kpayne on VMOFRWIN702 with $$_JOB

Pt. 60, App. A

14 CFR Ch. I (1-1-19 Edition)

(d) Envelope limiting functions on Computer Controlled Aircraft.
Reduce airspeed to below level flight buffet
onset speed, start a turn, and check the following:
(e) High Speed buffet increases with G
loading.
Reduce throttles to idle and start descent,
deploy the speedbrake, and check the following:
(f) Speedbrake indications.
(g) Symmetrical deployment.
(h) Airframe buffet.
(i) Aircraft response hands off.
(3) Yaw Damper Operation. Switch off yaw
dampers and autopilot. Initiate a Dutch roll
and check the following:
(a) Aircraft dynamics.
(b) Simulator motion effects.
Switch on yaw dampers, re-initiate a
Dutch roll and check the following:
(c) Damped aircraft dynamics.
(4) APU Operation.
(5) Engine Gravity Feed.
(6) Engine Shutdown and Driftdown Check:
FMC operation Aircraft performance.
(7) Engine Relight.
l. Descent. Select one of the following test
cases:
(1) Normal Descent. Descend while maintaining recommended speed profile and note
fuel, distance and time.
(2) Cabin Depressurization/Emergency Descent.
m. Medium Altitude Checks. Select one or
several of the following test cases:
(1) High Angle of Attack/Stall. Trim the
aircraft at 1.4 Vs, establish 1 kt/sec 2 deceleration rate, and check the following - 
(a) System displays/operation satisfactory.
(b) Handling characteristics satisfactory.
(c) Stall and Stick shaker speed.
(d) Buffet characteristics and onset speed.
(e) Envelope limiting functions on Computer Controlled Aircraft.
Recover to straight and level flight and
check the following:
(f) Handling characteristics satisfactory.
(2) Turning Flight. Roll aircraft to left, establish a 30Section to 45Section bank angle, and check the
following:
(a) Stick force required, satisfactory.
(b) Wheel requirement to maintain bank
angle.
(c) Slip ball response, satisfactory.
(d) Time to turn 180Section.
Roll aircraft from 45Section bank one way to 45Section
bank the opposite direction while maintaining altitude and airspeed - check the following:
(e) Controllability during maneuver.
(3) Degraded flight controls.
(4) Holding Procedure (check the following:)
(a) FMC operation.
(b) Autopilot auto thrust performance.
(5) Storm Selection (check the following:)

(a) Weather radar controls.
(b) Weather radar operation.
(c) Visual scene corresponds with WXR
pattern.
(Fly through storm center, and check the
following:)
(d) Aircraft enters cloud.
(e) Aircraft encounters representative turbulence.
(f) Rain/hail sound effects evident.
As aircraft leaves storm area, check the following:
(g) Storm effects disappear.
(6) TCAS (check the following:)
(a) Traffic appears on visual display.
(b) Traffic appears on TCAS display(s).
As conflicting traffic approaches, take relevant avoiding action, and check the following:
(c) Visual and TCAS system displays.
n. Approach and Landing. Select one or several of the following test cases while monitoring flight control and hydraulic systems
for normal operation and with malfunctions
selected:
(1) Flaps/Gear Normal Operation. Check
the following:
(a) Time for extension/retraction.
(b) Buffet characteristics.
(2) Normal Visual Approach and Landing.
Fly a normal visual approach and landing - check the following:
(a) Aircraft handling.
(b) Spoiler operation.
(c) Reverse thrust operation.
(d) Directional control on the ground.
(e) Touchdown cues for main and
nosewheel.
(f) Visual cues.
(g) Motion cues.
(h) Sound cues.
(i) Brake and anti-skid operation.
(3) Flaps/Gear Abnormal Operation or with
hydraulic malfunctions.
(4) Abnormal Wing Flaps/Slats Landing.
(5) Manual Landing with Control Malfunction.
(a) Aircraft handling.
(b) Radio aids and instruments.
(c) Airport model content and cues.
(d) Motion cues.
(e) Sound cues.
(6) Non-precision Approach - All Engines
Operating.
(a) Aircraft handling.
(b) Radio Aids and instruments.
(c) Airport model content and cues.
(d) Motion cues.
(e) Sound cues.
(7) Circling Approach.
(a) Aircraft handling.
(c) Radio Aids and instruments.
(d) Airport model content and cues.
(e) Motion cues.
(f) Sound cues.
(8) Non-precision Approach - One Engine
Inoperative.

160

VerDate Sep<11>2014

16:30 Jun 25, 2019

Jkt 247047

PO 00000

Frm 00170

Fmt 8010

Sfmt 8002

Q:\14\14V2.TXT

PC31