BASIC TECHNICAL DATA.
AN-124-100 Ruslan Unique Civil Transport Aircraft
Herewith we present to your attention the civil transport aircraft An-124-100 manufactured by Ulyanovsk Aviation Industrial Complex Aviastar-SP. This aircraft is intended for intercontinental transportation of bulky and oversized cargo of up to 120 ton weight.
At the customer’s option, three airborne cranes can be installed on the aircraft.
To carry superheavy monocargo of up to 120 tons weight (L=20 m, W=6 m, H=4m) An-124-100 aircraft is equipped with the special cargo handling equipment.
At the customer’s option, An-124-100 aircraft can be equipped with the special two-level system for transportation of up to 50 motor cars measuring 4.4m x 1.7m x 1.5m each.
At the customer’s option, the aircraft can be equipped with the transportation system to carry ISO international-class cargo containers arranged in two lines.
Up-to-date digital Integrated Flight and Navigation Complex installed on An-124-100 aircraft complies with all effective ICAO regulations for flights on international routes and provides the following:
• vertical separation of 1000 ft (300 m) between flight levels 290-360 (RVSM);
• RNP-5 requirements for BRNAV area navigation flights.
At the customer’s option, An-124-100 aircraft can be equipped with the following:
• Engine nacelles with noise suppressing devices to meet the noise level requirements of ICAO Enclosure 16, Chapter 3;
• Traffic Collision Avoidance System TCAS-2000 with mode S transponder of Honeywell (USA);
• VHF radio stations with 8.33/25 kHz channel spacing;
• Storage batteries 20ÍÊÁÍ-40Ä with signalling device ÓÑËÍ-250Ñ or VARTA 20FP38H1CT2-R to prevent from heat runaway;
• Airborne integrated radio navigation system ABRIS;
• Satellite communication equipment Mini-M of INMARSAT system;
• Comfortable compartment for maintenance crew.
 Today An-124-100 aircraft are successfully operated by the leading Russian airlines (Volga-Dnepr, Flight, etc.) and foreign airlines specialized in intercontinental transportation of bulky and oversized cargoes. |
AN-124-100 Aircraft Performance
|
Item |
Performance Description |
Value |
|
Dimensions and Areas |
||
|
1. |
Aircraft Length |
69.10m |
|
2. |
Aircraft Height (Maximum) |
21.08m |
|
3. |
Wing Span |
73.30m |
|
4. |
Cargo Cabin Length (with front and aft ramps) |
43.45m |
|
5. |
Cargo Cabin Length (without front and aft ramps) |
36.48m |
|
6. |
Cargo Cabin Width (Maximum) |
6.80m |
|
7. |
Cargo Cabin Floor Width |
6.40m |
|
8. |
Maximum Height of Cargo Cabin |
4.40m |
|
9. |
Front Cargo Door Dimensions |
6.40õ4.40m |
|
10. |
Aft Cargo Door Dimensions |
6.40õ4.40m |
|
11. |
Cargo Cabin Volume |
1014 m3 |
|
12. |
Track between Main LG Axis |
8m |
|
13. |
Wheelbase at Parking |
22.280-22.990m |
|
14. |
Turn Radius |
25m |
|
15. |
Distance From Ground to Cargo Door Sill: to the front one without kneeling to the front one with kneeling to the aft one without kneeling to the aft one with kneeling |
2.4...2.8m 1.43m 2.4...2.9m 2.1...2.2m |
|
Weight Calculations |
||
|
1. |
Maximum Taxi Weight |
398 t |
|
2. |
Maximum Take-off Weight |
392 t |
|
3. |
Maximum Landing Weight |
330 t |
|
4. |
Maximum Zero Fuel Operational Weight |
301 t |
|
5. |
Maximum Payload |
120 t |
|
6. |
Empty Aircraft Weight |
178.4 t |
|
Performance |
||
|
1. |
Crew |
6 persons+2 load masters |
|
2. |
Maximum True Speed of Horizontal Flight |
850 km/h |
|
3. |
Service Ceiling: - with take-off weight of 365t - with weight of 300t |
10000 m 11,200 m |
|
4. |
Service Range: - with cargo of 120t - with cargo of 40t |
4,600 km 10,840 km |
|
5. |
Landing Run |
1,350 m |
|
6. |
Take-off Run |
2,300 m |
|
7. |
Aerodrome Code Letter |
“À” and “Á” as per the classification of |
|
8. |
Landing category |
I |
|
9. |
Specific fuel consumption with maximum payload, (g/t*km) |
144 |
|
10. |
Fuel consumption per kilometer with maximum payload, kg/km |
13.4-14 |
|
11. |
Fuel flow per hour, t/hr |
11.3-13.6 t/hr |
|
12. |
BRNAV flights |
RNP-5 |
|
13. |
Vertical separation |
300 m (RVSM) |
|
14. |
Traffic collision avoidance |
TCAS-2000 |
|
15. |
VHF channel spacing |
8.33/25 kHz |
|
16. |
Field noise level |
Chapter 3, Enclosure 16 ICAO |
|
Engine Data |
||
|
1. |
Type of Main Engines |
D-18T |
|
2. |
Number of Engines x Take-off Thrust |
4õ23430 kgf/ 229.614kN |
|
3. |
Cruise Thrust |
4860 kgf/ 47.628kN |
|
4. |
Cruising Specific Fuel Consumption |
not greater than |
|
5. |
Engine Weight upon Delivery |
5700kg |
|
6. |
Assigned Service Life for D18Ò ser.3 Engine, cycles |
890 |
|
7. |
Number and Type of APUs |
2 õ ÒÀ-12 |
|
8. |
APUs Start Altitude: - on ground at aerodrome altitude - inflight |
up to 1610m up to 7000m |
|
9. |
Fuel Consumption, not greater than |
260 kg/h |
|
10. |
Power of APU, not less than |
395 hp |
