Limitations Flashcards
1
Q
Global 6000 model designation
A
BD700-1A10
2
Q
Structural weight limits Max Taxi/ramp Max T.O. Max landing Max zero fuel Min flight Min op. Empty
A
MRW 99,750 MTO 99,500 MLW 78,600 MZFW 58,000 MFW 48,200 MOEW 45,000
3
Q
T.O. and land near body of water
Above max landing weight
A
Outflow valve 2 closed and 1 pack off
4
Q
VMO < 8,000
> 8,000
A
< 8,000 300
> 8,000 340
5
Q
MMO
30,260’ - 35,000’
A
0.89 M
6
Q
VMCG / VMCA 6/16 flaps
A
80 kts / 86kts
7
Q
VMCG / VMCA 0 flaps, sup. 24
A
92 kts / 95 kts
8
Q
Slats extended
A
225 kts
9
Q
Flaps 6
16
30
A
210 kts
210 kts
185 kts
10
Q
Gear VLO / VLE
A
200 kts
250 kts / 0.70M
11
Q
Tire limit
A
183 kts
12
Q
Turbulence
A
300 kts / 0.80M
13
Q
Load Factor Limits
Slats / flaps retracted
Slats / flaps extended
A
-1.0 to +2.5G
- 0 to +2.0G
14
Q
Approach
Max glide angle _____
Glide angle between ___ and___ must be……
Glide angle ___ to ___ see supplement ___
A
3.5
3.5 and 4.5
w/restrictions listed in sup. 29
4.5 to 5.5….40
15
Q
Spoilers retracted by
A
300’ AGL
16
Q
Max occupancy
A
22 including 19 pax or the number of certified seats, whichever is less.
17
Q
Min crew
A
1 pilot and 1 copilot
18
Q
Slope
A
+2% to -2%
19
Q
Max alt. for T.O. and land
A
10,000’
20
Q
Max alt for T.O. and land IAW sup. 20
A
13,700’
21
Q
Max operating alt.
A
51,000’
22
Q
Max alt. With gear extended
A
20,000’
23
Q
Max alt. With flaps extended
A
18,000’
24
Q
Min. Temp
Max. Temp
A
-40 C
+50 C
note:
See AFM 02-04-01 for temp.
Limits at altitude
25
Cowl AI on ( ground )
+10 C OAT or below and visible moisture,
Less than 1sm vis., or on contaminated surfaces
26
Wing AI on ( ground )
+5 C OAT or below and visible moisture,
Less than 1sm vis., or on contaminated surfaces
27
Wing and cowl AI on ( in flight )
+10 C TAT to -40C SAT in visible moisture
28
**AI holding limitation**
No slats
29
**Min N2 ( accept on final Aprch ) with green wing ice indications**
76%
30
**Cold weather supplement**
FCOM 1, sup. 1
31
**True or False**
**T.O. permitted with frost on bottom of wing**
True
32
**True or False**
**Takeoff prohibited with contamination on any surface**
False
T.O. Prohibited with contamination on critical surfaces
33
**AI switch position when ice is detected**
ON
34
**True or False**
**AI auto prohibited for T.O.**
True
35
**Max demonstrated crosswind**
29 kts
36
**Max tailwind T.O. and land**
10 kts
37
**Max tailwind for start**
20 kts
38
**Max X wind comp. for engine start**
35 kts
39
**Max X wind comp. for take off**
35 kts
40
**Thrust limit when wind exceeds**
**20 kts ( taxi )**
Minimum thrust
41
**Crosswind T.O. Over 20 kts**
**N1 66% max below 30 kts**
42
Tailwind start
**Any external or EICAS indication of N1 rotation**
**Crank for 30 seconds then immediate**
**Auto start and Run**
43
**True or False**
**OMS mode can be engaged for flight**
False
44
**True or False**
**One stall pusher can be off in flight**
False
Both must be on
45
**True or False**
**IMS panel must be closed for flight**
True
46
**APU type and max rpm**
RE 220 and 106%
47
**APU Altitudes**
**Max operating**
**Max start**
**Max bleed extraction**
**Max operating 45,000’**
**Max start 37,000’**
**Max bleed 30,000’**
48
**Min temp ( ground ) APU**
-40 C
49
**APU Gen. Load limit**
**Ground**
**In flight**
**40 KVA**
50
APU starter limit
**3 start attempts with 1 min. Rest**
**Between then 60 min. Rest**
51
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
```
52
**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
53
Ground operation with flight compartment
Temp in excess of ___ for greater than ___ minutes is ___
40 C
30 minutes
Prohibited
54
Engine type
BR700-710A2-20
55
**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. )
56
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.
