Caudron C.684: Difference between revisions
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{{infobox Aircraft | {{infobox Aircraft | ||
|image = C684-2.jpg | |image = C684-2.jpg | ||
|name = Caudron C.684 | |name = Caudron C.684 | ||
|type = | |type = | ||
|fdm = JSBSim | |fdm = JSBSim | ||
|status = beta (0.4.12) | |status = beta (0.4.12) | ||
|authors = Guillaume Chauvat | |authors = Guillaume Chauvat<br/>Laurent Hayvel (texture) | ||
|fgname = C684 | |fgname = C684 | ||
}} | }} | ||
The '''Caudron C.684''' was a single piston engine sport plane of the 1930s. | The '''Caudron C.684''' was a single piston engine sport plane of the 1930s. | ||
== Aircraft help == | == Aircraft help == | ||
{| | {| | ||
! Key | |||
! Description | |||
|- | |||
|G | |G | ||
|Select propeller low pitch (takeoff / landing) | |Select propeller low pitch (takeoff / landing) | ||
Line 25: | Line 27: | ||
|Apply selected pitch | |Apply selected pitch | ||
|} | |} | ||
=== User's Manual === | === User's Manual === | ||
Line 31: | Line 32: | ||
==== Standard procedures ==== | ==== Standard procedures ==== | ||
===== Startup ===== | ===== Startup ===== | ||
# Battery: On | # Battery: On | ||
Line 73: | Line 73: | ||
==== Emergency procedures ==== | ==== Emergency procedures ==== | ||
===== Accidental spin ===== | ===== Accidental spin ===== | ||
* Rudder: in the direction of the spin | * Rudder: in the direction of the spin | ||
Line 89: | Line 88: | ||
* Max continuous RPM: 2500 for 5 minutes | * Max continuous RPM: 2500 for 5 minutes | ||
== External link == | |||
== External | |||
* http://www.aviafrance.com/aviafrance1.php?ID=9849&ID_CONSTRUCTEUR=313 | * http://www.aviafrance.com/aviafrance1.php?ID=9849&ID_CONSTRUCTEUR=313 | ||
[[Category: | [[Category:Single-engine aircraft]] | ||
[[Category:Sport aircraft]] |
Revision as of 14:16, 27 April 2012
Author(s) |
|
---|---|
FDM | JSBSim |
--aircraft= | C684 |
Status | beta (0.4.12) |
The Caudron C.684 was a single piston engine sport plane of the 1930s.
Aircraft help
Key | Description |
---|---|
G | Select propeller low pitch (takeoff / landing) |
g | Select high pitch (cruise) |
! | Toggle battery |
$ | Apply selected pitch |
User's Manual
The propeller is an old variable pitch propeller. It has only two configurations: low and high pitch. Use low pitch for low speeds: takeoff and landing. Use high pitch for cruise (more than 180 km/h).
Standard procedures
Startup
- Battery: On
- Magnetos: both
- Starter: 10 seconds max
Takeoff
- Flaps: 20°
- Full power
- Lift tail wheel at 100 km/h
- Initial climb: 140 km/h
- 100 m (300 ft): Flaps: 0°
- Climb: 150 km/h
Climb
- 150 km/h
- Pitch: low
- Full power
Cruise climb
- Full power
- Pitch: high
- 200 km/h
Change pitch
- Apply pitch: Off
- Select pitch
- Apply pitch: On
- When the light is off, apply pitch: Off
Remark: there are only two different pitches: low and high. "Slow high" ("grand pas lent") makes just the pitch change more slowly than "high pitch" ("grand pas").
Cruise
- Propeller Pitch: High
- 2200 rpm, 275 km/h
- Above 1500 m (4500 ft), mixture in order to maximize rpm.
Landing
- Flaps: 45°
- Speed: 140 km/h
Emergency procedures
Accidental spin
- Rudder: in the direction of the spin
- Elevator: neutral position
- Ailerons: neutral position, DO NOT USE AILERONS
- When the spin stops: pull (<3.5g) to raise the plane
Limitations
Remark: since I didn't find any manual, most of speeds are just estimates
- VNE: 400 km/h (215 kt)
- VFE: 190 km/h (103 kt)
- Max positive G: +3.5
- Max negative G: -1.5
- Max RPM: 2800
- Max continuous RPM: 2500 for 5 minutes