B777 Study Guide (Emirates)

B-777 STUDY GUIDE

The pages following are designed to be a study guide. This information is not updated, any

differences between this guide and the Company Manuals are unintentional, the Company Manuals

are controlling.

Selected personal techniques have been added in green highlighted text and are additional to

company SOP and are not intended to change existing SOP.

If errors are found, corrections are required, or you have additional information to

add to the guide please forward your comments to [email protected]

STUDY

GUIDE

TABLE OF CONTENTS

1. QRH NON-NORMAL MEMORY ITEMS ... 7

UNANNUNCIATED CHECKLISTS ... 7

AIRSPEED UNRELIABLE ... 8

ABORTED ENGINE START L,R ... 9

ENGINE AUTOSTART L,R ... 9

ENG LIM/SURGE/STALL L,R ... 10

ENG SVR DAMAGE/SEP L,R ... 11

FIRE ENG L,R ... 12

DUAL ENG FAIL/STALL (RR) ... 13

DUAL ENG FAIL/STALL (GE) ... 14

STABILIZER ... 15

CABIN ALTITUDE ... 15

2. FCOM SUPPLEMENTARY PROCEDURES ... 17

3. QRH NON-NORMAL MANEUVERS ... 25

APPROACH TO STALL RECOVERY ... 25

REJECTED TAKEOFF ... 25

TRAFFIC AVOIDANCE ... 27

UPSET RECOVERY ... 28

FOM EMERGENCY PROCEDURES ... 29

FCOM STANDARD ENGINE OUT PROCEDURE ... 29

4. QRH & FCTM FLIGHT PATTERNS ... 31

180° CIRCULAR TURNAROUND ... 31

180° HAMMERHEAD INTO TURNAROUND ... 32

180° HAMMERHEAD FROM TURNAROUND ... 33

TAKEOFF - VNAV ... 34

TAKEOFF ... 35

TAKEOFF – BASIC MODES ... 36

ILS APPROACH ... 37

INSTRUMENT APPROACH USING VNAV ... 38

INSTRUMENT APPROACH USING V/S OR FPA ... 39

VISUAL TRAFFIC PATTERN ... 40

CIRCLING APPROACH ... 41

GO-AROUND AND MISSED APPROACH ... 43

5. FCOM LIMITATIONS ... 45

AIRPLANE GENERAL ... 45

TAKE OFF CROSSWINDS ... 46

LANDING CROSSWINDS ... 47

WEIGHTS ... 48

DOORS ... 49

AIR SYSTEMS ... 49

AUTO FLIGHT ... 49

AUTOMATIC LANDING ... 49

RADIOS ... 50

ENGINES... 50

AIRPLANE STRUCTURE ... 51

FLIGHT INSTRUMENTS, DISPLAYS ... 51

FLIGHT MANAGEMENT, NAVIGATION ... 51

FUEL SYSTEM ... 52

GEAR DOWN DISPATCH ... 52

TABLE OF CONTENTS

STUDY GUIDE

6. LIMITATIONS AND POLICIES ... 53

PREFLIGHT ... 53

LIDO ROUTE MANUAL ... 57

TAXI ... 66

REJECTED TAKEOFF ... 66

TAKEOFF ... 67

CLIMB ... 69

CRUISE ... 70

DESCENT ... 72

HOLDING ... 72

APPROACH ... 73

MISSED APPROACH ... 76

LANDING ... 76

POST FLIGHT ... 79

BOEING FCOM BULLETINS... 80

EMIRATES FCOM BULLETINS ... 82

7. FUEL POLICY ... 85

8. PERFORMANCE ... 87

9. SOP GUIDE ... 89

PREFLIGHT CHECKS ... 89

WALK AROUND COMPONENT LOCATOR GUIDE ... 90

BRIEFINGS... 97

BEFORE START PROCEDURE ... 98

START PROCEDURE ... 98

BEFORE TAXI PROCEDURE ... 98

BEFORE TAKEOFF PROCEDURE ... 98

TAKEOFF PROCEDURE ... 99

CLIMB/CRUISE PROCEDURE ... 99

TOP OF CLIMB PROCEDURE ... 99

DESCENT PREPARATION ... 99

APPROACH PROCEDURE ... 100

ILS PROCEDURE ... 100

INSTRUMENT APPROACH USING VNAV ... 100

GO-AROUND PROCEDURE ... 101

AFTER LANDING PROCEDURE ... 101

TURNING ONTO THE PARKING STAND PROCEDURE ... 101

SHUTDOWN PROCEDURE ... 101

SECURE PROCEDURE ... 102

DEPARTURE SOP ... 104

ARRIVAL SOP ... 105

EMIRATES MANAGEMENT MODEL ... 106

MEL & CDL GUIDELINES ... 107

RTO ACTIONS ... 108

ENGINE MALFUNCTION AFTER V1 ... 109

EICAS MESSAGE PROCEDURE ... 110

ENGINE FAILURE AT CRUISE ALTITUDE ... 110

ENGINE FAILURE AT CRUISE ALTITUDE MANUAL PROCEDURE ... 110

ENGINE HANDLING AFTER AN AIRSTART ... 111

ENGINE OUT PROCEDURE ... 111

LANDING PROCEDURE – G/S INTERCEPT FROM ABOVE ... 111

PRESSURIZATION PROBLEMS ... 112

ILS PRM APPROACHES ... 113

LOW VISIBILITY OPERATIONS ... 114

CONTAMINATED RUNWAYS ... 118

COLD WEATHER OPERATIONS ... 120

DE-ICE PROCEDURES ON THE GATE ... 122

DE-ICE PROCEDURES ON A REMOTE DE-ICING BAY ... 123

HOT WEATHER OPERATIONS ... 124

SEVER TURBULENCE OPERSTIONS ... 124

THUNDERSTORM AVOIDANCE ... 124

WINDSHEAR ... 126

EGPWS ... 128

QFE OPERATIONS ... 129

DIVERSION PROCEDURE ... 130

DIVERSION CONSIDERATIONS ... 131

INHIBITS DURING TAKEOFF... 132

INHIBITS DURING LANDING ... 133

ETOPS FUEL REQUIREMENTS ... 134

ETOPS ALTERNATE WEATHER REQUIRMENTS ... 135

MNPS PROCEDURES ... 136

NAT CROSSING PROCEDURES ... 137

10. LESSONS LEARNED ... 139

11. REPORTS AND FORMS ... 145

MOR REPORT ... 145

AIR SAFETY REPORT ... 145

CAPTAIN’S SPECIAL REPORT ... 146

PASSENGER / AIRCREW ACCIDENT REPORT ... 147

CONFIDENTIAL HUMAN FACTORS REPORT ... 147

GROUP SAFETY REPORT ... 147

MISSING PASSENGERS REPORT ... 148

CAPTAINS DISCRETION REPORT ... 148

C15 ... 148

FMS NAVIGATION REPORT ... 148

FMS NAVIGATION DATA REPORT ... 148

GEN DEC ... 148

OM-C RAIG FEEDBACK FORM ... 148

E6 LOCKER STOWAGE WAYBILL FORM ... 148

PED INTERFERENCE ... 149

VOYAGE REPORT REQUIREMENTS ... 149

12. PA ANNOUNCEMENTS ... 151

HOLDING PA ... 151

GO-AROUND PA ... 151

WEATHER DIVERSION PA ... 151

TECHNICAL DIVERSION PA... 151

SICK PASSENGER DIVERSION PA ... 151

FIRE PA ... 152

EMERGENCY DESCENT PA ... 152

DEICING PA ... 152

PARTIAL OR ALL GEAR UP LANDING PA ... 152

PRECAUTIONARY DISEMBARKATION ... 153

SABOTAGE / BOMB THREATS ON GROUND ... 154

SABOTAGE / BOMB THREATS IN FLIGHT ... 155

SUSPICIOUS ARTICLE DISCOVERED ... 155

WORLD TIME ZONE MAP ... 156

DAYLIGHT SAVINGS TIME ... 157

CABIN CREW BRIEFING ... 158

WELCOME ABOARD PA ... 158

TABLE OF CONTENTS

STUDY GUIDE

