Difference between revisions of "Template:Airspec-imp"
Jump to navigation
Jump to search
↑ Empty citation (help)
blackwiki>Karl Dickman (update to changes in the template) |
blackwiki>Karl Dickman m (ref format) |
||
| Line 6: | Line 6: | ||
|jet or prop?=<!-- options: jet/prop/both/neither --> | |jet or prop?=<!-- options: jet/prop/both/neither --> | ||
| − | |ref={name of source}<ref>{{cite | + | |ref={name of first source}<ref>{{ |
| + | cite web | ||
| + | |url= | ||
| + | |title= | ||
| + | |last= | ||
| + | |first= | ||
| + | |date= | ||
| + | |accessdate= | ||
| + | |work= | ||
| + | |publisher= | ||
| + | }}</ref> | ||
<!-- Now, fill out the specs. Please include units where appropriate (main comes first, alt in parentheses). If an item doesn't apply, like capacity, leave it blank. For instructions on using |more general=, |more performance=, |power original=, and |thrust original= see [[Template talk:Aircraft specifications]]. To add a new line, end the old one with a right parenthesis ")", and start a new fully formatted line beginning with * --> | <!-- Now, fill out the specs. Please include units where appropriate (main comes first, alt in parentheses). If an item doesn't apply, like capacity, leave it blank. For instructions on using |more general=, |more performance=, |power original=, and |thrust original= see [[Template talk:Aircraft specifications]]. To add a new line, end the old one with a right parenthesis ")", and start a new fully formatted line beginning with * --> | ||
|crew= | |crew= | ||
Revision as of 23:47, 9 May 2006
Specifications ()
Data from {name of first source}[1]
General characteristics
- Length: ft in (m)
- Wingspan: ft in (m)
- Height: ft in (m)
- Wing area: ft² (m²)
- Empty weight: lb (kg)
- Useful load: lb (kg)
- Loaded weight: lb (kg)
- Max. takeoff weight: lb (kg)
Performance
- Maximum speed: knots (mph, km/h)
- Cruise speed: knots (mph, km/h)
- Stall speed: knots (mph, km/h)
- Never exceed speed: knots (mph, km/h)
- Range: nm (mi, km)
- Service ceiling: ft (m)
- Rate of climb: ft/min (m/s)
- Wing loading: lb/ft² (kg/m²)