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CL-65 Study Guide > Limitations > Flashcards

Limitations Flashcards

0
Q

Nose wheel steering

A

Rudder pedals - 8 degrees

Tiller - 80 degrees

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1
Q

Turning Radius

A

80’ 1”

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2
Q

Max ramp weight

A

82,750 lbs

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3
Q

Max T/O weight

A

82,500 lbs

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4
Q

Max Landing weight

A

73,500 lbs

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5
Q

Max Zero Fuel Weight

A

70,000 lbs

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6
Q

Min flight weight

A

45,000 lbs

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7
Q

Cargo weight limits

A

FWD - 850 lbs
CTR - 850 lbs
AFT - 4375

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8
Q

Headset must be worn

A

Below FL180

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9
Q

Max airport pressure altitude

A

10,000 feet

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10
Q

Takeoff, landing, and operating limits (for pressure altitude above 8,000 feet and CABIN ALT WARN HI displayed.

A

One pilot must use oxygen from TO until message goes out, and landing until the airplane has vacated the runway after landing. The regulator should be set to the normal (N) position

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11
Q

Max operating altitude

A

41,000 feet

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12
Q

Max temp for T/O and landing

A

ISA + 35 C

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13
Q

Min temp for takeoff

A

ISA - 40 C

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14
Q

Engine type

A

GE CF34-8C5

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15
Q

APR arms when thrust is within _____ of scheduled thrust setting

A

8%

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16
Q

APR Activates on takeoff if:

A

Thrust levers are in TOGA detent
Either normal, flex or GA power is programmed
Engine fail (N1 rpm differ by 15%

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17
Q

APR Activates on GA if:

A 
OEO operations, or
Engine failure (N1 RPM differ by 15%)
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18
Q

Set OEO fuel scheduling for MCT by:

A

Placing thrust levers in the Max Power detent

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19
Q

Engine thrust

A

APR - 14,750

Non-APR - 13,560

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20
Q

Cold soaked definition:

A
  • 30 degrees C (22 F) or below for more than 8 hours
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21
Q

Cold soaked engine prep

A

Motored 60 seconds
Fan rotation observed
Thrust reversers cycles - 2 seconds or less

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22
Q

Engine warm-up

A

IDLE - Normal operating range

Do not exceed 75% N1 for 2 minutes or until in normal operating range whichever is longer

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23
Q

Engine ground start

A

ITT below 120 degrees C

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24
Q

Engine air start

A

ITT below 90 degree C

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25
Q

Do not accelerate engine until oil pressure has stabilized ???

A

Below 116 psi

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26
Q

Engine to engine N2 split?

A

Not be greater than 2% N2

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27
Q

If N2 is ______ or less with an OAT of _______ do not accelerate above idle

A

57%, - 20 degrees C

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28
Q

Min N2 for start

A

20%

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29
Q

Min N1 for start

A

Rotation

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30
Q

Min oil temp for start

A
  • 40 degrees C
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31
Q

Min oil pressure min steady state

A

25 psi

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32
Q

When the engines are operating and oil quantity is below ______ or engines not operating and oil quantity is below ____ the L(R) OIL LEVEL LO status message is displayed

A

57%, 80%

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33
Q

Oil level is checked?

A

3 minutes - 2 hours after every engine shutdown

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34
Q

EICAS limit display status message colors

A

Green - Normal operating range
Amber - Caution range
Red - Max and min limitations

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35
Q

Continuos Ignition Must be used when:

A

T/O & LDG on contaminated runways
MDT or HVY rain
MDT or HVY turbulence
Vicinity of TS

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36
Q

Engine starter cracking limits:

A

1st & 2nd attempts - 90 seconds on, 10 seconds off

3rd - 5th attempts- 90 seconds on, 5 minutes off

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37
Q

Engine starter cracking limits (flight)

A

1st attempt - 120 seconds on, 10 seconds off

2 - 5 attempts - 60 seconds on, 5 minutes off

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38
Q

Engine dry motor cycle (ground)

A

1st attempt: 90 seconds on, 5 minutes off

2 - 5 attempts: 30 seconds on, 5 minutes off

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39
Q

Air start limits:

A

Windmill and starter assist 21,000 feet and below

Rapid Relight: 10,000 feet and below

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40
Q

Max fuel imbalance between main tanks:

A

Takeoff - 300 lbs

Flight - 800 lbs

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41
Q

Gravity fuel total:

A

14,810 lbs

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42
Q

Pressure refueling:

A

Total: 19,595 lbs
Mains: 7,492 lbs
Center: 4,610 lbs

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43
Q

Max fuel in center tank with less than ________ lbs in each main tank is _______ :

A

4,400 lbs, 500 lbs

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44
Q

Min fuel in each main tank for GA:

A

600 lbs

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45
Q

Min engine fuel temp limit for takeoff:

A

5 degrees C at engine inlet

46
Q

Min temp for bulk fuel takeoff limit:

A

Jet A - 30 degrees C

47
Q

Mixing of certain fuel types is permitted per CFM: T or F

A

True

48
Q

APU Min temp cold soaked start:

A
  • 40 degrees C
49
Q

APU min battery voltage for start:

A

22 volts

50
Q

APU max number of start attempts:

A

3 per hour

51
Q

APU Min time between start attempts:

A

2 minutes

52
Q

APU min time before pneumatic load:

A

2 minutes

53
Q

APU max ops altitude

A

FL410

54
Q

APU max starting altitude:

A

FL370

55
Q

APU max altitude for bleed air:

A

FL250

56
Q

APU ALT to use bleed air for engine starts:

A

FL250

57
Q

APU max gen loading _____ KVA to _____:

A

40, FL410

58
Q

APU max airspeed with door open & APU not running:

A

220 KTS

59
Q

Ground icing requirements:

A

Cowl Anti-ice on in icing conditions or when OAT 10 degrees C or less and operating on RWY and/or TWY with snow, ice, slush, or standing water. Wing Anti-ice must be on when: OAT is 5 degrees C or below and visible moisture in any form is present (1sm vis) and/or OAT IS 5 degrees C or below and RWY is comtaimented with slush, snow, or standing water

60
Q

In-flight icing:

A

Cowl Anti-ice on in icing conditions or ICE is annunciated by the ice detector system. Wing Anti-ice must be on when annunicated by the ice detection system or in icing conditions and IAS is less then 230 KTS

61
Q

Holding in Super-cooled Large Droplet Icing conditions or operating in severe conditions is:

A

Prohibited

62
Q

Continued operations in areas of super-cooled large droplet is:

A

Prohibited

63
Q

Max RWY slope is:

A

+/- 2 degrees

64
Q

Max tailwind component:

A

10 KTS

65
Q

If cargo is in the cargo compartment the flight must be within ______ minutes of a suitable airport

A

60

66
Q

Flap speeds:

A

1 & 8 degrees - 230 KTS
20 degrees- 220 KTS
30 degrees - 185 KTS
45 degrees - 170 KTS

67
Q

Can flaps be used enroute?

A

No

68
Q

Max altitude for flap extension?

A

15,000 feet

69
Q

When holding in icing conditions, flaps must be _______ ?

A

Retracted

70
Q

Max speed for turbulence?

A

280 KTS, 0.75 MACH

71
Q

Max gear extension?

A

220 KTS

72
Q

Max gear operational speed?

A

220 KTS

73
Q

Max gear retract speed?

A

200 KTS

74
Q

Max tire speed on ground?

A

195 KTS

75
Q

Max crosswind component?

A

700 - 27 KTS dry, 15 KTS slippery

900 - 22 KTS dry, 15 KTS slippery

76
Q

ADG supplies power to:

A

ADG bus to AC Ess bus to ESS TRU to ESS BUSS and DC BATT bus ( thru ESS TIE), ACMP 3B, Flaps/slats, pitch trim are available, Stab ch 2

77
Q

ADG deploy speed with no time limit:

A

Vmo/Mmo

78
Q

Max speed for windshield wiper operations or parked in non-parked position?

A

250 KTS

79
Q

Maneuvering Limit Load Factors?

A

Flaps up: -1.0 to 2.5 G

Flaps down: 0.0 to 2.0 G

80
Q

Max differential pressure is:

A

8.7 psi

81
Q

Maximum negative differential pressure is:

A
  • 0.5 psi
82
Q

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

A

0.1 psi

83
Q

The cabin must be completely depressurized prior to -____________ ?