QRH NON-NORMAL MEMORY ITEMS

It is a requirement to know all of the checklists in the Unannunciated Chapter of the QRH; however, only a few of them

have RECALL items.

UNANNUNCIATED CHECKLISTS

Checklist

Conditional Statement

Remarks

ABORTED ENGINE START L,R

During Ground Start, an abort engine start condition occurs.

Do an ABORTED ENGINE START checklist if there is no oil pressure rise after EGT increases.

FCOM 21.32 Can also be completed for FOD. (If FOD consider not reengaging starter)

AIRSPEED UNRELIABLE

Airspeed or Mach indication suspected to be unreliable.

AUTOMATIC UNLOCK

Flight deck door auto unlock light illuminated indicates correct emergency access code has been entered and flight deck door is programmed to automatically unlock after a time delay.

BOMB ON BOARD

Specific threat that a bomb is on board, or suspected or confirmed bomb on board.

DITCHING

Airplane ditching and evacuation are required.

DUAL ENGINE FAIL/STALL

Engine speed for both engines is below idle.

ENGINE IN-FLIGHT START L,R

Engine start is needed after a shutdown with no fire or apparent damage.

ENGINE LIMIT/SURGE/STALL L,R

Engine indications are abnormal or are approaching or exceeding limits, abnormal engine noises are heard, or there is no response to thrust lever movement.

ENGINE SVR DAMAGE/SEP L,R

Engine has severe damage, vibration, or has separated.

FIRE ENGINE TAILPIPE L,R

An engine tailpipe fire is reported on the ground with no engine fire warning. _{Remember it is a FOM requirement to call the Fire Department for assistance ASAP FOM 20.3.2}

FUEL JETTISON

Fuel jettison is required.

- This Unannunciated Checklist is to be used when Fuel Jettison is required. There are other Checklists triggered by EICAS messages.

- The EICAS message should be left displayed until the Fuel Jettison has been completed. The Checklist may be covered on the Lower EICAS display as it will be the displayed again when the checklist is displayed. TM B777 Part 1 Chapter 4 page 10

FUEL LEAK

An in flight fuel leak is suspected or confirmed.

GEAR LEVER LOCKED DOWN

Landing gear lever cannot be positioned to UP.

LOCK FAIL

Flight deck door lock fail light illuminated indicates flight deck door lock has failed, or flight deck access system switch is OFF.

OVERWEIGHT LANDING

A landing at greater than maximum landing weight is required.

SMOKE/FUMES AIR COND

A concentration of air conditioning smoke/fumes are identified.

SMOKE/FUMES/FIRE ELEC

Electrical smoke/fumes/fire is identified.

SMOKE/FUMES REMOVAL

Smoke/fumes removal is required.

TAT PROBE ICING

Airplane TAT probe or engine TAT probe icing is suspected.

VOLCANIC ASH

Static discharge around the windshield, bright glow in the engine inlets, smoke or dust on the flight deck, or acrid odor indicates the airplane is in volcanic ash.

For Expanded Procedures see

FCTM 7.6, or Study Guide Chap. 9

SOP, Pressurization Problems

1. QRH NON-NORMAL MEMORY ITEMS

STUDY GUIDE

Page 20 of 158

EXPANDED SUPPLEMENTARY PROCEDURES STUDY

GUIDE

1. AIRPLANE GENERAL, EM EQUIP, DOORS, WINDOWS

HOT WEATHER OPERATION

COLD WEATHER OPERATION

SECURING FOR COLD WEATHER

AIRFRAME DE-ICING

OPERATION WITH DE-ICING / ANTI ICING FLUIDS

SEVERE TURBULENCE

• Turbulence Penetration Speed: 270 below 25000 ft. 280/0.82M at or above 25000ft –

whichever the less

• Seat Belt Sign - ON

• No Smoking Sign - ON

• PA: “CABIN CREW BE SEATED”

• Advise Flight Attendants to secure Pax and Galleys, suspend service and sit down and fasten

seat belts

• Use

Autopilot

• Use V/S Mode during Climbs and Descents. VNAV/ALT may be used during cruise

• Fly at Turbulence Penetration Speed

• Select Manual Thrust. Thrust to be set slightly above Magenta EPR Target

• Delay flap extension or divert

• Secure Flight Deck of loose items

• Fasten Shoulder Harnesses

• Consider Altitude and Buffet Margins

• Purser to advise when cabin is secure

WINDSHEAR

DOORS

EMERGENCY EQUIPMENT

REFUELING

2. AIR SYSTEMS

GROUND AIR CONDITIONING CART USE

PACKS OFF TAKEOFF

3. ANTI-ICE, RAIN

ANTI-ICE USE

ENGINE ANTI ICE USE

WING ANTI-ICE USE

4. AUTOMATIC FLIGHT

6. ELECTRICAL

ELECTRICAL POWER DOWN

NOTES

• This is the procedure to be followed if completing the SECURE CHECKLIST.

• Refer

to FCOM SP.6.1 for this eventuality

ELECTRICAL SAFETY CHECK PROCEDURE

NOTES

• This procedure must be performed by reference to FCOM SP.6.2 in the event one has to

power up an unpowered aircraft. This must not be performed by recall

7. ENGINES, APU

APU GROUND PNEUMATIC START

CONDITION:

• The APU requires to be started using Ground pneumatics to provide duct pressure so that the

APU air turbine starter can be used to start the APU

REASON:

• The electric start motor is unavailable. This may be due to starter motor or circuit problems

CHECKLIST:

• FCOM SP 7.1

• The Packs must be off before the manifold is pressurised. This is to ensure that the min duct

pressure of 15 PSI is achieved

• After a normal APU start the ground pneumatics are disconnected before the Packs are put to

Auto

NOTES:

ENGINE BATTERY START

CONDITION:

• No Ground Power Unit or APU is available to provide the electrical power to start the engines.

Pneumatics from the APU or Ground cart is required to provide duct pressure.

