B767 Flightdeck and Avionics
February 26, 2017 | Author: oscar | Category: N/A
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767 Flight Deck and Avionics January 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)
(767-400ER covered in separate book)
767-300ER
767-300 Freighter
412,000 lb (186,880 kg)
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 - General
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 Overhead stowage Spare bulb stowage Coat and hat stowage
Lavatory
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 ARM F R E Q
WARNING
C R S
L NAV
3 3 0
VERT SPD
HDG
IAS/MACH
F/D ON
1 2 6
A/P ENGAGE
ALT 3 2 0 0 0
0 0 0 0
L CMD
B CRS
C
R
CMD
CMD
CWS
CWS
F/D ON
F R E Q
OFF SEL
EPR CAUTION
Master caution and warning lights (2)
6
EW
V NAV
OFF
5 NORM
AUTO MAN
SPD
FL CH
SEL
25 BANK LIMIT
DN
CWS
LOC
V/S
HOLD
HOLD
C R S
AUTO MAN
DISENGAGE
UP
VOR/DME
WARNING CAUTION
OFF
APP
VOR/DME
CLOCK
CLOCK
PANEL
PANEL
OFF
OFF
CHART
CHART
FLOOD
Miscellaneous warning, caution, and advisory lights
OFF MAP PTT
PTT
1
Instrument source select (2)
HDG SEL
LAND 3
FD
BRAKE TEMP w
CAUTION
1.63 2
a
1.8 1.47 1.4
TRUE
1.0
D O O R Sa
TAIL SKID
a
NOSE g
G E A R
Altimeter (2)
CLB
CON
CRZ
1
Marker beacon lights (2)
1
PRESS PSI
X 1000
0 2
g
TO GA
AUTOLAND STATUS
BRAKE
4 3
P/RST
LAND 2
TEST
a
1
THR HLD
NO AUTOLND
VNAV PTH
HDG SEL
FD
2
RIGHT
LEFT
1.8 1.47 1.4
1.0
Thrust management
g
2
EPR
ILS OFF B/CRS
MIDDLE
599
5
a
3
TRK
DME-L
OVSPD r
2
6
MA C H
583
LEADING TRAILING EDGE a EDGE a
140
KNOTS
160 180
200
N1
1114 .
650
EGT
650
UP FLAPS
STW
BWZ
SBJ
KILMR 12000
30 190K
1055 . AUTO
CHR
7
V
10
40
IN. HG
5
a
OUTER b
INSTR SOURCE SEL FLT DIR R
a
29 92 4
3
PRESS
118
OIL
TEMP
13
4
4.4 NM
252
TRK
M
0835.4
0
Z
NAV FMC-L CDU-L
6
OFF
DME-L
ALTN GEAR EXTEND 250K-.75M 20
QTY
.5
DME-R
4 1
KTEB
OFF
2
JFK LGA KJFK KLGA
7.0
167 343 AMBO COL
25 30
7.0 LE
SAX
DN
TE
ALTN
MMU
KILMR 12000
40
FF
GND PROX
ALTN w
w
w
w
FLAP OVRD
N1
0.5 VIB
GEAR OVRD
TERR OVRD
STW
BWZ
SBJ
CHR
BLM
ALTN w
60
EFI w
50
REV
10 GMT
HARRY
ET/CHR
OVRD
OVRD
KTTN ARB 12000 KPNE MUI
OVRD
w
w
w
w
w
w
40
ALTN
20 RUN
30
HLD
w
HLD SS
FS
20
ADE ABE
WARNT 12000
FS RESET
AIR DATA w
w
IRS
RUN
HLD SS
RESET
ALTN
FMC-R
1000 FPM
ALTN FLAPS 5 15
NORM
13
OIL N2
0.5 RTO
1
UP
N2
4
KEWP
118
MAX AUTO
OFF
BARO
95
232
OIL
2 VERTICAL SPEED
.5
LOCK OVRD
DN
RUN
30
HLD
MIDDLE
3
IN.HG
29 92 4
1
20
RUN
ABE
a
AUTO BRAKES 2 3 1
DISARM
ALT MB
1013 6 BRAKE SOURCE a
ET/CHR
T K
w
ADE
R ENG OIL PRESS
AUTO BRAKESa
95 232
L ENG OIL PRESS
a
50 GMT
WARNT 12000
2
8
VALVE
60 REV
KTTN
20
1
w
HARRY
ARB 12000 KPNE MUI
IRS
5
BARO
599
EXTEND OR EXTENDED 270K-.82M
162K N2
ON
ON
259
40
EFI
ALTN
.730
C
195K
20 25
T
0
079
SAX
ALTN
700
GS
A S
15
L
1114 .
1055 .
BLM
COL
1013 6
KNOTS
OFF 210K
5
120
9
167 343 AMBO
INNER/ AIRWAYSw
2
MB ALT
IN OP
MO
FLAP LIMIT IAS 220K
EGT
1
RESERVE BKS & STRG
KEWP
MMU
1
NEG
R
584
240K
4 2
8
EPR
IAS
250 240 220
4
OFF
1
w
0
9
a
PROX G/S INHB a
100
300
VERTICAL SPEED
.5 JFK LGA KJFK KLGA KTEB
ALT
RETRACT 270K
UP
N1
r
GND
a
FMC
80
1000 FPM
DME-R
w
88.3
a
60
0
FMC-R
AUTO PILOT
a
0
350
NAV FMC-L
ALT ALERT a A/T DISC
b
400
1
CABIN ALT
OUTER
29 92 4
BARO
.5
SPEED BRAKESa
259
2
MB ALT IN.HG
1013 6
700
GS .730
88.2 r
MACH
8 NEG
R IN OP
AS
r
INNER/ AIRWAYSw
079
MA C H
KNOTS
TEMP SEL r
A/P DISC
PULL UP
r
1
R
w
1.63
CONFIG r
WINDSHEAR
w
0
C
w
CRZ
CANCEL RECALL
FIRE ALT
FLT DIR L
CDU-L
WHL WELL FIRE r
TAT - 46 C
TEST
g
NO LAND 3
9
MACH
MO
INSTR SOURCE SEL
VNAV PTH
Electronic attitude director indicator (EADI)
REG SELCAL
HDG REF NORM AUTOLAND STATUS P/RST
THR HLD
Heading reference
Engine indication and crew alerting system (EICAS)
Standby attitude indicator Autoland status (2)
Mach/airspeed indicator (2)
FLOOD
OFF MAP
AIR DATA
ALTN w
w
w
Radio distance magnetic indicator (RDMI) (2)
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
Pilots’ Main Panel 767-200ER/-300ER Standby magnetic compass Mode control panel VOR (2)
Lighting controls (2)
15
12
E
NS
A/T ARM F R E Q
WARNING
C R S
L NAV
3 3 0
VERT SPD
HDG
IAS/MACH
F/D ON
1 2 6
A/P ENGAGE
ALT 3 2 0 0 0
0 0 0 0
L CMD
B CRS
C
R
CMD
CMD
CWS
CWS
F/D ON
F R E Q
OFF SEL
EPR CAUTION
Master caution and warning lights (2)
6
EW
V NAV
OFF
5 NORM
AUTO MAN
SPD
FL CH
SEL
25 BANK LIMIT
DN
CWS
LOC
V/S
HOLD
HOLD
C R S
AUTO MAN
DISENGAGE
UP
VOR/DME
WARNING CAUTION
OFF
APP
VOR/DME
CLOCK
CLOCK
PANEL
PANEL
OFF
OFF
CHART
CHART
FLOOD
Miscellaneous warning, caution, and advisory lights
OFF MAP PTT
PTT
1
Instrument source select (2)
HDG SEL
LAND 3
FD
BRAKE TEMP w
CAUTION
1.63 2
a
1.8 1.47 1.4
TRUE
1.0
D O O R Sa
TAIL SKID
a
NOSE g
G E A R
Altimeter (2)
CLB
CON
CRZ
1
Marker beacon lights (2)
1
PRESS PSI
X 1000
0 2
g
TO GA
AUTOLAND STATUS
BRAKE
4 3
P/RST
LAND 2
TEST
a
1
THR HLD
NO AUTOLND
VNAV PTH
HDG SEL
FD
2
RIGHT
LEFT
1.8 1.47 1.4
1.0
Thrust management
g
2
EPR
ILS OFF B/CRS
MIDDLE
599
5
a
3
TRK
DME-L
OVSPD r
2
6
MA C H
583
LEADING TRAILING EDGE a EDGE a
140
KNOTS
160 180
200
N1
1114 .
650
EGT
650
UP FLAPS
STW
BWZ
SBJ
KILMR 12000
30 190K
1055 . AUTO
CHR
7
V
10
40
IN. HG
5
a
OUTER b
INSTR SOURCE SEL FLT DIR R
a
29 92 4
3
PRESS
118
OIL
TEMP
13
4
4.4 NM
252
TRK
M
0835.4
0
Z
NAV FMC-L CDU-L
6
OFF
DME-L
ALTN GEAR EXTEND 250K-.75M 20
QTY
.5
DME-R
4 1
KTEB
OFF
2
JFK LGA KJFK KLGA
7.0
167 343 AMBO COL
25 30
7.0 LE
SAX
DN
TE
ALTN
MMU
KILMR 12000
40
FF
GND PROX
ALTN w
w
w
w
FLAP OVRD
N1
0.5 VIB
GEAR OVRD
TERR OVRD
STW
BWZ
SBJ
CHR
BLM
ALTN w
60
EFI w
50
REV
10 GMT
HARRY
ET/CHR
OVRD
OVRD
KTTN ARB 12000 KPNE MUI
OVRD
w
w
w
w
w
w
40
ALTN
20 RUN
30
HLD
w
HLD SS
FS
20
ADE ABE
WARNT 12000
FS RESET
AIR DATA w
w
IRS
RUN
HLD SS
RESET
ALTN
FMC-R
1000 FPM
ALTN FLAPS 5 15
NORM
13
OIL N2
0.5 RTO
1
UP
N2
4
KEWP
118
MAX AUTO
OFF
BARO
95
232
OIL
2 VERTICAL SPEED
.5
LOCK OVRD
DN
RUN
30
HLD
MIDDLE
3
IN.HG
29 92 4
1
20
RUN
ABE
a
AUTO BRAKES 2 3 1
DISARM
ALT MB
1013 6 BRAKE SOURCE a
ET/CHR
T K
w
ADE
R ENG OIL PRESS
AUTO BRAKESa
95 232
L ENG OIL PRESS
a
50 GMT
WARNT 12000
2
8
VALVE
60 REV
KTTN
20
1
w
HARRY
ARB 12000 KPNE MUI
IRS
5
BARO
599
EXTEND OR EXTENDED 270K-.82M
162K N2
ON
ON
259
40
EFI
ALTN
.730
C
195K
20 25
T
0
079
SAX
ALTN
700
GS
A S
15
L
1114 .
1055 .
