITIONS

3-5.1 Cowl Anti-Ice System

3-5.1.1 Ground Operations

Answer

A

Cowl anti-ice system must be ON when the OAT is 10°C (50°F) or below:

and visible moisture in any form is present (such as fog with visibility of 1,500 meters [1 mile] or less, rain, snow, sleet and ice crystals)
when operating on runways, ramps or taxiways where surface snow, ice, standing water, or slush is present

photo

Question 13

Q

Memory Item - Double Boxed

3-5 OPERATION IN ICING CONDITIONS

3-5.1 Cowl Anti-Ice System

3-5.1.3 Flight Operations

Answer

A

Icing conditions exist in-flight at a TAT of 10°C (50°F) or below, and visible moisture in any form is encountered (such as clouds, rain, snow, sleet or ice crystals), except when the SAT is -40°C (-40°F) or below.

The engine cowl anti-ice system must be ON when:

in icing conditions, or
ICE is annunciated by the ice detection system

photo

Question 14

Q

Memory Item - Double Boxed

3-5 OPERATION IN ICING CONDITIONS

3-5.3 Wing Anti-Ice System

3-5.3.1 Ground Operations

Answer

A

Wing anti-ice system must be ON for takeoff when the OAT is 5°C (41°F) or below and:

visible moisture in any form is present (such as fog with visibility of 1,500 meters [1 mile] or less, rain ,snow, sleet and ice crystals)
the runway is contaminated with surface snow, slush or standing water

When Type II or Type IV anti-icing fluids have been applied:

• wing anti-ice system must only be selected ON, if required, just prior to thrust increase for takeoff

photo

Question 15

Q

Memory Item - Double Boxed

3-5 OPERATION IN ICING CONDITIONS

3-5.3 Wing Anti-Ice System

3-5.3.3 Flight Operations

Answer

A

Icing conditions exist in-flight at a TAT of 10°C (50°F) or below, and visible moisture in any form is encountered (such as clouds, rain, snow, sleet or ice crystals), except when the SAT is -40°C (-40°F) or below.

The wing anti-ice system must be ON when:

ICE is annunciated by the ice detection system, or
in icing conditions and the airspeed is less than 230 KIAS

NOTE Do not hold in icing conditions with Slats/Flaps extended.

photo

Question 16

Q

Memory Item - Double Boxed

3-5 OPERATION IN ICING CONDITIONS

3-5.5 Supercooled Large Droplet Icing

Answer

A

Continued operation in areas where supercooled large droplet (SLD) icing conditions exist is prohibited.

SLD icing conditions are indicated by ice accretion on the flight deck side windows.

wing and cowl anti-icing systems must be ON in SLD icing conditions
leave icing conditions when side window icing occurs

photo

Question 17

Q

Memory Item - Double Boxed

3-6 COLD WEATHER OPERATIONS

Answer

A

Take-off is prohibited with frost, ice, snow or slush adhering to any critical areas (wings, upper fuselage, horizontal stabilizer, vertical stabilizer, control surfaces, and engine inlets).

Question 18

Q

3-6 COLD WEATHER OPERATIONS

Takeoff is permitted with frost adhering to:

Answer

A

• The upper surface of the fuselage if it is possible to distinguish surface features. See WOP 2.13.1;

and/or

• Maximum 1/8 in (3.0 mm) layer of frost on the underside of the wing that is caused by cold soaked fuel.

Comprehensive procedures for operating in cold weather are provided in the WOP.

Question 19

Q

3-7 RUNWAY SLOPES

The maximum runway slopes approved for takeoff and landing are:

Answer

A

+2% (uphill)
-2% (downhill)

Question 20

Q

Memory Item - Double Boxed

3-8 TAILWIND CONDITIONS

The maximum tailwind component approved for takeoff and landing is ====== knots.

Answer

A

10 knots.

Question 21

Q

3-9 MINIMUM FLIGHT CREW

The minimum flight crew is

Answer

A

one (1) pilot and one (1) copilot.

Question 22

Q

3-10 FLIGHT DECK DOOR

Answer

A

The flight deck door must be kept closed and locked at all times during flight except to permit access and egress in accordance with the approved procedures for opening, closing and locking the door.
Any time 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.
Any time one of the required flight crew leaves the flight deck another crew member must be present in the flight deck to ensure that the required crew member is not locked out of the flight deck.

