CAT II/III
FAMILIARIZATION
CAT II/III
FAMILIARIZATION
Copyright © 2009
The Boeing Company
All Rights Reserved
Copyright © 2009
The Boeing Company
All Rights Reserved
Document Number 757/767-O19
Document Number 757/767-O19
Revision Number: 1
Revision Date: November 1, 2017
Revision Number: 1
Revision Date: November 1, 2017
Copyright Information
Boeing claims copyright in each page of this document only to the extent that the
page contains copyrightable subject matter. Boeing also claims copyright in this
document as a compilation and/or collective work.
The right to reproduce, distribute, display, and make derivative works from this
document, or any portion thereof, requires a license from Boeing. For more
information, contact The Boeing Company, P. O. Box 3707, Seattle, Washington
98124.
Boeing 707, 717, 727, 737, 747, 757, 767, 777, DC-8, DC-9, DC-10, MD-10,
MD-11, MD-80, MD-90, BBJ, Boeing Business Jet, the Boeing logo symbol, and
the red-white-and-blue Boeing livery are all trademarks owned by The Boeing
Company; and no trademark license (either expressed or implied) is granted in
connection with this document or otherwise.
This document has EAR data with Export Control Classification Numbers
(ECCN) of 9E991.
Export of this technology is controlled under the United States Export
Administration Regulations (EAR) (15 CFR 730-774). An export license may be
required before it is used for development, production or use by foreign persons
from specific countries. The controller of this data has the individual
responsibility to abide by all export laws.
Copyright Information
Boeing claims copyright in each page of this document only to the extent that the
page contains copyrightable subject matter. Boeing also claims copyright in this
document as a compilation and/or collective work.
The right to reproduce, distribute, display, and make derivative works from this
document, or any portion thereof, requires a license from Boeing. For more
information, contact The Boeing Company, P. O. Box 3707, Seattle, Washington
98124.
Boeing 707, 717, 727, 737, 747, 757, 767, 777, DC-8, DC-9, DC-10, MD-10,
MD-11, MD-80, MD-90, BBJ, Boeing Business Jet, the Boeing logo symbol, and
the red-white-and-blue Boeing livery are all trademarks owned by The Boeing
Company; and no trademark license (either expressed or implied) is granted in
connection with this document or otherwise.
This document has EAR data with Export Control Classification Numbers
(ECCN) of 9E991.
Export of this technology is controlled under the United States Export
Administration Regulations (EAR) (15 CFR 730-774). An export license may be
required before it is used for development, production or use by foreign persons
from specific countries. The controller of this data has the individual
responsibility to abide by all export laws.
757/767 Training Manual
757/767 Training Manual
Full Flight Simulator
Full Flight Simulator
CAT II/III Familiarization
CAT II/III Familiarization
INTRODUCTION
INTRODUCTION
This training program is flown at night and is designed to familiarize
757/767 flight crews with CAT II/III operations. Training procedures
include low visibility taxi, takeoffs (500 RVR), and approaches, missed
approaches and landings under CAT II/III conditions.
These profiles are conducted following completion of the CAT II/III CBT.
The lesson includes a one-hour briefing followed by a two-hour flight
profile and a short debriefing.
The lesson includes practice in low visibility taxi and takeoff procedures
followed by CAT II/III approaches and landings using radio altitude
procedures.
Completion of this course does not authorize low visibility takeoffs or
operation to minimums below Category I. Upon completion of this
training, pilots must get authorization from their regulatory authority to
conduct low visibility taxi and takeoff as well as approaches, missed
approaches and landings at less than published Category I minimums.
This training program is flown at night and is designed to familiarize
757/767 flight crews with CAT II/III operations. Training procedures
include low visibility taxi, takeoffs (500 RVR), and approaches, missed
approaches and landings under CAT II/III conditions.
These profiles are conducted following completion of the CAT II/III CBT.
The lesson includes a one-hour briefing followed by a two-hour flight
profile and a short debriefing.
The lesson includes practice in low visibility taxi and takeoff procedures
followed by CAT II/III approaches and landings using radio altitude
procedures.
Completion of this course does not authorize low visibility takeoffs or
operation to minimums below Category I. Upon completion of this
training, pilots must get authorization from their regulatory authority to
conduct low visibility taxi and takeoff as well as approaches, missed
approaches and landings at less than published Category I minimums.
Copyright © The Boeing Company. See title page for details. EAR 9E991.
November 1, 2017
757/767-O19
Copyright © The Boeing Company. See title page for details. EAR 9E991.
1.1
November 1, 2017
757/767-O19
1.1
Full Flight Simulator
CAT II/III
Familiarization
Full Flight Simulator
CAT II/III
Familiarization
757/767 Training Manual
Intentionally
Blank
Intentionally
Blank
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757/767-O19
757/767 Training Manual
November 1, 2017
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1.2
757/767-O19
November 1, 2017
Full Flight Simulator
CAT II/III
Familiarization
757/767 Training Manual
757/767 Training Manual
ROUTE OF FLIGHT
ROUTE OF FLIGHT
ORIGIN
ORIGIN
ROUTE
DESTINATION
FLIGHT NUMBER
Seattle-Tacoma International Airport (KSEA)
Gate C12
N47°26.8 W122°18.2
RWY 16C
Direct ANVIL
Seattle-Tacoma International Airport (KSEA)
BOEING TRAINER 55 or
BOEING TRAINER 66 HEAVY
ROUTE
DESTINATION
FLIGHT NUMBER
PERFORMANCE
GR WT
FUEL
ZFW
RESERVES
CRZ ALT
COST INDEX
THRUST LIM
FLAPS
CG
Full Flight Simulator
CAT II/III
Familiarization
Seattle-Tacoma International Airport (KSEA)
Gate C12
N47°26.8 W122°18.2
RWY 16C
Direct ANVIL
Seattle-Tacoma International Airport (KSEA)
BOEING TRAINER 55 or
BOEING TRAINER 66 HEAVY
PERFORMANCE
757
767-200/300
767-400
757
767-200/300
767-400
LBS (KGS)
LBS (KGS)
LBS (KGS)
LBS (KGS)
LBS (KGS)
LBS (KGS)
180,000 (81,600)
20,000 (9,000)
160,000 (72,600)
10,000 (4,500)
3,200’
60
TO, CLB
5
28.5%
300,000 (136,100)
80,000 (36,300)
220,000 (99,800)
10,000 (4,500)
3,200’
60
TO, CLB
5
22%
330,000 (149,700)
50,000 (22,700)
280,000 (127,000)
10,000 (4,500)
3,200’
60
TO, CLB
5
22%
180,000 (81,600)
20,000 (9,000)
160,000 (72,600)
10,000 (4,500)
3,200’
60
TO, CLB
5
28.5%
300,000 (136,100)
80,000 (36,300)
220,000 (99,800)
10,000 (4,500)
3,200’
60
TO, CLB
5
22%
330,000 (149,700)
50,000 (22,700)
280,000 (127,000)
10,000 (4,500)
3,200’
60
TO, CLB
5
22%
GR WT
FUEL
ZFW
RESERVES
CRZ ALT
COST INDEX
THRUST LIM
FLAPS
CG
WEATHER
WEATHER
SEA Wind calm // Visibility less than 1/4 mile / Runway 16C RVR 500 /
Fog // Ceiling 100 Overcast // Temperature 15°C / Dew Point 14°C
// Altimeter 29.73 (1007 MB) // CAT II/III operations in effect // ILS
RWY 16C in use / Landing and departing RWY 16C.
