3.
Chapter 0 Preface
Section 0 Chapter Table of Contents
0.TOC.2 February 06, 2013
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Volume 1
INTENTIONALLY LEFT BLANK
4.
Preface Chapter 0
V1 V2 V3 Model Identification Section 1
April 18, 2014 0.1.1
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Volume 1
General
The airplanes listed in the table below are covered in the Flight Crew
Operations Manual (FCOM). The numbers are used to distinguish data
peculiar to one or more, but not all of the airplanes. Where data applies to all
airplanes listed, no reference is made to individual airplane numbers.
Use of the table below permits flight crew correlation of configuration
differences by number within an operator's fleet for airplanes covered in this
manual. Configuration data reflects the airplane as delivered configuration and
is updated for service bulletin incorporations in conformance with the policy
stated in the introduction section of this chapter.
Registry number is supplied by the national regulatory agency. Serial and
tabulation numbers are supplied by Boeing.
Registry Number Serial Number Tabulation Number
N531UA 25042 NE041
N557CM 23687 NC042
N605DL 22812 NA505
N620DL 22910 NA520
N751CX 26273 NC071
N752CX 24451 NA198
N753CX 26152 NB324
N754CX 26154 NB326
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Chapter 0 Preface
Section 1 V1 V2 V3 Model Identification
0.1.2 May 6, 2013
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6.
Preface Chapter 0
Introduction Section 2
February 06, 2013 0.2.1
757-200
Flight Crew Operations Manual
Volume 1
General
This Flight Crew Operations Manual has been prepared by Air Transport
International. The purpose of this manual is to:
• provide the operating limitations, procedures, performance, and
systems information the flight crew needs to safely and efficiently
operate the 757 airplane during all anticipated operations
• serve as a comprehensive reference for use during transition training
for the 757 airplane
• serve as a review guide for use in recurrent training and proficiency
checks
• provide necessary operational data from the FAA approved airplane
flight manual (AFM) to ensure that legal requirements are satisfied
• establish standardized procedures and practices to enhance Boeing
operational philosophy and policy.
This manual is prepared for the owner/operator named on the title page
specifically for the airplanes listed in the "Model Identification" section. It
contains operational procedures and information, which apply only to these
airplanes. The manual covers the Boeing delivered configuration of these
airplanes. Changes to the delivered configuration are incorporated when
covered by contractual revision agreements between the owner/operator and
The Boeing Company.
This manual is not suitable for use for any airplanes not listed in the "Model
Identification" section. Further, it may not be suitable for airplanes that have
been transferred to other owners/operators.
Owners/operators are solely responsible for ensuring the operational
documentation they are using is complete and matches the current
configuration of the listed airplanes. This includes the accuracy and validity of
all information furnished by the owner/operator or any other party. Owners/
operators receiving active revision service are responsible to ensure that any
modifications to the listed airplanes are properly reflected in the operational
procedures and information contained in this manual.
The manual is periodically revised to incorporate pertinent procedural and
systems information. Items of a more critical nature will be incorporated in
operational bulletins and distributed in a timely manner. In all cases, such
revisions and changes must remain compatible with the approved AFM with
which the operator must comply. In the event of conflict with the AFM, the
AFM shall supersede.
7.
Chapter 0 Preface
Section 2 Introduction
0.2.2 February 06, 2013
757-200
Flight Crew Operations Manual
Volume 1
This manual is written under the assumption that the user has had previous
multi-engine jet aircraft experience and is familiar with basic jet airplane
systems and basic pilot techniques common to airplanes of this type.
Therefore, the operations manual does not contain basic flight information that
is considered prerequisite training.
8.
Preface Chapter 0
Introduction Section 2
February 06, 2013 0.2.3
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Flight Crew Operations Manual
Volume 1
Organization
The Flight Crew Operations Manual (FCOM) is organized in the following
manner.
Volume 1 -
• Preface - contains general information regarding the manual's
purpose, structure, and content. It also contains lists of abbreviations,
a record of revisions, bulletins, and a list of effective pages.
• Limitations and Normal Procedures chapters cover operational
limitations and normal procedures. All operating procedures are based
on a thorough analysis of crew activity required to operate the
airplane, and reflect the latest knowledge and experience available.
• Supplementary Procedures chapter covers those procedures
accomplished as required rather than routinely on each flight.
• Performance Inflight chapter contains performance information to
supplement data from the Flight management Computer (FMC).
Volume 2 - Chapters 1 through 15 contain general airplane and systems
information. These chapters are generally subdivided into sections covering
controls and indicators and systems descriptions.
Quick Reference Handbook (QRH) - The QRH covers normal checklists, in-
flight performance, non-normal checklists, and non-normal maneuvers.
Page Numbering
The FCOM uses a decimal page numbering system. The page number is
divided into three fields; chapter, section, and page. An example of a page
number for the hydraulics chapter follows: chapter 13, section 20, page 3.
Example Page Number
CHAPTER (HYDRAULICS)
SECTION (SYSTEMS DESCRIPTION)
PAGE NUMBER
13.20.3
9.
Chapter 0 Preface
Section 2 Introduction
0.2.4 February 06, 2013
757-200
Flight Crew Operations Manual
Volume 1
Warnings, Cautions, and Notes
The following levels of written advisories are used throughout the manual and
are not to be confused with EICAS messages, which are separately identified
in the text.
WARNING: An operating procedure, technique, etc., that may result
in personal injury or loss of life if not carefully followed.
CAUTION: An operating procedure, technique, etc., that may result in
damage to equipment if not carefully followed.
Note: An operating procedure, technique, etc., considered essential to
emphasize. Information contained in notes may also be safety related.
Flight Crew Operations Manual Configuration
Customer airplane configuration determines the data provided in this manual.
The Boeing Company keeps a list of each airplane configuration as it is built
and modified through the Service Bulletin process. The FCOM does not reflect
customer originated modifications without special contract provisions.
10.
Preface Chapter 0
Introduction Section 2
February 06, 2013 0.2.5
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Flight Crew Operations Manual
Volume 1
Airplane Effectivities
Differences in airplane configuration are shown by use of airplane effectivities
throughout Volumes 1 and 2, and the Quick Reference Handbook.
The following rules are used to express airplane effectivities:
1 Airplane effectivities are listed in alpha-numeric order. A range of
airplanes is defined by the word "through", e.g. N501BC through
N505BC includes all N5xxBC series aircraft in order as listed on the
model ID page. A comma in the range, e.g. N501BC through
N503BC, N505BC indicates that N504BC is excluded from the
range.
2 Airplane effectivities apply only to the paragraph, illustration,
operational note, procedural step, etc. and to subordinate items (if
any).
Example (with subordinate items):
N501BC through N504BC
Right radio tuning panel............................................................... Set
Verify that the OFF light is extinguished.
First officer's audio control panel ................................................ Set
In this example, the effectivity N501BC through N504BC applies to
the first procedural step and further indented (subordinate) step only.
The effectivity does not include the next equivalently indented step.
The first step (Right radio tuning panel) is effective for airplanes
N501BC through N504BC, the second step (First officer's audio
control panel) is effective for all airplanes:
Example (without subordinate items):
N501BC through N502BC
Thrust reversers inoperative.
Autobrake system inoperative.
In this example, the effectivity N501BC through N502BC applies to
the first operational note only. The effectivity does not apply to the
next equivalently indented operational note.
The first operational note (Thrust reverser inoperative.) is effective
for airplanes N501BC through N502BC only, the next operational
note Autobrake...) is effective for all airplanes.
11.
Chapter 0 Preface
Section 2 Introduction
0.2.6 February 06, 2013
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Flight Crew Operations Manual
Volume 1
3 When airplane effectivities are stated immediately below a checklist
title, the entire checklist applies to the listed airplanes only. In the
following example, the OIL FILTER checklist is applicable to
N501BC through N503BC only:
4 When Boeing has been notified airplanes are to be modified by
service bulletin (SB), the effectivity statement will include 'Add' and
'Delete' versions, as appropriate, in parentheses. Depending upon the
modification, there may not be both an 'Add' and an 'Delete' version.
