2013 MAI Performance Specs Jul202012REV2

2013 MAI Performance Specs Jul202012REV2

2013 Maule Aircraft Buyer's Guide
2099 Georgia Highway 133 South – Moultrie, GA 31788
Sales Phone (229) 985-2045 ext. 4930 – Fax (229) 890-2402
www.mauleairinc.com
MX-7 Series
MX-7 Series
Performance Specifications
Oleo Strut Gear
Aluminum Spring Gear
Nosewheel
MX-7-180B
MX-7-180C
MXT-7-180
180HP Models
Engine (Lycoming) (2000 hr. TBO):
0-360-C1F
0-360-C1F
0-360-C1F
2500 lbs. (1136 kg)
2500 lbs. (1136 kg)
2500 lbs. (1136 kg)
Empty Weight (avg.):
1438 lbs. (654 kg)
1483 lbs. (674 kg)
1528 lbs. (695 kg)
Useful Load (avg.):
1062 lbs. (483 kg)
1017 lbs. (462 kg)
972 lbs. (442 kg)
40 mph (35 kts)
40 mph (35 kts)
40 mph (35 kts)
300 ft. (92 m)
300 ft. (92 m)
300 ft. (92 m)
700 ft. (214 m)
700 ft. (214 m)
700 ft. (214 m)
1000 fpm (5.1 m/s)
1000 fpm (5.1 m/s)
1000 fpm (5.1 m/s)
900 ft. (274 m)
900 ft. (274 m)
900 ft. (274 m)
15,000 ft. (4572 m)
15,000 ft. (4572 m)
15,000 ft. (4572 m)
9 gph (34 lph)
9 gph (34 lph)
9 gph (34 lph)
138 mph (120 kts)
138 mph (120 kts)
138 mph (120 kts)
Gross Weight
Stall Speed (full flaps / power off / light weight)
Take Off, Ground Roll (light weight):
Take Off (light weight) over 50’ Obstacle:
Rate of Climb, Initial (light weight):
Landing (light weight) over 50’ Obstacle:
Service Ceiling:
Fuel Consumption (avg.) (US gals.)
(65% power):
Cruise (75% power / Opt. Alt.) (TAS):
Performance Observations are for One Person, 22 gals. Fuel, Sea Level, Standard Day Conditions (Do Not Use For Flight Planning)
MX-7 Series Aircraft Specifications
Engine (Lycoming):
0-360-C1F
Horsepower: 180
Wing Span:
32 ft. 11 in. (10.03 m)
Wing Area:
165.6 sq. ft. (15.39 sq. m)
Standard Propeller:
76" Hartzell 2 Blade Constant Speed
Length:
23 ft. 8 in. (7.21 m)
At Shoulders:
Front Seats
42 in. (1.07 m)
Passenger Seat
38 in. (0.97 m)
Main Gear Track:
6 ft. (1.83 m) Oleo Strut TW
7 ft. 10 in. (2.39 m) Aluminum Spring TW
7 ft. 8 in. (2.34 m) Nosewheel model
Rear Passenger Seat
33 in. (0.84 m)
At Hips:
37 in. (0.94 m)
34 in. (0.86 m)
28 in. (0.71 m)
Standard Fuel Capacity:
73 US gal. (276.3 l)
Cabin Width:
Flap Settings (degrees):
-7, 0, 24, 40, 48 Tailwheel
-7, 0, 24, 40 Nosewheel
Height:
6 ft. 4 in. (1.93 m) Tailwheel
8 ft. 4 in. (2.54 m) Nosewheel
Seating Configuration:
Four
Cargo Area (with rear seats removed):
Approximately 38 cubic feet
Performance That Counts!
