King Air 350i Limitations M.F.Ö Flashcards Preview

B-350 > King Air 350i Limitations M.F.Ö > Flashcards

Flashcards in King Air 350i Limitations M.F.Ö Deck (47):
1

King Air 350i ProLine 21

Flash Cards with Limitations


::: FLYRIGHT ::::
::: M.F.Ö:::

INTENTIONALLY LEFT BLANK
;)

2

AIRSPEED LIMITATIONS

Maneuvering Speed (VA)


184 KIAS

3

AIRSPEED LIMITATIONS

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

Approach
202 KIAS

Full Down
158 KIAS

4

AIRSPEED LIMITATIONS

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

Extension
184 KIAS

Retraction
166 KIAS

5

AIRSPEED LIMITATIONS

Maximum Landing Gear Extended Speed (VLE).

184 KIAS

6

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

7

AIRSPEED INDICATOR DISPLAY

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


81 KIAS

8

AIRSPEED INDICATOR DISPLAY

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


89 KIAS

9

AIRSPEED INDICATOR DISPLAY

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


96 KIAS

10

AIRSPEED INDICATOR DISPLAY

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


125 KIAS

11

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

12

ENGINE OPERATING LIMITS

Gas Generator RPM % N1

Max Cruise.....
Takeoff ...

Max Cruise..104

Takeoff ..........104

13

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

14

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

15

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%

16

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%

17

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,

18

AVIATION GASOLINE LIMITATIONS


What are the limitations on the use of
AVGAS ?

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

19

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.)

20

FUEL MANAGEMENT

FUEL IMBALANCE

Maximum allowable fuel imbalance between the wing fuel system?


300 pounds

21

FUEL MANAGEMENT

FUEL CROSSFEED

Permitted only when ....


..one engine is inoperative

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.


265 lbs

23

FUEL MANAGEMENT

OPERATING WITH LOW FUEL PRESSURE

Operation with the L/R fuel pressure annunciator illuminated is limited to_ hours


10

24

PROPELLERS

PROPELLER ROTATIONAL SPEED LIMITS

Minimum idle speed....


1050 rpm

25

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

26

MISCELLANEOUS INSTRUMENT MARKINGS

PNEUMATIC PRESSURE GAUGE

Green Arc
(Normal Operating Range).


12 to 20 psi

27

MAXIMUM OPERATING ALTITUDE LIMITS

Normal Operation ...


35,000 feet

28

MAXIMUM OUTSIDE AIR TEMPERATURE LIMITS

Sea Level to 25,000 feet pressure altitude ...


ISA + 37°C

29

CABIN PRESSURIZATION LIMIT

Maximum Cabin Pressure Differential....


6.6 psi

30

SYSTEMS AND EQUIPMENT LIMITS

RUDDER BOOST

Must be operational for _


all flights

31

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.

32

SYSTEMS AND EQUIPMENT LIMITS

BRAKE DEICE (IF INSTALLED)

Is not to be operated above ..


15°C

33

ICING LIMITATIONS

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


-40°C

34

ICING LIMITATIONS

Min airspeed for sustained icing flight....


140 knots

35

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

36

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.

37

AUTOPILOT

Minimum engage height after takeoff.....


400 ft AGL

38

AUTOPILOT

Minimum use height during cruise...


1000 ft AGL

39

AUTOPILOT

Minimum use height during approach...


79 ft AGL

40

AUTOPILOT

Minimum use height during steep approach....


160 ft AGL

41

AUTOPILOT

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


Less than 90°

42

AUTOPILOT

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


70°

43

WEIGHTS

Maximum Ramp Weight...


15,100 lbs

44

WEIGHTS

Maximum Take-off Weight..


15,000 lbs

45

WEIGHTS

Maximum Landing Weight...


15,000 lbs

46

WEIGHTS

Maximum Zero-Fuel Weight..


12,500 lbs

47

WEIGHTS

Maximum Weight in Baggage Compartment:


550 lbs