SEA Wind calm // Visibility less than 1/4 mile / Runway 16C RVR 500 /
Fog // Ceiling 100 Overcast // Temperature 15°C / Dew Point 14°C
// Altimeter 29.73 (1007 MB) // CAT II/III operations in effect // ILS
RWY 16C in use / Landing and departing RWY 16C.
PDX Wind calm // Visibility less than 1/4 mile / Runway 10R RVR 500 /
Fog // Ceiling 100 Overcast // Temperature 15°C / Dew Point 14°C
// Altimeter 29.73 (1007 MB) // CAT II/III operations in effect // ILS
RWY 10R in use / Landing and departing RWY 10R.
PDX Wind calm // Visibility less than 1/4 mile / Runway 10R RVR 500 /
Fog // Ceiling 100 Overcast // Temperature 15°C / Dew Point 14°C
// Altimeter 29.73 (1007 MB) // CAT II/III operations in effect // ILS
RWY 10R in use / Landing and departing RWY 10R.
CLEARANCE
CLEARANCE
Boeing Trainer ____ is cleared to ANVIL. Maintain three thousand two
hundred. After takeoff, right turn direct ANVIL. Expect ILS approach
runway 16C. Departure control 119.2, squawk 2442.
Boeing Trainer ____ is cleared to ANVIL. Maintain three thousand two
hundred. After takeoff, right turn direct ANVIL. Expect ILS approach
runway 16C. Departure control 119.2, squawk 2442.
Copyright © The Boeing Company. See title page for details. EAR 9E991.
November 1, 2017
757/767-O19
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1.3
November 1, 2017
757/767-O19
1.3
1.4
757/767-O19
ALTITUDE FEET X 1,000
ALTITUDE FEET X 1,000
30
40
6
11
12
13
14
15
16
R
30
17
R
18
40
19
50
SHUT
DOWN
20
30
40
2:00
November 1, 2017
Copyright © The Boeing Company. See title page for details. EAR 9E991.
1.4
30
40
6
11
12
13
14
15
16
17
R
18
40
40
0
2:00
19
50
SHUT
DOWN
20
30
40
2:00
KPDX (Night)
50
757/767-O19
0
5
10
KSEA (Night)
1
2
3
4
20
55
30
R
7
40
8
9
50
10
R
TIME
1:00
10
20
30
40
0
2:00
KPDX (Night)
50
5
10
R
30
30
IN TAXI POSITION
AT HOLD POINT 66
R
20
20
10
R
10
10
15
R
TIME
1:00
TIME
1:00
5
PREFLIGHT &
ENGINE START
BY INSTRUCTOR
REPOSITION TO KPDX
TAXI POSITION
RWY 10R (Day)
50
50
10
ALTITUDE FEET X 1,000
15
0
20
40
8
9
R REPOSITION TO 6 MILE FINAL
10
30
7
Full Flight Simulator
CAT II/III
Familiarization
20
0
20
55
R
PROFILE
30
10
KSEA (Night)
1
2
3
R
757/767 Training Manual
40
0
5
4
10
R
20
IN TAXI POSITION
AT HOLD POINT 66
R
10
10
R
TIME
1:00
15
REPOSITION TO KPDX
TAXI POSITION
RWY 10R (Day)
50
PREFLIGHT &
ENGINE START
BY INSTRUCTOR
0
20
R REPOSITION TO 6 MILE FINAL
10
15
20
30
40
0
Full Flight Simulator
CAT II/III
Familiarization
757/767 Training Manual
PROFILE
ALTITUDE FEET X 1,000
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1.5
November 1, 2017
757/767-O19
Select: ENGINE FAIL (at 500’)
757 Select: LEFT EDP and EMP, then RIGHT EDP and
EMP (at 200’)
767 Select: HYD SYS PRESS (L AND R) (at 200’)
(NO AUTOLAND annunciation)
757/767 Training Manual
Reposition to 6 mile final - Clear Malfunction
12 CAT II/III, ILS 10R, missed approach
PROFILE DATA
Reposition to 6 mile final - Clear Malfunction
Preflight and engine start by instructor
In taxi position at HOLD POINT 66
13 CAT II/III, ILS 10R, full stop landing (wet runway)
757 Select: RIGHT GEN OVERVOLTAGE (at 500’),
1
SMGCS taxi
CENTER HYD SYS LEAK (at 300’)
2
Departure RWY 16C
767 Select: GENERATOR OFF (at 500’)
(LAND 2 annunciation)
3
Low visibility takeoff (wind calm)
14
After
touchdown (manual rollout with low visibility)
4
Approach lighting DEMO
757 Select: CENTER HYD SYS LEAK (selected previ5
CAT II/III, ILS 16C, full stop landing
ously) causes autopilot to fail
767 Select: AUTOPILOT FAIL
Reposition to 6 mile final
15 Low visibility RTO, ENGINE FAIL (wind calm)
6
CAT III, ILS 16C, missed app at AH (CAT IIIb) or
16 Low visibility takeoff, ENGINE FAIL after V1
DA(H) (CAT IIIa)
Reposition
to 6 mile final - Clear Malfunction
Reposition to 6 mile final
17 CAT II/III, ILS 10R, missed approach
7
Man F/D, CAT II, ILS 16C, full stop (15 knot x-wind)
Select: ENGINE FAIL (at 500’)
8
SMGCS Taxi
Reposition to 6 mile final - Clear Malfunction
Reposition to KPDX, taxi position RWY 10R (Day)
18 CAT II/III, ILS 10R, missed approach
9
Low visibility RTO, ENGINE FAIL (15 knot x-wind)
757 Select: LEFT EDP and EMP, then RIGHT EDP
and EMP (at 200’)
10 Low vis takeoff, ENGINE FAIL after V1 (wind calm)
767 Select: HYD SYS PRESS (L AND R) (at 200’)
Reposition to 6 mile final - Clear Malfunction
(NO AUTOLAND annunciation)
11 CAT II/III, ILS 10R, missed approach
19 CAT II/III, ILS 10R, full stop landing
757 Select: LEFT EDP and EMP, then RIGHT EDP and
EMP (at 200’)
767 Select: HYD SYS PRESS (L AND R) (at 200’)
(NO AUTOLAND annunciation)
Reposition to 6 mile final - Clear Malfunction
12 CAT II/III, ILS 10R, missed approach
Select: ENGINE FAIL (at 500’)
Reposition to 6 mile final - Clear Malfunction
Preflight and engine start by instructor
In taxi position at HOLD POINT 66
13 CAT II/III, ILS 10R, full stop landing (wet runway)
757 Select: RIGHT GEN OVERVOLTAGE (at 500’),
1
SMGCS taxi
CENTER HYD SYS LEAK (at 300’)
2
Departure RWY 16C
767 Select: GENERATOR OFF (at 500’)
(LAND 2 annunciation)
3
Low visibility takeoff (wind calm)
14
After
touchdown (manual rollout with low visibility)
4
Approach lighting DEMO
757 Select: CENTER HYD SYS LEAK (selected previ5
CAT II/III, ILS 16C, full stop landing
ously) causes autopilot to fail
767 Select: AUTOPILOT FAIL
Reposition to 6 mile final
15 Low visibility RTO, ENGINE FAIL (wind calm)
6
CAT III, ILS 16C, missed app at AH (CAT IIIb) or
16 Low visibility takeoff, ENGINE FAIL after V1
