Hoover Dam and The Mike O'Callaghan – Pat Tillman Memorial Bridge / Hoover Dam Bypass

Gassing up for L. A. @ Primm Valley Resorts and Casinos in Nevada.

View from hotel room in Cin Sity

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.

Gassing up for L. A. @ Primm Valley Resorts and Casinos in Nevada.

Our rest stop in Cin Sity

Marine Attack Squadron 311 (VMA-311) is a United States Marine Corps fighter squadron known as the "Tomcats", 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).

BuNo:

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)

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

Mesa, AZ on 1/20/2017 Friday. This is the entrance to the unisex bathroom.

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: 559th Flying Training Squadron (559 FTS) "Billy Goats" is part of the 12th Flying Training Wing based at Randolph Air Force Base, Texas

Sn:07-0868

Specifications (T-6A)

General characteristics

Crew: 2, tandem seating

Length: 33 ft 4 in (10.2 m)

Wingspan: 33 ft 5 in (10.2 m)

Height: 10 ft 8 in (3.3 m)

Empty weight: 4,900 lb (2,087 kg)

Loaded weight: 6,550 lb (2,971 kg)

Max takeoff weight: 6,500 lb (2,958 kg)

Powerplant: 1× Pratt & Whitney Canada PT6A-68 turboprop, 1,100 shp (820 kW)

Performance

Maximum speed: 316 knots IAS (Mach 0.67 at high altitude, 585 km/h)

Range: 850 nm (1,575 km)

Service ceiling: 31,000 ft (9,448 m)

Rate of climb: 4,500 ft/min (1,372 m/min)

The Beechcraft T-6 Texan II is a single-engined turboprop aircraft built by the Raytheon Aircraft Company (now Hawker Beechcraft). It is used by the United States Air Force for basic pilot training and by the United States Navy for Primary and Intermediate Joint Naval Flight Officer (NFO) and Air Force Navigator / Weapon Systems Officer (WSO) training. It is replacing the Air Force's T-37B Tweet and the Navy's T-34C Turbo Mentor. The T-6A is also used as a basic trainer by the Canadian Forces (CT-156 Harvard II) and the Greek Air Force.

Variants

T-6A Texan II

Standard version for the USAF, USN, and Hellenic Air Force (25).

T-6A NTA Texan II

Armed version of the T-6A for the HAF (20). T-6A NTA has the capability to carry rocket pods, gun pods, external fuel tanks, and bombs.

T-6B Texan II

Upgraded version with a digital glass cockpit that includes a Head-Up Display (HUD), six multi-function displays (MFD) and Hands On Throttle And Stick (HOTAS).[9]

AT-6B Texan II

Armed version of the T-6B for primary weapons training or light attack roles. It has the same digital cockpit, but upgraded to include datalink and integrated electro-optical sensors along with several weapons configurations.[10]

CT-156 Harvard II

Version of the T-6A for NTFC with the Canadian Forces; Cockpit layoutbased on that of the CT-155 Hawk.

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: Native Air

Serial Number 9015

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)

MFR Year 2000

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 entrance. Learn more about our apartment community for 55+ seniors: Senior Retirement Living in Phoenix.

Loaded and headed to a fire.

The follow-on to the successful TBM Avenger (WW2 Torpedo bomber), the AF-2S Guardian was designed to work in pairs to attack and destroy enemy submarines. One aircraft had a look down radar (installed in the belly) and the second plane had the weapons to launch the attack.

Taxiing in.

Hoover Dam and The Mike O'Callaghan – Pat Tillman Memorial Bridge / Hoover Dam Bypass

SkiPro Rail Jam 2012

The Growler is a variant of the F/A-18E/F. It is designed to replace the EA-6 Prowler that is starting to be retired from active duty.

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)

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 swimming pool. Learn more about our apartment community for 55+ seniors: Senior Retirement Living in Phoenix.

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)

Rotating on the way to the Dean Peak Fire near Kingman, Arizona.