REASON:

• APU is inop or APU GEN inop and no GPU is available

CHECKLIST:

• SP

7.1

NOTES:

• If using a ground cart, the FCOM SP ENGINE GROUND PNEUMATIC START and then the

ENGINE CROSSBLEED START procedures may need to be performed in the course of this

checklist

• Accomplish the drill by reference to the Supplementary Procedures. If Autostart is available, it

should be used. (Autostart is a normal engine start, which is to be accomplished in these

procedures).

• Read SP procedure. Careful planning is required

• Find out if there is any slot time and plan accordingly

• Ensure that extra fuel is on board for the increased ground run time (25 Kg per min) 500 Kg

min

• Ensure that the flight deck is set-up as far as possible including completing paperwork,

loadsheet, RTOW figures etc. to minimise delays after start

• Loading should be complete and all passengers on board, doors closed

• Ensure Ground Crew are ready, Pneumatic Air (if required) is available and Aircraft is clear

• Get permission to start one engine in the bay and advise that it will run for a while until ready

• Do SP procedure asking for air when applicable

• Perform Ground Pneumatic Start if required

• Start Left Engine in bay

• Complete SP and restore pack operation for air conditioning

• Complete cockpit set-up

• Get start and pushback clearance

• Pushback, set brake and start second engine (if no APU then this will require an ENGINE

CROSSBLEED START)

• If there are additional problems like Autostart inop. De-icing required or ENG START VALVE,

this could become quite complicated. Plan carefully and Take each stage slowly

Page 22 of 158

EXPANDED SUPPLEMENTARY PROCEDURES STUDY

GUIDE

ENGINE CROSSBLEED START

CONDITION:

• Air from an engine is used to start the other engine when APU air is not available

REASON:

• APU is inop or APU Bleed Air is not available

CHECKLIST:

• With the APU Bleed Valve OFF, and the aircraft clear, thrust is increased 5% on the operating

engine to provide a minimum 25 psi duct pressure from which the second engine is started (If

the duct pressure is above 25psi at idle thrust then a thrust increase to 5% N3 above idle is

not necessary)

NOTES:

• In this case a Ground Pneumatic Source starts the first engine on the stand. The second

engine could also be started but in some cases this may prove too much for the Tow Truck or

the Tow Bar Pin

• This case must be used if a 777 Tow Bar is not available

ENGINE GROUND PNEUMATIC START

CONDITION:

• Ground pneumatics are used to start the engines

REASON:

• APU is inop or APU Bleed Air is not available

CHECKLIST:

• Select

both packs to OFF. (The OFF lights will be illuminated, but packs must be selected off).

• A min duct pressure of 25 psi (less 1 psi/1000 ft Press Alt)

• Engine(s) are started normally

• Ground Pneumatics must be disconnected then Packs are selected to Auto

NOTES:

• If APU is inop then an ENGINE START WITH EXTERNAL ELECTRIC POWER must also be

performed. See FCOM SP.7.3

• Ensure Ground Crew are ready and Tow Truck and Pneumatic Air are available and Aircraft is

clear

• Get permission to start one engine in the bay

• Read FCOM SP.7.2 procedure

• Before connecting the ground air conditioning cart, switch the packs and recirculation fans off.

• Do SP procedure asking for air when applicable

• Start one engine at a time

• Start in bay

• Disconnect Ground Pneumatics and reinstate Packs

• Get clearance to push and start 2

nd

_engine

• The second engine may have to be started using an Engine Crossbleed Start

• Advise the Purser to reinstate the power to the cabin if required (See ENGINE START WITH

EXTERNAL ELECTRIC POWER)

ENGINE START WITH EXTERNAL ELECTRIC POWER

This Procedure has been removed from the removed from FCOM SP but I left this note in as helpful information.

CONDITION:

• An Engine start is required while using a Ground Power Unit as the only AC power source.

REASON:

• APU is inoperative or APU GEN inoperative.

CHECKLIST:

•

NOTES:

• If APU is inop, this will also require an ENGINE GROUND PNEUMATIC START and possibly

an ENGINE CROSSBLEED START

• This will require a start on the stand. Either 1 or Both Engines

• Get permission to start in the bay

• If a 777 tow bar and pin is available, and tow truck is capable, start both on the stand

• Refer

to FCOM SP.7.3 ENGINE GROUND PNEUMATIC START if required

• Disconnect GPU and Ground Pneumatics

• Get Pushback clearance

• Set Brake and start 2

nd

_{Engine if required using ENGINE CROSSBLEED START}

FCOM SP.7.2

• Advise purser to reinstate the power to the cabin if required

MANUAL ENGINE START

CONDITION:

• An engine start is required without the use of the Autostart System (Engine start using the

autostart system is the normal method to start the engine)

REASON:

• The Autostart is inoperative or selected off.

CHECKLIST:

• SP.7.4 or Laminated checklist under glareshield

NOTES:

• Read the checklist through together first as a crew, and then perform the checklist as an

action list.

• Start one engine at a time.

• Don't forget that you only put the fuel control switch to run when fOil pressure increases gEGT

below 100ºC and hN3 at max motoring or 25%.

• Unlike during an autostart the spar and engine fuel valves open as soon as the fuel control

switches are placed to Run. If the autostart switch is selected off and the fuel control switch is

placed in Run before max motoring you'll get an ENG AUTOSTART L/R caution. This should

prompt you to carry out the recall items, which is to abort the engine start. Clever!

• The procedure lists the start parameters to be monitored in a sequential order. CM2 to keep

CM1 in the picture as each stage of the engine start approaches. E.g. Once fuel control

switches are to Run, CM2 can say something like "We're looking for EGT within 30secs, we

have EGT rise it must remain within limits, now we need N1 rotation by 45%N3".

• In the event of a start problem / need to abort the start, do the recall items and call for the

aborted engine start checklist. Advise ground crew and decide next course of action i.e.

restart or not. Contact EK engineering if necessary.

Page 24 of 158

EXPANDED SUPPLEMENTARY PROCEDURES STUDY

GUIDE

MANUAL OVERRIDE ENGINE START

CONDITION:

• The engine start valve must be manually opened and closed with a tool

REASON:

• The engine starter valve has failed.

CHECKLIST:

• FCOM SP.7.4

NOTES:

• This procedure is used after the ENG START VALVE L/R has appeared or the aircraft is

dispatched with the start valve inoperative

• Following the EICAS message ENG START VALVE L/R; complete the start on the good

engine.

• Put on EAI if required on the operating engine

• Read the ENG START VALVE L/R checklist

• Consult the MEL for dispatch

• Advise the ground crew that a Manual Override Engine Start is required and ask them to get

the Tool from the E&E compartment

• Read the SP

• Arrange a system of hand signals and demonstrate this with the ground engineer while he still

can speak to you (when at the engine he may not be able to use his interphone)

APU INOP DISPATCH

NOTES:

• Considerations:

• MEL - Backup generators must operate. ETOPS limited to 120minutes. Etc.

• Next stations - Is ground power available and ground cart for air start available. Is ground air

conditioning required?

• Consult EK engineering. Get them to advice ground staff at destination of requirements.