The text before the semicolon in the parentheses lists the range of
airplanes being modified. The text after the semicolon indicates the
'before' or 'after' version and briefly describes what the SB does. The
following examples illustrate this:
Example ('Add' version):
(SB Adds N504BC when Improved Oil Filters are installed) The
engine may be operated normally.
"SB Adds N504BC" means the incorporation of the SB (i.e.
installation of improved Oil Filters in this example) is scheduled to
begin for airplane N504BC. The words “SB Adds, when improved
Oil Filters are installed” indicate the associated operational note (The
engine may be operated normally.) applies to N504BC when the SB
has been incorporated.
Example ('Deletes' version):
(SB Deletes N504BC when improved Oil Filters are installed) The
engine must be operated at idle thrust.
For airplane N504BC the SB (i.e. installation of improved Oil Filters
in this example) has not been incorporated. The associated operational
note (The engine must be operated at idle thrust) applies N504BC.
"SB Deletes N504BC" means the incorporation of the SB (i.e.
installation of improved Oil Filters in this example) is scheduled to
begin for airplane N504BC. The words "The engine must be operated
at idle thrust" will apply to N504BC until the SB has been
incorporated.
OIL FILTER
N501BC through N503BC
12.
Preface Chapter 0
Abbreviations Section 3
February 06, 2013 0.3.1
757-200
Flight Crew Operations Manual
Volume 1
General
The following abbreviations may be found throughout the manual. Some
abbreviations may also appear in lowercase letters. Abbreviations having very
limited use are explained in the chapter where they are used.
A
ABV Above
AC Alternating Current
ACARS AircraftCommunications
Addressing and
Reporting System
ACP Audio Control Panel
ACT Active
ADC Air Data Computer
ADF Automatic Direction
Finder
ADI Attitude Director
Indicator
ADIRS Air Data Inertial
Reference System
ADIRU Air Data Inertial
Reference Unit
AFDS Autopilot Flight Director
System
AFM Airplane Flight Manual
(FAA approved)
A/G Air/Ground
AGL Above Ground Level
AIL Aileron
ALT Altitude
ALTN Alternate
AM Amplitude Modulation
AMI Airline Modifiable
Information
ANP Actual Navigational
Performance
ANT Antenna
AOA Angle of Attack
A/P Autopilot
APL Airplane
APP Approach
APU Auxiliary Power Unit
ARINC Aeronautical Radio,
Incorporated
ARPT Airport
ARR Arrival
ASA Autoland Status
Annunciator
ASYM Asymmetry
A/T Autothrottle
ATA Actual Time of Arrival
ATC Air Traffic Control
ATT Attitude
AUTO–
THROT
Autothrottle
AUTO Automatic
13.
Chapter 0 Preface
Section 3 Abbreviations
0.3.2 February 06, 2013
757-200
Flight Crew Operations Manual
Volume 1
AUX Auxiliary
AVAIL Available
B
BARO Barometric
BAT Battery
B/CRS Back Course
BFO Beat Frequency
Oscillator
BKR Breaker
BLD Bleed
BLW Below
BRG Bearing
BRT Bright
BTL Bottle
C
C Captain
Celsius
Center
Cool
CANC Cancel
CAP Capture
CAPT Captain
CB Circuit Breaker
CDSS Cockpit Door
Surveillance System
CDU Control Display Unit
CG Center of Gravity
CHR Chronograph
CKT Circuit
CL Close
CLB Climb
CLR Clear
CMD Command
CO Company
COMM Communication
COMP Comparator
COMPT Compartment
CON Continuous
CONFIG Configuration
CONT Control
COOL Cooling
CRS Course
CRT Cathode Ray Tube
CRZ Cruise
CTL Control
CTR Center
CWS Control Wheel Steering
D
DA(H) Decision Altitude
(Height)
DC Direct Current
DDG Dispatch Deviations
Guide
DEL Delete
DEP Departure
DEPR Depressurize
DES Descent
DH Decision Height
DIFF Differential
DISC Disconnect
DISCH Discharge
DK Deck
14.
Preface Chapter 0
Abbreviations Section 3
February 06, 2013 0.3.3
757-200
Flight Crew Operations Manual
Volume 1
DME Distance Measuring
Equipment
DN Down
DSPL Display
E
E/D End of Descent
E/E Electrical/Electronic
EEC Electronic Engine
Control
EFI Electronic Flight
Instruments
EFIS Electronic Flight
Instrument System
EGT Exhaust Gas
Temperature
EICAS Engine Indication and
Crew Alerting System
ELEC Electrical
ELEV Elevator
EMER Emergency
ENG Engine
ENT Entry
EO Engine Out
EPR Engine Pressure Ratio
EQPT or
EQUIP
Equipment
ETOPS Extended Range
Operation with Twin
Engine Airplanes
EVAC Evacuation
EXEC Execute
EXT Extend or External
F
F Fahrenheit
FADEC Full Authority Digital
Engine Control
FCC Flight Control Computer
FCOM Flight Crew Operations
Manual
FD, F/D or
FLT DIR
Flight Director
FF Fuel Flow
FILT Filter
FL CH or
FLCH
Flight Level Change
FLT Flight
FMA Flight Mode
Annunciations
FMC Flight Management
Computer
FMS Flight Management
System
F/O or F O First Officer
FPA Flight Path Angle
FPM Feet Per Minute
FPV Flight Path Vector
FREQ Frequency
F/S Fast/Slow
FT Feet
FWD Forward
FWSOV Fire Wall Shut Off Valve
G
GA Go–Around
GEN Generator
GMT Greenwich Mean Time
GND Ground
15.
Chapter 0 Preface
Section 3 Abbreviations
0.3.4 February 06, 2013
757-200
Flight Crew Operations Manual
Volume 1
GPS Global Positioning
System
GPWS Ground Proximity
Warning System
G/S Glideslope
GS Ground Speed
H
HDG Heading
HF High Frequency
HI High
HLD Hold
HPSOV High Pressure Shut Off
Valve
HSI Horizontal Situation
Indicator
HYD Hydraulic
I
IAS Indicated Airspeed
IDENT Identification
IGN Ignition
IGS Instrument Guidance
System
IND LTS Indicator Lights
INIT Initialization
INSTR Instrument
ILS Instrument Landing
System
INBD Inboard
IND Indicator
INOP Inoperative
INT or
INTPH
Interphone
INTC Intercept
IRS Inertial Reference
System
ISA International Standard
Atmosphere
ISLN Isolation
ISFD Integrated Standby Flight
Display
K
K or KTS Knots
KGS Kilograms
L
L Left
LBS Pounds
LD Load
LDA Localizer-type
Directional Aid
LDG Landing
LE Leading Edge
LIM Limit
LKD Locked
L NAV or
LNAV
Lateral Navigation
LOC Localizer
LT Light
M
M Mach
MAG Magnetic
MAN Manual
MAX Maximum
MCP Mode Control Panel
MDA(H) Minimum Descent
Altitude (Height)
16.
Preface Chapter 0
Abbreviations Section 3
February 06, 2013 0.3.5
757-200
Flight Crew Operations Manual
Volume 1
MEL Minimum Equipment
List
MFD Multifunction Display
MIC Microphone
MIN Minimum
MLS Microwave Landing
System
MMO Maximum Mach
Operating Speed
MOD Modify
MSG Message
MTRS Meters
N
N Normal
NAV Navigation
NGS Nitrogen Generating
System
NM Nautical Miles
NORM Normal
N1 Low Pressure Rotor
Speed
N2 High Pressure Rotor
Speed (Pratt & Whitney
engines)
Intermediate Pressure
Rotor Speed
(Rolls–Royce engines)
N3 High Pressure Rotor
Speed (Rolls–Royce
engines)
O
OAT Outside Air Temperature
OFST Offset
OP Open
OVHT Overheat
OVRD Override
OVSPD Overspeed
OXY or O2 Oxygen
P
PA Passenger Address
PASS Passenger
PCP Pilot Call Panel
PERF Performance
PES Pitch Enhancement
System
PF Pilot Flying
PM Pilot Monitoring
PNL Panel
POS Position
PPOS Present Position
PRES or
PRESS
Pressure
PREV Previous
P/RST Push To Reset
PROX Proximity
PRV Pressure Regulating
Valve
PSI Pounds Per Square Inch
PTH Path
PTT Push To Talk
PTU Power Transfer Unit
PWR Power
PWS Predictive Windshear
System
Q
17.
