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Cj3 > Limitaitions > Flashcards

Limitaitions Flashcards

1
Q

Maximum design ramp weight

A

14,070 pounds

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2
Q

Maximum design, takeoff weight

A

13,870 pounds

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3
Q

Maximum design landing weight

A

12,750 pounds

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4
Q

Maximum design, zero fuel weight

A

10,510 pounds

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5
Q

Maximum takeoff thrust time limit one engine

A

10 minutes

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6
Q

Maximum takeoff thrust time limit two engines

A

Five minutes

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7
Q

The engine should not be operated above 80% N2 until oil temperature is above ___________

A

10° C 50° F

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8
Q

Engine start limitations ground aircraft configuration AH
•ENG CTRL SYS L/R annunciators
•max tail wind
•max Xwind
•max time to light out
•min oil temp(EIS)

A

Extinguish
10kts(12kts)
10kts(16kts)
10 seconds
-40° C

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9
Q

Engine start limitations ground

• maximum Airport elevation for ground battery_______
External power start______
• Minimum battery voltage for battery start_____
• Minimum\maximum external power current capacity for start
_________/_______

A

14,000ft
14,000ft
24v
800/1100amps

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10
Q

At what temperature must the airplane battery be preheated to prior to engine start if it has been cold, soaked for more than two hours at what temperature?

A

Temps below -18° C(0° F)
Must be preheated above those temperatures for Engine start

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11
Q

The engine indicating system EIS may take _______minutes to become usable after power is applied when cold soak below _________temperatures

A

• 1 to 6 minutes
•-10° C (+14° F )

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12
Q

At what oil temperature must the engine be preheated before conducting a start?

A

-40° C (-40° F)

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13
Q

How many engine starts can you do and how many minutes and what are the rest periods between them

A

• three engine starts in 30 minutes
• 60 second resting. Between the engine starts.

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14
Q

The battery temperature warning system must be operational for all _____and ________operations

A

Ground and flight

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15
Q

How many battery cycle, limitations, _______engine starts per ______

A

Three engine starts per hour 

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16
Q

How many generator assist cross starts are equal to how many battery starts?

A

Three generator assisted cross starts is equal to one battery start.

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17
Q

How many battery cycles are counted if you use an external power unit?

A

No battery cycle is counted

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18
Q

Maximum current per generator

A

200amps

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19
Q

Maximum time on the ground for the pitot/static heat?

A

Two minutes

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20
Q

What is the maximum time on the ground for engine wing and or windshield anti-ice?

A

2 minutes @ 75% N2
And no more than one minute after the wing anti-ice L/R, annunciators have extinguished 

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21
Q

Ambient service temperature must be obtained from the ____ display at the bottom of each ______ with either or both engines operating or from an appropriate ground station. The SAT display is unreliable on the ground.

A

RAT/PFD

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22
Q

When will the fuel low level L and/ or R caution lights illuminate

A

210 pounds

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23
Q

Max fuel imbalance

A

200lbs

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24
Q

What is the maximum emergency demonstrated fuel in balance?

A

 600 pounds

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25
Q

EGME/DIEGME additive is________ but not required and not to exceed_____ percent by volume

A

Approved
.15%

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26
Q

MMO(above _________ is?

A

29,300ft
.737 Mach

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27
Q

VMO(between________and_______ ft is?

A

8000ft and 29300ft is 278 kts

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28
Q

Vmo below________ ft is?

A

8,000ft is 260kts

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29
Q

Max flap extended speed-vfe
Takeoff and approach (15°)_____
Land position (35°)______
Max speed failed to grnd (55°)____

A

200kts
161kts
140kts

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30
Q

Max landing gear
Extend speed VLE_____
Operating speed VLO extending_____
VLO retracting______

A

(200KTS)

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31
Q

Max speed Brakes VSB-

A

No Limit

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32
Q

Max autopilot speed

A

278kts/.737mach

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33
Q

Min speed in icing conditions
(Except during tkoff app and landing)

A

180kts

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34
Q

Maximum altitude for takeoff and landing

A

14,000 feet 

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35
Q

Maximum tail wind component for takeoff and landing

A

10kts

36
Q

Minimum ambient temperature for takeoff and landing

A

-54°C (-65°F)

37
Q

In prolonged ground cold soaked of two hours or more in temperatures of______ the cabin temps must be held above temps of_______ for ____ minutes

A

-10° C or colder
0° centigrade, 32°F
20 minutes

38
Q

The auto pilot, yaw damper, and engine sync must be ______for takeoff and landing

A

Off

39
Q

Take off is prohibited if the ______system is inoperative

A

Antiskid

40
Q

Cabin must be _________ for takeoff and landing

A

Depressurized 

41
Q

Takeoffs and landings are limited to_______ runway surfaces

A

Paved

42
Q

Speed brakes must be retracted prior to ______ feet AGL before landing

A

50 feet 

43
Q

Extending ground flaps during touch and go landings is ______

A

Prohibited

44
Q

The ground idle switch must be in the _______ position when conducting touching go landings 

A

High

45
Q

For normal takeoff operations, the ground idle switch must be in the _______ position

A

Normal

46
Q

Max tire groundspeed

A

165Kts

47
Q

When using type two three or four anti-ice fluid, what settings are the flaps limited to?

A

Flaps up

48
Q

Can you take off with a warning annunciator displayed?

A

No

49
Q

When can you take off with a caution annunciator displayed?

A

Only when it has been deferred per and approved minimum equipment list (MEL)

50
Q

Takeoff is prohibited with the following forms of contamination with frost adhering to the following critical areas
a.
b.
c.