• Use

the FCOM SP ENGINE GROUND PNEUMATIC START

and the FCOM SP ENGINE

START WITH EXTERNAL ELECTRIC POWER

to start the engines at the stand. If a B777

tow bar is not available, then use the above procedure to start one engine. Disconnect the

Ground Pneumatic Air and GPU and push back.

• Then, accomplish the S.P ENGINE CROSSBLEED START procedure using the running

engine to provide duct pressure.

QRH NON-NORMAL MANEUVERS

QRH MAN 1.1

QRH MAN 1.2

No further aft trim

Stick Shaker activates, and the Slats automatically extend from the midrange position to the fully extended position

AIRSPEED LOW Displays A/T Advances

ADVISE ATC FOM 13.4 ADVISE ATC FOM 13.4

QRH MAN 1.8

FCOM L.10.9 FCOM 10.10.31

Weather RADAR and TCAS are not displayed in CTR APP, CTR VOR, and PLAN modes on the ND.

FCOM 15.20.17

The STATUS message TCAS displays if the ADIRU is off or not aligned.

3. QRH NON-NORMAL MANEUVERS

STUDY GUIDE

QRH MAN 1.9

Emergency Procedures

FOM 20.2

FCOM NP.40.5

3. QRH NON-NORMAL MANEUVERS

STUDY GUIDE

QRH FCOM FLIGHT PATTERNS

Min width of pavement for a 180 turn 772

155.8 feet, 47.5 meters for nose gear

FCOM 1.10.5

Min width of pavement for a 180 turn 773

183.8 feet, 56 meters for nose gear

FCOM 1.10.7

4. QRH & FCOM FLIGHT PATTERNS

STUDY GUIDE

180 Degree Turns in less than 45 m

FCTM 2.12

777-200 ... 38.4m

777-300 ... 43.6m

777-300ER ... 43.7m

Min width of pavement for a 180 turn 772

155.8 feet, 47.5 meters for nose gear

FCOM 1.10.5

Min width of pavement for a 180 turn 773

183.8 feet, 56 meters for nose gear

FCOM 1.10.7

-

Line up outside tires on outside edge.

-

Come to complete stop.

-

Turn tiller to maximum steering angle.

-

Apply full inside brake.

-

Apply sufficient outside thrust to turn the aircraft.

-

Keep the inside brake locked until nose wheel clears the far edge of the turn.

-

Inspection of runway and aircraft required

.

Non Normal Ops. (Not an Emirates approved procedure)

Min width of pavement for a 180 turn 772

155.8 feet, 47.5 meters for nose gear

FCOM 1.10.5

Min width of pavement for a 180 turn 773

183.8 feet, 56 meters for nose gear

4. QRH & FCOM FLIGHT PATTERNS

STUDY GUIDE

This diagram is for reference only. Boeing has removed it from the current QRH.

4. QRH & FCOM FLIGHT PATTERNS

STUDY GUIDE

This diagram is for reference only. Boeing has removed it from the current QRH.

T

ran

sitio

n

Check

T

Tr ansi ti on

C

Ch e cklist

C

C abi n R e ady

L

LOC… Id entifie d

P

P A Co mp le te d

4. QRH & FCOM FLIGHT PATTERNS

STUDY GUIDE

A/P Of f by 50´bel o w MDA

T

ran

sitio

n

Check

T

Tra n s itio n

C

Ch e cklist

C

C abi n R e ady

L

L O C… Ide n tified

P

P A Co mp le te d

CHE

CKI

NG OF

R

A

W DA

TA

FCTM 5.

27

LOC, LO

C B/

C, LD

A, SDF

, IGS

- Raw data m ust be monitored.

VOR, TA

CA

N, NB

D, R

N

A

V, GPS…et

c.

Checking raw da ta may be accomplished by : -

Pushing the POS

switch on the EF

IS control panel

and comparing t

he displayed data with the navaid

symbols on the map. Example: The VOR radials and raw

DME da

ta should overlay the VOR/

DME

stations shown on the MAP and t

he GPS position

symbol should n

early coincide wit

h the tip of the

airplane symbol. - Displaying the V O R and or AD F pointers on the map

display and usin

g them to verify you position relative

to

the

MAP

T

ran

sitio

n

Check

T

Tra n s itio n

C

Ch e cklist

C

C abi n R e ady

L

L O C… Ide n tified

P

P A Co mp le te d

V/S 1 click =

100fpm

FPA 1 click = .1°

B

o

th F/D

s Off

PNF F/D O

N

CHE

CKI

NG OF

R

A

W DA

TA

FCTM 5.

27

LOC, LO

C B/

C, LD

A, SDF

, IGS

- Raw data m ust be monitored.

VOR, TA

CA

N, NB

D, R

N

A

V, GPS…et

c.

Checking raw da ta may be accomplished by : -

Pushing the POS

switch on the EF

IS control panel

and comparing t

he displayed data with the navaid

symbols on the map. Example: The VOR radials and raw

DME da

ta should overlay the VOR/

DME

stations shown on the MAP and t

he GPS position

symbol should n

early coincide wit

h the tip of the

airplane symbol. - Displaying the V O R and or AD F pointers on the map

display and usin

g them to verify you position relative

to the MAP display.

FCTM 5.4

5

- If th e ne xt al titude constrain t i s not a t a n even 100 foo t incre m ent se t the MCP altitude to th e nea re st 100 foot in crem ent below the al titud e con stra int . - Con sider establi shi ng fi nal approa ch pi tch mode and co nfig uri ng for the approa ch and landing e arlier th an the FAF.

4. QRH & FCOM FLIGHT PATTERNS

STUDY GUIDE

Min Altitud

e

1,500 AAL

FOM 15.1 0 .5 .5

Recommendation

Use PROG page

2 to Disp

lay cross track info

and to give Head

wind / Crosswin d components.

FOM 0.1

Briefing P

o

ints

-

Missed App

ro

ach Procedu

re

-

Terrain a

w

ar

ene

ss a

nd EGPWS co

nce

rns

-

Confirm missed app

roa

ch

pro

ced

ure wit

h

ATC

-

Cat D 20

5 kts

.

-

3 se

ctors mu

st be flown

-

Do

wn

wind le

g must comm

ence abe

am the

upwi

nd thre

shold.

-

The re

quired

visual refe

re

nc

e mu

st be

maintaine

d throug

hout the

approa

ch.

-

Significant m

et and terrain

con

side

ratio

ns

that may cause opti

cal illusions.

-

Whe

re po

ssib

le instru

ment

approa

ch aid

s

sho

uld be utili

zed.

Company VMC

-

5,000m o

r 3sm visibilit

y

-

1,000 feet ve

rtically fro

m

cl

oud

-

2,000m o

r 1.5 nm’ hori

zo

nt

al from clou

d

FOM 15.10.5.

5

F/Ds OFF

_{PNF F/D O}

N

Min Visibili ty 50 00 M or Jep p Min i f hi gher FOM C h ap 19 p a ge 6 Min Alti tu de hi g h er of 1,000 A A L rou nde d up t o ne arest 10 0 or Jep p Mini m a FO M Chap 19 p a ge 6

Recommendation

Use PROG page

2 to Display cross track info and

to give Headwind / Crosswind com ponents.