Chapter 0 Preface
Section 3 Abbreviations
0.3.6 February 06, 2013
757-200
Flight Crew Operations Manual
Volume 1
Q Quantity
QFE Local Station Pressure
QNH Local Station Pressure
corrected to MSL
QTY Quantity
R
R Right
RA Radio Altitude
Resolution Advisory
RAD Radio
RAT Ram Air Turbine
RDMI Radio Distance Magnetic
Indicator
REC Recorder
RECIR or
RECIRC
Recirculation
REF Reference
REV Reverse
RF Refill
RMI Radio Magnetic Indicator
RNP Required Navigational
Performance
RNV Area Navigation
(RNAV)
RPM Revolutions Per Minute
RST Reset
RSVR Reservoir
R/T Radio Transmit
RTE Route
RTO Rejected Takeoff
RUD Rudder
RVSM Reduced Vertical
Separation Minimum
S
SAT Static Air Temperature
SB Service Bulletin
S/C Step Climb
SEL Select
SDF Simplified Directional
Facility
SELCAL Selective Calling
SENS Sensitivity
SERV Service
SPD Speed
SPDBRK Speedbrake
STAB Stabilizer
STBY Standby
SYS System
T
T or TRU True
T or TK or
TRK
Track
TA Traffic Advisory
TAI Thermal Anti–Ice
TAT Total Air Temperature
T/C Top of Climb
TCAS Traffic Alert and
Collision Avoidance
System
T/D Top of Descent
TE Trailing Edge
TEMP Temperature
TERR Terrain
TFC Traffic
18.
Preface Chapter 0
Abbreviations Section 3
February 06, 2013 0.3.7
757-200
Flight Crew Operations Manual
Volume 1
TFR Transfer
THR Throttle
Thrust
TO or T/O Takeoff
TO/GA Takeoff/Go–Around
TURB Turbine
Turbulence
U
UNLKD Unlocked
UNSCHD
or
UNSCHED
Unscheduled
USB Upper Side Band
UTC Universal Time
Coordinated
UTIL Utility
V
VA Design maneuvering
Speed
VAL Valve
VERT Vertical
VHF Very High Frequency
VIB Vibration
VLV Valve
VMO Maximum Operating
Speed
V NAV or
VNAV
Vertical Navigation
VOR VHF Omnidirectional
Range
VR Rotation Speed
VREF Reference Speed
VSI Vertical Speed Indicator
V/S Vertical Speed
VTK Vertical Track
V1 Takeoff Decision Speed
V2 Takeoff Safety Speed
W
W Warm
WHL Wheel
WPT Waypoint
WXR Weather Radar
X
X–FEED Crossfeed
XPDR or
XPNDR
Transponder
XTK Cross Track
20.
AIR TRANSPORT INTERNATIONAL
RECORD OF REVISIONS
TYPE MANUAL: ATI 757 FCOM Vol. 1 thru 3
REVISION
NO.
DATE
INSERTED
INSERTED BY REVISION
NO.
DATE
INSERTED
INSERTED BY
Complete
thru Rev. 4
09/18/13 Publications
5 01/22/14 Publications
6 4/8/14 Publications
7
4/18/14 Publications
21.
Summary Of Bulletins
Page1
B757 FLIGHT CREW OPERATIONS MANUAL VOLUMES 1-3
SUMMARY OF BULLETINS
A revised Summary of Bulletins page will be reissued when a bulletin is incorporated into this manual or
is rescinded.
BULLETIN
NUMBER
BULLETIN
DATE
INSERTED
BY
VOL NO.
PG NO (s)
REV NO &
DATE
INCORPORATED
DATE
REMOVED
2014-01 03-19-14 TP
Vol. 2
20.2 pg 2
20.7 pg 21
2014-02 04-25-14 TP Vol. 1
NP.21.8
2014-03 05-02-14 TP Vol. 2
20.15 pg 37
22.
Summary Of Bulletins
Page 2
B757 FLIGHT CREW OPERATIONS MANUAL VOLUMES 1-3
BULLETIN
NUMBER
BULLETIN
DATE
INSERTED
BY
VOL NO.
PG NO (s)
REV NO &
DATE
INCORPORATED
DATE
REMOVED
23.
Bulletin 2014-01
Page1
B757 FLIGHT CREW OPERATIONS MANUAL VOLUMES 1-3
757 FCOM VOL 2 BULLETIN 2014-01 IS FAA APPROVED
DATE: _____________________ SUBMITTAL LEVEL: __B__
SIGNATURE: _______________________________________________________________________________
DARREL FORSBERG
PRINCIPAL OPERATIONS INSPECTOR, FAA-DFW CMO
B757 FCOM Bulletin 2014-01
The following pages have been updated in B757 FCOM Vol. 2 and will be incorporated into the next
revision.
20.2 CONFIGURATION COMPARISON MATRIX, pg 2
20.7 AIR SYSTEMS, pg. 21
25.
Bulletin 2014-02
Page1
B757 FLIGHT CREW OPERATIONS MANUAL VOLUMES 1-3
757 FCOM VOL. 1 BULLETIN 2014-02 IS FAA APPROVED
DATE: _____________________ SUBMITTAL LEVEL: __A__
SIGNATURE: _______________________________________________________________________________
DARREL FORSBERG
PRINCIPAL OPERATIONS INSPECTOR, FAA-DFW CMO
B757 FCOM Bulletin 2014-02
The following pages have been updated in B757 FCOM Vol. 1 and will be incorporated into the next
revision.
Normal Procedures - Amplified Procedures page NP.21.8
27.
Bulletin 2014-03
Page1
B757 FLIGHT CREW OPERATIONS MANUAL VOLUMES 1-3
757 FCOM VOL. 2 BULLETIN 2014-03 IS FAA APPROVED
DATE: _____________________ SUBMITTAL LEVEL: __A__
SIGNATURE: _______________________________________________________________________________
DARREL FORSBERG
PRINCIPAL OPERATIONS INSPECTOR, FAA-DFW CMO
B757 FCOM Bulletin 2014-03
The following pages have been updated in B757 FCOM Vol. 2 and will be incorporated into the next
revision.
Chapter 20 - 751CX Combi page 37/38
29.
