Excel (N560VS) Limitations Flashcards
(145 cards)
1
Q
Maximum Design Ramp Weight
A
20,200
2
Q
Maximum Design Takeoff Weight
A
20,000
3
Q
Maximum Design Landing Weight
A
18,700
4
Q
Maximum Design Zero Fuel Weight
A
15,000
5
Q
Minimum Flight Weight
A
12,400
6
Q
Maximum Tailcone Baggage Weight
A
700
7
Q
Takeoff weight is limited by the most restrictive of…
A
- Maximum Certified Takeoff Weight
- Max Weight Permitted by Climb Requirements
- Takeoff Field Length
8
Q
Landing weight is limited by the most restrictive of…
A
- Maximum Certified Landing Weight
- Max Landing Weight Permitted by Climb Requirements or Brake Energy Limit
- Landing Distance
9
Q
Center of Gravity Limits Envelope
A
Refer to Figure 2-1
10
Q
Max Takeoff Thrust Time Limit
A
5 minutes (10 minutes for OEI)
11
Q
Max Takeoff ITT
A
720
12
Q
Max Continuous ITT
A
720
13
Q
Max Starting ITT
A
720** (Refer to Figure 2-3)
14
Q
Max Transient ITT
A
760 - 20 seconds (Refer to Figure 2-3)
15
Q
Max Takeoff N2
A
101.8%
16
Q
Max Continous N2
A
101.8%
17
Q
Min Ground Idle N2
A
47.0% MIN (EEC Mode Only)
18
Q
Min Flight Idle N2
A
51.5% MIN (EEC or MANUAL Mode)
19
Q
Max Transient N2
A
103.0% - 20 seconds (Refer to Figure 2-4)
20
Q
Max Takeoff N1
A
100.0%
21
Q
Max Continuous N1
A
100.0%
22
Q
Max Transient N1
A
102.0% - 20 seconds (Refer to Figure 2-4)
23
Q
Normal Oil Pressure - Takeoff and Max Continuous
A
45 - 140 (Above 60% N2)
24
Q
Start Oil Pressure may exceed 140PSI…
A
(Not to exceed 250) for up to 300 seconds
25
Normal Oil Pressure - Ground Idle
25(MIN) - 140
26
Normal Oil Pressure - Flight Idle
25(MIN) - 140
27
Min Transient Oil Pressure - 20 Seconds
0
28
Transient Oil Pressure - 120 Seconds
20(MIN)
| 250(MAX)
29
Normal Oil Temp - Takeoff and Max Continuous
10 - 121.1
30
Min Oil Temp - Ground and Flight Idle
-40 - 121.1
31
Min Oil Temp - Starting
-40
32
Max Transient Oil Temp
135 - 120seconds
33
Starter Limitation
3 cycles per 30 minutes w/ 90 second rest
34
Battery Limitation
3 cycles per hour
35
Cross-Gen Start =
1/3 battery start
36
EPU Start
0 battery start
37
APU Start =
Same as Battery Start Limits per SB
38
EPU Requirement
28VDC and 800amp (MIN)
39
EPU Limits
>28VDC or 1000amp may damage starter
40
Ground operation of pitot static heat is limited to...
2 min to preclude damage to pitot tubes and AOA vane
41
Max Generator Load for Ground Operations
200amp (w/ transients 250amp - 4 minutes)
42
Normal Avionics Gound Operating Limit
See Figure 2-5
43
N560VS Hydraulic Fluid
Skydrol
44
Approved Hydraulic Fluids
See List
45
Approved Engine Oils
See List
46
N560VS Engine Oil
Mobil Jet Oil II
47
Max Oil Consumption
1qt per 10hr
| See maint. manual if more
48
Max mixing of approved oils
2qt per 400hr
| >2qt - drain and flush
49
If non-approved oils mixed
Drain and Flush
50
Single Point Refueling Pressure
10-55 psi
51
Max De-Fueling Pressure
-10 psi
52
FUEL BOOST pumps ON when...
