Supplement POH
Cessna 172 R&S
(FAA-Version)
Page 4-11
Issue 3
Revision 1, Jan. 2018
(14) Thrust Lever – FULL FORWARD, load display min. 94%,
RPM 2240 - 2300
(15) Thrust Lever – IDLE
(16) Engine Instruments and Ammeter – CHECK
(17) Suction gage – CHECK
(18) Annunciator Panel – Ensure no annunciators are
illuminated
(19) Wing Flaps – SET for Take-off (0° or 10°).
(20) Electric Fuel Pump – ON
(21) Strobe Lights – AS DESIRED
(22) Radios and Avionics – ON and SET
(23) Autopilot (if installed) – OFF
(24) Air Conditioning (if installed) – OFF
(25) Thrust Lever Friction Control – ADJUS
(26) Brakes – RELEASE
Note: If the test button is released before the self
test is over, the FADEC immediately
switches over to normal operation.
Note: While switching from one FADEC to
another, it is normal to hear and feel a
momentary surge in the engine.
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