Question 23

Q

3-11 CARGO

Flight must be within ==== minutes of a suitable airport, if cargo is carried in any ===========

Answer

A

Flight must be within 60 minutes of a suitable airport, if cargo is carried in any labeled cargo compartment.

Question 24

Q

Aircraft Stowage/Cargo Dimensions

3-11 CARGO

Question 25

Q

3-12 OZONE CONCENTRATION

limits?

Answer

A

Airplane operations are prohibited on routes where ozone concentrations will exceed the following limits:

0.25 parts per million by volume, sea level equivalent, at any time above flight level 320, and
0.1 parts per million by volume, sea leve

Question 26

Q

3-12 OZONE CONCENTRATION

‘Sea level equivalent’ refers to ???

Answer

A

‘Sea level equivalent’ refers to conditions of 25°C and 760 millimeters of mercury pressure.

Airplane operations are prohibited on routes where ozone concentrations will exceed the following limits:

0.25 parts per million by volume, sea level equivalent, at any time above flight level 320, and
0.1 parts per million by volume, sea level equivalent, time-weighted average during any three (3) hour interval above flight level 270

Question 27

Q

3-12 OZONE CONCENTRATION

Data to determine flight altitudes and/or duration at altitude in compliance with these requirements are given in

Answer

A

Flight Planning and Cruise Control Manual, Chapter 6, SPECIAL OPERATIONS, Maximum Allowable Cabin Ozone Concentration. Flight crews may utilize SOP 3-28.3, Maximum Flight Duration at Altitude Due to Cabin Ozone Concentration, for determining flight duration at altitudes higher than originally planned by Dispatch.

Question 28

Q

3-13 ENGINES

3-13.1 Engine Indications

The CRJ700 and CRJ550 aircraft use two (2) General Electric ============= engines.

The CRJ900 aircraft uses two (2) General Electric ============= engines.

Answer

A

The CRJ700 and CRJ550 aircraft use two (2) General Electric CF34-8C5B1 engines.

The CRJ900 aircraft uses two (2) General Electric

CF34-8C5 engines.

Question 29

Q

3-13 ENGINES

3-13.1 Engine Indications

The engine limit display markings on ======= must be used to determine compliance with the maximum/minimum limits and precautionary ranges.

If EICAS markings show more conservative limits than those specified in sop chapter 3, the limit markings on the ======== must be used.

Answer

A

The engine limit display markings on EICAS must be used to determine compliance with the maximum/minimum limits and precautionary ranges.

If EICAS markings show more conservative limits than those specified sop chapter 3, the limit markings on the EICAS must be used.

Question 30

Q

3-13 ENGINES

3-13.1 Engine Indications

Question 31

Q

3-13.2 Powerplant Intermix

Answer

A

Powerplant intermix operations are prohibited

Question 32

Q

3-13.3 Engine Warm-up

The engine must remain at ———– until oil pressure reaches

Answer

A

The engine must remain at IDLE until oil pressure reaches normal operating range.

Question 33

Q

3-13.3 Engine Warm-up

During all starts, do not exceed —- for ——- minutes after start, or ——————–]

???

Answer

A

During all starts, do not exceed 75% N1 for

two (2) minutes after start,

or until all operating indications are in the normal range, whichever is longer.

Question 34

Q

3-13.4 Thrust Management Data

With the engines running and bleeds configured for take-off, the crew must verify ………………….. .

Refer to ……………. .

With the thrust levers set for take-off, ——-and ——— values should ————–.

Answer

A

3-13.4 Thrust Management Data

With the engines running and bleeds configured for take-off, the crew must verify that the target N1 values correspond to the data presented in the thrust setting charts (± 1.0%).

Refer to PERFORMANCE – THRUST SETTINGS. With the thrust levers set for take-off, target and actual N1 values should match.

Question 35

Q

**** Memory Item - Double Boxed *****

3-13.5 Engines High-Power Schedule Switchlight

Answer

A

Use of the ENGINES HIGH PWR SCHEDULE switchlight is

prohibited.

Question 36

Q

3-13.7 Engine Operating Limits

N1?

Question 37

Q

3-13.7 Engine Operating Limits

N2?

Question 38

Q

**** Memory Item - Double Boxed *****

3-13.7 Engine Operating Limits

ITT?

Question 39

Q

3-13.7 Engine Operating Limits

OIL TEMP?

