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
Max temp for start, takeoff and landing
52c
26
Flaps up max load factor
2.5g
27
Flaps extended max load factor
2.0g
28
If landing above MLW what’s the max load factor with flaps 3/full?
1.5g
29
When must the interior doors be secured open?
Taxi, TO, and landing
30
Can XM weather be used as a primary source of wx data?
No
31
Total usable fuel capacity
13,050lbs (500) +100lbs unusable
32
Praetor 600 individual usable tank capacities
Wing tanks: 6,525lbs FWD tank: 1,430lbs VTRL tank: 1,650lbs
33
What type of APU
Honeywell 36-150
34
Max altitude APU start/operation
31,000ft
35
Min temp for inflight APU start
-37c
36
Max altitude for APU assist engine start
23,000ft
37
Max alt for APU powered ECS
20,000ft
38
APU max rotor speed
106%
39
APU max start EGT
985c
40
APU max continuous EGT
757c
41
APU starter limits
3 consecutive start attempts with 30 sec inbetween
42
APU shutoff button pushed in…
Fuel SOV closes Bleed air closes Arms “B” fire bottle Overrides FADEC Initiates a power down
43
Engine
Honeywell AS907-3-1E
44
Ground start ITT Inflight?
650c 800c
45
Max continuous ITT
950c
46
Min and max oil temps
15c to 138c (-40c to 5c is allowed if engines left at ground idle)
47
Engine starter limits
3 consecutive cycles within 5 min requires 15 min cool down.
48
Engine starter max duty time
80sec
49
When do icing conditions exist?
10c and below with visible moisture OAT = ground TAT = inflight
50
Max alt with single bleed source
20,000ft (max altitude that APU can assist)
51
AP min engagement height
400ft
52
AP min use heights with and without vertical path
80ft with vertical path 180 without vertical path
53
APU auto shutdown inflight
Over speed Under speed ECU internal failure APU bleed leak
54
APU auto shutdown on ground
Same as inflight PLUS APU fire EGT over temp High oil temp Low oil press Starter not disengaged Fuel SOV fail
55
Are FMS speeds approved for OEI operations?
No
56
RNP less than what is not approved?
Less than RNP 0.3
57
What is required when using VNAV?
Flight director
58
When can you arm the ILS with the APPR button?
Less than 90 degrees and within 30 miles.
59
If the HI FIELD flag doesn’t extinguish by 24,800ft…
Max alt is now 25,000
60
On landing, Delta-P must be what psi?
Below 0.2psi
61
Xwind TO above 25kts, when do we engage auto throttle?
Above 400ft
62
Speed knob position before takeoff
MAN
63
Radar altimeter trigger altitude
2500ft
64
Max pressure diff at 5800ft cabin
9.73psid
65
Max diff over pressure
10.4psid
66
Max diff negative pressure
-0.5psid
67
Max diff pressure for TO and landing
0.2psid