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BE 350 > KA350 Limitations > Flashcards

KA350 Limitations Flashcards

1
Q

Limitations: Airspeed Limits (KIAS)

Maneuvering speed (Va) (ER/Non ER)

A

182 kts / 184 kts)

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2
Q

Limitations: Engine Limits

Engine Prop - N2: (RPM)

Idle:
T/O:
Max Cont:
Cruise Climb:
Max Cruise:
Max Reverse:
Transient:
A

Engine Prop - N2: (RPM)

Idle: 1050 RPM min
T/O: 1700 RPM (up to 1735 RPM for 7 mins)
Max Cont: 1700 RPM (up to 1735 RPM for 7 mins)
Cruise Climb: 1700 RPM (up to 1735 RPM for 7 mins)
Max Cruise: 1700 RPM (up to 1735 RPM for 7 mins)
Max Reverse: 1650 RPM
Transient: 1870 RPM (limited to 20 sec)

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3
Q

Limitations: Pressurization/Environmental

The “CABIN DIFF HI” Annunciator illuminates at:

A

6.9 PSID

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4
Q

Limitations: Aircraft Weights

Max Weight in Baggage Compartment

A

550 lbs

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5
Q

Limitations: Airspeed Limits (KIAS)

One-Engine Inop Best Angle of Climb (Vxse) (ER/Non ER)

A

135 kts / 125 kts

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6
Q

Limitations: Airspeed Limits (KIAS)

One-Engine Inop Best Rate of Climb (Vyse, Blue Line)

  • ER
  • Non ER
A

ER - 135 kts

Non ER - 125 kts

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7
Q

Limitations: Ice and Rain

The left and right Engine Anti-Ice shall be OFF for takeoff operations in ambient temperatures above ____ *C.

A

10*C

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8
Q

Limitations: Ice and Rain

Engine Anti-Ice shall be ON for operation in ambient temperatures of ____ *C or below when flight free of visible moisture cannot be assured.

A

5*C

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9
Q

Limitations: Airspeed Limits (KIAS)

Max Operating Speed (Vmo)

ER / Non ER
To: FL240 / FL210

Above: FL240 / FL210

A

Max Operating Speed (Vmo)

To: FL240 - 245 kts / FL210 - 263 kts

Above: FL240 .58 M / FL210 - .58M

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10
Q

Limitations: Pressurization (psi)

Max Cabin Differential

A

6.6 psi

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11
Q

Limitations: Weight (lbs)

Max Landing Weight (ER/NonER)

A

15,675 lbs / 15,000 lbs

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12
Q

Limitations: Fuel (lbs)

Usable Fuel (ER/Non ER)

A

5192 lbs / 3611 lbs

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13
Q

Limitations: Pressurization/Environmental

The “CABIN ALTITUDE” Annunciator illuminates when:

A

Cabin altitude above 10,000’

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14
Q

Limitations: Electrical

Generator Load Limits:

  • In Flight - Sea Level to 34,000’ Altitude: ____
  • In Flight - Above 34,000’ Altitude: ____
  • Ground Operation - 62-70% N1: ____
  • Ground Operation - 70-100% N1: ____
A

Generator Load Limits:

  • In Flight - Sea Level to 34,000’ Altitude: 100%
  • In Flight - Above 34,000’ Altitude: 95%
  • Ground Operation - 62-70% N1: 75%
  • Ground Operation - 70-100% N1: 100%
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15
Q

Limitations: Weight (lbs)

Max T/O Weight

  • ER
  • Non ER
A

ER - 16,500 lbs

Non ER - 15000 lbs

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16
Q

Limitations: Electrical (VDC)

Min Battery to Connect External Power:

A

20 VDC

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17
Q

Limitations: Airspeed Limits (KIAS)

Intentional One-Engine Inoperative Speed (Vsse)

  • ER
  • Non ER
A

ER - 135 kts

Non ER - 110 kts

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18
Q

Limitations: General

Max Operating Altitude

  • Normal Operation: ____
  • Yaw Damper System - Inoperative
    • Single strake: ____
    • Dual strake: ____
A

