767 Flight Deck a nd Avionics
Ja nua ry 2002
767 Size Comparison
767-200ER/-300ER/-400ER
767-200ER
767-300ER
156 ft 1 in
(47.57 m)
767-200ER
61 ft 1 in
(18.60 m)
52 ft 0 in
(15.8 m)
64 ft 7 in
(19.6 m)
155 ft 0 in
(47.2 m)
767-400ER
170 ft 4 in
(51.92 m)
767-300ER
52 ft 0 in
(15.8 m)
61 ft 1 in
(18.60 m)
74 ft 8 in
(22.76 m)
176 ft 1 in
(53.67 m)
767-400ER
55 ft 4 in
(16.8 m)
85 ft 10 in
(26.1 m)
201 ft 4 in
(61.37 m)
797-FD-0052C
1-18-2-MT/CF
767 Evolution
767-400ER
450,000 lb (204,120 kg)
767-300ER
412,000 lb (186,880 kg)
(767-400ER covered in
separate book)
767-300 Freighter
412,000 lb (186,880 kg)
767-300ER
387,000 lb (175,540 kg)
767-300*
351,000 lb (159,210 kg)
767-200*
767-200*
767-200ER
767-200ER
300,000 lb (136,080 kg)
315,000 lb (142,880 kg)
351,000 lb (159,210 kg)
395,000 lb (179,170 kg)
*No longer offered.
797-FD-0053C
1-18-2-MT/CF
BOEING PROPRIETARY
797-FD-0054C
11/27-0-MT
Boeing Flight Deck Design Philosophy
• The pilot is the final authority for safe airplane
operation; the hierarchy of tasks is
• Safety
• Passenger comfort
• Efficiency
• Automation is applied as a tool to aid but not
replace the pilot
• New technology is used only when there is a
clear advantage with no adverse impact on
human-machine interface
• System designs are error tolerant; the hierarchy
of design alternatives is
• Simplicity
• Redundancy
• Automation
• Designs address fundamental human strengths,
limitations, individual differences, and pilots’
past operational experience
797-FD-0055C
1-18-2-whp/CF
757/767 Commonality
Design Features
• Similar handling characteristics
• Same crew procedures
• Identical recall items
• Identical aural warnings
• Similar checklists
• Similar visual alerts
• Same flight deck arrangement
• Windshield
• Main instrument panel
• Overhead panel
• Aislestand
• Glareshield panels
• Panels/controls
- Location
- Arrangement
- Nomenclature
• Initial and recurring training will
qualify crew for both airplanes
Pilots’ main
instrument panel
No. 1
windshields
Flt
kit
Captain’s
seat
First
Officer’s
seat
Flt
kit
Aislestand
Overhead panel
• Same flight training simulator can
be used for both airplanes
797-FD-0056C
1-18-2-whp/CF
767 Flight Deck - Genera l
Flight Deck and Forward Cabin
767-200ER/-300ER Passenger
First Observer
First Officer
Galley
Closet
Galley
Lavatory
Captain
Second Observer
(optional)
STA
239
797-FD-0058C
1-18-2-MT/CF
Flight Deck and Forward Cabin
767-300 Freighter
STA
273.5
Supernumerary seats
First Observer
(track mounted)
Lavatory
First Officer
Rigid barrier
Access door
to cargo bay
Captain
Galley
Entry door
STA
360.7
797-FD-0059C
1-18-2-MT/CF
Flight Deck Accommodations
767-200ER/-300ER Passenger
• Emergency evacuation can be
accomplished through the
no. 2 side windows.
Hat stowage
Fire extinguisher,
crash axe, and
spare bulb stowage
Coat stowage
• Flight deck escape ropes are
attached to the airplane structure
above each sliding window. They
are stowed in compartments in
the overhead lining above the
pilots’ seats.
Portable light
First Observer’s seat
• Oxygen mask, smoke goggles,
and life vest are located at each
crewmember station.