DA(H) (CAT IIIa)
Reposition
to 6 mile final - Clear Malfunction
Reposition to 6 mile final
17 CAT II/III, ILS 10R, missed approach
7
Man F/D, CAT II, ILS 16C, full stop (15 knot x-wind)
Select: ENGINE FAIL (at 500’)
8
SMGCS Taxi
Reposition to 6 mile final - Clear Malfunction
Reposition to KPDX, taxi position RWY 10R (Day)
18 CAT II/III, ILS 10R, missed approach
9
Low visibility RTO, ENGINE FAIL (15 knot x-wind)
757 Select: LEFT EDP and EMP, then RIGHT EDP
and EMP (at 200’)
10 Low vis takeoff, ENGINE FAIL after V1 (wind calm)
767 Select: HYD SYS PRESS (L AND R) (at 200’)
Reposition to 6 mile final - Clear Malfunction
(NO AUTOLAND annunciation)
11 CAT II/III, ILS 10R, missed approach
19 CAT II/III, ILS 10R, full stop landing
757/767 Training Manual
Full Flight Simulator
CAT II/III
Familiarization
Full Flight Simulator
CAT II/III
Familiarization
PROFILE DATA
Copyright © The Boeing Company. See title page for details. EAR 9E991.
1.5
Full Flight Simulator
CAT II/III
Familiarization
Full Flight Simulator
CAT II/III
Familiarization
757/767 Training Manual
PREFLIGHT
757/767 Training Manual
PREFLIGHT
Accomplished by the instructor
Accomplished by the instructor
Complete all required CDU entries
Complete all required CDU entries
ENGINE START
ENGINE START
Fast start accomplished by the instructor
Fast start accomplished by the instructor
TAXI OUT AND TAKEOFF
TAXI OUT AND TAKEOFF
Normal procedures
Normal procedures
In taxi position at HOLD POINT 66
In taxi position at HOLD POINT 66
1
2
3
Surface Movement Guidance and Control System (SMGCS)
Low visibility taxi procedures
Stop Bar lighting
Taxi routes, lighting, and surface markings
Departure RWY 16C
Low visibility takeoff (wind calm)
DEMONSTRATION OF APPROACH LIGHTING
4
At the following RA heights, freeze the simulator to
demonstrate approach lighting. Show DAY and NIGHT conditions
CAT I
200' RA RVR 2400 feet (750 m)
CAT II
100' RA RVR 1200 feet (350 m)
CAT IIIa
50' RA
RVR 700 feet (200 m)
CAT IIIb
50' RA
RVR 600 feet (175 m)
Touchdown
0' RA
RVR 300 feet (75 m)
Characteristics of ILS and runway lighting systems
Runway lighting systems required for CAT II/III
Use of visual cues under reduced RVR
Conditions required to descend below DA(H) or AH
Descent to runway/touchdown zone
Visual references
Approach light system
Threshold markings
REIL
VASI
1
2
3
DEMONSTRATION OF APPROACH LIGHTING
4
Copyright © The Boeing Company. See title page for details. EAR 9E991.
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757/767-O19
November 1, 2017
Surface Movement Guidance and Control System (SMGCS)
Low visibility taxi procedures
Stop Bar lighting
Taxi routes, lighting, and surface markings
Departure RWY 16C
Low visibility takeoff (wind calm)
At the following RA heights, freeze the simulator to
demonstrate approach lighting. Show DAY and NIGHT conditions
CAT I
200' RA RVR 2400 feet (750 m)
CAT II
100' RA RVR 1200 feet (350 m)
CAT IIIa
50' RA
RVR 700 feet (200 m)
CAT IIIb
50' RA
RVR 600 feet (175 m)
Touchdown
0' RA
RVR 300 feet (75 m)
Characteristics of ILS and runway lighting systems
Runway lighting systems required for CAT II/III
Use of visual cues under reduced RVR
Conditions required to descend below DA(H) or AH
Descent to runway/touchdown zone
Visual references
Approach light system
Threshold markings
REIL
VASI
Copyright © The Boeing Company. See title page for details. EAR 9E991.
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757/767-O19
November 1, 2017
757/767 Training Manual
Full Flight Simulator
CAT II/III
Familiarization
757/767 Training Manual
TDZ markings/lights
RWY markings/lights
Procedures/techniques to transition from non-visual to visual flight
under reduced RVR
TDZ markings/lights
RWY markings/lights
Procedures/techniques to transition from non-visual to visual flight
under reduced RVR
PF, PM procedures
PF, PM procedures
APPROACH AND LANDING
APPROACH AND LANDING
5
Autopilot, CAT II/III, ILS approach RWY 16C, full stop landing,
night
Configuration
Flaps 30
Select autobrakes 2 or 3
Use of landing lights
Approach briefing
CAT II/III approach plate
Radio altitude (RA) vs barometric altitude
CAT II DA(H) - set RA equivalent to 100’ above TDZ
(where authorized)
CAT III operations:
Fail Passive: DA(H) - RA 50
(visual reference required)
Fail Operational: Alert Height AH - RA 50
(no visual reference required)
Standard callouts
DA(H) and AH callouts - MINS selector RADIO and/or BARO
CAT II/III required equipment
Second-in-command duties during CAT II/III approaches
757 Autoland procedure
Autopilot, CAT II/III, ILS approach RWY 16C, full stop landing,
night
Configuration
Flaps 30
Select autobrakes 2 or 3
Use of landing lights
Approach briefing
CAT II/III approach plate
Radio altitude (RA) vs barometric altitude
CAT II DA(H) - set RA equivalent to 100’ above TDZ
(where authorized)
CAT III operations:
Fail Passive: DA(H) - RA 50
(visual reference required)
Fail Operational: Alert Height AH - RA 50
(no visual reference required)
Standard callouts
DA(H) and AH callouts - MINS selector RADIO and/or BARO
CAT II/III required equipment
Second-in-command duties during CAT II/III approaches
Autoland status annunciator
1,500 feet radio altitude
FLARE and ROLLOUT armed
ADI annunciations
ASA display LAND 2/3
Autopilot control of the rudder
500 feet radio altitude
Runway align maneuver
Copyright © The Boeing Company. See title page for details. EAR 9E991.
