Van's Aircraft RV 12iS, Production Acceptance Procedures

Page: 32 / 50

Revision: 2.3 Date: 10/30/20
F1-2
FLIGHT PROCEDURE (continued):
Systems Checkout:
Engine Indications:

Oil Pressure indicating and within limits:

Oil temperature indicating and within limits:

Cylinder Head Temperature L indicating and within limits:

Cylinder Head Temperature R indicating and within limits:

(ULS) Exhaust Gas Temperature L & R indicating and within limits:

(iS) Exhaust Gas Temperatures indicating and within limits:
1
2 3 4

Fuel Pressure indicating and within limits:

(iS) Fuel Flow indicating a reasonable value:

All voltages indicating and within limits:

Amperage indicating and within limits:
Engine Power Output:

RPM appropriate during various phases of flight

No unusual vibrations, noises, etc.

No fuel or exhaust smell in cockpit
EFIS Indications:

Airspeed

Altitude

Slip/Skid indicator - ball moves opposite direction of rudder input

Attitude

Outside Air Temperature
Avionics:

Comm radio functionality

GPS functionality

Intercom (Check for side tone)

Transponder
Initial Flying Qualities Evaluation:
Control Response appropriate?

Pitch

Roll

Yaw
Control Forces appropriate?

Pitch

Roll

Yaw