Human Resource Management

Presented To: Sir Ahmad Tisman Pasha

Presented By: Farrukh Ali Sahu Computer Science Department Computer Science Department Bahauddin Zakariya University Bahauddin Zakariya University Multan Multan

F-16 Fighter plane Fighter plane

History The Lockheed Martin F-16 Fighting Falcon is a multirole jet fighter aircraft originally developed by general dynamic for the United States Airfoece.Designed as a lightweight fighter, it evolved into a successful multirole aircraft.. 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 nations. The F-16 is the largest Western fighter program with over 4,400 aircraft built since production was approved in The F-16 is the largest Western fighter program with over 4,400 aircraft built since production was approved in Though no longer being bought by the U.S. Air Force, advanced versions are still being built for export customers. In 1993, General Dynamics sold its aircraft manufacturing business to the Lockeed corpotation which in turn became part of Lockheed Martin after a 1995 merger with Martin Marittea In 1993, General Dynamics sold its aircraft manufacturing business to the Lockeed corpotation which in turn became part of Lockheed Martin after a 1995 merger with Martin Marittea

Role Multirole fighter National origin United States United StatesUnited States ManufacturerGeneral Dynamics Lockheed Martin General DynamicsLockheed MartinGeneral DynamicsLockheed Martin First flight2 February 1974 Introduction17 August 1978 StatusActive Primary usersUnited States Air Force 25 other users United States Air ForceUnited States Air Force

Operational history Operational history First combat successes: Bekaa Valley and Osiraq raid (1981) First combat successes: Bekaa Valley and Osiraq raid (1981) First combat successes: Bekaa Valley and Osiraq raid (1981) First combat successes: Bekaa Valley and Osiraq raid (1981) Operation Peace for Galilee (1982) Operation Peace for Galilee (1982) Operation Peace for Galilee (1982) Operation Peace for Galilee (1982) Incidents during the Soviet-Afghan War ( ) Incidents during the Soviet-Afghan War ( ) Incidents during the Soviet-Afghan War ( ) Incidents during the Soviet-Afghan War ( ) Operation Desert Storm (1991) Operation Desert Storm (1991) Operation Desert Storm (1991) Operation Desert Storm (1991) Interwar Air Operations over Iraq ( ) Interwar Air Operations over Iraq ( ) Interwar Air Operations over Iraq ( ) Interwar Air Operations over Iraq ( ) Venezuelan coup attempt (1992) Venezuelan coup attempt (1992) Venezuelan coup attempt (1992) Venezuelan coup attempt (1992) Balkans ( and 1999) Balkans ( and 1999) Balkans ( and 1999) Balkans ( and 1999) Aegean incidents (1996 and 2006) Aegean incidents (1996 and 2006) Aegean incidents (1996 and 2006) Aegean incidents (1996 and 2006) Kargil War (1999) Kargil War (1999) Kargil War (1999) Kargil War (1999) Operations in Afghanistan (2001-date) Operations in Afghanistan (2001-date) Operations in Afghanistan (2001-date) Operations in Afghanistan (2001-date) Invasion of Iraq and post-war operations (2003-date) Invasion of Iraq and post-war operations (2003-date) Invasion of Iraq and post-war operations (2003-date) Invasion of Iraq and post-war operations (2003-date) Second Lebanon War (2006) Second Lebanon War (2006) Second Lebanon War (2006) Second Lebanon War (2006) Operation Sun (2008) Operation Sun (2008) Operation Sun (2008) Operation Sun (2008)

General characteristics Length: 49 ft 5 in (14.8 m) WingspanWingspan: 32 ft 8 in (9.8 m) Wingspan Height: 16 ft (4.8 m) Wing area: 300 ft² (27.87 m²) AirfoilAirfoil: NACA 64A204 root and tip NACA 64A204 AirfoilNACA 64A204 Empty weight: 18,900 lb (8,670 kg) Loaded weight: 26,500 lb (12,000 kg) Max takeoff weightMax takeoff weight: 42,300 lb (19,200 kg) Max takeoff weight Powerplant: 1× Pratt & Whitney F100-PW-220 afterburning turbofan Pratt & Whitney F100turbofanPratt & Whitney F100turbofan

Maximum speedMaximum speed: Maximum speed At altitude: Mach 2+ (1,500 mph, 2,414 km/h) At altitude: Mach 2+ (1,500 mph, 2,414 km/h) Combat radius: 340 NM (295 mi, 550 km) on a hi-lo- hi mission with six 1,000 lb (450 kg) bombs NM At sea level: Mach 1.2 (915 mph, 1,470 km/h) At sea level: Mach 1.2 (915 mph, 1,470 km/h)Mach Ferry rangeFerry range: 2,280 NM (2,620 mi, 4,220 km) with drop tanks Ferry range Service ceilingService ceiling 50,000+ ft (15,200+ m) Service ceiling Rate of climbRate of climb: 50,000 ft/min (254 m/s) Rate of climb Wing loadingWing loading: 88.3 lb/ft² (431 kg/m²) Wing loading Thrust/weightThrust/weight: For F100 engine: 0.898, For F110: Thrust/weight

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