adventure awaits · pdf file235 hp carbureted 260 hp fuel injected m-7-235b m-7-260 engine...

2013 MAULE AIRCRAFT SELECTION GUIDE 2099 Georgia Highway 133 South – Moultrie, GA 31788

www.mauleairinc.com Aircraft Sales Phone (229) 985-2045 ext. 4930 – Fax (229) 890-2402

MAULE - It's Why You Fly! Equipment and Options subject to change without notice. For Optional Equipment and Upgrades, please refer to the AUTHENTIC MAULE 2013 brochure.

For Pricing Information please refer to the 2013 MAULE AIRCRAFT ORDER FORM Available from your Authorized Maule Dealer 2013EFFMAR01REV2

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Adventure Awaits...... MAULE





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• Fun, Easy To Fly, 4 Seat Taildragger or Nosewheel STOL aircraft

• Perfect Blend of Performance and Fuel Efficiency

• Very Agile and Versatile with Substantial Cargo Area

• Used Extensively for Recreation, Flight Training, and Pure Enjoyment

• Preferred Aircraft for Various Law Enforcement and Military Missions

• 4+ 1 Seat Taildragger or Nosewheel STOL aircraft

• More Power, More Room, More Performance

• Enlarged Cargo Area for Carrying Longer and Larger Items

• A Perfect Choice for Operating in High Altitude, Mountainous Terrain

• Extensive Use by Commercial / Governmental Land and Seaplane Operators





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4 Seat Performance STOL Aircraft Oleo Strut Gear

Taildragger Aluminum Spring Gear

Taildragger Nosewheel

180 HP Models MX-7-180B MX-7-180C MXT-7-180

Engine (Lycoming) (2000 hr. TBO): 0-360-C1F 0-360-C1F 0-360-C1F

Gross Weight 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)

Stall Speed (full flaps / power off / light weight) 40 mph (35 kts) 40 mph (35 kts) 40 mph (35 kts)

Take Off, Ground Roll (light weight): 300 ft. (92 m) 300 ft. (92 m) 300 ft. (92 m)

Take Off (light weight) over 50’ Obstacle: 700 ft. (214 m) 700 ft. (214 m) 700 ft. (214 m)

Rate of Climb, Initial (light weight): 1000 fpm (5.1 m/s) 1000 fpm (5.1 m/s) 1000 fpm (5.1 m/s)

Landing (light weight) over 50’ Obstacle: 900 ft. (274 m) 900 ft. (274 m) 900 ft. (274 m)

Service Ceiling: 15,000 ft. (4572 m) 15,000 ft. (4572 m) 15,000 ft. (4572 m) Fuel Consumption (avg.) (US gals.) (65% power): 9 gph (34 lph) 9 gph (34 lph) 9 gph (34 lph)

Cruise (75% power / Opt. Alt.) (TAS): 138 mph (120 kts) 138 mph (120 kts) 138 mph (120 kts) Performance Observations are for One Person, 22 gals. Fuel, Sea Level, Standard Day Conditions (Do Not Use For Flight Planning)

MX-7 & MXT-7 Series Aircraft Specifications

Engine (Lycoming): 0-360-C1F Horsepower: 180 Standard Propeller:

76" Hartzell 2 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) Tailwheel

8 ft. 4 in. (2.54 m) Nosewheel

Fuel Capacity: 85 US gal. (321.7 l)

Flap Settings (degrees): -7, 0, 24, 40, 48 Tailwheel

-7, 0, 24, 40 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:

Four

Cabin Width: Front Seats Passenger Seat Rear Passenger Seat Cargo Area (with rear seats removed):

Approximately 38 cubic feet 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)





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4+1 Seat High-Performance STOL Taildragger

235 HP Carbureted 260 HP Fuel Injected

M-7-235B M-7-260

Engine (Lycoming) (2000 hr. TBO): 0-540-B4B5 I0-540-V4A5 Gross Weight 2500 lbs. (1136 kg) 2500 lbs. (1136 kg)

Empty Weight (avg.): 1605 lbs. (730 kg) 1610 lbs. (732 kg)

Useful Load (avg.): 895 lbs. (407 kg) 890 lbs. (405 kg)

Stall Speed (full flaps / power off / light weight) 40 mph (35 kts) 40 mph (35 kts)

Take Off, Ground Roll (light weight): 250 ft. (76 m) 250 ft. (76m)

Take Off (light weight) over 50’ Obstacle: 600 ft. (183 m) 600 ft. (183 m)

Rate of Climb, Initial (light weight): 1500 fpm (7.6 m/s) 1650 fpm (8.4 m/s)

Landing (light weight) over 50’ Obstacle: 900 ft. (274 m) 900 ft. (274 m)

