Seneca II Panel Reference
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This is a quick reference to the instruments and controls in the Seneca's cockpit. (Piper PA34-200T Seneca II)
The Controls of the Seneca II
- magneto - left engine
- magneto - right engine
- starter - press left for left engine, right for right engine
- primer - left/right engine
- taxi/landing lights
- nav lights
- anit collision lights - left half: fin (beacon), right half: wing (strobes)
- pitot and stall warning heat
- fuel boost pumps - up: high, down: low, center: off
- battery master
- alternator on/off
- switch panel lights dimmer (noop)
- clock
- airspeed indicator
- attitude indicator (artificial horizon)
- altimeter (barometric)
- radar altimeter
- adf indicator [1]
- turn coordinator
- horizontal situation indicator (hsi) [2]
- vertical speed indicator (vsi)
- vor/ils indicator NAV2 [3]
- alternator ampere meter (shows alternator load)
- cylinder head temperature
- oil temperature
- oil pressure
- fuel
- RPM left engine
- dual manifold pressure gauge
- RPM right engine
- landing gear lever and emergency gear extension
- landing gear indicator
- autopilot control
- autopilot pitch control
- parking brake
- engine alternate air
- cowl flaps
- instrument lights dimmer
- fuel flow meter
- exhaust gas temperature (EGT) left/right engine
- DME frequency source (NAV1/Hold/NAV2) and ON/OFF
- DME indicator
- HSI gyro control
- ADF radio
- KX165 COM2/NAV2 radio [4]
- KX165 COM1/NAV1 radio
- GMA340 intercom
- surface deice (boots)
- wing ice inspection light
- prop deice
- prop deice control gauge
- windshield deice
- annunciator with test button
- gear warning light
- autopilot capture light
- flap lever
- autopilot mode
- gyro pressure
- cicruit breaker panel
- magnetic compass
- fuel selectors - forward: on, center: off, backwards: cross-feed
- elevator trim
- rudder trim
References
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