BLM
COL
1013 6
KNOTS
OFF 210K
5
120
9
167 343 AMBO
INNER/ AIRWAYSw
2
MB ALT
IN OP
MO
FLAP LIMIT IAS 220K
EGT
1
RESERVE BKS & STRG
KEWP
MMU
1
NEG
R
584
240K
4 2
8
EPR
IAS
250 240 220
4
OFF
1
w
0
9
a
PROX G/S INHB a
100
300
VERTICAL SPEED
.5 JFK LGA KJFK KLGA KTEB
ALT
RETRACT 270K
UP
N1
r
GND
a
FMC
80
1000 FPM
DME-R
w
88.3
a
60
0
FMC-R
AUTO PILOT
a
0
350
NAV FMC-L
ALT ALERT a A/T DISC
b
400
1
CABIN ALT
OUTER
29 92 4
BARO
.5
SPEED BRAKESa
259
2
MB ALT IN.HG
1013 6
700
GS .730
88.2 r
MACH
8 NEG
R IN OP
AS
r
INNER/ AIRWAYSw
079
MA C H
KNOTS
TEMP SEL r
A/P DISC
PULL UP
r
1
R
w
1.63
CONFIG r
WINDSHEAR
w
0
C
w
CRZ
CANCEL RECALL
FIRE ALT
FLT DIR L
CDU-L
WHL WELL FIRE r
TAT - 46 C
TEST
g
NO LAND 3
9
MACH
MO
INSTR SOURCE SEL
VNAV PTH
Electronic attitude director indicator (EADI)
REG SELCAL
HDG REF NORM AUTOLAND STATUS P/RST
THR HLD
Heading reference
Engine indication and crew alerting system (EICAS)
Standby attitude indicator Autoland status (2)
Mach/airspeed indicator (2)
FLOOD
OFF MAP
AIR DATA
ALTN w
w
w
Radio distance magnetic indicator (RDMI) (2)
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
Passenger oxygen*
Engine start Window heat EMER DOORS
CARGO DOORS
ACCESS DOORS
CAPT PITOT
FO PITOT
L AOA
R AOA
L AUX PITOT
R AUX PITOT
TAT
ENTRY DOORS
IRS MODE SEL W
DSPL SEL PPOS WIND TK/GS
Inertial reference
1
N 2
3
W 4
H 5
E 6
7
S 8
9
ENT
0
CLR
HDG
FWD
Yaw damper
STAB TRIM
SPOILERS
UNSCHED STAB TRIM
RUDDER RATIO
ARMED
AUTO SPDBRK
BULK
ON
ON
OVHT
OVHT
ON
ON
WINDOW HEAT L
R FWD
FWD
SIDE
PRESS
ON
ON
ON
ON
UNLKD
INOP
INOP
INOP
INOP
INOP
R
ALIGN
ALIGN
ALIGN
BOTH
L
ON DC
ON DC
ON DC
DC FAIL
DC FAIL
VALVE C
ALIGN NAV ATT
OFF
C
W
AUTO
AUTO
OFF
OFF
GND
ON
CONT
CONT
FLT
FLT
OFF
ON
ON
INOP
INOP
FAULT
ELEC ENG CONT
ALTN
ON D I S C H
NORM ALTN
SYS PRESS
O F F
QTY
QTY
L ENG
APU GEN EXT PWR
QTY
R ENG
C 1-ELEC-2 ON
ON
ON
PRESS
PRESS
PRESS
I
A OVHT
OVHT
Y
R PUMPS
VALVE
PRESS
AIR
ELEC
PRESS
PRESS
PRESS
BUS OFF
R
P R E S S
R BUS
R
ON
ON
OFF
OFF
MANUAL
ON
BUS OFF
P R E S S
DESCEND
034 0
OVHT
MODE SELECT AUTO 2
LB
KG
LB KG FUEL QTY X 1000
M AUTO
AUTO
A OFF
ON
OFF
AUTO ON
OFF
O F F
A ON
N
O F F
ON DRIVE
DRIVE
TEMP
LB
CABIN
WING ANTI-ICE ON START
OFF
FAULT
2
8
4 6
L
R
ON
ON
VALVE
VALVE
R
VALVE
VALVE
PSI
DIFF
DUCT LEAK
ERASE
BLEED
L ENG 1 2
FT X 1000
ALT
Bleed air and pneumatic
FPM X
RATE 1000
O F F
V A L V E
OVHT
ADP
APU
R ENG
Fuel jettison
O F F
EQUIP COOLING VALVE AUTO
PRESS DIFF LIMIT: T/O & LDG .125 PSI
OFF
Electrical
V A L V E
1 2 0
CABIN ALTITUDE
WIPER TEST
VALVE
DL UE CA TK
OVHT
0 2 25 4 20 15 6 10 8
0
10
ENGINE
ON L
RUN
R ISLN
BLEED
C
ON
0
C ISLN
KG
TOTAL
D
APU
80
MAN
AUTO 1
R
DUCT LEAK
GEN CONT
R
E
OVHT
OVHT
GEN DRIVE DISC L
C
L
R
L GEN CONT
60
20
VALVE
AUTO INOP R
S T B Y
W
DUCT PRESS PSI
L ISLN
LDG ALT
L
C
W
MAX
MIN
ON
S T B Y
AUTO RATE
CLIMB
CL
UTILITY BUS L
VALVE OP
FUEL CONFIG
N
OFF C
PRESS
C PUMPS
M
D
M
D
VALVE
PRESS
PACK OFF AUTO
N
AFT
FWD
FWD
INOP
W
MAN
ON
OFF
OFF
ON
ON
ISLN
L BUS
ON
Y ELEC
D
N
BUS TIE
RESET C
PACK OFF
ON
PRESS
AVAIL AUTO
A OVHT
ON
ISLN
R PACK
INOP SEATBELTS AUTO
AUTO
FUEL XFEED
W
AUTO L PACK
CABIN ALTITUDE CONTROL
AUTO
R
ON PRESS OVHT
AFT
P
I
E
Passenger signs*
C
PASS SIGNS
ON
O F F
BUS TIE
PUMPS
HYD
R
INOP
RESET
OFF L PUMPS
GND CALL
ALERT
NO SMOKING AUTO
OFF
SYS PRESS
AFT
ALERT
BAT
OFF
MID
ON
ON VALVE
ON SYS PRESS
FWD
OFF
ON VALVE
STBY POWER AUTO
R
NORM
M
INOP
INOP
CABIN CALL
FUEL JETTISON
L
Hydraulic
ON
R
L–NOZZLE–R
R
ON
FLT DK
BAT
P
Air-conditioning
W
OFF
L - RECIRC FAN - R
YAW DAMPER
Electronic engine control (EEC)
C
W
OFF
TRIM AIR
OFF GND
L
Pilot’s call panel
AFT CAB AUTO
R
2
1
VALVE
FAULT
FAULT ALIGN NAV ATT
INOP
MID CAB AUTO
ENG START
DC FAIL
OFF
INOP
FWD CAB AUTO
C
NAV ATT
COMPT TEMP
AIL LOCK
ANTISKID
Compartment temperature
UNARMED
RAM AIR TURB
L
FAULT ALIGN
CARGO HEAT
PASS OXY
SIDE
SYS DSPL C R
L
OFF
EMER LIGHTS OFF
N
STBY
LOW
OVHT
OVRD SMOKE NO COOLING
HIGH
COCKPIT VOICE RECORDER
HEADPHONE CKT BKR
OVHD PANEL
DOME
Cabin altitude
PANEL/FLOOD
APU
GLARESHIELD
LT OVRD
ANTI COLLISION
POSITION
RED
ON
OFF
Voice recorder
AISLE STAND
OFF
ON
WING OFF
ON
OFF
FLT DK DOOR
ON
UNLKD UNLKD
R
Fuel Equipment cooling
LANDING WING L
NOSE GEAR R
ON
Miscellaneous lighting
LOGO ON
TAXI RUNWAY TURNOFF L
OFF
OFF
WHITE
ON
OFF
OFF
ON
ON
IND LTS DIM
TEST BRT
Wing/engine anti-ice Windshield controls
*Passenger airplanes only. 797-FD-0061C 12-5-1-whp
Center Aislestand 767-200ER/-300ER EICAS control C
VNAV
C MM
PROG
C
SP
INIT REF
RTE
FIX
LEGS
MENU
NAV RAD
BRT
EXEC
E
D
H
I
J
M
N
O
R
S
T
W
X
DEL
/
M S G
D S P Y
O F S T
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2
3
4
5
6
Y
7
8
9
CLR
.
0
+/-
Fuel control
RS
MCDU (2) Throttle levers Stab trim switches Flap lever Speed brake lever
TE
EFIS control (2) Stab trim cutout
20 10
PLAN APL NOSE DN
APL NOSE UP
Stab trim indicator (2)
ALTN STAB TRIM
0
APL NOSE ON S T A B
ENG VALVE SPAR VALVE
ENG VALVE SPAR VALVE
2 4
Parking brake
L
6
FUEL CONTROL R RUN
T R I M APL O NOSE F UP F
8 NORM
CUT OFF
10 12
L O E F F
14 CUT OUT L
Weather radar
C STAB TRIM
WX EST
L ENG OVHT
MAP
ATC/TCAS
+5
TILT +10
0 1
-15 -10
VE
ENG BTL 2 DISCH
DISCH
-5
ILS
ENG BTL 1 DISCH
R ENG OVHT
+15
ARMED
FWD
AFT
1
2
A C A R G O
DISCH
2
F I R E DISCH
Radio communications panel (3)
STANDBY VHF C
VHF R
AM
HF R
R
ACTIVE
FLT
VHF
CAB
L
VHF L
VHF C
VHF R
HF L
AM
HF R
HF SOL
PA
L VHF
BOOM R
Engine, cargo, and APU fire control
BTL DISCH
R I G H T
L E F T
O F F
ADF
ARMED
R
C VHF
R VHF
FLT
Audio selector (2)
ALT OFF ALT ON
SAT
OXY
VOR V B R
APP C R L MKR
ATC
ATC 2
TA
STBY TEST
MIC
TA/RA
FAIL
L 1
ATC
2
IDENT
INT
ATC
VOR ADF R L R L
R TONE L R
L
R HF
SAT VOR V B R
F.
