| PERFORMANCE |
|
|
| MAXIMUM SPEED (kts./kmh) |
|
| (TAS at Mid Cruise Weight) |
234/433 |
|
| CRUISING SPEEDS |
|
| (TAS at Mid Cruise Weight) |
|
| Optimum Altitude |
|
| High Speed Cruise Power (75%) (kts./kmh) |
215/398 |
| Economy Cruise Power (65%) (kts./kmh) |
205/380 |
| Long Range Cruise Power (55%) (kts./kmh) |
196/363 |
|
| CRUISE RANGE |
|
(Cruising range
includes 45 minute fuel reserve at long range cruise power
plus allowance
for fuel used during taxi, take-off, climb at MCP, cruise at
optimum
altitude and stated mixture plus descent) |
| High Speed Cruise Power (75%) (nm/km) |
1330/2465 |
| Economy Cruise Power (65%) (nm/km) |
1420/2631 |
| Long Range Cruise Power (55%) (nm/km) |
1555/2881 |
|
| PRESSURIZATION (PSI) |
5.5 |
| Actual Aircraft Altitude |
Cabin Altitude |
| 12,300 ft./3749 m |
Sea Level |
| 25,000 ft./7620 m |
8000 ft./2438m |
|
| RATE OF CLIMB |
|
| (At Sea Level and Gross Wt.) |
|
| Full Power (fpm/mpm) |
1143/348 |
|
| STALL SPEED (CAS) |
|
| Flaps Down Full 400 (kts./kmh) |
58/107.4 |
| Flaps Up (kts./kmh) |
68/126.0 |
|
| SERVICE CEILING (100 fpm) (ft/m) |
*25,000+/7620+ |
|
| TAKE-OFF DISTANCE 200 Flaps |
|
| (Sea Level, Zero Wind, Standard Temperature) |
|
| Ground Run (ft/m) |
1440/439 |
| Total over 50-ft. obstacle (ft/m) |
2025/617 |
| LANDING DISTANCE |
|
| (Sea Level, Zero Wind, Standard Temperature) |
|
| Ground Roll (ft/m) |
1070/326 |
| Total over 50-ft Obstacle (ft/m) |
1800/549 |
|
| *25,000 ft is the maximum approved altitude for the Malibu. |
|