Service Ceiling: 20,000 ft. (6096 m) 20,000 ft. (6096 m)

Fuel Consumption (avg.) (US gals.) (65% power): 12 gph (45 lph) 14 gph (53 lph)

Cruise (75% power / Opt. Alt.) (TAS): 158 mph (137 kts) 162 mph (141 kts) Performance Observations are for One Person, 22 gals. Fuel, Sea Level, Standard Day Conditions (Do Not Use For Flight Planning)

Engine (Lycoming) 0-540-B4B5 Carbureted

I0-540-V4A5 Injected

Horsepower 235 HP 0-540-B4B5 260 HP I0-540-V4A5

Standard Propeller 78" McCauley 2 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 6 ft. (1.83 m)

Main Landing Gear Type Oleo Strut

Cabin Width Front Seats Passenger Seat Rear Passenger Seat Seating Configuration

4 + 1 (optional 5th seat)

At Shoulders 42 in. (1.07 m) 38 in. (0.97 m) 33 in. (0.84 m) Cargo Area (with rear seats removed): Approximately 42 cubic feet At Hips 37 in. (0.94 m) 34 in. (0.86 m) 28 in. (0.71 m)





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4+1 Seat High-Performance STOL Nosewheel Aircraft 235 HP Fuel Injected 260 HP Fuel Injected

MT-7-235 MT-7-260

Engine (Lycoming) (2000 hr. TBO): I0-540-W1A5 I0-540-V4A5 Gross Weight 2500 lbs. (1136 kg) 2500 lbs. (1136 kg)

Empty Weight (avg.): 1665 lbs. (757 kg) 1696 lbs. (771 kg)

Useful Load (avg.): 835 lbs. (380 kg) 804 lbs. (366 kg)

Stall Speed (full flaps / power off / light weight) 40 mph (35 kts) 40 mph (35 kts)

Take Off, Ground Roll (light weight): 250 ft. (76 m) 250 ft. (76m)

Take Off (light weight) over 50’ Obstacle: 600 ft. (183 m) 600 ft. (183 m)

Rate of Climb, Initial (light weight): 1500 fpm (7.6 m/s) 1650 fpm (8.4 m/s)

Landing (light weight) over 50’ Obstacle: 900 ft. (274 m) 900 ft. (274 m)

Service Ceiling: 20,000 ft. (6096 m) 20,000 ft. (6096 m)

Fuel Consumption (avg.) (US gals.) (65% power): 11 gph (42 lph) 14 gph (53 lph)

Cruise (75% power / Opt. Alt.) (TAS): 158 mph (137 kts) 162 mph (141 kts) Performance Observations are for One Person, 22 gals. Fuel, Sea Level, Standard Day Conditions (Do Not Use For Flight Planning)

Engine (Lycoming) I0-540-W1A5 I0-540-V4A5

Horsepower 235 HP I0-540-W1A5 260 HP I0-540-V4A5

Standard Propeller 81" McCauley 2 Blade Constant Speed with I0-540-W1A5

78" McCauley 2 Blade Constant Speed with I0-540-V4A5

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 8 ft. 4 in. (2.54 m)

Fuel Capacity 85 US gal. (321.7 l)

Flap Settings (degrees) -7, 0, 24, 40

Main Gear Track 7 ft. 8 in. (2.34 m)

Landing Gear Type Spring Aluminum Main Gear

Steerable Hydraulic Nose Strut

Cabin Width Front Seats Passenger Seat Rear Passenger Seat Seating Configuration


At Shoulders 42 in. (1.07 m) 38 in. (0.97 m) 33 in. (0.84 m) Cargo Area (with rear seats removed): Approximately 42 cubic feet At Hips 37 in. (0.94 m) 34 in. (0.86 m) 28 in. (0.71 m)





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Maule Series Legendary MAULE Performance @ 2800 Lbs. GRWT

Enhancements found on the M-9 Series

• Gross Weight Increase of 300 lbs. to 2800 lbs. Gross Weight

• Extremely Rugged Spring Aluminum Main Gear with Gun-Drilled Internal Brake Line

• High Lift, All Metal Wings with Substantially Reinforced Spars and Attach Points

• Larger Rivets and Bolts in Key Areas for Enhanced Strength

• Structural Reinforcements in the Fuselage Including Reinforced Mounting Tube for

Tailwheel Forward Leaf Spring Attach Point

• Cross-Country Cruiser: Carry 4 Adults plus 100 lbs. of luggage and over 4 hours of fuel

• Multi-Mission Aircraft: Carry 2 Adults plus 250 lbs. of equipment and over 7 hours of fuel

• Modular Cabin with Quick Removal Seats:

Pilot plus 4 Passengers,

Pilot plus 3 Passengers and Luggage,

Pilot and Copilot plus approximately 42 cubic feet of Cargo Area





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4+1 Seat Enhanced Gross Weight Taildragger