757/767-O19
5
757 Autoland procedure
Autoland status annunciator
1,500 feet radio altitude
FLARE and ROLLOUT armed
ADI annunciations
ASA display LAND 2/3
Autopilot control of the rudder
500 feet radio altitude
Runway align maneuver
November 1, 2017
Full Flight Simulator
CAT II/III
Familiarization
Copyright © The Boeing Company. See title page for details. EAR 9E991.
1.7
November 1, 2017
757/767-O19
1.7
Full Flight Simulator
CAT II/III
Familiarization
Full Flight Simulator
CAT II/III
Familiarization
757/767 Training Manual
330 feet radio altitude
Auto nose up trim
Effect on control when reverting to manual landing
200 feet radio altitude
NO LAND 3 annunciation inhibited
Electrical system auto power transfer inhibited
45 feet radio altitude
FLARE replaces G/S pitch annunciation
ADI annunciations
25 feet radio altitude
A/T retards thrust levers to idle
IDLE replaces SPD autothrottle annunciation
ADI annunciations
5 feet radio altitude
ROLLOUT replaces LOC roll annunciation
Wings leveled when ROLLOUT engaged
ADI annunciations
Rollout
FLARE annunciation disappears at touchdown
A/T disconnects with thrust levers in reverse
330 feet radio altitude
Auto nose up trim
Effect on control when reverting to manual landing
200 feet radio altitude
NO LAND 3 annunciation inhibited
Electrical system auto power transfer inhibited
45 feet radio altitude
FLARE replaces G/S pitch annunciation
ADI annunciations
25 feet radio altitude
A/T retards thrust levers to idle
IDLE replaces SPD autothrottle annunciation
ADI annunciations
5 feet radio altitude
ROLLOUT replaces LOC roll annunciation
Wings leveled when ROLLOUT engaged
ADI annunciations
Rollout
FLARE annunciation disappears at touchdown
A/T disconnects with thrust levers in reverse
767 Autoland procedure
767 Autoland procedure
Autoland status annunciator
1,500 feet radio altitude
FLARE and ROLLOUT armed
ADI annunciations
ASA display LAND 2/3
Autopilot control of the rudder
500 feet radio altitude
Runway align maneuver
330 feet radio altitude (767-200)
Auto nose up trim
Effect on control when reverting to manual landing
200 feet radio altitude
NO LAND 3 annunciation inhibited
Electrical system auto power transfer inhibited
Autoland status annunciator
1,500 feet radio altitude
FLARE and ROLLOUT armed
ADI annunciations
ASA display LAND 2/3
Autopilot control of the rudder
500 feet radio altitude
Runway align maneuver
330 feet radio altitude (767-200)
Auto nose up trim
Effect on control when reverting to manual landing
200 feet radio altitude
NO LAND 3 annunciation inhibited
Electrical system auto power transfer inhibited
Copyright © The Boeing Company. See title page for details. EAR 9E991.
1.8
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757/767 Training Manual
November 1, 2017
Copyright © The Boeing Company. See title page for details. EAR 9E991.
1.8
757/767-O19
November 1, 2017
757/767 Training Manual
Full Flight Simulator
CAT II/III
Familiarization
100 feet radio altitude (767-300/400)
Auto nose up trim
Effect on control when reverting to manual landing
50 feet radio altitude
FLARE replaces G/S pitch annunciation
ADI annunciations
15 feet radio altitude
A/T retards thrust levers to idle
IDLE replaces SPD autothrottle annunciation
ADI annunciations
5 feet radio altitude
ROLLOUT replaces LOC roll annunciation
Wings leveled when ROLLOUT engaged
ADI annunciations
Rollout
FLARE annunciation disappears at touchdown
A/T disconnects with thrust levers in reverse
Complete AUTOLAND and ROLLOUT
757/767 Training Manual
Full Flight Simulator
CAT II/III
Familiarization
100 feet radio altitude (767-300/400)
Auto nose up trim
Effect on control when reverting to manual landing
50 feet radio altitude
FLARE replaces G/S pitch annunciation
ADI annunciations
15 feet radio altitude
A/T retards thrust levers to idle
IDLE replaces SPD autothrottle annunciation
ADI annunciations
5 feet radio altitude
ROLLOUT replaces LOC roll annunciation
Wings leveled when ROLLOUT engaged
ADI annunciations
Rollout
FLARE annunciation disappears at touchdown
A/T disconnects with thrust levers in reverse
Complete AUTOLAND and ROLLOUT
APPROACH AND LANDING
APPROACH AND LANDING
Reposition to 6 mile final
6
Autopilot, CAT III, ILS approach RWY 16C,
missed approach at AH (CAT IIIb) or DA(H) (CAT IIIa)
Autopilot missed approach
Reposition to 6 mile final
6
Autopilot, CAT III, ILS approach RWY 16C,
missed approach at AH (CAT IIIb) or DA(H) (CAT IIIa)
Autopilot missed approach
GA switch
Flight Mode Annunciations
Pitch and roll commands activate in GA
Flap retraction
Missed approach waypoints
LNAV use
GA switch
Flight Mode Annunciations
Pitch and roll commands activate in GA
Flap retraction
Missed approach waypoints
LNAV use
Copyright © The Boeing Company. See title page for details. EAR 9E991.
