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CRJ 550 Mem items/Limitations > LIMITATIONS > Flashcards

LIMITATIONS Flashcards

1
Q

RVSM REQUIRED EQUIPMENT LIST

A

1.AUTOPILOT (1) ……. MUST BE OPERATIONAL
2.ALTITUDE ALERTING SYSTEM ……. MUST BE OPERATIONAL
3.ALTITUDE REPORTING TRANSPONDER (2) ……. ONE (1) MUST BE OPERATIONAL
4.AIR DATA COMPUTERS (2) ……. TWO (2) MUST BE OPERATIONAL

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2
Q

MAX TAXI & RAMP WEIGHT

A

66,000LBS

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3
Q

MAX TAKEOFF WEIGHT

A

65,000LBS

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4
Q

MAX LANDING WEIGHT

A

61,000LBS

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5
Q

MAX ZERO FUEL WEIGHT

A

59,000LBS

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6
Q

MINIMUM FLIGHT WEIGHT

A

42,000LBS

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7
Q

MAX PRESSURE ALTITUDE FOR TAKEOFF AND LANDING

A

8,000’

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8
Q

MAX OPERATING ALTITUDE

A

41,000’

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9
Q

MAX TAKEOFF & LANDING TEMPERATURE °C

A

ISA +35°C

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10
Q

MIN TEMPERATURE °C for TAKEOFF

A

-40°C (-40°F)

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11
Q

COWL ANTI ICE MUST BE ON WHEN (ground operation) …

A

When OAT is 10°C (50°F) or below:
•Any form of visible moisture (fog with vis 1500m [1mi], rain, snow, sleet, ice crystals)
•Operating on runways, ramps, taxiways where surface snow, ice, standing water or slush is present

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12
Q

COWL ANTI ICE MUST BE ON WHEN (flight operation) …

A

icing conditions exist in flight when TAT is 10°C (50°F) or below & vis moisture is encountered except when SAT is -40°C (-40°F) or below
•In icing conditions, or
•ICE is annunciated by the ice detection system

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13
Q

WING ANTI ICE (ground operations)

A

Must be on for takeoff when OAT 5°C (41°F) or below and:
•vis moisture present
•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

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14
Q

SUPERCOOLED LARGE DROPLET ICING

A

Continued operation PROHIBITED
SLD icing conditions indicated by ice accretion on flight deck side windows.

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

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15
Q

Takeoff is permitted with frost adhering to:

A

•the upper surface of the fuselage if it is possible to distinguish surface features and/or
•Maximum 1/8 in (3.0mm) layer of frost on the underside of the wing that is caused by cold soaked fuel

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16
Q

MAX RUNWAY SLOPES FOR TAKEOFF AND LANDING

A

• +2% (uphil)
• -2% (downhill)

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17
Q

MAX TAILWIND COMPONENT TAKEOFF &LANDING

A

10knots

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18
Q

MINIMUM FLIGHT CREW

A

One (1) pilot and one (1) copilot

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19
Q

FLIGHT DECK DOOR

A

-Must be closed at all times except for approved opening, closing, and locking procedures
-if opened in flight, challenge and response verification must be used to verify door is closed and locked
-if one required flight crew leaves another must be present to ensure required crew member is not locked out

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20
Q

CARGO

A

•flight must be within 60mins of suitable airport if cargo is carried in any labeled cargo compartment

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21
Q

UNDERSEAT STOWAGE/CARGO DIMENSIONS

A

Total volume 99cu ft ……. Intended capacity 12lbs per seat

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22
Q

OVERHEAD STOWAGE/CARGO DIMENSIONS

A

Total Volume 97.8 cu ft ……. Max total capacity of 1,180lbs

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23
Q

FWD CARGO STOWAGE/CARGO DIMENSIONS

A

109 cu ft … MAX 1,000lbs

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24
Q

AFT CARGO STOWAGE/CARGO DIMENSIONS

A

374 cu ft/296 cu ft ……. MAX 3,740lbs/2710lbs

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25
Q

LH FWD TOP/LH FWD BOTTOM Carry-on Baggage Monument

A

100lbs/133.5lbs

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26
Q

LH MID TOP/LH MID BOTTOM Carry-on Baggage Monument

A

83.5lbs/167lbs

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27
Q

RH MID FWD TOP/RH MID FWD BOTTOM Carry-on Baggage Monument

A

125lbs/125lbs

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28
Q

RH MID AFT TOP/RH MID AFT BOTTOM Carry-on Baggage Monument

A

125lbs/125lbs

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29
Q

Takeoff is permitted with frost adhering to:

A

•Upper surface of fuselage
•Underside of wing, caused by cold-soaked fuel (<1/8”)

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30
Q

MIN OPERATING EMPTY WEIGT

A

CRJ 700 - 39,835 lbs.

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31
Q

1/2 Bank automatically turns on at …

A

36,000 feet

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32
Q

Passenger bags

A

Standard: 35
Heavy: 58

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33
Q

Jumpseat Max Weight (front)

A

254

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34
Q

Supercooled Large Droplets

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

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35
Q

Engines High-Power Schedule Switchlight

A

Commands both engines to apt thrust

Use of the ENGINES HIGH PWR SCHEDULE switchlight is prohibited.