```
57
Engine Max continuous operation
ITT
N2
N1
ITT 860 C
N2 98.9%
N1 102.0%
58
What rpm range is to be avoided
During ground ops?
Steady operation
66 -80% N1
( FADEC will not allow it )
59
What min. Oil pressure is engine
Required to be shut down?
25 PSI
As directed by checklist
60
Engine oil temps
Start
Above idle
Max
-40 C
+20 C
+160 C
61
Engine oil
consumption rate and
Replenishment lim.
0.21 qt / hr max
Prohibited below -12 C
62
Engine oil replenishment time
Between 5 - 30 minutes post shutdown
63
T.O. thrust time lim.
2 engine
1 engine
5 min.
10 min.
64
**Engine start max N2 engage**
42%
65
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
66
**Pack discharge temp in manual**
5 - 60 C
67
**Air cond. and pres. in manual mode**
1 pack off
68
Aux press max alt.
41,000’
69
**APU bleed extraction for air cond.**
45 C OAT max
70
**Air cond. and press QFE ops**
**Manually set 0 landing elevation**
71
**Emer Depress max alt**
15,000’
72
Differential pressure
Pos.
Neg.
Taxi T.O.
Landing
10. 73 psi max
- 0.5 psi max
0.1 psi max
1.0 psi max
73
**Fuel imbalance max inflight**
1100 lbs
74
Fuel imbalance max ground
Below 19,450 lbs 1100 lbs
19,450 - 20,250
1100 - 600
Above 20,250 600
75
Useable fuel
Wings
Center
Aft
Total
15,050 lbs each
12,700
2,300
45,100
76
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
77
Towing fuel
5000 lb min. Unfinished interior. In actuality, 1900 lbs on nose wheel.
12000 max per wing to avoid spillage
78
Engine fuel temp for T.O.
+5 C min
79
**True or False**
**Cross feed can be on for T.O. And land**
False
80
Min fuel go around
600 lbs / wing and max 10 deg. NU
81
Wide cut fuel limited to FL___ and below
Until fuel temp is
>? Or < ? ___C
FL130
Below 15 C
82
Recirculation system lim.
Prohibited with wide cut fuel
Asymmetric use prohibited
83
**Yaw damp off max alt**
41,000’
84
**Autothrottle engage on T.O.**
Below 60 kts
85
**True or False**
**AT is permitted with one inop.**
False
86
**Autopilot height**
**Engage ( climbing )**
**Precision**
**Non prec w/o VNAV**
**Non prec w/ VNAV**
400’
80’
400’
160’
87
**True or False**
**Remaining in TO / VTO vertical mode**
**After eng. failure is prohibited**
True
88
**EDM selection below FL____ prohibited**
FL250
89
Max available reverse thrust above
65 KIAS
70% N1 for 30 sec.
EEC controls this value
90
What is required for a flight
To China
Ask JT
91
**True or False**
**FMS TOLD can be used on**
**Contaminated runways**
False
92
**True or False**
**FMS TOLD prohibited for**
**QFE operations**
True
93
**True or False**
**Use of VNAV during**
**QFE ops. Prohibited**
True
94
At What altitude is switching from
SVS to EVS prohibited
Below 800’
95
Max crosswind for HUD EVS
Approach
15 kts
96
Is HUD EVS approach without
FD and AP authorized
No
FD or AP guidance is required
97
Is HUD EVS approach
Authorized with
flaps half speed
No
