CFPH
問題一覧
1
To protect the engine and tramsmission
2
To prevent coning and overpitching
3
To protect the structural limitations of the blades and the rotor hub
4
To retain inertia available, so we can glide instead of fall in the event of an engine failure.
5
To avoid retreating blade stall or compressibility. Also to protect the structural components of the aircraft.
6
To prevent the horizontal stabiliser from exerting an excessive upward force on the tail boom.
7
For aircraft controllability. There will be more parasite drag with sideways travel, no stabilizers, increased risk of dynamic rollover (if low)
8
For aircraft controllability. Also cannot see behind you. AIrcraft is not aerodynamically shaped to travel backwards. Risk of CO2 entering the cockpit.
9
To achieve successful take-off. Excess weight reduces performance.
10
To prevent structural damage. And limit the reduction in performance due to increased weight.
11
To prevent adverse handling characteristics. At weights below minimum, the ROD in autorotation may not be sufficient to maintain a safe rotor RPM.
12
To prevent structural damage and maintain controllability of the aircraft
CNAV
CNAV
Jonny Preece · 46問 · 2年前CNAV
CNAV
46問 • 2年前CADH
CADH
Jonny Preece · 106問 · 2年前CADH
CADH
106問 • 2年前CMET
CMET
Jonny Preece · 21問 · 2年前CMET
CMET
21問 • 2年前CHUF - Chapter 1 - The Human Condition
CHUF - Chapter 1 - The Human Condition
Jonny Preece · 37問 · 2年前CHUF - Chapter 1 - The Human Condition
CHUF - Chapter 1 - The Human Condition
37問 • 2年前CHUF - Chapter 2 - Pilot Medical, Drugs, Scuba Diving
CHUF - Chapter 2 - Pilot Medical, Drugs, Scuba Diving
Jonny Preece · 31問 · 2年前CHUF - Chapter 2 - Pilot Medical, Drugs, Scuba Diving
CHUF - Chapter 2 - Pilot Medical, Drugs, Scuba Diving
31問 • 2年前CHUF - Chapter 3 - The Human Ear
CHUF - Chapter 3 - The Human Ear
Jonny Preece · 32問 · 2年前CHUF - Chapter 3 - The Human Ear
CHUF - Chapter 3 - The Human Ear
32問 • 2年前CHUF - Chapter 4 - The Human Eye - Functions & Limitations
CHUF - Chapter 4 - The Human Eye - Functions & Limitations
Jonny Preece · 31問 · 2年前CHUF - Chapter 4 - The Human Eye - Functions & Limitations
CHUF - Chapter 4 - The Human Eye - Functions & Limitations
31問 • 2年前CHUF - Chapter 5 - Disorientation in Flight
CHUF - Chapter 5 - Disorientation in Flight
Jonny Preece · 36問 · 2年前CHUF - Chapter 5 - Disorientation in Flight
CHUF - Chapter 5 - Disorientation in Flight
36問 • 2年前CHUF - Chapter 6 - The Effects of G Loads & Toxic Hazards
CHUF - Chapter 6 - The Effects of G Loads & Toxic Hazards
Jonny Preece · 20問 · 2年前CHUF - Chapter 6 - The Effects of G Loads & Toxic Hazards
CHUF - Chapter 6 - The Effects of G Loads & Toxic Hazards
20問 • 2年前CHUF - Chapter 7 - Circulation, Respiration & Hypoxia
CHUF - Chapter 7 - Circulation, Respiration & Hypoxia
Jonny Preece · 42問 · 2年前CHUF - Chapter 7 - Circulation, Respiration & Hypoxia
CHUF - Chapter 7 - Circulation, Respiration & Hypoxia
42問 • 2年前問題一覧
1
To protect the engine and tramsmission
2
To prevent coning and overpitching
3
To protect the structural limitations of the blades and the rotor hub
4
To retain inertia available, so we can glide instead of fall in the event of an engine failure.
5
To avoid retreating blade stall or compressibility. Also to protect the structural components of the aircraft.
6
To prevent the horizontal stabiliser from exerting an excessive upward force on the tail boom.
7
For aircraft controllability. There will be more parasite drag with sideways travel, no stabilizers, increased risk of dynamic rollover (if low)
8
For aircraft controllability. Also cannot see behind you. AIrcraft is not aerodynamically shaped to travel backwards. Risk of CO2 entering the cockpit.
9
To achieve successful take-off. Excess weight reduces performance.
10
To prevent structural damage. And limit the reduction in performance due to increased weight.
11
To prevent adverse handling characteristics. At weights below minimum, the ROD in autorotation may not be sufficient to maintain a safe rotor RPM.
12
To prevent structural damage and maintain controllability of the aircraft