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Markings: HSL-49 "Scorpions" Naval Air Station, North Island San Diego CA .
Specifications (SH-60B)
General characteristics
Crew: 3-4
Capacity: 5 passengers in cabin or slung load of 6,000 lb or internal load of 4,100 lb for -B, -F and -H models and 11 passengers or slung load of 9,000 lb for -S
Length: 64 ft 8 in (19.75 m)
Rotor diameter: 53 ft 8 in (16.35 m)
Height: 17 ft 2 in (5.2 m)
Disc area: 2,262 ft² (210 m²)
Empty weight: 15,200 lb (6,895 kg)
Loaded weight: 17,758 lb (8,055 kg)
Useful load: 6,684 lb (3,031 kg)
Max takeoff weight: 21,884 lb (9,927 kg)
Powerplant: 2× General Electric T700-GE-401C turboshaft, 1,890 shp (1,410 kW) take-off power each
Performance
Maximum speed: 180 knots (333 km/h, 207 mph)
Cruise speed: 146 knots
Range: 450 nmi (834 km) at cruise speed
Service ceiling: 12,000 ft (3,580 m)
Rate of climb: 1,650 ft/min (8.38 m/s)
Armament
Up to three Mark 46 torpedo or Mark 50 torpedo,
AGM-114 Hellfire missile, 4 Hellfire missiles for SH-60B and HH-60H, 8 Hellfire missiles for MH-60S Block III.
AGM-119 Penguin missile (being phased out),
M60 machine gun or, M240 machine gun or GAU-16/A machine gun or GAU-17/A Minigun
Rapid Airborne Mine Clearance System (RAMICS) using Mk 44 Mod 0 30mm Cannon.
SH-60B Seahawk
The SH-60B maintained 83% commonality with the UH-60A.[4] The main changes are corrosion protection, more powerful T700 engines, shifting the tail landing gear 13 ft forward, replacing left side door with fuselage structure, and adding two weapon pylons. Other changes included larger fuel cells, an electric blade folding system, folding horizontal stabilators for storage, and adding a 25-tube pneumatic sonobuoy launcher on left side. Shifting the tail landing gear reduced the footprint for shipboard landing.
NETJETS SALES INC
Serial Number 258586
Specifications (Hawker 850XP)
General characteristics
Crew: 2 pilots
Capacity: 8 passengers typical, 13 maximum
Length: 51 ft 2 in (15.6 m)
Wingspan: 54 ft 4 in (16.5 m)
Height: 18 ft 1 in (5.5 m)
Empty weight: 15,670 lb (7,108 kg)
Max takeoff weight: 28,000 lb (12,701 kg)
Powerplant: 2× Honeywell TFE731-5BR turbofan, 4660 lbf () each
Performance
Maximum speed: 448 kts (514 mph) 830 km/h
Cruise speed: 402 kts (463 mph) 745 km/h
Range: 2,642 nm (4,893 km)
Service ceiling: 41,000 ft (12,497 m)
The Hawker 800 is a mid-size twin-engine corporate aircraft. It is a development of the British Aerospace BAe 125, and is currently assembled by Hawker Beechcraft.
The Hawker 800 is a derivative of the de Havilland 125. The British Aerospace Board sanctioned the programme to improve the, then current and strongly selling, BAe 125 700 series in April 1981. By May 1983 the new aircraft was ready for its first test flight.
The 800 series has a number of modifications and changes over the 700; most noticeable was the redesigned cockpit windscreen. Accompanying this are a modified rear fuselage fairing as well as a glass cockpit and uprated (from 3,700 to 4,300 lb) Garrett TFE731-5R-1H engines. British Aerospace also improved the wing by incorporating new outer wing sections. This helped to reduce drag and improve aerodynamic efficiency.
The 800 series would become a sales success. From the first BAe 125 flight in August 1961 it took nineteen years until the 500th airframe was sold. In a little over five years British Aerospace were registering the 200th sale of the 800 series.
The Hawker 800 is similar to most modern airframes in requiring sub-assemblies to be constructed away from the final point of manufacture. The fuselage sections, wings and control surfaces are manufactured and assembled in the UK in a combination of Hawker Beechcraft's own facility and those owned by Airbus UK, which inherited much of BAE System's civil aircraft manufacturing capacity. These sections are partially fitted out and installed with control surfacing and major systems before being shipped to Hawker Beechcraft's main manufacturing site in Wichita, Kansas for final assembly, fitting out and testing
In 1994 Beech Aircraft (which was also controlled by Raytheon) merged with Raytheon Corporate Jets to form Raytheon Aircraft. In March 2007, Raytheon Aircraft Company was sold to Hawker Beechcraft Corp., a company formed and controlled by GS Capital Partners (an affiliate of Goldman Sachs) and Onex Partners of Canada.