Recommendation

If Approach is an ILS use V/S to d escend. If not it is difficu lt to chan ge from G/ S /S to ALT .

4. QRH & FCOM FLIGHT PATTERNS

STUDY GUIDE

PNF F/D

ON

Min Alti tu de hi g h er of 1,000 A A L rou nde d up t o ne arest 10 0 or Jep p Mini m a FO M C h ap 19 p a ge 6 Min Visibili ty 50 00 M or Jep p Min i f hi gher FOM C h ap 19 p a ge 6

This diagram is for reference only. The procedure is still valid; however, Emirates have cancelled the FCTM Vol 2.

Recommendation

Use PROG page

2 to Disp

lay cross track info

and to give Head

wind / Crosswin d components.

Recommendation

If Approach is an ILS use V/S to d escend. If not it is difficu lt to chan ge from G/ S /S to ALT .

Cau

tion for

Single Engine Go-Aroun

d

Loss of c o n trol prior t o reachi n g stick shaker may occur a fter a n e ngin e fail ure at l ight wei g h ts. Minim u m R eco mme nde d Spee d is Vref+5. Fleet Fact s July /Aug ust 2 007

The accel

eration altitude o

n a missed a

ppro

ach will b

e

Jep

pe

sen p

ublish

ed misse

d approa

ch al

titude.

F O M 15. 11

4. QRH & FCOM FLIGHT PATTERNS

STUDY GUIDE

FCOM LIMITATIONS

.

-

The Overhead rest compartment must not be occupied

when the aircraft is below 25,000 feet. FCI 2006/77

-

Max Speed to Extend Landing Gear 270KIAS /M.82

5. FCOM LIMITATIONS

STUDY GUIDE

.

RTOW User Manual

FCI 2006-103 - Assumed Temperature Method is not permitted SLUSH,

SNOW, STANDING WATER, it is permitted for takeoff

on a wet runway.

- Take-off from an icy runway is not allowed.

-

Icy runway is more that 25% of the runway surface area

within the required length and width being used is covered

by ice, including wet ice. FCI 2006/03

FCOM SP 16.2

FCOM SP 16.3

AFM Section 1 page 9A

– Max Tire Speed for Takeoff is 235 mph – 204kts

.

Metric Winds

1 meter / second = 2 kts

FCTM 4.15 FCOM 16.4

V

REF

Adjustments

FCTM 1.16

A/T Engaged

-

VREF + 5 knots.

A/T Disengaged

-

VREF + ½ the headwind component

+ All of the Gust component to a

maximum of 20 knots.

- Calculate

HW

as:

- 50% Direct HW

- 35% for 45°HW

- Interpolate between

AFM Section 1 page 9A

– Max Tire Speed for Landing is 260 mph – 226kts

5. FCOM LIMITATIONS

STUDY GUIDE

.

Landing Weight + Trip Fuel + Under load = Allowed Take-off Weight

TRENT 877 TRENT 892 TRENT 892 TRENT 892 GE90-115B GE90-115BL1 GE90-110B1L1 FMC IDENT 777-200 FMC IDENT 777-200.1 FMC IDENT 777-200.1 FMC IDENT 777-200.2 FMC IDENT 777-300 FMC IDENT 777-300.1 FMC IDENT 777-300.2

.

.

.

.

FOM 15.10.5.1 FCI 2007-98

5. FCOM LIMITATIONS

STUDY GUIDE

FCOM L.10.7 Engine Limit Display Markings. Maximum and minimum limits are red, caution limits are amber.

The Limits in the table below are from the AFM are provided for reference only.

AFM

_{RR Trent 877}

777-200

777-200ER 777-300

_{RR Trent 892}

_GE90-110B1L1

777-200LR

_GE90-115B

777-300ER

777-300ER/ULR

_GE90-115BL1

Max Rated Thrust

76,900 lbs

90,000 lbs

110,000 lbs

115,000 lbs

115,000 lbs

Thrust Bump

When TO B is selected, the thrust increase provides additional take-off thrust at runway pressure altitudes between -2000 and 3,000 feet at ambient temperature between 32°C and 53°C. FCOM 11.40.42

NO

NO

YES

NO

YES

Max EGT

TOGA

920°C 20 seconds

900°C 5 minutes*

920°C 20 seconds

900°C 5 minutes*

(17,000 and Below)

1095°C 30 seconds

(All Altitudes)

1090°C 5 minutes*

(17,000 and Below)

1095°C 30 seconds

(All Altitudes)

1090°C 5 minutes*

(17,000 and Below)

1095°C 30 seconds

(All Altitudes)

1090°C 5 minutes*

*10 minutes allowed in the event of loss of thrust on one engine during take-off

Max Cont.

850°C

850°C

1050°C

1050°C

1050°C

Starting

700°C

700°C

750°C

750°C

750°C

In-flight Starting

700°C

700°C

825°C

825°C

825°C

Jet A -40°C Jet A1 -47°C

.

.

_{QNH/QFE Selection is on the APPROACH REF page}

AFM Section 1 page 7

– MMO is .89

5. FCOM LIMITATIONS

STUDY GUIDE

.

.

LIMITATIONS AND POLICIES

Item

Limit / Policy

Reference

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www.flightcrew.emirates.com

- Standard sign-on procedure

- To Access GABI sign-on with Staff number (s---) second password_____________ - To Access LH FIV Web Applications / Flight Operations / LH Systems FIV

User ID UAEFLEET Password uae4XzB

http://emirates.pelesys.com/ - Access to the Emirates training website

- Sign-on with Staff number (s---) and pelesys password_____________

www.emiratesstaff.com - Access to the Emirates travel website _{- Sign-on with Staff number (---) and PIN_____________} www.flyzed.com - Website providing information on ZED flights _{- Sign on with Userid _____________and Password_____________}

Uniform Policy

Summer 15th _{Apr – 31 Oct Jacket only required for Layover Flights, Jacket may be} carried at the discretion of the commander.

Winter 1st _{Nov – 14}th _{Apr Jacket required for all flights.} FOM Chap 14 page 3 Sickness Notification

- Every effort should be made to provide Crew Scheduling with early notification, whenever sickness occurs prior to a flying or standby duty. Any crew member reporting sick less than 4 hours before the commencement of duty will be required to explain the reason for the late notification to his Chief Pilot.

FOM 2.8

Transport to CBC

- Pickup time is STD -2:15

- If transport has not arrived :10 after expected pickup time call Central Services. - If transport has not arrived :20 after expected pickup time make your own transport

arrangements.

FOM 14.2

Minimum requirements for Preflight Planning / Briefing

- OFP for accuracy and validity

- NOTAMS and weather for departure, destination, alternate, and enroute airfields within the 1st _{hour of flight.}

- Relevant FCIs

FOM 12.2

New Commander Restrictions

- Two Recently Trained Pilots must not fly together until they have completed a 45 day consolidation period.

- No CAT II III approaches until 50 hours or 20 sectors on type. - + 100 meters for CAT II III Approaches until 100 hours or 40 sectors.

