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CAE > KA350 Limitations > Flashcards

KA350 Limitations Flashcards

1
Q

Limitations: General

Minimum Crew

A

One pilot

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2
Q

Limitations: Fuel

Fuel Crossfeed is permitted only when _____.

A

one engine is inoperative

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3
Q

Limitations: Ice and Rain

Prop Deice Ammeter Normal Operating Range

A

26 to 32 Amps

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4
Q

Limitations: Electrical

Min Battery Volts for Battery Start

A

23 VDC

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5
Q

Limitations: Avionics and Autopilot

Operating in the composite mode is limited to _____ and _____ _____ conditions.

A

training

display failure

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6
Q

Limitations: Aircraft Weights

Max Weight in Baggage Compartment

A

Max Weight in Baggage Compartment - 550 lbs (250 kg)

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7
Q

Limitations: Emergency Airspeeds (15,000 lbs)

Emergency Descent Speed

A

184 Kts

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8
Q

Limitations: Engine and Propeller

Propeller Autofeather must be armed for _____.

A
  • Take off
  • Climb
  • Approach
  • Landing
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9
Q

Limitations: Emergency Airspeeds (15,000 lbs)

Air Minimum Control Speed (Vmca)

A

Flaps up: 94 Kts

Flaps approach: 93 Kts

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10
Q

Limitations: Pressurization / Environmental

Cabin Differential Pressure Gauge Red Arc

A

6.6 psi to end of scale

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11
Q

Limitations: Fuel

Do not put any fuel into the _____ tanks unless the _____ tanks are full.

A

auxiliary

main

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12
Q

Limitations: Speed

Maximum Flap Extension/Extended Speed (Vfe):

  • Approach: _____
  • Full Down: _____
A

Maximum Flap Extension/Extended Speed (Vfe):

  • Approach: 202 KIAS
  • Full Down: 158 KIAS
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13
Q

Limitations: Electrical

Generator Load Limits:

  • In Flight:
    • Sea Level to 34,000 ft Altitude: _____
    • Above 34,000 ft Altitude: _____
  • Ground Operations:
    • 62-70% N1: _____
    • 70-100% N1: _____
A

Generator Load Limits:

  • In Flight:
    • Sea Level to 34,000 ft Altitude: 100%
    • Above 34,000 ft Altitude: 95%
  • Ground Operations:
    • 62-70% N1: 75%
    • 70-100% N1: 100%
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14
Q

Limitations: General

Passenger Seating Limitations

A

FAR, Part 91 Operations

MAX - 15 passengers

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15
Q

Limitations: Engine and Propeller

The rudder boost must be operational for _____.

A

all phases of flight

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16
Q

Limitations: Aircraft Weights

Max Landing Weight

A
  • 15000 lbs
  • Or as limited by:
    • Max Landing weight to achieve climb requirements
    • Max Landing distance - Flaps Down
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17
Q

Limitations: Speed

Maximum Operating Speed (Vmo)

A

263 KIAS / 0.58 M

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18
Q

Limitations: Engine and Propeller

Engine Max ITT:

  • Starting: _____
  • Idle: _____
  • Takeoff: _____
  • Max Continuous: _____
  • Cruise Climb: _____
  • Max Cruise: _____
  • Max Reverse: _____
  • Transient: _____
A

Engine Max ITT:

  • Starting: 1,000*C for 5 sec
  • Idle: 750*C
  • Takeoff: 820*C
  • Max Continuous: 820*C
  • Cruise Climb: 785*C
  • Max Cruise: 820*C
  • Max Reverse: 760*C
  • Transient: 850*C for 20 sec
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19
Q

Limitations: Fuel

Max Fuel Imbalance

A

300 lbs

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20
Q

Limitations: Engine and Propeller

Engine Torque %:

  • Take off: _____
  • Max Continuous: _____
  • Transient: _____
  • Below 1,000 Propeller RPM (N2): _____
A

Engine Torque %:

  • Take off: 100% (up to 102% for 7 mins)
  • Max Continuous: 100% (up to 102% for 7 mins)
  • Transient: 156% (limited to 20 secs)
  • Below 1,000 Propeller RPM (N2): 62%
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21
Q

Limitations: Pressurization / Environmental

The [CABIN DIFF HI] Annunciator illuminates at _____ PSID.