The current version is identified as the Hawker 850XP and was certified for operation in March 2006. The 850XP is identical to the 800XP except that it includes winglets which have extended its operating range by 100 nautical miles (190 km). This version also incorporates upgraded avionics and a redesigned interior. The Hawker 850XP essentially fills the gap left behind by the Hawker 1000 when production of that aircraft ceased.
Mesa Royale Apartments for Rent - Retirement Living in Mesa, AZ. Enjoy active senior living in Mesa, near Phoenix, at our retirement community. This photo is of our community putting greens. Learn more about our apartment community for 55+ seniors: Senior Retirement Living in Phoenix.
The Harrier II Plus is very similar to the Night Attack variant, with the addition of an APG-65 radar in an extended nose, making it capable of operating advanced missiles such as the AIM-120 AMRAAM. The radars were removed from early F/A-18 Hornets, which had been upgraded with the related APG-73. The Harrier II Plus is in service with the USMC,
Specifications (AV-8B+ Harrier II Plus)
AV-8 Harrier II being refueled by a KC-10 Extender.Data from Norden, Aerospaceweb
General characteristics
Crew: 1 pilot
Length: 46 ft 4 in (14.12 m)
Wingspan: 30 ft 4 in (9.25 m)
Height: 11 ft 8 in (3.55 m)
Wing area: 243.4 ft² (22.61 m²)
Airfoil: supercritical airfoil
Empty weight: 13,968 lb (6,340 kg)
Loaded weight: 22,950 lb (10,410 kg)
Max takeoff weight:
Rolling: 31,000 lb (14,100 kg)
Vertical: 20,755 lb (9,415 kg)
Powerplant: 1× Rolls-Royce F402-RR-408 (Mk 105) vectored-thrust turbofan, 23,500 lbf (105 kN)
Performance
Maximum speed: .89 Mach (662 mph, 1,070 km/h) at sea level
Range: 1,200 nm (1,400 mi, 2,200 km)
Combat radius: 300 nmi (556 km)
Ferry range: 1,800 nmi (3,300 km)
Rate of climb: 14,700 ft/min (4,485 m/min)
Wing loading: 94.29 lb/ft² (460.4 kg/m²)
Armament
Guns: 1× GAU-12U "Equalizer" 25 mm (0.98 in) cannon (left pod) and 300 rounds of ammunition (right pod)
Hardpoints: 7 with a capacity of 13,200 lb (STOVL) of stores, including gravity bombs, cluster bombs, napalm canisters, laser-guided bombs, AGM-65 Maverick or AGM-84 Harpoon missiles, a LITENING targeting pod, up to four AIM-9 Sidewinder or similar-sized infrared-guided missiles. Radar equipped AV-8B+ variants can carry up to four AIM-120 AMRAAM missiles. An upgrade program is currently fitting airframes with wiring and software to employ 1760 bus-based smart weapons, such as Joint Direct Attack Munitions,
Avionics
APG-65
Specifications (2005 model Tiger Aircraft AG-5B Tiger)
General characteristics
Crew: one, pilot
Capacity: 3 passengers
Length: 22 ft 0 in (6.7 m)
Wingspan: 31 ft 6 in (9.6 m)
Height: 8 ft 0 in (2.4 m)
Wing area: 140 ft² (13 m²)
Empty weight: 1,500 lb (680 kg)
Loaded weight: 2,400 lb (1090 kg)
Max takeoff weight: 2,400 lb (1090 kg)
Powerplant: 1× Lycoming O-360-A4K air-cooled, 4-cylinder, horizontally-opposed piston engine, 180 hp (134 kW)
Performance
Maximum speed: 143 knots (163 mph, 265 km/h)
Range: 686 nm (789 mi, 1,270 km)
Service ceiling: 13,800 ft (4,200 m)
Rate of climb: 850 ft/min (259 m/min)
Wing loading: 17.1 lb/ft² (83 kg/m²)
Power/mass: 0.08 hp/lb (0.12 kW/kg)
The US Grumman American AA-5 series is a family of all-metal, 4-seat, light aircraft used for touring and training. The line includes the original American Aviation AA-5 Traveler, the Grumman American AA-5 Traveler, AA-5A Cheetah, and AA-5B Tiger, the Gulfstream American AA-5A Cheetah, and AA-5B Tiger, the American General AG-5B Tiger, and the Tiger Aircraft AG-5B Tiger.
