King Air 350 Limitations M.F.Ö

Question 1

King Air 350i ProLine 21

Flash Cards with Limitations

::: FLYRIGHT ::::
::: M.F.Ö:::

Answer 1

INTENTIONALLY LEFT BLANK

;)

Question 2

AIRSPEED LIMITATIONS

Maneuvering Speed (VA)

Answer 2

184 KIAS

Question 3

AIRSPEED LIMITATIONS

Maximum Flap Extension/Extended Speed (VFE)
Approach ◄ APP
Full Down ◄ DN

Answer 3

Approach
202 KIAS

Full Down
158 KIAS

Question 4

AIRSPEED LIMITATIONS

Maximum Landing Gear Operating Speed (VLO)
Extension……
Retraction…..

Answer 4

Extension
184 KIAS

Retraction
166 KIAS

Question 5

AIRSPEED LIMITATIONS

Maximum Landing Gear Extended Speed (VLE).

Answer 5

184 KIAS

Question 6

AIRSPEED LIMITATIONS

Maximum Operating Speed (VMO)
Sea Level to 21,000’
21,000 to 35,000’

Answer 6

Sea Level to 21,000’
263 KIAS

21,000 to 35,000’
263-194* KIAS

*0.58 Mach

Question 7

AIRSPEED INDICATOR DISPLAY

Solid Red Bar
Stalling Speed (VSO)
Maximum weight, flaps down
idle power..

Answer 7

81 KIAS

Question 7

Maximum Demonstrated Crosswind Component

Answer 7

20 Knots

Question 7

Maximum Demonstrated Crosswind Component for Coupled Approaches

Crosswind …..

Tailwind ….

Answer 7

Crosswind ….. 32 Knots

Tailwind …. 14 Knots

Question 8

AIRSPEED INDICATOR DISPLAY

Solid Red Bar
Stalling Speed (VS1)
Maximum weight, flaps approach
idle power…

Answer 8

89 KIAS

Question 9

AIRSPEED INDICATOR DISPLAY

Solid Red Bar
Stalling Speed (VS1)
Maximum weight, flaps up
idle power…

Answer 9

96 KIAS

Question 9

Air Minimum Control Speeds
(VMCA)

Flaps Up ……………………………

Flaps Approach…………………..

Answer 9

Flaps Up …………………….94 KIAS

Flaps Approach……………93 KIAS

Question 10

AIRSPEED INDICATOR DISPLAY

Blue Line
One-Engine-Inoperative
Best Rate-of-Climb Speed

Answer 10

125 KIAS

Question 11

ENGINE OPERATING LIMITS

Maximum ITT °C

Starting ....
Idle..
Takeoff..
Max Cruise..
Max Reverse..

Answer 11

Starting .....1000°C
Idle..............750°C
Takeoff........820°C
Max Cruise.820°C
Max Reverse.760°C

Question 12

ENGINE OPERATING LIMITS

Gas Generator RPM % N1

Max Cruise…..
Takeoff …

Answer 12

Max Cruise..104

Takeoff ……….104

Question 13

ENGINE OPERATING LIMITS

Oil Temperature Limits

Minimum.
Maximum…
Limited to a maximum of 10 minutes..

Answer 13

Minimum..-40°C

Maximum…+110°C

Ltd. to a max. of 10 min.
between 99°C and 110°C

Question 14

EXTERNAL POWER LIMITS

Set to __- __ volts
minimum of __ amps momentarily
and __amps continuously

Answer 14

Set to 28.0-28.4 volts minimum of 1000 amps momentarily and 300 amps continuously

Question 14

Maximum Range Glide

Answer 14

135 KIAS

Question 15

GENERATOR LIMITS

Maximum sustained generator load is limited as follows:

In Flight:
Sea Level to 34,000’..
Above 34,000’…

Answer 15

Sea Level to 34,000’
100%

Above 34,000’..
95%

Question 16

GENERATOR LIMITS

Maximum sustained generator load is limited as follows:
Ground Operation:
N1- 62% to 70% …
N1- 70% to 100%

Answer 16

N1- 62% to 70% …
75%

N1- 70% to 100%…
100%

Question 17

STARTER LIMITS

___ON,___ OFF,
___ON,___ OFF,
___ON,___ OFF,

Answer 17

30 sec.ON, 
5 min.OFF,
30 sec.ON, 
5 min. OFF,
30 sec.ON, 
30 min.OFF,

Question 18

AVIATION GASOLINE LIMITATIONS

What are the limitations on the use of
AVGAS ?

