1969 Cessna 421A
Description
The Cessna 421A is a twin-engined light aircraft produced by Cessna between 1967 and 1972. It is an improved version of the Cessna 421 and features a higher gross weight, improved pressurization, and more powerful engines. The aircraft is commonly used for personal and business aviation, and can hold up to six passengers. The Cessna 421A is capable of reaching speeds of up to 200 knots and has a range of 1,100 nautical miles.
Features
- Total Time: 3835
- Engines / Mods / Prop:
- Continental GTSIO520-D21B
- SN: 219477-R
- 1208.8 SFRM (1600 TBO)
- Rebuild Date - 4/1999
- Rebuild by - Teledyne Continental Motors
- Last Compressions -
- 79-79-74-74-78-80 over 80.
- McCauley 3 Blade Prop
- 1208.8 SNEW (2000 TBO)
- Installed - 9/1999
- Built - 10/1997
- Hot Prop - Boots in very good condition.
- Continental GTSIO520-D21B
- SN: 1001377
- 469.1 SFRM (1600 TBO)
- Rebuild Date - 12/2009
- Rebuild by - Teledyne Continental Motors
- Last Compressions -
- 75-75-77-80-78-80 over 80.
- McCauley 3 Blade Prop
- 1208.8 SNEW (2000 TBO)
- Installed - 9/1999
- Built - 10/1997
- Avionics / Equipment:
- Well upgraded Panel!
- G3 Touch PFD
- GTN-750 GPS/Nav/Comm
- KX-165 Nav/Comm (w/Glidslope)
- KN-64 DME
- GTX-345R Transponder (ADS-B In/Out)
- STec 3100 Digital Autopilot
- GA32 Audio Panel (750)
- Shadin Fuel Flow
- DavTron M800 Chrono
- Vortex Generators
- De-Ice Boots on Outer Leading Edges
- De-Ice Boots on Tail/Rudder Leading Edges
- Alcohol Wind Shield
- Hot Props
- 406 EL
Location