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757/767-O19
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1.9
November 1, 2017
757/767-O19
1.9
Full Flight Simulator
CAT II/III
Familiarization
Full Flight Simulator
CAT II/III
Familiarization
757/767 Training Manual
757/767 Training Manual
APPROACH AND LANDING
APPROACH AND LANDING
Reposition to 6 mile final
7
Manual, F/D, CAT II, ILS approach RWY 16C,
full stop landing (15 knot crosswind), night
Configuration
Reposition to 6 mile final
7
Manual, F/D, CAT II, ILS approach RWY 16C,
full stop landing (15 knot crosswind), night
Configuration
8
Flaps 30
Select autobrakes 2 or 3
Use of landing lights
Decision Height DA(H) recognition
Flaps 30
Select autobrakes 2 or 3
Use of landing lights
Decision Height DA(H) recognition
DA(H) callouts - PM voice backup
DA(H) callouts - PM voice backup
RVR information and limitations
RVR information and limitations
RA display/authorization/inoperative
RA display/authorization/inoperative
Flare and touchdown
Flare and touchdown
SMGCS taxi procedures
8
SMGCS taxi procedures
TAKEOFF
TAKEOFF
Reposition to KPDX, taxi position RWY 10R
9
Low visibility rejected takeoff (RTO), engine failure, 500 RVR
(15 knot crosswind)
Timely engine failure recognition
Reasons for reject (high speed/low speed)
PM call out malfunction and 60 knots
Autobrake use
Speedbrake use
Actions after stopping
Notify tower
Notify passengers/cabin crew
Perform non-normal checklist (if required)
Evacuate the airplane (if required)
Taxi clear of runway (if appropriate)
Review Brake Cooling Schedule
10 Low visibility takeoff, engine failure after V1, 500 RVR
(wind calm)
ENGINE FAILURE OR SHUTDOWN
Reposition to KPDX, taxi position RWY 10R
9
Low visibility rejected takeoff (RTO), engine failure, 500 RVR
(15 knot crosswind)
Timely engine failure recognition
Reasons for reject (high speed/low speed)
PM call out malfunction and 60 knots
Autobrake use
Speedbrake use
Actions after stopping
Notify tower
Notify passengers/cabin crew
Perform non-normal checklist (if required)
Evacuate the airplane (if required)
Taxi clear of runway (if appropriate)
Review Brake Cooling Schedule
10 Low visibility takeoff, engine failure after V1, 500 RVR
(wind calm)
ENGINE FAILURE OR SHUTDOWN
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1.10
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November 1, 2017
757/767 Training Manual
Full Flight Simulator
CAT II/III
Familiarization
757/767 Training Manual
Full Flight Simulator
CAT II/III
Familiarization
APPROACH AND LANDING
APPROACH AND LANDING
Reposition to 6 mile final - Clear Malfunction
11 Autopilot, CAT II/III, ILS approach RWY 10R, missed approach
Approach briefing
CAT II/III approach plate
Radio altitude (RA) vs barometric altitude
CAT II DA(H) - set RA equivalent to 100’ above TDZ
(KPDX - RA 107)
CAT III operations:
Reposition to 6 mile final - Clear Malfunction
11 Autopilot, CAT II/III, ILS approach RWY 10R, missed approach
Approach briefing
CAT II/III approach plate
Radio altitude (RA) vs barometric altitude
CAT II DA(H) - set RA equivalent to 100’ above TDZ
(KPDX - RA 107)
CAT III operations:
Fail Passive: DA(H) - RA 50 (visual reference required)
Fail Operational: Alert Height AH - RA 50
(no visual reference required)
Engine failure (at 500 feet)
Fail Passive: DA(H) - RA 50 (visual reference required)
Fail Operational: Alert Height AH - RA 50
(no visual reference required)
Engine failure (at 500 feet)
Instrument and equipment failure warning systems
Autopilot/Flight Director
Respective electronic displays
PF, PM procedures
Positive monitoring
Non-normal procedures/indications/actions
Missed approach
Instrument and equipment failure warning systems
Autopilot/Flight Director
Respective electronic displays
PF, PM procedures
Positive monitoring
Non-normal procedures/indications/actions
Missed approach
APPROACH AND LANDING
APPROACH AND LANDING
Reposition to 6 mile final - Clear Malfunction
12 Autopilot, CAT II/III, ILS approach RWY 10R, missed approach
757 - LEFT EDP and EMP, then RIGHT EDP and EMP (at 200’)
Reposition to 6 mile final - Clear Malfunction
12 Autopilot, CAT II/III, ILS approach RWY 10R, missed approach
757 - LEFT EDP and EMP, then RIGHT EDP and EMP (at 200’)
767 - HYDRAULIC SYSTEM PRESSURE (L AND R) (at 200’)
767 - HYDRAULIC SYSTEM PRESSURE (L AND R) (at 200’)
NO AUTOLAND annunciation
Instrument and equipment failure warning systems
Autopilot/Flight Director
Respective electronic displays
PF, PM procedures
Positive monitoring
Non-normal procedures/indications/actions
Missed approach
NO AUTOLAND annunciation
Instrument and equipment failure warning systems
Autopilot/Flight Director
Respective electronic displays
PF, PM procedures
Positive monitoring
Non-normal procedures/indications/actions
Missed approach
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November 1, 2017
757/767-O19
Copyright © The Boeing Company. See title page for details. EAR 9E991.
1.11
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757/767-O19
1.11
Full Flight Simulator
CAT II/III
Familiarization
Full Flight Simulator
CAT II/III
Familiarization
757/767 Training Manual
757/767 Training Manual
APPROACH AND LANDING
APPROACH AND LANDING
Reposition to 6 mile final - Clear Malfunction
13 Autopilot, CAT II/III, ILS approach RWY 10R,
full stop landing (wet runway), night
757 - RIGHT GENERATOR OVERVOLTAGE (at 500 feet),
CENTER HYDRAULIC SYSTEM LEAK (at 300 feet)
Reposition to 6 mile final - Clear Malfunction
13 Autopilot, CAT II/III, ILS approach RWY 10R,
full stop landing (wet runway), night
757 - RIGHT GENERATOR OVERVOLTAGE (at 500 feet),
CENTER HYDRAULIC SYSTEM LEAK (at 300 feet)
14
767 - GENERATOR OFF (at 500 feet)
767 - GENERATOR OFF (at 500 feet)
LAND 2 annunciation
After touchdown (manual rollout with low visibility)
757 - CENTER HYDRAULIC SYSTEM LEAK
(selected previously) causes autopilot to fail
LAND 2 annunciation
After touchdown (manual rollout with low visibility)
757 - CENTER HYDRAULIC SYSTEM LEAK
(selected previously) causes autopilot to fail
14
767 - AUTOPILOT FAIL
767 - AUTOPILOT FAIL
TAKEOFF
TAKEOFF
In taxi position RWY 10R, KPDX
15 Low visibility rejected takeoff (RTO), engine failure,
500 RVR (wind calm)
16 Low visibility takeoff, engine failure after V1, 500 RVR
In taxi position RWY 10R, KPDX
15 Low visibility rejected takeoff (RTO), engine failure,
500 RVR (wind calm)
16 Low visibility takeoff, engine failure after V1, 500 RVR
APPROACH AND LANDING
APPROACH AND LANDING
Reposition to 6 mile final - Clear Malfunction
17 CAT II/III, ILS approach RWY 10R, missed approach
Engine failure (at 500 feet)
Reposition to 6 mile final - Clear Malfunction
17 CAT II/III, ILS approach RWY 10R, missed approach
Engine failure (at 500 feet)
APPROACH AND LANDING
APPROACH AND LANDING
Reposition to 6 mile final - Clear Malfunction
18 CAT II/III, ILS approach RWY 10R, missed approach
757 - LEFT EDP and EMP, then RIGHT EDP and EMP
(at 200 feet)
767 - HYDRAULIC SYSTEM PRESSURE (L AND R)
(at 200 feet)
NO AUTOLAND annunciation
Reposition to 6 mile final - Clear Malfunction
18 CAT II/III, ILS approach RWY 10R, missed approach
757 - LEFT EDP and EMP, then RIGHT EDP and EMP
(at 200 feet)
767 - HYDRAULIC SYSTEM PRESSURE (L AND R)
(at 200 feet)
NO AUTOLAND annunciation
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November 1, 2017
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1.12
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November 1, 2017
757/767 Training Manual
Full Flight Simulator
CAT II/III
Familiarization
APPROACH AND LANDING
19
757/767 Training Manual
APPROACH AND LANDING
Autopilot, CAT II/III, ILS approach RWY 10R, full stop landing,
night
TAXI IN AND SHUTDOWN
19
Autopilot, CAT II/III, ILS approach RWY 10R, full stop landing,
night
TAXI IN AND SHUTDOWN
After landing procedures
After landing procedures
Shutdown procedures/checklist
Shutdown procedures/checklist
Copyright © The Boeing Company. See title page for details. EAR 9E991.
