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CJ3+ > Limitations > Flashcards

Limitations Flashcards

1
Q

MAX RAMP WEIGHT

A

14,070 lbs

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2
Q

MAX TAKEOFF WEIGHT

A

13,870 lbs

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3
Q

MAX LANDING WEIGHT

A

12,750 lbs

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4
Q

MAX ZERO FUEL WEIGHT

A

10,510 lbs

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5
Q

NOSE BAGGAGE WEIGHT LIMIT

A

400 lbs

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6
Q

TAIL BAGGAGE WEIGHT LIMIT

A

600 lbs

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7
Q

MMO (>29,300 ft)

A

Mach .737

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8
Q

VMO (8,000’ – 29,300’)

A

278 KIAS

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9
Q

VMO (< 8,000’)

A

260 KIAS

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10
Q

VFE (15° / 35°/ Failed at 55°)

A

200 / 161 / 140 KIAS

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11
Q

VLE/VLO

A

200 KIAS

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12
Q

VSB

A

No Limit

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13
Q

Max speed for Autopilot Operation

A

278 KIAS / Mach .737

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14
Q

Tire Limit Speed

A

165 Knots

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15
Q

Minimum Speed in Icing Conditions

Flaps 0°

A

180 KIAS

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16
Q

Is engine start with an ENG CNTRL FAULT L and/or R message displayed permitted?

A

Not Permitted

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17
Q

Battery start limit

A

3 per hour

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18
Q

One battery start = __ generator starts

A

3 generator starts

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19
Q

External power start = __ battery starts

A

Zero battery starts

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20
Q

What power source is used in an Air Start?

A

Battery

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21
Q

Engine start duty cycles

A

3 starts per 30 minutes with 60 seconds rest between cycles.

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22
Q

Abort if N1 does not indicate before __

A

25% N2

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23
Q

Abort start if engine stops accelerating for

A

30 seconds

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24
Q

Max time to light-off

A

10 seconds (first indication of fuel flow to increase in ITT)

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25
Q

Minimum oil temperature prior to power increase above 80% N2

A

10°C

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26
Q

Max elevation for battery or cross generator starts

A

14,000 ft

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27
Q

Max tailwind/crosswind component for engine start

A

10 kts

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28
Q

Minimum battery voltage for engine start

A

24 VDC

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29
Q

Max external power voltage for start

A

29 VDC

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30
Q

Min/Max external power current for start

A

800/1100 AMPS

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31
Q

Minimum oil temperature

A

-40°C

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32
Q

Minimum battery temperature

A

-18°C

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33
Q

If aircraft has been cold soaked below ____, the FADEC must be warmed with electrical
power for at least _ minutes followed by a power cycle with the battery switch.

A

-40°C; 3 minutes

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34
Q

Pitot/static heat ground time limit.

A

2 minutes

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35
Q

Engines above 75% N2 with wing, engine, and/or windshield anti-ice on is limited to ______ on the ground.

A

2 minutes

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36
Q

Wing anti-ice limited to ______ after WING ANTI-ICE COLD message has extinguished
during preflight checks.

A

1 minute

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37
Q

Temperature must be obtained by _______ with either/both engines running or from an
___________ when the engines are not running.

A

RAT on MFD; appropriate ground station

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38
Q

N1 is limited to ___ with a tailwind component greater than _____.

A

60%; 10 knots

39
Q

Max takeoff/landing altitude.

A

14,000 ft

40
Q

Max Tailwind Component

A

10 kts

41
Q

Takeoff prohibited if:

A

-Any red message is displayed
-Any amber message is displayed unless the MEL is complied with
-ENG CNTRL FAULT L and/or R message is displayed
-Antiskid system is inoperative
-Battery charging amps is more than 20 amps
-Frost, ice, snow, or slush is adhering to critical areas (refer to AFM for
specifics)

42
Q

__________ must be disengaged for takeoff/landing.

A

Autopilot and yaw damper

43
Q

Cabin must be ________ prior to landing.

A

depressurized

44
Q

Takeoffs/landings limited to _____ runway surfaces.

A

paved

45
Q

Speed brakes must be retracted prior to ____ for landing (except where required by AFM
procedures).

A

50’ AGL

46
Q

Extending ground flaps during touch-and-go landings is ________.

A

prohibited

47
Q

Takeoff limited to flaps __° when Type II, III or IV anti-ice has been applied.

A

0

48
Q

A visual and tactile check of the wing leading edge and upper surface when the OAT is __°C or if it cannot be determined the wing fuel temp is __°C and there is visible moisture present, or water is present on the upper wing surface, or the difference between the dew point and OAT is __°C, or the atmospheric conditions have been conductive to frost formation.