LO FUEL LEVEL annunciator or 400lb or less
53
FUEL BOOST pumps ON when...
LO FUEL LEVEL annunciator or 400lb or less
54
Approved Fuels
See Figure 2-6
55
Fuel ANTI-ICE Additive required?
NO
56
Jet A Min Fuel Temp
-40C
57
Jet A Max Fuel Temp
+57C
58
Jet A Max Altitude
45000
59
Max Fuel Imbalance - Normal Operation
400lb
60
Max Fuel Imbalance - Emergency Return
800lb
61
Mmo
.75 (above 26,515)
62
Vmo 8000-26,515
305
63
Vmo <8000
260
64
Va
See Figure 2-9
65
Vfe (7-15 deg)
200
66
Vfe ( 35 deg)
175
67
Vle
250
68
Vlo
Extend - 250
| Retract - 200
69
Vsb
No Limit
70
Vmca
90
71
Vmcg
81
72
Vmcl
92
73
Max Autopilot Speed
305 / .75
74
Max Takeoff and Landing Altitude
14,000
75
Max Tailwind
10
76
Max Takeoff and Landing Ambient Temp
ISA+39 (Figure 2-8)
77
Min Takeoff and Landing Ambient Temp
-54C (See Figure 2-8)
78
The autopilot and yaw damper must be...
OFF for takeoff and landing
79
Max Tire Ground Speed
165
80
Lavatory doors...
must be latched open for takeoff and landing.
| Emergency Exit
81
Engine sync must be...
OFF for takeoff and landing
82
Takeoffs and landings are limited to...
paved runway surfaces.
83
Takeoffs and landings are limited to...
paved runway surfaces.
84
Takeoff from a wet runway when using thrust reversers for for performance credit is limited to...
75ft MIN
85
Antiskid must...
be operational for takeoff and landing
86
Rudder Bias Requirements for Takeoff
1. Bias - Operational
2. Rudder Bias Heat - Operational
3. Satisfactory Preflight Test - Section III, Normal Proc.
87
Takeoff prohibited with frost adhering to...
1. Wing Leading Edge
2. Upper Wing Surface
3. Windshield
88
Takeoff prohibited with ice, snow or slush adhering to...
1. Wing Leading Edge and Upper Surface
2. Flight Control Surfaces Including All Hinge Gaps
3. Horizontal Stabilizer
4. Vertical Stabilizer
5. Engine Inlets
6. Top of Engine Pylons
7. Top of Fuselage
8. Windshield
9. All Static Ports
10. Angle of Attack Vane
11. Upper Surface of Nose Forward of Windshield
89
Takeoff prohibited with ice, snow or slush adhering to...
1. Wing Leading Edge and Upper Surface
2. Flight Control Surfaces Including All Hinge Gaps
3. Horizontal Stabilizer
4. Vertical Stabilizer
5. Engine Inlets
6. Top of Engine Pylons
7. Top of Fuselage
8. Windshield
9. All Static Ports
10. Angle of Attack Vane
11. Upper Surface of Nose Forward of Windshield
90
Refer to ... for information on Ground Deicing
Section VII, Advisory Information
91
A visual and tactile inspection of wing leading edge and upper surface must be performed when...
< +6C or Unknown Fuel Temp >0C when
1. Visible moisture, or
2. Water on upper wing surface, or
3. <3C temp/dew point spread
4. Conditions conducive to frost
92
Takeoff with Red Annunciator?
NO
93
Takeoff with Amber Annunciator?
Only if Deferred per MEL
94
Min Icing Airspeed (Except TO and Ldg)
160
95
Max Operating Altitude
45,000
96
Max VGs Missing
3
97
Max Altitude w/ 1-3 VGs Missing
41,000
98
Max Enroute Ambient Temp
See Fig 2-8
99
Min Enroute Ambient Temp
See Figure 2-8
100
Max Generator Load
300amp
101
When the airplane has been exposed to prolonged (>2hr) at temps < -7C cabin must be warmed to at least...
