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Murphy Maverick

 

murphmave


Designed by Daryl Murphy, the Maverick is a side by side seated, high wing airplane has always had great appeal to a wide variety of flyers. From the every day pilot who likes to fly around his own patch to the outdoorsman or others who want to land in small strips, many pilots prefer the Maverick for it’s performance, visibility and visual appeal.

murphmave-2


The Design has been analyzed and tested to meet these Regulations:
1. Airworthiness Standards, Chapter 522 Subchapter C - Structures Gliders and Powered Gliders issued by: Transport Canada, Jan. 1986
2. European Joint Airworthiness Standards JAR 22 Subpart C - Structure
3. British Civil Airworthiness Requirements Section S Small Light Aeroplanes (CAP 482)
4. FAA - CFR - Part 23 Airworthiness Standards, Normal, Utility & Acrobatic Category Airplanes Subpart C-Structure, Jan. 1982
5. Canadian Advanced Ultralight Regulation TP 101.41.

The design is eligible for certification in the Normal Category at a Gross Weight of 950 lbs to all the above Standards. A lightweight version of the Rebel kitplane, the Maverick uses riveted shee construction, although the wings are partially fabric covered.

The Phoenix Aircraft Maverick PA is a further development of the Murphy Maverick from Canada. The Maverick PA is almost entirely built in Germany.

 

Gallery

 

Standard Wing
Engine: Rotax 503 53 hp
Propeller: GSC 68" GA
Power range: 53-65 HP
Wing span: 29' 5"
Gross weight: 950 lb
Empty weight: 395-460 lb
G-loading (normal): +5.7 -3.8
Length: 20' 8"
Fuselage width: 37"
Wing chord: 60"
Tail span: 106"
Airfoil: 4415 (Modified)
Gross Weight: 950 lb
Empty Weight: 395-420 lb
Useful Load: 530-555 lb
G Loading (Ultimate): +5.7 -3.8
Wing Area: 147 sq. ft
Power Loading: 17.9 lb./hp
Rate of Climb: 600 ft/min
Take Off Run: 150 ft
Landing Roll: 200 ft
Stall Speed: 32 mph
Vne: 120 mph
Top Speed: 95 mph
Cruise @ 75%: 80 mph
Fuel Capacity (std): 5 USG
Fuel Capacity (opt.): 14 USG
Fuel Burn @ 75%: 4 USG/hp
Range @ 75%: 280 sm
Service ceiling: 13,000 ft
Height: 6.42 ft
Seats: 2
Landing gear: tail wheel

Extended Wing
Engine: Rotax 503 53 hp
Propeller: GSC 68" GA
Power range: 53-65 HP
Wing span: 32' 5"
Gross weight: 950 lb
Empty weight: 395-460 lb
G-loading (normal): +5.7 -3.8
Length: 20' 8"
Fuselage width: 37"
Wing chord: 60"
Tail span: 106"
Airfoil: 4415 (Modified)
Gross Weight: 850 lb
Empty Weight: 395-420 lb
Useful Load: 430-455 lb
G Loading (Ultimate): +5.7 -3.8
Wing Area: 162 sq. ft
Power Loading: 16.0 lb./hp
Rate of Climb: 800 ft/min
Take Off Run: 100 ft
Landing Roll: 200 ft
Stall Speed: 28 mph
Vne: 120 mph
Top Speed: 90 mph
Cruise @ 75%: 75 mph
Fuel Capacity (std): 5 USG
Fuel Capacity (opt.): 14 USG
Fuel Burn @ 75%: 4 USG/hp
Range @ 75%: 262 miles
Top Speed: 110 mph
Cruise @ 75%: 85 mph
Fuel Capacity (std): 5 USG
Fuel Capacity (opt.): 14 USG
Fuel Burn @ 75%: 4.5 USG/hp
Range @ 75%: 264 sm

 

Engine: Rotax 503, 52 hp
Wing span: 10.15 m
Wing area: 15.06 sq.m
MAUW: 385 kg
Max speed: 145 kph
Cruise speed: 120 kph
Minimum speed: 50 kph
Climb rate: 3 m/s
Empty weight: 179 kg
Fuel capacity: 62 lt
Certification: PFA
Seats: 2
Fuel consumption: 14 lt/hr
Price (1998): $18,485
Kit price (1998): 114 900 Fttc

 

Standard Wing
Engine: Rotax 582 65 hp
Propeller: GSC 68" GA
Power range: 53-65 HP
Wing span: 29' 5"
Gross weight: 950 lb
Empty weight: 395-460 lb
G-loading (normal): +5.7 -3.8
Length: 20' 8"
Fuselage width: 37"
Wing chord: 60"
Tail span: 106"
Airfoil: 4415 (Modified)
Gross Weight: 950 lb
Empty Weight: 440-460 lb
Useful Load: 4 90-510 lb
G Loading (Ultimate): +5.7 -3.8
Wing Area: 147 sq. ft
Power Loading: 14.6 lb./hp
Rate of Climb: 900 ft/min
Take Off Run: 100 ft
Landing Roll: 200 ft
Stall Speed: 32 mph
Vne: 120 sm

Extended Wing
Engine: Rotax 582 65 hp
Propeller: GSC 68" GA
Power range: 53-65 HP
Wing span: 32' 5"
Gross weight: 950 lb
Empty weight: 395-460 lb
G-loading (normal): +5.7 -3.8
Length: 20' 8"
Fuselage width: 37"
Wing chord: 60"
Tail span: 106"
Airfoil: 4415 (Modified)
Gross Weight: 850 lb
Empty Weight: 440-460 lb
Useful Load: 390-410 lb
G Loading (Ultimate): +5.7 -3.8
Wing Area: 162 sq. ft
Power Loading: 13.1 lb./hp
Rate of Climb: 1200 ft/min
Take Off Run: 80 ft
Landing Roll: 200 ft
Stall Speed: 28 mph
Vne: 120 mph
Top Speed: 100 mph
Cruise @ 75%: 80 mph
Fuel Capacity (std): 5 USG
Fuel Capacity (opt.): 14 USG
Fuel Burn @ 75%: 4.5 USG/hp
Range @ 75%: 248 sm

Engine: HKS-700E
Cruise: 77 mph
ROC: 700 fpm
Stall: 20 mph.

Engine: Jabiru 2200, 80 hp
Empty wt: 487 lb
Max wt: 950 lb
Useful load: 463 lb
Stall: 30 mph
TO run: 100 ft
Ldg roll: 200 ft
Cruise 75%: 85 mph

Phoenix Aircraft Maverick PA
Engine: Rotax 582, 50 hp
HP range: 53-65
Stall: 32 kt / 37 mph / 60 kmh
Cruise: 76 kt / 87 mph / 140 kmh
VNE: 97 kt / 112 mph / 180 kmh
Empty Weight: 265 kg / 584 lbs
MTOW Weight: 472 kg / 1041 lbs Top speed: 110 mph
Stall: 32 mph
Range: 264 sm
Rate of climb: 900 fpm
Takeoff dist: 80 ft
Landing dist: 200 ft
Service ceiling: 13,000 ft
Fuel capacity: 5 USG
Height: 6.4 ft
Length: 20.7 ft
Wing span: 29.4 ft
Wing area: 147 sq.ft
Seats: 2
Landing gear: tailwheel

 

 

 


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