Question 40

Q

**** Memory Item - Double Boxed *****

3-13.7 Engine Operating Limits

OIL Pressure?

Question 41

Q

3-13.7 Engine Operating Limits

MINIMUM OIL LEVEL FOR FLIGHT?

Question 42

Q

**** Memory Item - Double Boxed *****

3-13.7 Engine Operating Limits

[1] Normal takeoff power and maximum power (two engines) is limited to ——– minutes.

Answer

A

[1] Normal takeoff power and maximum power (two engines) is limited to 5 minutes.

Question 43

Q

**** Memory Item - Double Boxed *****

3-13.7 Engine Operating Limits

[2] APR power (one engine) is limited to 10 minutes.

Answer

A

[2] APR power (one engine) is limited to 10 minutes.

Question 44

Q

**** Memory Item - Double Boxed *****

3-13.7 Engine Operating Limits

[3] ITT must be below ———- before attempting to ground start engine.

Answer

A

[3] ITT must be below 120°C before attempting to ground start engine.

Question 45

Q

3-13.7 Engine Operating Limits

[4] ITT must be below ———- before attempting to air start engine.

Answer

A

[4] ITT must be below 90°C before attempting to air start engine.

Question 46

Q

3-13.7 Engine Operating Limits

[5] Maximum oil pressure is limited to ——— psi when oil temperature transient is less than ———— .

Answer

A

[5] Maximum oil pressure is limited to 156 psi when oil temperature transient is less than 60°C.

Question 47

Q

3-13.7 Engine Operating Limits

[6] Oil pressures (above IDLE) between ………………..

????

Answer

A

[6] Oil pressures (above IDLE) between 25 and 45 psi require oil temperature monitoring.

Question 48

Q

3-13.7 Engine Operating Limits

[7] Oil pressures should show ——— value during start and may peak beyond———- max display value).
Oil pressures ———- are displayed as amber dashes.
Oil pressure may be greater than …………….. minutes

Answer

A

[7] Oil pressures should show positive value during start and may peak beyond 182 psi (max display value).
Oil pressures above 182 psi are displayed as amber dashes.
Oil pressure may be greater than 95 psi for a maximum of ten (10) minutes

Question 49

Q

3-13.9 Airplane Cold Soak

Answer

A

Before the first flight of a day, when the airplane is cold-soaked at an ambient temperature of -30°C (-22°F)

or below for more than eight (8) hours:

the engines must be motored for 60 seconds and the fan rotation must be verified before an engine start is initiated
thrust reversers must be actuated until the deploy and stow cycles are two (2) seconds or less

Question 50

Q

**** Memory Item - Double Boxed *****

3-13.11 Continuous Engine Ignition

Answer

A

Continuous engine ignition must be used during the following:

takeoffs and landings on contaminated runways
flight through moderate or heavier intensity rain
flight through moderate or heavier intensity turbulence
flight in the vicinity of thunderstorms

Question 51

Q

**** Memory Item - Double Boxed *****

3-13.12 Reduced (FLEX) Takeoff Thrust

Note: FLEX thrust may be used for takeoff on wet runways, ….

????

Answer

A

Note: FLEX thrust may be used for takeoff on wet runways, provided the flight crew selects “WET” runway performance data on the FMS MCDU (ACARS) PERF WT & BALANCE, CONDITIONS, page 1

Question 52

Q

**** Memory Item - Double Boxed *****

3-13.12 Reduced (FLEX) Takeoff Thrust

The use of Reduced/FLEX thrust for takeoff is not authorized when:

Answer

A

Wing and/or cowl anti-ice bleeds are in use
Runway is contaminated with standing water, slush, snow, or ice*
Warnings or forecasts of windshear or downdrafts exist (including LLWAS advisories)
Antiskid system is inoperative
The engine cannot achieve full rated thrust **

Question 53

Q

3-13.13 Engine Starter

3-13.13.1 Associated Starter Conditions

The starter must not be used if

Answer

A

The starter must not be used if indicated N2 rpm exceeds 45%.