+13C prior to flight above FL250 to verify proper deployment of passenger oxygen masks.
102
Severe Icing Limits
See AFM Limitations
103
Number of VGs
52 (26 per wing)
104
Number of Boundary Layer Energizers (BLE)
22 (11 per wing)
105
Max Number of BLEs missing
0
106
Min Flight Crew for All Operations
1 pilot and 1 copilot
107
Max Load Factor
Flaps 0: -1.2G to +3.0G at 20,000lb
Flaps 7-35: 0.0G t0o +2.0G at 20,000lb
(Limits bank angle and pull-up maneuvers)
Landing: 0.0G to +2.0G at 18,700
(Limits rate of descent to 600fpm)
108
Max Load Factor
Flaps 0: -1.2G to +3.0G at 20,000lb
Flaps 7-35: 0.0G t0o +2.0G at 20,000lb
(Limits bank angle and pull-up maneuvers)
Landing: 0.0G to +2.0G at 18,700
(Limits rate of descent to 600fpm)
109
Normal Cabin Pressurization Limits
0.0 - 9.6 +/-0.1 PSI
110
Pressure Relief Valve
9.5 +/-0.1 PSI
111
Pressurization Gauge Redline
9.7 +/-0.1 PSI
112
No acrobatic maneuvers, including spins above...
25,000
113
For all takeoffs and landings, passenger seats must be...
1. fully upright and outboard
| 2. seat belts and shoulder harnesses fastened
114
Max number of passengers (per AFM, not configuration)
12
115
If BATT O'TEMP illuminates during ground operation...
...do not takeoff.
116
One pilot must be seated w/ seatbelt fastened for...
...all autopilot operations.
117
Autopilot operation is prohibited if any ... illuminates during flight.
Comparison Monitor Annunciator
118
Minimum Autopilot Altitudes
Enroute - 1000AGL
Non-Precision Approach - 300AGL
Precision Approach - 180AGL
119
Max Altitude for Continuous O2 Mask Use
Crew - 40,000
| Passenger - 25,000
120
Reverse thrust must be reduced to idle detent by...
...60kt
121
Max Reverse Thrust
Approx 75% of Takeoff Thrust
122
Engine static ground operation is limited to ... with thrust reversers deployed
... idle power ...
123
Use of thrust reversers is prohibited for...
...touch and go landings
124
Thrust reversers must be checked...
1. First Flight of the Day
2. Any Flight using TR for Performance Credit
3. First Flight after ANY Maintenance
125
The use of thrust reversers is prohibited to...
...back the airplane
126
APU operation is prohibited until a...
...satisfactory test has been accomplished.
127
Starting the APU is prohibited whenever...
APU FAIL illuminated
128
APU start is prohibited...
after a dual generator failure
129
Following shutdown for any reason, APU restart must not be attempted until...
...30 sec after RPM reads 0%
130
Applying deice/anti-ice fluid is prohibited with...
APU operating
131
Max Thrust Reverser Deployed Time w/ APU Operating
30 seconds
132
APU is not approved for...
unattended operation
133
APU is not approved for...
unattended operation
134
Max APU Start Altitude
20,000
135
Max APU Operating Altitude
30,000
136
Max APU EGT
690 (will shut down automatically if EGT limit exceeded)
137
Max APU RPM%
108%
138
Max/Min APU Fuel Temp
Same as Engine Limitations
139
Max APU Generator Load
Ground: 200amp
Flight: 230amp
140
Max/Min APU Operating Temp
-54C/+54C
141
APU Starter Limits
3 cycles per 30min w/ 90sec rest between cycles
142
APU Battery Start Limits
9 per hour (0 if Ext Pwr used to start APU)
143
APU ... assist during main engine start.
DOES NOT
144
Min Tail Deice Temp (RAT)
<150kt: -40C
| >150kt: -35C
145
If AHRS moved to DG mode, it must...
...remain in DG mode for remainder of flight.
