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An-148 - Aircraft family

An-148 - Aircraft family

Development and testing

ANTONOV ASTC (Ukraine)

Assembly

VASO (Russia)

Sale/Leasing/Technical support

Ilyushin Finance Co. (Russia)

Summary

An-148 family of regional aircraft, designed by «Antonov»

ASTC (Kiev, Ukraine) and manufactured by Voronezh

Aircraft Manufacturing Company (Voronezh, Russia).

Version	Seats	Range, km
Аn-148-100А	70-80	2000–3000
Аn-148-100B	70-80	3000–4000
Аn-148-100E	70-80	4000-4400
Аn-148-100E1	40-55	6000–7000
Аn-148-100E2	10–30	7500–7700

An-148 design concept based on maximum airframe and

aircraft systems unification provides multiple tasks

fulfillment.

Freighter An-148C with a side loading door for

pallets and containers;

An-148-200 – stretch version (97 seats)

Combi (passengers + cargo) for payload flexibility

Multipurpose ramp freighter An-148T

An-148-100A/B/E/E1/E2 Types Commonality

Airframe and onboard systems

Powerplant (D436-148 engine with FADEC)

APU (AI-450MS)

Cockpit and flight control systems

Modular passenger cabin

Maintenance

Documentation

Crew training

Dimensions Dimensions

Design features Weight of sucked-in particle, grams (concrete)

Engines and wing high positioning reduces risk of

damage by foreign objects High-wing design scheme

reduces the number of shop visits

Payload/Range

Cockpit

The An-148 cockpit incorporates up-to-date concepts in ergonomics, navigation, communication and automatic

flight control.

• The electronic flight instrument system (EFIS) and engine indication and crew alerting system

(EICAS) display the flight and navigation information of power plant condition and aircraft systems on

multifunctional multicolor LCDs.

• The Aircraft equipment features flight management system, TCAS, EGPWS, color radar with wind shear

detector, inertial and satellite navigation systems.

• The Aircraft avionics meet the RNP-1, RVSM and ICAO IIIA landing category requirements.

Passenger cabin arrangements

	Wide fuselage cross-section allows “3+2” seats layout for economy-class and “2+2” seats layout for businessclass with comfort level similar to mainline airliners.
	The seats and passenger equipment can be altered to meet specific customer requirements considering specific operations.
	High passenger comfort provisions: • Successful engineering solutions are used in cabin space arrangement (wide aisle, optimum aisle height, large overhead bins (4,7 m3) accepting 25 x 66 cm roll-aboard bags); • Comon and individual areas are ergonomically optimized; • Low noise level; • In-flight entertainment, information and notification systems provide several stereo and video programs, satellite communication and Internet access

Performance


	–100A	–100B	–100E
Passenger capacity	75 passenger (32”), 80 passenger (30”)
Range	2100 km	3500 km	4400 km
Maximum fuel capacity	12 100 kg.
Cruising speed	800–870 km/h
Flight altitude	up to 12 200 m
Take-off length required	1560 m	1800 m	1885 m
Aerodrome elevation	up to 3000 m
Ambient temperature range	– 55 °С…+45 °C
Fuel consumption	1560 kg/h	1600 kg/h	1650 kg/h
Landing category	kkII (IIIA)
Community noise level	Chapter IV ICAO
Maximum take-off weight	38 550 kg	41 550 kg	43 700 kg

Engine

An-148 aircraft is powered by two D436-148 engines manufaсtured by “Motor Sich” plant (Ukraine). Depending on aircraft version, engine max takeoff thrust varies from 6400 up to 7500 kgf.
D 436-148 features:
• Full-authority digital electronic control (FADEC)
• Nacelles with thrust reversers
• Long engine lifetime of 40,000 flight hours and 20,000 cycles
• Rare shop visits: 10–12 000 hours “on-wing” between removals
• Specific fuel consumption: 0.360 kg/kgfh
The engine is designed for operations from hot-and-high airports.
Derated thrust setting for takeoff under normal conditions ensures longer engine lifetime.

Production Program Milestones

An-148 assembly lines are set up at Russia’s VASO
(Voronezh aircraft manufacturing facility) and Ukraine’s
AVIANT (Kyiv Aviation Plant). The two factories will be
able to manufacture up to 35 An-148s annually starting
from the year 2009.

• First flight – December 2004

• First deliveries – 2008

• Launch customers:

STC “Russia”

Air company “Polet” (Russia)

Alliance “AiRUnion”

Cubana de Aviacion

AN-148 Certification

Aircraft has an Airworthiness Certificate and complies with AP-25 Aviation Regulations (Russia) harmonized with CS-25 EASA (European Aviation Safety Agency) requirements.D-436-148 engine meets Russian AP-33 regulations, harmonized with CS-33. AI-450-MS APU meets Russian AP-VD regulations, harmonized with CS-APU.

Aircraft Noise requirements are in compliance with Chapter 4 of International Standart “Environmental protection”, Annex 16 to the Chicago Convention on International Civil Aviation (volume I “Aircraft noise”, issue 4) requirements and Russian AP-36 Aviation Regulations;

Engine Emission is in compliance with Annex 16 to the Chicago Convention on International Civil Aviation (volume II “Aircraft Engine Emissions”, issue 1981 with Amendments 1-4) requirements and Russian AP-34 Aviation Regulations.

AP-34 and AP-36 Aviation Regulations are harmonized with FAR/JAR-34, -36 requirements.

Aircraft service life and warranties
• Airframe: 80 000 hrs/40 000 landings/30 years
• D-436-148 engine: 40 000 hrs/ 20 000 cycles

Airframe and Engine warranties cover 24months/4000 hours/2000 cycles starting from the Aircraft delivery date.

Crew training

Simulator training is performed on the KTC-148 integrated aircraft simulator. Interactive training computer programs for flight crew and maintenance personnel have been developed on the basis of aircraft cockpit 3D model.

Crew and technical personnel training program features theoretical course, computer based training, fixed base simulator, full-flight simulator.

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