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CRJ700 > Limitations > Flashcards

Limitations Flashcards

1
Q

RVSM Required Equipment List

A

Equipment, Requirements:
Autopilot(1), Must be operational
Altitude Alerting System, Must be operational
Altitude Reporting Transponder (2),
One must be operational
Air Data Computers (2),
Two must be operational

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2
Q

Maximum Taxi and Ramp Weight

A

75,250 lbs.

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3
Q

Maximum Takeoff Weight

A

75,000 lbs.

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4
Q

Maximum Landing Weight

A

67,000 lbs.

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5
Q

Effect of landing gear retraction on CG position is:

A

Negligible.

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6
Q

Max airport pressure altitude for takeoff and landing is:

A

8,000 feet

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7
Q

Max operating altitude is

A

41,000 feet

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8
Q

Max ambient air temperature approved for for takeoff is:

A

ISA +35C

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9
Q

Minimum ambient temperature approved for takeoff is:

A

-40C

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10
Q

Cowl Anti-Ice, Ground Operations

A

Must be on when OAT is 10C or below AND visible moisture in any form is present (such as fog with visibility of 1,500 meters (1mile) 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.

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11
Q

Cowl Anti-Ice, Flight Operations

A

Must be on when in icing conditions, or ice is annunciated by the ice detection system.

EXCEPT when SAT is -40 or below

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12
Q

Define Icing Conditions (in-flight)

A

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

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13
Q

Wing Anti-Ice, Ground Operations

A

Must be on for takeoff when the OAT is 5C or below AND visible moisture in any form is present (such as fog with visibility of 1,500 meters (1mile) or less, rain, snow, sleet or ice crystals)

AND/OR the runway is contaminated with surface snow, slush, or standing water.

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14
Q

Wing Anti-Ice, Ground Operations – When Type II or Type IV anti-icing fluids have been applied:

A

Wing anti-ice system must only be selected on, if required, just prior to thrust increase for takeoff.

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15
Q

Wing Anti-Ice, Flight Operations

A

The wing anti-ice system must be on (EXCEPT when SAT is -40C or below) when:
Ice is annunciated by the ice detection system
In icing conditions and the airspeed is less than 230 KIAS

DO NOT HOLD IN ICING CONDITIONS WITH SLATS/FLAPS EXTENDED.

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16
Q

Supercooled Large Droplet Icing

A

Continued operations in areas where SLD icing conditions exist is prohibited.

Wing and cowl anti-icing systems must be on in SLD icing conditions.

Leave icing conditions when side window icing occurs.

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17
Q

How are SLD icing conditions indicated?

A

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

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18
Q

Cold Weather Ops

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)

Takeoff is permitted with frost adhering to:
Upper surface of the fuselage if it is possible to distinguish surface features.
Max 1/8in layer of frost on the underside of the wing that is caused by cold soaked fuel.

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19
Q

Runway Slopes

A

Max runway slopes approved for takeoff and landing are: +2% uphill and -2% downhill

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20
Q

Max tailwind component approved for takeoff and landing is

A

10knots

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21
Q

Ozone Concentration

A

Airplane operations prohibited on routes where ozone concentrations exceed:

.25 ppm by volume, sea level equivalent, at any time above FL320

.1 ppm by volume, sea level equivalent, time-weighted average during any 3 hour interval above FL270.

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22
Q

Engines

A

General Electric CF34-8C5B1

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23
Q

Engines High PWR Schedule Switchlight

A

Use of the Engines High PWR schedule switchlight is prohibited.

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24
Q

ITT Ground Start Temp Limit

A

815C

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25
Q

Oil Pressure Ground Start Limit

A

182PSI, 95PSI after 10min

Should show + value during start and may peak beyond 182PSI.

Oil pressure may be greater than 95PSI for a max of 10 minutes.

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26
Q

Engine Op Limits

A

Normal takeoff power and max power (two engines) is limited to 5 minutes.

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

ITT must be below 120C before attempting to ground start engine.

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27
Q

Continuous Engine Ignition must be used during:

A

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.

28
Q

Reduced (FLEX) Takeoff Thrust for takeoff is NOT authorized when:

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**

*FLEX thrust may be used for takeoff on wet runways, provided the flight crew selects “WET” runway performance data on the FMS MCDU

**GoJet utilizes a FAA-approved engine trend monitoring program, which continuously monitors engine parameters, and alerts maintenance when an engine begins to approach its deterioration limits. this program ensures compliance with rated thrust limitation, above.

29
Q

3-13.13.3 (Engine Start times) PG 17

A

See tablet.

30
Q

The max permissible fuel imbalance between the contents of left wing tank and right wing tank are:

A

During takeoff: 300 lbs

all other phases of flight: 800 lbs

31
Q

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

A

each main wing tank is above 4,400 lbs OR

each main wing tank is less than 4,400 lbs consult AFM limitations.

32
Q

Minimum fuel quantity for go-around is:

A

600 lbs per wing tank (airplane level) and assuming a max airplane climb altitude of 10deg nose up.