F R E Q
C R S TEST
ILS RUDDER TRIM
Fire/overheat test
15
STANDBY VHF C
VHF R
AM
HF R
10
NOSE LEFT
0
5
10
15
UNITS NOSE RIGHT
AILERON NOSE LEFT
FIRE/OVHT TEST ENG/APU CARGO
5
SYS FAIL
LEFT WING DOWN
RIGHT WING DOWN
R U D D E R
NOSE RIGHT
Aileron/rudder trim
FAIL P-RESET
797-FD-0062C 1-18-2-whp
Right Side Panel 767-200ER/-300ER Gasper air
Flight recorder and service interphone Avionics cooling monitor Data loader selector switch AIR DATA L COMPTR R
TEST
FLT REC CONFIG T/O
Miscellaneous test
SERV INTPH
First Observer’s oxygen
TEST
OFF OFF
WING ANTI ICE
TO
ON
ON NORM TEST
GND PROX
LDG
EADI
DUCT LEAK
VOR-L EHIS
E1 / E2
FMCDU-L
IRU-C
IRU-R
E5 IRU-L RESET TEST
YAW DMPR L EQUIP COOL
STRUT LEAK
E / E COOLING MONITOR
Squib test
R
WINDOW/ FUEL QTY PROBE HEAT
SQUIB TEST
TEST
ENG R
L
Generator reset
L
1
DATA LOAD SELECTOR
1
APU
L (k / mgk (k / mgk
EMER ESCAPE R TEST 1 SLIDE TEST 2 SPOILER CARGO 2 2A TEST 1 FWD TEST 2 AFT
C (k / mgkcjcj fg
C
FIELD OFF
Portable data loader connection (shown here) or airborne data loader
R fhfdhfh (k / mgk (k / mgk
Smoke goggles
SYSTEM SELECT (k / mgkzz (k / mgkzz (k / mgkzz (k / mgkzz zzOzz zzOzz (zzhfh / C lknmv zzOzz l zzOzz zzOzz
Flight control shutoff
MO173
OXYGEN MASK
2
APU
FIELD OFF
l zzOzz
zzOzz zzOzz zzOzz zzOzz
GEN FIELD MAN RESET L
N 100% PUSH
HYD GEN
FIELD OFF
lCOC
l zzOzz
lFlS zzOzz zzOzz
DATA TRANSFER UNIT RECEPTICAL
MO173
FLT CONTROL SHUTOFF - GND USE ONLY L
C T A I L
ON OFF
OFF
W I N G
ON OFF
R T A I L
ON
ON OFF
W I N G
ON OFF
ON OFF
EICAS MAINT EVENT READ
DISPLAY SELECT AUTO ECS
ELEC
PERF
MSG
HYD
APU
CONF
ENG
MCDP
EXCD
EEC maintenance
TEST
REC
MAN
ERASE
EPCS
Book stowage
RESERVE BRAKES & STRG RESET/ DISABLE
C HYD SYS ISLN
NORM
FLIGHT RECORDER SYS TEST PLUG
Lighting control
L VHF
C VHF
R VHF
FLT
CAB
PA
EICAS maintenance
EEC MAINT L ENG POWER
R ENG POWER
MIC
BOOM L
TEST
INT
First Observer’s audio First Observer’s jack panel
MAP
R
L
HF
VOR ADF R L R L
NORM
LIGHTING
R SAT
VOR V B R
OXY APP C R L MKR
PANEL BOOM MIC/HEADSET
HEADPHONE
HANDMIC
Flight recorder system test plug
OFF
Reserve brakes and steering test Ashtray/cup holder 797-FD-0063C 2-27-2-whp/CF
767 Flight Deck - EFIS
Electronic Flight Instrument System (EFIS) 767-200ER/-300ER
Captain’s instrument source select panel
Left EADI
Right EHSI
Left EHSI
Left EFIS control panel
Left EFIS symbol generator
• Thrust management system • ILS navigation system • Radio altimeter system
• PWS system • VOR system • DME system
Right EADI
Right EFIS control panel
Center EFIS symbol generator
First Officer’s instrument source select panel
Right EFIS symbol generator
• Autopilot flight director system • Weather radar system • ADC system
• ADF system • EGPWS • FMCS
• TCAS • IRS 797-FD-0069C 2-26-2-whp/CF
797-FD-0071 1-18-2-PW/CF
EFIS/IRS Switching 767-200ER/-300ER Captain’s instruments EADI - Electronic attitude director indicator EHSI - Electronic horizontal situation indicator EFI - Electronic flight instrument IRS - Inertial reference system RDMI - Radio distance magnetic indicator SG - EFIS symbol generator -Vertical speed indicator VSI
First Officer’s instruments
EADI
EADI RDMI
RDMI
EHSI
EHSI
VSI
VSI
N
Capt EFIS control panel
Capt EFI switch
ALTN
Capt IRS switch
ALTN
A
C-SG
L-SG
N
R-SG
1 N
N
F/O EFIS control panel
ALTN
F/O EFI switch
ALTN
F/O IRS switch
A
A
L-IRS 1
A
A
C-IRS
N
R-IRS
This switch remains in the N position when the Capt EFI switch is selected to ALTN. 797-FD-0070 1-18-2-whp/CF
Electronic Attitude Director Indicator 767-200ER/-300ER Attitude comparator annunciations
Pitch limit indicator
PITCH
Ground speed
GS250
20
ROLL
DH100
2500
20
Selected decision height Radio altitude
F 10
Speed deviation scale and pointer
Autothrottle status Autothrottle mode AFDS pitch mode
Localizer deviation scale and pointer
Split axis flight director cue
10
Glideslope deviation scale and pointer
10
S A/T
SPD G/S VNAV
10
WINDSHEAR 20
20
Windshear annunciation
CMD
AFDS status
LOC LNAV
AFDS roll mode
Slip/skid indicator
797-FD-0073 2-26-2-whp/CF
Electronic Horizontal Situation Indicator 767-200ER/-300ER—Expanded Map Mode • Map mode displays include reference data programmed in the FMC, such as • ETA, distance to go, range to altitude • Top-of-climb, step-climb, top-of-descent, and bottom-of-descent points • Holding pattern • Procedure turns
Distance to active waypoint
Magnetic (M) or true (T) reference
L ADF (head) Track-up annunciation Aircraft track
18.3
NM
TRK
252 M
0835.4z VAR/+TWX +12
Selected heading
Aircraft heading ETA at active waypoint Waypoint not on flight plan (selectable) Weather radar mode, gain, and antenna tilt R ADF (head) Compass rose
MLF
Instantaneous track
Airport (selectable)
AST
VORTAC (selectable)
40 STW
Estimated time and altitude at waypoint (selectable)
KILMR 12000 0841Z
Active flight plan
Range scale (number is half selected range)
Range to selected altitude
KTTN 0 32
Weather radar return (selectable)
0 14 WARNT
20
Wind speed and direction
Vertical deviation scale and pointer Waypoint on flight plan Manually selected VOR course
Airplane symbol
Trend vector
797-FD-0074 2-26-2-whp
Electrical Horizontal Situation Indicator 767-200ER/-300ER—Center Map Mode
Current track
Magnetic/true reference ETA at active waypoint
Distance to active waypoint
25.5
TRK
NM
138
1335.4z WX +12
M FGH I J
15
12
Weather radar mode, gain, and tilt Selected heading bug
9
18
Heading pointer
20
KLMNO 35000 1335Z
Active route
6
21
NOP
3
24
Position trend vector Airplane symbol Vertical deviation scale and pointer
20 27
VWXYZ
0
30
33
20
797-FD-0075C 12-4-1-whp
Electronic Horizontal Situation Indicator 767-200ER/-300ER—Expanded VOR/Approach Mode
DME distance to VOR or LOC DME
140
HDG
262 M VAR/WX +T +12
Selected course (VOR mode) or runway heading (approach mode)
Instantaneous track 20
Course deviation scale and pointer (VOR or approach mode)
Glideslope deviation scale and pointer (approach mode only) To-from VOR station (VOR mode only)
System source annunciation (VOR or approach mode)
20
TO
VOR R
110.10
ILS frequency (approach mode only)
797-FD-0076C 1-19-2-whp
Electronic Horizontal Situation Indicator 767-200ER/-300ER—Center VOR/Approach Mode
Drift angle pointer DME
140 HDG 038
To-from VOR station (VOR mode only)
M
Airplane symbol
Glideslope deviation (approach mode only)
20 VOR R
TO
110.10
797-FD-0077C 1-19-2-whp
Electronic Horizontal Situation Indicator 767-200ER/-300ER—Plan Mode
ACT
RTE
1
LEGS
1 / 9
250 • H D G
ACY
028 •
158 /
530A
178 /
FL560
.824 /
FL340
.824 /
FL340
4.4 NM
TRK
252
M
0835.4 Z
2 NM
WTP 08 322 •
1 1 1 NM
SBY 032 •
9 6 NM
WPT 07 055 •
3 9 NM
WPT 06
.824 / FL340 M AP C TR
WPT 10 INIT REF
RTE
CLB
CRZ
DES
ACY
BRT
WPT 11
SBY
WPT 08 FLY P1
HAR
N
Plan mode displays active flight plan referenced to true north. Pilots can step through flight plan on MCDU and EHSI by pushing “STEP” line select key.
797-FD-0078C 1-19-2-whp
EFIS Control Panel 767-200ER/-300ER
EHSI brightness control • Outer knob - EHSI display • Inner knob - weather radar return
Decision height alert reset
ADI RST
BRT
DH REF
EADI brightness control
1 0 0
Terrain data displayed when in MAP, CENTER MAP, EXPANDED APPROACH, and EXPANDED VOR modes
Decision height selector
TERR
WXR
BRT
EHSI range selection • Outer knob - selects desired nautical mile display range for MAP, CENTER MAP, EXPANDED APPROACH, and EXPANDED VOR modes • Center switch (TFC) - displays TCAS data when in MAP, CENTER MAP, EXPANDED APPROACH, and EXPANDED VOR modes
NOTE: Terrain data and weather radar cannot be shown on the same EFIS display at the same time. Selection of the TERR switch turns off weather radar display if showing. Selection of the WXR switch turns off terrain display if showing. It is possible, and a common practice, to show weather radar on one pilot’s EFIS display and show terrain data on the other pilot’s EFIS display.
40
80 160
20 10
TFC
320
APP VOR
ON
PLAN CTR
MAP NAVAID ARPT INOP
MAP
ON
DATA
WPT
ON
ON
Weather radar return displayed when in MAP, CENTER MAP, EXPANDED APPROACH, and EXPANDED VOR modes EHSI mode selector • Outer knob - selects VOR, APPROACH, MAP, and PLAN display modes • Center switch (CTR) - alternates display modes between center and expanded formats for VOR, APPROACH, and MAP modes
Map switches - select information to be displayed in MAP or CENTER MAP mode: • NAVAID - displays high altitude navigation aids in FMC database if selected range is 80 nmi or greater • ARPT - displays airports in FMC database • DATA - displays altitude and ETA for each waypoint on the active route • WPT - displays waypoints in the FMC database but not on the active route if selected range is 40 nmi or less 797-FD-0079C 1-19-2-whp
Weather Radar 767-200ER/-300ER ADI RST
BRT
DH REF
Brightness control (inner knob) • Adjusts brightness of WXR return on EHSI
1 0 0
18.3
NM
TRK
252 M
0835.4z VAR/+TWX +12
Weather radar mode, gain, and antenna tilt data displayed on EHSI.
MLF AST
WXR
TERR
40
BRT
40 10
160
TFC
320
APP VOR
ON
0 32
MAP 0 14 WARNT
PLAN CTR
MAP NAVAID ARPT INOP
KILMR 12000 0841Z
KTTN
80
20
STW
ON
20
DATA
WPT
ON
ON
Weather radar switch • Pushing the WXR switch displays returns on the MAP, EXPANDED MAP, EXPANDED APPROACH, and EXPANDED VOR modes of the EHSI.
Weather radar returns • When the WXR switch is pushed on the EFIS control panel, the weather radar returns are displayed on the respective on-side EHSI. • The most intense areas of precipitation are displayed in red, less intense in amber, and least intense in green. • Detected turbulence is displayed in magenta.
Aislestand
WX
Gain control • AUTO presents an optimum receiver sensitivity for best weather radar display. • Preset gain occurs automatically only in WX mode. • Rotate manually to set receiver gain.
TEST
MAP TILT +10 +5
+15
GAIN
Radar mode selector • TEST – displays maintenance test pattern • WX – displays weather radar returns • MAP – displays ground returns
0 -5 AUTO
MAX
-15 -10
Antenna tilt control • Controls antenna tilt angle with reference to horizon
Weather radar panel (representative)
797-FD-0080 C 1-19-2-whp
Flight Instruments 767 ALT
9
MACH
604
8
0
1 3,6 9 5 MB ALT
6 245 4
1013 6
KNOTS
Mach/airspeed indicator • Each Mach/airspeed indicator displays airspeed, Mach, and Vmo data from its on-side air data computer (ADC). • Each indicator displays data from the off-side ADC when the respective air data switch is selected to the ALTN position. • The command speed bug can be moved automatically from the FMC CDU or manually from the IAS/Mach selector on the MCP.
