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FUSELAGE FUEL GRAVITY FILL ACCESS DOOR
The fuselage fuel gravity fill access door is located on the right side of
the fuselage. This door is hinged at the top, has a spring-loaded latch at
the bottom edge, and opens upward. The fuselage fuel gravity filler
port is installed behind the door. The fuselage fuel gravity filler cap is
tethered to the airplane with a lanyard to prevent dropping or
misplacing it.
SINGLE-POINT PRESSURE REFUELING ACCESS DOOR
The Single-Point Pressure Refueling (SPPR) access door is located on
the fuselage below the right engine pylon. The SPPR adapter and
precheck valve lever are installed behind this door. The door is hinged
at the bottom and is secured with two spring-loaded latches near the
top of the door.
SINGLE-POINT PRESSURE REFUELING CONTROL PANEL ACCESS
DOOR
The Single-Point Pressure Refueling (SPPR) control panel access door is
located aft of the SPPR access door on the right side of the fuselage. The
refueling control panel access door is hinged at the lower edge and
opens down from the top.
OIL SERVICING DOORS
The oil servicing doors are located on the forward outboard side of each
engine nacelle. The oil quantity sight gauge (on the right nacelle) and
dipstick (on the left nacelle) are accessed through the oil servicing
doors. The doors are hinged at the bottom and are secured by two
spring-loaded latches at the top of each door.
Pilot’s Manual
PM-132A 1-23
TURNING RADIUS
Figure 1-13
37 ft 10 in
(11.53 m)
27 ft 10 in
(8.48 m)
NOSE WHEEL
WING TIP
NOTE: Turning radius expressed above is based upon 60° nose-wheel
deflection.
Pilot’s Manual
1-24 PM-132A
NOTE:
Engine exhaust danger areas are
shown for idle RPM. Values are
approximately double for takeoff RPM.
40 ft (12.19 m) from tailpipe 100° F (38° C)
ENGINE INTAKE
12 ft (3.66 m)
from intake
ENGINE INTAKE
12 ft (3.66 m)
from intake
WEATHER RADAR
15 ft (4.57 m)
ENGINE EXHAUST
750° F (399° C)
at tailpipe
DANGER AREAS
Figure 1-14
Pilot’s Manual
PM-132A
2
4
8
1
23 49
S L CT ON R L
D V RON
M 50
CH ONO ET R
H AD HO E
I
D
B TH
V
O
I
C
E
1 2
F1
NA 1 N V2 AD 1 DF2
MKR MUTE
VH 1 HF2
NPH
DM
PE KER
H 2 CO 3 PA
LS
H l
S D
MNM MS ARO
AB RO
L NG
Y ON
O HT
B E D
AR
EAK
R ENG
PY ON
VHT
R F EL
PR SS
OW
R OL
RE S
L W
L U L
P E S
L W
O L
P E S
LOW
EAR
T B
VHT
WNG
OV T
R EV
UN A E
L AK
B E D
R
L AK
R B TT
VHT
MER
B TT
L B TT
VHT
GE F IL
NORM L
RA ES
A L
R V
NS FE
EA PH NE
2
4
6
AB RO S D
SQ MNM MS B RO
TUNE
DME
STO
TST
1 2
GE
D M
D
0
0
5
0
5 20
16
4
2
10
6
01
V B
P
A T
D 2
NORM
FD
U H
C S/
FD
EV
AV
OFF
BRG
IM
FPA WX FMS
MS1
FF
N V1
ADF1 A F2
N V2
MS2
CUE
n
hPa
BRG
HSI
PU H
O
TE T
NBD
DU DU
OU BD
HDG
PP
NK
N V LT
PU H SYNC P SH SYNC P SH AS M SH SYNC
YD
FR
AP SPD LC
VS
V
RS 2
CRS 1 HDG SPD ASEL
HSI
USH
TO
EST
NBD
DU
OUTBD
DU
NAV
OFF
BRG
DM
FPA WX MS
1
O F
N V1
A F1 ADF
NA 2
FM 2
E
In
Pa
D
REE
O D
P X XYGEN
R
C R
F
AHRS
L VE
NV RONM NTA CON ROL
OFF
R DDER
ED L
L
E D NG
R REW
I HTS
FWD
N TR
FF
FF
C LD OT
F
CB AN L
ED S AL
VR D
MANU L
T MP
OT
C B N PR SSU E CON ROL
DG A T
DN
12
FPM
S D
1 00
3 5 0
C B A T
D L A P
C B R TE
3 T
UP
MANUAL
N UP
L GH S RE SU I ATON
OWN D WN
OWN
V E
2 0
V O
2 0
O F
F
R DG
F FF
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