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The East Valley Regional Cadet Program (EVRC) is a fun and exciting opportunity for youth to participate in an educational program that is challenging yet, rewarding! The EVRC Program is supported by Mesa Fire & Medical Department and it's regional partners such has Gilbert Fire & Rescue, Superstition Fire & Medical District, and Queen Creek Fire & Medical Department. It is designed for youth between the ages of 14-18 interested in developing their leadership and teamwork skills.
www.mesaaz.gov/residents/fire-medical/divisions-sections/...
Markings of TW-2, Naval Air Station (NAS) Kingsville
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.
Markings: 445th Flight Test Squadron (445 FLTS) is part of the 412th Test Wing and is based at Edwards Air Force Base, California.
SN:60-0582
Technical Specifications
Wingspan 25 ft 3 in
Length 44 ft 2 in
Height 12 ft 10 in
Weight 11,550 lbs (loaded)
Maximum Speed 820 mph
Service Ceiling 42,400 ft
Range 1,135 miles
Engines 2 General Electric J85-GE-5 turbojets 3,850 lbs thrust
Crew 2
Northrop T-38A-35-NO Talon 60-0582 to US Navy as NT-38A
Serial Number 22-1181
MFR Year 1975
LYCOMING
Engine Model LYCOMING I0360
M20F & M20G
Mooney stretched the fuselage and added a third fuselage side window for the first time with the M20F Executive 21, which was produced between 1966–1977. The M20F is otherwise similar to the M20E.
The M20G Statesman, produced 1968–1970, was a stretched M20C incorporating the carburated 180hp engine. Many M20G owners later converted to the 200hp engine.[citation needed]
In 1969 Mooney made electrically-operated landing gear and flaps standard across all its aircraft. Prior to that, pilots extended and retracted the standard landing gear using a heavy metal Johnson bar. Electrically-extended landing gear was an option.[citation needed]
The M20F was type certified on 25 July 1965 with the M20G following on 13 November 1967.[
Markings of TW-2, Naval Air Station (NAS) Kingsville
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.
Chartered C-172 today to shoot projects. Good pilot Aaron Grissum with Classic Air Aviation got us into Phoenix surface area. December 12, 2012 © Artist in the Sky, LLC
Markings of TW-2, Naval Air Station (NAS) Kingsville
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.
Markings: 62nd AW, 446th Airlift Wing, McChord Air Force Base, Wash
SN: 98-0057
Specifications (C-17)
General characteristics
Crew: 3: 2 pilots, 1 loadmaster
Capacity:
102 troops with standard centerline seats or
134 troops with palletized seats or
36 litter and 54 ambulatory patients
Payload: 170,900 lb (77,519 kg) of cargo distributed at max over 18 463L master pallets or a mix of palletized cargo and vehicles
Length: 174 ft (53 m)
Wingspan: 169.8 ft (51.75 m)
Height: 55.1 ft (16.8 m)
Wing area: 3,800 ft² (353 m²)
Empty weight: 282,500 lb (128,100 kg)
Max takeoff weight: 585,000 lb (265,350 kg)
Powerplant: 4× Pratt & Whitney F117-PW-100 turbofans, 40,440 lbf (180 kN) each
Fuel capacity: 35,546 US gal (134,556 L)
Performance
Cruise speed: Mach 0.76 (450 knots, 515 mph, 830 km/h)
Range: 2,420 nmi[87] (2,785 mi, 4,482 km)
Service ceiling: 45,000 ft (13,716 m)
Max wing loading: 150 lb/ft² (750 kg/m²)
Minimum thrust/weight: 0.277
Boeing C-17A Lot X Globemaster III 98-0057 c/n P-57 was with 97th AMW at Altus but noted as 62nd AW McChord. Hit by missile nearBaghdad Apt, Iraq Dec 9, 2003, but was able to land safely.Returned to McChord AFB Jan 3, 2004 for repair.