Suitcase stowage
Coat stowage
Second
Observer’s
seat (optional)
Suitcase
stowage
Captain’s seat
Flight kit stowage
(2 places)
797-FD-0067C
1-18-2-whp/PW
Flight Deck Accommodations
767-300 Freighter
Coat and
hat stowage
Lavatory
Overhead stowage
Spare bulb stowage
Supernumerary
seats (3)
Main deck
cargo door
control panel
Galley
First
Officer’s
seat
Captain’s
seat
Life raft stowage
Fire extinguisher
Suitcase
stowage (2)
Illuminated step
797-FD-0068
1-18-2-whp/CF
Pilots’ Main Panel
767-200ER/-300ER
Standby magnetic compass
Mode control panel
VOR (2)
Lighting
controls (2)
15
12
E
NS
A /T A RM
F
R
E
Q
W ARN IN G
C
R
S
HD G
L NAV
3 3 0
SEL
1 2 6
V NAV
OFF
AU TO
Master caution and
warning lights (2)
EW
V ERT SP D
A LT
0 0 0 0
3 2
0
A /P E N GAG E
L
0 0
B CRS
CM D
C
R
CM D
CM D
CWS
CWS
F/D
ON
F
R
E
Q
OFF
EPR
CAU TI ON
I A S/M AC H
F/D
ON
6
5
N ORM
MAN
SPD
FL CH
S EL
25
BA NK
L IM I T
DN
CW S
L OC
HOLD
V /S
H OL D
C
R
S
W ARNIN G
CA UTI ON
OFF
A PP
A UT O
MAN
D IS ENGA GE
UP
VO R/DM E
V OR/D ME
CLOCK
CL OCK
PAN EL
PAN EL
O FF
O FF
C HA RT
FLOO D
OFF
MA P
PT T
Engine indication
and crew alerting
system (EICAS)
Standby
attitude indicator
Autoland
status (2)
Instrument source
select (2)
HD G S E L
L AN D 3
FD
1
CAUT ION
2
CA NC EL RECA LL
B R AKE
TEM P w
1. 6 3
1 .4
MA C H
8
R
AS
W INDSHEA R
r
2
GS
1 013
6
70 0
599
B A RO
5
3
I N.HG
0
0
.5
LGA K JF KJ F K
K LGA
40
EF I
S TW
B WZ
SB J
K ILMR
1 20 00
1
50
V
7
10
A LT N
w
Radio distance
magnetic indicator
(RDMI) (2)
A DE
AB E
WA RN T
12000
2
40
AL T
MB
1 013
6
B RA K E
S OU RCE a
ET /C HR
T
MU I K
20
BAR O
I N. HG
5
2 9 92
4
1
P/RS T
L AN D 2
2
3
T HR H LD
V N AV P TH
HD G SE L
g
A LT
UP
RETR ACT
27 0 K
584
w
1
IN N ER/
A IRW A YSw
2
R
5 83
L EAD I N G T RA IL I NG
ED GE
EDGE
a
M B A LT
IN
OP
MO
a
1013
6
K N OTS
FLA P LI MI T I AS
22 0K
EGT
A S
OFF
.7 30
GS
70 0
B ARO
5 99
5
IN.H G
M ID DL E
3
a
29 92
4
O U TER
b
650
EG T
N2
C
15
L
19 5K
20
EX TE ND OR
EX TE NDE D
27 0K -.8 2M
25
30
6 50
10 55
.