Equipment and Options subject to change without notice. For Pricing Information please refer to the Maule Air, Inc. Aircraft Order Form
Available from your Authorized Maule Dealer
2012EFFJUL20REV2
1
2013 Maule Aircraft Buyer's Guide
2099 Georgia Highway 133 South – Moultrie, GA 31788
Sales Phone (229) 985-2045 ext. 4930 – Fax (229) 890-2402
www.mauleairinc.com
M-7 SERIES
Performance Specifications
Oleo Strut Gear
235HP Models
M-7 SERIES
Engine (Lycoming) (2000 hr. TBO):
Gross Weight
M-7-235B
M-7-235C
MT-7-235
0-540-B4B5
2500 lbs. (1136 kg)
I0-540-W1A5
2500 lbs. (1136 kg)
1605 lbs. (730 kg)
1653 lbs. (751 kg)
1665 lbs. (757 kg)
895 lbs. (407 kg)
847 lbs. (385 kg)
835 lbs. (380 kg)
40 mph (35 kts)
40 mph (35 kts)
40 mph (35 kts)
250 ft. (76 m)
250 ft. (76 m)
250 ft. (76 m)
Useful Load (avg.):
Stall Speed (full flaps / power off / light weight)
Take Off, Ground Roll (light weight):
Take Off (light weight) over 50’ Obstacle:
600 ft. (183 m)
600 ft. (183 m)
600 ft. (183 m)
1500 fpm (7.6 m/s)
1500 fpm (7.6 m/s)
1500 fpm (7.6 m/s)
Landing (light weight) over 50’ Obstacle:
Service Ceiling:
Nosewheel
0-540-B4B5
2500 lbs. (1136 kg)
Empty Weight (avg.):
Rate of Climb, Initial (light weight):
Aluminum Spring Gear
900 ft. (274 m)
900 ft. (274 m)
900 ft. (274 m)
20,000 ft. (6096 m)
20,000 ft. (6096 m)
20,000 ft. (6096 m)
12 gph (45 lph)
12 gph (45 lph)
11 gph (42 lph)
158 mph (137 kts)
158 mph (137 kts)
158 mph (137 kts)
Fuel Consumption (avg.) (US gals.) (65% power):
Cruise (75% power / Opt. Alt.) (TAS):
Performance Observations are for One Person, 22 gals. Fuel, Sea Level, Standard Day Conditions (Do Not Use For Flight Planning)
Engine (Lycoming):
O-540-B4B5
IO-540-W1A5
Horsepower:
235
Standard Propeller:
81" McCauley 2 Blade Constant Speed
O-540-B4B5 & IO-540-W1A5
O-540-B4B5 & IO-540-W1A5
Wing Span:
32 ft. 11 in. (10.03 m)
Wing Area:
165.6 sq. ft. (15.39 sq. m)
Standard Fuel Capacity:
73 US gal. (276.3 l)
Flap Settings (degrees):
-7, 0, 24, 40, 48 Tailwheel
-7, 0, 24, 40 Nosewheel
Length:
23 ft. 8 in. (7.21 m)
Height:
6 ft. 4 in. (1.93 m) Tailwheel
8 ft. 4 in. (2.54 m) Nosewheel
Main Gear Track:
6 ft. (1.83 m) Oleo Strut TW
7 ft. 10 in. (2.39 m) Aluminum Spring TW
7 ft. 8 in. (2.34 m) Nosewheel model
Seating Configuration:
4 + 1 (optional 5th seat)
Cabin Width:
Front Seats
Passenger Seat
Rear Passenger Seat
At Shoulders:
42 in. (1.07 m)
38 in. (0.97 m)
33 in. (0.84 m)
At Hips:
37 in. (0.94 m)
34 in. (0.86 m)
28 in. (0.71 m)
Cargo Area (with rear seats removed):
Approximately 42 cubic feet
Performance That Counts!
Equipment and Options subject to change without notice. For Pricing Information please refer to the Maule Air, Inc. Aircraft Order Form
Available from your Authorized Maule Dealer
2012EFFJUL20REV2
2
2013 Maule Aircraft Buyer's Guide
2099 Georgia Highway 133 South – Moultrie, GA 31788
Sales Phone (229) 985-2045 ext. 4930 – Fax (229) 890-2402
www.mauleairinc.com
M-7 SERIES
Performance Specifications
Oleo Strut Gear
260HP Models
M-7 SERIES
Engine (Lycoming) (2000 hr. TBO):
Gross Weight
M-7-260
M-7-260C
MT-7-260
I0-540-V4A5
2500 lbs. (1136 kg)
I0-540-V4A5
2500 lbs. (1136 kg)
1610 lbs. (732 kg)
1671 lbs. (760 kg)
1696 lbs. (771 kg)
890 lbs. (405 kg)
829 lbs. (377 kg)
804 lbs. (366 kg)
40 mph (35 kts)
40 mph (35 kts)
40 mph (35 kts)
250 ft. (76m)
250 ft. (76m)
250 ft. (76m)
Useful Load (avg.):
Stall Speed (full flaps / power off / light weight)
Take Off, Ground Roll (light weight):
Take Off (light weight) over 50’ Obstacle:
600 ft. (183 m)
