KA350 Limitations Flashcards
Limitations: General
Minimum Crew
One pilot
Limitations: Fuel
Fuel Crossfeed is permitted only when _____.
one engine is inoperative
Limitations: Ice and Rain
Prop Deice Ammeter Normal Operating Range
26 to 32 Amps
Limitations: Electrical
Min Battery Volts for Battery Start
23 VDC
Limitations: Avionics and Autopilot
Operating in the composite mode is limited to _____ and _____ _____ conditions.
training
display failure
Limitations: Aircraft Weights
Max Weight in Baggage Compartment
Max Weight in Baggage Compartment - 550 lbs (250 kg)
Limitations: Emergency Airspeeds (15,000 lbs)
Emergency Descent Speed
184 Kts
Limitations: Engine and Propeller
Propeller Autofeather must be armed for _____.
- Take off
- Climb
- Approach
- Landing
Limitations: Emergency Airspeeds (15,000 lbs)
Air Minimum Control Speed (Vmca)
Flaps up: 94 Kts
Flaps approach: 93 Kts
Limitations: Pressurization / Environmental
Cabin Differential Pressure Gauge Red Arc
6.6 psi to end of scale
Limitations: Fuel
Do not put any fuel into the _____ tanks unless the _____ tanks are full.
auxiliary
main
Limitations: Speed
Maximum Flap Extension/Extended Speed (Vfe):
- Approach: _____
- Full Down: _____
Maximum Flap Extension/Extended Speed (Vfe):
- Approach: 202 KIAS
- Full Down: 158 KIAS
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: _____
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%
Limitations: General
Passenger Seating Limitations
FAR, Part 91 Operations
MAX - 15 passengers
Limitations: Engine and Propeller
The rudder boost must be operational for _____.
all phases of flight
Limitations: Aircraft Weights
Max Landing Weight
- 15000 lbs
- Or as limited by:
- Max Landing weight to achieve climb requirements
- Max Landing distance - Flaps Down
Limitations: Speed
Maximum Operating Speed (Vmo)
263 KIAS / 0.58 M
Limitations: Engine and Propeller
Engine Max ITT:
- Starting: _____
- Idle: _____
- Takeoff: _____
- Max Continuous: _____
- Cruise Climb: _____
- Max Cruise: _____
- Max Reverse: _____
- Transient: _____
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
Limitations: Fuel
Max Fuel Imbalance
300 lbs
Limitations: Engine and Propeller
Engine Torque %:
- Take off: _____
- Max Continuous: _____
- Transient: _____
- Below 1,000 Propeller RPM (N2): _____
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%
Limitations: Pressurization / Environmental
The [CABIN DIFF HI] Annunciator illuminates at _____ PSID.
6.9 PSID
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: _____
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.
Limitations: Emergency Airspeeds (15,000 lbs)
Maximum Range Glide Speed
135 Kts
Limitations: Engine and Propeller
What is the Range of the Primary Governor?
1,450 to 1,700 RPM
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
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
Limitations: Autopilot
The autopilot and yaw damper must be used for _____ and _____.
takeoff and landing
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
Limitations: Autopilot
Do not manually override the autopilot during _____ _____.
normal flight
Limitations: Pressurization / Environmental
The “CABIN ALTITUDE” Annunciator illuminates when?
Cabin altitude is above 10,000 ft
Limitations: Pressurization / Environmental
The “CABIN ALTITUDE HI” Annunciator illuminates when?
Cabin altitude is above 12,000 ft
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
Limitations: Pressurization / Environmental
Above what altitude do the oxygen masks automatically deploy?
12,500 ft
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%
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.
Limitations: Speed
Maximum Demonstrated Crosswind
20 Kts
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
Limitations: Electrical
Starter Limits
- 30 sec ON / 5 mins OFF
- 30 sec ON / 5 mins OFF
- 30 sec ON / 30 mins OFF
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.
Limitations: Avionics and Autopilot
During _____ operations, a pilot must be seated at the controls with the seat belt and shoulder harness fastened.
autopilot
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
Limitations: General
AHRS 1 and 2 must be _____ for takeoff.
operative
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
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
Limitations: Engine and Propeller
Propeller Type
- Constant speed
- Full-feathering
- Reversing
- Counter-weighted
- Hydraulically-actuated
Limitations: Avionics and Autopilot
The MFD must be _____ prior to engine start.
operational
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.
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
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: 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
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 / Environmental
Cabin Differential Pressure Gauge Green Arc
0 to 6.6 psi
Limitations: Ice and Rain
Minimum Ambient Temperature for Operation of Deicing Boots
-40 *C
Limitations: Landing Gear and Brakes
Brakes Deice Temp Operating Limit
Not above 15*C
Limitations: Aircraft Weights
Max Allowable Takeoff Weight
- 15000 lbs
- Or as limited by:
- Takeoff climb requirements
- Tire speed
- Takeoff field length
Limitations: Avionics and Autopilot
The pilot’s and copilot’s Air Data Computers must be _____ for takeoff.
operative
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
Limitations: Speed
Max Demonstrated Wind Component for Coupled Approaches:
- Crosswind: _____
- Tailwind: _____
Maximum Demonstrated Wind Component for Coupled Approaches:
- Crosswind: 32 Kts
- Tailwind: 14 Kts
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
Limitations: Aircraft Weights
Max Ramp Weight & Max Zero Fuel Weight
Max Ramp Weight - 15,100 lbs
Max Zero Fuel Weight - 12,500 lbs
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
Limitations: Ice and Rain
The left and right Engine Anti-Ice shall be OFF for takeoff operations in ambient temperatures above _____ *C.
10 *C
Limitations: Engine and Propeller
The Overspeed Governor governs to _____.
1,768 RPM
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.
Limitations: Speed
Maneuvering Speed (Va)
184 Kts
Limitations: Electrical
Below _____ volts, battery must be recharged or replaced with a battery indicating at least 20 volts before connecting external power.
20 volts
Limitations: Autopilot
Operation of the autopilot system with a _____ _____ _____ is prohibited.
pitch trim malfunction
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.
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
Limitations: General Overview
Aircraft
- Height: _____
- Length: _____
- Wingspan: _____
Aircraft
- Height: 14’ 4”
- Length: 46’ 8”
- Wingspan: 57’ 11”
Limitations: Engine and Propeller
Engine Model Number and Type
PT6A-60A, turboprop engine