23 2
L E NG
O IL PR ES S
R E NG
OI L P RE S S
a
a
A U TO
B RA K E Sa
95
A UT O B RA K ES
2
3
1
P RE SS
1 90 K
DN
V ER TI CA L
S PE ED
LOCK OVR D
2 52
T RK
M
08 35 .4
0
Z
4
C D U- L
6
OFF
N AV
F MC-L
F MC -R
10 00 FP M
DM E -L
A L TN GE A R
EX TE ND
25 0K -.7 5M
20
.5
DM E-R
K TEB
O FF
4
1
J FK
L GA KJ FK
K L GA
2
K E WP
T E MP
13
Q TY
30
7 .0
LE
SAX
DN
TE
A LT N
w
w
A L TN
G ND P RO X
w
M MU
K ILM R
12 00 0
40
FF
N1
0 .5
V IB
16 7 3 43
AM B O
CO L
25
NORM
7 .0
13
OIL
N2
0 .5
RT O
2
1
.5
4 .4 NM
AL T N FL AP S
5
15
UP
N2
1 18
OIL
MA X
A U TO
OF F
1
2 32
OIL
11 8
4
DI SA RM
95
I N ST R SOU RCE S EL
F L T D IR
R
2 10 K
5
UP
FL AP S
F LA P OV RD
GE AR O V R D
TE RR O V RD
ST W
BW Z
S BJ
CHR
BL M
ALT N
60
EF I
10
GM T
E T/CHR
OV RD
w
OV RD
w
w
OVR D
K T TN
A RB
1 20 00
K PN EM
w
w
w
w
50
RE V
HA RR Y
w
40
ALT N
20
w
I RS
RU N
UI
RU N
30
HL D
w
H LD
H LD
SS
SS
R ESE T
0
9
8 N EG
RU N
30
HLD
FD
M A C H
11 14
.
Marker beacon
lights (2)
1
TEST
NO AU TOL N D
1
2
w
RU N
20
CR Z
X 1 00 0
0
a
1055
.
a
60
REV
H ARRY
K TTN
ARB
12000
KP NE
I RS
w
PS I
RIGH T
g
CL B
CON
a
PR OX
G/S I NH B
a
N1
ON
1
w
8
L EFT
TO
GA
PRESS
EPR
11 14
.
T
0
9
ON
V A LV E
G MT
w
GN D
a
FMC
a
Altimeter (2)
AU TOL AN D STA TUS
B RA K E
4
3
1 62 K
RE S E RV E
B K S & ST RG
2
CH R
g
MA C H
AU T O
B LM
25 9
167 343
A MB O
COL
G
E
A
Ra
a
T EM P SE L
88. 3
1
160
18 0
200
TA IL
SK ID
NOSE
N1
2 40 K
140
4
K E WP
M MU
079
K T EB
w
6
1 .0
D
O
O
R
Sa
2
1 .8 1 .47
1 .4
EP R
8 8.2
r
10 00 FP M
DME -R
SA X
w
250
24 0
2 20
4
OF F
A UTO
PI LOT
a
120
K NO TS
TRUE
r
OV SPD
r
80
100
IA S
3 00
2
VER TICAL
SPEED
.5
TR K
D M E-L
A LT N
60
40 0
35 0
FM C-R
A LT N
A/T
DIS C
b
R
NA V
FM C-L
AL T
A LERT
a
OU T E R
29 92
4
C
1
CA BI N
A LT
a
B /CRS
M ID DL E
MB A LT
.73 0
S PEED
BRA K ES
IL S
OF F
1. 63
Thrust
management
r
A/ P
DI SC
P UL L UP
r
INN E R/
A IRWA Y Sw
1. 0
CONF IG
r
AL T
w
1
N EG
IN
OP
K N OTS
FLT D IR
L
C D U-L
CRZ
1 .8 1.47
FI RE
0
9
MA C H
WH L W EL L
FIRE r
T AT - 4 6 C
TE S T
g
N O LA ND 3
a
MO
IN ST R SOUR CE SE L
VN AV PT H
Electronic attitude
director indicator
(EADI)
REG
SEL CAL
H DG REF
NORM
AU T OLA N D ST AT US
P /RS T
T HR H LD
Heading
reference
25 9
MAP
0 79
