 |
|||
|
|
|||
| ||||||||||
|
| MIL-D-23222A(AS)
3.3.5.1
(CONT)
Performance. - Items of paragraph 3.8.3, item
(3)
specified by NAVAIR in the addendum to this speci-
fication for the particular model helicopter at
the basic design gross weight and normal c.g.,
and the following:
Vmax at sea level.
(a)
Maximum rate of climb in forward flight at sea
(b)
level with NRP.
Power required to hover out of' ground effect at
(c)
sea level.
(d] Rate of descent in steady state automation at
various Combinations of forward speed and roter Speed.
Mission profile and preliminary cruise control.
(e)
Service ceiling with NRP.
(f)
Other items not included above that are contract
(g)
guarantees.
(4)
Special Equipment. - All installed and operating
special equipment such as photographic, armament,
sonar, and rescue and cargo hoists, shall be tested
or checked for safe and proper functioning, and
ability to perform the mission intended within the
limitations of the established flight envelope.
The applicable functional tests listed in 3.3.5.2.8.2
and 3.3.5.2.9.2 shall be used as guides by COMNAVAIR-
tESTCEN to accomplish the desired test program.
3.3.5.2
REQUIREMENTS PRIOR TO PHASE-I NAVY PRELIMINARY
EVALUATION
FLYING QUALITIES . - The contractor shall have
3.3.5.2.1
demonstrated safety of flight throughout the
flight envelope under the following conditions:
(1) Takeoffs, hovering, landings, sideward and rearward
flight, autorotative characteristics with power
recoveries, one-engine-out landings for multi-engine,
and autorotative landings for single-engine helicopters
in accordance with tests (b), (c. 1 to 20 knots, c.2,
c.3), (d), (f.1b) and (p) of Table 3.
24
|
|
Privacy Statement - Press Release - Copyright Information. - Contact Us |
Click
here for thousands of PDF manuals