FOM 4.2 FOM 18.17.2

Emergency Procedures - The commander should conduct the landing in non-normal situations where the _{aircrafts performance is affected…} FCI 2007-97

FO Restrictions

No ops on contaminated runways. No crosswinds in excess of 20 knots. Take-off vis. Is more than 500 meters.

FOM Chap 3.4.10 FCI 2007-080

Minimum Width of Runway

Minimum width of runway for Emirates operations is 45 meters. In cases where runway is less than 45 meters approval of the VPFOT is required.

Minimum width of cleared runway for operation on Contaminated Runways 30 Meters.

FOM Chap 15 page 5 FOM 18.13

-200LR,-300s OPT - For MACTOW C of G 26% and greater use alternate C of G. FCOM Bulletin 10R3

OPT Laptop - To Reset OPT to original page, ALT TAB Instructor Technique

Printing from EFB - The OPT T/O PERF page can be printed _{- Select an invisible button at L8, “SEND TO FLT DECK PRINTER”, “COMPLETE”.} OPT T/O Performance Preference -200, -200ER, -300 1) PACKS ON 2) PACKS OFF -300ER 1) PACKS ON 2) APU to PACKS or PACKS OFF -200LR, -300ER/ULR 1) PACKS ON

2) APU to PACKS or PACKS OFF 3) T/O BUMP

FCOM 11.40.42 FCOM NP.21.26 FCOM SP2.1

T/O Bump

- Available on the 772LR, 773-ER/ULR

- Additional thrust is provided from PA -2,000 to+3,000 and temperatures between 32°C and 53°C.

FCOM 11.40.42

Assumed Temperature Not Authorized

- Alternate EEC mode operation; MEL 73-21-02 - Contaminated Runways;

- Potential Windshear conditions exist. - At Pilots discretion full thrust can be used.

RTOW Chart User’s Manual 1-10 FOM15.4 FCOM SP.16.1 FCOM.SP.16.19

New OFP - If the ZFW changes by 3000 kgs the commander may request a new OFP FOM 11.4.1

FMS Auto Init Failure After 2nd _{failure send message to DXBOVEK}

FCOM SP. 5.3

Cockpit Printer Paper

End of Roll Indication A single line means there is 5 meters of paper left. A double line means there is 2 meters of paper left.

Door Entry code 1 ENT Generates a doorbell tone in the cockpit FCOM S.P.1.2

Door Emergency Code - 345 ENT will open the Door after 30 seconds. If denied keypad is inhibited for :10 min. _{- Must only be used if Pilot Incapacitation is suspected.} FCOM S.P.1.2

FOM 10.10

Upper Crew Rest Area Door Entry Code 123 ENT _{Must not be occupied when the aircraft is below 25,000 feet.} FCOM 1.47.2

FCOM 1.46.5

Oxygen Minimum for DXB departures 1500psi _{Out stations approximate min 1,000 psi. If lower check manual for dispatch requirements.} Daily Inspection Sheet

6. LIMITATIONS AND POLICIES

STUDY GUIDE

Item

Limit / Policy

Reference

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Useful Telephone Numbers SMNC ... 971 4 229 6061 971 4 218 2200 FDM ... [email protected] 971 4 229 8089 971 4 218 4410 DISPATCH ... Duty Manager 971 4 708 1012 Dispatch General 971 4 708 1014 971 4 299 1042 MCC ... [email protected] 971 4 208 5540 971 4 208 5539 971 4 208 5710 971 4 208 5711 FAX 971 4 224 4380 Crew Control ... 971 4 218 2221 971 4 218 2220 CBC ... 971 4 218 4407 971 4 218 4408 CS Transport ... 971 4 218 4537 971 4 218 4540 971 4 218 4539 971 4 218 4538 Medlink ... 001 602 236 3627 Ed Davidson ... Office 971 4 703 6408 Mobile 971 50 550 8351 Caution

With the move to the new HQ these numbers

may have changed

PIC Responsibility for the Passengers.

The PIC becomes responsible for the Passengers when he accepts the release of the aircraft from an authorized member of the ground staff, the aircraft doors are closed, and the boarding ramps are withdrawn.

FOM 16.1.1

Passenger Care Flight and Cabin Crews must be on board whenever passengers are on board or embarking/disembarking at all stations. One member of Flight Crew will be sufficient to

meet the above requirement. FOM 16.1.3

INAD

- INAP Inadmissible Passengers are not limited to any number and do not require special authorization to travel.

- For INAD pax a C15 form must be completed by ground staff and given to the Purser and PIC.

FOM 16.1.6

DEPO

- Emirates Security evaluates each DEPO and determines if they may travel unaccompanied or require an escort.

- No more than 1 unaccompanied DEPO should be carried on any flight with an exception permitted for families.

- If more than one unaccompanied DEPO is to be carried, prior approval and authorization Chief of Group Security is required.

- No more than a total of 8 DEPOs and Prisoners should be carried on any flight. - If the total number of DEPOs and Prisoners exceeds 8 the Chief of Group Security or

his deputy must give permission and provide Flight Operations with the required criteria.

- For DEPO pax a C15 form must be completed by ground staff and given to the Purser and PIC and their travel documents and tickets are handed to the Purser or SFS.

FOM 16.1.6

Prisoners

- Emirates Security evaluates each Prisoner and determines if they may travel. - Prisoners are escorted at all times and remain under close supervision of the escort. - For prisoner pax a C15 form must be completed by ground staff and given to the

Purser and PIC and there travel documents and tickets are handed to the Purser or SFS.

FOM 16.1.6

Disabled Passengers

- Ambulatory Passengers… no Restrictions

- Non-Ambulatory Passengers… must be able to feed themselves and manage own body functions… if not the must be accompanied by an able body person/attendant. - PIC must be advised of all passengers who could require special assistance in the

event of an evacuation.

FOM 16.1

Wheel Chair Codes When ordering a wheelchair _{use the appropriate code.}

WCHR Pax can exit aircraft, use steps but cannot walk

long distances.

FOM 16.10.3 WCHS Pax can exit aircraft, but cannot use steps but or

walk long distances.

WCHC Pax are completely immobile and require

wheelchairs to and from their cabin seats.

Pregnant Passengers

- No Letter is required up to the end of the 27th _week;

- When a pregnancy has entered the 28th _{week a medical certificate or letter is required}

stating fitness to fly and confirming the delivery date. - The letter must be returned to the passenger after verification.

- No approval required from Medical services up to the end of the 36th _week.

- Multiple pregnancies accept up to the end of the 32nd _week.

FOM 16.1.8

Falcons

- The number of falcons on a wide body aircraft should not exceed 15 - Economy or Business 1 per seat, if additional seat purchased an additional 2. - First Class 2 per seat, if additional seat purchased an additional 3.

- SVPFO or rep may grant exceptions for VIP passengers.