Preface Chapter 0
List of Effective Pages Section 0
April 18, 2014 0.LEP.1
REV 7 SUB B TO THIS MANUAL IS FAA APPROVED
DATE: ______________________________________
SIGNATURE: ________________________________
NAME: DARREL FORSBERG ___________________
PRINCIPAL OPERATIONS INSPECTOR
DFW - CMO
757-200
Flight Crew Operations Manual
Volume 1
LOG OF REVISIONS:
0 02-06-13 7 04-18-14
1 04-30-13
2 05-06-13
3 06-05-13
4 08-08-13
5 11-01-13
6 04-01-14
PAGE DATE
VOLUME 1
PREFACE
0.TOC.1 FEB 06, 2013
0.TOC.2 FEB 06, 2013
0.1.1 April 18, 2014
0.1.2 MAY 6, 2013
0.2.1 FEB 06, 2013
0.2.2 FEB 06, 2013
0.2.3 FEB 06, 2013
0.2.4 FEB 06, 2013
0.2.5 FEB 06, 2013
0.2.6 FEB 06, 2013
0.3.1 FEB 06, 2013
0.3.2 FEB 06, 2013
0.3.3 FEB 06, 2013
0.3.4 FEB 06, 2013
0.3.5 FEB 06, 2013
0.3.6 FEB 06, 2013
0.3.7 FEB 06, 2013
0.3.8 FEB 06, 2013
0.LEP.1 APR 18, 2014
0.LEP.2 APR 18, 2014
0.LEP.3 APR 18, 2014
0.LEP.4 APR 18, 2014
0.LEP.5 APR 18, 2014
0.LEP.6 APR 18, 2014
0.LEP.7 APR 18, 2014
0.LEP.8 APR 18, 2014
0.LEP.9 APR 18, 2014
0.LEP.10 APR 18, 2014
0.LEP.11 APR 18, 2014
0.LEP.12 APR 18, 2014
0.LEP.13 APR 18, 2014
0.LEP.14 APR 18, 2014
0.LEP.15 APR 18, 2014
0.LEP.16 APR 18, 2014
0.LEP.17 APR 18, 2014
0.LEP.18 APR 18, 2014
0.LEP.19 APR 18, 2014
0.LEP.20 APR 18, 2014
0.LEP.21 APR 18, 2014
0.LEP.22 APR 18, 2014
0.LEP.23 APR 18, 2014
0.LEP.24 APR 18, 2014
0.LEP.25 APR 18, 2014
0.LEP.26 APR 18, 2014
0.LEP.26 APR 18, 2014
0.LEP.27 APR 18, 2014
0.LEP.28 APR 18, 2014
0.LEP.29 APR 18, 2014
0.LEP.30 APR 18, 2014
0.LEP.31 APR 18, 2014
0.LEP.32 APR 18, 2014
LIMITATIONS
L.TOC.1 APR 18, 2014
L.TOC.2 APR 30, 2013
L.10.1 NOV 01, 2013
L.10.2 NOV 01, 2013
L.10.3 APR 18, 2014
L.10.4 APR 18, 2014
L.10.5 APR 18, 2014
L.10.6 APR 18, 2014
L.10.7 APR 18, 2014
L.10.8 APR 30, 2013
PAGE DATE
30.
Chapter 0 Preface
Section 0 List of Effective Pages
0.LEP.2 April 18, 2014
REV 7, SUB B TO THIS MANUAL IS FAA APPROVED
DATE: ______________________________________
SIGNATURE: ________________________________
NAME: DARREL FORSBERG____________________
PRINCIPAL OPERATIONS INSPECTOR
DFW - CMO
757-200
Flight Crew Operations Manual
Volume 1
NORMAL PROCEDURES
NP.TOC.1 NOV 01, 2013
NP.TOC.2 APR 18, 2014
NP.11.1 FEB 06, 2013
NP.11.2 FEB 06, 2013
NP.11.3 FEB 06, 2013
NP.11.4 FEB 06, 2013
NP.11.5 FEB 06, 2013
NP.11.6 FEB 06, 2013
NP.11.7 FEB 06, 2013
NP.11.8 FEB 06, 2013
NP.21.1 FEB 06, 2013
NP.21.2 FEB 06, 2013
NP.21.3 APR 01, 2014
NP.21.4 APR 01, 2014
NP.21.5 NOV 01, 2013
NP.21.6 APR 30, 2013
NP.21.7 NOV 01, 2013
NP.21.8 NOV 01, 2013
NP.21.9 NOV 01, 2013
NP.21.10 NOV 01, 2013
NP.21.11 NOV 01, 2013
NP.21.12 NOV 01, 2013
NP.21.13 NOV 01, 2013
NP.21.14 NOV 01, 2013
NP.21.15 NOV 01, 2013
NP.21.16 NOV 01, 2013
NP.21.17 NOV 01, 2013
NP.21.18 NOV 01, 2013
NP.21.19 NOV 01, 2013
NP.21.20 NOV 01, 2013
NP.21.21 NOV 01, 2013
PAGE DATE
NP.21.22 NOV 01, 2013
NP.21.23 NOV 01, 2013
NP.21.24 NOV 01, 2013
NP.21.25 NOV 01, 2013
NP.21.26 NOV 01, 2013
NP.21.27 NOV 01, 2013
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NP.21.29 NOV 01, 2013
NP.21.30 NOV 01, 2013
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NP.21.34 NOV 01, 2013
NP.21.35 NOV 01, 2013
NP.21.36 NOV 01, 2013
NP.21.37 NOV 01, 2013
NP.21.38 NOV 01, 2013
NP.21.39 NOV 01, 2013
NP.21.40 NOV 01, 2013
NP.21.41 NOV 01, 2013
NP.21.42 NOV 01, 2013
NP.21.43 NOV 01, 2013
NP.21.44 NOV 01, 2013
NP.21.45 NOV 01, 2013
NP.21.46 NOV 01, 2013
NP.21.47 APR 18, 2014
NP.21.48 APR 18, 2014
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List of Effective Pages Section 0
April 18, 2014 0.LEP.3
REV 7 SUB B TO THIS MANUAL IS FAA APPROVED
DATE: ______________________________________
SIGNATURE: _________________________________
NAME: DARREL FORSBERG ____________________
PRINCIPAL OPERATIONS INSPECTOR
DFW - CMO
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Flight Crew Operations Manual
Volume 1
NP.21.54 APR 18, 2014
NP.21.55 APR 18, 2014
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SUPPLEMENTARY PROCEDURES
PAGE DATE
SP.TOC.1 FEB 06, 2013
SP.TOC.2 FEB 06, 2013
SP.TOC.3 FEB 06, 2013
SP.TOC.4 FEB 06, 2013
SP.TOC.5 FEB 06, 2013
SP.TOC.6 FEB 06, 2013
SP.05.1 FEB 06, 2013
SP.05.2 FEB 06, 2013
SP.1.1 FEB 06, 2013
SP.1.2 NOV 01, 2013
SP.1.3 FEB 06, 2013
SP.1.4 FEB 06, 2013
SP.2.1 FEB 06, 2013
SP.2.2 FEB 06, 2013
SP.3.1 FEB 06, 2013
SP.3.2 FEB 06, 2013
SP.4.1 FEB 06, 2013
SP.4.2 FEB 06, 2013
SP.4.3 FEB 06, 2013
SP.4.4 FEB 06, 2013
SP.4.5 FEB 06, 2013
SP.4.6 APR 18, 2014
SP.4.7 FEB 06, 2013
SP.4.8 FEB 06, 2013
SP.5.1 FEB 06, 2013
SP.5.2 FEB 06, 2013
SP.6.1 FEB 06, 2013
SP.6.2 FEB 06, 2013
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SP.6.4 MAY 6, 2013
SP.6.5 FEB 06, 2013
SP.6.6 FEB 06, 2013
PAGE DATE
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Section 0 List of Effective Pages
0.LEP.4 April 18, 2014
REV 7, SUB B TO THIS MANUAL IS FAA APPROVED
DATE: ______________________________________
SIGNATURE: ________________________________
NAME: DARREL FORSBERG____________________
PRINCIPAL OPERATIONS INSPECTOR
DFW - CMO
757-200
Flight Crew Operations Manual
Volume 1
SP.7.1 NOV 01, 2013
SP.7.2 FEB 06, 2013
SP.7.3 FEB 06, 2013
SP.7.4 FEB 06, 2013
SP.8.1 FEB 06, 2013
SP.8.2 FEB 06, 2013
SP.10.1 FEB 06, 2013
SP.10.2 FEB 06, 2013
SP.11.1 FEB 06, 2013
SP.11.2 APR 01, 2014
SP.11.3 APR 01, 2014
SP.11.4 FEB 06, 2013
SP.11.5 FEB 06, 2013
SP.11.6 FEB 06, 2013
SP.11.7 FEB 06, 2013
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SP.12.1 FEB 06, 2013
SP.12.2 FEB 06, 2013
SP.15.1 FEB 06, 2013
SP.15.2 FEB 06, 2013
SP.16.1 FEB 06, 2013
SP.16.2 NOV 01, 2013
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PERFORMANCE INFLIGHT
PI.TOC.10.1 FEB 06, 2013
PI.TOC.10.2 FEB 06, 2013
PI.TOC.10.3 FEB 06, 2013
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PI.10.1 FEB 06, 2013
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List of Effective Pages Section 0
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REV 7 SUB B TO THIS MANUAL IS FAA APPROVED
DATE: ______________________________________
SIGNATURE: _________________________________
NAME: DARREL FORSBERG ____________________
PRINCIPAL OPERATIONS INSPECTOR
DFW - CMO
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Flight Crew Operations Manual
Volume 1
PI.10.16 FEB 06, 2013
PI.10.17 FEB 06, 2013
PI.10.18 FEB 06, 2013
PI.11.1 FEB 06, 2013
PI.11.2 FEB 06, 2013
PI.11.3 FEB 06, 2013
PI.11.4 FEB 06, 2013
PI.11.5 FEB 06, 2013
PI.11.6 FEB 06, 2013
PI.12.1 FEB 06, 2013
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0.LEP.6 April 18, 2014
REV 7, SUB B TO THIS MANUAL IS FAA APPROVED
DATE: ______________________________________
SIGNATURE: ________________________________
NAME: DARREL FORSBERG____________________
PRINCIPAL OPERATIONS INSPECTOR
DFW - CMO
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Flight Crew Operations Manual
Volume 1
PI.17.2 FEB 06, 2013
PI.17.3 FEB 06, 2013
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REV 7 SUB B TO THIS MANUAL IS FAA APPROVED
DATE: ______________________________________
SIGNATURE: _________________________________
NAME: DARREL FORSBERG ____________________
PRINCIPAL OPERATIONS INSPECTOR
DFW - CMO
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Volume 1
PI.22.12 FEB 06, 2013
PI.23.1 FEB 06, 2013
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VOLUME 2
Master Table of Contents
i NOV 01, 2013
ii MAY 6, 2013
