Performance Data
CSP–FF–1
ROTORCRAFT FLIGHT MANUAL
MD 530F Plus
(Model 369FF)
Revision 5
5–11
FAA Approved
F40−037A
CONTROLLABILITY
LIMIT
− 3 PERCENT
PEDAL
MARGIN IN 17− KT
SIDEWIND FROM
THE RIGHT
REAR QUAR
TER
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
NO WIND
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
°
−30
−20
−10
0
10
20
30
40
50
OA
T − DEG C
2600
2800
3000
3200
3400
3600
3800
GROSS WEIGHT
− LB
EXAMPLE:
PRESS.
AL
T −−−−−−−−−8000 FT
OA
T−−−−−−−−−−−−−−−−12 C
°
ENTER CHAR
T
AT
12 C ON OA
T SCALE
MOVE UP
T
O 8000 PRESS
AL
T LINE
MOVE RIGHT
T
O GROSS WEIGHT
LINE,
READ HOVER GROSS WEIGHT
= 3580LB
°
MAXIMUM GROSS WEIGHT INTERNAL
LOAD OPERA
TION
HOT
DA
Y (ISA
+ 23 C)
°
CAUTION: ADEQUA
TE
COOLING
HAS BEEN DEMONSTRA
TED UP
T
O
8800 FT
FOR HOT
DA
Y (ISA
+ 20 C)
°
AVOID PROLONGED HOVER
ABOVE
THIS AL
TITUDE.
Figure 5–6. Hover Ceiling IGE, 3.5–Foot Skid Clearance
Extended Landing Gear, Standard Engine Inlet
