Adventure Awaits... MAULE 1
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 2
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) Engine (Lycoming): 0-360-C1F Wing Span: 32 ft. 11 in. (10.03 m) Fuel Capacity: 85 US gal. (321.7 l) MX-7 & MXT-7 Series Aircraft Specifications Horsepower: 180 Wing Area: 165.6 sq. ft. (15.39 sq. m) Flap Settings (degrees): -7, 0, 24, 40, 48 Tailwheel -7, 0, 24, 40 Nosewheel Standard Propeller: 76" Hartzell 2 Blade Constant Speed Length: 23 ft. 8 in. (7.21 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 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) 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 3
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): At Hips 37 in. (0.94 m) 34 in. (0.86 m) 28 in. (0.71 m) Approximately 42 cubic feet 4
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 Wing Span 32 ft. 11 in. (10.03 m) Fuel Capacity 85 US gal. (321.7 l) Horsepower 235 HP I0-540-W1A5 260 HP I0-540-V4A5 Wing Area 165.6 sq. ft. (15.39 sq. m) Flap Settings (degrees) -7, 0, 24, 40 Standard Propeller 81" McCauley 2 Blade Constant Speed with I0-540-W1A5 78" McCauley 2 Blade Constant Speed with I0-540-V4A5 Length 23 ft. 8 in. (7.21 m) Main Gear Track 7 ft. 8 in. (2.34 m) Cabin Width Front Seats Passenger Seat Rear Passenger Seat Height 8 ft. 4 in. (2.54 m) Landing Gear Type Spring Aluminum Main Gear Steerable Hydraulic Nose Strut 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): At Hips 37 in. (0.94 m) 34 in. (0.86 m) 28 in. (0.71 m) Approximately 42 cubic feet 5
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 6
2013 MAULE AIRCRAFT SELECTION GUIDE www.mauleairinc.com Aircraft Sales Phone (229) 985-2045 ext. 4930 Fax (229) 890-2402 4+1 Seat Enhanced Gross Weight Taildragger 235 HP Carbureted M-9-235 235 HP Fuel Injected M-9-235 Estimated (Not Yet Approved) Engine (Lycoming) (2000 hr. TBO) Gross Weight 260 HP Fuel Injected M-9-260 Estimated (Not Yet Approved) 0-540-B4B5 2800 lbs. (1270 kg) I0-540-W1A5 2800 lbs. (1270 kg) I0-540-V4A5 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) 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) 20,000 ft. (6096 m) 20,000 ft. (6096 m) 20,000 ft. (6096 m) 11 gph (42 lph) 11 gph (42 lph) 14 gph (53 lph)) 158 mph (137 kts) 158 mph (137 kts) 162 mph (141 kts) Stall Speed (full flaps / power off / @ 2800) (IAS) Service Ceiling Fuel Consumption (avg. @ 65% power) Cruise (75% power / Opt. Alt.) (TAS) 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) 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 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) Height: 6 ft. 4 in. (1.93 m) Cargo Area (with rear seats removed): Approximately 42 cubic feet 7
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 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 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 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 5 th Seat M(T)-7 / M-9 Series 8
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 Final Panel Layout May Vary 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 9
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 10