ATI 757 AC Configuration Matrix
1 NOV 1, 2013
2 NOV 1, 2013
Chapter 1
I FEB 06, 2013
II FEB 06, 2013
1 FEB 06, 2013
2 FEB 06, 2013
3 FEB 06, 2013
4 FEB 06, 2013
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PAGE DATE
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Section 0 List of Effective Pages
0.LEP.8 April 18, 2014
REV 7, SUB B TO THIS MANUAL IS FAA APPROVED
DATE: ______________________________________
SIGNATURE: ________________________________
NAME: DARREL FORSBERG____________________
PRINCIPAL OPERATIONS INSPECTOR
DFW - CMO
757-200
Flight Crew Operations Manual
Volume 1
10 FEB 06, 2013
11 FEB 06, 2013
12 FEB 06, 2013
13 FEB 06, 2013
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Chapter 2
I FEB 06, 2013
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Chapter 3
I FEB 06, 2013
II FEB 06, 2013
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List of Effective Pages Section 0
April 18, 2014 0.LEP.9
REV 7 SUB B TO THIS MANUAL IS FAA APPROVED
DATE: ______________________________________
SIGNATURE: _________________________________
NAME: DARREL FORSBERG ____________________
PRINCIPAL OPERATIONS INSPECTOR
DFW - CMO
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Flight Crew Operations Manual
Volume 1
1 FEB 06, 2013
2 FEB 06, 2013
3 FEB 06, 2013
4 FEB 06, 2013
5 FEB 06, 2013
6 FEB 06, 2013
7 FEB 06, 2013
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Chapter 4
I FEB 06, 2013
II FEB 06, 2013
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Chapter 5
I FEB 06, 2013
II FEB 06, 2013
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0.LEP.10 April 18, 2014
REV 7, SUB B TO THIS MANUAL IS FAA APPROVED
DATE: ______________________________________
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PRINCIPAL OPERATIONS INSPECTOR
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Flight Crew Operations Manual
Volume 1
7 FEB 06, 2013
8 FEB 06, 2013
9 FEB 06, 2013
10 FEB 06, 2013
11 FEB 06, 2013
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Chapter 6
I FEB 06, 2013
II FEB 06, 2013
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List of Effective Pages Section 0
April 18, 2014 0.LEP.11
REV 7 SUB B TO THIS MANUAL IS FAA APPROVED
DATE: ______________________________________
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NAME: DARREL FORSBERG ____________________
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Volume 1
32 FEB 06, 2013
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I FEB 06, 2013
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I FEB 06, 2013
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0.LEP.12 April 18, 2014
REV 7, SUB B TO THIS MANUAL IS FAA APPROVED
DATE: ______________________________________
SIGNATURE: ________________________________
NAME: DARREL FORSBERG____________________
PRINCIPAL OPERATIONS INSPECTOR
DFW - CMO
757-200
Flight Crew Operations Manual
Volume 1
24 FEB 06, 2013
Chapter 10
I FEB 06, 2013
II FEB 06, 2013
1 FEB 06, 2013
2 FEB 06, 2013
3 FEB 06, 2013
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Chapter 11
I FEB 06, 2013
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41.
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List of Effective Pages Section 0
April 18, 2014 0.LEP.13
REV 7 SUB B TO THIS MANUAL IS FAA APPROVED
DATE: ______________________________________
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NAME: DARREL FORSBERG ____________________
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II FEB 06, 2013
III FEB 06, 2013
IV FEB 06, 2013
1 FEB 06, 2013
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0.LEP.14 April 18, 2014
REV 7, SUB B TO THIS MANUAL IS FAA APPROVED
DATE: ______________________________________
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NAME: DARREL FORSBERG____________________
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60 FEB 06, 2013
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SIGNATURE: _________________________________
NAME: DARREL FORSBERG ____________________
PRINCIPAL OPERATIONS INSPECTOR
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Flight Crew Operations Manual
Volume 1
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DATE: ______________________________________
SIGNATURE: ________________________________
NAME: DARREL FORSBERG____________________
PRINCIPAL OPERATIONS INSPECTOR
DFW - CMO
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Flight Crew Operations Manual
Volume 1
8 FEB 06, 2013
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DATE: ______________________________________
SIGNATURE: _________________________________
NAME: DARREL FORSBERG ____________________
PRINCIPAL OPERATIONS INSPECTOR
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Flight Crew Operations Manual
Volume 1
26 FEB 06, 2013
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REV 7, SUB B TO THIS MANUAL IS FAA APPROVED
DATE: ______________________________________
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NAME: DARREL FORSBERG____________________
PRINCIPAL OPERATIONS INSPECTOR
DFW - CMO
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Flight Crew Operations Manual
Volume 1
I FEB 06, 2013
II FEB 06, 2013
1 FEB 06, 2013
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DATE: ______________________________________
SIGNATURE: _________________________________
NAME: DARREL FORSBERG ____________________
PRINCIPAL OPERATIONS INSPECTOR
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Volume 1
61 FEB 06, 2013
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REV 7, SUB B TO THIS MANUAL IS FAA APPROVED
DATE: ______________________________________
SIGNATURE: ________________________________
NAME: DARREL FORSBERG____________________
PRINCIPAL OPERATIONS INSPECTOR
DFW - CMO
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Flight Crew Operations Manual
Volume 1
125 FEB 06, 2013
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DATE: ______________________________________
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PRINCIPAL OPERATIONS INSPECTOR
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Flight Crew Operations Manual
Volume 1
14 MAY 6, 2013
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REV 7, SUB B TO THIS MANUAL IS FAA APPROVED
DATE: ______________________________________
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NAME: DARREL FORSBERG____________________
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Flight Crew Operations Manual
Volume 1
77 MAY 6, 2013
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Chapter 19
I AUG 08, 2013
II AUG 08, 2013
1 MAY 6, 2013
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DATE: ______________________________________
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PRINCIPAL OPERATIONS INSPECTOR
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Flight Crew Operations Manual
Volume 1
26 MAY 6, 2013
27 MAY 6, 2013
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0.LEP.24 April 18, 2014
REV 7, SUB B TO THIS MANUAL IS FAA APPROVED
DATE: ______________________________________
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NAME: DARREL FORSBERG____________________
PRINCIPAL OPERATIONS INSPECTOR
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Flight Crew Operations Manual
Volume 1
89 MAY 6, 2013