Question 54

Q

3-13.13 Engine Starter

3-13.13.1 Associated Starter Conditions

At initiation of thrust lever movement from SHUT OFF to IDLE:

Answer

A

ITT must be 120°C or less for all ground starts
ITT must be 90°C or less for all air starts

Question 55

Q

**** Memory Item - Double Boxed *****

3-13.13.3 CRJ Starter Cranking Limits

All

Question 56

Q

3-13.13.3 CRJ Starter Cranking Limits

Ground Start

Question 57

Q

**** Memory Item - Double Boxed *****

3-13.13.3 CRJ Starter Cranking Limits

Ground , Motoring

Question 58

Q

**** Memory Item - Double Boxed *****

3-13.13.3 CRJ Starter Cranking Limits

Flight

Motoring & Starter

Question 59

Q

**** Memory Item - Double Boxed *****

3-13.13.3 CRJ Starter Cranking Limits

All

Question 60

Q

3-13.13.5 Engine Relight Limitations

3-13.13.5.1 CRJ550/700 (CF34-8C5B1) Engine Relight Limitations

3-13.13.5.3 CRJ900 (CF34-8C5) Engine Relight Limitations

Windmilling

Starter Assisted

All-Engine-Out Rapid Relight

Answer

A

Note: FADEC rapid relight capability has been demonstrated at 200 KIAS for up to 15-second fuel interruptions.

Question 61

Q

3-13.13.5 Engine Relight Limitations

3-13.13.5.1 CRJ550/700 (CF34-8C5B1) Engine Relight Limitations

Windmilling

Starter Assisted

All-Engine-Out Rapid Relight

Question 62

Q

3-13.13.5 Engine Relight Limitations

3-13.13.5.3 CRJ900 (CF34-8C5) Engine Relight Limitations

Windmilling

Starter Assisted

All-Engine-Out Rapid Relight

Question 63

Q

900 Engine Start Envelope Figure

Note: Special All-Engine-Out rapid relight envelope is from ——————– to ————— and ——————- to ———————- KIAS.

Answer

A

Note: Special All-Engine-Out rapid relight envelope is from 10,000’ to SL and 200 to 250 KIAS.

Question 64

Q

550/700 Engine Start Envelope Figure

Note: Special All-Engine-Out rapid relight envelope is from ——————– to ————— and ——————- to ———————- KIAS.

Answer

A

Note: Special All-Engine-Out rapid relight envelope is from 10,000’ to SL and 200 to 250 KIAS.

Answer 47

A

Center tank fuel quantity must be monitored throughout the flight.

Answer 48

A

• during takeoff: 300 lbs (136 kg)

Answer 49

A

• all other phases of flight: 800 lbs (363 kg)

Answer 50

A

is not usable.

Answer 51

A

Fuel quantities are based on 6.75 lbs per U.S. gal and 2.2046 lbs per kg conversion factors.

Answer 52

A

550 , 700 and 900 all are the same

Answer 53

A

550 , 700 and 900 all are the same

Answer 54

A

Takeoff with a fuel load in excess of 500 lbs in the center tank is not permitted unless:

each main wing tank is above 4,400 lbs, or
if each main wing tank is less than 4,400 lbs consult the Aircraft Flight Manual’s Limitations section for additional requirements

Answer 55

A

is 600 lbs per wing tank (with the airplane level)

and

assuming a maximum airplane climb altitude of 10° nose up.

Answer 56

A

For ground operations, the right and left tank quantities should never have a difference greater than 2500 lbs.

Answer 57

A

5°C (41°F) is prohibited.

Answer 58

A

During flight, bulk fuel temperature must remain above the applicable bulk fuel freezing point

Answer 59

A

Airplane Flight Manual.

Answer 60

A

consult the Aircraft Flight Manual’s Limitations section.

Answer 61

A

Powered crossflow and gravity crossflow must be OFF for takeoff.

Answer 62

A

Maximum oil consumption on each engine is 189 cubic centiliters per hour

(6.4 U.S. ounces per hour)

(0.05 U.S. gallons per hour).

Answer 63

A

Mixing of different types of oils is prohibited.

Answer 64

A

the maximum duration without engine oil servicing is 36 operating hours
for airplane operations in excess of 36 operating hours (without engine oil tank servicing), the engine oil level must be checked within three (3) minutes to two (2) hours after every engine shutdown

Answer 65

A

36 operating hours

Answer 66

A

within three (3) minutes to two (2) hours after every engine shutdown

Answer 67

A

If use of the oil replenishment system is required, then the engine(s) should be replenished within 15 minutes to two (2) hours after engine shutdown.

