Rockwell Commander 114, 114A and 114B

STC – Data

• Type of Aircraft: Commander 114, 114A and 114B0
• LBA: SA0867 (issued Aug. 22, 1997)
• FAA: SA09632AC (issued Oct. 04, 2004)
• Applicable Aircraft: Rockwell Commander 114, -A, -B
• Engines: Lycoming IO-540-T4A5D, -T4B5D
  RPM limitation: max. 2500 RPM
• Propeller: MTV-9-B/190-18b

Advantages:

• Best vibration damping characteristics
• Bonded on stainless steel leading edge for best erosion
  protection of the blades
• Unlimited blade life
• FOD repairable blades