Specifications

SECTION 4 CESSNA
NORMAL PROCEDURES MODEL 172R NAV III
GFC 700 AFCS
U.S.
DESCENT
1. Power - AS DESIRED
2. Mixture - ADJUST (if necessary to make engine run smoothly)
3. Altimeters:
a. PFD (BARO) - SET
b. Standby Altimeter - SET
4. ALT SEL - SET
5. CDI Softkey - SELECT NAV SOURCE
6. FMS/GPS - REVIEW and BRIEF (OBS/SUSP softkey operation
for holding pattern procedure (IFR))
CAUTION
THE G1000 HSI SHOWS A COURSE DEVIATION
INDICATOR FOR THE SELECTED GPS, NAV 1 OR NAV 2
NAVIGATION SOURCE. THE G1000 HSI DOES NOT
PROVIDE A WARNING FLAG WHEN A VALID
NAVIGATION SIGNAL IS NOT BEING SUPPLIED TO THE
INDICATOR. WHEN A VALID NAVIGATION SIGNAL IS
NOT BEING SUPPLIED, THE COURSE DEVIATION BAR
(D-BAR) PART OF THE INDICATOR IS NOT SHOWN ON
THE HSI COMPASS CARD. THE MISSING D-BAR IS
CONSIDERED TO BE THE WARNING FLAG.
WARNING
WHEN THE AUTOPILOT IS ENGAGED IN NAV, APR OR
BC OPERATING MODES, IF THE HSI NAVIGATION
SOURCE IS CHANGED MANUALLY, USING THE CDI
SOFTKEY, THE CHANGE WILL INTERRUPT THE
NAVIGATION SIGNAL TO THE AUTOPILOT AND WILL
CAUSE THE AUTOPILOT TO REVERT TO ROL MODE
OPERATION. NO AURAL ALERT WILL BE PROVIDED.
IN ROL MODE, THE AUTOPILOT WILL ONLY KEEP THE
WINGS LEVEL AND WILL NOT CORRECT THE
AIRPLANE HEADING OR COURSE. SET THE HDG BUG
TO THE CORRECT HEADING AND SELECT THE
CORRECT NAVIGATION SOURCE ON THE HSI, USING
THE CDI SOFTKEY, BEFORE ENGAGING THE
AUTOPILOT IN ANY OTHER OPERATING MODE.
7. FUEL SELECTOR Valve - BOTH
8. Wing Flaps - AS DESIRED (UP - 10° below 110 KIAS)
(10° - FULL below 85 KIAS)
172RPHBUS-00
4-20