5
IN.HG
2
1
w
1
VERTICAL SPEED
.5 2
4
0 3
29 92 4
6 1000 FPM
.5
4 1
2
BARO
Altimeter • Each primary altimeter displays altitude data from its on-side ADC. • Each indicator displays data from the off-side ADC when the respective air data switch is selected to the ALTN position. • An ALT light on each indicator provides visual indication of altitude alerting.
Vertical speed indicator (VSI) • Each vertical speed indicator displays vertical speed data from its on-side inertial reference unit (IRU) and on-side ADC. • Each indicator displays data from the center IRU when the respective IRS switch is selected to the ALTN position and from the off-side ADC when the respective ADC switch is selected to the ALTN position.
0 3 6.0 0 9 5.7 DME-L
DME-R
CHR
DATE
60 50
10 GMT ET/CHR
40
20
RUN
RUN
30
HLD
HLD SS FS
RESET
Radio distance magnetic indicator (RDMI) • Each indicator displays magnetic heading; VOR and/or ADF bearings; and VOR, ILS, DME, or VORTAC distance. • Each indicator displays magnetic heading data from its on-side IRU. • Each indicator displays magnetic heading data from the center IRU when the respective IRS switch is selected to the ALTN position.
• Both indicators display magnetic heading when the HSI heading reference switch is in the NORM position and the airplane is between 73 N and 60 S latitude (with standard MAGVAR table) or 82 N and 82 S latitude (with extended MAGVAR table). The heading flag is displayed when the switch is in the TRUE position or the airplane is outside of these latitudes.
Clock • Provides Greenwich mean time (GMT) in day, month, and year or hours and minutes on the GMT indicator. Provides elapsed time or chronograph on the ET/CHR indicator. • The chronograph is controlled by the pushbutton on the clock or the remote switch on the glareshield. 797-FD-0081 C 1-18-2-whp/CF
Instrument Source Select Panel 767-200ER/-300ER Flight director selector • Selects the flight control computer (L, C, or R) for flight director command bar operation INSTR SOURCE SEL FLT DIR L C
IRS switch (alternate action) BLANK - selects normal configuration: • L IRS supplies L and C EFIS SG, CAPT VSI, and F/O RDMI • R IRS supplies R and C EFIS SG, F/O VSI, and CAPT RDMI • C IRS is available as the alternate IRS source ALTN - selects center IRS for attitude, heading, and track data for the appropriate systems above Air data switch (alternate action)
R
NAV FMC-L CDU-L
FMC-R
ALTN w
EFI
w
NAV instrument source selector • Selects source supplying FMS information to symbol generators and flight control computers Captain’s side: - FMC-L – supplies L and C EFIS SG, and L and C FCC - FMC-R – supplies L and C EFIS SG, and L and C FCC - CDU-L– supplies L and C EFIS SG First Officer’s side: - FMC-R – supplies R EFIS SG and R FCC - FMC-L – supplies R EFIS SG and R FCC - CDU-R – supplies R EFIS SG
ALTN w
IRS
w
BLANK - selects normal configuration: • L ADC supplies CAPT MACH/AIRSPEED and primary altimeter • R ADC supplies F/O MACH/AIRSPEED and primary altimeter ALTN - selects opposite air data computer to supply above instruments INSTR SWITCH EICAS advisory message • Indicates each pilot has selected ALTN with EFI switch
ALTN w
AIR DATA
w
INSTR SWITCH
EFI switch (alternate action) BLANK - selects normal configuration: • L EFIS SG supplies CAPT ADI and HSI • R EFIS SG supplies F/O ADI and HSI • C EFIS SG is available as the alternate SG ALTN - selects center EFIS SG for ADI and HSI display • CAPT has display control if each pilot has selected ALTN (C-SG) • Causes EICAS message of INSTR SWITCH if each pilot has selected ALTN
EICAS display
797-FD-0082C 1-19-2-whp/CF
Standby Flight Instruments 767-200ER/-300ER
15
Standby attitude indicator • The self-contained standby attitude indicator incorporates an ILS display with backcourse capability.
12
NS
OFF
E
6
Standby magnetic compass • A direct reading compass is installed on the center window post.
EW
ILS B/CRS
0
Standby airspeed indicator • The standby airspeed indicator (pneumatic) receives input from the L AUX pitot and the alternate static system.
60
80
400
100
350
IAS
120
15
12
NS
E
6
EW
300 250 240 220
140
KNOTS
200
160 180
0
Standby altimeter • The standby altimeter (pneumatic) receives input from the alternate static system.
1
9 8
7
03
ALT MB
1013 6 BARO
6 95 IN. HG
2
3
29 92 4 5
Pilots’ main panel
797-FD-0083C 1-19-2-whp/CF
767 Flight Deck - EICAS and Other Alerting Systems
797-FD-0085C 1-19-2-MT/CF
Engine Indication and Crew Alerting System 767-200ER/-300ER (EICAS)
Engine indication and crew alerting system (EICAS) features: • Operational displays: • Primary and secondary engine parameters • Crew alerting messages • Status page provides additional systems data for determining the readiness of the airplane for dispatch • Maintenance pages • Automatic and manual recording of maintenance data • Automatic display of in-flight start envelope
Pilots’ main panel
797-FD-0084C 1-19-2-whp/CF
EICAS Display Upper display
Standby engine indicator EPR
Lower display
EICAS maintenance panel
104.7
N1
104.7
625
EGT
625
102
N2
102 AUTO ON
Analog data Digital data Discrete inputs From airplane subsystems
CAUTION
CANCEL
Warning electronic unit
Speaker Speaker
Speaker Speaker
Dedicated caution and warning lights
RECALL
EICAS fail
Left EICAS computer unit
Right EICAS computer unit
Engine sensors
splay select pa WARNING WARNING CAUTION CAUTION
Master caution/warning switches
797-FD-0086C 1-19-2-whp/CF
EICAS Display Select Panel 767-200ER/-300ER
EICAS display brightness control • Inner knob controls brightness of upper display unit • Outer knob controls brightness of lower display unit
EICAS computer select knob AUTO Selects the left computer and automatically switches to the right computer upon detected failure L, R Manually selects the left or right computer
DISPLAY
COMPUTER
ENGINE STATUS
EVENT RECORD
L
AUTO
R
Aislestand
Engine display switch • Pushing selects or deselects SECONDARY ENGINE display on lower CRT Status display switch • Pushing selects or deselects the STATUS display on lower CRT
BRT
THRUST REF SET L
BOTH
R MAX IND RESET
PULL
Event record switch • Records maintenance data into nonvolatile memory
Maximum indication reset switch • Resets displayed overlimit readouts
Manual thrust set knob • Inner knob • Push - reference thrust automatically set by TMC • Pull and rotate - manually sets reference thrust bug on PRIMARY ENGINE display • Outer knob • Rotate - selects engine(s) for manual thrust reference control 797-FD-0087C 1-19-2-whp/CF
Typical Normal EICAS Formats 767-200ER/-300ER
TAT
-12o C
TAT -12oC 1.63
2.0
1.63
CRZ 2.0
1.32 1.0
1.63 2.0
1.32 1.0
1.5
TAT -12oC
2.0
1.32
1.0
1.5
1.5 EPR
54.2
54.2
55.3
N1
70
OIL PRESSURE
105 OIL TEMP 428
441
1.32
1.0
1.5
N1
428
2.0
EPR
55.3
1.63
CRZ
1.32
1.0
1.5
EPR
54.2
2.0
1.0
1.5
1.63
1.63
CRZ
1.32
441
18
OIL QTY
3.1 VIS
55.3
N2
70 105
528
EGT
528
18
104
N2
104
3.1
15.3
FF
15.3
EGT
EGT
L 0.76
HYD QTY
92 70 OIL
105 OIL
18 OIL
0.6
94
APU
R 0.25RF CABIN ALT AUTO1 CARGO FAN
OXY PRESS 1750
35 PRESS
N2
70 TEMP
12.4
12.6
12 RUD
FF
QTY
2.0
AIL
DISPLAY ENGINE STATUS
C 1.00
EGT 640
COMPUTER EVENT RECORD
L
AUTO
R
BRT
THRUST REF SET L
BOTH
PULL
R
MAX IND RESET
ELEV
AIL
DISPLAY ENGINE STATUS
COMPUTER EVENT RECORD
L
AUTO
R
BRT
THRUST REF SET L
BOTH
R
MAX IND RESET
PULL
797-FD-0088R1C 1-19-2-MT/CF
797-FD-0089C 1-19-2-MT/CF
797-FD-0090C 1-19-2-MT/CF
797-FD-0091C 2-19-2-MT/CF
EICAS Maintenance Displays 767-200ER/-300ER Postflight • Logbook entry of status and maintenance messages and data • MCDP checkout
PERF/APU ________
_______ ECS/MSG
GROSS WT
227.5
CAS L
2 9 1 96 44 171 193 40 62 0.75 0.62
PACK OUT TURB IN SEC HX OUT COMPR OUT PRIM HX OUT PRIM HX IN PRECOOL OUT DUCT PRESS PACK FLOW TEMP VALVE RAM IN DOOR FLT DK TRIM VALVE
3 10 3 98 46 173 196 42 64 0.80 0.71
FWD
30 0.75
DUCT TEMP
28 0.80
R
FWD EQ SUP FAN 1
TAT
MACH
ZONE TEMP BITE
95 130 12
OIL PRESS OIL TEMP OIL QTY
ALT
95 130 12
1.008 1.008
VIB
0.7 0.5
18.8
0.3 0.9
N1 N2
428
APU: BULK CARGO TEMP
AUX FWD
28 0.80
MID
17 0.00
AUX MID
17 0.00
25 AFT
EGT
640
RPM
100
EPR CMD EPR ACT
+15 21030
1.008 1.008 18.8
N1
428
EGT
60.4
N2
60.4
1.013
FF
1.010
86
FP
84
17 0.00
AFT CABIN TEMP
APU OIL QTY
ECS/status messages
STATUS ELEC/HYD ________
A
21.3
TRA
54.2
LOAD
9.3
SVA
12.4
AC-V
12
BVA
102
FREQ
104.2
NC 2 T2
73.2
12
12
IDG OUT
10.5
PS
9.2
IDG RISE
12.3
P2
11.3
-0.2
RP
-12.7
12
OIL T YEL
SCAV
HYD GEN
STBY /BAT
0 0
120 400 +10 28
DC-A DC-V
0
L
R
0.78 120 402 140 28 145 35
0.85 125 398 150 28 150 36
L RSVR PRESS
10
HYD QTY
79
P5
106
HYD PRESS
46
AOC
102
HYD TEMP
4
TCC
6
LOW 0.76 3230 50
C
APU /BAT
GND PWR
0.00 120 400 0 28
0.04 120 400
R RF
Electrical/hydraulics
:06 :12
STATUS
N1 RED EGT START EGT RED
113.9
N2RED
649
NORM HIGH 1.29 OF 0.25 3210 2140 47 115
ENG EXCD ________
116.7 649
MAX
EGT RED
Electronic propulsion control system
EGT RED
Performance APU
PAGE 1
EPCS ____
B
N1 RED
:03
PART NO S242N701-603 ENGINE CONFIGURATION
EICAS
PW 4060
PW 4060
TMC FMC
PW 4060 PW 4060
PW 4060 PW 4060
EPCS A
PW 40603-B5
EPCS B
PW 40603-B5
L EGT START
645 635 625 615 605 595 585 575 565 555 545
:02.7 :03.5 :04.4 :05.2 :06.3 :07.6 :08.5 :09.1 :10.4 :11.3 :12.2
PROG PINS
1
9C23
SUPL PINS
1
1000
EICAS ADC TMC R EGT REDLINE
MAX