FOM 16.2.3

Human Eyes - Treated as unaccompanied valuables and stored in lockable stowage in the cabin. _{- E6 Locker Stowage waybill form will be filled out and Captain advised via NOTOC.} FOM 16.2.3

Aircraft Designators

The following new ICAO aircraft designators are shown in the ICAO ATS-FPL:

B-777-200ER ... B772 B-777-200LR ... B77L B-777-300 ... B773 B-777-300ER ... B77W

Standard aircraft identifications are required in the Tech Log.

Boeing 777-200 ... B772 Boeing 777-300 ... B773

Company NOTAMS FOM 15.3.2

1 2

3

Item

Limit / Policy

Reference

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Daily Inspection - The Validity period of a Daily check is 48 hours. - The inspection must not expire before the planned arrival time.

(sufficient time to divert and recover the aircraft should be considered)

FOM Chap 15.3.3

MEL Repair Intervals

A ... Specified Interval B ... 3 days C ... 10 days D ... 120 days

- The time period specified shall start at 00:01 UTC on the day following the day of discovery.

- Day of Discovery: The calendar day an equipment/instrument malfunction was recorded in the aircraft maintenance log and or record. This day is excluded from the calendar days or flight days specified in the MEL for the repair of an inoperative item of equipment. This provision is applicable to all MEL items, i.e. categories “A, B, C, & D.

MEL Preamble MEL Definitions 2.00-01-00.2

MEL Deferred Defect DD Types

P ... Performance Penalty, Autoland or ETOPS restriction R ... Repeat Inspection M ... No Performance / Penalty C ... Passenger Cabin / Entertainment L... Loan / Pool N ... Any other defects not covered by above codes

Tech Log Page Divider

Stations without an Authorized Engineer

The PIC is authorized to certify the Tech Log for: 1) Refueling

2) Transit Checks

3) Transfer of acceptable Defects to the ADD section

FOM 16.3.3.2

Use of Conti. Fuel Contingency fuel can be used after the fueler disconnects. FOM 11.1.2.3

STATUS messages

- STATUS messages are checked prior to engine start and the condition should be corrected or dispatched per the operator’s MEL.

- There are no inflight crew procedures associated with STATUS messages.

- STATUS messages are inhibited from beginning of first engine start until :30 minutes after lift-off.

FCOM 15.10.2 MEL Section 1 General

EICAS Mess. page 2

Dispatch - The moment at which the Ground Engineer is released prior to taxi. _{- ETOPS Items are to be considered as Inflight Dispatch Items} MEL Preamble

FOM 19.1.6

Use of MEL after Dispatch

- MEL does not apply.

- Continuation of flight is at Captain’s discretion.

- Consult EICAS complete required FCOM/QRH procedures. - Contact Company and review situation. (FMGS or RM Chapter 10) - Review MEL for considerations. Return to the stand if:

o Failed equipment does not allow the continued safety of the flight. o If maintenance actions are required.

o Continuing the flight with the failed equipment is determined inappropriate.

(e.g. can the problem be repaired or dispatched from the destination airport) Check Performance for return flight

MEL Section 2 Introduction MEL Preamble

MEL Concession

- Used to dispatch an aircraft with unserviceabilities not normally permitted by the MEL.

- Initiation of a request must be the Commander’s exclusive prerogative. - The aircraft commander must receive a written copy of any concession prior to

dispatch and this copy is to be kept with the aircraft Technical Log.

MEL Section 0 Introductions Concessions FOM 15.3.2

Tire location for entering

defects FCOM 14.10.6

Window Locations for reporting window heat

problems MEL 30-41

Power Outlets Medical Power Outlets locations are described in FCOM AIRPLANE GENERAL. FCOM 1.30.26

Circuit Breakers

- A ground reset of a CB by the flight crew should only be done after maintenance has determined that it is safe to reset the CB. Any tripped CB event must be recorded in the Tech Log or Cabin/IFE Defect Log.

- Flight crew reset of a tripped CB in flight is not recommended; however, if not prohibited by manufacture’s instructions a tripped CB may be reset after a 2 min cooling period if in the captains judgment the Tripped CB would have a significant adverse effect on safety.

- Flight crew cycling of CBs to clear non-normal conditions is prohibited unless directed by a non-normal checklist or FCOM procedure/bulletin.

- Resetting of buss tie sws on ground after ELEC BUS ISOL EICAS message comes on after engine start is permitted.

FOM 17.11

EKIB-8R1

6. LIMITATIONS AND POLICIES

STUDY GUIDE

Item

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Reference

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Flight Time Limitations - 100 hours in 28 days _{- 900 hours in 12 months} FOM 21.1

Take-off/Landing Requirements

- At least one take-off and landing as PF in an aircraft or simulator within the preceding

35 days. Emirates Policy

- In exceptional circumstances the SVP-FO or his nominated deputy can alleviate all recency requirements except CARS-OPS 1.970.

- 3 take-offs and landing as PF in the preceding 90 days. CARS-OPS 1.970 - May be exceeded up to 120 days by flying under supervision of a Training Captain. - Beyond 120 days the recency requirement must be satisfied by simulator training.

FOM 3.4.4.1

Days Off

- Crew Members shall not be on duty more than 7 days between days off, but may be positioned to the usual operating base on the 8th _{day provided they are allocated at least 2}

consecutive days off.

- Crew members shall have 2 days off in any consecutive 14 days following the previous 2 consecutive days off.

- Crew members shall have a minimum of 7 days off in any consecutive 28 days. - Crew members shall have an average of at least 8 days off in each consecutive 28 day

period, averaged over three such consecutive periods.

FOM 21.20.4 Documents Required on Board AIRCRAFT DOCUMENTS 1) C of R 2) C of A Check Date

3) Original Copy of Noise Certificate 4) Original Air Operator Certificate. 5) Aircraft Radio Station License Check Date

6) Third party liability insurance certificates. Check Date

CREW DOCUMENTS 1) Crew Licenses 2) Crew Passports 3) Certificates of vaccination. 4) Copy of LPC/OPC 5) Company ID card FOM 2.1 MANUALS 1) FOM 2) FCOM Vol 1 3) QRH 4) MEL

FLIGHT SPECIFIC DOCUMENTATION

1) OFP

2) Aircraft Tech/Journey Log 3) Filed ATS flight plan 4) NOTAMs 5) Weather

6) Load and Trim Sheet 7) Notice of Special Pax C15 8) NOTOC

9) Maps and Charts 10) FCIs

11) Forms Binder Prioritization of Manuals

The FOM shall take precedence over all Manuals. The FCOM shall have second priority after the FOM. FCIs may supersede any document except the AFM. Jeppesen Manual takes precedence over OM-C/RAIG

FOM 2.1 FOM 13.4

FOM Part A Chapters

0) Definitions and Abbreviations 1) Duties and Responsibilities 2) Company Regulations

3) Training, Checking, Qualifications, Recency 4) Flight Crew Rostering

5) Administrative Instructions and Forms

FOM

FOM Part B Chapters

10) Safety and Security 11) Fuel Policy

12) Flight Preparation & Planning 13) General Flight Rules 14) General Crew Procedures 15) Normal Operations 16) Handling Operations 17) Use of Equipment 18) Adverse and AWO 19) Special Operations 20) Abnormal Operations 21) Flight Time Limitations

FOM

MEL Chapters

0) Introduction, Concessions, ETOPS Sensitive Items, Autoland 1) EICAS Messages

2) MEL

3) CDL… Now relocated to the AFM

4) MISC

MEL

LIDO Route Manual

.