A

6.9 PSID

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22
Q

Limitations: Engine and Propeller

Engine Oil Temp:

  • Starting: _____
  • Idle: _____
  • Takeoff: _____
  • Max Continuous: _____
  • Cruise Climb: _____
  • Max Cruise: _____
  • Max Reverse: _____
  • Transient: _____
  • Min for Fuel Heat at T/O: _____
A

Engine Oil Temp:

  • Starting: -40*C min
  • Idle: -40 to 110*C
  • Takeoff: 0 to 110*C
  • Max Continuous: 0 to 110*C
  • Cruise Climb: 0 to 110*C
  • Max Cruise: 0 to 110*C
  • Max Reverse: 0 to 99*C
  • Transient: 0 to 110*C
  • Min for Fuel Heat at T/O: 55*C (Recommended)

NOTE: Temperatures between 99C and 110C are limited to a maximum of 10 minutes.

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23
Q

Limitations: Emergency Airspeeds (15,000 lbs)

Maximum Range Glide Speed

A

135 Kts

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24
Q

Limitations: Engine and Propeller

What is the Range of the Primary Governor?

A

1,450 to 1,700 RPM

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25
Q

Limitations: Landing Gear and Brakes

Landing Gear Cycle Limits

A

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

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26
Q

Limitations: Fuel

For Fuel System, do not takeoff if Fuel Quantity Gauges indicate _____ arc or indicate less than _____ lbs in each Wing System.

A

Yellow

265 lbs

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27
Q

Limitations: Autopilot

The autopilot and yaw damper must be used for _____ and _____.

A

takeoff and landing

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28
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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29
Q

Limitations: Autopilot

Do not manually override the autopilot during _____ _____.

A

normal flight

30
Q

Limitations: Pressurization / Environmental

The “CABIN ALTITUDE” Annunciator illuminates when?

A

Cabin altitude is above 10,000 ft

31
Q

Limitations: Pressurization / Environmental

The “CABIN ALTITUDE HI” Annunciator illuminates when?

A

Cabin altitude is above 12,000 ft

32
Q

Limitations: Engine and Propeller

Engine PROP RPM (N2):

  • Idle: _____
  • Takeoff: _____
  • Max Continuous: _____
  • Cruise Climb: _____
  • Max Cruise: _____
  • Max Reverse: _____
  • Transient: _____
A

Engine PROP RPM (N2):

  • Idle: 1,050 min
  • Takeoff: 1,700 (up to 1,735 for 7 mins)
  • Max Continuous: 1,700 (up to 1,735 for 7 mins)
  • Cruise Climb: 1,700 (up to 1,735 for 7 mins)
  • Max Cruise: 1,700 (up to 1,735 for 7 mins)
  • Max Reverse: 1,650
  • Transient: 1,870 for 20 secs
33
Q

Limitations: Pressurization / Environmental

Above what altitude do the oxygen masks automatically deploy?

A

12,500 ft

34
Q

Limitations: Engine and Propeller

Engine Gas Generator (%N1):

  • Idle: _____
  • Takeoff: _____
  • Max Continuous: _____
  • Cruise Climb: _____
  • Max Cruise: _____
  • Transient: _____
A

Engine Gas Generator (%N1):

  • Idle: 62% min
  • Takeoff: 104%
  • Max Continuous: 104%
  • Cruise Climb: 104%
  • Max Cruise: 104%
  • Transient: 104%
35
Q

Limitations: Avionics and Autopilot

When must an autopilot preflight check be conducted?

A

An autopilot preflight check must be conducted and found satisfactory prior to each flight on which the autopilot is to be used.

