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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
Limitations: Landing Gear and Brakes Landing Gear Cycle Limits
1 cycle (up/down) every 5 mins for a total of 6 cycles, followed by a 15 min cool-down
26
Limitations: Fuel For Fuel System, do not takeoff if Fuel Quantity Gauges indicate _____ arc or indicate less than _____ lbs in each Wing System.
Yellow 265 lbs
27
Limitations: Autopilot The autopilot and yaw damper must be used for _____ and _____.
takeoff and landing
28
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.
+5 *C
29
Limitations: Autopilot Do not manually override the autopilot during _____ _____.
normal flight
30
Limitations: Pressurization / Environmental The "CABIN ALTITUDE" Annunciator illuminates when?
Cabin altitude is above 10,000 ft
31
Limitations: Pressurization / Environmental The "CABIN ALTITUDE HI" Annunciator illuminates when?
Cabin altitude is above 12,000 ft
32
Limitations: Engine and Propeller Engine PROP RPM (N2): - Idle: _____ - Takeoff: _____ - Max Continuous: _____ - Cruise Climb: _____ - Max Cruise: _____ - Max Reverse: _____ - Transient: _____
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
Limitations: Pressurization / Environmental Above what altitude do the oxygen masks automatically deploy?
12,500 ft
34
Limitations: Engine and Propeller Engine Gas Generator (%N1): - Idle: _____ - Takeoff: _____ - Max Continuous: _____ - Cruise Climb: _____ - Max Cruise: _____ - Transient: _____
Engine Gas Generator (%N1): - Idle: _62% min_ - Takeoff: _104%_ - Max Continuous: _104%_ - Cruise Climb: _104%_ - Max Cruise: _104%_ - Transient: _104%_
35
Limitations: Avionics and Autopilot When must an autopilot preflight check be conducted?
An autopilot preflight check must be conducted and found satisfactory prior to each flight on which the autopilot is to be used.
36
Limitations: Speed Maximum Demonstrated Crosswind
20 Kts
37
Limitations: Fuel Usable Fuel: - Total Usable Fuel Quantity: _____ - Each Main Fuel Tank System: _____ - Each Auxiliary Fuel Tank: _____
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
Limitations: Electrical Starter Limits
- 30 sec ON / 5 mins OFF - 30 sec ON / 5 mins OFF - 30 sec ON / 30 mins OFF
39
Limitations: Ice and Rain Min Airspeed for Sustained Icing Flight
140 Kts NOTE: Sustained flight in icing with flaps extended is prohibited except for approach and landing.
40
Limitations: Avionics and Autopilot During _____ operations, a pilot must be seated at the controls with the seat belt and shoulder harness fastened.
autopilot
41
Limitations: Engine and Propeller Engine Oil Pressure: - Starting: _____ - Idle: _____ - Takeoff: _____ - Max Continuous: _____ - Cruise Climb: _____ - Max Cruise: _____ - Max Reverse: _____ - Transient: _____
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
Limitations: General AHRS 1 and 2 must be _____ for takeoff.
operative
43
Limitations: Avionics and Autopilot The pilot's PFD and MFD and copilot's PFD must be installed and operational in the _____ mode for takeoff.
normal
44
Limitations: Autopilot Min Engage Height after Takeoff: _____ Min Use Height during Cruise: _____ Min Use Height during Approach: _____ Min Use Height during Steep Approach: _____
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
Limitations: Engine and Propeller Propeller Type
- Constant speed - Full-feathering - Reversing - Counter-weighted - Hydraulically-actuated
46
Limitations: Avionics and Autopilot The MFD must be _____ prior to engine start.
operational
47
Limitations: Engine and Propeller Why should the power levers not be lifted in-flight?
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
Limitations: Emergency Airspeeds (15,000 lbs) One Engine Inoperative: - Best Angle of Climb (Vxse): _____ - Best Rate of Climb (Vyse): _____ - Enroute Climb: _____
One Engine Inoperative: - Best Angle of Climb (Vxse): _125 Kts_ - Best Rate of Climb (Vyse): _125 Kts_ - Enroute Climb: _125 Kts_
49
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)
10 hours
50
Limitations: Pressurization / Environmental Outside Air Temperature Limits: - Sea Level to 25,000 ft Pressure Altitude: _____ - Above 25,000 ft Pressure Altitude: _____
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
Limitations: Avionics and Autopilot Autopilot Max Coupled INCPT Angle for Back Course: _____ Autopilot Max Coupled INCPT Angle for NAV/LOC: _____
Autopilot Max Coupled INCPT Angle for Back Course: _70*_ | Autopilot Max Coupled INCPT Angle for NAV/LOC: _< 90*_
52
Limitations: Pressurization / Environmental Cabin Differential Pressure Gauge Green Arc
0 to 6.6 psi
53
Limitations: Ice and Rain Minimum Ambient Temperature for Operation of Deicing Boots
-40 *C
54
Limitations: Landing Gear and Brakes Brakes Deice Temp Operating Limit
Not above 15*C
55
Limitations: Aircraft Weights Max Allowable Takeoff Weight
- 15000 lbs - Or as limited by: - Takeoff climb requirements - Tire speed - Takeoff field length
56
Limitations: Avionics and Autopilot The pilot's and copilot's Air Data Computers must be _____ for takeoff.
operative
57
Limitations: General Flight Load Factor Limits Flaps up Flaps Down ____ Positive G ____ Positive G ____ Negative G ____ Negative G
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
Limitations: Speed Max Demonstrated Wind Component for Coupled Approaches: - Crosswind: _____ - Tailwind: _____
Maximum Demonstrated Wind Component for Coupled Approaches: - Crosswind: _32 Kts_ - Tailwind: _14 Kts_
59
Limitations: Electrical External Power Amps Limits: _____ External Power Volt Range: _____
External Power Amps Limits: _1000 Amps (momentary), 300 Amps (continuously)_ External Power Volt Range: _28.0 to 28.4 Volts_
60
Limitations: Aircraft Weights Max Ramp Weight & Max Zero Fuel Weight
Max Ramp Weight - 15,100 lbs Max Zero Fuel Weight - 12,500 lbs
61
Limitations: Speed Maximum Landing Gear Operating Speed (Vlo): - Extension: _____ - Retraction: _____ Maximum Landing Gear - Extended Speed (Vle): _____
Maximum Landing Gear Operating Speed (Vlo): - Extension: _184 KIAS_ - Retraction: _166 KIAS_ Maximum Landing Gear - Extended Speed (Vle): _184 KIAS_
62
Limitations: Ice and Rain The left and right Engine Anti-Ice shall be OFF for takeoff operations in ambient temperatures above _____ *C.
10 *C
63
Limitations: Engine and Propeller The Overspeed Governor governs to _____.
1,768 RPM
64
Limitations: General Overview Aft Facing Seats
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
Limitations: Speed Maneuvering Speed (Va)
184 Kts
66
Limitations: Electrical Below _____ volts, battery must be recharged or replaced with a battery indicating at least 20 volts before connecting external power.
20 volts
67
Limitations: Autopilot Operation of the autopilot system with a _____ _____ _____ is prohibited.
pitch trim malfunction
68
Limitations: General Max Operating Altitude Normal Operation: ______ Yaw Damper System - Inoperative: _____
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
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: _____
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
Limitations: General Overview Aircraft - Height: _____ - Length: _____ - Wingspan: _____
Aircraft - Height: _14' 4"_ - Length: _46' 8"_ - Wingspan: _57' 11"_
71
Limitations: Engine and Propeller Engine Model Number and Type
PT6A-60A, turboprop engine

CAE (5 decks)

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