A

Opening any doors

84
Q

Max single pack operation altitude?

A

FL250

85
Q

Autopilot use below 600 AGL is PROHIBITED, except?

A

Precision - 80 feet AGL
Single-engine precision - 110 feet AGL
Non-precision/Visual - 400 feet AGL

86
Q

During RNAV departures and arrivals the autopilot must be -_______ ?

A

On

87
Q

Using _______ sub mode during appr is not permitted?

A

DES

88
Q

_________ mode use during VOR approaches is not permitted:

A

APPR

89
Q

General load altitude limit (feet):

A

0-41,000 feet

90
Q

Generator Load limitation each main:

A

40 KVA

91
Q

General APU limitation:

A

40 KVA

92
Q

TRU LOAD LIMIT:

A

120 amps

93
Q

CRT display max time (ground) DC power only:

A

5 minutes

94
Q

Wing and/or cowl anti-ice selection is _________ with the APU as a bleed source in manual mode:

A

Prohibited

95
Q

Multi-function flight spoilers use Min altitude _______, Min Speed ________?

A

300 AGL, Vapp + 10 KTS

96
Q

Min Multi-function flight spoilers altitude for stabilized approach:

A

1000 feet

97
Q

Are thrust reversers approved to be used in flight?

A

No

98
Q

By _______ KIAS reverse thrust must be reduced to idle?

A

60

99
Q

Both stall protection systems switches must be _______ for all phases of flight:

A

ON

100
Q

When on the ground and stationary, the taxi lights must be turned off after ________?

A

10 minutes

101
Q

FMS is approved for use only during _______ and _____________ phases of flight:

A

Enroute, terminal, non-precision approach

102
Q

Approaches prohibited using the FMS:

A 
ILS
LOC/ LOC BC
VOR
LDA
SDF
MLS
103
Q

What does the FMS message “NO APPR” mean when it is displayed on the PDF?

A

FMS must not be used past the FAF

104
Q

Takeoff is prohibited with _________________ adhering to any critical surface:

A

Ice, snow, frost, and slush

105
Q

Takeoff is permitted with a maximum of 1/8 inch of frost adhering to ____________ caused by ___________ in the wing:

A

The underside of the wing, cold-soaked fuel

106
Q

RVSM required equipment?

A

1 operational autopilot
1 operational Altitude Alerting System
2 Altitude Reporting Transponders, 1 must be operational
2 operational ADC’s

107
Q

OAT above ________, delay WSHLD to LOW until after ________?

A

30 degrees C, takeoff

108
Q

Max cruise MACH number during flight in RSVM airspace is ______?

A

0.82 MACH

109
Q

Cross bleed start:
BLEED VALVES
Thrust lever Min ______ psi
Min _______ N2

A

Switch to AUTO
42 psi
80% N2

110
Q

Engine start sequence: too many steps!!!!

A

Fuel pumps ON, Check boost pump INOP light out
Boost pump light ON, FUEL PUMP ON advisory message comes on
FUEL LO PRESS caution messages out, XFLOW INHIBIT not on
Engine - START, applicable START light on
Engine status - isolation valve opens, both pack valves close
Associated start valve opens, ATS engages,
50% - ATS Disengages, start valve closes, PAC/ISO valves previous
Settings

111
Q

FUEL FEED CHECK VALVE TEST

A

Fuel pumps (both) OFF, observe FUEL LO PRESS caution on for. On-operating engine
FUEL LO PRESS caution (2 min max) displayed on the non-op engine
Dry motor non-operating engine max 30 seconds
Applicable FUEL LO PRESS caution should be displayed, if not-check valve failed
Fuel pumps (both) ON, L and R BOOST PUMP ON - lights come on
L and R BOOST PUMP INOP lights go out
L and R FUEL PUMP advisory message comes on
Applicable FUEL LO PRESS caution message goes out

112
Q

SE taxi engine bleed

A

Only associated PACK

113
Q

Bleeds may be transfer to APU when:

A

BLEED SOURCE - APU
ISOL - OPEN
BLEED VALVES - MANUAL

Automatic bleed operation restored by:
BLEED VALVE - AUTO
ISOL - CLOSED
BLEED SOURCE - BOTH ENG

CL-65 Study Guide (25 decks)

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