AA-5B Tiger
The final variant of the AA-5 line is the AA-5B Tiger. The Tiger was designed by Grumman engineers and was first produced in late 1974 as the 1975 model.
The Tiger was the outcome of the same redesign work on the AA-5 Traveler that resulted in the 150 hp (110 kW) Cheetah and it was originally little more than the same aircraft with a Lycoming O-360-A4K 180 hp (130 kW) engine, resulting in a 139-knot (257 km/h) cruise speed. Gross weight was increased from the AA-5/AA-5A's 2,200 lb (1,000 kg) to 2,400 lb (1,100 kg) on the Tiger. Externally the Tiger looked much like the AA-5 Traveler and AA-5A Cheetah so once again Grumman’s marketing department came up with a distinctive decal package to differentiate the design – this time a "galloping tiger".
While the earlier AA-1s and AA-5s did not change much from year to year the AA-5B Tiger underwent almost continual improvement. As with the AA-5A, the AA-5B was continued in production by Gulfstream when they purchased Grumman's American division. Gulfstream ceased production of all piston-engined aircraft in 1979 and the highly successful Tiger design went out of production after 1323 aircraft had been delivered.
[edit] AG-5B Tiger
For eleven years the design was not produced and then in the late 1980s a new company was formed to produce the Tiger. American General Aviation Corporation carried out further design improvements including introducing a new split nose bowl (engine cover) that could be removed without removing the propeller, a new instrument panel and improved exterior lighting, a new fuel quantity indication system, a 28 volt electrical system replacing the older 14 volt system, a new style throttle quadrant and improvements to the heat and ventilation systems. Aerodynamic improvements raised the optimal altitude cruise speed from 139 knots (257 km/h) true airspeed to 143 knots (265 km/h) TAS. The redesigned aircraft was put into production under an amended type certificate as the American General AG-5B Tiger. The new company had considered producing AA-1s and AA-5A Cheetahs, but those plans were never fulfilled before it closed its doors in 1993. American General produced Tigers for model years 1990-93 and delivered 181 aircraft in that time.
The design has a strong following amongst pilots and aircraft owners and so in 1999 a new company was formed to put the Tiger back into production. Tiger Aircraft LLC started production of the AG-5B Tiger in 2001 at their plant in Martinsburg, West Virginia. Tiger Aircraft did not produce any other models of the AA-1 or AA-5 family, although they owned the type certificates for the complete line of aircraft. Between 2001 and 2006 Tiger Aircraft produced 51 AG-5Bs. By the middle of 2006 Tiger Aircraft was experiencing financial problems and production of AG-5Bs had been halted and production workers laid off. [1] [2] Tiger Aircraft filed for bankruptcy in January 2007.[3]
On August 2, 2007 The Federal Bankruptcy Court approved the sale of Tiger Aircraft assets to True Flight Holdings LLC. True Flight has indicated its intention to produce parts and also return the AG-5B Tiger to production as soon as possible at a planned 60,000-square-foot (5,600 m2) facility on a 13 acre lot at the Valdosta, Georgia Airport.[4][5][6]
If True Flight Holdings does put the Tiger into production, they will be the fifth manufacturer to do so.
MArkings:Marine Attack Squadron 513 (VMA-513) is a United States Marine Corps attack squadron consisting of AV-8B Harrier (V/STOL) jets. Known as the "Flying Nightmares", the squadron is based at Marine Corps Air Station Yuma, Arizona and falls under the command of Marine Aircraft Group 13 (MAG-13) and the 3rd Marine Aircraft Wing (3rd MAW).
