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Flexjet Praetor > Limitations > Flashcards

Limitations Flashcards

1
Q

Dimensions (600)

A

Rounded up to nearest foot

Length: 68ft
Width: 71ft
Height: 22ft

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2
Q

Min pavement width for 180 turn (600)

A

56ft

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3
Q

Wingtip wall to wall (600)

A

105’

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4
Q

Max ramp weight

A

42,990 (600)

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5
Q

Max takeoff weight

A

42,858 (600)

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6
Q

Max landing weight

A

37,479 (600)

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7
Q

Max zero fuel weight

A

28,660 (600)

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8
Q

Vmo/Mmo

A

Below 10,000 = 300kts

Above 10,000 = 320kts

Mmo = .83m

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9
Q

Min Mach speeds

A

-57c to -60c = .40m

-60c to -65c = .55m

-65c to -70c = .67m

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10
Q

Va (maneuvering speed)

A

205-225kts

Predicated on pressure altitude.

It’s the max speed that full application of flight controls can be made without over stressing the plane.

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11
Q

Turbulent air penetration speeds

A

Below 10,000: 230kts

Above 10,000: 265kts/.77m (the lower)

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12
Q

Vlo/vle

A

250kts

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13
Q

Flexjet Flap speeds (Vfe)

Embraer difference?

A

Flaps 1: 200kts
Flaps 2/3: 175kts
Flaps full: 160kts

+10kts for per Embraer limits

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14
Q

Max flap extension altitude

A

20,000ft pa

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15
Q

Max tire speed

A

182kts

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16
Q

Max crosswind limits

A

Takeoff = 35kts (FODM will be be called at 25kts for permission)

Landing = 25kts demonstrated

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17
Q

With crosswinds above 25kts, where should N1 be stabilized?

A

71-80% N1

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18
Q

Max crosswind for contaminated runways?

With wet ice?

A

20kts

15kts with wet ice.

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19
Q

Min takeoff and landing altitude

A

-1000ft

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20
Q

Max takeoff and landing altitude with and without HALTO

A

With: 13,800ft

Without: 9,600ft

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21
Q

Max tailwind

A

10kts

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22
Q

Max runway slope

A

+/- 2%

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23
Q

Max weights of

Forward cabinet
Stowage compartment
Cargo compartment

A

Forward cabinet: 88lbs
Stowage: 330lbs
Cargo: 880lbs

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24
Q

Min temp for start, takeoff, and landing

A

-40c

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25
Q

Max temp for start, takeoff and landing

A

52c

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26
Q

Flaps up max load factor

A

2.5g

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27
Q

Flaps extended max load factor

A

2.0g

28
Q

If landing above MLW what’s the max load factor with flaps 3/full?

A

1.5g

29
Q

When must the interior doors be secured open?

A

Taxi, TO, and landing

30
Q

Can XM weather be used as a primary source of wx data?

A

No

31
Q

Total usable fuel capacity

A

13,050lbs (500)

+100lbs unusable

32
Q

Praetor 600 individual usable tank capacities

A

Wing tanks: 6,525lbs
FWD tank: 1,430lbs
VTRL tank: 1,650lbs

33
Q

What type of APU

A

Honeywell 36-150

34
Q

Max altitude APU start/operation

A

31,000ft

35
Q

Min temp for inflight APU start

A

-37c

36
Q

Max altitude for APU assist engine start

A

23,000ft

37
Q

Max alt for APU powered ECS

A

20,000ft

38
Q

APU max rotor speed

A

106%

39
Q

APU max start EGT

A

985c

40
Q

APU max continuous EGT

A

757c

41
Q

APU starter limits

A

3 consecutive start attempts with 30 sec inbetween

42
Q

APU shutoff button pushed in…

A

Fuel SOV closes
Bleed air closes
Arms “B” fire bottle
Overrides FADEC
Initiates a power down

43
Q

Engine

A

Honeywell AS907-3-1E

44
Q

Ground start ITT

Inflight?

A

650c

800c

45
Q

Max continuous ITT

A

950c

46
Q

Min and max oil temps

A

15c to 138c

(-40c to 5c is allowed if engines left at ground idle)

47
Q

Engine starter limits

A

3 consecutive cycles within 5 min requires 15 min cool down.

48
Q

Engine starter max duty time

A

80sec

49
Q

When do icing conditions exist?

A

10c and below with visible moisture

OAT = ground
TAT = inflight

50
Q

Max alt with single bleed source

A

20,000ft (max altitude that APU can assist)

51
Q

AP min engagement height

A

400ft

52
Q

AP min use heights with and without vertical path

A

80ft with vertical path

180 without vertical path

53
Q

APU auto shutdown inflight

A

Over speed
Under speed
ECU internal failure
APU bleed leak

54
Q

APU auto shutdown on ground

A

Same as inflight PLUS

APU fire
EGT over temp
High oil temp
Low oil press
Starter not disengaged
Fuel SOV fail

55
Q

Are FMS speeds approved for OEI operations?

A

No

56
Q

RNP less than what is not approved?

A

Less than RNP 0.3

57
Q

What is required when using VNAV?

A

Flight director

58
Q

When can you arm the ILS with the APPR button?

A

Less than 90 degrees and within 30 miles.

59
Q

If the HI FIELD flag doesn’t extinguish by 24,800ft…

A

Max alt is now 25,000

60
Q

On landing, Delta-P must be what psi?

A

Below 0.2psi

61
Q

Xwind TO above 25kts, when do we engage auto throttle?

A

Above 400ft

62
Q

Speed knob position before takeoff

A

MAN

63
Q

Radar altimeter trigger altitude

A

2500ft

64
Q

Max pressure diff at 5800ft cabin

A

9.73psid

65
Q

Max diff over pressure

A

10.4psid

66
Q

Max diff negative pressure

A

-0.5psid

67
Q

Max diff pressure for TO and landing

A

0.2psid

Flexjet Praetor (4 decks)

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