 |
|||
|
|
|||
| ||||||||||
|
| MIL-D-23222A(AS)
3.3.5.1
(Cont)
(1) General. -
(a) Functional checks of all installed and oper-
ating equipment in the test helicopter
(power-plant, flight-control, hydraulic,
electrical, avionic, instrument, arnanebtm
photographic, and other important Systems)
for conformance with the design missions
of the helicopter.
(b) Evaluation of equipment installations in each
Cockpit.
(2) Handling Qualities. - Evaluation of longitudinal,
lateral, and directional stability and control at
basiC design gross weight and mid-cg as follows:
(a) Taxi, ground handling, and mechanical instabi-
lity characteristics.
(b) Takeoff and landing Characteristics, including
hovering, sideward and rearward flight, climb
out,and and transition Characteristics.
(c) Hydrodynamic characteristics, including take-
Off, hovering in ground effect, landings,
taxiing, trim-angle limits, and spray character-
istics as applicable.
(d) Hover, climb, cruise, maneuvering, descent,
and autorotative characteristics, including
effects of power, and configuration changes.
(e) Buffet, vibration, and noise characteristics
in steady unaccelerated flight in 10 knot
increments from hover to maximun permissible
airspeed.
(f) Control characteristics with alternate and
emergency system in operation as appli-
cable.
(g) Other applicable item that may be specifi-
cally requested by NAVAIR.
23
|
|
Privacy Statement - Press Release - Copyright Information. - Contact Us |
Click
here for thousands of PDF manuals