Max Operating Altitude

  • Normal Operation: 35000’
  • Yaw Damper System - Inoperative
    • Single strake: 5000’
    • Dual strake: 19000’ (STSC Supplemental 91-111)
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19
Q

Limitations: Airspeed Limits (KIAS)

Air Minimum Controlable Speed (Vmca)
(ER/Non ER)
Flaps Up:

Flaps Down:

A

Air Minimum Controlable Speed (Vmca)

Flaps Up: 101 kts / 94 kts

Flaps Down: 98 kts / 93 kts

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20
Q

Limitations: General

Altitude Limitations

Operation with AvGas:

  • Both Standby Fuel Pumps Operative: ____
  • Either Standby Fuel Pumps Inoperative: ____
  • Climb Altitude Limitation Without Crossfeed Capability: ____
A

Operation with AvGas:

  • Both Standby Fuel Pumps Operative: 35000’
  • Either Standby Fuel Pumps Inoperative: Flight Prohibited
  • Climb Altitude Limitation Without Crossfeed Capability: 20000’
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21
Q

Limitations: Winds (kts)

Max X-WindT/O

A

25 kts

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22
Q

Limitations: AutoPilot

Min Engage Height after Takeoff: ____

Min Use Height during Cruise: ____

Min Use Height during Approach: ____

Min Use Height during Steep Approach: ____

A

Min Engage Height after Takeoff: 400’

Min Use Height during Cruise: 1000’

Min Use Height during Approach: 79’

Min Use Height during Steep Approach: 160’

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23
Q

Limitations: Airspeed Limits (KIAS)

Two Engine Best Rate of Climb (Vy) (ER/Non ER)

A

135 kts / 140 kts

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24
Q

Limitations: Engine Limits

Torque: (%)

T/O:
Max Cont:
Transient:

Propeller (N2) below 1000 RPM:

A

Torque: (%)

T/O: 100% (up to 102% for 7 min)
Max Cont: 100% (up to 102% for 7 min)
Transient: 156% (limited to 20 sec)

Propeller (N2) below 1000 RPM: 62%

Note: Cruise TQ values vary with altitude and temperature.

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25
Q

Limitations: Winds (kts)

Max Tailwind Component

A

10 kts

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26
Q

Limitations: Pressurization/Environmental

Cabin Differential Pressure Gauge RED Arc

A

6.6 to end of scale

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27
Q

Limitations: Engine and Propeller

Propeller Type

A
  • Constant speed
  • Reversing
  • Counter weighted
  • Hydraulically actuated
  • Full feathering
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28
Q

Limitations: Airspeed Limits (KIAS)

Min Airspeed for Sustained Flight in Icing

A

140 kts

Note: Sustained flight in icing conditions with flaps extended is prohibited except for approach and landing.

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29
Q

Limitations: Ice and Rain

Minimum Ambient Temperature for Operation of Deicing Boots

30
Q

Limitations: Ice and Rain

Prop Deice Ammeter Normal Operating Range

A

26 to 32 Amps

31
Q

Limitations: Fuel (lbs)

Min T/O Fuel (per side)

32
Q

Limitations: Weight (lbs)

Max Ramp Weight (ER/Non ER)

A

16,600 lbs / 15,100 lbs

33
Q

Limitations: Airspeed Limits (KIAS)

Max Flap Extension/Extended (Vfe)

Approach:

Full Down:

A

Max Flap Extension/Extended (Vfe)

Approach: 202 kts

Full Down: 158 kts

34
Q

Limitations: Engine Limits

Oil Temperature: (*C)

Starting:
Idle:
T/O:
Max Cont:
Cruise Climb:
Max Cruise:
Max Reverse:
Transient:
Min for Fuel Heater operation at T/O:
A

Oil Temperature: (*C)