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36
Q

N1 % RPM

A

Green = 0% - 99.4%

Red = 99.5%

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37
Q

N2 % RPM

A

Green = 0% - 99.3%

Red = 99.4%

38
Q

Engine Oil Temp °C

A

Green = -40° - 155°
Amber = 156° - 163°
Red = 164°

39
Q

Engine Oil Pressure psi

A

Green & Amber = varible

Red = 0-24psi

40
Q

Max ITT °C Ground Start

A

815°C

41
Q

Oil Pressure Ground Start Max
(Amber)

A

Amber(max displayed temp) = 182psi
(may exceed 182psi during start)

-oil pressure may be greater than 95psi for a max of 10mins

42
Q

External Aircraft Dimensions

A

(Dimensions depend on the aircraft weight and cg)

Height = 24’ 10”
Wingspan = 76’ 3”
Length = 106’ 8”

43
Q

At what pressure is oxygen cylinder pressure vented overboard?

A

2500-2775psi

44
Q

Max engine performance at sea level

A

Normal takeoff thrust = 12670lb
Max Takeoff Thrust (APR) = 13790lb
Max continuous thrust = 13280lb

45
Q

The Accessory Gearbox (AGB) drives:

A

•Lubricating pumps
•FADEC alternator
•Hydraulic pump
•Engine fuel pump
•Fuel control unit (FCU)
•Integrated drive generator (IDG)
•Air Turbine Starter (ATS)

46
Q

Normal takeoff power and maximum power (two engines) is limited to:

A

5 minutes

47
Q

APR power (one engine) is limited to

A

10 minutes

48
Q

ITT must be below ______ before attempting to ground start engine.

A

120°C

49
Q

ITT must be below ____ before attempting to air start engine.

A

90°C

50
Q

Continuous engine ignition must be used during the following:

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

51
Q

Starter cranking limits
Engine Start (ground)

A

1&2 / 90 seconds / 10 second cool down
3-5 / 90 seconds / 5 minutes cool down

52
Q

Starter cranking limits
Engine start or motoring (flight)

A

1 / 120 seconds / 10 second cool down
2 through 5 / 60 seconds / 5min cool dn

53
Q

Starter cranking limits
Motoring (ground)

A

1 / 90 seconds / 5 min cool down
2-5 / 30 seconds / 5 min cool down

54
Q

Starter must not be used if N2 rpm exceeds ____

A

45%

55
Q

The use of Reduced/FLEX 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 **

56
Q

Windmilling Relight

A

Altitude from 25,000’ to sea level:

Speed 250 KIAS to VMO and 7.2% N2 minimum

57
Q

Starter Assisted relight

A

Altitude from 21,000’ to sea level:
Speed from VREF up to VMO and from 0 to 45% N2.

58
Q

All engine out rapid relight

A

Altitude from 10,000’ to sea level:

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

59
Q

Max fuel imbalances between L&R wing tanks

A

• ground operations 2500 lbs
• during takeoff: 300 lbs
• all other phases of flight: 800 lbs

60
Q

Min fuel qty for a go around

A

600 lbs per wing tank (with the airplane level) and assuming a maximum airplane climb altitude of 10° nose up.

61
Q

Takeoff with engine fuel temperature indications below _____ is prohibited.

A

5°C (41°F)

62
Q

Bulk Fuel Takeoff Limit – Minimum Temperature

A

-30°C

63
Q

Bulk Fuel Freezing Point

A

-40°C

64
Q

Max oil consumption

A

.05 Gallons per hour

65
Q

APU Type

A

Allied Signal RE 220 (RJ)

66
Q

Maximum APU EGT (dependant upon altitude and temperature)

A

1038°C

67
Q

The APU starter motor duty cycle is limited to not more than

A

3 starts/start attempts in one hour with a 2 min delay between cranking attempts

68
Q

APU MAX RPM

A

106%

69
Q

APU MAX EGT

A

1038°C

70
Q

APU bleed air extraction is not permitted above

A

25,000ft

71
Q

The maximum permissible load on the APU generator is

A

40 kVA

72
Q

APU EICAS indications

A

APU EGT °C - green=0-806°C/red=807°C

APU RPM% - green=0-106%/red=107°C

73
Q

APU GENERATOR LOADING LIMIT
(ALTITUDE)

A

41,000ft

74
Q

APU altitude starting limit

A

37,000ft

75
Q

Ground starting altitude limit (APU)

A

15,000ft

76
Q

The CRJ Maximum cruise Mach number during flight in RVSM airspace is

A

Mach .83

77
Q

The maximum speeds at which the flaps may be extended are:

A

Flaps 1 = 230
Flaps 8 = 230
Flaps 20 = 230
Flaps 30 = 185
Flaps 45 = 170

78
Q

Max landing gear operating speeds

A

Extension = 220
Down & Locked = 220
Retraction = 200

79
Q

Tire limit speed

A

CRJ maximum tire limit speed is 182 knots ground speed.

80
Q

MMO

A

.85

81
Q

Max & Min speeds for ADG operation

A

The maximum speed for ADG operation is VMO/MMO.

The min speed is 135kias

82
Q

Turbulence penetration speed

A

The airspeed limitation for severe turbulence penetration is 280 KIAS or 0.75 Mach, whichever is lower.

83
Q

Windshield wiper operating limits

A

The windshield wiper must not be operated above 250 KIAS.

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

84
Q

Maneuvering limit load factors

A

Flaps retracted = -1 to 2.5g
Flaps extended = 0 to 2g

85
Q

Differential pressure limits

A

•The maximum relief differential pressure is 8.7psi

•The maximum negative differential pressure is -0.5 psi.

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

86
Q

The CRJ maximum altitude for single pack operation is

A

31,000ft

87
Q

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

A

5 minutes

88
Q

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

A

AIRPLANE FLIGHT MANUAL

89
Q

Slats/Flaps Limits
(Alt & enroute)

A

•Enroute use of Slats/Flaps is prohibited.

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

90
Q

Flight spoiler limits

A

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

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

91
Q

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

A

10 minutes

CRJ 550 Mem items/Limitations (4 decks)

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