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

King Air 350 Limitations M.F.Ö Flashcards

1
Q

King Air 350i ProLine 21

Flash Cards with Limitations

::: FLYRIGHT ::::
::: M.F.Ö:::

A

INTENTIONALLY LEFT BLANK

;)

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2
Q

AIRSPEED LIMITATIONS

Maneuvering Speed (VA)

A

184 KIAS

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3
Q

AIRSPEED LIMITATIONS

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

A

Approach
202 KIAS

Full Down
158 KIAS

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4
Q

AIRSPEED LIMITATIONS

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

A

Extension
184 KIAS

Retraction
166 KIAS

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5
Q

AIRSPEED LIMITATIONS

Maximum Landing Gear Extended Speed (VLE).

A

184 KIAS

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6
Q

AIRSPEED LIMITATIONS

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

A

Sea Level to 21,000’
263 KIAS

21,000 to 35,000’
263-194* KIAS

*0.58 Mach

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7
Q

AIRSPEED INDICATOR DISPLAY

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

A

81 KIAS

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7
Q

Maximum Demonstrated Crosswind Component

A

20 Knots

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7
Q

Maximum Demonstrated Crosswind Component for Coupled Approaches

Crosswind …..

Tailwind ….

A

Crosswind ….. 32 Knots

Tailwind …. 14 Knots

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8
Q

AIRSPEED INDICATOR DISPLAY

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

A

89 KIAS

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9
Q

AIRSPEED INDICATOR DISPLAY

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

A

96 KIAS

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9
Q

Air Minimum Control Speeds
(VMCA)

Flaps Up ……………………………

Flaps Approach…………………..

A

Flaps Up …………………….94 KIAS

Flaps Approach……………93 KIAS

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10
Q

AIRSPEED INDICATOR DISPLAY

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

A

125 KIAS

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11
Q

ENGINE OPERATING LIMITS

Maximum ITT °C

Starting ....
Idle..
Takeoff..
Max Cruise..
Max Reverse..
A 
Starting .....1000°C
Idle..............750°C
Takeoff........820°C
Max Cruise.820°C
Max Reverse.760°C
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12
Q

ENGINE OPERATING LIMITS

Gas Generator RPM % N1

Max Cruise…..
Takeoff …

A

Max Cruise..104

Takeoff ……….104

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13
Q

ENGINE OPERATING LIMITS

Oil Temperature Limits

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

A

Minimum..-40°C

Maximum…+110°C

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

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14
Q

EXTERNAL POWER LIMITS

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

A

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

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14
Q

Maximum Range Glide

A

135 KIAS

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15
Q

GENERATOR LIMITS

Maximum sustained generator load is limited as follows:

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

A

Sea Level to 34,000’
100%

Above 34,000’..
95%

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16
Q

GENERATOR LIMITS

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

A

N1- 62% to 70% …
75%

N1- 70% to 100%…
100%

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17
Q

STARTER LIMITS

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

A 
30 sec.ON, 
5 min.OFF,
30 sec.ON, 
5 min. OFF,
30 sec.ON, 
30 min.OFF,
18
Q

AVIATION GASOLINE LIMITATIONS

What are the limitations on the use of
AVGAS ?

A
  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
Q

FUEL MANAGEMENT

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

A 
Total Quantity..
3611 pounds(539 gl.)
Each Main Fuel Tank ..
1273 pounds(190 gl) 
Each Aux. Fuel Tank..
533 pounds(79.5 gl.)
20
Q

FUEL MANAGEMENT

FUEL IMBALANCE

Maximum allowable fuel imbalance between the wing fuel system?

A

300 pounds

21
Q

FUEL MANAGEMENT

FUEL CROSSFEED

Permitted only when ….

A

..one engine is inoperative

22
Q

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.

A

265 lbs

23
Q

FUEL MANAGEMENT

OPERATING WITH LOW FUEL PRESSURE

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

A

10

24
Q

PROPELLERS

PROPELLER ROTATIONAL SPEED LIMITS

Minimum idle speed….

A

1050 rpm

25
Q

PROPELLERS

PROPELLER AUTOFEATHER

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

A

Must be operable for all flights and must be armed for

takeoff, climb, approach, and landing

26
Q

MISCELLANEOUS INSTRUMENT MARKINGS

PNEUMATIC PRESSURE GAUGE

Green Arc
(Normal Operating Range).

A

12 to 20 psi

27
Q

MAXIMUM OPERATING ALTITUDE LIMITS

Normal Operation …

A

35,000 feet

28
Q

MAXIMUM OUTSIDE AIR TEMPERATURE LIMITS

Sea Level to 25,000 feet pressure altitude …

A

ISA + 37°C

29
Q

CABIN PRESSURIZATION LIMIT

Maximum Cabin Pressure Differential….

A

6.6 psi

30
Q

SYSTEMS AND EQUIPMENT LIMITS

RUDDER BOOST

Must be operational for _

A

all flights

31
Q

SYSTEMS AND EQUIPMENT LIMITS

LANDING GEAR CYCLE LIMITS

Limited to .. every__ for a total of _,
followed by a __ cool-down period.

A

Limited to one every 5 minutes for a total of 6 cycles,

followed by a 15-minute cool-down period.

32
Q

SYSTEMS AND EQUIPMENT LIMITS

BRAKE DEICE (IF INSTALLED)

Is not to be operated above ..

A

15°C

33
Q

ICING LIMITATIONS

Min ambient temp for operation of deicing boots….

A

-40°C

34
Q

ICING LIMITATIONS

Min airspeed for sustained icing flight….

A

140 knots

34
Q

MAXIMUM OUTSIDE AIR TEMPERATURE LIMITS

Above 25,000 feet pressure altitude …

A

ISA +31 C

35
Q

ICING LIMITATIONS

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

A

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
Q

ICING LIMITATIONS

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

A

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

37
Q

AUTOPILOT

Minimum engage height after takeoff…..

A

400 ft AGL

38
Q

AUTOPILOT

Minimum use height during cruise…

A

1000 ft AGL

39
Q

AUTOPILOT

Minimum use height during approach…

A

79 ft AGL

40
Q

AUTOPILOT

Minimum use height during steep approach….

A

160 ft AGL

41
Q

AUTOPILOT

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

A

Less than 90°

42
Q

AUTOPILOT

What are the maximum coupled intercept angles?
Back Course…

A

70°

43
Q

WEIGHTS

Maximum Ramp Weight…

A

15,100 lbs

44
Q

WEIGHTS

Maximum Take-off Weight..

A

15,000 lbs

45
Q

WEIGHTS

Maximum Landing Weight…

A

15,000 lbs

46
Q

WEIGHTS

Maximum Zero-Fuel Weight..

A

12,500 lbs

47
Q

WEIGHTS

Maximum Weight in Baggage Compartment:

A

550 lbs

B-350 (2 decks)

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