Specifications (AV-8B+ Harrier II Plus)
General characteristics
Crew: 1 pilot
Length: 46 ft 4 in (14.12 m)
Wingspan: 30 ft 4 in (9.25 m)
Height: 11 ft 8 in (3.55 m)
Wing area: 243.4 ft² (22.61 m²)
Airfoil: supercritical airfoil
Empty weight: 13,968 lb (6,340 kg)
Loaded weight: 22,950 lb (10,410 kg)
Max takeoff weight:
Rolling: 31,000 lb (14,100 kg)
Vertical: 20,755 lb (9,415 kg)
Powerplant: 1× Rolls-Royce F402-RR-408 (Mk 105) vectored-thrust turbofan, 23,500 lbf (105 kN)
Performance
Maximum speed: .89 Mach (662 mph, 1,070 km/h) at sea level
Range: 1,200 nm (1,400 mi, 2,200 km)
Combat radius: 300 nmi (556 km)
Ferry range: 1,800 nmi (3,300 km)
Rate of climb: 14,700 ft/min (4,485 m/min)
Wing loading: 94.29 lb/ft² (460.4 kg/m²)
Armament
Guns: 1× GAU-12U "Equalizer" 25 mm (0.98 in) cannon (left pod) and 300 rounds of ammunition (right pod) (American/Spanish/Italian configuration)
Hardpoints: 7 with a capacity of 13,200 lb (STOVL) of stores, including gravity bombs, cluster bombs, napalm canisters, laser-guided bombs, AGM-65 Maverick or AGM-84 Harpoon missiles, a LITENING targeting pod, up to four AIM-9 Sidewinder or similar-sized infrared-guided missiles. Radar equipped AV-8B+ variants can carry up to four AIM-120 AMRAAM missiles. An upgrade program is currently fitting airframes with wiring and software to employ 1760 bus-based smart weapons, such as Joint Direct Attack Munitions,
Avionics
APG-65
AV-8B Harrier II Night Attack
Fielded in 1991; incorporates a Navigation Forward Looking Infrared camera (NAVFLIR). Upgraded cockpit, including compatibility with night vision goggles. More powerful Rolls Royce Pegasus 11 engine
Poor '55 Chevy. This was once a complete restoration, but now in in less then fair shape. Either it's turned into a daily driver with no tender loving car or it just sits out in the elements 24-7. Somebody has riped the top and tried to pull it back.
VMA-513 Flying Nightmares
The Harrier II Plus is very similar to the Night Attack variant, with the addition of an APG-65 radar in an extended nose, making it capable of operating advanced missiles such as the AIM-120 AMRAAM. The radars were removed from early F/A-18 Hornets, which had been upgraded with the related APG-73. The Harrier II Plus is in service with the USMC,
Specifications (AV-8B+ Harrier II Plus)
AV-8 Harrier II being refueled by a KC-10 Extender.Data from Norden, Aerospaceweb
General characteristics
Crew: 1 pilot
Length: 46 ft 4 in (14.12 m)
Wingspan: 30 ft 4 in (9.25 m)
Height: 11 ft 8 in (3.55 m)
Wing area: 243.4 ft² (22.61 m²)
Airfoil: supercritical airfoil
Empty weight: 13,968 lb (6,340 kg)
Loaded weight: 22,950 lb (10,410 kg)
Max takeoff weight:
Rolling: 31,000 lb (14,100 kg)
Vertical: 20,755 lb (9,415 kg)
Powerplant: 1× Rolls-Royce F402-RR-408 (Mk 105) vectored-thrust turbofan, 23,500 lbf (105 kN)
Performance
Maximum speed: .89 Mach (662 mph, 1,070 km/h) at sea level
Range: 1,200 nm (1,400 mi, 2,200 km)
Combat radius: 300 nmi (556 km)
Ferry range: 1,800 nmi (3,300 km)
Rate of climb: 14,700 ft/min (4,485 m/min)
Wing loading: 94.29 lb/ft² (460.4 kg/m²)
Armament
Guns: 1× GAU-12U "Equalizer" 25 mm (0.98 in) cannon (left pod) and 300 rounds of ammunition (right pod)
Hardpoints: 7 with a capacity of 13,200 lb (STOVL) of stores, including gravity bombs, cluster bombs, napalm canisters, laser-guided bombs, AGM-65 Maverick or AGM-84 Harpoon missiles, a LITENING targeting pod, up to four AIM-9 Sidewinder or similar-sized infrared-guided missiles. Radar equipped AV-8B+ variants can carry up to four AIM-120 AMRAAM missiles. An upgrade program is currently fitting airframes with wiring and software to employ 1760 bus-based smart weapons, such as Joint Direct Attack Munitions,
Avionics
APG-65
BuNo165006 c/n 262McDonnell Douglas AV-8B(+)-21-MC Harrier II Plus
1997 Eurocopter AS 350 B2 (C/N): 3004 N945AE
Markings: Phi Inc. Lafayette, LA United States
The Eurocopter AS350 Ecureuil ("Squirrel") is a single-engined light helicopter originally manufactured by Aérospatiale (now part of Eurocopter Group). The AS350 is marketed in North America as the AStar. The AS355 Ecureuil 2 is a twin-engined variant, while the Eurocopter EC130 is a much-improved version of the AS350 airframe
Number of Seats: 6
Number of Engines: 1
Engine Manufacturer and Model: Turbomeca ARRIEL 1SER
AS350
Prototype.