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DATE: ______________________________________
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DATE: ______________________________________
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Flight Crew Operations Manual
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Chapter 20
I NOV 01, 2013
II NOV 01, 2013
1 NOV 01, 2013
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DATE: ______________________________________
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Volume 1
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42 NOV 01, 2013
43 NOV 01, 2013
44 NOV 01, 2013
VOLUME 3
Table of Contents
TOC-i FEB 06, 2013
Preface
00.00.1 FEB 06, 2013
00.01.1 FEB 06, 2013
00.01.2 FEB 06, 2013
00.01.3 FEB 06, 2013
00.01.4 FEB 06, 2013
00.01.5 FEB 06, 2013
00.01.6 FEB 06, 2013
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Chapter 1
01.00.1 FEB 06, 2013
01.00.2 FEB 06, 2013
01.00.3 NOV 1, 2013
01.01.1 FEB 06, 2013
01.01.2 FEB 06, 2013
01.01.3 FEB 06, 2013
01.01.4 FEB 06, 2013
01.01.5 FEB 06, 2013
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Preface Chapter 0
List of Effective Pages Section 0
April 18, 2014 0.LEP.29
REV 7 SUB B TO THIS MANUAL IS FAA APPROVED
DATE: ______________________________________
SIGNATURE: _________________________________
NAME: DARREL FORSBERG ____________________
PRINCIPAL OPERATIONS INSPECTOR
DFW - CMO
757-200
Flight Crew Operations Manual
Volume 1
01.01.28 NOV 1, 2013
01.01.29 FEB 06, 2013
01.01.30 FEB 06, 2013
01.01.31 FEB 06, 2013
01.01.32 FEB 06, 2013
01.01.33 FEB 06, 2013
Chapter 2
02.00.1 FEB 06, 2013
02.01.1 FEB 06, 2013
02.01.2 FEB 06, 2013
02.01.3 FEB 06, 2013
02.01.4 FEB 06, 2013
02.01.5 FEB 06, 2013
02.01.6 FEB 06, 2013
02.01.7 FEB 06, 2013
02.01.8 FEB 06, 2013
02.01.9 FEB 06, 2013
02.01.10 FEB 06, 2013
02.01.11 FEB 06, 2013
02.01.12 FEB 06, 2013
02.01.13 FEB 06, 2013
02.01.14 FEB 06, 2013
02.01.15 FEB 06, 2013
Chapter 3
03.00.1 FEB 06, 2013
03.00.2 FEB 06, 2013
03.01.1 FEB 06, 2013
03.01.2 FEB 06, 2013
03.01.3 FEB 06, 2013
PAGE DATE
03.01.4 FEB 06, 2013
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Chapter 0 Preface
Section 0 List of Effective Pages
0.LEP.30 April 18, 2014
REV 7, SUB B TO THIS MANUAL IS FAA APPROVED
DATE: ______________________________________
SIGNATURE: ________________________________
NAME: DARREL FORSBERG____________________
PRINCIPAL OPERATIONS INSPECTOR
DFW - CMO
757-200
Flight Crew Operations Manual
Volume 1
Chapter 4
04.00.1 FEB 06, 2013
04.00.2 FEB 06, 2013
04.01.1 FEB 06, 2013
04.01.2 FEB 06, 2013
04.01.3 FEB 06, 2013
04.01.4 FEB 06, 2013
04.01.5 FEB 06, 2013
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04.01.25 FEB 06, 2013
Chapter 5
05.00.1 NOV 1, 2013
05.00.2 NOV 1, 2013
PAGE DATE
05.00.3 FEB 06, 2013
05.01.1 FEB 06, 2013
05.01.2 FEB 06, 2013
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April 18, 2014 0.LEP.31
REV 7 SUB B TO THIS MANUAL IS FAA APPROVED
DATE: ______________________________________
SIGNATURE: _________________________________
NAME: DARREL FORSBERG ____________________
PRINCIPAL OPERATIONS INSPECTOR
DFW - CMO
757-200
Flight Crew Operations Manual
Volume 1
05.01.31 NOV 1, 2013
05.01.32 FEB 06, 2013
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Chapter 6
06.00.1 FEB 06, 2013
06.00.2 FEB 06, 2013
06.01.1 FEB 06, 2013
06.01.2 FEB 06, 2013
06.01.3 FEB 06, 2013
06.01.4 FEB 06, 2013
06.01.5 FEB 06, 2013
06.01.6 FEB 06, 2013
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Chapter 0 Preface
Section 0 List of Effective Pages
0.LEP.32 April 18, 2014
REV 7, SUB B TO THIS MANUAL IS FAA APPROVED
DATE: ______________________________________
SIGNATURE: ________________________________
NAME: DARREL FORSBERG____________________
PRINCIPAL OPERATIONS INSPECTOR
DFW - CMO
757-200
Flight Crew Operations Manual
Volume 1
06.01.19 FEB 06, 2013
06.01.20 FEB 06, 2013
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Chapter 7
07.00.1 FEB 06, 2013
07.00.2 FEB 06, 2013
07.01.1 FEB 06, 2013
07.01.2 FEB 06, 2013
07.01.3 FEB 06, 2013
07.01.4 FEB 06, 2013
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Chapter 8
08.00.1 FEB 06, 2013
08.00.2 FEB 06, 2013
08.00.3 FEB 06, 2013
08.01.1 FEB 06, 2013
08.01.2 FEB 06, 2013
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63.
Limitations Chapter L
Operating Limitations Section 10
November 01, 2013 L.10.1
757-200
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Volume 1
General
This chapter contains AFM limitations and Boeing recommended non-AFM
operating limitations. Limitations that are obvious, shown on displays or
placards, or incorporated within an operating procedure are not contained in
this chapter.
This chapter contains:
• Airplane Flight Manual (AFM) operational information
• Non-AFM operational information.
Information is included if it is:
• operationally significant
• required by FAA Airworthiness Directive
• required by another regulatory requirement
Information is not included if it is:
• incorporated into FCOM normal, supplementary, or non-normal
procedures, with a few exceptions
• shown on a placard, display, or other marking
Operational information listed in this chapter that must be memorized
(memory items) are marked with a (#) symbol. They meet the following
criterion - flight crew access by reference can not assure timely compliance,
e.g., severe turbulence penetration speeds. They need only be memorized to
the extent that compliance is assured. Knowing the exact wording of the
limitation is not required.
Assuming that the remaining items are available to the flight crew by
reference, they do not need to be memorized.
Airplane General, Emergency Equipment, Doors, Windows
Operational Limitations
Non-AFM Operational Information
NOTE: The following items are not AFM limitations, but are provided for
flight crew information.
# Turbulent air penetration speed is: 290 KIAS/.78 Mach, whichever is lower.
Runway slope ± 2%
Maximum Operating Altitude 42,000 feet pressure altitude
Maximum Takeoff/Landing Altitude 8,400 feet pressure altitude
# Maximum Takeoff and Landing
Tailwind Component
15 knots (N751CX-N754CX
10 knots (N531UA-N620DL)
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The navigation and display system does not support operations at latitudes
greater than 87° North or South.
# Do not operate HF radios during refueling operations.
RVSM Altimeter Cross Check Limits
Standby altimeters do not meet altimeter accuracy requirements of RVSM.
The maximum allowable in-flight difference between Captain and First
Officer altitude displays for RVSM operations is 200 feet.
The maximum allowable on-the-ground differences between Captain and First
Officer altitude displays for RVSM operation are:
Weather Radar
# Do not operate the weather radar in a hangar or within 50 feet of any
personnel or fuel spill.
NOTE: The hangar and personnel restrictions do not apply to the weather
radar test mode.
Flight Deck Security Door
Verify that an operational check of the Flight Deck Access System has been
accomplished according to approved procedures once each flight day.
Door Mounted Escape Slides
Entry door evacuation slide systems must be armed and engagement of the girt
bar with door sill verified prior to taxi, takeoff, or landing whenever
passengers are carried.
