CSP–FF–1
ROTORCRAFT FLIGHT MANUAL
Additional Operations
and Performance Data
MD 530F Plus
(Model 369FF)
Revision 5
8–4
−30
−20
−10
0
10
20
30
40
50
OA
T − DEG C
2600
2800
3000
3200
3400
3600
3800
GROSS WEIGHT
− LB
NO WIND
HOT
DA
Y (ISA
+ 23 C)
°
REDUCE WEIGHT
CAP
ABILITIES lbs
AS FOLLOWS:
(APPLICABLE T
O ALL
TEMPERA
TURES)
PRESSURE
AL
T. FT
.
CABIN
HEA
T
ANTI−
ICE
BOTH
SL
T
O 6000
8000
12000
16000
0
0
0
90
0
0
335
450
0
100
510
603
MAXIMUM GROSS WEIGHT
INTERNAL
LOAD OPERA
TION
F40–036
CONTROLLABILITY
LIMIT
− 3 PERCENT
PEDAL
MARGIN IN 17− KT
SIDEWIND FROM
THE RIGHT
REAR QUAR
TER
INCREASE (OR DECREASE) WEIGHT
CAP
ABILITY
POUNDS (ABOVE CRITICAL
AL
TITUDE) PER 10
AMPERE REDUCTION
(OR INCREASE) IN ELECTRICAL
LOAD
OA
T, C
−5
15
35
WEIGHT
3
9
14
D
°
CAUTION: ADEQUA
TE
COOLING
HAS BEEN DEMONSTRA
TED UP
TO
8800 FT
FOR HOT
DA
Y (ISA
+ 20 C)
°
AVOIOD PROLONGED HOVER
ABOVE
THIS AL
TITUDE.
EXAMPLE:
PRESS.
AL
T −−−−−−−−− 8000 FT
OA
T−−−−−−−−−−−−−−−− 6 C
°
ENTER CHAR
T A
T 6 C ON OA
T SCALE
MOVE UP
TO
10,000 PRESS.
AL
T LINE,
MOVE RIGHT
TO
GROSS WEIGHT
LINE,
READ HOVER GROSS WEIGHT
= 3290 LB
°
SCA
VENGE AIR
ON
Figure 8–3. Hover Ceiling, OGE, Engine Air Particle Separator Inlet with
Mist Eliminator
