Kelly Aerospace E-drive Aircraft Starter: The Only True In-Line Starter

Starter Comparison Facts:
Kelly Aerospace E-drive vs. Sky-tec 149-NL

Performance is the most important aspect to evaluating your new starter. The important key measurements in assessing a starter's performance are engine Cranking Speed (rpm), electric Current Draw (amps), and Duty Cycle.

Cranking Speed (rpm) is the speed at which your starter rotates the engine's crankshaft during a start. You may think that a higher cranking speed would be better but this is not always the case. Your starter is part of the engine's starting system which also includes the fuel and ignition systems. These systems have been designed to provide good starting characteristics for a particular starting speed range. For most engines this speed is between 120 and 180 rpm. Cranking your engine faster than 200 rpm may disengage the magneto impulse couplings thereby advancing the ignition timing which will result in poor engine starting and can even induce kickbacks! A typical 6 cylinder Lycoming engine requires 50-60 ft*lbs of torque to start. For this load condition, consider the following comparison (see chart, point B for Edrive and point D for Sky-Tec).

  • Sky-Tec - 295/305 rpm at 50 ft*lbs of torque.
    (spins the engine too fast)
  • E-drive - 145/155 rpm at 50 ft*lbs of torque.
    (ideal cranking, well below limit)

Current Draw directly affects the amount of heat that builds up in your starter when cranking your engine. The more current your starter pulls, the more heat that is generated in the starter. Increased heat reduces cranking performance, shortens the overall life of your starter and drains your battery. The rate of temperature increase also decreases the duty cycle of the starter which means fewer starts before the starter reaches its temperature limit. Current draw also affects other components in the aircraft starter electrical system. Contactors, terminals, and cables are all adversely affected by high current draw. Current draw is particularly important to pilots who have the battery located in the rear of the aircraft. The cable between the battery and the starter acts as a resistor which causes a voltage drop over its length. As current increases so does this voltage drop. The resulting electrical power lost to heat over the length of the cable is not available for use by the starter. Higher current draw results in greater voltage drop and less power to the starter. For cranking a typical Lycoming 6-cylinder engine with a 24-volt system and assuming a 50 ft*lb torque load the following comparison should be considered (see chart).

  • Sky-Tec - 165/175 amps
    (pulls about 2-1/2 times as much current, shortening starter life)
  • E-drive - 60/70 amps
    (More than double the number of starts and duty cycle of Sky-Tec!)

Current Draw also determines the number of starts you can get from your battery. For a given charge condition, your battery is capable of delivering a given number of starts and that number is directly related to the amount of current your starter draws while cranking. A starter drawing twice the current will only give you half the number of starts before battery depletion.

E-Drive Starter - Features

  • Immune to kick-back damage
  • No mechanical Bendix
  • Suitable for installation on all Lycoming engines without modification
  • Solid-state solenoid control
  • Non-cantilevered pinion support
  • Only 9.5 lbs.
  • 3,000 maintenance free starts, minimum
  • New high performance PM motor
  • Same envelope as existing certified starters

New High Torque Motor

Edrive Starter High Torque Motor
  • High Performance Armature
    - Increased commutator bar length
    - Thin laminations
    - High quality magnetic alloy
  • 12 & 24 volt winding configuration
  • Redesigned Brush Holder
    - Metal construction for heat sinking
    - Offset brush position for increased brush contact area
  • Robust spring design
  • High performance field housing
    - Rare earth neodymium magnets
    - Small package
    - Stronger flux field
  • Improved temperature stability

Duty Cycle Reliability

  • Duty cycle limitation exceeds other starter designs by over 40%.
  • Improved duty cycle results in lower operational temperatures and longer starter life.
  • More starts, lower maintenance, and less cost.