kpayne on VMOFRWIN702 with $$_JOB

Federal Aviation Administration, DOT

Pt. 60, App. A

g. Visual Scene - Ground Assessment. Select 3
different airport models and perform the following checks with Day, Dusk and Night selected, as appropriate:
(1) Visual Controls.
(a) Daylight, Dusk, Night Scene Controls.
(b) Flight deck  - Daylight -  ambient lighting.
(c) Environment Light Controls.
(d) Runway Light Controls.
(e) Taxiway Light Controls.
(2) Airport Model Content.
(a) Ramp area for buildings, gates,
airbridges, maintenance ground equipment,
parked aircraft.
(b) Daylight shadows, night time light
pools.
(c) Taxiways for correct markings, taxiway/runway, marker boards, CAT I and II/III
hold points, taxiway shape/grass areas, taxiway light (positions and colors).
(d) Runways for correct markings, lead-off
lights, boards, runway slope, runway light
positions, and colors, directionality of runway lights.
(e) Airport environment for correct terrain
and significant features.
(f) Visual scene quantization (aliasing),
color, and occulting levels.
(3) Ground Traffic Selection.
(4) Environment Effects.
(a) Low cloud scene.
(i) Rain:
(A) Runway surface scene.
(B) Windshield wiper - operation and sound.
(ii) Hail:
(A) Runway surface scene.
(B) Windshield wiper - operation and sound.
(b) Lightning/thunder.
(c) Snow/ice runway surface scene.
(d) Fog.
h. Takeoff. Select one or several of the following test cases:
(1) T/O Configuration Warnings.
(2) Engine Takeoff Readings.
(3) Rejected Takeoff (Dry/Wet/Icy Runway)
and check the following:
(a) Autobrake function.
(b) Anti-skid operation.
(c) Motion/visual effects during deceleration.
(d) Record stopping distance (use runway
plot or runway lights remaining).
Continue taxiing along the runway while
applying brakes and check the following:
(e) Center line lights alternating red/white
for 2000 feet/600 meters.
(f) Center line lights all red for 1000 feet/300
meters.
(g) Runway end, red stop bars.
(h) Braking fade effect.
(i) Brake temperature indications.
(4) Engine Failure between VI and V2.
(5) Normal Takeoff:
(a) During ground roll check the following:
(i) Runway rumble.
(ii) Acceleration cues.

(iii) Groundspeed effects.
(iv) Engine sounds.
(v) Nosewheel and rudder pedal steering.
(b) During and after rotation, check the
following:
(i) Rotation characteristics.
(ii) Column force during rotation.
(iii) Gear uplock sounds/bumps.
(iv) Effect of slat/flap retraction during
climbout.
(6) Crosswind Takeoff (check the following):
(a) Tendency to turn into or out of the
wind.
(b) Tendency to lift upwind wing as airspeed increases.
(7) Windshear during Takeoff (check the
following):
(a) Controllable during windshear encounter.
(b) Performance adequate when using correct techniques.
(c) Windshear Indications satisfactory.
(d) Motion cues satisfactory (particularly
turbulence).
(8) Normal Takeoff with Control Malfunction.
(9) Low Visibility T/O (check the following):
(a) Visual cues.
(b) Flying by reference to instruments.
(c) SID Guidance on LNAV.
i. Climb Performance. Select one or several
of the following test cases:
(1) Normal Climb - Climb while maintaining recommended speed profile and note fuel,
distance and time.
(2) Single Engine Climb - Trim aircraft in a
zero wheel climb at V2.
NOTE: Up to 5Section bank towards the operating
engine(s) is permissible. Climb for 3 minutes
and note fuel, distance, and time. Increase
speed toward en route climb speed and retract flaps. Climb for 3 minutes and note
fuel, distance, and time.
j. Systems Operation During Climb.
Check normal operation and malfunctions
as appropriate for the following systems:
(1) Air conditioning/Pressurization/Ventilation.
(2) Autoflight.
(3) Communications.
(4) Electrical.
(5) Fuel.
(6) Icing Systems.
(7) Indicating and Recording Systems.
(8) Navigation/FMS.
(9) Pneumatics.
k. Cruise Checks. Select one or several of
the following test cases:
(1) Cruise Performance.
(2) High Speed/High Altitude Handling
(check the following):
(a) Overspeed warning.
(b) High Speed buffet.
(c) Aircraft control satisfactory.

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