A

< 6; > 0; ≤ 3

49
Q

The tactile check must be accomplished within _ minutes of takeoff.

A

5

50
Q

If the aircraft is treated with deice/anti-ice fluid, the tactile check may be done anytime between _______and_____, provided the time is within the max holdover time.

A

the final application and takeoff

51
Q

Max Operating Altitude

A

FL450

52
Q

Max Operation Altitude with autopilot and yaw damper inop.

A

FL300

53
Q

Max Altitude for flaps/landing gear extension.

A

FL180

54
Q

Minimum speed in RVSM airspace.

A

150 KIAS

55
Q

Minimum weight in RVSM airspace.

A

8,750 lbs

56
Q

Prohibited maneuvers.

A

Acrobatic maneuvers including spins.

57
Q

Intentional stalls above ______ are prohibited.

A

18,000 ft

58
Q

Load factor limits @ 13,870 lbs.

A

Flaps 0° – -1.44 to 3.6G

Flaps 15° or 35° – 0.0 to +2.0G

59
Q

Takeoff with a display in _______ mode is prohibited.

A

reversion

60
Q

Are CAT II approaches approved?

A

NO

61
Q

Minimum autopilot use heights:
Takeoff and Climb?
Enroute and Descent?
Approaches?

A

350 ft AGL
1000 ft AGL
160 ft above runway

62
Q

The V-speeds, required field length and other performance information for a specific
operation must be obtained from ________.

A

a single source; i.e., either the AFM, CPCalc, or FMS

Takeoff and Landing Performance Data.

63
Q

If the BATTERY OVERTEMP message appears on the ground, __________.

A

maintenance must be performed before takeoff, even if the message clears.

64
Q

Generator Loads (max):
Ground
Air ≤ FL410
Air > FL410

A

200 Amps
300 Amps
250 Amps

65
Q

Max fuel imbalance for normal ops.

A

200 lbs

66
Q

Max demonstrated fuel imbalance for emergency return.

A

600 lbs

67
Q

T/F, Unusable fuel (fuel remaining when fuel quantity reads 0) is not usable in flight.

A

True

68
Q

Engine type

A

Williams International FJ44-3A turbofan

69
Q

Engine thrust

A

2820 lbs. @ sea level up to 22°C

70
Q

Approved Oils

A

Mobil Jet II & Mobil 254

71
Q

Mixing of approved oils (IS / IS NOT) permissible.

A

Is permissible.

72
Q

Max oil consumption

A

0.023 gallons / 1 hr (1 qt or L / 11 hrs)

73
Q

Engine limited to __ seconds of continuous flight at 0 or negative Gs.

A

10

74
Q

Structural cabin pressure

A

-0.5 to 9.0 PSI

75
Q

What is the approved type of oxygen?

A

Aviator’s breathing oxygen (MIL-O-27210)

Medical oxygen is prohibited.

76
Q

Crew and passenger masks are not approved for use above ____ft cabin altitude.

A

40,000

77
Q

Prolonged use of passenger masks above ____ft cabin altitude is not recommended.

A

25,000

78
Q

Crew masks must be _______________ to qualify as quick donning.

A

checked and stowed properly

79
Q

For single-pilot ops, a _________ must be available for a passenger occupying the right crew seat.

A

crew mask

80
Q

If a prolonged ground cold soak (≥2 hours) at ambient temperatures of __°C or colder has
occurred, cabin temperature must be __°C for a minimum of __ minutes prior to operations
above ____ to ensure proper deployment and operation of the passenger masks.

A

-10; ≥ 0; 20 minutes; FL240

81
Q

Which light must be operable for flight into know or forecast icing at night?

A

Wing inspection light.

82
Q

Tail De-ice must be off when SAT is below ____.

A

-35°C

83
Q

Wing and engine anti-ice may be operated in the ENG ONLY position when _______________________.

A

SAT is

84
Q

Engine anti-ice must be __ during ground ops in icing conditions.

A

on

85
Q

Engine anti-ice is prohibited for _____ after ground engine start.

A

1 minute

86
Q

If engine anti-ice is selected before 1 minute, must be turned off for _______.

A

2 minutes

87
Q

Required aircraft configuration in icing conditions.

A

Clean (except for approach and landing)

88
Q

Minimum N2 for effective wing anti-ice

A

75% N2

89
Q

Can the CJ3+ operate in severe icing?

A

No, it is prohibited.

90
Q

Intentional selection of GROUND FLAPS (55°) in flight?

A

Prohibited

91
Q

Maximum occupants

A

10 (including crew seats)

92
Q

Lavatory door must be latched open for…

A

taxi, takeoff, and landing.

93
Q

Lavatory max occupancy?

A

One

CJ3+ (2 decks)

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