33
Q

APU starter motor duty cycle is limited to:

A

Not more than 3 starts/start attempts in 1 hour.

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

34
Q

VFE

A

Max flap extension speed.

Flaps 1 / 230KIAS
Flaps 8 / 230KIAS
Flaps 20 / 230KIAS
Flaps 30 / 185KIAS
Flaps 45 / 170KIAS
35
Q

VLO

A

Max gear extension/retract speed.

Extension: 220KIAS
Retraction: 200KIAS

36
Q

VLE

A

Max gear extended speed: 220KIAS (down and locked)

37
Q

Turbulence Penetration Speed

A

Max airspeed for turbulence penetration is 280KIAS or .75 Mach (whichever is lower)

38
Q

Minimum Operating Speed Limit

A

Intentional speed reduction below 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.

39
Q

Windshield Wiper Operations

A

Must not be operated above 250KIAS

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

40
Q

Maneuvering Limit Load Factors

A

Flaps Retracted: -1.0 to 2.5 G

Flaps Extended: 0.0 to 2.0 G

**Avoid unnecessary and large side-slip maneuvers during low speed high altitude cruise.

41
Q

Max Relief Differential Pressure (A/C & Pressurization)

A

8.7PSI

42
Q

Max Negative Differential Pressure (A/C & Pressurization)

A

-0.5PSI

43
Q

During taxi, takeoff and landing, the pressure differential must not exceed:

A

0.1PSI

44
Q

The airplane must be completely depressurized prior to:

A

Opening any of the airplane doors.

45
Q

To preclude possible crew and/or passenger ear damage:

A

use of the EMERG DEPRESS switch above 15,000 feet is prohibited.

46
Q

Max altitude for single pack operations is:

A

31,000 feet

47
Q

What does QRH Volume 1 contain?

A

Max allowable flight duration at altitude in accordance with 14CFR 25.832 (a)(2)

48
Q

Autopilot minimum use height: Takeoff

A

Minimum Use Height: 600 feet AGL

49
Q

Autopilot minimum use height: Non-Precision Approach

A

Airport elevation 4,000 feet approved

Minimum use height: 400 feet AGL

50
Q

Autopilot minimum use height: Precision Approach (Glidepath 3.5deg)

A

Airport elevation 4,000 feet approved

Minimum Use Height: 80 feet AGL

51
Q

Autopilot minimum use height: Precision Approach (Glidepath > 3.5deg, <= 4.0deg)

A

Airport elevation 4,000 feet prohibited

Minimum Use Height: 120 feet AGL

52
Q

ADC Source and flight in RVSM airspace

A

The ADC source coupled to the active autopilot must be the same as that coupled to the ATC Transponder during flight in RVSM airspace.

53
Q

Permissible AC Electrical System Loads

A

Individual AC generator loading must not exceed:

0 to 41,000 feet: Main Generator (each) 40kVA
0 to 41,000 feet: APU Generator 40kVA

54
Q

In-Flight, Max permissible continuous load on each TRU is:

A

120 amps

55
Q

Ground Operation, Protect CRT displays

A

Max permissible time for ground operations with DC power is 5 minutes.

56
Q

Circuit Breaker Reset (in-flight)

A

A circuit breaker must not be reset or cycled unless doing so is consistent with explicit procedures specified in the Airplane Flight Manual or unless PIC deems necessary for safe completion of the flight.

57
Q

Slats/Flaps

A

Enroute use of slats/flaps is prohibited.

Flight with slats/flaps extended at altitudes above 15,000 feet is prohibited.

58
Q

Flight Spoilers

A

Flight spoilers must not be extended in-flight below an altitude of 300 feet AGL.

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

59
Q

Stall Protection

A

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

60
Q

Thrust Reversers

A

Approved for ground use only.

Intended for use during full stop landings

Go-around not to be attempted after activating thrust reversers

Takeoff with thrust reverser icons or EICAS warning and/or caution message displayed is prohibited.

Below 75KIAS, reverse thrust must be less than 60% N1

Backing up using reverse thrusters is prohibited.

61
Q

Taxi Lights

A

Must be switched off whenever airplane is stationary in excess of 10 minutes

62
Q

Wheel brake cooling limitations

A

There must be sufficient time to allow brake cooling between a rejected takeoff and subsequent takeoff to make sure there is enough brake energy to bring the aircraft to a stop in the event of another rejected takeoff.

63
Q

Nose Wheel Steering System (Towbarless Towing)

A

Towbarless towing is prohibited unless performed in compliance with Airplane Maintenance Manual towbarless towing requirements.

64
Q

When setting MDA marker on the barometric altimeter using the DH/MDA knob on the altitude reference panel the next highest 10-foot increment must be:

A

selected if the altitude is not at a 10-foot increment.

65
Q

TCAS (Authorized, action after TCAS RA)

A

Authorized to deviate from ATC clearance in order to comply with TCAS resolution advisory (RA) command.

Notify dispatch after compliance with TCAS RA.

CRJ700 (2 decks)

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