Normal Procedures
Pilot's Flight Manual
4-11.1
Reissued: 16 Jan 2019
Fig ure 4-2B. In stru ment Panel (269A4540-7, S/N 1750 & Subs.)
CLUTCH DISENGAGED
WARNING LIGHT
BATTERY SWITCH
FUEL BOOST PUMP
SWITCH-CIRCUIT BREAKER
TRIM-CIRCUIT BREAKER
CLUTCH-CIRCUIT
BREAKER
INSTRUMENT-CIRCUIT
BREAKER
MICROPHONE
SWITCH
LAND'G LIGHT-CIRCUIT
BREAKER
FUEL MIX CONTROL
RADIO-CIRCUIT
BREAKER
ADF-CIRCUIT
BREAKER
HEATER-CIRCUIT
BREAKER
XPDR-CIRCUIT
BREAKER
HOUR METER
PANEL LIGHT DIMMER
ALTERNATOR SWITCH
CYCLIC TRIM SELECTOR
SWITCH
AMMETER
LOW VOLTAGE WARNING LIGHT
COMPASS
M/R XMSN CHIPS (OPT.)
FUEL LOW WARNING LIGHT
M/R XMSN TEMPERATURE & OIL
PRESSURE WARNING LIGHT
T/R XMSN CHIPS
ALTIMETER
AIRSPEED INDICATOR
MANIFOLD PRESSURE INDICATOR
ENGINE & ROTOR
TACHOMETER
CYLINDER HEAD
TEMPERATURE
INDICATOR
FUEL PRESSURE GAUGE
FUEL QUANTITY GAUGE
(GALLONS)
ENGINE OIL
TEMPERATURE
INDICATOR
ENGINE OIL
PRESSURE
INDICATOR
LIGHTS: PANEL-
POSITION-BEACON
FUEL SHUTOFF
CONTROL
MAGNETO
SWITCH
CLUTCH CONTROL
SWITCH
NOTE:
STANDARD EQUIPMENT ON
269C HELICOPTERS, S/N 1750
AND SUBSEQUENT.
This Document contains technical data subject to EAR. See WARNING and classifications on first page.
SCHWEIZER
Model 269C Helicopter
FAA Approved
CSP Book 1 CSP-C-1.indd 98 8/4/19 12:45 PM
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