MC-12 Critical Action Procedures v5 and Ops Limits v3

ENGINE FIRE ON GROUND

EMERGENCY ENGINE SHUTDOWN ON GROUND

TAKEOFF ABORT

ENGINE FAILURE TAKEOFF CONTINUED

ENGINE FIRE / FAILURE IN FLIGHT

ENVIRONMENTAL SMOKE / FUMES

Maneuvering Speed (V_A) Non-ER

Maneuvering Speed (V_A) ER

Max Flap Extension/Extended (V_FE) Approach Non-ER

Max Flap Extension/Extended (V_FE) Approach ER

Max Flap Extension/Extended (V_FE) Full Down Non-ER

Max Flap Extension/Extended (V_FE) Full Down ER

Max Landing Gear Operating Speed (V_LO) Extension Non-ER

Max Landing Gear Operating Speed (V_LO) Extension ER

Max Landing Gear Operating Speed (V_LO) Retraction Non-ER

Max Landing Gear Operating Speed (V_LO) Retraction ER

Air Min Control Speed (V_MCA) Flaps Up Non-ER

Air Min Control Speed (V_MCA) Flaps Up ER

Air Min Control Speed (V_MCA) Flaps Down Non-ER

Air Min Control Speed (V_MCA) Flaps Down ER

Max Operating Speed (V_MO) To 21,000’ Non-ER

Max Operating Speed (V_MO) To 24,000’ ER

Max Operating Speed (V_MO) Above 21,000’ Non-ER

Max Operating Speed (V_MO) Above 24,000’ ER

Two Engine Best Rate of Climb (V_Y) Non-ER

Two Engine Best Rate of Climb (V_Y) ER

Turbulent Air Penetration Non-ER

Turbulent Air Penetration ER

Max Airspeed for Effective Windshield Anti-icing Non-ER

Max Airspeed for Effective Windshield Anti-icing ER

Min Airspeed for Sustained Flight in Icing Non-ER

Min Airspeed for Sustained Flight in Icing ER

Intentional One-Engine Inop Speed (V_SSE) Non-ER

Intentional One-Engine Inop Speed (V_SSE) ER

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

One-Engine Inop Best Angle of Climb (V_XSE) ER

One-Engine Inop Best Rate of Climb (V_YSE, Blue Line) Non-ER

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

Emergency Descent Non-ER

Emergency Descent ER

Max Range Glide Non-ER

Max Range Glide ER

Max Ramp Weight Non-ER

Max Ramp Weight ER

Max TO Weight Non-ER

Max TO Weight ER

Max Landing Weight Non-ER

Max Landing Weight ER

Usable Fuel Non ER

Usable Fuel ER

Planned Recovery Fuel

Minimum Fuel

Emergency Fuel

Min TO Fuel (per side)

Max Wind (any direction)

Max Wind with RCR 12 and above

Max Tailwind Component

Max Cabin Diff

CABIN DIFF HI

CABIN ALTITUDE HI

Max Starting ITT

Max Idle ITT

Max TO, Cont, Cruise ITT

Max Cruise Climb ITT

Max Transient ITT

Max Throttle Push ITT

Max TO, Cont, Cruise Torque

Max Cruise Climb Torque

Max Transient Torque

Max Throttle Push Torque

Min Idle N₁%

Max N₁% for TO, Cont, Cruise, Cruise Climb, Transient, and Throttle Push

Min Idle N₂

Max TO, Cont, Cruise N₂

Max Cruise Climb N₂

Max Transient N₂

Max Throttle Push N₂

Oil Press Starting Limits

Min Idle Oil Press

TO, Max Cont, Cruise Oil Press Limits

Cruise Climb Oil Press Limits

Max Transient Oil Press

Throttle Push Oil Press Limits

Min Starting Oil Temp

Idle Oil Temp Limits

TO, Cont, Cruise, Cruise Climb, Transient, and Throttle Push Oil Temp Limits

Inadvertent torque excursions up to     are time limited to   min.

Sustained prop overspeeds faster than ____ RPM indicate failure of the primary governor. Flight may be continued at propeller overspeeds up to ____ RPM, provided torque is limited to ____. Sustained propeller overspeeds faster than ____ RPM indicate failure of both the primary governor and the secondary governor and such overspeeds are not approved. Inadvertent propeller excursions up to ____ RPM are time limited to ___ min.

Oil pressures under___ psi are undesirable. Under emergency conditions, to complete a flight, a lower oil pressure limit of ___ psi is permissible at a reduced power level not to exceed ___ torque. Oil pressures below  psi are unsafe and require that either the engine be shut down or a landing be made at the nearest suitable airport, using the minimum power required to sustain flight. Fluctuations of ___ psi are acceptable.

Starter is limited to ____. ON, ____. OFF, ____. ON, ____. OFF, ____. ON, then ____ OFF.

Load Factor Limits Flaps Up Non-ER

Load Factor Limits Flaps Down Non-ER

Load Factor Limits Flaps Up ER

Load Factor Limits Flaps Down ER

Min Battery Volts for start

Min Battery Volts to use ext power

External Power Cart Voltage Limits

Max Cart Amps - Sustained / Momentary

Landing gear cycles (1 up - 1 down) limited to ____ every ___ min. for ____ cycles followed by a ____ min. cool down.

Rudder boost must be ____ for ____ .

Autofeather must be operable for ____ , and must be armed during __,__,__,and ___.

Engine Anti-ice must be __ for operation in ambient temperatures of __ °C or below when flight free of _______ cannot be assured.

Engine Anti-ice must be OFF for takeoff operations when ambient temperature exceeds ___.

The order in which the fuel tanks must be filled is____ , ____ , then _____.

Sustained flight in icing conditions with flaps extended is prohibited except for ____ and ____.