Beriev A-42
| Specifications | |
|---|---|
| Countries of Origin | |
| Similar Aircraft | Wing span, m | 41.62 |
| Aircraft length,m | 45.04 |
| Aircraft height, m | 11.07 |
| Wing area, m2 | 200 |
| Wheel base, m | 14.835 |
| Wheel track, m | 5.71 |
| Maximum take-off weight, kg | 96000 |
| Combat load: | |
| - normal, kg | 4000 |
| - maximum, kg | 8500 |
| Maximum speed (ISA, 8000m), km/h | 770 |
| Cruise speed (ISA, 8000m), km/h | 650-710 |
| Operatinal altitude, m | 12000 |
| Mission flight altitude, m | 100-2000 |
| Maximum range, km | 11500 |
| Base requirements | I class airfield, hydrodrome |
| Runway length requiered in ISA conditions, m | 1800 |
| Seaworthiness: | |
| - Sea state | 4-5 |
| - Wind wave hight, m | 2 |
| Crew | 7 |
| Radius action for antisubmarine warfare with normal combat load
and 5% fuel reserve with sonar buoys deployment (4 hours patrolling): |
|
| - without refueling, km | 3500 |
| - with refueling, km | 5000 |
| - with deployment of dipping sonar module
(12 hours patrolling while the amphibian is afloat), kg |
4000 |
|
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