600 ft. (183 m)
600 ft. (183 m)
1650 fpm (8.4 m/s)
1650 fpm (8.4 m/s)
1650 fpm (8.4 m/s)
Landing (light weight) over 50’ Obstacle:
Service Ceiling:
900 ft. (274 m)
900 ft. (274 m)
900 ft. (274 m)
20,000 ft. (6096 m)
20,000 ft. (6096 m)
20,000 ft. (6096 m)
14 gph (53 lph)
14 gph (53 lph)
14 gph (53 lph)
162 mph (141 kts)
162 mph (141 kts)
162 mph (141 kts)
Fuel Consumption (avg.) (US gals.) (65% power):
Cruise (75% power / Opt. Alt.) (TAS):
Nosewheel
I0-540-V4A5
2500 lbs. (1136 kg)
Empty Weight (avg.):
Rate of Climb, Initial (light weight):
Aluminum Spring Gear
Performance Observations are for One Person, 22 gals. Fuel, Sea Level, Standard Day Conditions (Do Not Use For Flight Planning)
Engine (Lycoming):
IO-540-V4A5
Horsepower:
260
Wing Span:
32 ft. 11 in. (10.03 m)
Wing Area:
165.6 sq. ft. (15.39 sq. m)
Standard Fuel Capacity:
73 US gal. (276.3 l)
Standard Propeller:
78" McCauley 2 Blade Constant Speed
Flap Settings (degrees):
-7, 0, 24, 40, 48 Tailwheel
-7, 0, 24, 40 Nosewheel
Length:
23 ft. 8 in. (7.21 m)
Height:
6 ft. 4 in. (1.93 m) Tailwheel
8 ft. 4 in. (2.54 m) Nosewheel
Main Gear Track:
6 ft. (1.83 m) Oleo Strut TW
7 ft. 10 in. (2.39 m) Aluminum Spring TW
7 ft. 8 in. (2.34 m) Nosewheel model
Seating Configuration:
4 + 1 (optional 5th seat)
Cargo Area (with rear seats removed):
Approximately 42 cubic feet
Cabin Width:
Front Seats
Passenger Seat
Rear Passenger Seat
At Shoulders:
42 in. (1.07 m)
38 in. (0.97 m)
33 in. (0.84 m)
At Hips:
37 in. (0.94 m)
34 in. (0.86 m)
28 in. (0.71 m)
Performance That Counts!
Equipment and Options subject to change without notice. For Pricing Information please refer to the Maule Air, Inc. Aircraft Order Form
Available from your Authorized Maule Dealer
2012EFFJUL20REV2
3
2013 Maule Aircraft Buyer's Guide
2099 Georgia Highway 133 South – Moultrie, GA 31788
Sales Phone (229) 985-2045 ext. 4930 – Fax (229) 890-2402
www.mauleairinc.com
MAULE M-9-235
M-9-235 Performance Specifications
Gross Weight
2800 lbs. (1270 kg)
Empty Weight (Standard Aircraft):
1700 lbs. (771 kg)
Useful Load (Standard Aircraft):
1100 lbs. (499 kg)
Stall Speed (full flaps / power off / @ 2800) (IAS)
46 mph (40 kts)
Take Off, Ground Roll (@ 2800 lbs.):
406 ft. (124 m)
Take Off (@ 2800 lbs.) over 50’ Obstacle:
791 ft. (242 m)
Landing (@ 2800 lbs.) over 50’ Obstacle:
900 ft. (274 m)
Service Ceiling:
20,000 ft. (6096 m)
Fuel Consumption (avg. @ 65% power):
Cruise (75% power / Opt. Alt.) (TAS):
11 gph (42 lph)
158 mph (137 kts)
Performance Observations are from Certification Flight Test - Sea Level, Standard Day Conditions
(Do Not Use For Flight Planning)
M-9-235 Aircraft Specifications
Engine (Lycoming):
I0-540-W1A5
Horsepower:
235
Standard Propeller:
80" McCauley 3 Blade Constant Speed
Wing Span:
32 ft. 11 in. (10.03 m)
Wing Area:
165.6 sq. ft. (15.39 sq. m)
Length:
23 ft. 8 in. (7.21 m)
Height:
6 ft. 4 in. (1.93 m)
Fuel Capacity:
85 US gal. (321.7 l)
Flap Settings (degrees):
-7, 0, 24, 40, 48
Main Gear Track:
7 ft. 10 in. (2.39 m)
Seating Configuration:
4 + 1 (optional 5th seat)
Cabin Width:
Front Seats
Passenger Seat
Rear Passenger Seat
At Shoulders:
42 in. (1.07 m)
38 in. (0.97 m)
33 in. (0.84 m)
At Hips:
37 in. (0.94 m)
34 in. (0.86 m)
28 in. (0.71 m)
Cargo Area (with rear seats removed):
Approximately 42 cubic feet
Performance That Counts!
Equipment and Options subject to change without notice. For Pricing Information please refer to the Maule Air, Inc. Aircraft Order Form
Available from your Authorized Maule Dealer
2012EFFJUL20REV2
4