IL-114, IL-114T, IL-114-100 foto

PosNo.	Denomination	Unit	IL-114	IL-114T	IL-114-100
1	Quantity of passengers (economy/business class)	Person	52-64	-	52-64
2	Crew	Person	2+1(steward)	2	2+1(steward)
3	Maximum payload	t	-	7	-
4	Service range with 64 passengers	km	1000	1000	1800
5	Ferry range with load of 1.5 t	km	4800	4800	4800
6	Takeoff mass, t	t	23.5	23.5	24
7	Operational mass, t	t	15	15	15.2
8	Two integral fuel tanks capacity	l	8360	8360	8360
9	Altitude	m	7600	7600	7200
10	Cruising speed	km/h	500	500	520
11	Takeoff distance required	km	1.5	1.5	1.35
12	Landing distance required	km	1.3	1.3	1.35
13	Aircraft length	m	26.2	26.2	26.2
14	Fuselage diameter	m	2.86	2.86	2.86
15	Cabin width by floor	m	-	2.294	-
16	Cargo compartment volume	m3	-	76	-
17	Passenger cabin overall dimensions	mm	18930 x 2640 x 1920	-	18930 x 2640 x 1920
18	Entrance door dimensions	m	1.7 x 0.9	1.7 x 0.9	1.7 x 0.9
19	Cargo door dimensions	m	-	1.715 x 3.250	-
20	Engines	quantity x equivalent horse power	2 x 2500 TB7-117C (TV7-117C)	2 x 2500 TB7-117C (TV7-117C)	2 x 2640 PW-127H
21	CB-34 propellers with 6 blades (2pcs), diameter	m	3.6	3.6	3.93 propellers of Hamilton Standard (USA) Company
22	Fuel flow	g/passenger/km	17.5	17.5	16

Assigned service life of PW-127H engine is 6000 flying hours.
Aircraft total service life is:
30 000 flying hours, or
30 000 landings, or
30 years of operation
depending on whatever comes first.

Successful cooperation between the Ilyushin Aviation Complex and Tchkalov Aircraft Production Facility of Tashkent taking its origin in the 1950-es has given birth to a large fleet of passenger and cargo "Il" aircraft of various models. The latest among them is the Il-114T cargo aircraft based on the Il-114 passenger aircraft operated on the local airlines. This aircraft is designed for shot-range cargo operations and can use small poorly equipped paved and unpaved airfields that will allow it to win new markets in different regions. The modern quick-removable floor cargo handling devices and the large cargo door ensure quick and effective cargo loading/unloading and safe transportation of containerized (eight containers), palletized or bulky cargo. The cargo attendant compartment located in the forward section of the fuselage and separated from the cargo cabin by means of a smoke protection curtain has two passenger seats and a lavatory. If the number of attendants is increased the curtain will be moved backwards. Such cargo cabin configuration will accommodate six standard containers. Two turboprop TB7-117C engines with power of 2500 h.p. and quite six-blade propellers provide high fuel efficiency of the aircraft and low perceivable noise levels. New modified engines of 2800 h.p. will be installed beginning from 1997. When designing the Il-114T much attention was paid to providing high level of flight safety. For this purpose the elevator control mechanical linkage was replaced with the fly-by-wire with a backup cable control system. The engine nacelle structure was considerably simplified. Two-man flight crew. The digital flight navigation system the ensures aircraft reliable operation in any weather conditions, takeoff and landing of ICAO category II. The Il-114T's good lift-to drag ratio combined with low fuel consumption and modern aircraft equipment offer high operating economy. Maintenance and overhaul programs for the aircraft, its systems and equipment should be performed "on condition"; airframe service life is 30,000 landings. Ilyushin Aviation Complex and production facility provide aircraft aftersale support. Certification 1997.

Äëÿ âñåõ, êòî ðåøèë èììèãðèðîâàòü ÷åðåç çàïðîñ ïîëèòè÷åñêîãî óáåæèùà, à òàêæå äëÿ òåõ, êòî íàõîäèòñÿ â Ôåäåðàëüíîì Ðîçûñêå, ëèáî êîãî ìîãóò îáúÿâèòü â Ôåäåðàëüíûé Ðîçûñê. Ìû ðåøèì Âàøó ïðîáëåìó. 27 ëåò óñïåøíîé ðàáîòû. Îãðîìíûå àðõèâû. Ó íàøèõ êëèåíòîâ íå áûâàåò îòêàçîâ. Ðàáîòàòü ñ Âàìè áóäåì äî ïîñëåäíåãî, ïîêà Âû íå ïîëó÷èòå ñòàòóñ áåæåíöà è ðåçèäåíöèþ (ÏÌÆ) áåç âîçìîæíîñòè ýêñòðàäèöèè. Íèêòî êðîìå íàñ ðåøèòü Âàøó ïðîáëåìó íå ñìîæåò.

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