MCDP
680 660 640 620
687
AVM
1:09.5 1:11.2 1:13.3 1:15.7
Engine exceedance
PW 40603-B5 PW 40603-B5
6FE8
32
MCDP OFF
16
DSP ON TEST RA ON FMC OFF FUEL ON ON EPCS A ON ON EPCS B ON
ON OFF ON ON
Configuration MCDP
797-FD-0092R1C 1-19-2-MT/CF
Non-Normal EICAS Operation 767-200ER/-300ER
TAT -12oC
TAT
1.50
1.50 2.0
2.0
1.28 1.0
1.28 1.0
1.5
DISPLAY ENGINE STATUS
COMPUTER EVENT RECORD
L
AUTO
R
BRT
-12o C 1.50
THRUST REF SET L
BOTH
R
2.0
MAX IND RESET
1.50
CRZ 2.0
1.28 1.0
1.5
1.28 1.0
1.5
1.5
EPR
EPR PULL
54.2
54.2
54.2
N1
428
N1
428
428
EGT
70
25
OIL
PRESS
70
OIL
TEMP
18
12
OIL
QTY
93 OIL
105 OIL
18 OIL
0.2
Low oil pressure, temperature, and quantity are displayed automatically
428
EGT
70 105
54.2
93
35 PRESS
N2
70 TEMP
12.4
12.4
12 QTY
FF
2.0
Secondary engine parameters selected
797-FD-0093R1C 1-19-2-whp/CF
Standby Engine Indicator 767-200ER/-300ER
The standby engine indicator (SEI) display is in view automatically if • AC power is lost • Either EICAS CRT fails and status is selected on the ground • Both EICAS CRTs fail
EPR
104.7
N1
104.7
625
EGT
625
102
N2
102 AUTO ON
The ON position manually activates the SEI
797-FD-0094C 1-19-2-whp/CF
Crew Alerting Features 767-200ER/-300ER
• Master warning and caution lights in Pilots’ primary field of view • Discrete alert lights repeated by EICAS messages • Consistent use of colors • Red for warnings • Amber for cautions and advisories • White for communications • Reduced number of aurals: bell, siren, beeper, voice, and chime • Sound intensity automatically adjusted to compensate for flight deck background noise • Predictive windshear and reactive windshear detection systems installed • Enhanced ground proximity warning system (EGPWS) installed • Traffic alert and collision avoidance system (TCAS) installed
797-FD-0095C 1-19-2-MT/CF
Crew Warning and Alerting System 767-200ER/-300ER Captain’s warning speaker
First Officer’s warning speaker
Speaker Speaker
Speaker Speaker
CAUTION
CANCEL
RECALL
CONFIG
FIRE
r
r
WINDSHEAR r
PULL UP r
WARNING
SPEED BRAKES
a
CABIN ALT
r
ALT ALERT
a
AUTO PILOT
a
A/P DISC
r
OVSPD r
GND a
CAUTION
Level B aural command Siren/owl modules (L and R)
Master warning module Bell/chime module
Warning electronic unit • • • • •
Master warning module Bell/chime module Siren/owl module (left or right) Takeoff configuration module Landing configuration module
EICAS computers (L and R) • • • • •
A/T DISC
Fire warnings Other warnings Communications system Ground proximity warning system Altitude alert module
Takeoff configuration module
PROX G/S INHB
FMC a
a
a
Landing configuration module
Radio altitude Airplane configuration • Flaps position • Stabilizer position • Parking brake position • Speedbrake handle position • Air/ground
Airplane configuration • Throttle position • Flaps position • Gear position • Speedbrake handle position
797-FD-0096C 1-19-2-whp/CF
Crew Alerting System 767 Discrete alerting lights Warnings CAUTION
TAT
Advisories CANCEL RECALL
Communication CONFIG
FIRE
r
r
WINDSHEAR r
PULL UP r
SPEED BRAKESa
CABIN ALT
r
ALT ALERT a
AUTO PILOT
a
A/P DISC
r
OVSPD r
-15o C
+46C 88.0
CABIN ALTITUDE OVERSPEED R ENG OVHT L FUEL SYS PRESS FMC MESSAGE PASS OXYGEN ON R ENG FUEL VAL AFT CARGO DOOR •SATVOICE AVAIL •PRINTER RECALL PAGE 1
D-TO
88.0
88.0
88.0
N1
760
760
EGT
GND a a
A/T DISC
PROX G/S INHB
FMC a
a
WARNING CAUTION
Speaker Speaker Master warning and caution switch lights
Aural speakers
797-FD-0028 2-26-2-whp/CF
EICAS Message Definitions 767-200ER/-300ER
Warning (red)
An operational or aircraft system condition that requires immediate corrective or compensatory action by the crew • Associated with warning aural or fire bell and red master warning lights and dedicated system warning annunciators
Caution (amber)
An operational or aircraft system condition that requires immediate crew awareness and future compensatory action • Associated with master caution aural and amber master caution lights and dedicated system caution annunciators
Advisory (amber)
An operational or aircraft system condition that requires crew awareness • Associated with system alert annunciators
Communication (white)
A normal communications condition that may require crew attention • Associated with chime aural
Status (white)
An MEL-related aircraft system fault requiring crew awareness prior to dispatch • Displayed on status page
797-FD-0097C 1-19-2-MT/CF
Alerting Inhibits During Takeoff 767-200ER/-300ER
Master warning lights and aural alerts for takeoff configuration are inhibited Master warning lights and aural alerts for fire, cabin altitude, and overspeed are inhibited Master caution lights and aural alerts for all cautions are inhibited
80 knots
V1
Air-ground transition
400-ft radio altitude or 20 seconds after air-ground transition
797-FD-0098C 1-19-2-MT/CF
Altitude Alert System 767-200ER/-300ER
+900 ft
Visual and aural alerts
Visual and aural alerts
+300 ft Selected altitude (MCP) Visual and aural alerts
-300 ft
-900 ft
No indications White light on primary altimeters illuminated EICAS caution message ALTITUDE ALERT Dedicated amber light ALT ALERT Caution aural
Indications and aurals are inhibited when landing gear is down and locked
797-FD-0099C 1-19-02-MT/DD
TCAS EADI Display 767-200ER/-300ER
Resolution advisory (RA) • Displayed automatically when the traffic alert and collision avoidance system (TCAS) calculates a collision threat with another aircraft • Provides vertical guidance for a pitch maneuver to ensure adequate vertical separation with the traffic airplane 797-FD-0100C 1-18-02-MT/DD
TCAS EHSI Display 767-200ER/-300ER Aislestand 4.4nm
TRK
140
M
0325.4z
ADI RST
15
12
BRT
DH REF
1 0 0
DADES
18
TCAS mode annunciation • TFC • TA only • TCAS fail • TCAS test • TCAS off
10
TFC
BRT
HOM
+05
20 10
-11
TFC
Other traffic symbol
160 320
APP VOR
MAP PLAN
CTR
MAP
NAVAID ARPT ON
ON
DATA
WPT
ON
ON
RA
Definition of RA
- Resolution advisory Other aircraft is 15 to 35 seconds from closest point of approach
TA
- Traffic advisory Other aircraft is 20 to 48 seconds from closest point of approach
Proximate traffic
- Other aircraft is less than 6 nmi away and within 앐 1,200 vertical feet from own aircraft and not currently a potential conflict
Other traffic
40 80
INOP
Proximate traffic
WXR
TERR
TRAFFIC
+06
-10
TA display annunciation
TA or RA annunciation (red or amber)
CAMPO
- Other aircraft is more than 6 nmi away or greater than 앐 1,200 vertical feet from own aircraft and not currently a potential conflict
Arrow
- Indicates traffic climbing or descending at a rate greater than or equal to 500 fpm
Altitude
- Number and associated sign (+ or -) indicates altitude of traffic in hundreds of feet relative to the airplane. The number is below the traffic symbol when the traffic is below and above the traffic symbol when the traffic is above
TCAS mode selector (TFC) • Push for TCAS display Traffic symbols are available in the EHSI modes: • Center map • Expanded map • Expanded VOR • Expanded approach
797-FD-0101C 1-19-2-whp
Enhanced Ground Proximity Warning System (EGPWS) 767-200ER/-300ER The enhanced ground proximity warning system (EGPWS) is a basic installation on Boeing airplanes. EGPWS provides caution and warning level alerts to the flight crew about potential terrain conflicts. The alerts are based primarily on airplane position, flight path, and barometric altitude information in conjunction with the EGPWS self-contained worldwide airport and terrain databases.
Master warning lights (2)
ADI RST
Terrain display select switch
BRT
DH REF
1 0 0
TERR
WXR WARNING
BRT
20 10
40 80 TFC
160 320
CAUTION
APP VOR
MAP PLAN
CTR
PU
MAP
NAVAID ARPT
DATA
WPT
I
Aislestand
Terrain display on EHSI (2)
EGPWS flap override switch
EGPWS landing gear override switch
EGPWS terrain override switch
797-FD-0103C 1-19-2-whp
Enhanced Ground Proximity Warning System 767-200ER/-300ER
25.5
Look-ahead distance Speaker
Altitude offset
NM
TRK
136
M
1335.4z
"CAUTION TERRAIN, CAUTION TERRAIN"
Caution
Warning 20 to 30 seconds 40 to 60 seconds
40
GND
TERRAIN
TERR
PROX
The enhanced ground proximity warning system computes two levels of terrain alerting envelopes: caution and warning.
EHSI
The enhanced ground proximity warning system look-ahead caution alert includes unique voice aural, terrain display, and map annunciations. Airplane altitude
25.5
NM
TRK
136
M
1335.4z
+2,000 ft 25.5
Speaker
+1,000 ft
TRK
136
M
1335.4z
"TERRAIN TERRAIN, PULL UP!"
40
0 ft
NM
40
TERRAIN
-500 ft PULL UP
-1,000 ft
WARNING
TERR
TERR
CAUTION
-2,000 ft
EHSI EGPWS display color coding EHSI
Terrain display colors indicate the height of the terrain relative to the current airplane altitude.
The enhanced ground proximity warning system lookahead warning alert aurals are nearly identical to those for the basic GPWS warnings in order to elicit the same pilot response. In addition, threatening terrain is presented on the map display.
797-FD-0102C 1-19-2-whp
Reactive and Predictive Windshear Systems 767-200ER/-300ER Both a reactive windshear system (RWS) and a predictive windshear system (PWS) are basic equipment on Boeing airplanes. The systems provide windshear detection capability during all operations below 1,500 feet (460 m) above ground level.
