You are here: HomeAircraft Engine PartsFAA-PMA Approved Aircraft Engine Alternator KitsPlane-Power AL24-F60C FAA-PMA Alternator replaces 24/28V Ford, 60 amp alternators in most Cessna aircraft with Continental engines

Plane-Power AL24-F60C FAA-PMA Alternator replaces 24/28V Ford, 60 amp alternators in most Cessna aircraft with Continental engines

Plane-Power AL24-F60C FAA-PMA Alternator replaces 24/28V Ford, 60 amp alternators in most Cessna aircraft with Continental engines
Plane-Power AL24-F60C FAA-PMA Alternator replaces 24/28V Ford, 60 amp alternators in most Cessna aircraft with Continental enginesPlane-Power AL24-F60C FAA-PMA Alternator replaces 24/28V Ford, 60 amp alternators in most Cessna aircraft with Continental engines
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Item #:AL24-F60C
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Price:$492.95
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The Plane Power AL24-F60C FAA-PMA approved Alternator is a direct replacement for Ford 24/28 volt, 60 amp Alternators typically installed on Cessna Aircraft with Lycoming Engines.

The Plane-Power AL24-F60C should be consider as a direct replacement for the following:

  • Cessna Part Number: C611503-0102
  • Cessna Part Number: 1570213-7

    Please use the "Application" to see if your planes model is listed.

  • 24/28 volt
  • 70 amp*
  • Weight: 9 Pounds, 12.8 Ounces
  • Warranty: 2-Year Limited

    *Aircraft electrical system will be limited by existing wiring and output breaker not to exceed 60 amps. The Plane-Power alternator can produce all 70 amps if proper size wiring and circuit breaker is installed and approved.

    • The Plane-Power AL24-F60C is FAA-PMA approved for installation on the following:

    Cessna

  • 182P, 182Q, 182R, T182
  • 180J, 180K
  • 188, 188A, 188B, A188, A188A, A188B, T188C
  • U206E, U206F, U206G, TU206E, TU206F, TU206G
  • 207, T207
  • 210K, 210L, 210M, 210N, 210R, P210N, P210R, T210K, T210L, T210M, T210N, T210R
    • Installation Instructions

    1. Disconnect aircraft battery.
    2. Install alternator per included drawing.
    3. Refer to appropriate engine and airframe service manuals for belt tension and bolt torques.
    4. Install battery wire with MS25171-2S terminal nipple on 6mm output terminal and torque to 50 in. lb.
    5. Install ground wire to any of the three 5mm studs on rear of alternator and torque to 35 in. lb.
    6. Install field wire with MS25171-1S terminal nipple to F1 terminal on rear of alternator and torque to 20 in. lb.
    7. NOTE: F2 terminal to remain grounded with ground strap UNLESS aircraft voltage regulator is a type "A" regulator using a 2-wire field circuit, in this case remove and discard ground strap from F2 terminal and connect wiring from voltage regulator to F1 and F2 terminals, torque to 20 in. lb.
    8. If aircraft is equipped with an "alternator out light" circuit, connect that wire to the AUX terminal and torque to 20 in. lbs. Other wise leave AUX terminal open.
    9. Reconnect aircraft battery.
    10. Start aircraft and check alternator output for proper operation.

    Instructions For Continued Airworthiness

    Annual / 100 hour inspections

    1. Remove drive belt and turn alternator rotor to check condition of bearings for abnormal noise or roughness.

    5 year or 1,000 hour intervals
    1. Repeat: Annual / 100 hour inspection.
    2. Remove field brush assembly and inspect brushes for excess wear. Replace brush assembly if brushes extend less than .250" from edge of brush holder case.
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