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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-126A 1-23
TURNING RADIUS
Figure 1-13
NOTE: Turning radius expressed above is based upon 60° nose-wheel
deflection.
39 FT 4 in
(12.0 m)
NOSE WHEEL
WING TIP
30 FT 1 in
(9.17 m)
A09-2001
Pilot’s Manual
1-24 PM-126A
15 feet
(4.57 m)
12 feet (3.66 m)
from intake
12 feet (3.66 m)
from intake
750° F
(399° C)
ENGINE EXHAUST
ENGINE INTAKE
WEATHER RADAR
100° F
(38° C)
40 feet (12.19 m) from tailpipe
APU INTAKE APU EXHAUST
Exhaust danger area
shown for idle RPM.
Values approximately
double for takeoff RPM.
DANGER AREAS
Figure 1-14 A06-7001
Pilot’s Manual
PM-126A 1 - 11/ 1 - 12 (Blank)
1.0
.2
.4
.6
.8
.2
.4
.6
.8
1.0
ON
1
2
3
4
5
6
8
9 10 11 12 13 14 15 16 17
18
19
21
22
23
24
25
26
35 34 33 32 31 30 29 28 27
7 20
12--295//21--1206 ((BBllaannkk))
INSTRUMENT PANEL (TYPICAL)
Figure 1-15
1. Pilot’s Rudder Pedal Adjustment
2. Pilot’s Crew Lighting Panel
3. #1 AHRS Mode Control
4. Pilot’s Audio Control Panel
5. Pilot’s Angle of Attack Indicator (opt)
6. Pilot’s Digital Chronometer
7. Pilot’s GPWS Fail Annunciator
8. Pilot’s Primary Flight Display (DU-1)
9. DU-2 Reversion Panel / Master Warning
Flashers
10. Pilot’s Display Controller
11. EICAS Display (DU-2)
12. Flight Guidance Controller
13. Standby Instruments
14. Crew Warning Panel
15. Cockpit Voice Recorder Microphone
16. Copilot’s Display Controller
17. Multi-Function Display (DU-3)
18. DU-3 Reversion Panel / Master Warning
Flashers
19. Copilot’s Primary Flight Display (DU-4)
20. Copilot’s GPWS Fail Annunciator
21. Copilot’s Digital Chronometer
22. Copilot’s Angle of Attack Indicator (opt)
23. Copilot’s Audio Control Panel
24. #2 AHRS Mode Control
25. Copilot’s Crew Lighting Panel
26. Copilot’s Rudder Pedal Adjustment
27. Cockpit Voice Recorder Panel
28. Environmental Control Panel
29. Cabin Pressurization / Oxygen Control Panel
30. Landing Gear / Hydraulic Control Panel
31. Radio Management Units
32. Aircraft Light Control Panel
33. Anti-Ice Panel
34. Reversion Control Panel
35. Electrical Control Panel
Updated 8-29-97 1:45 pm
updated graphic
A31-1001

Pilot’s Manual
PM-126A 1-27
A31-1001a
PEDESTAL (TYPICAL)
Figure 1-16
ON
1 2
3
4
5
6
7
8
10
11
12
13
14
19
20
21
22
23
24
25
15
18
GO AROUND MUTE
}
Optional
Pedestal
Extension
16
17
9
1. Pitch Trim Bias
Switch
2. Clearance Delivery
Radio (CDR)
3. Gear Freefall Lever
4. Ground Proximity
Warning System
Switches (opt)
5. Thrust Reverser
Levers
6. Thrust Levers
7. Flap Lever
8. MFD Joystick
9. HF Control Panel
10. SELCAL Panel (opt)
11. APU Control
Panel (opt)
12. ELT Switch
Panel (opt)
13. Weather Radar
　
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