Answer 18

1. Operation is limited to 150 hours between
   engine overhauls.
2. Operation is prohibited
   if either standby fuel pump is inoperative.
3. Crossfeed capability is required for flight above FL200

Question 19

FUEL MANAGEMENT

USABLE FUEL (gallons X 6.7 = pounds)
Total Quantity..
Each Main Fuel Tank ..
Each Aux. Fuel Tank..

Answer 19

Total Quantity..
3611 pounds(539 gl.)

Each Main Fuel Tank ..
1273 pounds(190 gl) 

Each Aux. Fuel Tank..
533 pounds(79.5 gl.)

Question 20

FUEL MANAGEMENT

FUEL IMBALANCE

Maximum allowable fuel imbalance between the wing fuel system?

Answer 20

300 pounds

Question 21

FUEL MANAGEMENT FUEL CROSSFEED Permitted only when ....

Answer 21

..one engine is inoperative

Question 22

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.

Answer 22

265 lbs

Question 23

FUEL MANAGEMENT OPERATING WITH LOW FUEL PRESSURE Operation with the L/R fuel pressure annunciator illuminated is limited to_ hours

Answer 23

10

Question 24

PROPELLERS PROPELLER ROTATIONAL SPEED LIMITS Minimum idle speed....

Answer 24

1050 rpm

Question 25

PROPELLERS PROPELLER AUTOFEATHER Must be operable for _ and must be armed for __, ___, __, and __.

Answer 25

Must be operable for all flights and must be armed for | takeoff, climb, approach, and landing

Question 26

MISCELLANEOUS INSTRUMENT MARKINGS PNEUMATIC PRESSURE GAUGE Green Arc (Normal Operating Range).

Answer 26

12 to 20 psi

Question 27

MAXIMUM OPERATING ALTITUDE LIMITS Normal Operation ...

Answer 27

35,000 feet

Question 28

MAXIMUM OUTSIDE AIR TEMPERATURE LIMITS Sea Level to 25,000 feet pressure altitude ...

Answer 28

ISA + 37°C

Question 29

CABIN PRESSURIZATION LIMIT Maximum Cabin Pressure Differential....

Answer 29

6.6 psi

Question 30

SYSTEMS AND EQUIPMENT LIMITS RUDDER BOOST Must be operational for _

Answer 30

all flights

Question 31

SYSTEMS AND EQUIPMENT LIMITS LANDING GEAR CYCLE LIMITS Limited to .. every__ for a total of _, followed by a __ cool-down period.

Answer 31

Limited to one every 5 minutes for a total of 6 cycles, | followed by a 15-minute cool-down period.

Question 32

SYSTEMS AND EQUIPMENT LIMITS BRAKE DEICE (IF INSTALLED) Is not to be operated above ..

Answer 32

15°C

Question 33

ICING LIMITATIONS Min ambient temp for operation of deicing boots....

Answer 33

-40°C

Question 34

ICING LIMITATIONS Min airspeed for sustained icing flight....

Answer 34

140 knots

Question 34

MAXIMUM OUTSIDE AIR TEMPERATURE LIMITS Above 25,000 feet pressure altitude ...

Answer 34

ISA +31 C

Question 35

ICING LIMITATIONS ENGINE ANTI-ICE, LEFT and RIGHT, shall be ___ for operation in ambient temperatures of ___ or below when ___ cannot be assured.

Answer 35

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

Question 36

ICING LIMITATIONS ENGINE ANTI-ICE, LEFT and RIGHT, shall be ____ for __ in ambient temperatures of above___

Answer 36

ENGINE ANTI-ICE, LEFT and RIGHT, shall be OFF for take-off operations in ambient temperatures of above +10°C.

Question 37

AUTOPILOT Minimum engage height after takeoff.....

Answer 37

400 ft AGL

Question 38

AUTOPILOT Minimum use height during cruise...

Answer 38

1000 ft AGL

Question 39

AUTOPILOT Minimum use height during approach...

Answer 39

79 ft AGL

Question 40

AUTOPILOT Minimum use height during steep approach....

Answer 40

160 ft AGL

Question 41

AUTOPILOT What are the maximum coupled intercept angles? Nav and Localizer ....

Answer 41

Less than 90°

Question 42

AUTOPILOT What are the maximum coupled intercept angles? Back Course...

Answer 42

70°

Question 43

WEIGHTS Maximum Ramp Weight...

Answer 43

15,100 lbs

Question 44

WEIGHTS Maximum Take-off Weight..

Answer 44

15,000 lbs

Question 45

WEIGHTS Maximum Landing Weight...

Answer 45

15,000 lbs

Question 46

WEIGHTS Maximum Zero-Fuel Weight..

Answer 46

12,500 lbs

Question 47

WEIGHTS Maximum Weight in Baggage Compartment:

Answer 47

550 lbs