Airplane Maximum Weight Limitations
Maximum Taxi Weight
N751CX-N754CX
251,000 Pounds
N605DL-N620DL
233,000 Pounds
N531UA-N557CM
241,000 Pounds
Field Elevation Max Difference
Between Captain & F/O
Max Difference Between
Captain or F/O & Field Elevation
SEA LEVEL 40 feet 75 feet
5,000 feet 45 feet 75 feet
10,000 feet 50 feet 75 feet
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Maximum Takeoff Weight
N751CX-N754CX
250,000 Pounds
N605DL-N620DL
232,000 Pounds
N531UA-N557CM
240,000 Pounds
Maximum Landing Weight
N531UA-N620DL, N751CX-N754CX
198,000 Pounds
Maximum Zero Fuel Weight
N531UA-N620DL, N752CX-N754CX
184,000 Pounds
N751CX
185,400 Pounds
NOTE: These weights may be further restricted by field length limits, climb
limits, tire speed limits, brake energy limits, obstacle clearance, or
enroute and landing requirements.
Air Systems
When the airplane is electrically powered for more than 20 minutes on the
ground, equipment cooling must be provided as shown below.
Auto Flight
# After takeoff, the autopilot must not be engaged below 200 feet AGL.
# Minimum Altitude for Use of Autopilot Enroute
(except approaches) ....................................................................... 1000 (AFE)
# Use of aileron trim with the autopilot engaged is prohibited.
# The autopilot must be disconnected at or above 50 feet AGL on all
approaches.
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NOTE: Landing. Notwithstanding the above 50 foot AGL limitations, the
autopilot minimum use altitudes do not apply to autopilot
operations when an approved automatic landing system mode is
being used for landing. Automatic landing systems must be
authorized in an operations specification issued ATI.
Maximum allowable wind speeds for weather minima CAT 1 or greater
autoland operations:
# Maximum allowable crosswind 15 knots when landing weather minima are
predicated on CAT 2 or 3 autoland operations.
Aircraft Communications Addressing and Reporting System
(ACARS)
ACARS is limited to the transmission and receipt of messages which will not
create an unsafe condition if the message is improperly received, such as the
following conditions:
• the message or parts of the message are delayed or not received,
• the message is delivered to the wrong recipient, or
• the message content may be frequently corrupted.
However, Pre-Departure, Digital Automatic Terminal Information Service,
Oceanic Clearances, Weight and Balance and Takeoff Data messages can be
transmitted and received over ACARS if they are verified per approved
operational procedures.
Flight Deck Door Surveillance System (CDSS) (N751CX)
The CDSS monitor must be turned off prior to taxi, takeoff, approach, and
landing. (Sterile cockpit)
Engine, APU
# Flight crew shall not blank engine vibration display during takeoff.
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Engine Fuel System
The maximum fuel temperature is 49° C (120° F) {JP4/Jet B: 29° C (84° F)}.
The maximum fuel temperature is 49° C (120° F).
The minimum fuel temperature is minus 45° C (minus 49° F) or 3° C (5° F)
above the freeze point, whichever is higher.
The center tank may contain up to 2000 pounds of fuel with less than full main
tanks provided center tank fuel weight plus actual zero fuel weight does not
exceed the maximum zero fuel weight, and center of gravity limits are
observed.
Reverse Thrust
# Reverse thrust is for ground use only.
# Backing the airplane with use of reverse thrust is prohibited.
Flight Controls
# The maximum altitude for flap extension is 20,000 ft.
# Avoid rapid and large alternating control inputs, especially in combination
with large changes in pitch, roll, or yaw (e.g. large side slip angles) as they
may result in structural failure at any speed, including below VA.
Lateral Fuel Imbalance
Maximum fuel imbalance for all operations is 1950 pounds.
Navigation
Do not operate under IFR or at night into airports north of 73° North or south
of 60° South latitude whose navigation aids are referenced to magnetic north.
Photo Luminescent Aisle Path Marking System
N752CX-N754CX
Photo Luminescent Floor Emergency Lighting must be charged in accordance
with approved procedures.
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Warning systems
Ground Proximity Warning System (GPWS) Look-Ahead Alerting
Do not use the terrain display for navigation.
The use of look-ahead terrain alerting and terrain display functions is
prohibited within 15 nm of takeoff, approach or landing at an airport or
runway not contained in the GPWS terrain database.
The use of look-ahead terrain alerting and terrain display functions is
prohibited during QFE operations.
757-200 Combi Limitations (STC ST01920LA)
N752CX-N754CX
Loading:
The airplane must be loaded in accordance with the instructions given in the
B757-200 WBM-SC-D043N520-LTU-1-Weight and Balance Control and
Loading Manual Supplement. Reference the B757/767 Flight Crew Weight
and Balance Manual.
9G Barrier Limitation
The maximum deck cargo load is 70,000 pounds/31,750 KG.
High Zero Fuel Weight Payload Distribution
When the Zero Fuel Weight exceeds 147,000 pounds/66,700 KG, position at
least a combined 8,000 pounds/3,630 KG forward of FS 1040. Select from
Positions A1-A7, B1-B7, M1-M7, AC1-AC4, BC1-BC6, and MC1-MC4 on
the Forward Lower Hold, in order to limit aft fuselage shell loads for gust
conditions.
Kind of Airplane Operations
Extended Operations
The type-design reliability and performance of this airplane-engine
combination has been evaluated under 14 CFR 25.1535 and found suitable for
180-minute extended operations (ETOPS) when the configuration,
maintenance, and procedures standard contained in Boeing Document
DOIIN002, “CMP for Extended Range (ER) Operation,” as supplemented by
Pemco CMP Supplement No. CMP. SC-D011N002, are complied with. The
actual maximum approved diversion time for this modified airplane may be
less based on its most limiting system time capability. This finding does not
constitute operational approval to conduct ETOPS.
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ETOPS Significant System Time Capabilities
The most limiting ETOPS significant system other than fire suppression
systems for Class C cargo or baggage compartments is 195 minutes.
Flight Crew and Passengers
Required Flight Crew - Pilot and Copilot
The total number of passengers, cabin crew and additional crew, shall not
exceed the maximum values listed below, and shall not exceed the number for
which seating accommodation approved for takeoff and landing is provided.
Children under two years of ago and carried in the arms of passengers may be
excluded from account for this purpose.
Flight Deck - 2 required flight crew and 2 ACM’s (4 Maximum)
Vestibule Area - This area is to be occupied by ACM’s only (3 Maximum)
Passenger Compartment - 42 passengers and 5 cabin/additional crew (47
Maximum)
Cargo Fire
The cabin pressurization system must be operable at takeoff whenever cargo is
carried in the main deck of the lower cargo compartments.
Access To Main Deck Cargo Compartment (MDCC)
Access to the Main Deck Cargo Compartment in flight is prohibited.
The Main Deck Cargo Compartment Smoke Barrier Doors must be closed
prior to takeoff and must remain closed in flight.
PA/Cabin Interphone and Auxiliary Interphone
Prior to the first flight of each day, conduct functional test of both PA/
Interphone and Aux Interphone systems to verify communication using each
available handset.
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73.
Normal Procedures Chapter NP
Introduction Section 11
February 06, 2013 NP.11.1
757-200
Flight Crew Operations Manual
Volume 1
General
This chapter gives:
• an introduction to the normal procedures philosophy and assumptions
• step by step normal procedures
Scan Flow and Areas of Responsibility
The scan flow and areas of responsibility diagrams shown are representative
and may not match the configuration(s) of your airplanes.
The scan flow diagram provides general guidance on the order each flight
crew member should follow when doing the preflight and postflight
procedures. Specific guidance on the items to be checked are detailed in the
amplified Normal Procedures. For example, preflight procedure details are in
the Preflight Procedure - Captain and Preflight Procedure - First Officer.
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Section 11 Introduction
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Normal Procedures Philosophy and Assumptions
Normal procedures verify for each phase of flight that:
• the airplane condition is satisfactory
• the flight deck configuration is correct
Normal procedures are done on each flight. Refer to the Supplementary
Procedures (SP) chapter for procedures that are done as needed, for example
the adverse weather procedures.