O FF
P TT
Mach/airspeed
indicator (2)
CH ART
Miscellaneous warning,
caution, and advisory lights
FL O O D
FS
20
A DE A B E
W AR NT
120 00
FS
R ES ET
AI R
D AT A
AI R
DA T A
ALT N
w
w
w
Reserve brakes
and steering
Vertical speed
indicator (2)
Standby airspeed
Standby altimeter
Standby engine indicator
Autobrakes
Clock (2)
Alternate gear
Alternate flaps
Flap position indicator
Enhanced ground
proximity warning
system (EGPWS)
override
Electronic horizontal
situation indicator (EHSI)
797-FD-0060C
1-18-2-whp/CF
Overhead Panel
767-200ER/-300ER
Emergency lights
Miscellaneous annunciation
Cargo heat
Engine start
Passenger oxygen*
Window heat
E N TRY
DO ORS
CA PT
PI TOT
EM ER
DO ORS
CA RGO
DOOR S
A CCESS
DOORS
F O
P IT OT
L A OA
R A OA
L AUX
PI TOT
R AUX
PI TOT
S TA B
T RI M
SP OI LE RS
U N SCHE D
S TA B TRI M
R U DDER
RA T I O
I RS MODE SEL
W
TK /GS
Inertial reference
1
HD G
W
4
H
5
E
6
7
S
8
9
EN T
0
CLR
ON
A N T I SK I D
B U LK
ON
ON
OV H T
OV H T
L
PRE SS
C
R
A L IGN
A LI GN
ON DC
ON DC
ON DC
DC FA I L
DC FA I L
D C FA IL
FA U LT
N A V A TT
R
FWD
FWD
SI DE
ON
ON
ON
ON
I N OP
I NOP
I NOP
IN O P
I NOP
A LI GN
I N OP
FW D CA B
A U TO
I N OP
M ID CAB
A U TO
B OTH
L
R
2
1
V A LV E
VALVE
C
N A V A TT
OFF
C
W
GN D
A U TO
OFF
AUT O
GN D
OFF
C ON T
CONT
FL T
FL T
L
R
ON
ON
BAT
P
I
M
A
R
N ORM
A LT N
SY S
PR ES S
SY S
PR ES S
SYS
P RE SS
QT Y
Q TY
QTY
ON
ON
OFF
IN OP
I N OP
ON
P RES S
OV H T
OV HT
OV H T
Y
EL E C
AIR
P RES S
P RES S
D
VALVE
P RES S
A FT
FWD
ON
R
ON
OFF
P
R
E
S
S
FU EL
CO N FI G
L
P
R
E
S
S
OV H T
A U TO
D
O FF
ON
OFF
ON
OFF
ON
N
O
F
F
ON
DRI V E
DR I V E
LB
KG
ON
TEMP
DE SCE ND
R
034 0
80
20
0
S TAR T
RUN
V AL VE
0
10
8
ENGI NE
L
R
ON
ON
VAL VE
V AL VE
6
PSI
DI FF
OFF
Electrical
L OW
1 2
1 2
FT X
1000
A LT
L EN G
0
FPM X
RAT E 10 00
O
F
F
APU
V
A
L
V
E
OVH T
R EN G
Fuel jettison
O
F
F
VA LV E
AU T O
PRESS DIFF
LI MI T : T /O &
LD G .1 2 5 PSI
ST BY
OVH T
OVRD
SM OKE
NO
COOL I N G
H I GH
COCK P IT VO I CE RECORDER
DU CT
L EAK
B LEED
A DP
EQUI P CO OLI N G
CAB IN
AL TIT U DE
WI PER
ER A SE
T ES T
V
A
L
V
E
DL
UE
CA
T K
OVH T
0
2
25
4
20
15
6
10 8
2
4
Bleed air and
pneumatic
MAN
CA BI N
R
VAL VE
VAL VE
B L EED
ON
L
R I SL N