Hyper-kool architectural designs in Cin Sity

Cin Sity

Markings: MARQUIS JET HOLDINGS INC,OKLAHOMA CITY ,OKLAHOMA .

Serial Number RK-520

Specifications (Hawker 400XP)

General characteristics

Crew: 2 pilots

Capacity: 7 passengers

Length: 48 ft 5 in (14.8 m)

Wingspan: 43 ft 6 in (13.3 m)

Height: 13 ft 11 in (4.2 m)

Empty weight: 10,550 lb (4,786 kg)

Max takeoff weight: 16,300 lb (7,394 kg)

Powerplant: 2× Pratt & Whitney Canada JT15D-5 , 2965 lbf () each

Performance

Maximum speed: 450 kts (518 mph) 833 km/h

Cruise speed: 414 kts (476 mph) 767 km/h

Range: 1,482 nm (2,744 km)

Service ceiling: 45,000 ft (13,716 m)

The Hawker 400 is a small twin-engine corporate aircraft, designed by Raytheon's Beech Aircraft Company subsidiary, now part of Hawker Beechcraft.

The aircraft was originally designed as the Mitsubishi MU-300 Diamond, an all-new, all-jet development to complement and slot above the Mitsubishi MU-2 and provide Mitsubishi Heavy Industries with their top-of-the-line corporate aircraft model (hence the name "Diamond")[1]. Beechcraft bought the production rights and began manufacturing it as their own model, initially redesignated as the Beechjet 400. The Beechjet 400 was certified by the FAA in May 1985.

Raytheon/Beechcraft steadily developed their own improvements to the model, leading to the 400A in 1990. Improvements in the 400A include longer range, higher take-off weights and improved luxury appointments. An all-glass flight deck was also offered. Beechcraft also developed a version for the United States Air Force known as the T-1A Jayhawk, used as a trainer for large aircraft crews (such as tankers and strategic transports). A total of 180 T-1A trainers were delivered between 1992-1997. Another military variant is the Japan Air Self-Defense Force T-400 trainer which shares the same Type Certificate as the T-1A.[2]

In 1993 Raytheon purchased the Hawker business jet product line from British Aerospace. The Beechjet 400 was eventually renamed the Hawker 400 to map it into the Hawker product line. The Hawker 400XP incorporates further aerodynamic, mechanical and interior improvements gleaned from the Hawker 800XP.

In October 2008, Hawker Beechcraft announced upgrades to the design, resulting in the new model designation Hawker 450XP.[citation needed] Upgrades include new, more fuel efficient engines (Pratt & Whitney PW535D models with 2,965 pounds of thrust apiece) Collins Pro Line 21 avionics and Collins Venue cabin management/entertainment system and a complete interior upgrade.[

MFR Year 2007

Boulder City / Lake Mead area

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)

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 gardens. Learn more about our apartment community for 55+ seniors: Senior Retirement Living in Phoenix.

Air tanker lead plane climbing out.

Hoover Dam and The Mike O'Callaghan – Pat Tillman Memorial Bridge / Hoover Dam Bypass

Hyper-kool architectural designs in Cin Sity

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: Omniflight

N4204

Serial Number 4204

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)

MFR Year 2007

The sign at the front of the Glendale 9 Drive-In Theater

The Mike O'Callaghan – Pat Tillman Memorial Bridge / Hoover Dam Bypass

Cin Sity

Marine Attack Squadron 311 (VMA-311) is a United States Marine Corps fighter squadron known as the "Tomcats", 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).

BuNo:

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)

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

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

Hoover Dam and The Mike O'Callaghan – Pat Tillman Memorial Bridge / Hoover Dam Bypass

Headed to Las Vegas

This sign mimics the famous marquee at Chicago's Wrigley Field.

I thought the bright colors in front of the stormy could were awesome. The is a teen couple standing on the back platform. No children. Kind of symbolic of days gone by.