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Piper PA-39 Twin Comanche C/R - DESCRIPTION AIRPLANE AND SYSTEMS

Piper PA-39 Twin Comanche C/R
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DESCRIPTION
AIRPLANE AND SYSTEMS
Engine and Propeller ............................................
1
Tile Optional Rajay Turbocharger ..................................... 1
Fuel Injection ................................................ 3
St~ctures ................................................... 3
LandingGear ................................................. 3
Control System ............................................... 4
Fuel System . ................................................. 5
Electrical System .............................................. 7
\‘dcuumSystem ................................... : ........... 9
Instrument Panel ............................................... 10
Instrument Static Pressure System ..................................... 10
Heating and Ventilating System ...................................... 12
Seats ...................................................... 14
Finish .................................................... . . 14
Baggage Area ................................................. 14
Srall Warning System ........ .;. .................................. 14
Propeller Synchrophaser ............ -.-. ............................ 15

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