Markings: 445th Flight Test Squadron (445 FLTS) is part of the 412th Test Wing and is based at Edwards Air Force Base, California.
SN:60-0582
Technical Specifications
Wingspan 25 ft 3 in
Length 44 ft 2 in
Height 12 ft 10 in
Weight 11,550 lbs (loaded)
Maximum Speed 820 mph
Service Ceiling 42,400 ft
Range 1,135 miles
Engines 2 General Electric J85-GE-5 turbojets 3,850 lbs thrust
Crew 2
Northrop T-38A-35-NO Talon 60-0582 to US Navy as NT-38A
Markings of TW-2, Naval Air Station (NAS) Kingsville
BuNo 163621
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.
The 90th Flying Training Squadron (90 FTS) is part of the 80th Flying Training Wing based at Sheppard Air Force Base, Texas. It operates T-38 Talon aircraft conducting flight training.
Origanl built as T-38A-65-NO
Markings of TW-2, Naval Air Station (NAS) Kingsville
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.
Markings: 729th Airlift Squadron (729 AS) is part of the 452d Air Mobility Wing (452d AMW) is an Air Force Reserve Command (AFRC) air mobility unit located at March ARB, California. It is operationally gained by the Air Mobility Command (AMC).
05- 5142
Specifications (C-17)
General characteristics
Crew: 3: 2 pilots, 1 loadmaster
Capacity:
102 troops with standard centerline seats or
134 troops with palletized seats or
36 litter and 54 ambulatory patients
Payload: 170,900 lb (77,519 kg) of cargo distributed at max over 18 463L master pallets or a mix of palletized cargo and vehicles
Length: 174 ft (53 m)
Wingspan: 169.8 ft (51.75 m)
Height: 55.1 ft (16.8 m)
Wing area: 3,800 ft² (353 m²)
Empty weight: 282,500 lb (128,100 kg)
Max takeoff weight: 585,000 lb (265,350 kg)
Powerplant: 4× Pratt & Whitney F117-PW-100 turbofans, 40,440 lbf (180 kN) each
Fuel capacity: 35,546 US gal (134,556 L)
Performance
Cruise speed: Mach 0.76 (450 knots, 515 mph, 830 km/h)
Range: 2,420 nmi[87] (2,785 mi, 4,482 km)
Service ceiling: 45,000 ft (13,716 m)
Max wing loading: 150 lb/ft² (750 kg/m²)
Minimum thrust/weight: 0.277
Boeing C-17A Globemaster III Lot XV
CN:P-142
Markings of TW-2, Naval Air Station (NAS) Kingsville
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.
FUEL FRESH INC ,PHOENIX, Arizona
Serial Number 104633
CN:5303
Technical Specifications
Wingspan 21.94 ft
Length 54.77 ft
Height 13.49 ft
Weight 24,388 lbs (loaded)
Maximum Speed Mach 2
Service Ceiling 57,500 ft
Range 1,388 miles
Engines 1 Canadian-built J79-OEL-7 engines
Crew 2
5303 (104633) to Norway in 1973. WFU Dec 1982. Now on US civil
registry as N104JR
25th Flying Training Squadron (25 FTS) is part of the 71st Flying Training Wing based at Vance Air Force Base, Oklahoma.
VT-7 of TW-1 at Naval Air Station Meridian.
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.