1,500 AGL (RWS)
RWS WARNING
PWS WARNING
CAUTION
1,200 AGL (PWS)
Leading edge
0.5 nmi
1.5 nmi
3 nmi
797-FD-0104C 19-1-02-MT/DD
Reactive and Predictive Windshear Systems 767-200ER/-300ER • Predictive windshear system • Provides aural and visual alerts of an impending windshear condition based on weather radar returns • Reactive windshear system • Provides recovery guidance and aural and visual alerts when the EGPWS detects the aircraft has entered a windshear condition • The AFDS provides windshear recovery guidance by means of the normal go-around pitch and roll modes when windshear is detected: – If an autopilot is engaged and the go-around mode is armed, the autopilot commands a pitch-up of 15 degrees or slightly below the pitch limit (whichever is lower) when a GA switch is actuated – If an autopilot is not engaged when the go-around is initiated, the pilot must fly the windshear recovery following the flight director commands. If the autothrottle is not armed or engaged, the pilot must advance the throttle levers manually
797-FD-0042 1-19-02-CF/DD
Predictive Windshear System (PWS) 767-200ER/-300ER The predictive windshear system begins the windshear alerting sequence with a caution to the flight crew, including a voice aural alert and an amber WINDSHEAR message on the EHSI. The predictive windshear alerts are generated by the weather radar system.
Speaker Speaker
F
“MONITOR "MONITOR RADAR DISPLAY" DISPLAY”
S
A/P ENGAGE L
0 0
B CRS
LOC
CMD
CWS
C
R
CMD
CMD
CWS
CWS
F/D ON
F R E Q
C R S
OFF AUTO
APP
DISENGAGE
MAN VOR/DME
25.5 NM
TRK
136 M
1335.4z
15
12
40
797-FD-0105C 1-19-2-whp
Predictive Windshear System (PWS) 767-200ER/-300ER The predictive windshear system next generates one of two warning voice aural alerts, as well as a red WINDSHEAR message on the EHSI and EADI, and illumination of the master warning lights. “WINDSHEAR AHEAD” voice aural alert is annunciated during takeoff phase of flight. “GO AROUND, WINDSHEAR AHEAD” voice aural alert is annunciated during the approach phase of flight.
Speaker Speaker F
S
“WINDSHEAR "WINDSHEAR AHEAD WINDSHEAR AHEAD” AHEAD" or “GO "GO AROUND WINDSHEAR AHEAD” AHEAD"
WARNING
WINDSHEAR
A/P ENGAGE L B CRS
LOC
CMD
CWS
C
R
CMD
CMD
CWS
CWS
F/D ON
F R E Q
C R S
OFF AUTO
APP
DISENGAGE
MAN VOR/DME
25.5 NM
TRK
136 M
1335.4z
WINDSHEAR
15
12
40
WINDSHEAR
797-FD-0105 R1C 1-19-2-whp
Reactive Windshear System (RWS) 767-200ER/-300ER The reactive windshear system warning provides a voice aural alert and a red WINDSHEAR message when the airplane enters a performance-decreasing windshear. The reactive windshear alert is generated by the EGPWS.
Speaker Speaker F
S
“WINDSHEAR "WINDSHEAR WINDSHEAR WINDSHEAR" WINDSHEAR”
WARNING
WINDSHEAR
A/P ENGAGE L
0 0
B CRS
LOC
CMD
CWS
C
R
CMD
CMD
CWS
CWS
F/D ON
F R E Q
C R S
OFF AUTO
APP
DISENGAGE
MAN VOR/DME
25.5 NM
TRK
136 M
1335.4z
15
12
WINDSHEAR
40
797-FD-0106C 1-19-2-whp
767 Flight Deck - Autoflight
Autopilot Flight Director System 767-200ER/-300ER (MCP) WARNING
WARNING
CAUTION
CAUTION
Electronic de director
Engine
Thrus mode selec
utoland status (ASA
The autopilot flight director system (AFDS) provides • Triple-redundant flight control computers (FCC), autopilot servos, multi-mode receivers (MMR), and radio altimeters • Autopilot available from 200 ft after takeoff through climb, cruise, descent, landing, and go-around • Category IIIb, 0 ft decision height and 300 ft RVR, approach, landing, and rollout capability
Flight management computer Thrust management computer
• Automatic thrust management through full-flight regime Flight control computer
• Flap placard and alpha floor protection • Optimum vertical and lateral navigation capabilities when coupled to the flight management computer (FMC)
Throttle quadrant Autopilot servo
797-FD-0108C 1-19-02-whp/DD
Autopilot Flight Director System Diagram
Flight management computer A/T ARM
Flight director command bars
L NAV
F/D ON OFF SEL OFF
VERT SPD
HDG
IAS/MACH
V NAV
Roll 1 2 6 Pitch 5
NORM
25 BANK LIMIT
ALT
C
R
CMD
CMD
CMD
DN
V/S
FLT DIR L
F/D ON
F A I L
RTE
DEP ARR
ATC
VNAV
FIX
LEGS
HOLD
FMC COMM
PROG
NAV RAD
PREV PAGE
BRT
EXEC
A
B
F
G
H
I
J
K
L
M
N
O
P
Q
R
S
T
9
U
V
W
X
Y
+/-
Z
SP
DEL
/
CLR
NEXT PAGE
1
2
3
4
5
6
7
8
.
0
C
D
E M S G O F S T
OFF
HOLD
DISENGAGE
UP
INSTR SOURCE SEL
D S P Y
A/P ENGAGE L
INIT REF
MENU
Multipurpose control display unit
Left flight control computer
C R
NAV FMC-L CDU-L
FMC-R
Center flight control computer Right flight control computer Left hyd sys servo Center hyd sys servo Right hyd sys servo
Autoland status annunciator
Flight control actuators Flight controls 797-FD-0044C 1-19-02-whp/DD
Mode Control Panel 767-200ER/-300ER
Vertical navigation switch
IAS/Mach window
Autothrottle arm switch
A/T ARM F/D ON
Heading window
Lateral navigation switch
L NAV
3 3 0
Vertical speed window
VERT SPD
HDG
IAS/MACH
Altitude window
1 2 6
Backcourse switch
A/P ENGAGE
ALT
0 0 0 0
Autopilot engage switches
3 2 0 0 0
B CRS
L
C
R
CMD
CMD
CMD
F/D ON
OFF
Thrust mode switch (EPR on PW and RR powered aircraft or N1 on GE powered aircraft)
SEL OFF
V NAV
EPR
Autothrottle speed mode
Speed select switch • Alternates display between IAS and Mach
5 NORM
FL CH
SPD
SEL
25 BANK LIMIT
DN
LOC
V/S
HOLD
HOLD
APP
OFF DISENGAGE
UP
Flight level change switch Speed select knob
Heading select knob Heading hold switch
Bank-angle limit select knob
Localizer mode select switch
Altitude select knob Vertical speed switch
Altitude hold switch
Flight director on/off switches Autopilot disengage bar
Approach mode select switch
Vertical speed selector
797-FD-0109C 1-19-02-PW/DD
Thrust Management System 767-200ER/-300ER
Mode control panel * Thrust mode select panel
Thrust management computer Autothrottle servo
* Thrust mode select panel Thrust rating • Thrust limit computation • Thrust reduction • Fixed climb derates • Variable reduction by assumed temperature Autothrottle control • Controls to thrust limit • Controls to IAS/Mach or selected thrust setting • Speed protection
Selector switches • TO/GA - Selects takeoff limit while on the ground and go-around limit while in flight • CLB - Selects maximum climb thrust • CON - Selects maximum continuous thrust • CRZ - Selects maximum cruise thrust
TO GA
CLB
CON
CRZ
1
2
Derate switches • Select fixed derate for climb
TEMP SEL
Temperature selector • Selects assumed temperature reduced thrust for takeoff • Reduced thrust assumed temperature shown in degrees Celsius on EICAS primary display • Maximum 25% assumed temperature reduced thrust 797-FD-0110C 1-19-02-MT/DD
Maintenance Control and Display Panel 767-200ER/-300ER Collins GROUND TEST SEL UP
• The maintenance control and display panel (MCDP) provides flight fault recording for the FCC, TMC, and FMC systems and ground test BITE for the flight control and thrust management systems. • The MCDP can store up to 350 faults for up to 99 flights.
01 R/P DISC ROC SYST L
DOWN
POWER OFF
FLT FAULTS
INSTRUCTIONS XXXXXXXXXXXX XXXXXX XXXX
GRD TEST
NO/SKIP
EICAS maintenance panel (P61)
MCDP (located in E/E bay)
GROUND TESTS
XXXXX XXXXX XXXX XXXXXXXXXXXX XXXXXXXXXXX XXXX
YES/ADV
LRU
XXXXXXX
SUPPORT
XXX XXXXXX XXXXXXXXX XXXXXX XXXXXXXXX XXXXX XXXXX XXXXXXXXX
XXXXXXXXXXXX
XXXXXX
XXX
XXXXXX
XX XXXXXXXXXX XXXXXXXX
XXXXXX XXXXXXXXXXX XXXXXXXXXXX
XXXXXXXXXXX
XXXXX XXXXXX XXXXXXXXX
XXX XXXXXX XXXXXX XXXXXX XXX
XXXXXXXXXXXXXXX
XXXXX XXXXXXXXXX XXXX
XXX XXXX XXXXXXXXXX
XXXXX XXXXX XXXX XXXX XXXXX XXX XXXXXXXXX
XXXXXXX
XXXX XXX
XXX XXXX XXXX XXXXXXXX
XXXX
XXXX
XXXX XXXX XXXX XXXX
XXXXXX XXXXXX XXXX
XXX XXXXXXXXX
XXXXXXXX XXXX
XXX XXXXXX XXXXXXXXX X XXXX XXXXX
XXX XXX XXX XXXXXXX
XXXXXXXXXXXX XXXXXX XXXX
XXXXXXX
XXX XXXXXX XXXXXXXXX XXXXXX XXXXXXXXX
XXXXXXX XXX XXX
SYSTEM
XXXXX XXXXX XXXX XXXXXXXX XX XXXXXXXXXXXX XXXX
XXX
XXXX
XXX XXXXXXXX
XXXXX XXX XXX XX
XXXXXXX XXX
XXXXXX XXXXX
XXXX
XXXXX XXXX X
XXXXX XXXXXX XXXXX XXX
XXXXXXX
EICAS computer
XXXXXXX XXXXXX XXXX
XXXXX XXX XXXXX
XXXXXX
XXXXXXX
XXXXX
Flight management computers
Thrust management computer Flight control computers
• Central fault recording and fault isolation • Allow faster airplane turnaround • Ensure that the proper LRU is replaced • Help lower the cost of ownership
Lower EICAS display STATUS
PART NO S242N701-603 ENGINE CONFIGURATION
EICAS
PW 4060
TMC
PW 4060 PW 4060
FMC
PW 4060 PW 4060 PW 4060
EPCS A
PW 40603-B5
EPCS B
PW 40603-B5
PROG PINS
1
9C23
SUPL PINS
1
1000
EICAS ADC TMC MCDP AVM
PW 40603-B5 PW 40603-B5
6FE8
32
MCDP OFF
16
ON DSP RA TEST ON FMC OFF FUEL ON ON EPCS A ON ON EPCS B ON
ON OFF ON ON
Configuration MCDP
MCDP maintenance page
Inertial reference unit
• Faults and diagnostic data are displayed on the MCDP or on the EICAS maintenance page.
