Limitations Flashcards
Global 6000 model designation
BD700-1A10
Structural weight limits Max Taxi/ramp Max T.O. Max landing Max zero fuel Min flight Min op. Empty
MRW 99,750 MTO 99,500 MLW 78,600 MZFW 58,000 MFW 48,200 MOEW 45,000
T.O. and land near body of water
Above max landing weight
Outflow valve 2 closed and 1 pack off
VMO < 8,000
> 8,000
< 8,000 300
> 8,000 340
MMO
30,260’ - 35,000’
0.89 M
VMCG / VMCA 6/16 flaps
80 kts / 86kts
VMCG / VMCA 0 flaps, sup. 24
92 kts / 95 kts
Slats extended
225 kts
Flaps 6
16
30
210 kts
210 kts
185 kts
Gear VLO / VLE
200 kts
250 kts / 0.70M
Tire limit
183 kts
Turbulence
300 kts / 0.80M
Load Factor Limits
Slats / flaps retracted
Slats / flaps extended
-1.0 to +2.5G
- 0 to +2.0G
Approach
Max glide angle _____
Glide angle between ___ and___ must be……
Glide angle ___ to ___ see supplement ___
3.5
3.5 and 4.5
w/restrictions listed in sup. 29
4.5 to 5.5….40
Spoilers retracted by
300’ AGL
Max occupancy
22 including 19 pax or the number of certified seats, whichever is less.
Min crew
1 pilot and 1 copilot
Slope
+2% to -2%
Max alt. for T.O. and land
10,000’
Max alt for T.O. and land IAW sup. 20
13,700’
Max operating alt.
51,000’
Max alt. With gear extended
20,000’
Max alt. With flaps extended
18,000’
Min. Temp
Max. Temp
-40 C
+50 C
note:
See AFM 02-04-01 for temp.
Limits at altitude
Cowl AI on ( ground )
+10 C OAT or below and visible moisture,
Less than 1sm vis., or on contaminated surfaces
Wing AI on ( ground )
+5 C OAT or below and visible moisture,
Less than 1sm vis., or on contaminated surfaces
Wing and cowl AI on ( in flight )
+10 C TAT to -40C SAT in visible moisture
AI holding limitation
No slats
Min N2 ( accept on final Aprch ) with green wing ice indications
76%
Cold weather supplement
FCOM 1, sup. 1
True or False
T.O. permitted with frost on bottom of wing
True
True or False
Takeoff prohibited with contamination on any surface
False
T.O. Prohibited with contamination on critical surfaces
AI switch position when ice is detected
ON
True or False
AI auto prohibited for T.O.
True
Max demonstrated crosswind
29 kts
Max tailwind T.O. and land
10 kts
Max tailwind for start
20 kts
Max X wind comp. for engine start
35 kts
Max X wind comp. for take off
35 kts
Thrust limit when wind exceeds
20 kts ( taxi )
Minimum thrust
Crosswind T.O. Over 20 kts
N1 66% max below 30 kts
Tailwind start
Any external or EICAS indication of N1 rotation
Crank for 30 seconds then immediate
Auto start and Run
True or False
OMS mode can be engaged for flight
False
True or False
One stall pusher can be off in flight
False
Both must be on
True or False
IMS panel must be closed for flight
True
APU type and max rpm
RE 220 and 106%
APU Altitudes
Max operating
Max start
Max bleed extraction
Max operating 45,000’
Max start 37,000’
Max bleed 30,000’
Min temp ( ground ) APU
-40 C
APU Gen. Load limit
Ground
In flight
40 KVA
APU starter limit
3 start attempts with 1 min. Rest
Between then 60 min. Rest
APU above 37,000’
Associated hydraulic pump must be selected off 1B - AC bus 3 2B - AC bus 2 3B - AC bus 1 3A- AC bus 4
When is APU oil replenishment allowed?