Starting: -40*C min
Idle: -40 - 110*C
T/O: 0 - 110*C
Max Cont: 0 - 110*C
Cruise Climb: 0 - 110*C
Max Cruise: 0 - 110*C
Max Reverse: 0 - 99*C
Transient: 0 - 110*C
Min for Fuel Heater operation at T/O: 55*C

Note: Temperatures between 99C and 110C are limited to 10 mins

35
Q

Limitations: Landing Gear

Cycle Limit:

A

1 cycle (up/down) every 5 mins for a total of 6 cycles, followed by 15 mins cool down

36
Q

Limitations: Pressurization (psi)

[CABIN DIFF HI]

A

6.9 +/-0.3 psi

37
Q

Limitations: Load Factor (Gs)

Flaps up: Neg ____ Pos ____ (Non ER)

Flaps Down: Neg ____ Pos ____ (Non ER)

A

Flaps up: Neg -1.21 Pos 3.01 (-1.24 to 3.1)

Flaps Down: Neg 0.0 Pos 2.0 (0.0 to 2.0)

38
Q

Limitations: Engine Limits

Oil Pressure: (psi)

Oil pressure below __ psi is undesirable. Under emergency conditions, to complete flight, a lower oil pressure limit of __ psi is permissible at reduced power level not exceeding __% TQ.

A

Oil pressure below 90 psi is undesirable. Under emergency conditions, to complete flight, a lower oil pressure limit of 60 psi is permissible at reduced power level not exceeding 62% TQ.

39
Q

Limitations: Airspeed Limits (KIAS)

Max Range Glide

40
Q

Limitations: Airspeed Limits (KIAS)

Turbulent Air Penetration

41
Q

Limitations: Fuel (lbs)

Minimum Landing

42
Q

Limitations: Fuel

Operation of either engine with its corresponding fuel pressure annunciator (L FUEL PRESS LO or R FUEL PRESS LO) illuminated is limited to ____ hours before overhaul or replacement of the engine-driven fuel pump. (windmilling time is not counted against this time)

43
Q

Limitations: Landing Gear and Brakes

Brake Deice Temp Operation Limit

A

Not above 15*C

44
Q

Limitations: Engine and Propeller

Engine Model Number and Type

A

PT6A-60A turboprop engine

45
Q

Limitations: Avionics and Autopilot

Autopilot Max Coupled INCPT Angle for Back Course: ____

Autopilot Max Coupled INCPT Angle for NAV/LOC: ____

A

Autopilot Max Coupled INCPT Angle for Back Course: 70*

Autopilot Max Coupled INCPT Angle for NAV/LOC: <90*

46
Q

Limitations: Pressurization (ft)

[CABIN ALTITUDE HI]

47
Q

Limitations: Electrical (VDC)

Min Battery for Battery Start:

48
Q

Limitations: Electrical (VDC)

External Power Voltage Range:

A

28 - 28.4 VDC

49
Q

Limitations: Engine Limits

Oil Pressure: (psi)

In flight, oil pressures above ____ psi, but not exceeding ____ psi are permitted only for the duration of the flight.

A

135 psi, 200 psi

50
Q

Limitations: Winds (kts)

Max Wind (any direction)

51
Q

Limitations: Pressurization/Environmental

The “CABIN ALTITUDE HI” Annunciator illuminates when:

A

Cabin altitude above 12,000’

52
Q

Limitations: Engine Limits

Oil Pressure: (psi)

Oil pressures below ____ psi are unsafe and requires that either the engine be shut down or a landing be made at the nearest suitable airport, using min power required to sustain flight.

53
Q

Limitations: Electrical

Generator Load

If OAT > 10*C and the A/C is being used, DC % Loadmeters - Both must be < or =: ____

A

30%

Note: If either Loadmeter is >30%, the A/C Compressor must be disabled, CABIN TEMP MODE - OFF of MAN HEAT for T/O.