235 HP Carbureted 235 HP Fuel Injected 260 HP Fuel Injected

M-9-235 Estimated (Not Yet Approved) M-9-235 M-9-260

Estimated (Not Yet Approved) Engine (Lycoming) (2000 hr. TBO) 0-540-B4B5 I0-540-W1A5 I0-540-V4A5 Gross Weight 2800 lbs. (1270 kg) 2800 lbs. (1270 kg) 2800 lbs. (1270 kg)

Empty Weight (Standard Aircraft) 1710 lbs. (776 kg) 1700 lbs. (771 kg) 1716 lbs. (778 kg)

Useful Load (Standard Aircraft) 1090 lbs. (494 kg) 1100 lbs. (499 kg) 1084 lbs. (492 kg)

Stall Speed (full flaps / power off / @ 2800) (IAS) 46 mph (40 kts) 46 mph (40 kts) 46 mph (40 kts)

Take Off, Ground Roll (@ 2800 lbs.) 406 ft. (124 m) 406 ft. (124 m) 406 ft. (124 m)

Take Off (@ 2800 lbs.) over 50’ Obstacle 791 ft. (242 m) 791 ft. (242 m) 791 ft. (242 m)

Landing (@ 2800 lbs.) over 50’ Obstacle 900 ft. (274 m) 900 ft. (274 m) 900 ft. (274 m)

Service Ceiling 20,000 ft. (6096 m) 20,000 ft. (6096 m) 20,000 ft. (6096 m)

Fuel Consumption (avg. @ 65% power) 11 gph (42 lph) 11 gph (42 lph) 14 gph (53 lph))

Cruise (75% power / Opt. Alt.) (TAS) 158 mph (137 kts) 158 mph (137 kts) 162 mph (141 kts)

Performance Observations are from Certification Flight Test - Sea Level, Standard Day Conditions (Do Not Use For Flight Planning)

M-9 Series Aircraft Specifications Engine (Lycoming):

0-540-B4B5 Carbureted I0-540-W1A5 Fuel Injected I0-540-V4A5 Fuel Injected

Horsepower: 235 Carbureted or Fuel Injected

260 Fuel Injected

Standard Propeller: 77" Hartzell 3 Blade Scimitar Constant Speed with 0-540-B4B5

80" McCauley 3 Blade Constant Speed I0-540-W1A5 77" Hartzell 3 Blade Scimitar Constant Speed with I0-540-V4A5

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)

Landing Gear Type Spring Aluminum Main Gear

Cabin Width: Front Seats Passenger Seat Rear Passenger Seat Seating Configuration:


At Shoulders: 42 in. (1.07 m) 38 in. (0.97 m) 33 in. (0.84 m) Cargo Area (with rear seats removed): Approximately 42 cubic feet At Hips: 37 in. (0.94 m) 34 in. (0.86 m) 28 in. (0.71 m)





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Standard Equipment (ALL MODELS, Unless Otherwise Noted) Airframe and Wings:

• Welded Tubular 4130 Chromoly Steel Fuselage and Tail Section, Stabilizers, Elevators, and Rudder

• Airframe Float Reinforcements • Float Fittings - Aft Attach Points: Weld-In • Float Fittings - Forward Set: (Nosewheel Models Only)

• Fuselage, Tail Surface and Rudder Covering: Ceconite • Grab Handles on Fuselage for Lifting/Moving • Stainless Steel Main Horizontal Stabilizer Tail Strut • All Metal Ailerons and Flaps: Aluminum Spars, Ribs, Skin • All Metal Wings: Aluminum Spars, Ribs, Skin • Steel Tie Down Rings • Tail Surface and Rudder Covering: Ceconite

Corrosion and Covering Protection:

• Powder Coating on Airframe, Engine Mount, Door Frames and Other Steel Parts

• Urethane Paint System • Wing Corrosion Proofing. • Sealed Wing Lift struts are internally coated with oil.

Cabin and Cargo:

• Adjustable Front Seats with Integrated Seat Back Pockets: Pilot and Copilot - Side-by-Side

• Rear Seats - Completely Removable Rear Sling Seat: Side-by-Side - Adjustable Two Position M7 / MT7 / M-9

• Cargo Tie Down Straps • Full Cabin Floorboards • Fully Upholstered Interior: Seats, Headliner, Door/Side

Panel/Trim • Lockable Cabin Entry Doors: Pilot (Keyed), Copilot, Rear

Passenger and Cargo • Stainless Steel Entry Door Sills

Comfort and Convenience:

