STC - Data
- Type of Aircraft: Mitsubishi MU-2B
- EASA: 10043855 (issued Feb. 28, 2013)
- FAA: SA03315NY (issued July 31, 2013)
- ANAC Argentina: CTS 1409.13 (issued Sept. 15, 2014)
- ANAC Brazil: CST 2022S08-01 (issued Aug. 01, 2022)
- Applicable Aircraft: MU-2B Series
- Engines: for the 2000RPM engine: Honeywell, USA
TPE331-25AA, TPE331-1-151A,
TPE331-6(A)-251M or -252M
TPE331-10-( ) installed per approved STCs which
do not exceed 715 shp and 2000 rpm
- Engines: for the 1591RPM engine: Honeywell, USA
TPE331-10-501M or TPE331-10-511M or
TPE331-5-252M or any TPE331-( ) installed per
approved STCS which do not exceed 715 shp and
1591 rpm.
- Propeller: for the 2000RPM engine with CW rotating propellers:
MTV-27-1-E-C-F-R(G)/CFR210-58d
For the 1591RPM engine with CCW rotating propellers:
MTV-27-1-E-C-F-R(G)/CFRL240-55d.
- Advantages:
- Best vibration damping characteristics
for almost vibration free propeller operations
- Bonded on nickel alloy leading edge for best erosion
protection of the blades
- Dramatically reduced inside noise by up to 8 dB(A)
- Increased Deice Boot Area for better de-icing capabilities
- No life limited parts
- Lower weight and Jet Like comfort
- Reduced propeller weight
- Improved take off, climb and top speed
- Unlimited blade life
- FOD repairable blades
more
information about the STC (.pdf 100kb)
more
information about the STC (.pdf 78kb)
MT-Propeller
