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: ____

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%_

Limitations: General Max Operating Altitude - Normal Operation: ____ - Yaw Damper System - Inoperative - Single strake: ____ - Dual strake: ____

Max Operating Altitude - Normal Operation: _35000'_ - Yaw Damper System - Inoperative - Single strake: _5000'_ - Dual strake: _19000'_ (STSC Supplemental 91-111)

Limitations: General Altitude Limitations Operation with AvGas: - Both Standby Fuel Pumps Operative: ____ - Either Standby Fuel Pumps Inoperative: ____ - Climb Altitude Limitation Without Crossfeed Capability: ____

Operation with AvGas: - Both Standby Fuel Pumps Operative: _35000'_ - Either Standby Fuel Pumps Inoperative: _Flight Prohibited_ - Climb Altitude Limitation Without Crossfeed Capability: _20000'_

KA350 Limitations Flashcards by Jerry Leger

Limitations: Airspeed Limits (KIAS)

Maneuvering speed (Va) (ER/Non ER)

182 kts / 184 kts)

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Limitations: Engine Limits

Engine Prop - N2: (RPM)

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

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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Limitations: Pressurization/Environmental

The “CABIN DIFF HI” Annunciator illuminates at:

6.9 PSID

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Limitations: Aircraft Weights

Max Weight in Baggage Compartment

550 lbs

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Limitations: Airspeed Limits (KIAS)

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

135 kts / 125 kts

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Limitations: Airspeed Limits (KIAS)

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

ER
Non ER

ER - 135 kts

Non ER - 125 kts

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Limitations: Ice and Rain

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

10*C

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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

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Limitations: Airspeed Limits (KIAS)

Max Operating Speed (Vmo)

ER / Non ER
To: FL240 / FL210

Above: FL240 / FL210

Max Operating Speed (Vmo)

To: FL240 - 245 kts / FL210 - 263 kts

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

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Limitations: Pressurization (psi)

Max Cabin Differential

6.6 psi

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Limitations: Weight (lbs)

Max Landing Weight (ER/NonER)

15,675 lbs / 15,000 lbs

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Limitations: Fuel (lbs)

Usable Fuel (ER/Non ER)

5192 lbs / 3611 lbs

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Limitations: Pressurization/Environmental

The “CABIN ALTITUDE” Annunciator illuminates when:

Cabin altitude above 10,000’

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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: ____

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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Limitations: Weight (lbs)

Max T/O Weight

ER
Non ER

ER - 16,500 lbs

Non ER - 15000 lbs

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Limitations: Electrical (VDC)

Min Battery to Connect External Power:

20 VDC

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Limitations: Airspeed Limits (KIAS)

Intentional One-Engine Inoperative Speed (Vsse)

ER
Non ER

ER - 135 kts

Non ER - 110 kts

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Limitations: General

Max Operating Altitude

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

Max Operating Altitude

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

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Limitations: Airspeed Limits (KIAS)

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

Flaps Down:

Air Minimum Controlable Speed (Vmca)

Flaps Up: 101 kts / 94 kts

Flaps Down: 98 kts / 93 kts

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Limitations: General

Altitude Limitations

Operation with AvGas:

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

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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Limitations: Winds (kts)

Max X-WindT/O

25 kts

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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’

Min Use Height during Cruise: 1000’

Min Use Height during Approach: 79’

Min Use Height during Steep Approach: 160’

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Limitations: Airspeed Limits (KIAS)

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

135 kts / 140 kts

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Limitations: Engine Limits

Torque: (%)

T/O:
Max Cont:
Transient:

Propeller (N2) below 1000 RPM:

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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Limitations: Winds (kts) Max Tailwind Component

10 kts

Limitations: Pressurization/Environmental Cabin Differential Pressure Gauge RED Arc

6.6 to end of scale

Limitations: Engine and Propeller Propeller Type

- Constant speed - Reversing - Counter weighted - Hydraulically actuated - Full feathering

Limitations: Airspeed Limits (KIAS) Min Airspeed for Sustained Flight in Icing

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

Limitations: Ice and Rain Minimum Ambient Temperature for Operation of Deicing Boots

-40*C

Limitations: Ice and Rain Prop Deice Ammeter Normal Operating Range

26 to 32 Amps

Limitations: Fuel (lbs) Min T/O Fuel (per side)

265 lbs

Limitations: Weight (lbs) Max Ramp Weight (ER/Non ER)

16,600 lbs / 15,100 lbs

Limitations: Airspeed Limits (KIAS) Max Flap Extension/Extended (Vfe) Approach: Full Down:

Max Flap Extension/Extended (Vfe) Approach: 202 kts Full Down: 158 kts

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: ```

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 99*C and 110*C are limited to 10 mins

Limitations: Landing Gear Cycle Limit:

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

Limitations: Pressurization (psi) [CABIN DIFF HI]

6.9 +/-0.3 psi

Limitations: Load Factor (Gs) Flaps up: Neg ____ Pos ____ (Non ER) Flaps Down: Neg ____ Pos ____ (Non ER)

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)

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.

