King Air 350 Limitations M.F.Ö Flashcards
King Air 350i ProLine 21
Flash Cards with Limitations
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AIRSPEED LIMITATIONS
Maneuvering Speed (VA)
184 KIAS
AIRSPEED LIMITATIONS
Maximum Flap Extension/Extended Speed (VFE)
Approach ◄ APP
Full Down ◄ DN
Approach
202 KIAS
Full Down
158 KIAS
AIRSPEED LIMITATIONS
Maximum Landing Gear Operating Speed (VLO)
Extension……
Retraction…..
Extension
184 KIAS
Retraction
166 KIAS
AIRSPEED LIMITATIONS
Maximum Landing Gear Extended Speed (VLE).
184 KIAS
AIRSPEED LIMITATIONS
Maximum Operating Speed (VMO)
Sea Level to 21,000’
21,000 to 35,000’
Sea Level to 21,000’
263 KIAS
21,000 to 35,000’
263-194* KIAS
*0.58 Mach
AIRSPEED INDICATOR DISPLAY
Solid Red Bar
Stalling Speed (VSO)
Maximum weight, flaps down
idle power..
81 KIAS
Maximum Demonstrated Crosswind Component
20 Knots
Maximum Demonstrated Crosswind Component for Coupled Approaches
Crosswind …..
Tailwind ….
Crosswind ….. 32 Knots
Tailwind …. 14 Knots
AIRSPEED INDICATOR DISPLAY
Solid Red Bar
Stalling Speed (VS1)
Maximum weight, flaps approach
idle power…
89 KIAS
AIRSPEED INDICATOR DISPLAY
Solid Red Bar
Stalling Speed (VS1)
Maximum weight, flaps up
idle power…
96 KIAS
Air Minimum Control Speeds
(VMCA)
Flaps Up ……………………………
Flaps Approach…………………..
Flaps Up …………………….94 KIAS
Flaps Approach……………93 KIAS
AIRSPEED INDICATOR DISPLAY
Blue Line
One-Engine-Inoperative
Best Rate-of-Climb Speed
125 KIAS
ENGINE OPERATING LIMITS
Maximum ITT °C
Starting .... Idle.. Takeoff.. Max Cruise.. Max Reverse..
Starting .....1000°C Idle..............750°C Takeoff........820°C Max Cruise.820°C Max Reverse.760°C
ENGINE OPERATING LIMITS
Gas Generator RPM % N1
Max Cruise…..
Takeoff …
Max Cruise..104
Takeoff ……….104
ENGINE OPERATING LIMITS
Oil Temperature Limits
Minimum.
Maximum…
Limited to a maximum of 10 minutes..
Minimum..-40°C
Maximum…+110°C
Ltd. to a max. of 10 min.
between 99°C and 110°C
EXTERNAL POWER LIMITS
Set to __- __ volts
minimum of __ amps momentarily
and __amps continuously
Set to 28.0-28.4 volts minimum of 1000 amps momentarily and 300 amps continuously
Maximum Range Glide
135 KIAS
GENERATOR LIMITS
Maximum sustained generator load is limited as follows:
In Flight:
Sea Level to 34,000’..
Above 34,000’…
Sea Level to 34,000’
100%
Above 34,000’..
95%
GENERATOR LIMITS
Maximum sustained generator load is limited as follows:
Ground Operation:
N1- 62% to 70% …
N1- 70% to 100%
N1- 62% to 70% …
75%
N1- 70% to 100%…
100%
STARTER LIMITS
___ON,___ OFF,
___ON,___ OFF,
___ON,___ OFF,
30 sec.ON, 5 min.OFF, 30 sec.ON, 5 min. OFF, 30 sec.ON, 30 min.OFF,
AVIATION GASOLINE LIMITATIONS
What are the limitations on the use of
AVGAS ?
- Operation is limited to 150 hours between
engine overhauls. - Operation is prohibited
if either standby fuel pump is inoperative. - Crossfeed capability is required for flight above FL200
FUEL MANAGEMENT
USABLE FUEL (gallons X 6.7 = pounds)
Total Quantity..
Each Main Fuel Tank ..