• Adjustable Window Vents • Auxiliary Power Plug in Instrument Panel • Cabin Fresh Air Vents: Pilot and Copilot • Cabin Heater Vents: Front and Rear Passenger • Cabin Sound Proofing and Insulation • Cabin Steps: Pilot and Copilot Doors • Rear Passenger Entry Door Cabin Step (MXT-7 &MT-7 Only) • Door Pockets: Pilot and Copilot Doors • Skylight (Smoke Tint) with Retractable Sun Shade • Smoke Tint Windshield • Swing Out Window (Fully Opening): Pilot Side • Windshield Defroster

Electrical and Lighting System:

• Alternator (60 Amp) • Battery - 12V (14V system) • Circuit Breakers • Instrument and Dome Lights • Landing Light In Wing: Left (Taxi) and Right • Lightweight Starter • Navigation Lights • Omni Antenna • Wing Tip Strobe Lights

Firewall Forward:

• Composite Two-Piece Split Engine Cowling • Spin-On Oil Filter • Stainless Steel Exhaust System with Muffler Heat Shroud

• Stainless Steel Firewall

Fuel System:

• Auxiliary Fuel Pump • Fuel Drains (7): One Fuel Sump Drain in Each Tank,

Two Low-Point Drains, One Gascolator • Fuel Tanks (Aluminum) – 4 Tanks: 85 gals. Useable

o 2 Main Tanks: 21.5 gals. Useable o 2 Auxiliary Tanks: 21 gals. Useable

• Fuel Transfer Pumps for Auxiliary Tanks • Fuel Selector Valve (Left, Right, Both, and Off) • Gravity Feed Fuel System - No Header tanks

Wheels and Brakes:

• Aluminum Wheels and Hydraulic Brakes • 7.00 x 6 Main Landing Gear Tires • Parking Brakes • Maule Steerable Tundra Tailwheel

Instrument Panel:

• Clock - Analog • Compass - Magnetic • Full Gyro Panel with Vacuum System

o Airspeed Indicator o Altimeter o Attitude Gyro o Directional Gyro o Electric Turn Coordinator o Vertical Speed Indicator � Dry Air Pump � Filter � Regulator � Suction Gauge

• Amp Meter (Analog) • Cylinder Head Temperature -1 cylinder (Analog) • Fuel Pressure • Fuel Quantity - Left/Right Main and Aux. Tanks (Analog)

• Manifold Pressure • Oil Pressure (Analog) • Oil Temperature (Analog) • Outside Air Temperature • Tachometer

Safety Features:

• 3 Point, Inertia Reel Shoulder Harnesses: All Seats • 406 MHz Emergency Locator Transmitter (ELT) • Audible and Visual Stall Warning Indicator • Complete 4130 Chromoly Steel Fuselage • Dual Control Yokes • Dual Rudder Pedals and Toe Brakes • Four Position Fuel Selector Valve

with Integrated Safety Features • Heated Pitot Tube

Maule Unique Standard Features:

• Flap -7 Degree Setting for Increased Cruise Speed • Four Doors and Four Seats • Easy Access Rear Passenger / Cargo Doors:

Open Away from Each Other which Allows for Loading of Long Objects

• Side-by-Side Pilot and Copilot Seating • Side-by-Side Passenger Seating • Quick Removal Rear Passenger Seats for More Cargo Area • Larger Cargo Area for Optional 5th Seat – M(T)-7 / M-9 Series





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VFR Avionics Package Included in Basic Aircraft Price

VFR SEVEN 96 VFR Only - Optional Upgrades Available (May Be Installed Post-Production, Under FAA 337 Approval) • Garmin aera 796 with GA-25 GPS and GXM 40A Antennas • Air Gizmos Mounting Tray • Garmin SL 40 Comm (Requires use of headsets, unless used with optional PMA 8000BT) • Garmin GTX 327 Digital Transponder with Antenna • Avionics Cooling Blower, Altitude Encoder, Broad Band Antenna • Mike and Phone Jacks, 2 Front / 2 Rear, Pilot & Copilot Push-To-Talk Switches • Radio Master Switch

Standard Aircraft Paint and Stripe Scheme Stripe Scheme 2 (Additional Stripe Colors Available) Choose From 15 Available Stripe Colors (Color Chart in Authentic Maule 2013 Options Sheets) Base Colors (Optional Base Color Available) • Glacier White (White) • Dune White (Ivory/Beige) - May be specified in lieu of Glacier White

Shown in Dune White with Optional Stripe Color

Final Panel Layout May Vary





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Standard Interior Appointments

Standard Interior: Vinyl Headliner, Vinyl Seats with Fabric Seating Surfaces and Side Panel Centers, Vinyl Side Panels and Trim Pieces, Full Cabin Floorboards

Standard Interior Colors

adventure awaits · pdf file235 hp carbureted 260 hp fuel injected m-7-235b m-7-260 engine...

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