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Y-7-100 (Yunshuji-7-100) Chinese Cargo Transport Aircraft

Y-7-100

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Basic Information
Name
Y-7-100 (Yunshuji-7-100) Chinese Cargo Transport Aircraft
Designation
Y-7-100
Alternate Designation
Equipment Type
Manufacturer
Xi'an Aircraft Industry Corporation
Date of Introduction
1997
Description

Y-7-100 This is an improved version developed with the assistance of the Hong Kong Aircraft Engineering Co. (HAECO). This version has greater wing span and winglets, Hamilton Standard environmental control system, three-man flight deck, updated avionics and revised Noordam cabin layout with reclining seats. The Xian Y-7 (Chinese: 运-7; pinyin: Yùn-qī) is a transport/passenger aircraft built in China. It is based on the Soviet-designed Antonov An-24 series. China imported the Antonov An-24 from early in its production run and also negotiated licences for production of the aircraft and its engines. In 1966, Xi'an aircraft factory started the project of local production of An-24. The first Chinese-assembled An-24T had its maiden flight on 25 December 1970. Production was launched in 1977 at the Xi'an aircraft factory but progress was slow due to the deleterious effects of the Cultural Revolution, with a pre-production aircraft displayed to the public at Nanyuan air base, near Beijing, on 17 April 1982. The WJ-5A1 turboprop engine was chosen as the Y-7's power source. The first production aircraft was not flown until February 1984, illustrating the slow progress (eighteen years from licence to production). The Chinese aircraft equated to the An-24RV, having a full complement of windows and the booster jet engine. The majority of early deliveries were to the People's Liberation Army Air Force (PLAAF), mostly as transports, with a few in 52-seat airliner configuration for the Civil Aviation Administration of China (CAAC). After the initial licensed production run, the Y-7 was developed separately from the An-24 with a succession of upgrades culminating in the Xian MA60 (Modern Ark) series. A tactical transport derivative was copied, unlicensed, from the Antonov An-26 and emerged as the Y-7H, incorporating the cargo ramp door and military equipment of the An-26.

Air & Air Defense Specifications
Crew 3
Engine Turboprop (2790 hp)
Max Speed 518.0 km/h
Variants
Variants Xian Y-7E Speculative designation for a 'Hot and High" version with more powerful engines. Xian Y-7G A military variant of the MA60 produced for the PLAAF. Xian Y-7H (Huo -cargo) A reverse-engineered An-26 with rear loading ramp for the PLAAF, entering production in 1992. Xian Y7H-500 Civil variant of the Y-7H certified in 1994. Xian Y-14 The original designation for the An-26 copy/Y-7H. Xian Y-7-100 Improved version, developed in co-operation with HAECO (Hong Kong Aircraft Engineering Company), with redesigned cockpit and cabin, as well as winglets. This variation has an upgraded passenger cabin interior, with new avionics sourced from western providers. Flight crew reduced to three, it is capable of carrying 52 passengers. Xian Y-7-100C1 Five-crew variant with equipment changes. Xian Y-7-100C2 Five-crew variant with equipment changes. Xian Y-7-100C3 Five-crew variant with equipment changes. Xian Y-7-200 Fitted with new avionics; without winglets. Xian Y-7-200A Powered by two Pratt & Whitney PW127C turboprop engines. Xian Y-7-200B Stretched version (74cm (29in)) with WJ5A-1G engines, built for the Chinese domestic market. Xian HYJ-7 (Hongzhaji Yunshuji Jiaolianji - Bomber/transport/trainer) A pilot and crew trainer for H-6 heavy bombers fitted with a stabilised HM-1A bombsight, bomb-aiming radar and a TNL-7880 combined navigation system. Xian MA60 (Y-7-MA60) (Modern Ark 60 seats) A westernised variant of the Y-7 intended to attract more western customers and meet Joint Airworthiness Requirements. Xian JZY-01 experimental aircraft / Y-7 AWACS Carrier-based airborne early warning and control (AEW&C) variant. JZY stands for Jian (舰) Zai (载) Yu (预), meaning carrier borne AEW&C, has 4 rudders like E-2 AEW It is being used as a testbed for Xian KJ-600.
System
Alternate Designation(s) Y-7-100; Yunshuji-7-100
Primary Function / Type Cargo Transport Aircraft
Manufacturer Xi'an Aircraft Industrial Corporation
Crew 3 or 5
Passengers 48-52 passengers
Number of Engines 2
Number of Hard Points INA
Dimensions
Length 23.71 m
Width (Wing Span) 29.64 m
Height 8.55 m
Wing Area 74.98 sq m
Cabin Length 10.50 m
Cabin Width 2.80 m
Cabin Height 1.90 m
Cabin Volume 56 cu m
Empty Weight 14,952 kg
Maximum Takeoff Weight 21,800 kg
Maximum Payload Weight 5,500 kg
Automotive
Engine Name 2 x Shanghai WJ-5A-1
Number of Engines 2
Engine Type Turboprop
Engine Power 2,790 shaft hp each
Standard Internal Fuel Capacity 5,106 liters
Optional Internal Fuel Capacity 6,192 liters
Maximum Speed 518 km/h
Cruise Speed at 4,000 m 487 km/h
Economical Speed 423 km/h
Range with Maximum Payload 910 km
Range with Maximum Fuel 2,420 km
Climb Rate 458 m/min
Ceiling 8,750 m
Fire Control System / Avionics
FCS Name INA
Computerized FCS No
Navigation Radar INA
Protection
Stealth Properties No
Heat Signature Reduction No
Add on Armor INA
NBC Protection INA
EW Counter Measures INA
Chaffs/Flares INA
Details
Country of Origin China
Category Fixed Wing Aircraft
Air > Fixed Wing Aircraft
Filter Label
Y
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
23.71 m
Width
29.64 m
Height
8.55 m
Weight
21800 kg
Operators (6)
China
Iran
Cambodia
Laos
Mauritania
Zimbabwe
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