The USAF developed a requirement for a new air superiority fighter to replace the F-15 Eagle.
Advanced Tactical Fighter (ATF). The aircraft is constructed using 39% titanium, 24% composite
material, 16% aluminum and 1% thermoplastic by weight. All these components contribute to the
F-22 being a light weight, extremely maneuverable, extremely fast aircraft that uses stealth
technology. The F-22 is also capable of ground attack, electronic warfare and signals intelligence.

Lockheed F-22A Raptor 02-4040 “The Pride Of Bay County” was delivered on March 22, 2005
and then in 2006 was assigned to the 43rd FS “Hornets” as part of the 325 FW located at
Tyndale AFB. The 43rd FS received the first F-22 in 2003 and its primary function is to provide
F-22 pilots with advanced air-dominance training. The 43rd FS was organized in 1917 and saw
combat during WW I, WW II, Vietnam and formed part of the Alaskan Air Command during the
Cold War.

Planned Production - 750 aircraft initial program objective

Altered plan in 1990 - 648 aircraft

Altered plan in 1994 - 442 aircraft

In 1997 Department of Defense report – 339 aircraft

In 2006 the Pentagon wanted -183 aircraft

2008 approval for 4 additional aircraft bringing the total to 187

Number built as of August 2009 - 145 (187 planned)

Role - Air superiority fighter

Crew – (1) pilot

Performance
Engines – (2) Pratt & Whitney F119-PW-100 engines producing 35,000 lbst of thrust
Speed - Mach 1.8 (super cruise: Mach 1.5)
G Limit - +9 G
Ceiling - 60,000 ft   (18,290 m)
The F-22 and other fighters can reach this altitude, but only the F-22 can perform tactical
maneuvers at this level, which is about twice the altitude at which other jets can perform tactical
maneuvers.

Dimensions
Length - 62.08 ft   (18.90 m)
Height -16.67 ft   (5.08 m)
Wingspan - 44.5 ft   (13.56 m)
Wing Area - 840 sq ft   (78.04 sq m)
Horizontal Tail-span - 29 ft   (8.84 m)

Weights
Empty Weight - 31,670 lb   (14,365 kg)
Maximum Takeoff Weight - 60,000 lb   (27,000 kg)

Armament
Internal
(1) 20mm Cannon
(4) AIM-9 Sidewinders (side weapon bays)
(4) AIM-120A AMRAAM (internal ventral bay)
(6) AIM-120Cs (internal ventral bay)
(6) GBU-32 JDAM PGMs (internal ventral bay)
(8) GBU-39 Small Diameter Bombs (250lbs ea)
External
(4) under-wing hard-points with a maximum of 5,000lbs   (2,270kg) of mission-specific weaponry
or fuel drop-tanks.

This new site is being updated regularly and it will be much improved before too long. Please be patient, give it time, and check back regularly. Opportunities for community collaboration are in the works for a little further down the road.