Copyright Dmitry Osipov
BAe ATP Specifications
| ATP | |
Dimensions | |
|---|---|
| Length (m) | 26.0 |
| Wingspan (m) | 30.6 |
| Height (m) | 7.6 |
| Wing area (m2) | 78.3 |
Weight | |
| Maximum take-off weight (kg) | 23 680 |
| Maximum landing weight (kg) | 23 130 |
| Operating empty weight (kg) | 15 130 |
| Maximum zero fuel weight (kg) | 21 770 |
| Maximum payload (kg) | 6 640 |
| Standard fuel capacity (litres) | 6 360 |
Performance | |
| Range with max payload (km) | 1 740 |
| Maximum operating altitude (m) | 7 600 |
| Take-off field length (m) | 1 350 |
| Landing field length (m) | 1 130 |
| Engines | P&WC PW126A, 2 x 2665 hp |
Cabin Data | |
| Passengers (1-class) | 64 |
| Cabin width (m) | 2.5 |
BAe ATP Airplane
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Discussion of Airplane
22.07.2017
WHAT REMEDIAL ACTION WAS THERE FOR LANDING GEAR DIFFICULTIES...
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