A

a. Wing leading edge
b. Upper wing surface.
c. Windshield.

51
Q

Takeoff and landing operation limits with ice snow or/adhering to the following critical areas
A.
B.
C.
D.
E.
F.
G.
H.
I.
J.
K.

A

A. Wing leading edge and upper wing surface
B. Flight control services, including all hinge gaps.
C. Horizontal stabilizer.
D. Vertical stabilizer.
E. Engine and inlets.
F. Top of Engine pylons.
G. Top of fuselage.
H. Windshield.
I. All pitot probes and static ports.
J. Angle of attack veins.
K. Upper surface of nose forward of the windshield. 

52
Q

A visual and ________check of the wing leading edge and wing upper surface must be performed to ensure the wing is free from frost ice, snow or slush when the outside air temperature is less than _______, or if it cannot be determined that the wing fuel temperature is above _______in any of the following conditions exist

A

Tactile(hand on surface)
10°C, (50°F)
0°C, (32°F)

53
Q

Max operating altitude

A

45,000 feet 

54
Q

Maximum generator current per generator in flight

A

300 Amperes up to 41,000 feet
250 Amperes above for 41,000 feet

55
Q

Maximum altitude for extension of flaps and or landing gear

A

18,000 feet

56
Q

Maximum operating altitude with inoperative yaw damper 

A

30,000 feet

57
Q

Normal cabin, pressurization limitations 

A

0.0 to 8.9psi +/-0.1 psi differential

58
Q

Icing conditions may exist when the indicated RAT is ______ or below, and there is visible moisture invisibility, less than ______

A

10°C, (50°F)
1 mile

59
Q

Minimum airspeed and flap setting for sustained flight and ice and conditions except Approach Landing is _______

A

Flaps zero
180 kts

60
Q

Minimum engine N2 speed for effective wing anti-icing 

A

75% N2

61
Q

Minimum temperature for operation of tail deicing boots indicated RAT 

A

-35°C (-31°F)

62
Q

The wing engine anti-ice switches must be on ______or ______ for operations with indicated RAT of 10°C, 50°F or below when the flight is in visible moisture cannot be assured failure to observe this limitation may result in ENGCTRLSYSFAULTL\R annunciations due to accumulation on the engine _____ probe

A

ENG ON
WING\ENG
PT2\TT2.

63
Q

If engine anti-ice was inadvertently, turned on prior to one minute of engine operation, the anti-ice must be turned off for a ______minutes before turning it back on if minor engine vibrations are felt or heard during ground operations, the crew must momentarily increase the engine, speed, typically ________ N1 to assist with shedding the accumulation of ice from the spinner fan and stators

A

Two minutes
20 to 30%

64
Q

Severe icing conditions that exceed those for which the airplane was certificated, shall be determined by the following visual cues

A
  1. unusual, extensive ice accumulation on the air frame and windshield in areas not normally observed to collect ice 2. accumulation of ice on the upper surface of the wing that extends more than 12 to 18 inches after the heated leading edge
65
Q

Can you use the auto pilot in severe icing conditions?

A

No it’s prohibited

66
Q

Use of auto pilot is prohibited in severe icing and conditions when 1.
2.

A
  1. Unusual lateral trim is required.
  2. auto pilot trim warnings are encountered. 
67
Q

Auto pilot limitations-
1. One pilot must remain seated with a seatbelt fastened during all ______operations.
2. Operating in the _____mode is limited to training and display failure conditions
3. The pilots PFD CO pilots, PFD and MFD must be installed and operational in the normal mode for _____

A
  1. auto pilot.
  2. composite
  3. take off
68
Q

The auto pilot minimum engage height during climb, following takeoff or go around is _____AGL

A

350 feet

69
Q

Auto pilot minimum use height is a.ILS CAT 1____
b. non-precision approaches_____
c.Cruise _____
CAT2 approaches are________

A

a.180ft
b.350ft
c.1000ft
Not approved

70
Q

VOR approaches must use the _____ mode

A

APPR mode

71
Q

What is the maximum distance you can be from a vor while doing a VOR approach or you must use the heading mode to track that approach.

A

15 miles

72
Q

It is ______to display the non-coupled side flight Director unless a couple side Flight, Director is being displayed failure to adhere to this limitation will result in incorrect Flight Director guidance use the couple side Flight Director by itself will operate correctly

A

Prohibited

73
Q

How long does the standby flight display attitude indicator run on its battery? 

A

88 minutes

74
Q

What are the power settings on the EPU

A

28 V 800 and1100 AMps

75
Q

 Types of batteries, amps and volts 

A

Nicad 25v 44 amp hours
Lead acid 24v 42 amp hours

76
Q

Baggage nose

A

400 pounds32 pounds per square foot 

77
Q

Engine Type 
And thrust

A

Fj44-3a turbofan
2780 lbs of thrust

78
Q

Wingspan

A

 53 feet 

79
Q

Horizontal, stabilizer length

A

20.8 feet.

80
Q

Tail height

A

15.3 feet.

81
Q

Turning radius

A

70 feet 

82
Q

How many locking pins in the main cabin door? 

A

12

83
Q

Aft baggage compartment

A

600 pounds 50 ft.³ space 

84
Q

How many electrical buses are there? 

A

10 buses

Crossfeed bus
Hot battery bus
2 feed busses
2 feed extension buses
2 cross over buses
2 emergency buses

85
Q

How many static wicks are there?and how many can be missing

A

15 total and 1 can be missing from any control surface no more than 2 total

Cj3 (7 decks)

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