On ground with APU off
Reservoir quantity greater than 1.5 qt
Within 45 min after APU shutdown
OAT -12 C or above
Ground operation with flight compartment
Temp in excess of ___ for greater than ___ minutes is ___
40 C
30 minutes
Prohibited
Engine type
BR700-710A2-20
Engine ITT limits
Start ground
Start flight
Idle
T.O.
Max cont.
Transit
Start ground 700 C
Start flight 850 C
Idle 860 C
Take off 900 C
Max cont. 860 C
Trans. 905 C
( 20 sec. )
Engine T.O. Thrust lim.
ITT
N2
N1
Time
ITT Max 900 C N2 99.6% N1 102.0% 5 min 2 eng. 10 min 1 eng.
Engine Max continuous operation
ITT
N2
N1
ITT 860 C
N2 98.9%
N1 102.0%
What rpm range is to be avoided
During ground ops?
Steady operation
66 -80% N1
( FADEC will not allow it )
What min. Oil pressure is engine
Required to be shut down?
25 PSI
As directed by checklist
Engine oil temps
Start
Above idle
Max
-40 C
+20 C
+160 C
Engine oil
consumption rate and
Replenishment lim.
0.21 qt / hr max
Prohibited below -12 C
Engine oil replenishment time
Between 5 - 30 minutes post shutdown
T.O. thrust time lim.
2 engine
1 engine
5 min.
10 min.
Engine start max N2 engage
42%
Engine starter cycle limit
1st attempt 3 min on / 15 sec off
2nd attempt 3 min on / 15 sec off
3rd attempt 3 min on / 15 min off
Pack discharge temp in manual
5 - 60 C
Air cond. and pres. in manual mode
1 pack off
Aux press max alt.
41,000’
APU bleed extraction for air cond.
45 C OAT max
Air cond. and press QFE ops
Manually set 0 landing elevation
Emer Depress max alt
15,000’
Differential pressure
Pos.
Neg.
Taxi T.O.
Landing
- 73 psi max
- 0.5 psi max
0.1 psi max
1.0 psi max
Fuel imbalance max inflight
1100 lbs
Fuel imbalance max ground
Below 19,450 lbs 1100 lbs
19,450 - 20,250
1100 - 600
Above 20,250 600
Useable fuel
Wings
Center
Aft
Total
15,050 lbs each
12,700
2,300
45,100
Min fuel aft and center
500 lbs min aft and center
Aft and center unusable unless
Center - wing full and cruise alt > FL300
Aft - wing above 5,500 and cruise > FL300
Towing fuel
5000 lb min. Unfinished interior. In actuality, 1900 lbs on nose wheel.
12000 max per wing to avoid spillage
Engine fuel temp for T.O.
+5 C min
True or False
Cross feed can be on for T.O. And land
False
Min fuel go around
600 lbs / wing and max 10 deg. NU
Wide cut fuel limited to FL___ and below
Until fuel temp is
>? Or < ? ___C
FL130
Below 15 C
Recirculation system lim.
Prohibited with wide cut fuel
Asymmetric use prohibited
Yaw damp off max alt
41,000’
Autothrottle engage on T.O.
Below 60 kts
True or False
AT is permitted with one inop.
False
Autopilot height
Engage ( climbing )
Precision
Non prec w/o VNAV
Non prec w/ VNAV
400’
80’
400’
160’
True or False
Remaining in TO / VTO vertical mode
After eng. failure is prohibited
True
EDM selection below FL____ prohibited
FL250
Max available reverse thrust above
65 KIAS
70% N1 for 30 sec.
EEC controls this value
What is required for a flight
To China
Ask JT
True or False
FMS TOLD can be used on
Contaminated runways
False
True or False
FMS TOLD prohibited for
QFE operations
True
True or False
Use of VNAV during
QFE ops. Prohibited
True
At What altitude is switching from
SVS to EVS prohibited
Below 800’
Max crosswind for HUD EVS
Approach
15 kts
Is HUD EVS approach without
FD and AP authorized
No
FD or AP guidance is required
Is HUD EVS approach
Authorized with
flaps half speed
No