AS350 Firefighter
Fire fighting version.
AS350B
Powered by one Turbomeca Arriel 1B engine.
AS350 B1
Powered by one Turbomeca Arriel 1D engine.
AS350 B2
Higher gross weight version powered by one Turbomeca Arriel 1D1 engine.
AS350 B3
High-performance version, is powered by a Turbomeca Arriel 2B engine equipped with a Full Authority Digital Engine Control (FADEC) system. This helicopter is the first ever to land on Mount Everest. Recently introduced AS350 B3/2B1 variant introduces enhanced engine with dual digital FADEC, dual hydraulics and a 2,370 kg (5,225 lb) M.T.O.W.
AS350 BA
Powered by a Turbomeca Arriel 1B engine and fitted with wider chord main rotor blades.
AS350 BB
AS350 B2 variant selected to meet rotary-wing training needs of UK MoD, through its Defence Helicopter Flying School in 1996. Powered by a derated Turbomeca Arriel 1D1 engine to improve the helicopters' life cycle.
Eurocopter Squirrel HT.1
Designation of AS350BB in operation with British RAF as a training helicopter.
Eurocopter Squirrel HT.2
Designation of AS350BB in operation with British Army Air Corps as a training helicopter.
AS350 C
Initial variant of Lycoming LTS-101-600A2 powered version developed for the North American market as the AStar. Quickly superseded by AS350D.
AS350 D
Powered by one Lycoming LTS-101 engine for the North American market as the AStar. At one stage marketed as AStar 'Mark III.'
AS350 L1
Military derivative of AS350 B1, powered by a 510-kW (684-shp) Turbomeca Arriel 1D turboshaft engine. Superseded by AS350 L2.
AS350 L2
Military derivative of AS350 B2, powered by a 546-kW (732-shp) Turbomeca Arriel 1D1 turboshaft engine. Designation superseded by AS550 C2.
HB350 B Esquilo
Unarmed military version for the Brazilian Air Force. Brazilian designations CH-50 and TH-50. Built under licence by Helibras in Brazil.
HB350 B1 Esquilo
Unarmed military version for the Brazilian Navy. Brazilian designation UH-12. Built under licence by Helibras in Brazil.
HB350 L1
Armed military version for the Brazilian Army. Brazilian designation HA-1. Built under licence by Helibras in Brazil.
Specifications (AS350 B3)
General characteristics
Crew: 1
Capacity: 6
Length: 12.94 m (42.45 ft)
Rotor diameter: 10.69 m (35.07 ft)
Height: 3.24 m (10.63 ft)
Empty weight: 1,241 kg (2,736 lbs)
Max takeoff weight: 2,250/2,570 kg (4,960/5,225 lbs)
Powerplant: 1× Turbomeca Arriel 2B or 2B1 turboshaft, 632 kW (847 shp)
Performance
Never exceed speed: 287 km/h (155 knots, 178 mph)
Cruise speed: 259 km/h (140 knots, 161 mph - Fast cruise (127 knots normal cruise speed).)
Range: 657 km (355 nm, 408 mi)
Service ceiling: 5,044 m (16,550 ft)
Rate of climb: 10.0 m/s (1,959 ft/min)
Markings of TW-2, Naval Air Station (NAS) Kingsville
BuNo:165644 cn:102
Specifications (T-45A)
General characteristics
Crew: 2 (student, instructor)
Length: 39 ft 4 in (11.99 m)
Wingspan: 30 ft 10 in (9.39 m)
Height: 13 ft 5 in (4.08 m)
Wing area: 190.1 ft² (17.7 m²)
Empty weight: 10,403 lb (4,460 kg)
Max takeoff weight: 14,081 lb (6,387 kg)
Powerplant: 1× Rolls-Royce Turbomeca F405-RR-401 (Adour) turbofan, 5,527 lbf (26 kN)
Performance
Maximum speed: 560 kt, 645 mph, 1,038 km/h
Range: 700 nmi (805 mi, 1288 km)
Service ceiling: 42,500 ft (12,950 m)
Rate of climb: 8,000 ft/min (40.6 m/s)
Armament
Usually none. One hardpoint under each wing can be used to carry practice bomb racks, rocket pods, or fuel tanks.
