Cessna Model 172S NAV III GFC 700 AFCS Pilot's Operating Handbook

Fill-in-the-blank style flashcards based on the Cessna Model 172S NAV III Pilot's Operating Handbook.

The maximum climb rate at sea level for the Cessna 172S is __ FPM.

730 FPM

Takeoff distance over a 50-foot obstacle is __ feet.

1630 feet

In the event of engine failure immediately after takeoff, airspeed should be __ KIAS with flaps up.

70 KIAS

The normal operating range for oil pressure is __ PSI.

50 to 90 PSI

The maximum structural cruising speed (VNO) is __ KIAS.

129 KIAS

Fuel capacity for the Cessna 172S is __ gallons.

56 gallons

Flaps should be set to __ degrees for short field takeoff.

10 degrees

The stall speed with flaps up for the Cessna 172S is __ KCAS.

53 KCAS

The aircraft is powered by a _ engine.

Lycoming IO-360-L2A engine.

The Cessna 172S has a maximum takeoff weight of __ pounds.

2550 pounds

The primary flight instrument data is displayed on the __.

Primary Flight Display (PFD)

The maximum climb rate at sea level for the Cessna 172S is __ FPM.\n\n

730 FPM\n\n

Takeoff distance over a 50-foot obstacle is __ feet.\n\n

1630 feet\n\n

In the event of engine failure immediately after takeoff, airspeed should be __ KIAS with flaps up.\n\n

70 KIAS\n\n

The normal operating range for oil pressure is __ PSI.\n\n

50 to 90 PSI\n\n

The maximum structural cruising speed (VNO) is __ KIAS.\n\n

129 KIAS\n\n

Fuel capacity for the Cessna 172S is __ gallons.\n\n

56 gallons\n\n

Flaps should be set to __ degrees for short field takeoff.\n\n

10 degrees\n\n

The stall speed with flaps up for the Cessna 172S is __ KCAS.\n\n

53 KCAS\n\n

The aircraft is powered by a _ engine.\n\n

Lycoming IO-360-L2A engine.\n\n

The Cessna 172S has a maximum takeoff weight of __ pounds.\n\n

2550 pounds\n\n

The primary flight instrument data is displayed on the __.\n\n

Primary Flight Display (PFD)\n\n

POH stands for __.

Pilot's Operating Handbook

The POH is legally considered part of the aircraft's __.

airworthiness requirements

Information on operating limitations can be found in Section __ of the POH.

2

Performance data for the aircraft is found in Section __ of the POH.

5

Normal operating procedures are detailed in Section __ of the POH.

4