GENERAL PART

PFL Preflight IFL Inflight ADR Aerodromes MET Meteorology NAV Navigation COM Communication

RAR Rules and Regulations - Approach add-ons for failed or downgraded ground equipment.

LAT Legends and Tables

ABB Abbreviations

SAI Special Airline Info BUL Bulletin

ADM Administration

NETWORK PART

CRAR Country Rules and Regulations - Contains differences to ICAO Standard. (Aerodrome specific differences located on the AOI page).

AOI 1-10 Airport Operations Information ‐ General 1-10 .. Airport Hours

Airport Information (RFF, PCN)

Operation Pref Runway, Rwy/Taxi restrictions APU restrictions. Warnings

Arrival 1-20 . Speed

Communications .. Com Failure Procedures

Arrival Procedures Vis approach, Diversions, LAHSO, and Reverse. Warnings

Departure 1-30 . Take-off Minima

 

Speed

Communications .. Com Failure Procedures ATC Slot, Clearance

Deicing

Departure Procedures Warnings

AFC 2-10 Airport Facility Chart ‐ Plan view, runway Information, and communication information

‐ Quick reference for approach and landing, after take-off and in case of emergency. ‐ Minimum Grid Altitude (MGA) provide 1,000 feet protection below 6,000 ASL and 2,000

feet protection for 6,000ASL and above. ‐ MGAs above 10,000 are in red. 101

AGC 2-20 Airport Ground Chart

APC 3-30 Airport Parking Chart ‐ Taxiways with limitations are shaded in brown. Limitations detailed on the AOI pages. ‐ Parking bays with a solid arrow are pushback bays, with an open arrow are self

maneuvering bays. LVC 3-X0 Low Visibility Chart

EOSID 4-01 Engine Out SID ‐ Altitudes in red represent Minimum Terrain Clearance altitudes up to the IAF. ‐ At or above 9600, at 9600, at or below 9600.

SID 4-X0 Departure Chart ‐ Altitudes in red represent Minimum Terrain Clearance altitudes up to the IAF. ‐ At or above 9600, at 9600, at or below 9600.

SIDPT 5-10 SID Procedure Text ‐ Lists departure frequencies, changeover instructions, and departure gradients >3.3%. ‐ Details of SID.

STAR 6-10 Arrival Chart ‐ Altitudes in red represent Minimum Terrain Clearance altitudes up to the IAF. ‐ At or above 9600, at 9600, at or below 9600.

STARPT 6-X0 STAR Procedure Text

IAC 7-10 Instrument Approach Chart ‐ Total approach distance indicators at the start of each transition to the FAF/FAP. ‐ Name of chart is in upper right side and required equipment is listed.

VAC 7-X0 Visual Approach Chart

MRC 8-10 Minimum Radar Vectoring Chart ‐ Altitudes in brackets indicate obstacle clearance at cold temperatures.

FAM 9-10 Familiarization Chart

TEMPO X-X0 Tempo Chart

ENROUTE PART

RFC Route Facility Chart ‐ Enroute Charts are oriented to True North. (Some may be oriented for polar grid navigation)

‐ Minimum Grid Altitude (MGA) provide 1,000 feet protection below 6,000 ASL and 2,000 feet protection for 6,000ASL and above.

‐ MGAs above 10,000 are in red. 101

RFC Supp. RFC Supplement ‐ HF frequencies and IFR cruising altitudes IOI Intermediate Operational Inform. ‐ Chart NOTAMS

6. LIMITATIONS AND POLICIES

STUDY GUIDE

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Application of TAF FOM 12.2

No Forecast Weather If no forecast is available for a selected airfield, it must be considered as being below

6. LIMITATIONS AND POLICIES

STUDY GUIDE

Item

Limit / Policy

Reference

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Critical Phases of Flight

1) Taxi to 10,000 AAL.

2) Approach to Land below 20,000 AAL, and Landing. 3) All other Flight Operations below 20,000 feet. - No Distractions permitted.

- Sterile Cockpit procedures.

- Restricted Electronics Devices must be switched off

FOM 0.1 FOM 13.1 FOM 15.2 FOM 17.1

Cabin Spraying Procedure

- Spraying should commence once catering is onboard and before passengers are boarded.

- Packs are turned off and turned on 5 minutes after spray completed. - Overhead/Side lockers open all doors closed except L1.

- 3 Cans sprayed, 1 row / sec.

- 4 cans sprayed into Cargo hold, Aircraft Hold Disinfection Certificate completed and given to Purser… Cabin Certificate completed by Purser.

OM-C RAI G Chap 2 Pg. 79

Cargo Smoke after Cargo Hold Spray with no evidence of smoke

- “ATTENTION CREW AT STATIONS”.

- On ramp have Ground Personnel inspect Cargo Hold.

o Aerobridges must be connected and/or Passenger Doors armed. FOM 20.3 - On taxiway or runway request Fire Department to inspect Cargo Hold.

o Aerobridges must be connected and/or Passenger Doors armed. FOM 20.3 - Next call “CABIN CREW REVERT TO NORMAL OPERATIONS” or “EVACUATION

CHECKLIST”.

Personal Procedure

Alternate Airport Planning Minima

- Weather required before Dispatch:

APPROACH

AVAILABLE MINIMA

CAT III CAT I

CAT II CAT I + 100 ft / 300 m

CAT I Non-precision 600 feet / 2,000 meters

Non-precision Company circling minima-higher of Jepp, or 1,000 feet/5,000 m. _{or, if no circling available- NP approach + 200 feet / 1,000 m.} Circling 1,200 / 5,000 meters

- Nav aids required to designate an airport as an Alternate: (Terminal radar is a Nav Aid)

o Wx CAVOK One Serviceable Nav Aid.

o Wx less than CAVOK 2 serviceable Nav aids - Weather required after Airbourne:

o Only Jeppesen chart minima need be considered.

FOM 12.4

Take-off Alternate

- When Performance or Met conditions preclude a return to the departure airport a take-off alternate airport must be selected.

- Within a distance of NON-ETOPS aircraft 420nm

ETOPS aircraft 840nm For USA Ops 420nm

(as long as no ETOPS MEL restrictions apply)

- Required weather 1 hour before and 1 hour after ETA above applicable landing minima. CAT II and III minima are applicable and ceiling is required for non-precision approaches. USA Ops require weather above USA Alternate Minima.

- Any limit. related to one engine inoperative operations must be taken into account.

FOM 12.4

USA Departure and T/O Alternate Planning Minima

FOM 19.10

NAV aid NOTAM Ground checked only

May be used for enroute navigation, but not as an approach aid. _{FOM 17.4} Night Operations - Runway edge and stop end lights are required for takeoff. - For night operations at least runway edge, threshold, and runway end lights must be

on.

FOM 15.7.1 FOM 17.5

HAIL and LIAL