Air data computer
Clock
VOR
Airline warning annunciators
Flap position Mode control panel
EFIS CP
Caution/warning system Instrument landing system
Thrust mode select panel
DME EICAS Flight management MCDU
Servos Speed brake handle position
Radio altimeter Stabilizer position 797-FD-0111C 1-19-02-MT/DD
767 Flight Deck - FMS and MCDU
Flight Management Computer System 767-200ER/-300ER LNAV and VNAV engage
VOR/DME tuning
FMC speed low ator
speed mmand g
nate FMC rce select switch
EHSI D S P Y F A I L
MCDU
INIT REF
RTE
DEP ARR
ATC
FIX
LEGS
HOLD
FMC COMM
MENU
NAV RAD
PREV PAGE
A
NEXT PAGE
F
BRT
VNAV
EXEC
PROG
B
C
G
H
D
E
I
J
INIT REF
RTE
DEP ARR
ATC
FIX
LEGS
HOLD
FMC COMM
MENU
NAV RAD
PREV PAGE
A
NEXT PAGE
BRT
VNAV
EXEC
PROG
B
C
D
E
F
I
J
K
G
H
L
M
N
O
L
M
N
O
4
5
6
P
Q
R
S
T
4
5
6
P
Q
R
S
T
7
8
9
U
V
W
X
Y
7
8
9
U
V
W
X
Y
.
0
+/-
Z
SP
DEL
/
CLR
.
0
+/-
Z
SP
DEL
/
CLR
1
2
3
K
M S G
D S P Y
O F S T
F A I L
M S G
1
2
3
O F S T
Flight control computers
Inertial reference units
Left FMC Thrust management
Right FMC Navigation and system sensors 797-FD-0112C 1-19-2-PW-whp
Flight Management Computer System 767-200ER/-300ER Pegasus FMC is basic Pegasus FMC features: • FANS-1 capable • Performance management • Economically efficient flight profiles – Climb – Cruise – Descent – Holding – Nonprecision approach • Cost index selection • Speed schedules • Engine out performance • Clean or speedbrake descent distances displayed • En route winds • Step-climb planning improvements • Flight planning • Range/fuel data • Takeoff and landing • Top of descent • Optimum altitude and step-climb point • Alternate airports • Required navigation performance (RNP) • Route offsets available • Active waypoint distance and predicted fuel displayed
• Navigation/guidance calculations • FMC calculates airplane position using navigation sensor data in the following priority: – GPS/LOC/INERTIAL – DME/DME/LOC/INERTIAL – DME/VOR/LOC/INERTIAL – LOC/INERTIAL – GPS/INERTIAL – DME/DME/INERTIAL – DME/VOR/INERTIAL – INERTIAL ONLY – GPS ONLY – All navigation sensors failed - none • Point-to-point great circle paths • Guidance commands (LNAV, VNAV, and autothrottle) • Auto tuning of DME and VOR for position updating • Database storage • Airplane and engine performance • Navigation data (VHF NAVAIDS, airports, SIDs, STARs, runways, airway approaches, and missed approaches) • Display data processing • Crew alertness monitor
797-FD-0113 1-19-02-MT/DD
Multipurpose Control Display Unit (MCDU) 767-200ER/-300ER
• Keyboard layout similar to 747-400 FANS CDU
D S P Y F A I L
INIT REF
RTE
DEP ARR
ATC
VNAV
FIX
LEGS
HOLD
FMC COMM
PROG
MENU
NAV RAD
A
B
C
D
E
PREV PAGE
NEXT PAGE
F
G
H
I
J
K
L
M
N
O
1
2
3
BRT
EXEC
4
5
6
P
Q
R
S
T
7
8
9
U
V
W
X
Y
.
0
+/-
Z
SP
DEL
/
CLR
M S G O F S T
• NAV RAD key - access to NAV RADIO page – VOR radio tuning • ATC COMM key - access to ATC data link • FMC COMM key - access to ACARS FMC data link • VNAV key - access to active CLB, CRZ, DES page • Alternate navigation function - The MCDUs can be used as an alternate navigation system if both FMCs fail. The MCDUs perform lateral navigation computations. LNAV and VNAV are not available. Each MCDU can display route information on its on-side EHSI.
797-FD-0114C 1-19-02-PW/DD
FMCS Position Updating 767-200ER/-300ER • The FMCS determines aircraft position using the available sources in this priority: 1. GPS/LOC/INERTIAL 2. DME/DME/LOC/INERTIAL 3. DME/VOR/LOC/INERTIAL 4. LOC/INERTIAL 5. GPS/INERTIAL 6. DME/DME/INERTIAL 7. DME/VOR/INERTIAL 8. INERTIAL ONLY 9. GPS ONLY
Multi-mode receivers
IRU
VOR/DME receivers
GPS position
FCC airplane guidance
FMC Radio updating (autotune)
FMCS LNAV guidance
• The FMCS automatically tunes VOR/DME radios. • If both VOR/DMEs are manually tuned, the FMC will use the range/bearing information as long as signal criteria are satisfied.
F R E Q
C R S
AUTO
Nav tuning panels (manual tuning)
MAN
• The frequency of a navigational aid on an active leg will be tuned if it is part of a published terminal area procedure.
VOR/DME
GPS satellites
Waypoint Active leg
VOR/DME VOR/DME
797-FD-0123C 1-19-02-whp/DD
Global Positioning System 767-200ER/-300ER
• Global positioning system (GPS) provides precision navigation for • FMC position • RNP operations • EGPWS • FANS operation • GPS supports required navigation performance (RNP) operations down to 0.2 nmi
Onboard GPS
• FMC automatically selects best sensors (GPS, DME, VOR, LOC)
797-FD-0115C 1-19-02-PW/DD
Global Positioning System With Pegasus FMC 767-200ER/-300ER
EHSI d
splay
GPS antenna POS REF
FMC position
FMC (GPS) N47 32.4 W 122 18.6 IN E R TIAL
Nav sensor positions Multi-mode receiver left
Multi-mode receiver right
Nav performance
2/4
Nav mode
N47 32.4 W 122 18.7 GP S
N47 32.4 W 122 18.6 R AD IO
N47 32.4 W 122 18.6 RNP/ACTUAL 2.00/0.30 NM
N757BB
T AI L
ON
DA TA LINK
< INDEX POS INIT > PERF INIT UPLINK
ALTN UPLINK
< REJECT ACCEPT > ALTN UPLINK INIT REF
RTE
CLB
CRZ
DES
BRT
797-FD-0168C 1-19-2-whp/CF
Options 4 —Flight Management Computer System 767-200ER/-300ER Takeoff Data Link • FMCS takeoff data link (shown below) is a separate option contingent on selection of AOC DL. This feature allows uplinks of takeoff data to the FMC.
TAKEOFF REF UPLINK 1/2
TAKEOFF REF UPLINK 1/2
V1
V1
134
134
VR
VR
140
140
V2
V2
147 GRWT
197.2
147
TOGW
GRWT
198.6
197.2
TAKEOFF DATA
< REJECT ACCEPT > < INDEX POS INIT > TAKEOFF DATA UPLINK
TOGW
198.6
TAKEOFF DATA
< REJECT ACCEPT > < INDEX POS INIT > TAKEOFF DATA LOADED INIT REF
RTE
CLB
CRZ
DES
BRT
797-FD-0168 R1C 1-19-2-whp/CF
Options 4 —Flight Management Computer System 767-200ER/-300ER Printer Interface • Provides for the printing of the FMC flight plan and ATC data link messages ------ CURRENT AIRCRAFT DATA --------LAST POS: YKM ATA AT LAST POS: 1328Z FUEL AT LAST POS: 131.7 FMC LAT/LON: N4700.0W12516.4 NAV SOURCE: INERTIAL RNP/ACTUAL: 2.0/0.4 FLT PHASE: CRZ ALT: 21100 TAS: 405KT GS: 425KT WIND: 270T/14KT OAT: -38C CURRENT FUEL: 128.7 ORIGIN/ATD: KBFI/1300Z DEST/ETA: KMWH/1610Z CO ROUTE: BFIMWH CRZ ALT: FL210 ZFW: 300.0 RESERVES: 25.0 CRZ CG: 30.0% COST INDEX: 90 ------------- ACT RTE 1 -------------VIA/TO SPD/ALT ETA/FUEL -------------------------------------LACRE3.VAMPS 080 1199NM 1320Z/141.3 VAM01 250/FL270AFL290B V2 070 30NM 1325Z/140.3 ELN (305)/(FL210) DIRECT 120 40NM 1330Z/139.3 ----------- ENTERED WINDS -----------FIX ALT DIR/SPD ALT/OAT -------------------------------------VAM01 FL270 240/130 FL210/-44C FL250 240/120 FL230 230/ 80 FL210 220/ 30 ---------- DESCENT FORECAST ---------ALT WIND DIR/SPD FL210 180/ 30KT 17000 170/ 20KT 13000 150/ 10KT 9000 120/ 5KT
• Option available for FMC printer interface • FMC prints uplinked and downlinked ATC messages DES DIR>
• To waypoint and altitude in 3R
• Vertical speed • Required to maintain vertical bearing
797-FD-0162C 1-19-2-PW/CF
Options 5 —Communications 767-200ER/-300ER
Feature
Basic
Option
HF Data Link
None
Installation and Activation of HF Data LinkPartial Provisions
8.33 kHz VHF Channel
None
Activation
Spacing
Partial Provisions
SATCOM
None
SATCOM System Installation Partial Provisions
ACARS/Data Link
None
VDL Mode 2/AOA Installation Level 0A CMU InstallationARINC 724B ACARS InstallationPartial Provisions
Voice Mode Protection
None
Provided
Emergency Locator Transmitter (ELT)
None
ELT InstallationPartial Provisions
Pilots Call Panel
PA-in-Use Light not included
PA-in-Use Light included
Boom Microphone Headset Jacks
Two Pin Jacks
Five Pin Jacks
Push to Talk Switch on Glareshield
None
Provided
Cockpit Voice Recorder Monitor Jack
None
Provided
797-FD-0215C 2-25-2-whp
Options 5 —Communications 767-200ER/-300ER Satellite Communications (SATCOM) • Options available for SATCOM system, or partial provisions for SATCOM • SATCOM provides two-way voice/data communication for the flight crew and cabin passengers anywhere in the world covered by INMARSAT global/spot beam • The services include • Flight deck voice, allowing instantaneous communication with Operations, Maintenance and Air Traffic Control • Flight deck data link data communication • 64 kbps circuit mode PC data communication planned for future with AERO-H+ system • A SATCOM installation consists of the following equipment • Avionics equipment — Satellite data unit (SDU) — Radio frequency unit (RFU) – not required on all SATCOM systems — High power amplifier (HPA) • Antenna systems – customers can select either an AERO-H+ or AERO-I system — High-gain antenna (HGA) – AERO-H+ system — Intermediate-gain antenna (IGA) – AERO-I system • Pilot interface — Multipurpose control and display unit (MCDU) – basic feature – no option required — Audio control panel (ACP) – basic feature — EICAS (communication messages) – basic features – no option required
797-FD-0033 1-19-02-PW/DD
Options 5 —Communications 767-200ER/-300ER Satellite Communications (SATCOM) INMARSAT 3
L-band digital link 1.5/1.6 GHz
RF C-band 4/6 GHz
Airborne earth station (AES)
Ground earth station (GES)
• PSTN - Publish switched telephone network • PSTDN - Publish switched telephone data network • Private networks • Aeronautical fixed network (AFTN, CIDN, SITA, ATN)
Airline operational control (AOC) or air traffic control (ATC)
Service provider network 797-FD-0034 1-19-02-whp/DD
Options 5 —Communications 767-200ER/-300ER Data Link • Data link provides a high-speed digital data transmission between the airplane and ground facilities. By transmitting and receiving data automatically, without the flight crew intervening, data link reduces flight crew workload. Pilots use the MCDU or an optional MIDU to interface with the data link system. Data link is used to exchange airline operations information and airplane operating data. • Options are available for installation of a flight deck printer. • Options are available for airline operational control data link (AOC DL) and air traffic services data link (ATS DL). See FMC system options 4 for further information on these optional features. • Three levels of data link provisions/installations are available: ARINC 724B ACARS, ARINC 758 level 0A, and ARINC 758 VDL mode 2/AOA. ARINC 724B ACARS • ARINC 724B aircraft communications addressing and reporting system (ACARS) transmits character-oriented data at 2.4 kbits/second. The modem, converting data to/from VHF sound transmission, is contained in the ACARS management unit. • The following options are required for ARINC 724B ACARS operations: • Partial provisions for a single ARINC 724B ACARS management unit. • Installation of an ARINC 724B ACARS management unit into partial provisions.
