Van's Aircraft RV 12iS, Процедуры приемки продукции

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Revision: 2.3 Date: 10/30/20
F4-2
Section F4 - Flight Test Card - Flight #4 Aircraft Registration:___________
FLIGHT PROCEDURE (continued):
Set altimeter to 29.92 in Hg.
Climb or descend as required to achieve 7500 ft density altitude, set throttle to 5500 RPM and
establish level flight. Allow airspeed to stabilize. Fly a 4-way speed box and fill in table.
(Optional: This may be accomplished using the autopilot.)
NOTE: Data recording for this task can be accomplished by extracting data from EFIS data log.
5500 RPM CRUISE PERFORMANCE @ 7500 ft DENSITY ALTITUDE
GPS GRND TRCK 0 deg 90 deg 180 deg 270 deg DENSITY ALT:
OBSERVED
AIRSPEED (KT)
PRESSURE ALT:
GPS GRND
SPEED (KT)
RPM:
FUEL FLOW
(GAL/HR)
MAP:
EFIS Pitch Offset adjustment:

If required, adjust the Pitch Attitude offset per the EFIS manufacturer’s instructions.
If necessary, climb to no lower than 3,000 ft AGL and establish slow flight at 50 kt full flaps, power
as required to maintain altitude. Allow time for everything to stabilize. Fly a 4 way speed box and
fill in table.
(Optional: This may be accomplished using the autopilot.)
NOTE: Data recording for this task can be accomplished by extracting data from EFIS data log.
50 kt & FULL FLAP AIRSPEED CALIBRATION
GPS GRND TRCK 0 deg 90 deg 180 deg 270 deg DENSITY ALT:
OBSERVED
AIRSPEED (KT)
PRESSURE ALT:
GPS GRND
SPEED (KT)
RPM:
FUEL FLOW
(GAL/HR)
MAP:
Descent:
Set power and re-trim for approx 500 ft/min descent to traffic pattern altitude.
Landing:
Power-off approach at minimum 55 kt with flaps as required for glide path control.