November 1, 2017
757/767-O19
Full Flight Simulator
CAT II/III
Familiarization
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1.13
November 1, 2017
757/767-O19
1.13
Full Flight Simulator
CAT II/III
Familiarization
Full Flight Simulator
CAT II/III
Familiarization
757/767 Training Manual
757/767 Training Manual
CAT II/III TRAINING
BRIEFING GUIDE
CAT II/III TRAINING
BRIEFING GUIDE
(FOR FAMILIARIZATION PURPOSES ONLY)
(FOR FAMILIARIZATION PURPOSES ONLY)
LOW VISIBILITY TAKEOFF BRIEFING
LOW VISIBILITY TAKEOFF BRIEFING
Weather at destination and alternate
Rejected Takeoff considerations
Weather at destination and alternate
Rejected Takeoff considerations
CAT II/III APPROACH BRIEFING
CAT II/III APPROACH BRIEFING
Weather at destination and alternate
Weather at destination and alternate
LANDING VISIBILITY REQUIREMENTS
LANDING VISIBILITY REQUIREMENTS
Required and
Must be used
Controlling Advisory
CAT
Minimum
1600’
Touchdown (TDZ)
TDZ
N/A
II
II
1200’
Touchdown & Rollout
TDZ
Rollout *
IIIa
700’
Touchdown, Mid, Rollout
TDZ, MID
IIIb
600’
Touchdown, Mid, Rollout
TDZ, MID,
Rollout
CAT
Minimum
II
Required and
Must be used
Controlling Advisory
1600’
Touchdown (TDZ)
TDZ
N/A
II
1200’
Touchdown & Rollout
TDZ
Rollout *
Rollout
IIIa
700’
Touchdown, Mid, Rollout
TDZ, MID
Rollout
N/A
IIIb
600’
Touchdown, Mid, Rollout
TDZ, MID,
Rollout
N/A
* If rollout is not available, MID may be substituted.
* If rollout is not available, MID may be substituted.
Controlling: RVR minimum required to begin final segment.
Advisory: Must be available but no minimum RVR required to
begin final segment.
LOWEST MINIMA AUTHORIZED FOR FAIL OPERATIONAL OR
FAIL PASSIVE LANDING AND ROLLOUT SYSTEMS
Controlling: RVR minimum required to begin final segment.
Advisory: Must be available but no minimum RVR required to
begin final segment.
LOWEST MINIMA AUTHORIZED FOR FAIL OPERATIONAL OR
FAIL PASSIVE LANDING AND ROLLOUT SYSTEMS
Landing System
Type
Rollout System
Type
TDZ
RVR
Mid
RVR
Rollout
RVR
Landing System
Type
Rollout System
Type
TDZ
RVR
Mid
RVR
Rollout
RVR
Fail Op or Fail
Passive
Any approved
rollout system
600
400
400
Fail Op or Fail
Passive
Any approved
rollout system
600
400
400
Fail Op
Fail Passive
400
400
400
Fail Op
Fail Passive
400
400
400
Fail Op
Fail Op
300*
300*
300*
Fail Op
Fail Op
300*
300*
300*
* Lowest operationally authorized.
* Lowest operationally authorized.
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November 1, 2017
Copyright © The Boeing Company. See title page for details. EAR 9E991.
1.14
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November 1, 2017
757/767 Training Manual
Full Flight Simulator
CAT II/III
Familiarization
757/767 Training Manual
Full Flight Simulator
CAT II/III
Familiarization
NOTAMS and ATIS for ILS performance and status or degradation
Airplane condition, systems status and CAT II/III MEL status
Standard callouts per Flight Crew Training Manual
Approach profile and go-around procedure
NOTAMS and ATIS for ILS performance and status or degradation
Airplane condition, systems status and CAT II/III MEL status
Standard callouts per Flight Crew Training Manual
Approach profile and go-around procedure
CAT II DA(H) - set RA equivalent to 100’ above TDZ
(where authorized)
CAT III operations:
Fail Passive: DA(H) - RA 50
(visual reference required)
Fail Operational: Alert Height AH - RA 50
(no visual reference required)
Consideration of rollout conditions, including visibility, runway exiting
Use of landing lights
CAT II DA(H) - set RA equivalent to 100’ above TDZ
(where authorized)
CAT III operations:
Fail Passive: DA(H) - RA 50
(visual reference required)
Fail Operational: Alert Height AH - RA 50
(no visual reference required)
Consideration of rollout conditions, including visibility, runway exiting
Use of landing lights
CAT II/III APPROACH TECHNIQUES
CAT II/III APPROACH TECHNIQUES
Select autobrakes 2 or 3
Start APU at 10,000 feet
Check winds (per regulatory authority)
Max. Headwind - 25 knots
Max. Tailwind - 10 knots or 15 knots (check AFM)
Max. Crosswind - 25 knots
Flaps 30 landing recommended
Captain makes all CAT II/III approaches and landings
Select autobrakes 2 or 3
Start APU at 10,000 feet
Check winds (per regulatory authority)
Max. Headwind - 25 knots
Max. Tailwind - 10 knots or 15 knots (check AFM)
Max. Crosswind - 25 knots
Flaps 30 landing recommended
Captain makes all CAT II/III approaches and landings
CAT II OPERATIONS
CAT II OPERATIONS
Category II approaches may be conducted using single or multiple
autopilots, or flight director only, with one or two engines. If an engine
fails prior to final approach, the rudder must be trimmed for this
condition. Autothrottles should be disconnected when the autopilot is
disengaged. For single autopilot operation, the autopilot must be
disengaged no lower than the minimum altitude listed in the Limitations
Chapter of the Operations Manual.
CATEGORY II APPROACH AUTOPILOT
CATEGORY II APPROACH AUTOPILOT
The following equipment must be operative for an automatic approach
requiring the use of Category II minima:
• 1 (or more) autopilots engaged
• 2 independent sources of electrical power. (The APU may be a
substitute source of power for the left or right electrical system.)
Copyright © The Boeing Company. See title page for details. EAR 9E991.
