Presenting IL-96-400T. The IL-96-400T aircraft is a cargo version of well-known IL-96-300 passenger aircraft with increased fuel capacity, stretched by.

Presenting

IL-96-400T

The IL-96-400T aircraft is a cargo version of well-known IL-96-300 passenger aircraft with increased fuel capacity, stretched by 9.35 m and equipped with new turbofan engines and improved avionics.

Designed by Ilyushin Aviation Complex (Moscow, Russia) and manufactured by Voronezh Aircraft Manufacturing Company (Voronezh, Russia), IL-96-400T is capable of transporting up to 92 tones.

The aircraft is powered by four turbofan two-shaft PS-90A1 engines complying with the international ecological requirements and with approved license to operate worldwide.

General

Specification

Operating Weights & Fuel CapacityMax taxi weight, t 266 / 271*Max takeoff weight, t 265 / 270*Max payload, t 92Max landing weight, t 220Max zero fuel weight, t 208 / 210*Max fuel, t 116,3

Aircraft Performance Characteristics (ISA)

Cruising speed, km/h 850-870Maximum flight altitude, km 13.1Required takeoff distance (with MTOW), m 2450Required landing distance (with MLW), m 1700Range with maximum payload, km 4750 / 5000*Range with 40 t payload, km 12000Range with maximum fuel, km 14500Airfield elevation (relative to sea level) -300 ÷ 1800Range of operational temperatures, С -45…+42Crew 3Maximum number of people on board 9

Specification

Main Deck:Large cargo door (4850x2875 mm) port side

Lower deck:Cargo door 1 (2690x1840 mm) starboardCargo door 2 (2690x1730 mm) starboard

Cargo CompartmentLower Deck

Cargo CompartmentLower Deck

3175 mm (125 in)

P9 / P6 / P1

1534 mm (60,4 in)

1625

mm

(64

in)

1625

mm

(64

in)

1625

mm

(64

in)

1625

mm

(64

in)

1625

mm

(64

in)

1562 mm (61,5 in)1534 mm (60,4 in) 1534 mm (60,4 in)

1534 mm (60,4 in)

2235 mm (88 in)

2438 mm (96 in)

2235 mm (88 in) 1562 mm (61,5 in)

3175 mm (125 in)

3175 mm (125 in) 2743mm (108 in)

3175 mm (125 in)1562 mm (61,5 in) 1562 mm (61,5 in)

LD-3 LD-6 P9 / P6 / P1 P 2 P 8

1562 mm (61,5 in) 1562 mm (61,5 in)

P 8 P 8

2743 mm (108 in)

P 2LD-6LD-3 LD-3

Pallets Types

Cargo CompartmentLower Deck

Variant Pallet type Dimensions

inch mm

Max weight

pound kg

Quantity

Front Back

1 LD – 3 60,4х61,5х64 1534х1562х1625 3300 1500 18 14

2 LD – 6 60,4х125х64 1534х3175х1625 7000 3175 9 7

3 P8 size K, NAS 3610 60,4х61,5х64 1534х1562х1625 3300 1500 18 14

4 P9 size L, NAS3610,LD-5/10/11 60,4х125х64 1534х3175х1625 6600 3000 9 7

5 P2 size B, NAS 3610 88х108х64 2235х2743х1625 8000 3628 5 4

6 P1 size A, NAS3610, LD-7/9/29 88х125х64 2235х3175х1625 10200 4627 5 4

7 P6 size M, NAS 3610 96х125х64 2438х3175х1625 11000 5000 5 4

8 Half size from size M NAS 3610 96х61,5х64 2438х1562х1625 5535 2500 10 8

Cargo CompartmentUpper Deck

Cargo CompartmentUpper Deck

Р6 (two row)

2438

mm

(96

in)

2438 mm (96 in)

3175 mm (125 in)

Р6 (one row)

2438

mm

(96

in)

3175 mm (125 in) 2438 mm (96 in)

2438

mm

(96

in)

Р4

2438 mm (96 in)4978mm (196 in)

Р2

2743 mm (108 in)2235 mm (88 in)

2235

mm

(88

in)

3175 mm (125 in)

Р1

2235 mm (88 in)

2235

mm

(88

in)

Р 6 Р 6 243

8 m

m (9

6 in

)

Р 4 Р 6 243

8 m

m (9

6 in

)

2438 mm (96 in) 2438 mm (96 in) 3175 mm (125 in)4978 mm (196 in)

Cargo CompartmentUpper Deck

Variant Pallet type Dimensions

inch mm

Max weight

Pound kg

Quantity

1 Р6 (two row) 96х125х96 2438х3175х2438 15000 6800 25+1Р2

2 Р1 88х125х88 2235х3175х2235 10000 6080 25+1Р2

3 Р2 88х108х88 2235х2743х2235 8000 4530 26

4 Р6 (one row) 96х125х96 2438х3175х2438 15000 6800 12+2Р2

5 Р 4 96х196х96 2438х4978х2438 25000 11340 12+2Р2

Cargo Area

The cargo floor has mechanization for moving of containers and pallets along the cargo compartment.