54
Q

Limitations: Electrical

Starter Limits

A
  • 30 secs ON / 5 mins OFF
  • 30 secs ON / 5 mins OFF
  • 30 secs ON / 30 mins OFF
55
Q

Limitations: Electrical (Amps)

External Power Amps Limit:

A

1000 Amps Momentarily

300 Amp Continuous

56
Q

Limitations: Electrical

Generator Load

DC % Loadmeters - Both must be < or =: ____

57
Q

Limitations: Pressurization/Environmental

Cabin Differential Pressure Gauge GREEN Arc

A

0 to 6.6 psi

58
Q

Limitations: Fuel (lbs)

ER/Non ER
ER:

Aux:

Main:

A

ER: 1581 lbs / 0 lbs

Aux: 1065 lbs / 1065 lbs

Main: 2546 lbs / 2546 lbs

59
Q

Limitations: Engine and Propeller

What is the Range of the Primary Governor?

A

1450 to 1700 RPM

60
Q

Limitations: Engine Limits

Max ITT: (*C)

Starting:
Idle:
T/O:
Max Cont:
Cruise Climb:
Max Cruise:
Max Reverse:
Transient:
A

Max ITT: (*C)

Starting: 1000*C
Idle: 750*C
T/O: 820*C
Max Cont: 820*C
Cruise Climb: 785*C
Max Cruise: 820*C
Max Reverse: 760*C
Transient: 850*C (limited to 20 sec)

Note: High ITT at ground idle may be corrected by reducing accessory load and/or increasing rpm.

61
Q

Limitations: Fuel (lbs)

Max Imbalance

62
Q

Limitations: Engine Limits

Gas Generator - N1: (%)

Idle:
T/O:
Max Cont:
Cruise Climb:
Max Cruise:
Transient:
A

Gas Generator - N1: (%)

Idle: 62% min
T/O: 104%
Max Cont: 104%
Cruise Climb: 104%
Max Cruise: 104%
Transient: 104%
63
Q

Limitations: Pressurization/Environmental

Above what altitude do the oxygen masks automatically deploy?

64
Q

Limitations: Airspeed Limits (KIAS)

Emergency Descent (ER/Non ER)

A

182 kts / 184 kts

65
Q

Limitations: Engine Limits

Oil Pressure: (psi)

Starting:
Idle:
T/O:
Max Cont:
Cruise Climb:
Max Cruise:
Max Reverse:
Transient:
A

Oil Pressure: (psi)

Starting: 0 - 200 psi (may reach 200 during extreme cold)
Idle: 60 psi min (below 62% TQ, normal oil temp 60-70*C)
T/O: 90 - 135 psi (above 72% N1)
Max Cont: 90 - 135 psi (above 72% N1)
Cruise Climb: 90 - 135 psi (above 72% N1)
Max Cruise: 90 - 135 psi (above 72% N1)
Max Reverse: 90 - 135 psi (above 72% N1)
Transient: 200 psi

Note: Oil pressure below 90 psi is undesirable. Under emergency conditions, to complete flight, a lower oil pressure limit of 60 psi is permissible at reduced power level not exceeding 62% TQ.

66
Q

Limitations: Fuel

Fuel Crossfeed is permitted only when ____

A

one engine is inoperative.

67
Q

Limitations: Flight Controls

____ must be operational for all phases of flight.

A

Rudder Boost

68
Q

Limitations: Airspeed Limits (KIAS)

Max Airspeed for Effective Windshield Anti-icing (Vmo)

69
Q

Limitations: Engine Limits

Oil Pressure: (psi)

Fluctuations of +/- ____ psi are acceptable.

A

+/- 10 psi

70
Q

Limitations: Airspeed Limits (KIAS)

Max Landing Gear Operating Speed (Vlo)

Extension: ER/Non ER

Retraction: ER/Non ER

A

Max Landing Gear Operating Speed (Vlo)

Extension: 182/184 kts

Retraction: 164/166 kts

71
Q

Limitations: Engine and Propeller

The Overspeed Governor governs to ____.

72
Q

Limitations: Engine and Propeller

Propeller Autofeather must be armed for:

A
  • Takeoff
  • Climb
  • Approach
  • Landing

BE 350 (5 decks)

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