November 1, 2017
757/767-O19
Category II approaches may be conducted using single or multiple
autopilots, or flight director only, with one or two engines. If an engine
fails prior to final approach, the rudder must be trimmed for this
condition. Autothrottles should be disconnected when the autopilot is
disengaged. For single autopilot operation, the autopilot must be
disengaged no lower than the minimum altitude listed in the Limitations
Chapter of the Operations Manual.
The following equipment must be operative for an automatic approach
requiring the use of Category II minima:
• 1 (or more) autopilots engaged
• 2 independent sources of electrical power. (The APU may be a
substitute source of power for the left or right electrical system.)
Copyright © The Boeing Company. See title page for details. EAR 9E991.
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757/767-O19
1.15
Full Flight Simulator
CAT II/III
Familiarization
Full Flight Simulator
CAT II/III
Familiarization
757/767 Training Manual
757-200 - 767-300
• 2 attitude indicators supplied by different symbol generators including
attitude, radio altitude, ILS deviation, DA(H) indication and AFDS
status
767-400
• 2 attitude indicators supplied by different display processing computers
including attitude, radio altitude, ILS deviation, DA(H) indication and
AFDS status
757-200, 767-200, 767-300
• 2 (or 3) IRU's associated with the engaged autopilot(s) in Nav mode
757-300, 767-400
• 2 (or 3) ADIRU's associated with the engaged autopilot(s) in Nav mode
CATEGORY II APPROACH FLIGHT DIRECTOR
The following equipment must be operative for a Flight Director (FD)
approach requiring the use of Category II minima:
• 2 independent sources of electrical power. (The APU may be a
substitute source of power for the left or right electrical system.)
• 2 separate flight directors, one of which must be the right FD
757-200 - 767-300
• 2 attitude indicators supplied by different symbol generators including
attitude, radio altitude, ILS deviation, DA(H) indication and AFDS
status
767-400
• 2 attitude indicators supplied by different display processing computers
including attitude, radio altitude, ILS deviation, DA(H) indication and
AFDS status
757-200, 767-200, 767-300
• 2 (or 3) IRU's in Nav mode
757-300, 767-400
• 2 (or 3) ADIRU's in Nav mode
757-200 - 767-300
• 2 attitude indicators supplied by different symbol generators including
attitude, radio altitude, ILS deviation, DA(H) indication and AFDS
status
767-400
• 2 attitude indicators supplied by different display processing computers
including attitude, radio altitude, ILS deviation, DA(H) indication and
AFDS status
757-200, 767-200, 767-300
• 2 (or 3) IRU's associated with the engaged autopilot(s) in Nav mode
757-300, 767-400
• 2 (or 3) ADIRU's associated with the engaged autopilot(s) in Nav mode
CATEGORY II APPROACH FLIGHT DIRECTOR
The following equipment must be operative for a Flight Director (FD)
approach requiring the use of Category II minima:
• 2 independent sources of electrical power. (The APU may be a
substitute source of power for the left or right electrical system.)
• 2 separate flight directors, one of which must be the right FD
757-200 - 767-300
• 2 attitude indicators supplied by different symbol generators including
attitude, radio altitude, ILS deviation, DA(H) indication and AFDS
status
767-400
• 2 attitude indicators supplied by different display processing computers
including attitude, radio altitude, ILS deviation, DA(H) indication and
AFDS status
757-200, 767-200, 767-300
• 2 (or 3) IRU's in Nav mode
757-300, 767-400
• 2 (or 3) ADIRU's in Nav mode
Copyright © The Boeing Company. See title page for details. EAR 9E991.
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November 1, 2017
757/767 Training Manual
Copyright © The Boeing Company. See title page for details. EAR 9E991.
1.16
757/767-O19
November 1, 2017
757/767 Training Manual
Full Flight Simulator
CAT II/III
Familiarization
CAT III OPERATIONS
CAT III OPERATIONS
Category III operations are based on an approach to touchdown using the
automatic landing system. Normal operations should not require pilot
intervention. However, pilot intervention should be anticipated in the
event inadequate airplane performance is suspected, or when an
automatic landing cannot be safely accomplished in the touchdown
zone. Guard the controls on approach through the landing roll and be
prepared to take over manually, if required.
The airplane is certified for Category IIIb operations with two engines
operating. The airplane is certified for Category IIIa operations with two
engines operating or with one engine inoperative if the engine failure
occurs during the final approach.
Note: Some airplanes are also certified for Category IIIa approach and
autoland through rollout, with an engine inoperative prior to
selecting landing flaps. See Engine Out Autoland tables in the ILS
- One Engine Inoperative section.
CATEGORY IIIA/AUTOLAND
Copyright © The Boeing Company. See title page for details. EAR 9E991.
757/767-O19
Category III operations are based on an approach to touchdown using the
automatic landing system. Normal operations should not require pilot
intervention. However, pilot intervention should be anticipated in the
event inadequate airplane performance is suspected, or when an
automatic landing cannot be safely accomplished in the touchdown
zone. Guard the controls on approach through the landing roll and be
prepared to take over manually, if required.
The airplane is certified for Category IIIb operations with two engines
operating. The airplane is certified for Category IIIa operations with two
engines operating or with one engine inoperative if the engine failure
occurs during the final approach.
Note: Some airplanes are also certified for Category IIIa approach and
autoland through rollout, with an engine inoperative prior to
selecting landing flaps. See Engine Out Autoland tables in the ILS
- One Engine Inoperative section.
CATEGORY IIIA/AUTOLAND
For Category IIIa operations the following equipment must be operative
and LAND 2 or LAND 3 annunciated:
• 2 independent sources of electrical power. (The APU generator may be
a substitute source of power for the left or right electrical system.)
• 2 or 3 autopilots
• 3 hydraulic systems
757-200 - 767-300
• 2 attitude indicators supplied by different symbol generators including
attitude, radio altitude, ILS deviation, DA(H) or AH indications, and
AFDS status
767-400
• 2 attitude indicators supplied by different display processing computers
including attitude, radio altitude, ILS deviation, DA(H) or AH
indications, and AFDS status
757-200 - 767-300
• 2 (or 3) IRU's (associated with the engaged autopilots) in Nav mode
767-400
• 2 (or 3) ADIRU's (associated with the engaged autopilots) in Nav mode
757-200 - 767-300
• autoland status annunciator for the pilot conducting the approach
November 1, 2017
757/767 Training Manual
Full Flight Simulator
CAT II/III
Familiarization
For Category IIIa operations the following equipment must be operative
and LAND 2 or LAND 3 annunciated:
• 2 independent sources of electrical power. (The APU generator may be
a substitute source of power for the left or right electrical system.)
• 2 or 3 autopilots
• 3 hydraulic systems
757-200 - 767-300
• 2 attitude indicators supplied by different symbol generators including
attitude, radio altitude, ILS deviation, DA(H) or AH indications, and
AFDS status
767-400
• 2 attitude indicators supplied by different display processing computers
including attitude, radio altitude, ILS deviation, DA(H) or AH
indications, and AFDS status
757-200 - 767-300
• 2 (or 3) IRU's (associated with the engaged autopilots) in Nav mode
767-400
• 2 (or 3) ADIRU's (associated with the engaged autopilots) in Nav mode
757-200 - 767-300
• autoland status annunciator for the pilot conducting the approach
Copyright © The Boeing Company. See title page for details. EAR 9E991.
