www.bzupages.com human resource management. presented to: sir ahmad tisman pasha

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Human Resource ManagementHuman Resource Management


Presented To:Presented To:

Sir Ahmad Tisman PashaSir Ahmad Tisman Pasha


Presented By:Presented By:

Farrukh Ali SahuFarrukh Ali Sahu 07-4307-43

Computer Science DepartmentComputer Science Department Bahauddin Zakariya University Bahauddin Zakariya University

MultanMultan


F-16F-16

Fighter planeFighter plane


HistoryHistoryThe Lockheed Martin The Lockheed Martin F-16 Fighting FalconF-16 Fighting Falcon is a multirole jet fighter aircraft is a multirole jet fighter aircraft originally developed by general dynamic for the United States originally developed by general dynamic for the United States Airfoece.Designed as a lightweight fighter, it evolved into a successful Airfoece.Designed as a lightweight fighter, it evolved into a successful multirole aircraft. .multirole aircraft. .

The Falcon's versatility is a paramount reason it has proven a success on The Falcon's versatility is a paramount reason it has proven a success on the export market, having been selected to serve in the air forces of 25 the export market, having been selected to serve in the air forces of 25 nations.nations.

The F-16 is the largest Western fighter program with over 4,400 aircraft The F-16 is the largest Western fighter program with over 4,400 aircraft built since production was approved in 1976.built since production was approved in 1976.

Though no longer being bought by the U.S. Air Force, advanced versions Though no longer being bought by the U.S. Air Force, advanced versions are still being built for export customers.are still being built for export customers.

In 1993, General Dynamics sold its aircraft manufacturing business to the In 1993, General Dynamics sold its aircraft manufacturing business to the Lockeed corpotation which in turn became part of Lockheed Martin after a Lockeed corpotation which in turn became part of Lockheed Martin after a 1995 merger with Martin Marittea1995 merger with Martin Marittea


RoleRole Multirole fighter Multirole fighter

National originNational origin United StatesUnited States

ManufacturerManufacturer General DynamicsGeneral Dynamics Lockheed MartinLockheed Martin

First flightFirst flight 2 February 19742 February 1974

IntroductionIntroduction 17 August 197817 August 1978

StatusStatus ActiveActive

Primary usersPrimary usersUnited States Air ForceUnited States Air Force 25 other users 25 other users


Operational historyOperational history First combat successes: Bekaa Valley and OsiraFirst combat successes: Bekaa Valley and Osira

q raid (1981)q raid (1981)

Operation Peace for Galilee (1982)Operation Peace for Galilee (1982) Incidents during the Soviet-Afghan War (1986-1Incidents during the Soviet-Afghan War (1986-1

988)988)

Operation Desert Storm (1991)Operation Desert Storm (1991) Interwar Air Operations over Iraq (1991-2003)Interwar Air Operations over Iraq (1991-2003) Venezuelan coup attempt (1992)Venezuelan coup attempt (1992) Balkans (1994-1995 and 1999)Balkans (1994-1995 and 1999) Aegean incidents (1996 and 2006)Aegean incidents (1996 and 2006) Kargil War (1999)Kargil War (1999) Operations in Afghanistan (2001-date)Operations in Afghanistan (2001-date) Invasion of Iraq and post-war operations (2003-dInvasion of Iraq and post-war operations (2003-d

ate)ate)

Second Lebanon War (2006)Second Lebanon War (2006) Operation Sun (2008)Operation Sun (2008)


General characteristicsGeneral characteristics

Length: 49 ft 5 in (14.8 m) Length: 49 ft 5 in (14.8 m) WingspanWingspan: 32 ft 8 in (9.8 m) : 32 ft 8 in (9.8 m) Height: 16 ft (4.8 m) Height: 16 ft (4.8 m) Wing area: 300 ft² (27.87 m²) Wing area: 300 ft² (27.87 m²) AirfoilAirfoil: : NACA 64A204NACA 64A204 root and tip root and tip Empty weight: 18,900 lb (8,670 kg) Empty weight: 18,900 lb (8,670 kg) Loaded weight: 26,500 lb (12,000 kg) Loaded weight: 26,500 lb (12,000 kg) Max takeoff weightMax takeoff weight: 42,300 lb (19,200 kg) : 42,300 lb (19,200 kg) Powerplant: 1× Powerplant: 1× Pratt & Whitney F100Pratt & Whitney F100-PW--PW-220 afterburning 220 afterburning turbofanturbofan


PerformancePerformanceMaximum speedMaximum speed:: At altitude: Mach 2+ (1,500 mph, 2,414 At altitude: Mach 2+ (1,500 mph, 2,414

km/h) km/h) Combat radius: 340 Combat radius: 340 NMNM (295 mi, 550 km) (295 mi, 550 km) on a hi-lo-hi mission with six 1,000 lb (450 on a hi-lo-hi mission with six 1,000 lb (450 kg) bombs kg) bombs At sea level: At sea level: MachMach 1.2 (915 mph, 1,470 1.2 (915 mph, 1,470

km/h) km/h) Ferry rangeFerry range:: 2,280 NM (2,620 mi, 4,220 2,280 NM (2,620 mi, 4,220 km) with drop tanks km) with drop tanks Service ceiling 50,000+ ft (15,200+ m) Service ceiling 50,000+ ft (15,200+ m) Rate of climb: 50,000 ft/min (254 m/s) Rate of climb: 50,000 ft/min (254 m/s) Wing loading: 88.3 lb/ft² (431 kg/m²) Wing loading: 88.3 lb/ft² (431 kg/m²) Thrust/weightThrust/weight:: For F100 engine: 0.898, For For F100 engine: 0.898, For F110: 1.095 F110: 1.095


Thank you!Thank you!

www.bzupages.com human resource management. presented to: sir ahmad tisman pasha

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