Range

Operating Weights & RangePayload 92 t 5200 kmPayload 70 t 7400 kmPayload 62 t 9000 kmPayload 40 t 12000 kmMain deck, cubic m 580Lower deck, cubic m 196 (114+82)

120000 2000 4000 6000 8000 10000

10

20

30

40

50

60

70

80

90

100

14000 16000

Tone

s

Range, km

Cockpit

The IL-96-400T aircraft operated by 3 crew members is equipped with modern avionics which includes six multifunctional color-LCD displays (EFIS), Flight Management System (FMS), Inertial Navigation System, Collision avoidance System (CAS) including mode “S” transponder, EGPWS system, VHF communications (compliant with ICAO requirements of item 4.7 Appendix 10), and equipment permitting flights in RVSM conditions.

The avionics complex comply with modern requirements on international routes in Europe and North America (RNP-1, RNP-5, RNP-10, RNP-12.6, RNP-20) and allows to navigate and land under ICAO CAT II category (IIIA category is optional), speed hold, automatic voice warning system (in English).

The crew and cargo cabins correspond to aircraft requirements for protection against the illegal intrusion (the Amendment 27 to a Part 1 of the Appendix 6 to ICAO) and to safety requirements (Chapter 11 of the Appendix 8 to ICAO).

Captain

Co-pilot

Flight engineer

First observer

Seat for supernumeraryCrew member

Cargo net

Rest places

Cockpit

Certification

IL-96-400T aircraft has Supplement to Type Certificate № 22-96-300/Д20 issued by Interstate Aviation Committee (MAK), corresponds to national aviation regulations and meets ICAO requirements (Chapter 4 of the Appendix 6). PS-90A1 engine has Supplement to Type Certificate № 16-Д/Д29 issued by Interstate Aviation Committee (MAK), corresponds to NLGS-3 national aviation regulations.

Noise requirements – IL-96-400T aircraft has Noise Type Certificate №СШ175-Ил-96-400Т and is in compliance with requirements of Chapter 4 International Standard “Environmental protection”.

Emissions – in compliance with requirements of Annex 16 to the Chicago Convention on International Civil Aviation (volume II “Aircraft Engine Emissions”, issue 1981 with Amendments 1-4).

Radio Unit Control PanelWith radio navigation system control separately from Flight Management System (FMS);and 8,33/25 kHz frequency range.Aerodynamic stability and controllability systemWith preflight control panelFlight Management System•compliance with RNP-1 requirements;•correction according satellite navigation system;•data base loading according to ARINС-424;•amount of non-volatile memory (data base) 4 Mb;•FDR access provision.FMS Interface Unit • data transmitting for FMS; • signals generation to voice alert system (on reaching the radio altitude)Multifunctional Flight Display (MFD) with MFD control panelInertial Navigation SystemEGPWSContains data base on terrain relief and provides early ground proximity warning of terrain relief data along trajectory having characteristics of TAWS level, A class. From 1 January, 2004 (Amendment 27 to Part 1 of Addendum 6, ICAO).EFISIncludes liquid crystal displays of 6,25” x 6,25” size, 1 set. TCAS-II, Early Ground Proximity Warning System and weather radar data display.Air data computerCritical Condition Warning System

Avionics specification

Collision Avoidance System (CAS)With changes 7, Mode S, 1 set providing aerial collision prevention and 2 Mode –S respondersEICAS with 6,25" x 6,25“ LCDFlight Data Recorder with solid state data storage.Weather Radar System•Featuring wind shear warning and turbulence detectionFault Detection Isolation System • interaction with upgraded equipment;• failure information indication on FMS display control panelAutomatic Direction FinderVHF Omni directional Radio Range (VOR)•Dual setDispatch transponder (Doubled)Distance Measuring Equipment with scanning mode (DME)Radio Altimeter•Featuring Rz code (H3)Instrument Landing System•Tripled set, improved jamming resistance of HF broadcast.Electronic ChronometerSet of stand-by equipment including - Radio Magnetic Indicator, Standby Giro Horizon, Magnetic Compass, Instrumental Speed Indicator, Mechanic Pressure Foot-Graduated Altimeter.Automatic Flight Control System and Thrust Control System enable:•automatic approach;•automatic go-around;•vertical speed hold with automatic and manual thrust control;•override control;

Avionics specification

•altitude hold;•“reaching of the prescribed level” with automatic and manual thrust control;•heading hold;•thrust hold;•automatic hold of speed and Mach number via thrust channel on route flight modes;automatic mode of horizontal navigationSelective Calling Systemproviding selective crew radio call (up to 5 channels VHF-HF).3 VHF RadioSatellite communication system operating in Inmarsat standard.2 HF Radio with Intercom functionEmergency VHF RadioTwo emergency locator-transmitter (ELT) portable radio buoy providing operation in COSPAS-CARCAT (in compliance with ICAO Part 5 vol.III Appendix 10 requirements )Cockpit Voice Recorder providing record of crew members talks and cockpit sound situation (4 channels) with keeping data records for more than 2 flight hours.

Avionics specification