36
Q

Limitations: Speed

Maximum Demonstrated Crosswind

A

20 Kts

37
Q

Limitations: Fuel

Usable Fuel:

  • Total Usable Fuel Quantity: _____
  • Each Main Fuel Tank System: _____
  • Each Auxiliary Fuel Tank: _____
A

Usable Fuel:

  • Total Usable Fuel Quantity: 539 Gal/3611 lbs
  • Each Main Fuel Tank System: 190 Gal/1273 lbs
  • Each Auxiliary Fuel Tank: 79.5 Gal/533 lbs
38
Q

Limitations: Electrical

Starter Limits

A
  • 30 sec ON / 5 mins OFF
  • 30 sec ON / 5 mins OFF
  • 30 sec ON / 30 mins OFF
39
Q

Limitations: Ice and Rain

Min Airspeed for Sustained Icing Flight

A

140 Kts

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

40
Q

Limitations: Avionics and Autopilot

During _____ operations, a pilot must be seated at the controls with the seat belt and shoulder harness fastened.

A

autopilot

41
Q

Limitations: Engine and Propeller

Engine Oil Pressure:

  • Starting: _____
  • Idle: _____
  • Takeoff: _____
  • Max Continuous: _____
  • Cruise Climb: _____
  • Max Cruise: _____
  • Max Reverse: _____
  • Transient: _____
A

Engine Oil Pressure:

  • Starting: 0 to 200 psi
  • Idle: 60 psi min
  • Takeoff: 90 to 135 psi
  • Max Continuous: 90 to 135 psi
  • Cruise Climb: 90 to 135 psi
  • Max Cruise: 90 to 135 psi
  • Max Reverse: 90 to 135 psi
  • Transient: 200 psi
42
Q

Limitations: General

AHRS 1 and 2 must be _____ for takeoff.

A

operative

43
Q

Limitations: Avionics and Autopilot

The pilot’s PFD and MFD and copilot’s PFD must be installed and operational in the _____ mode for takeoff.

A

normal

44
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 ft AGL
Min Use Height during Cruise: 1000 ft AGL
Min Use Height during Approach: 79 ft AGL
Min Use Height during Steep Approach: 160 ft AGL

45
Q

Limitations: Engine and Propeller

Propeller Type

A
  • Constant speed
  • Full-feathering
  • Reversing
  • Counter-weighted
  • Hydraulically-actuated
46
Q

Limitations: Avionics and Autopilot

The MFD must be _____ prior to engine start.

A

operational

47
Q

Limitations: Engine and Propeller

Why should the power levers not be lifted in-flight?

A

Lifting the power levers in-flight, or moving the power levers below flight idle position in-flight could result in a nose-down pitch and a descent rate that could lead to aircraft damage and injury to personnel.

48
Q

Limitations: Emergency Airspeeds (15,000 lbs)

One Engine Inoperative:

  • Best Angle of Climb (Vxse): _____
  • Best Rate of Climb (Vyse): _____
  • Enroute Climb: _____
A

One Engine Inoperative:

  • Best Angle of Climb (Vxse): 125 Kts
  • Best Rate of Climb (Vyse): 125 Kts
  • Enroute Climb: 125 Kts
49
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)

A

10 hours

50
Q

Limitations: Pressurization / Environmental

Outside Air Temperature Limits:

  • Sea Level to 25,000 ft Pressure Altitude: _____
  • Above 25,000 ft Pressure Altitude: _____
A

Outside Air Temperature Limits:

  • Sea Level to 25,000 ft Pressure Altitude: ISA +37*C
  • Above 25,000 ft Pressure Altitude: ISA +31*C
51
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*

52
Q

Limitations: Pressurization / Environmental

Cabin Differential Pressure Gauge Green Arc

A

0 to 6.6 psi

53
Q

Limitations: Ice and Rain

Minimum Ambient Temperature for Operation of Deicing Boots

A

-40 *C

54
Q

Limitations: Landing Gear and Brakes

Brakes Deice Temp Operating Limit

A

Not above 15*C

55
Q

Limitations: Aircraft Weights

Max Allowable Takeoff Weight

A
  • 15000 lbs
  • Or as limited by:
    • Takeoff climb requirements
    • Tire speed
    • Takeoff field length
56
Q

Limitations: Avionics and Autopilot

The pilot’s and copilot’s Air Data Computers must be _____ for takeoff.

