Excel (N560VS) Limitations Flashcards
Maximum Design Ramp Weight
20,200
Maximum Design Takeoff Weight
20,000
Maximum Design Landing Weight
18,700
Maximum Design Zero Fuel Weight
15,000
Minimum Flight Weight
12,400
Maximum Tailcone Baggage Weight
700
Takeoff weight is limited by the most restrictive of…
- Maximum Certified Takeoff Weight
- Max Weight Permitted by Climb Requirements
- Takeoff Field Length
Landing weight is limited by the most restrictive of…
- Maximum Certified Landing Weight
- Max Landing Weight Permitted by Climb Requirements or Brake Energy Limit
- Landing Distance
Center of Gravity Limits Envelope
Refer to Figure 2-1
Max Takeoff Thrust Time Limit
5 minutes (10 minutes for OEI)
Max Takeoff ITT
720
Max Continuous ITT
720
Max Starting ITT
720** (Refer to Figure 2-3)
Max Transient ITT
760 - 20 seconds (Refer to Figure 2-3)
Max Takeoff N2
101.8%
Max Continous N2
101.8%
Min Ground Idle N2
47.0% MIN (EEC Mode Only)
Min Flight Idle N2
51.5% MIN (EEC or MANUAL Mode)
Max Transient N2
103.0% - 20 seconds (Refer to Figure 2-4)
Max Takeoff N1
100.0%
Max Continuous N1
100.0%
Max Transient N1
102.0% - 20 seconds (Refer to Figure 2-4)
Normal Oil Pressure - Takeoff and Max Continuous
45 - 140 (Above 60% N2)
Start Oil Pressure may exceed 140PSI…
(Not to exceed 250) for up to 300 seconds
Normal Oil Pressure - Ground Idle
25(MIN) - 140
Normal Oil Pressure - Flight Idle
25(MIN) - 140
Min Transient Oil Pressure - 20 Seconds
0
Transient Oil Pressure - 120 Seconds
20(MIN)
250(MAX)
Normal Oil Temp - Takeoff and Max Continuous
10 - 121.1
Min Oil Temp - Ground and Flight Idle
-40 - 121.1
Min Oil Temp - Starting
-40
Max Transient Oil Temp
135 - 120seconds
Starter Limitation
3 cycles per 30 minutes w/ 90 second rest
Battery Limitation
3 cycles per hour
Cross-Gen Start =
1/3 battery start
EPU Start
0 battery start
APU Start =
Same as Battery Start Limits per SB
EPU Requirement
28VDC and 800amp (MIN)
EPU Limits
> 28VDC or 1000amp may damage starter
Ground operation of pitot static heat is limited to…
2 min to preclude damage to pitot tubes and AOA vane
Max Generator Load for Ground Operations
200amp (w/ transients 250amp - 4 minutes)
Normal Avionics Gound Operating Limit
See Figure 2-5
N560VS Hydraulic Fluid
Skydrol
Approved Hydraulic Fluids
See List
Approved Engine Oils
See List
N560VS Engine Oil
Mobil Jet Oil II
Max Oil Consumption
1qt per 10hr
See maint. manual if more
Max mixing of approved oils
2qt per 400hr
>2qt - drain and flush
If non-approved oils mixed
Drain and Flush
Single Point Refueling Pressure
10-55 psi
Max De-Fueling Pressure
-10 psi
FUEL BOOST pumps ON when…
LO FUEL LEVEL annunciator or 400lb or less
FUEL BOOST pumps ON when…
LO FUEL LEVEL annunciator or 400lb or less
Approved Fuels
See Figure 2-6
Fuel ANTI-ICE Additive required?
NO
Jet A Min Fuel Temp
-40C
Jet A Max Fuel Temp
+57C
Jet A Max Altitude
45000
Max Fuel Imbalance - Normal Operation
400lb
Max Fuel Imbalance - Emergency Return
800lb
Mmo
.75 (above 26,515)
Vmo 8000-26,515
305
Vmo <8000
260
Va
See Figure 2-9
Vfe (7-15 deg)
200
Vfe ( 35 deg)
175
Vle
250
Vlo
Extend - 250
Retract - 200
Vsb
No Limit
Vmca
90
Vmcg
81
Vmcl
92
Max Autopilot Speed
305 / .75
Max Takeoff and Landing Altitude
14,000
Max Tailwind
10
Max Takeoff and Landing Ambient Temp
ISA+39 (Figure 2-8)
Min Takeoff and Landing Ambient Temp
-54C (See Figure 2-8)
The autopilot and yaw damper must be…
OFF for takeoff and landing
Max Tire Ground Speed
165
Lavatory doors…
must be latched open for takeoff and landing.
Emergency Exit
Engine sync must be…
OFF for takeoff and landing
Takeoffs and landings are limited to…
paved runway surfaces.
Takeoffs and landings are limited to…
paved runway surfaces.
