1 Dash 1 Flashcards
Vmcg
Minimum airspeed at which the airplane may lose an outboard engine during the take-off ground run and still maintain directional control.
- # 1 engine inoperative with the propeller windmilling on NTS.
- Max power on all operating engines.
- Zero bleed (good also for normal bleed)
- Flaps 50% w/ 3000 PSI rudder boost.
- Max available rudder deflection limited by 180lbs pedal force or max rudder surface deflection, whichever occurs 1st.
- max deviation from runway center line of 30’.
- maintain wings level.
Vmca1 IN or OUT
The minimum speed at which directional or lateral control can be maintained for a given airplane configuration.
- # 1 engine inoperative with the propeller windmilling on NTS.
- Max power on all operating engines.
- Zero bleed (good also for normal bleed)
- Flaps 50%
- Max available rudder deflection limited by 180lbs of rudder pedal force or maximum rudder surface deflection, whichever occurs first.
- 5 degrees of bank angle (away from the inoperative engine).
- Landing gear down.
Vmca2
Minimum speed at which directional or lateral control can be maintained for a given airplane configuration.
- All bleed off.
- Max power on both operating engines.
- # 2 engine inoperative with propeller feathered.
- # 1 engine inoperative with the propeller windmilling on NTS.
- Utility hydraulic system inoperative.
- Max available rudder deflection limited by 180 lbs pedal force or maximum rudder surface deflection, whichever occurs first.
- Five degrees of bank angle (away from the inoperative engines).
- Landing gear down.
- Flaps 50% (3000 PSI rudder boost from the booster hydraulic system only).
Vr
Maximum speed to which the airplane can accelerate with engines at takeoff power and then stop within the remainder of the runway available, with 2 engines (symmetrical power) in reverse, one engine in ground idle, one propeller wind-milling, and max anti-skid braking.
Vrot
5 kts less than the greater of Vmca1 IN and Vto.
Normal OBS Clear
1.2 x power-off stall
Best initial short-term climb speed (best angle) based on initiating “gear up” in 3 seconds and initiating “feather” in 6 seconds after lift-off.
Normal 3 ENG CLIMB
Best long-term climb (best rate).
Vto
1.1 x power-off stall
When must you compute back of TOLD card? (CFL and Landing Distance)
30 deg OAT or more
130K lbs or more
6000’ RA or less
RCR 12 or less
RCR
Runway Condition Reading is a value that relates the average braking effectiveness of the particular runway surface to the braking capability of the airplane.
2-No brakes
5-Icy-poor/bill braking
12-wet-medium braking
20-wet, grooved rwy w/ standing water (no glare)
23-dry-good braking
When is new TOLD data required?
- 5K lb or more gross weight change.
- 1K’ or more pressure altitude change.
- 5 deg or more OAT change.
When is accel check time required?
When Vr less than Vto
When is CO’s permission required for a tactical takeoff?
When Vr less than Vrot
Normal takeoff configuration?
- All engines operating at takeoff power.
- Normal bleed
- 50% flaps
What parameters does takeoff factor consider?
- Torque
- Field Pressure Altitude
- Runway Temperature
- TIT
- Engine Efficiency
What speeds are increased by the full GUST increment, not to exceed 10 knots?
Rotation speed Takeoff speed Approach speed Threshold speed Touchdown speed
CFL
The greater of the total runway distances required to accelerate on all engines, experience an engine failure, and then to either continue the takeoff or stop.
Balanced CFL
Distance to accelerate to Vcef, lose an engine, then stop or go. The distance required to continue the takeoff is equal to the distance required to stop.
Unbalanced CFL
Distance to accelerate to the lesser of Vrot or Vmcg, lose an engine, then stop or go. The distance required to stop the aircraft is greater than the distance required to continue the takeoff.
Vcef
Based on critical field length. For balanced CFL it is that speed to which the airplane can accelerate, lose an engine, and then either continue the takeoff with the remaining engines or stop in the same total runway distance. When unbalanced CFL is established by Vmcg the critical engine failure speed will be the lower of the rotation speed or Vmcg.
What is climb out factor based on?
Takeoff factor and airplane gross weight. It represents a sea level, standard day equivalent gross weight.
Min flap retraction speed for normal takeoff? Normal flap retraction speed for normal takeoff?
Obstacle Clearance Speed.
Takeoff Speed + 20 kts
Min flap retraction speed for a max effort takeoff?
Max Effort Obstacle clearance speed + 10 kts.
Take off distance?
Total distance required to accelerate to takeoff speed, lift off, and climb to a 50’ height. It is further defined as the takeoff ground run (distance from brake release to liftoff point) plus the distance from the liftoff point to the 50’ obstacle.
