Transcript Slide 1

Presenting
IL-96-400T
General
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.
Specification
Operating Weights & Fuel Capacity
Max taxi weight, t
Max takeoff weight, t
Max payload, t
Max landing weight, t
Max zero fuel weight, t
Max fuel, t
266 / 271*
265 / 270*
92
220
208 / 210*
116,3
Aircraft Performance Characteristics (ISA)
Cruising speed, km/h
Maximum flight altitude, km
Required takeoff distance (with MTOW), m
Required landing distance (with MLW), m
Range with maximum payload, km
Range with 40 t payload, km
Range with maximum fuel, km
Airfield elevation (relative to sea level)
Range of operational temperatures, С
Crew
Maximum number of people on board
850-870
13.1
2450
1700
4750 / 5000*
12000
14500
-300 ÷ 1800
-45…+42
3
9
Specification
Main Deck:
Large cargo door (4850x2875 mm) port side
Lower deck:
Cargo door 1 (2690x1840 mm) starboard
Cargo door 2 (2690x1730 mm) starboard
Cargo Compartment
Lower Deck
Cargo Compartment
Lower Deck
Pallets Types
P9 / P6 / P1
LD-3
LD-3
1562 mm (61,5 in)
1562 mm (61,5 in)
LD-6
3175 mm (125 in)
P2
P8
P9 / P6 / P1
3175 mm (125 in)
1625 mm (64 in)
1625 mm (64 in)
1625 mm (64 in)
1625 mm (64 in)
LD-6
1625 mm (64 in)
LD-3
P2
2743 mm (108 in)
P8
1562 mm (61,5 in)
P8
1562 mm (61,5 in)
Cargo Compartment
Lower Deck
Variant
Pallet type
Dimensions
inch
Max weight
Quantity
mm
pound
Front
kg
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 Compartment
Upper Deck
Cargo Compartment
Upper Deck
2438 mm (96 in)
2438 mm (96 in)
2235 mm (88 in)
Р1
Р4
4978 mm (196 in)
Р6
3175 mm (125 in)
2438 mm (96 in)
Р6
2438 mm (96 in)
Р6
Р2
Р6 (one row)
2235 mm (88 in)
2438 mm (96 in)
2438 mm (96 in)
Р4
2438 mm (96 in)
Р6 (two row)
Cargo Compartment
Upper Deck
Variant
Pallet type
Dimensions
inch
mm
Max weight
Pound
Quantity
kg
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
Р4
96х196х96
2438х4978х2438
25000
11340
12+2Р2
Cargo Area
The cargo floor has mechanization for moving of
containers and pallets along the cargo compartment.
Range
100
90
80
Operating Weights & Range
Payload 92 t
5200 km
Payload 70 t
7400 km
Payload 62 t
9000 km
Payload 40 t
12000 km
Main deck, cubic m
580
Lower deck, cubic m
196 (114+82)
70
Tones
60
50
40
30
20
10
0
2000
4000
6000
8000 10000 12000 14000 16000
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).
Cockpit
Seat for supernumerary
Crew member
Co-pilot
Flight engineer
Rest places
Captain
Cargo net
First observer
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-96400Т 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).
Avionics specification
Radio Unit Control Panel
With radio navigation system control separately from
Flight Management System (FMS);
and 8,33/25 kHz frequency range.
Aerodynamic stability and controllability system
With preflight control panel
Flight 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 panel
Inertial Navigation System
EGPWS
Contains 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).
EFIS
Includes 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 computer
Critical Condition Warning System
Avionics specification
Collision Avoidance System (CAS)
With changes 7, Mode S, 1 set providing aerial collision prevention and 2 Mode –S responders
EICAS with 6,25" x 6,25“ LCD
Flight Data Recorder with solid state data storage.
Weather Radar System
•Featuring wind shear warning and turbulence detection
Fault Detection Isolation System
• interaction with upgraded equipment;
• failure information indication on FMS display control panel
Automatic Direction Finder
VHF Omni directional Radio Range (VOR)
•Dual set
Dispatch 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 Chronometer
Set 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 navigation
Selective Calling System
providing selective crew radio call (up to 5 channels VHF-HF).
3 VHF Radio
Satellite communication system operating in Inmarsat standard.
2 HF Radio with Intercom function
Emergency VHF Radio
Two 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.