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.

Limitations: Airspeed Limits (KIAS) Max Range Glide

135 kts

Limitations: Airspeed Limits (KIAS) Turbulent Air Penetration

170 kts

Limitations: Fuel (lbs) Minimum Landing

600 lbs

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

Limitations: Landing Gear and Brakes Brake Deice Temp Operation Limit

Not above 15*C

Limitations: Engine and Propeller Engine Model Number and Type

PT6A-60A turboprop engine

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*_

Limitations: Pressurization (ft) [CABIN ALTITUDE HI]

12,000 ft

Limitations: Electrical (VDC) Min Battery for Battery Start:

23 VDC

Limitations: Electrical (VDC) External Power Voltage Range:

28 - 28.4 VDC

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.

135 psi, 200 psi

Limitations: Winds (kts) Max Wind (any direction)

50 kts

Limitations: Pressurization/Environmental The "CABIN ALTITUDE HI" Annunciator illuminates when:

Cabin altitude above 12,000'

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.

60 psi

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

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

Limitations: Electrical Starter Limits

- 30 secs ON / 5 mins OFF - 30 secs ON / 5 mins OFF - 30 secs ON / 30 mins OFF

Limitations: Electrical (Amps) External Power Amps Limit:

1000 Amps Momentarily 300 Amp Continuous

Limitations: Electrical Generator Load DC % Loadmeters - Both must be < or =: ____

50%

Limitations: Pressurization/Environmental Cabin Differential Pressure Gauge GREEN Arc

0 to 6.6 psi

Limitations: Fuel (lbs) ER/Non ER ER: Aux: Main:

ER: 1581 lbs / 0 lbs Aux: 1065 lbs / 1065 lbs Main: 2546 lbs / 2546 lbs

Limitations: Engine and Propeller What is the Range of the Primary Governor?

1450 to 1700 RPM

Limitations: Engine Limits Max ITT: (*C) ``` Starting: Idle: T/O: Max Cont: Cruise Climb: Max Cruise: Max Reverse: Transient: ```

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.

Limitations: Fuel (lbs) Max Imbalance

300 lbs

Limitations: Engine Limits Gas Generator - N1: (%) ``` Idle: T/O: Max Cont: Cruise Climb: Max Cruise: Transient: ```

Gas Generator - N1: (%) ``` Idle: 62% min T/O: 104% Max Cont: 104% Cruise Climb: 104% Max Cruise: 104% Transient: 104% ```

Limitations: Pressurization/Environmental Above what altitude do the oxygen masks automatically deploy?

12,500'

Limitations: Airspeed Limits (KIAS) Emergency Descent (ER/Non ER)

182 kts / 184 kts

Limitations: Engine Limits Oil Pressure: (psi) ``` Starting: Idle: T/O: Max Cont: Cruise Climb: Max Cruise: Max Reverse: Transient: ```

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.

Limitations: Fuel Fuel Crossfeed is permitted only when ____

one engine is inoperative.

Limitations: Flight Controls ____ must be operational for all phases of flight.

Rudder Boost

Limitations: Airspeed Limits (KIAS) Max Airspeed for Effective Windshield Anti-icing (Vmo)

226 kts

Limitations: Engine Limits Oil Pressure: (psi) Fluctuations of +/- ____ psi are acceptable.

+/- 10 psi

Limitations: Airspeed Limits (KIAS) Max Landing Gear Operating Speed (Vlo) Extension: ER/Non ER Retraction: ER/Non ER

Max Landing Gear Operating Speed (Vlo) Extension: 182/184 kts Retraction: 164/166 kts

Limitations: Engine and Propeller The Overspeed Governor governs to ____.

1768 RPM

Limitations: Engine and Propeller Propeller Autofeather must be armed for:

- Takeoff - Climb - Approach - Landing