Term
Acceleration Limitations: |
|
Definition
+4.5g up to 280KIAS; -2.3g up to 220KIAS; decreasing to -1.0g at 280KIAS |
|
|
Term
Acceleration Limitations: During extension of the landing gear, |
|
Definition
|
|
Term
Acceleration Limitations: With flaps down, |
|
Definition
|
|
Term
Aerobatic Flight Limits: Max time inverted |
|
Definition
|
|
Term
Aerobatic Flight Limits: Max time vertical (nose down) |
|
Definition
|
|
Term
Aerobatic Flight Limits: Max time vertical (nose up) |
|
Definition
|
|
Term
Aerobatic Flight Limits: Max time wings vertical (knife edge) |
|
Definition
|
|
Term
Aerobatic Flight Limits: “Zero G” condition |
|
Definition
|
|
Term
Aerodynamic Limitations: Canopy Emergency Open: |
|
Definition
|
|
Term
Aerodynamic Limitations: Canopy Open: |
|
Definition
|
|
Term
Aerodynamic Limitations: Ceiling: |
|
Definition
|
|
Term
Aerodynamic Limitations: Clean, smooth, 20k-25k ft: |
|
Definition
|
|
Term
Aerodynamic Limitations: Clean, smooth, below 20,000 ft: |
|
Definition
|
|
Term
Aerodynamic Limitations: Flaps Down/Up and Gear retraction: |
|
Definition
|
|
Term
Aerodynamic Limitations: Gear Down: |
|
Definition
|
|
Term
Aerodynamic Limitations: Turbulent Air: |
|
Definition
|
|
Term
Crosswind Limits: Full Flap |
|
Definition
|
|
Term
Crosswind Limits: No Flap |
|
Definition
|
|
Term
|
Definition
10 Knots and 25 Knot Headwind |
|
|
Term
Dimensions: Height (at rest) / tread |
|
Definition
|
|
Term
|
Definition
|
|
Term
Dimensions: Prop clearance |
|
Definition
|
|
Term
Dimensions: Prop diameter |
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
PT6A-25, inverted flt capabilities, 550 shp max (1315), 425 shp norm ops (1015) |
|
|
Term
Engine Fail Ind - Comp Stall: TQ - N1 - ITT - Prop RPM - Fuel Flow - Oil Temp & Press |
|
Definition
TQ - Fluct N1 - Fluct (possible flameout or overspeed) ITT - Fluct (possible flameout or overspeed) Prop RPM - Minor surges Fuel Flow - Fluct Oil Temp - Norm Oil Press - Norm |
|
|
Term
Engine Fail Ind - Flameout: TQ - N1 - ITT - Prop RPM - Fuel Flow - Oil Temp & Press |
|
Definition
TQ - Zero N1 - 10-12% ITT -Decr towards 200⁰C Prop RPM - Airspeed Dependent (below 110 KIAS RPM will eventually decr to approx 200 RPM) Fuel Flow - Lass than 50 Lbs/hr Oil Temp - Decr Oil Press - Various (Windmilling eng may maintain oil press above 10 psi) |
|
|
Term
Engine Fail Ind - Rollback: TQ - N1 - ITT - Prop RPM - Fuel Flow - Oil Temp & Press |
|
Definition
TQ - Low N1 - 40 - 60% ITT --- Prop RPM - Airspeed Dependent (decarying below 2200) Fuel Flow - Approx 80 to 100 Lbs/hr Oil Temp - Norm Oil Press - Norm |
|
|
Term
Fuel/Fuel Flow: Critical Fuel (for flight) |
|
Definition
|
|
Term
|
Definition
|
|
Term
Fuel/Fuel Flow: No takeoff range |
|
Definition
|
|
Term
Fuel/Fuel Flow: Normal operation |
|
Definition
|
|
Term
Glide Performance - Gear down, Flaps down, Prop F |
|
Definition
Vbest glide - 88 KIAS Sink Rate @ 100 KIAS (FPM) - 1650 Glide Ratio @ 100 KIAS - 6 to 1 |
|
|
Term
Glide Performance - Gear down, Flaps up, Prop F |
|
Definition
Vbest glide - 87 KIAS Sink Rate @ 100 KIAS (FPM) - 1200 Glide Ratio @ 100 KIAS - 8 to 1 |
|
|
Term
Glide Performance - Gear up, Flaps down, Prop F |
|
Definition
Vbest glide - 93 KIAS Sink Rate @ 100 KIAS (FPM) - 1250 Glide Ratio @ 100 KIAS - 8 to 1 |
|
|
Term
Glide Performance - Gear up, Flaps up, Prop F |
|
Definition
Vbest glide - 100 KIAS Sink Rate @ 100 KIAS (FPM) - 800 Glide Ratio @ 100 KIAS - 12 to 1 |
|
|
Term
Glide Performance - Gear up, Flaps up, Prop UF |
|
Definition
Vbest glide - 117 KIAS Sink Rate @ 100 KIAS (FPM) - 2400 Glide Ratio @ 100 KIAS - 3 to 1 |
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
ITT Normal operating range |
|
Definition
|
|
Term
Landing: Max sink rate at ground contact |
|
Definition
|
|
Term
|
Definition
|
|
Term
N1: FCU stuck @ min. flow (rollback) |
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
N1: Minimum for flight (single flight) |
|
Definition
|
|
Term
N1: Normal operating range |
|
Definition
|
|
Term
N1: Note: For ever 10°C below -30°C ambient temperature, reduce maximum allowable N1 by ________ |
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
Oil Temperature: Min starting temperature |
|
Definition
|
|
Term
Oil Temperature: Normal Operating range |
|
Definition
|
|
Term
Oil pressure: Idle operating range |
|
Definition
|
|
Term
Oil pressure: Max oil pressure |
|
Definition
|
|
Term
Oil pressure: Maximum fluctuation |
|
Definition
|
|
Term
Oil pressure: Normal operating range (N1 above 75%) |
|
Definition
|
|
Term
|
Definition
Night Formation Flight Inverted flight above 220 KIAS Inverted Stalls Inverted Spins Spins with propeller feathered Spins with gear and/or flaps extended |
|
|
Term
Prop RPM Fuel topping governor |
|
Definition
|
|
Term
Prop RPM Idle operating range |
|
Definition
|
|
Term
Prop RPM Normal operating range |
|
Definition
|
|
Term
Prop RPM Overspeed governor |
|
Definition
|
|
Term
|
Definition
40s/60s/40s/60s/40s/30min |
|
|
Term
Torque: Auto ignition range |
|
Definition
|
|
Term
Torque: Idle operating range |
|
Definition
|
|
Term
|
Definition
|
|
Term
Torque: Max torque (oil malfunction) |
|
Definition
|
|
Term
|
Definition
|
|
Term
Torque: Normal operating range |
|
Definition
|
|
Term
Torque: Prop overspeed test range |
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
Weights: Touch-and-go/Aerobatic |
|
Definition
|
|