Normal procedures are used by a trained flight crew and assume:
• all systems operate normally
• the full use of all automated features (LNAV, VNAV, autoland,
autopilot, and autothrottle)
Normal procedures also assume coordination with the ground crew before:
• hydraulic system pressurization, or
• flight control surface movement, or
• airplane movement
Normal procedures do not include steps for flight deck lighting and crew
comfort items.
Normal procedures are done by memory and scan flow. The panel illustration
in this section shows the scan flow. The scan flow sequence may be changed as
needed.
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Configuration Check
It is the crew member's responsibility to verify correct system response.
Before engine start, use lights or indications to verify each system's condition
or configuration.
If there is an incorrect configuration or response:
• verify that the system controls are set correctly
• check the respective circuit breaker as needed. Maintenance must first
determine that it is safe to reset a tripped circuit breaker on the ground
• test the respective system light as needed
Before engine start, review the EICAS alert messages and status display. If
there are unexpected messages:
• check the Minimum Equipment List (MEL/CDL) to decide if the
condition has a dispatch effect
If, during or after engine start, there is an alert message:
• do the respective non-normal checklist (NNC)
• on the ground, check the MEL
After engine start, EICAS alert messages are the primary means of alerting the
flight crew to non-normal conditions or incorrect configurations.
After engine start, there is no need to check status messages. Any message that
has an adverse affect on safe continuation of the flight appears as an EICAS
alert message.
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Crew Duties
Preflight and postflight crew duties are divided between the captain and first
officer. Phase of flight duties are divided between the Pilot Flying (PF) and the
Pilot Monitoring (PM).
Each crewmember is responsible for moving the controls and switches in their
area of responsibility:
• The phase of flight areas of responsibility for both normal and non-
normal procedures are shown in the Area of Responsibility
illustrations in this section. Typical panel locations are shown.
• The preflight and postflight areas of responsibility are defined by the
"Preflight Procedure - Captain" and "Preflight Procedure - First
Officer".
The captain may direct actions outside of the crewmember's area of
responsibility.
The general PF phase of flight responsibilities are:
• taxiing
• flight path and airspeed control
• airplane configuration
• navigation
The general PM phase of flight responsibilities are:
• checklist reading
• communications
• tasks asked for by the PF
• monitoring taxiing, flight path, airspeed, airplane configuration, and
navigation
PF and PM duties may change during a flight. For example, the captain could
be the PF during taxi but be the PM during takeoff through landing.
Normal procedures show who does a step by crew position (C, F/O, PF, or
PM):
• in the procedure title, or
• in the far right column, or
• in the column heading of a table
The mode control panel is the PF's responsibility. When flying manually, the
PF directs the PM to make the changes on the mode control panel.
The captain is the final authority for all tasks directed and done.
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Control Display Unit (CDU) Procedures
Before taxi, the captain or first officer may make CDU entries. The other pilot
must verify the entries.
Make CDU entries before taxi or when stopped, when possible. If CDU entries
must be made during taxi, the PM makes the entries. The PF must verify the
entries before they are executed.
In flight, the PM usually makes the CDU entries. The PF may also make
simple, CDU entries when the workload allows. The pilot making the entries
executes the change only after the other pilot verifies the entries.
During high workload times, for example departure or arrival, try to reduce the
need for CDU entries. Do this by using the MCP heading, altitude, and speed
control modes. The MCP can be easier to use than entering complex route
modifications into the CDU.
Autopilot Flight Director System (AFDS) Procedures
The crew must always monitor:
• airplane course
• vertical path
• speed
When selecting a value on the MCP, verify that the respective value changes
on the flight instruments, as applicable.
The crew must verify manually selected or automatic AFDS changes. Use the
FMA to verify mode changes for the:
• autopilot
• flight director
• autothrottle
During LNAV and VNAV operations, verify all changes to the airplane's:
• course
• vertical path
• thrust
• speed
Announcing changes on the FMA and thrust mode display when they occur is
a good CRM practice.
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Preflight and Postflight Scan Flow
FIRST OFFICER ITEMS
CAPTAIN ITEMS
TYPICAL PANEL
LOCATIONS ARE
1
2
3
1 2 3 4 5
6
8
7
SHOWN
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Introduction Section 11
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Areas of Responsibility - Captain as Pilot Flying or Taxiing
FIRST OFFICER ITEMS
JOINT RESPONSIBILITY
ITEMS
AUDIO CONTROL PANEL
TRIM
CAPTAIN ITEMS
NOTE: TYPICAL PANEL
LOCATIONS ARE
SHOWN.
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Areas of Responsibility - First Officer as Pilot Flying or Taxiing
FIRST OFFICER ITEMS
JOINT RESPONSIBILITY
ITEMS
AUDIO CONTROL PANEL
TRIM
CAPTAIN ITEMS
NOTE: TYPICAL PANEL
LOCATIONS ARE
SHOWN.
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Amplified Procedures Section 21
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Preliminary Preflight Procedure - Captain or First Officer
The Preliminary Preflight Procedure assumes that the Electrical Power Up
supplementary procedure is complete.
IRS mode selectors..............................................................OFF, then NAV
Verify that the ON DC lights illuminate then extinguish.
Verify that the ALIGN lights are illuminated.
STATUS display ................................................................................ Check
Verify that only expected messages are shown.
Verify that the following are sufficient for flight:
• oxygen pressure
• hydraulic quantity
• engine oil quantity
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Do the remaining actions after a crew change or maintenance action.
Maintenance documents.....................................................................Check
FLIGHT DECK ACCESS SYSTEM switch ..........................Guard closed
POWER TRANSFER UNIT switch .......................................Guard closed
FLIGHT RECORDER switch..........................................................NORM
SERVICE INTERPHONE switch........................................................ OFF
Circuit breakers ..................................................................................Check
Emergency equipment........................................................................Check
Fire extinguisher - Checked and stowed
Crash axe - Stowed
Escape ropes - Stowed
Other needed equipment - Checked and stowed
Parking brake...............................................................................As needed
Set the parking brake if brake wear indicators will be checked during
the exterior inspection.
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CDU Preflight Procedure - Captain and First Officer
Start the CDU Preflight Procedure anytime after the Preliminary Preflight
Procedure. The Initial Data and Navigation Data entries must be complete
before the flight instrument check during the Preflight Procedure. The
Performance Data entries must be complete before the Before Start Checklist.
The captain or first officer may make CDU entries. The other pilot must verify
the entries.
Enter data in all the boxed items on the following CDU pages.
Enter data in the dashed items or modify small font items that are listed in this
procedure. Enter or modify other items at pilot's discretion.
Failure to enter enroute winds can result in flight plan time and fuel burn
errors.
Initial Data...............................................................................................Set
IDENT page:
Verify that the MODEL is correct.
Verify that the navigation data base ACTIVE date range is
current.
POS INIT page:
Verify that the time is correct.
Enter the present position on the SET IRS POS line using the
following order of preference:
1. GPS position (if installed)
2. Four letter ICAO identifier
3. Enter gate position LAT/LONG (if available)
4. Enter Airport Reference Point (ARP) LAT/LONG
Navigation Data.......................................................................................Set
RTE page:
Enter the route.
Enter the FLIGHT NUMBER.
Activate and execute the route.
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DEPARTURES page:
Select the runway and departure routing.
Execute the runway and departure routing.
POS REF page:
Verify or enter the correct RNP for the departure.
Verify that the route is correct on the RTE pages. Check the LEGS
pages as needed to ensure compliance with the flight plan.
Performance Data....................................................................................Set
PERF INIT page:
CAUTION: Do not enter the ZFW into the GR WT boxes.
The FMC will calculate performance data with
significant errors.
Enter the ZFW.
Verify that the FUEL on the CDU, the dispatch papers, and the
fuel quantity indicator agree.
Verify that the fuel is sufficient for flight.
Verify that the GR WT on the CDU and the dispatch papers agree.
TAKEOFF REF page:
Enter the CG.
Enter the takeoff V speeds.