“Bharat Swati”的意思、由来-开放百科全书

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Bharat Swati

释义

Design and development
Variants
Specifications
Incidents and Accidents
References
Notes Bibliography

name=Swati

image=BHEL_Swati.jpg

caption=

}}{{Infobox Aircraft Type

type=Two-seat training monoplane

national origin=India

manufacturer=Bharat Heavy Electricals Limited

designer = Directorate General of Civil Aviation

first flight=17 November 1990

introduced=

retired=

status=

primary user=

number built=~20

unit cost = {{Indian Rupee}}3.8 million (1998)^[1]

developed from=

variants with their own articles=
}}

The Bharat Swati (or sometimes BHEL Swati) is an Indian two-seat training monoplane designed by the Technical Centre of Directorate General of Civil Aviation and built by Bharat Heavy Electricals Limited.

Design and development

The Swati is a low-wing cantilever monoplane with a steel tube fuselage covered in fabric at the rear and composite material at the front. It has metal tail surfaces and wooden wings and a fixed landing gear with a steerable nosewheel. The Swati has a {{convert|116|hp|kW|0|abbr=on}} Lycoming O-235 piston engine at the front driving a two-bladed propeller. Directorate General of Civil Aviation ordered 40 to be distributed to civil flying clubs in India.

Variants

LT-1M Swati

LT-2M Swati

Specifications

{{aerospecs
|ref=Brassey's World Aircraft & Systems Directory 1996
|met or eng?=met
|genhide=
|crew=2
|capacity=
|length m=7.21
|length ft=23
|length in=8
|span m=9.2
|span ft=30
|span in=3
|height m=2.78
|height ft=9
|height in=1½
|wing area sqm=11.96
|wing area sqft=128.74
|empty weight kg=530
|empty weight lb=1168
|gross weight kg=770
|eng1 number=1
|eng1 type=Lycoming O-235-N2C piston engine
|eng1 kw=87
|eng1 hp=116
|eng2 number=
|eng2 type=
|perfhide=
|max speed kmh=268
|max speed mph=167
|cruise speed kmh=195
|cruise speed mph=121
|range km=453
|range miles=282
|endurance h=2
|endurance min=45
|ceiling m=3050
|ceiling ft=10000
}}

Incidents and Accidents

On 3 June 1993 a Swati aircraft registration number VT-STC being test flown at Haridwar crashed when its starboard wing broke off after coming out of a loop killing the test pilot.^[2]

On 29 November 2001 a Swati LT II aircraft registration number VT-STO of the Kerala Aviation Training Centre on a training flight at Tiruvanantpuram crashed due to pilot error destroying the aircraft.^[3]

References

Notes

1. ^{{cite web|url=http://www.aero.pub.ro/wp-content/themes/aero.pub.ro/uploads/JANE_S_ALL_THE_WORLD_S_AIRCRAF/JANE_S_ALL_THE_WORLD_S_AIRCRAF/jawa0378.htm#IMG |title=Archived copy |accessdate=2011-06-02 |deadurl=yes |archiveurl=https://web.archive.org/web/20110903093538/http://www.aero.pub.ro/wp-content/themes/aero.pub.ro/uploads/JANE_S_ALL_THE_WORLD_S_AIRCRAF/JANE_S_ALL_THE_WORLD_S_AIRCRAF/jawa0378.htm |archivedate=2011-09-03 |df= }}
2. ^CIVIL AVIATION AIRCRAFT ACCIDENT SUMMARY FOR THE YEAR 1993 DGCA 2 February 2016
3. ^CIVIL AVIATION AIRCRAFT ACCIDENT SUMMARY FOR THE YEAR 2001 DGCA 3 February 2016

Bibliography

{{cite book |last=Taylor |first= Michael J. H.|authorlink= |coauthors= |title= Brassey's World Aircraft & Systems Directory|year=1996 |publisher= Brassey's|location= London, England |isbn=1-85753-198-1|pages=}}

4 : Indian civil trainer aircraft 1990–1999|Low-wing aircraft|Single-engined tractor aircraft|Bharat aircraft

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