Limitaitions

Question 1

Maximum design ramp weight

Answer 1

14,070 pounds

Question 2

Maximum design, takeoff weight

Answer 2

13,870 pounds

Question 3

Maximum design landing weight

Answer 3

12,750 pounds

Question 4

Maximum design, zero fuel weight

Answer 4

10,510 pounds

Question 5

Maximum takeoff thrust time limit one engine

Answer 5

10 minutes

Question 6

Maximum takeoff thrust time limit two engines

Answer 6

Five minutes

Question 7

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

Answer 7

10° C 50° F

Question 8

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)

Answer 8

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

Question 9

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
_________/_______

Answer 9

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

Question 10

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?

Answer 10

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

Question 11

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

Answer 11

• 1 to 6 minutes
•-10° C (+14° F )

Question 12

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

Answer 12

-40° C (-40° F)

Question 13

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

Answer 13

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

Question 14

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

Answer 14

Ground and flight

Question 15

How many battery cycle, limitations, _______engine starts per ______

Answer 15

Three engine starts per hour 

Question 16

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

Answer 16

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

Question 17

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

Answer 17

No battery cycle is counted

Question 18

Maximum current per generator

Answer 18

200amps

Question 19

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

Answer 19

Two minutes

Question 20

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

Answer 20

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

Question 21

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.

Answer 21

RAT/PFD

Question 22

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

Answer 22

210 pounds

Question 23

Max fuel imbalance

Answer 23

200lbs

Question 24

What is the maximum emergency demonstrated fuel in balance?

Answer 24

 600 pounds

Question 25

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

Answer 25

Approved .15%

Question 26

MMO(above _________ is?

Answer 26

29,300ft .737 Mach

Question 27

VMO(between________and_______ ft is?

Answer 27

8000ft and 29300ft is 278 kts

Question 28

Vmo below________ ft is?

Answer 28

8,000ft is 260kts

Question 29

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

Answer 29

200kts 161kts 140kts

Question 30

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

Answer 30

(200KTS)

Question 31

Max speed Brakes VSB-

Answer 31

No Limit

Question 32

Max autopilot speed

Answer 32

278kts/.737mach

Question 33

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

Answer 33

180kts

Question 34

Maximum altitude for takeoff and landing

Answer 34

14,000 feet 

Question 35

Maximum tail wind component for takeoff and landing

Answer 35

10kts

Question 36

Minimum ambient temperature for takeoff and landing

Answer 36

-54°C (-65°F)

Question 37

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

Answer 37

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

Question 38

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

Answer 38

Off

Question 39

Take off is prohibited if the ______system is inoperative

Answer 39

Antiskid

Question 40

Cabin must be _________ for takeoff and landing

Answer 40

Depressurized 

Question 41

Takeoffs and landings are limited to_______ runway surfaces

Answer 41

Paved

Question 42

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

Answer 42

50 feet 

Question 43

Extending ground flaps during touch and go landings is ______

Answer 43

Prohibited

Question 44

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

Answer 44

High

Question 45

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

Answer 45

Normal

Question 46

Max tire groundspeed

Answer 46

165Kts

Question 47

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

Answer 47

Flaps up

Question 48

Can you take off with a warning annunciator displayed?

Answer 48

No

Question 49

When can you take off with a caution annunciator displayed?

Answer 49

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

Question 50

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

Answer 50

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

Question 51

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.

Answer 51

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. 

Question 52

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

Answer 52

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

Question 53

Max operating altitude

Answer 53

45,000 feet 

Question 54

Maximum generator current per generator in flight

Answer 54

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

Question 55

Maximum altitude for extension of flaps and or landing gear

Answer 55

18,000 feet

Question 56

Maximum operating altitude with inoperative yaw damper 

Answer 56

30,000 feet

Question 57

Normal cabin, pressurization limitations 

Answer 57

0.0 to 8.9psi +/-0.1 psi differential

Question 58

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

Answer 58

10°C, (50°F) 1 mile

Question 59

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

Answer 59

Flaps zero 180 kts

Question 60

Minimum engine N2 speed for effective wing anti-icing 

Answer 60

75% N2

Question 61

Minimum temperature for operation of tail deicing boots indicated RAT 

Answer 61

-35°C (-31°F)

Question 62

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

Answer 62

ENG ON WING\ENG PT2\TT2.

Question 63

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

Answer 63

Two minutes 20 to 30%

Question 64

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

Answer 64

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

Question 65

Can you use the auto pilot in severe icing conditions?

Answer 65

No it’s prohibited

Question 66

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

Answer 66

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

Question 67

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 _____

Answer 67

1. auto pilot. 2. composite 3. take off

Question 68

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

Answer 68

350 feet

Question 69

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

Answer 69

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

Question 70

VOR approaches must use the _____ mode

Answer 70

APPR mode

Question 71

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.

Answer 71

15 miles

Question 72

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

Answer 72

Prohibited

Question 73

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

Answer 73

88 minutes

Question 74

What are the power settings on the EPU

Answer 74

28 V 800 and1100 AMps

Question 75

 Types of batteries, amps and volts 

Answer 75

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

Question 76

Baggage nose

Answer 76

400 pounds32 pounds per square foot 

Question 77

Engine Type  And thrust

Answer 77

Fj44-3a turbofan 2780 lbs of thrust

Question 78

Wingspan

Answer 78

 53 feet 

Question 79

Horizontal, stabilizer length

Answer 79

20.8 feet.

Question 80

Tail height

Answer 80

15.3 feet.

Question 81

Turning radius

Answer 81

70 feet 

Question 82

How many locking pins in the main cabin door? 

Answer 82

12

Question 83

Aft baggage compartment

Answer 83

600 pounds 50 ft.³ space 

Question 84

How many electrical buses are there? 

Answer 84

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

Question 85

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

Answer 85

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