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
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
34
MAXIMUM OUTSIDE AIR TEMPERATURE LIMITS Above 25,000 feet pressure altitude ...
ISA +31 C
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