From Wikipedia, the free encyclopedia
The T-45 Goshawk is a highly modified version of the BAE Hawk land-based training jet aircraft. Manufactured by McDonnell Douglas (now Boeing) and British Aerospace (now BAE Systems), the T-45 is used by the United States Navy as an aircraft carrier-capable trainer.
The T-45's A and C models are currently in operational use. The T-45A, which became operational in 1991, contains an analog cockpit design while the newer T-45C, which was first delivered in December 1997, features a new digital "glass cockpit" design. All T-45A aircraft will eventually be converted to a T-45C configuration under the T-45 Required Avionics Modernization Program (T-45 RAMP).
T-45A
Two-seat basic and advanced jet trainer for the US Navy.
T-45B
Proposed land-based version for the US Navy, which would have been basically a conventional Hawk with a USN cockpit and no carrier capability. The USN had wanted the T-45B to get an earlier training capability, but abandoned the idea in 1984 in favor of less-costly updates to the TA-4 and T-2.
T-45C
Improved T-45A with glass cockpit, inertial navigation, and other improvements. Existing T-45As are being upgraded to the T-45C standard.
BuNo:165644 B/00
Interesting thing about this aircraft is that along with the double-nuts modex, it carries the name of the current CNATRA (Chief of Naval Air Training) on the canopy rail - Rear Admiral "Guad" Guadagnini. Pretty subdued for a boss-bird.
BuNo 165382 C/n B277
VMA-513 Flying Nightmares
The Harrier II Plus is very similar to the Night Attack variant, with the addition of an APG-65 radar in an extended nose, making it capable of operating advanced missiles such as the AIM-120 AMRAAM. The radars were removed from early F/A-18 Hornets, which had been upgraded with the related APG-73. The Harrier II Plus is in service with the USMC,
Specifications (AV-8B+ Harrier II Plus)
AV-8 Harrier II being refueled by a KC-10 Extender.Data from Norden, Aerospaceweb
General characteristics
Crew: 1 pilot
Length: 46 ft 4 in (14.12 m)
Wingspan: 30 ft 4 in (9.25 m)
Height: 11 ft 8 in (3.55 m)
Wing area: 243.4 ft² (22.61 m²)
Airfoil: supercritical airfoil
Empty weight: 13,968 lb (6,340 kg)
Loaded weight: 22,950 lb (10,410 kg)
Max takeoff weight:
Rolling: 31,000 lb (14,100 kg)
Vertical: 20,755 lb (9,415 kg)
Powerplant: 1× Rolls-Royce F402-RR-408 (Mk 105) vectored-thrust turbofan, 23,500 lbf (105 kN)
Performance
Maximum speed: .89 Mach (662 mph, 1,070 km/h) at sea level
Range: 1,200 nm (1,400 mi, 2,200 km)
Combat radius: 300 nmi (556 km)
Ferry range: 1,800 nmi (3,300 km)
Rate of climb: 14,700 ft/min (4,485 m/min)
Wing loading: 94.29 lb/ft² (460.4 kg/m²)
Armament
Guns: 1× GAU-12U "Equalizer" 25 mm (0.98 in) cannon (left pod) and 300 rounds of ammunition (right pod)
Hardpoints: 7 with a capacity of 13,200 lb (STOVL) of stores, including gravity bombs, cluster bombs, napalm canisters, laser-guided bombs, AGM-65 Maverick or AGM-84 Harpoon missiles, a LITENING targeting pod, up to four AIM-9 Sidewinder or similar-sized infrared-guided missiles. Radar equipped AV-8B+ variants can carry up to four AIM-120 AMRAAM missiles. An upgrade program is currently fitting airframes with wiring and software to employ 1760 bus-based smart weapons, such as Joint Direct Attack Munitions,
Avionics
APG-65
Boeing AV-8B+(R)-25-MC Harrier II Plus
165382 (VMA-513) suffered serious fuselage, wing, and tailplane
damage when collided with desert vegetation during nighttime
low-altitude at MCAS Yuma sometime in 2004. Was able to
land safely. Repaired and reported Oct 2007 with HMM-163