797-FD-0035C 1-19-02-PW/DD
Options 5 —Communications 767-200ER/-300ER Data Link ARINC 758 level 0A data link • Level 0A data link transmits character-oriented data at 2.4 kbits/second. The modem is contained in the communications management unit (CMU). • The following options are required for level 0A data link operation. • Partial provisions for a single ARINC 724B ACARS management unit • Limited partial provisions for dual ARINC 758 CMUs compatible with existing single ARINC 724B ACARS provisions • Installation of an ARINC 758 CMU into partial provisions ARINC 758 VDL mode 2/AOA data link • VDL mode 2/AOA (VHF data link mode 2/aircraft communications addressing and reporting system over aviation VHF link control) transmits high-speed character-oriented data at 31.5 kbits/second to suitably equipped ground stations. VDL model 2/AOA transmits character-oriented data at 2.4 kbits/second to ground stations not equipped for VDL mode 2/AOA high-speed data. The modem is contained in the VHF data radio transceivers (VDR). • The following options are required for VDL mode 2/AOA operation. • Partial provisions for a single ARINC 758 CMU. Partial provisions are also available for dual ARINC 758 CMUs to provide a possible future installation of a second CMU • Installation of an ARINC 758 CMU into partial provisions • Installation of ARINC 716/750 capable VHF data radio (VDR) transceivers
797-FD-0036C 1-19-02-PW/DD
Options 5 —Communications 767-200ER/-300ER - Data Link Installations ARINC 724B ACARS with dual ARINC 758 CMU provisions
Level 0A data link with single ARINC 724B, ACARS MU provisions, and dual ARINC 758 CMU provisions
CMU
ACARS
Left tray ARINC 758
Left tray ARINC 758
Right tray ARINC 724B
Right tray ARINC 758
APM ARINC 716 VHF wiring 429 bus
ARINC 758 CMU wiring
1 VHF
429 bus
ARINC 724B ACARS wiring
ARINC 716 VHF wiring
ARINC 724B ACARS wiring
429 bus
429 bus
3 VDRs
ARINC 758 CMU wiring
ARINC 758 CMU wiring
ARINC 758 CMU wiring
Other airplane systems
Other airplane systems
VDL mode 2 / AOA data link with dual ARINC 758 CMU provisions
CMU
Left tray ARINC 758
Right tray ARINC 758
APM
429 bus
429 bus
3 VDRs ARINC 758 CMU wiring
ARINC 758 CMU wiring
Other airplane systems
797-FD-0037C 1-19-02-whp/DD
Options 5 —Communications 767-200/767-300 - VDL Mode 2/AOA Architecture Data Link Air
Ground VDL mode
Interface systems: • FMC • ACMS • Printer
CMU
VDL ground network
Airline operational control (AOC)
ACARS ground network
ATC
VDR
ACARS • VDL mode 2/AOA data link interface with VDL mode 2/AOA ground stations and conventional ACARS ground stations
797-FD-0038C 1-19-02-whp/DD
Options 6 —Avionics 767-200ER/-300ER Feature Data Loader Printer ACMS - Expanded Engine Parameter Recording MIDU (Multipurpose Interactive Display Unit) Engine out Takeoff Thrust Operation
Basic Airborne Data Loader None Basic Parameters None Five Minutes
Option Portable Data Loader Connector ARINC 744 PrinterARINC 740 Printer Basic and Expanded Parameters Provided Ten Minutes
ECS Temperature Indications
Celsius
Fahrenheit
Instrumentation Display Units
English units
Metric units
Navigation Systems Feature Metric Altimeters
Standby Attitude Indicator Weather Radar System EGPWS Peaks & Obstacles
Basic None
Backcourse Switch Included Single System Inhibited
Option Two Metric Altimeters with Digital Display One Metric Altimeter with Analog DisplayTwo Metric Altimeters with Digital Display and One Metric Altimeter with Analog Display Backcourse Switch Deactivated Dual System Single System with Auto-Tilt Dual System with Auto-Tilt Enabled
EGPWS Altitude Callout Volume
Standard Volume
Low Volume
EGPWS "Smart 500" foot Callout
Inhibited
Enabled
EGPWS Altitude Callouts
Inhibited
Many options available
797-FD-0216C 2-25-2-whp
Options 6 —Navigation Systems 767-200ER/-300ER Peaks and Obstacles • Option provides for the display of man-made obstacles on the EHSI when an obstacle is contained in the Enhanced Ground Proximity Warning Computer (EGPWC) terrain database and a conflict is identified. Aural and visual caution and warning alerts are provided.
8.8 NM
TRK
194
18
“CAUTION CAUTION OBSTACLE CAUTION OBSTACLE OBSTACLE”
1717.1Z 21
15
Speaker Speaker
M
24
10
Amber for caution Red for warning
OBSTACLE
TERR
797-FD-0029 2-26-2-WHP/CF
Options 6 —Navigation Systems 767-200ER/-300ER EGPWS Peaks and Obstacles Peaks Display
8.8 NM
TRK
194 M
18
•
Provides a “look down” to the highest terrain ahead of the airplane
•
Displays terrain
•
Displays terrain altitudes
•
Blends with normal terrain colors when flying near terrain altitude
•
Peaks display when more than 2,000 feet above terrain
1717.1Z
24
10
Height of surrounding terrain
Peaks and obstacles is an optional feature of the EGPWS
21
15
Highest peak
•
TERR 144 050
797-FD-0030 2-26-2-whp/CF
Options 7 —Crew Accommodations 767-200ER/-300ER
Flight Deck Accommodations Feature Captain's and First Officer's Seats First Observer's Seat Second Observer's Seat Sun Visors
Basic Manually Operated Seats Wall Mounted None Standard Sun Visors
Option Power Operated Seats Track Mounted Provided Roller Sunshades and improved Sun Visors
Portable Breathing Equipment
None
Provided
Flight Deck Flashlights
None
One Flashlight with ShieldTwo Flashlights Two Flashlights with Shield
Emergency Evacuation Signal System
None
Provided
797-FD-0217C 2-26-2-whp
Options 7 —Crew Accomodations 767-200ER/-300ER • Powered IPECO Captain’s and First Officer’s seats • Second Observer’s station (not available on 767 Freighter) • Track-mounted First Observer’s seat (basic on 767 Freighter)
First Officer’s tiller wheel
• Flashlights • Protective breathing equipment • Emergency evacuation signal system • First Officer’s nose wheel steering tiller (not available on 767 Freighter)
Second Observer’s seat • Two headphone jacks • Oxygen mask • Life vest • Audio selector panel (optional)
797-FD-0177C 2-26-2-whp
Options 8 —Airframe Systems 767-200ER/-300ER
Feature
Basic
Option
Bulk Cargo Heating and Ventilation
None
Provided
Catalytic Converters for Ozone Control
None
Provided
APU - Additional Starting Capability
None
Provided
Duct Leak Detection System
Single Loop System
APU Fire Extinguisher Bottle
Single Standard APU Bottle
Dual Loop System (PW & GE engines only) Single APU Bottle, common with Engine fire bottlesDual Standard APU BottlesDual APU Bottles, common with Engine fire bottles
Ice Detection
None
Advisory Ice DetectionAutomatic Anti-Ice System
APU Hour Meter
None
Provided on Flight Deck Provided in E/E Bay
APU Cycle Meter
None
Provided on Flight Deck Provided in E/E Bay
797-FD-0218C 2-25-2-whp
Acronyms and Abbreviations ACARS ACMS ADC ADF ADL AFDS A/G ALTN AOA A/P APU ASP ATC AUX BFE BITE CONF CRT DME EADI ECS E/E EEC EFIS EGPWS EGT EHSI EICAS ELEC ENG EXCD EPCS EPR ER ETOPS FADEC FCC F/D FMC FPR GA GMT GPS GS HDG HMG HYD
– Aircraft communications addressing and reporting system – Airplane condition monitoring system – Air data computer – Automatic direction finder – Airborne data loader – Autopilot/flight director system – Air-ground – Alternate – Angle of attack – Autopilot – Auxiliary power unit – Audio selector panel – Air traffic control – Auxiliary – Buyer-furnished equipment – Built-in test equipment – Configuration – Cathode ray tube – Distance measuring equipment – Electronic attitude director indicator – Environmental control system – Electrical/electronic – Electronic engine control – Electronic flight instrument system – Enhanced ground proximity warning system – Exhaust gas temperature – Electronic horizontal situation indicator – Engine indication and crew alerting system – Electrical – Engine exceedance – Electronic propulsion control system – Engine pressure ratio – Extended range – Extended-range twin-engine operations – Full-authority digital engine control – Flight control computer – Flight director – Flight management computer – Flight plan request – Go-around – Greenwich mean time – Global positioning system – Ground speed – Heading – Hydraulic motor generator – Hydraulics
IAS ILS IRS LAT/LON LNAV LRC LRU MASI MCDP MCDU MCP MMR MSG OVRD PA PERF PLI PWS QAR RA RAT RDMI RTO RVR SAT SATCOM SEL SELCAL SID STAR STBY TAI TAS TAT TCAS TMC TMSP TO TRK VHF VNAV VOR VSI WEU WPT WXR
– Indicated airspeed – Instrument landing system – Inertial reference system – Latitude/longitude – Lateral navigation – Long-range cruise – Line replaceable unit – Mach/airspeed indicator – Maintenance control and display panel – Multifunction control display unit – Mode control panel – Multi-mode receiver – Message – Override – Passenger address – Performance – Pitch limit indicator – Predictive windshear system – Quick access recorder – Resolution advisory (or radio altimeter) – Ram air turbine – Radio distance magnetic indicator – Refused takeoff – Runway visual range – Static air temperature – Satellite communications – Standby engine indicator – Selective calling – Standard instrument departure – Standard terminal arrival route – Standby – Thermal anti-ice – True airspeed – Total air temperature – Traffic alert and collision avoidance system – Thrust management computer – Thrust mode select panel – Takeoff – Track – Very high frequency – Vertical navigation – Very high frequency omni range – Vertical speed indicator – Warning electronics unit – Waypoint – Weather radar 797-FD-0178C 1-19-2-whp/CF
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