C ISLN
KG
TOTAL
WI NG ANT I-I CE
ON
FA UL T
H EAD PH ON E
CK T B K R
OVH D PAN E L
D OM E
Cabin altitude
PA NEL /FL OOD
GL A RE SH I E LD
A IS LE STA N D
LT OV RD
AN TI
COL LI SI O N
POSI TI ON
R ED
ON
OFF
OFF
ON
WI N G
OFF
WH I T E
ON
ON
OFF
L OGO
ON
L
OFF
OFF
FL T D K D OOR
ON
U NL K D
TA X I RU N WA Y T U RN OFF
U NL K D
R
Fuel
Equipment cooling
LA NDI NG
L
WI N G
N O SE GE A R
R
ON
Miscellaneous lighting
M ODE S EL ECT
A U TO 2
AUT O 1
LB
S
T
B
Y
DUCT
PRESS
PSI
L ISLN
V AL VE
A UT O I N OP
R
LB
KG
FUEL QTY
X 10 0 0
C
D
OFF
Voice recorder
60
MAX
MIN
CL
DU CT
L EAK
GEN
CON T
R
M
O
F
F
C
W
A U TO RA TE
LD G A LT
C
L
R
GEN D RI V E DI SC
L
GE N
CON T
E
A
S
T
B
Y
W
OP
ON
OFF
A PU
APU
M ANUAL
C LI M B
N
OFF
C
V ALVE
PRESS
C P UM PS
ON
BU S
OFF
L
PRE SS
OVH T
A UTO
A U TO
N
OFF
ON
R BUS
R
PA C K
OFF
ON
AUT O
PRE SS
VALVE
I NOP
W
MAN
I SL N
L
BUS
OFF
A
OFF
C
ON
ON
FWD
R ESE T
I NOP
P A CK
OFF
CA BI N AL TI TUDE CONTROL
A U TO
R PA CK
R ESE T
R
PU M P S
U TI LI TY B U S
L B US
M
E L EC
OV HT
A U TO
M
N
FU EL
X FEE D
P RES S
B U S T IE
A VAIL
L P A CK
SE A T B EL TS
A U TO
ON
W
AU TO
AL ERT
Y
E
A
I
L
P UM P S
C
CA LL
PASS SI GNS
OFF
A FT
ON
A L ER T
ON
ON
VALVE
ON
O
F
F
R
ON
PRES S
D
Passenger signs*
I N OP
GN D
A FT
OFF
ON
ON
I SL N
P
ON
PRE SS
OV HT
O
F
F
A U TO
R
EN G
C
1 -EL EC-2
ON
PR ES S
M ID
N O S MOK I N G
A UTO
APU GEN EX T P WR
B U S TI E
FWD
BAT
OFF
OFF
PUMPS
H YD
L
ENG
R
ON
D
I
S
C
H
V A LV E
S TBY POWER
A U TO
R
ELEC
ENG
CO NT
A L TN
Hydraulic
FA U LT
IN OP
L
N ORM
Air-conditioning
W
OFF
L - RE CIR C FA N - R
ON
FLT DK
CA B I N CAL L
FUEL
J ETTI SON
L –N OZ ZL E–R
IN OP
C
W
OFF
T RI M A I R
OFF
Y A W D AMPER
Electronic engine
control (EEC)
Pilot’s call panel
A FT CA B
AUT O
EN G STA RT
FA U LT
N AV A TT
A L I GN
OFF
Compartment
temperature
COM PT TEM P
WI NDOW H EAT
UN L K D
L
OFF
U N A RM E D
ON
A IL
LOC K
RA M A I R TUR B
A L I GN
FA U LT
A L I GN
3
PA SS OX Y
OFF
A R ME D
A UT O
S PDB RK
SI DE
SYS DSPL
C
L
R
Yaw damper
N
2
EMER L I GHTS
FWD
TA T
N
DSPL SEL
PPOS
WIN D
CA RGO HEA T
OFF
OFF
ON
ON
I N D L TS
DI M
B RT
T EST
Wing/engine anti-ice
Windshield controls
*Passenger airplanes only.
797-FD-0061C
12-5-1-whp