Limitations Flashcards
Dimensions (600)
Rounded up to nearest foot
Length: 68ft
Width: 71ft
Height: 22ft
Min pavement width for 180 turn (600)
56ft
Wingtip wall to wall (600)
105’
Max ramp weight
42,990 (600)
Max takeoff weight
42,858 (600)
Max landing weight
37,479 (600)
Max zero fuel weight
28,660 (600)
Vmo/Mmo
Below 10,000 = 300kts
Above 10,000 = 320kts
Mmo = .83m
Min Mach speeds
-57c to -60c = .40m
-60c to -65c = .55m
-65c to -70c = .67m
Va (maneuvering speed)
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.
Turbulent air penetration speeds
Below 10,000: 230kts
Above 10,000: 265kts/.77m (the lower)
Vlo/vle
250kts
Flexjet Flap speeds (Vfe)
Embraer difference?
Flaps 1: 200kts
Flaps 2/3: 175kts
Flaps full: 160kts
+10kts for per Embraer limits
Max flap extension altitude
20,000ft pa
Max tire speed
182kts
Max crosswind limits
Takeoff = 35kts (FODM will be be called at 25kts for permission)
Landing = 25kts demonstrated
With crosswinds above 25kts, where should N1 be stabilized?
71-80% N1
Max crosswind for contaminated runways?
With wet ice?
20kts
15kts with wet ice.
Min takeoff and landing altitude
-1000ft
Max takeoff and landing altitude with and without HALTO
With: 13,800ft
Without: 9,600ft
Max tailwind
10kts
Max runway slope
+/- 2%
Max weights of
Forward cabinet
Stowage compartment
Cargo compartment
Forward cabinet: 88lbs
Stowage: 330lbs
Cargo: 880lbs
Min temp for start, takeoff, and landing
-40c
Max temp for start, takeoff and landing
52c
Flaps up max load factor
2.5g
Flaps extended max load factor
2.0g
If landing above MLW what’s the max load factor with flaps 3/full?
1.5g
When must the interior doors be secured open?
Taxi, TO, and landing
Can XM weather be used as a primary source of wx data?
No
Total usable fuel capacity
13,050lbs (500)
+100lbs unusable
Praetor 600 individual usable tank capacities
Wing tanks: 6,525lbs
FWD tank: 1,430lbs
VTRL tank: 1,650lbs
What type of APU
Honeywell 36-150
Max altitude APU start/operation
31,000ft
Min temp for inflight APU start
-37c
Max altitude for APU assist engine start
23,000ft
Max alt for APU powered ECS
20,000ft
APU max rotor speed
106%
APU max start EGT
985c
APU max continuous EGT
757c
APU starter limits
3 consecutive start attempts with 30 sec inbetween
APU shutoff button pushed in…
Fuel SOV closes
Bleed air closes
Arms “B” fire bottle
Overrides FADEC
Initiates a power down
Engine
Honeywell AS907-3-1E
Ground start ITT
Inflight?
650c
800c
Max continuous ITT
950c
Min and max oil temps
15c to 138c
(-40c to 5c is allowed if engines left at ground idle)
Engine starter limits
3 consecutive cycles within 5 min requires 15 min cool down.
Engine starter max duty time
80sec
When do icing conditions exist?
10c and below with visible moisture
OAT = ground
TAT = inflight
Max alt with single bleed source
20,000ft (max altitude that APU can assist)
AP min engagement height
400ft
AP min use heights with and without vertical path
80ft with vertical path
180 without vertical path
APU auto shutdown inflight
Over speed
Under speed
ECU internal failure
APU bleed leak
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
Are FMS speeds approved for OEI operations?
No
RNP less than what is not approved?
Less than RNP 0.3
What is required when using VNAV?
Flight director
When can you arm the ILS with the APPR button?
Less than 90 degrees and within 30 miles.
If the HI FIELD flag doesn’t extinguish by 24,800ft…
Max alt is now 25,000
On landing, Delta-P must be what psi?
Below 0.2psi
Xwind TO above 25kts, when do we engage auto throttle?
Above 400ft
Speed knob position before takeoff
MAN
Radar altimeter trigger altitude
2500ft
Max pressure diff at 5800ft cabin
9.73psid
Max diff over pressure
10.4psid
Max diff negative pressure
-0.5psid
Max diff pressure for TO and landing
0.2psid