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1.17
Full Flight Simulator
CAT II/III
Familiarization
Full Flight Simulator
CAT II/III
Familiarization
757/767 Training Manual
CATEGORY IIIB/AUTOLAND
CATEGORY IIIB/AUTOLAND
For Category IIIb operations, visual reference is not normally a specific
requirement for continuation of the approach to touchdown. Category
IIIb operations require the following equipment to be operative and
LAND 3 annunciated:
• 3 autopilots
• 3 hydraulic systems
• autothrottle
• 3 independent sources of electrical power. Normally the left generator,
the right generator and the battery bus. (The APU generator may be a
substitute source of power for the left or right engine driven generator.)
757-200 - 767-300
• 2 autoland status annunciators
757-200 - 767-300
• 2 attitude indicators supplied by different symbol generators including
attitude, radio altitude, ILS deviation, AH or DA(H) indications, and
AFDS status
767-400
• 2 attitude indicators supplied by different display processing computers
including attitude, radio altitude, ILS deviation, AH or DA(H)
indications, and AFDS status
757-200, 767-200, 767-300
• 3 IRU's in Nav mode
757-300, 767-400
• 3 ADIRU's in Nav mode approach, the following can be used for any
AFDS fault indication
For Category IIIb operations, visual reference is not normally a specific
requirement for continuation of the approach to touchdown. Category
IIIb operations require the following equipment to be operative and
LAND 3 annunciated:
• 3 autopilots
• 3 hydraulic systems
• autothrottle
• 3 independent sources of electrical power. Normally the left generator,
the right generator and the battery bus. (The APU generator may be a
substitute source of power for the left or right engine driven generator.)
757-200 - 767-300
• 2 autoland status annunciators
757-200 - 767-300
• 2 attitude indicators supplied by different symbol generators including
attitude, radio altitude, ILS deviation, AH or DA(H) indications, and
AFDS status
767-400
• 2 attitude indicators supplied by different display processing computers
including attitude, radio altitude, ILS deviation, AH or DA(H)
indications, and AFDS status
757-200, 767-200, 767-300
• 3 IRU's in Nav mode
757-300, 767-400
• 3 ADIRU's in Nav mode approach, the following can be used for any
AFDS fault indication
Copyright © The Boeing Company. See title page for details. EAR 9E991.
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757/767 Training Manual
November 1, 2017
Copyright © The Boeing Company. See title page for details. EAR 9E991.
1.18
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November 1, 2017
757/767 Training Manual
Full Flight Simulator
CAT II/III
Familiarization
PILOT RESPONSE TO APPROACH, LANDING, AND
GO-AROUND ALERTS
Alert
Above 200 ft.
AGL
Below 200
ft. AGL
During
Rollout
757/767 Training Manual
Full Flight Simulator
CAT II/III
Familiarization
PILOT RESPONSE TO APPROACH, LANDING, AND
GO-AROUND ALERTS
During GoAround
Alert
Master Warning/Caution Lights with EICAS Messages (see note)
Above 200 ft.
AGL
Below 200
ft. AGL
During
Rollout
During GoAround
Master Warning/Caution Lights with EICAS Messages (see note)
AUTOPILOT DISC
(Warning)
*Execute
manual goaround
**Execute
manual
go-around
Execute
Execute manual
manual rollout go-around
AUTOPILOT DISC
(Warning)
*Execute
manual goaround
**Execute
manual
go-around
Execute
Execute manual
manual rollout go-around
AUTOPILOT
(Caution)
*Execute goaround
**Execute
go-around
Disengage
A/P and
execute a
manual rollout
Disengage A/P
and execute a
manual goaround
AUTOPILOT
(Caution)
*Execute goaround
**Execute
go-around
Disengage
A/P and
execute a
manual rollout
Disengage A/P
and execute a
manual goaround
AUTOTHROT
DISC (Caution)
*Continue with
manual thrust
control (if Cat
IIIb-***)
***
N/A
Continue with
manual thrust
control
AUTOTHROT
DISC (Caution)
*Continue with
manual thrust
control (if Cat
IIIb-***)
***
N/A
Continue with
manual thrust
control
SPEEDBRAKES
EXT (Caution)
Retract
speedbrakes
**Execute
go-around
N/A
Retract
speedbrakes
SPEEDBRAKES
EXT (Caution)
Retract
speedbrakes
**Execute
go-around
N/A
Retract
speedbrakes
Autoland Status Annunciation
Autoland Status Annunciation
NO LAND 3
or
LAND 2
*Continue
approach
(if Cat IIIbgo-around)
N/A
(message
inhibited)
N/A
N/A
NO LAND 3
or
LAND 2
*Continue
approach
(if Cat IIIbgo-around)
N/A
(message
inhibited)
N/A
N/A
NO AUTOLAND
*Execute goaround
**Execute
go-around
N/A
N/A
NO AUTOLAND
*Execute goaround
**Execute
go-around
N/A
N/A
Flashing G/S or LOC Indicators (as installed)
ILS Deviation Alert
*Execute goaround
**Execute
go-around
N/A
Flashing G/S or LOC Indicators (as installed)
N/A
ILS Deviation Alert
*Execute goaround
**Execute
go-around
N/A
N/A
* If suitable visual reference is not established.
* If suitable visual reference is not established.
** If suitable visual reference is established, land.
** If suitable visual reference is established, land.
***Refer to the AFM or approved procedures for recommended pilot response.
***Refer to the AFM or approved procedures for recommended pilot response.
NOTE: All other EICAS messages are dealt with according to QRH procedures.
NOTE: Information in this table is based on FAA regulations and utilized for
training purposes only. Individual operators should ensure procedural
compliance with applicable regulatory requirements and AFM/company
limitations.
NOTE: All other EICAS messages are dealt with according to QRH procedures.
NOTE: Information in this table is based on FAA regulations and utilized for
training purposes only. Individual operators should ensure procedural
compliance with applicable regulatory requirements and AFM/company
limitations.
Copyright © The Boeing Company. See title page for details. EAR 9E991.
November 1, 2017
757/767-O19
Copyright © The Boeing Company. See title page for details. EAR 9E991.
1.19
November 1, 2017
757/767-O19
1.19
Full Flight Simulator
CAT II/III
Familiarization
Full Flight Simulator
CAT II/III
Familiarization
757/767 Training Manual
Intentionally
Blank
Intentionally
Blank
Copyright © The Boeing Company. See title page for details. EAR 9E991.
1.20
757/767-O19
757/767 Training Manual
November 1, 2017
Copyright © The Boeing Company. See title page for details. EAR 9E991.
1.20
757/767-O19
November 1, 2017