Each Aux. Fuel Tank..
Total Quantity.. 3611 pounds(539 gl.)
Each Main Fuel Tank .. 1273 pounds(190 gl)
Each Aux. Fuel Tank.. 533 pounds(79.5 gl.)
FUEL MANAGEMENT
FUEL IMBALANCE
Maximum allowable fuel imbalance between the wing fuel system?
300 pounds
FUEL MANAGEMENT
FUEL CROSSFEED
Permitted only when ….
..one engine is inoperative
FUEL MANAGEMENT
FUEL GAGES IN THE YELLOW ARC
Do not take off if fuel quantity gauges indicate in yellow arc or indicate less than_ lbs of fuel in each wing system.
265 lbs
FUEL MANAGEMENT
OPERATING WITH LOW FUEL PRESSURE
Operation with the L/R fuel pressure annunciator illuminated is limited to_ hours
10
PROPELLERS
PROPELLER ROTATIONAL SPEED LIMITS
Minimum idle speed….
1050 rpm
PROPELLERS
PROPELLER AUTOFEATHER
Must be operable for _ and must be armed for
__, ___, __, and __.
Must be operable for all flights and must be armed for
takeoff, climb, approach, and landing
MISCELLANEOUS INSTRUMENT MARKINGS
PNEUMATIC PRESSURE GAUGE
Green Arc
(Normal Operating Range).
12 to 20 psi
MAXIMUM OPERATING ALTITUDE LIMITS
Normal Operation …
35,000 feet
MAXIMUM OUTSIDE AIR TEMPERATURE LIMITS
Sea Level to 25,000 feet pressure altitude …
ISA + 37°C
CABIN PRESSURIZATION LIMIT
Maximum Cabin Pressure Differential….
6.6 psi
SYSTEMS AND EQUIPMENT LIMITS
RUDDER BOOST
Must be operational for _
all flights
SYSTEMS AND EQUIPMENT LIMITS
LANDING GEAR CYCLE LIMITS
Limited to .. every__ for a total of _,
followed by a __ cool-down period.
Limited to one every 5 minutes for a total of 6 cycles,
followed by a 15-minute cool-down period.
SYSTEMS AND EQUIPMENT LIMITS
BRAKE DEICE (IF INSTALLED)
Is not to be operated above ..
15°C
ICING LIMITATIONS
Min ambient temp for operation of deicing boots….
-40°C
ICING LIMITATIONS
Min airspeed for sustained icing flight….
140 knots
MAXIMUM OUTSIDE AIR TEMPERATURE LIMITS
Above 25,000 feet pressure altitude …
ISA +31 C
ICING LIMITATIONS
ENGINE ANTI-ICE, LEFT and RIGHT,
shall be ___ for operation in
ambient temperatures of ___ or below
when ___ cannot be assured.
ENGINE ANTI-ICE, LEFT and RIGHT,
shall be ON for operation in
ambient temperatures of +5°C or below
when flight free of visible moisture cannot be assured
ICING LIMITATIONS
ENGINE ANTI-ICE, LEFT and RIGHT,
shall be ____ for __
in ambient temperatures of above___
ENGINE ANTI-ICE, LEFT and RIGHT,
shall be OFF for take-off operations
in ambient temperatures of above +10°C.
AUTOPILOT
Minimum engage height after takeoff…..
400 ft AGL
AUTOPILOT
Minimum use height during cruise…
1000 ft AGL
AUTOPILOT
Minimum use height during approach…
79 ft AGL
AUTOPILOT
Minimum use height during steep approach….
160 ft AGL
AUTOPILOT
What are the maximum coupled intercept angles?
Nav and Localizer ….
Less than 90°
AUTOPILOT
What are the maximum coupled intercept angles?
Back Course…
70°
WEIGHTS
Maximum Ramp Weight…
15,100 lbs
WEIGHTS
Maximum Take-off Weight..
15,000 lbs
WEIGHTS
Maximum Landing Weight…
15,000 lbs
WEIGHTS
Maximum Zero-Fuel Weight..
12,500 lbs
WEIGHTS
Maximum Weight in Baggage Compartment:
550 lbs