A

operative

57
Q

Limitations: General

Flight Load Factor Limits

Flaps up Flaps Down
____ Positive G ____ Positive G
____ Negative G ____ Negative G

A

Flight Load Factor Limits

             Flaps up                     Flaps Down
        _3.1_ Positive G        _2.0_ Positive G
       _1.24_ Negative G      _0.0_ Negative G
58
Q

Limitations: Speed

Max Demonstrated Wind Component for Coupled Approaches:

  • Crosswind: _____
  • Tailwind: _____
A

Maximum Demonstrated Wind Component for Coupled Approaches:

  • Crosswind: 32 Kts
  • Tailwind: 14 Kts
59
Q

Limitations: Electrical

External Power Amps Limits: _____
External Power Volt Range: _____

A

External Power Amps Limits: 1000 Amps (momentary), 300 Amps (continuously)
External Power Volt Range: 28.0 to 28.4 Volts

60
Q

Limitations: Aircraft Weights

Max Ramp Weight & Max Zero Fuel Weight

A

Max Ramp Weight - 15,100 lbs

Max Zero Fuel Weight - 12,500 lbs

61
Q

Limitations: Speed

Maximum Landing Gear Operating Speed (Vlo):

  • Extension: _____
  • Retraction: _____

Maximum Landing Gear
- Extended Speed (Vle): _____

A

Maximum Landing Gear Operating Speed (Vlo):

  • Extension: 184 KIAS
  • Retraction: 166 KIAS

Maximum Landing Gear
- Extended Speed (Vle): 184 KIAS

62
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

63
Q

Limitations: Engine and Propeller

The Overspeed Governor governs to _____.

A

1,768 RPM

64
Q

Limitations: General Overview

Aft Facing Seats

A

The seat back of each occupied aft-facing seat must be in the upright position and the headrest fully extended for takeoff and landing.

65
Q

Limitations: Speed

Maneuvering Speed (Va)

A

184 Kts

66
Q

Limitations: Electrical

Below _____ volts, battery must be recharged or replaced with a battery indicating at least 20 volts before connecting external power.

A

20 volts

67
Q

Limitations: Autopilot

Operation of the autopilot system with a _____ _____ _____ is prohibited.

A

pitch trim malfunction

68
Q

Limitations: General

Max Operating Altitude

Normal Operation: ______
Yaw Damper System - Inoperative: _____

A

Max Operating Altitude

Normal Operation: 35000ft
Yaw Damper System - Inoperative: 5000ft

NOTE: If dual aft body strakes are installed, refer to STC Supplemental 91-111.

69
Q

Limitations: General

Altitude Limitations

Operation with Aviation Gasoline:
Both Standby Fuel Pumps Operative: ______
Either Standby Fuel Pumps Inoperative: _____
Climb Altitude Limit W/out Crossfeed Capability: _____

A

Altitude Limitations

Operation with Aviation Gasoline:
Both Standby Fuel Pumps Operative: 35000ft
Either Standby Fuel Pumps Inoperative: FLIGHT PROHIBITED
Climb Altitude Limit W/out Crossfeed Capability: 20000FT

70
Q

Limitations: General Overview

Aircraft

  • Height: _____
  • Length: _____
  • Wingspan: _____
A

Aircraft

  • Height: 14’ 4”
  • Length: 46’ 8”
  • Wingspan: 57’ 11”
71
Q

Limitations: Engine and Propeller

Engine Model Number and Type

A

PT6A-60A, turboprop engine

CAE (5 decks)

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