Answer 68

A

Allied Signal RE 220 (RJ)

Answer 69

A

-40°C (-40°F)

Answer 70

A

• 0 to 100 % RPM 692ºC to 1038ºC

Answer 71

A

3 starts/start attempts in 1 hour.

Answer 72

A

2 minute delay must be observed between cranking attempts to allow for cooling of starter and starter contactor and APU fuel drainage.

Answer 73

A

Maximum RPM: 106%

Maximum EGT: 1038°C (do not exceed under any operating condition).

Answer 74

A

APU bleed air extraction is not permitted above 25,000 feet.

Answer 75

A

No bleed air extraction limitation.

Each engine may be started using the APU as a bleed air source.

Answer 76

A

The maximum permissible load on the APU generator is 40 kVA.

Answer 77

A

The APU limit display markings on the EICAS must be used to determine compliance with the maximum limit and precautionary ranges.

If EICAS markings show more conservative limits than those specified below, the limit markings on the EICAS should be used.

NOTE

Red — Maximum Limitations

Green — Normal Operating Range

Answer 78

A

APU EGT

Red: 807 °C

Green: 0 to 806 °C

The APU limit display markings on the EICAS must be used to determine compliance with the maximum limit and precautionary ranges. If EICAS markings show more conservative limits than those specified below, the limit markings on the EICAS should be used.

Answer 79

A

APU RPM %

Red: 107

Green: 0 to 106

The APU limit display markings on the EICAS must be used to determine compliance with the maximum limit and precautionary ranges. If EICAS markings show more conservative limits than those specified below, the limit markings on the EICAS should be used.

Answer 80

A

The CRJ550/700 Maximum cruise Mach number during flight in RVSM airspace is 0.83.

The CRJ900 Maximum cruise Mach number during flight in RVSM airspace is 0.82.

Answer 81

A

CRJ550/700 VFE CRJ900 VFE

Answer 82

A

CRJ550/700 VFE CRJ900 VFE

Answer 83

A

CRJ550/700 VFE CRJ900 VFE

Answer 84

A

CRJ550/700 VFE CRJ900 VFE

Answer 85

A

CRJ550/700 VFE CRJ900 VFE

Answer 86

A

Extension 220 KIAS

Down and Locked 220 KIAS

Retraction 200 KIAS

Answer 87

A

CRJ550/700 maximum tire limit speed is 182 knots ground speed. CRJ900 maximum tire limit speed is 195 knots ground speed.

Answer 88

A

The maximum speed for ADG operation is VMO/MMO.

Answer 89

A

Maximum airspeed for turbulence penetration is 280 KIAS or 0.75 Mach, whichever is lower.

Answer 90

A

Intentional speed reduction below the onset of stall warning, as defined by stick shaker operation, is prohibited unless a lower speed is specifically authorized for flight test or training operations.

Answer 91

A

The windshield wiper must not be operated above 250 KIAS.

Answer 92

A

If the windshield wiper has failed in a non-parked position, the airplane speed must not exceed 250 KIAS

Answer 93

A

Phase of Operation Maximum “G” Loading

Flaps Retracted -1.0 to 2.5 G

Flaps Extended 0.0 to 2.0 G

Answer 94

A

Phase of Operation Maximum “G” Loading

Flaps Extended 0.0 to 2.0 G

Answer 95

A

The maximum relief differential pressure is 8.7 psi.

Answer 96

A

The maximum negative differential pressure is -0.5 psi.

Answer 97

A

During taxi, takeoff and landing, the pressure differential must not exceed 0.1 psi.

Answer 98

A

The airplane must be completely depressurized prior to opening any of the airplane doors.

Answer 99

A

To preclude possible crew and/or passenger ear damage, use of the EMERG DEPRESS switch above 15,000’ is prohibited.

Answer 100

A

The CRJ550/700 maximum altitude for single pack operation is 31,000’.

Answer 101

A

The CRJ900 maximum altitude for single pack operation is 25,000’.

Answer 102

A

0 to 41,000’

Load Limitation

Main Generator (each) 40 kVA

APU Generator 40 kVA

Answer 103

A

• maximum permissible continuous load on each TRU is 120 amps

Answer 104

A

Ground Operation:

• to protect the CRT displays, the maximum permissible time for ground operations with DC power is 5 minutes.

