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Mission Ready
After thousands of hours of design, each BT-67 is engineered to assure that
every component, assembly, or system is either new or the equivalent of new.
All workmanship and materials meet the highest standards of the U.S. Federal
Aviation Administration (FAA). The philosophy inherent in our manufacturing
process is to exceed industry standards by following an uncompromising
approach to excellence that produces a product of the highest quality.

| Airframe: |
- Inspected and overhauled to fully
re-engineer and strengthen airframe. Returns airframe to original
specification, or exceeds original specification. Includes a
structural reinforcement package. Rated as "zero accumulated fatigue
damage".
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Fuselage stretched 40-inches (forward of
wing).
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Cockpit bulkhead moved forward 60-inches
to increase payload cabin volume and aerodynamic performance.
- Redesigned
outer wing leading edge and
wing tip.
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| Payload and
Performance: |
Compared to the standard DC-3,
the BT-67 has:
- 35% more
interior volume
- 43% more useful load
- 24% more speed
- Up to 100% more fuel capacity
- Lower stall speed
- Lower approach speed
- Fuel mileage equal at equal speeds
- All metal control surfaces (optional)
- Center and outer
wings reinforced in 250
places to
reduce loads on lower wing attach angles and to support the increased
maximum gross weight.
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| Interior
Dimensions: |
| Width (At
Floor): |
7 feet |
| Height: |
6 feet, 6 inches |
| Length: |
42 feet, 2 inches |
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| Volume: |
1225 Cubic Feet |
| Documented 12,000
Hour Overhaul: |
- Douglas Supplemental Inspection (SID)
- FAA Airworthiness Directives
incorporated
- Service bulletin compliance
- New skin and ribs as required -
- Corrosion repair
- Damage repair
- Aesthetics
- New interior corrosion protection
- New or overhauled:
- Main landing gear
- Tail gear assembly
- Landing gear retract and compensating cylinders
- Tail wheel shock strut
- Hydraulic accumulator
- Wing flap actuating cylinder
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| Standard
Conversion Items Cockpit: |
- Overhead system panels
- Circuit breakers
- Electrical junction box
- New instrument panel
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View
Larger Image |
| Flight Control
System: |
- Including bob weight and down springs on
elevator system
- Servo assisted ailerons
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| De-Icing
Equipment: |
- Complete propeller and engine air inlet
de-icing system
- Bleed air supply for wing and empennage
de-icer boots (wing and empennage available as options)
- Electrically heated one-piece
windshields
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| Electrical
Systems: |
- Four-buss systems (left and right
generator, essential and emergency busses)
- 300 amp starter generators
- Completely new wiring harnesses
- (2) new higher energy 12-volt dry cell
batteries
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| Hydraulic System: |
- Engine driven variable displacement
pumps
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| Fuel System: |
- Electrically driven fuel pumps - (2)
left and right main, and (2) left and right standby
- Electrically driven transfer pumps (2)
- New fuel lines and fittings
- New leak-proof filler caps
- New fuel quantity transmitters and
indicators
- Fuel computer and flow indication system
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New Design Fire
Detection & Fire Extinguishers System: |
- FAR Part 25 compliant
- Dual sensing, 3 element,
4 bottle system
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| Manuals: |
- Flight manual
- Military flight manual
- Maintenance manual
- Structural repair manual
- Illustrated parts catalog
- Wiring manual
- Engine manual
- Propeller manual
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| Systems Replaced: |
- Electrical system replaced by complete
new system designed for FAR Part 25.
- Hydraulic system upgraded for improved
gear retraction time
- Fuel system engineered to FAR Part 25
- Brakes, B.F. Goodrich H2-445, expander
tube brake assembly installed
- Anti-ice and de-ice equipment
- Propellers
- Inlets
- Windshields
- New bleed-air heating system (muffled)
- Low infrared signature due to an
augmented exhaust system, which disperses over the upper wing surface
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| Power Plant: |
- Effective proven and
powerful Pratt &
Whitney Canada PT6A-67R certified to FAR Part 33 amendment 10 with Hartzell 5-blade aluminum reversing propeller. Reliable, clean,
efficient, and quiet ... certified to FAR Part 36 stage III
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| NEW Systems: |
- Power plant
- De-ice
- Hydraulics
- Avionics
- Autopilot
- Air conditioning
- Fuel
- Stall Warning
- Electrical
- Oxygen
- Fire protection
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STC: FAA Supplemental Type
Certificate SA4840NM and Part Manufacturing
Authorization held by: Basler Turbo
Conversions, LLC, Oshkosh, WI USA
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