STC M7 Aerospace LP SA227

STC – Data

• Type of Aircraft: SA226/SA227
• EASA: 10015216 (issued Dec 2011)
• FAA: SA03893AT (issued July 24, 2013)
• TCCA Canada: Letter of acceptance
  to the EASA STC 10015216 (former EASA.A.S.03631)
• SCT Mexico: Validation No. IA-237/2013 (issued Nov 4, 2013)
• Applicable Aircraft: M7 Aerospace LP SA226-T(B), SA 227-TT, -AC,
  -AT, -CC, -BC, -DC
• Engines:TPE331-10U-( ), TPE331-11U-(), TPE331-12UA-()
  TPE331-12UAR-(), TPE331-12UHR-()
• Propeller: MTV-27-1-E-C-F-R(G)/CFRL250-103
• Advantages:

• Best vibration damping characteristics
  for almost vibration free propeller operations
• Bonded on nickel alloy leading edge for best erosion
  protection of the blades
• No engine modifications (no cam or beta tube change)
• Ground roll distance reduced by approx. 50 m (165 ft)
• Take-off distance over 50 ft obstacle reduced by
  approx. 80 m (260 ft)
• Two engine and single engine climb performance
  slightly improved by up to 80 ft/min
• Cruise performance slightly improved by up to 2 kts
• Approx. 65 lbs less weight than the orig. metal propellers
• More ground clearance for less FODs
• Significant inside and outside noise reductions
• Aircraft noise level is about 5 dB(A) less than with the
  original metal propellers
• Cabin noise is reduced by 3 to 4 dB(A)
  depending on location
• Unlimited blade life
• FOD repairable blades

more information about the STC (.pdf 75k)