Takeoff from a wet runway when using thrust reversers for for performance credit is limited to…
75ft MIN
Antiskid must…
be operational for takeoff and landing
Rudder Bias Requirements for Takeoff
- Bias - Operational
- Rudder Bias Heat - Operational
- Satisfactory Preflight Test - Section III, Normal Proc.
Takeoff prohibited with frost adhering to…
- Wing Leading Edge
- Upper Wing Surface
- Windshield
Takeoff prohibited with ice, snow or slush adhering to…
- Wing Leading Edge and Upper Surface
- Flight Control Surfaces Including All Hinge Gaps
- Horizontal Stabilizer
- Vertical Stabilizer
- Engine Inlets
- Top of Engine Pylons
- Top of Fuselage
- Windshield
- All Static Ports
- Angle of Attack Vane
- Upper Surface of Nose Forward of Windshield
Takeoff prohibited with ice, snow or slush adhering to…
- Wing Leading Edge and Upper Surface
- Flight Control Surfaces Including All Hinge Gaps
- Horizontal Stabilizer
- Vertical Stabilizer
- Engine Inlets
- Top of Engine Pylons
- Top of Fuselage
- Windshield
- All Static Ports
- Angle of Attack Vane
- Upper Surface of Nose Forward of Windshield
Refer to … for information on Ground Deicing
Section VII, Advisory Information
A visual and tactile inspection of wing leading edge and upper surface must be performed when…
< +6C or Unknown Fuel Temp >0C when
- Visible moisture, or
- Water on upper wing surface, or
- <3C temp/dew point spread
- Conditions conducive to frost
Takeoff with Red Annunciator?
NO
Takeoff with Amber Annunciator?
Only if Deferred per MEL
Min Icing Airspeed (Except TO and Ldg)
160
Max Operating Altitude
45,000
Max VGs Missing
3
Max Altitude w/ 1-3 VGs Missing
41,000
Max Enroute Ambient Temp
See Fig 2-8
Min Enroute Ambient Temp
See Figure 2-8
Max Generator Load
300amp
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.
Severe Icing Limits
See AFM Limitations
Number of VGs
52 (26 per wing)
Number of Boundary Layer Energizers (BLE)
22 (11 per wing)
Max Number of BLEs missing
0
Min Flight Crew for All Operations
1 pilot and 1 copilot
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)
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)
Normal Cabin Pressurization Limits
0.0 - 9.6 +/-0.1 PSI
Pressure Relief Valve
9.5 +/-0.1 PSI
Pressurization Gauge Redline
9.7 +/-0.1 PSI
No acrobatic maneuvers, including spins above…
25,000
For all takeoffs and landings, passenger seats must be…
- fully upright and outboard
2. seat belts and shoulder harnesses fastened
Max number of passengers (per AFM, not configuration)
12
If BATT O’TEMP illuminates during ground operation…
…do not takeoff.
One pilot must be seated w/ seatbelt fastened for…
…all autopilot operations.
Autopilot operation is prohibited if any … illuminates during flight.
Comparison Monitor Annunciator
Minimum Autopilot Altitudes
Enroute - 1000AGL
Non-Precision Approach - 300AGL
Precision Approach - 180AGL
Max Altitude for Continuous O2 Mask Use
Crew - 40,000
Passenger - 25,000
Reverse thrust must be reduced to idle detent by…
…60kt
Max Reverse Thrust
Approx 75% of Takeoff Thrust
Engine static ground operation is limited to … with thrust reversers deployed
… idle power …
Use of thrust reversers is prohibited for…
…touch and go landings
Thrust reversers must be checked…
- First Flight of the Day
- Any Flight using TR for Performance Credit
- First Flight after ANY Maintenance
The use of thrust reversers is prohibited to…
…back the airplane
APU operation is prohibited until a…
…satisfactory test has been accomplished.
Starting the APU is prohibited whenever…
APU FAIL illuminated
APU start is prohibited…
after a dual generator failure
Following shutdown for any reason, APU restart must not be attempted until…
…30 sec after RPM reads 0%
Applying deice/anti-ice fluid is prohibited with…
APU operating
Max Thrust Reverser Deployed Time w/ APU Operating
30 seconds
APU is not approved for…
unattended operation
APU is not approved for…
unattended operation
Max APU Start Altitude
20,000
Max APU Operating Altitude
30,000
Max APU EGT
690 (will shut down automatically if EGT limit exceeded)
Max APU RPM%
108%
Max/Min APU Fuel Temp
Same as Engine Limitations
Max APU Generator Load
Ground: 200amp
Flight: 230amp
Max/Min APU Operating Temp
-54C/+54C
APU Starter Limits
3 cycles per 30min w/ 90sec rest between cycles
APU Battery Start Limits
9 per hour (0 if Ext Pwr used to start APU)
APU … assist during main engine start.
DOES NOT
Min Tail Deice Temp (RAT)
<150kt: -40C
>150kt: -35C
If AHRS moved to DG mode, it must…
…remain in DG mode for remainder of flight.