Markings:UND AEROSPACE FOUNDATION, GRAND FORKS ,ND
Serial Number 2844024
Specifications (1964 model PA-28-140 Cherokee 140)
General characteristics
Crew: one pilot
Capacity: three passengers
Length: 23.3 feet (7.16 m)
Wingspan: 30.0 feet (9.2 m)
Height: 7.3 feet (2.25 m)
Wing area: 160 sq ft (15.14 m²)
Airfoil: NACA 652-415
Empty weight: 1201 lb (544 kg)
Loaded weight: 2150 lb (975 kg)
Useful load: 949 lb (430 kg)
Max takeoff weight: 2150 lb (975 kg)
Powerplant: 1× Lycoming O-320-E2A Sensenich M74DM, 150 hp (113 kW)
Propeller diameter: 74 inches (1.9 m)
Performance
Maximum speed: 123 knots (142 mph, 230 km/h)
Cruise speed: 108 knots (124 mph (200 km/h), 201 km/h)
Stall speed: 47 knots (54 mph, 87 km/h)
Range: 465 nm (535 sm, 867 km)
Service ceiling: 14,300 feet (4400 m)
Rate of climb: 660 ft/min (3.4 m/s)
Wing loading: 13.4 lb/sq ft (64.4 kg/sq m)
Power/mass: 14.3 lb/hp (0.116 kW/kg)
New Piper Aircraft
The original Piper Aircraft company declared bankruptcy in 1991. In 1995, The New Piper Aircraft company was created. It was renamed Piper Aircraft once again in 2006. The company produces three PA-28 Cherokee variants: the 160 horsepower (119 kW) Warrior III (PA-28-161), the 180 horsepower (134 kW) Archer III (PA-28-181), and the 200 horsepower (149 kW) retractable Arrow (PA-28R-201). All are now available with Avidyne Entegra glass cockpits.
The view from right field. The berms at Sloan Park look like a pleasant place to spread out a blanket and watch the game. The berm would be completely full by game time.
Markings: 62nd AW, 446th Airlift Wing, McChord Air Force Base, Wash
SN: 02-1104
Specifications (C-17)
General characteristics
Crew: 3: 2 pilots, 1 loadmaster
Capacity:
102 troops with standard centerline seats or
134 troops with palletized seats or
36 litter and 54 ambulatory patients
Payload: 170,900 lb (77,519 kg) of cargo distributed at max over 18 463L master pallets or a mix of palletized cargo and vehicles
Length: 174 ft (53 m)
Wingspan: 169.8 ft (51.75 m)
Height: 55.1 ft (16.8 m)
Wing area: 3,800 ft² (353 m²)
Empty weight: 282,500 lb (128,100 kg)
Max takeoff weight: 585,000 lb (265,350 kg)
Powerplant: 4× Pratt & Whitney F117-PW-100 turbofans, 40,440 lbf (180 kN) each
Fuel capacity: 35,546 US gal (134,556 L)
Performance
Cruise speed: Mach 0.76 (450 knots, 515 mph, 830 km/h)
Range: 2,420 nmi[87] (2,785 mi, 4,482 km)
Service ceiling: 45,000 ft (13,716 m)
Max wing loading: 150 lb/ft² (750 kg/m²)
Minimum thrust/weight: 0.277
Boeing C-17A Lot XIV Globemaster III Cn: P-104
Markings: 445th Flight Test Squadron (445 FLTS) is part of the 412th Test Wing and is based at Edwards Air Force Base, California.
SN:60-0582
Technical Specifications
Wingspan 25 ft 3 in
Length 44 ft 2 in
Height 12 ft 10 in
Weight 11,550 lbs (loaded)
Maximum Speed 820 mph
Service Ceiling 42,400 ft
Range 1,135 miles
Engines 2 General Electric J85-GE-5 turbojets 3,850 lbs thrust
Crew 2
Northrop T-38A-35-NO Talon 60-0582 to US Navy as NT-38A
The East Valley Regional Cadet Program (EVRC) is a fun and exciting opportunity for youth to participate in an educational program that is challenging yet, rewarding! The EVRC Program is supported by Mesa Fire & Medical Department and it's regional partners such has Gilbert Fire & Rescue, Superstition Fire & Medical District, and Queen Creek Fire & Medical Department. It is designed for youth between the ages of 14-18 interested in developing their leadership and teamwork skills.
www.mesaaz.gov/residents/fire-medical/divisions-sections/...