Answer 105

A

A circuit breaker must not be reset or cycled (i.e., opened or closed) unless doing so is consistent with explicit procedures specified in the Airplane Flight Manual or unless, in the judgment of the Pilot in Command, that resetting or cycling of the circuit breaker is necessary for the safe completion of the flight.

Answer 106

A

Enroute use of Slats/Flaps is prohibited.

Flight with Slats/Flaps extended at altitudes above 15,000’ is prohibited.

Answer 107

A

1- Flight spoilers must not be extended in-flight below an altitude of 300’ AGL

2- To ensure adequate maneuver margins, flight spoilers must not be extended in-flight at airspeeds below the recommended approach speed plus 10 KIAS.

Answer 108

A

Both stall protection system switches must remain on for all phases of flight.

Answer 109

A

Thrust reversers are approved for ground use only, activation of the reverse thrust levers is prohibited in-flight.

Answer 110

A

The thrust reversers are intended for use during full stop landings.

Do not attempt a go-around maneuver after deployment of the thrust reversers.

Answer 111

A

Takeoff with any thrust reverser icons or EICAS warning and/or caution messages displayed is prohibited

Answer 112

A

During landing, maximum reverse thrust is prohibited below 75 KIAS, and reverse idle should be achieved by 60 KIAS.

Answer 113

A

Backing-up using thrust reversers is prohibited.

Answer 114

A

The taxi lights must be switched OFF whenever the airplane is stationary in excess of 10 minutes.

Answer 115

A

Brake cooling times must be observed between a landing or rejected takeoff (RTO) and a subsequent takeoff to:

ensure that sufficient brake energy is available to bring the airplane to a complete stop, if the subsequent takeoff is rejected.

Answer 116

A

With an anti-skid channel inoperative on the CRJ900, takeoff from a wet runway is prohibited.

Answer 117

A

When setting the MDA/DDA marker on the barometric altimeter using the DH/MDA/DDA knob on the altitude reference panel, the next highest 10-foot increment must be selected if the altitude is not at a 10-foot increment.

Answer 118

A

When setting the MDA/DDA marker on the barometric altimeter using the DH/MDA/DDA knob on the altitude reference panel, the next highest 10-foot increment must be selected if the altitude is not at a 10-foot increment.

Answer 119

A

Pilots are authorized to deviate from their Air Traffic Control (ATC) clearance in order to comply with a TCAS resolution advisory (RA) command.

Pilots shall notify Dispatch after compliance with a TCAS RA, as defined in GOM 1-8.6.5.

Answer 120

A

If the aircraft is to be operated with certain secondary airframe and/or any nacelle parts missing, operation must be in accordance with the limitations specified in the basic Airplane Flight Manual, and as amended by the Configuration Deviation List.

Answer 121

A

When NAV 1 is tuned to a valid ILS frequency, the ISI will display localizer and glideslope deviation while on the backcourse approach.

Use of the ISI localizer and backcourse information is prohibited during backcourse approaches.

Answer 122

A

• Airplane navigation must not be predicated upon the use of the terrain display.

Answer 123

A

• To avoid giving unwanted alerts, the terrain awareness alerting and display functions must be inhibited on takeoff, approach or landing within 15 nm of an airport not contained in the EGPWS airport database.

Answer 124

A

• If GPS is inoperative

identified by NO GPS RAIM,

GPS NOT AVAILABLE or

GPS-FMS DISAGREE

message on the FMS CDU)

Answer 125

A

• 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 United States and Mexico.

Answer 126

A

• The terrain awareness alerting and display functions must be inhibited during QFE (atmospheric pressure at airport elevation) operations

Answer 127

A

The EGPWS may fail to alert when a terrain threat exists, during ambient surface temperatures below ISA, during non-standard temperature lapse rates or if incorrect barometric settings are set on the altimeter.

Answer 128

A

The ACARS is approved for the transmission and receipt of messages that will not create an unsafe condition if the message is improperly received.

Answer 129

A

An unsafe condition may exist if:

The message or part of the message is delayed or not received,
The message is delivered to the wrong recipient, or
The message content is corrupted.

Answer 130

A

Crew actions based on messages such as pre-departure clearance, digital automatic terminal information service, weight and balance, take-off data (speeds, trim settings, runway distances), are prohibited, unless approved operational procedures are used to verify that the message is received by the intended recipient, that the message is valid and that the content is not corrupted.