ENGINE AND WING ANIT ICE

ICEING CONDITIONS EXIST WHEN OAT ON GROUND OR TAT IN AIR IS 10° OR BELOW
AND
VISIBLE MOISTURE mist is considered visible moisture/PRECEPITATION/( and so on)
or
FG 1 MILE OR LESS

OR
ICE SNOW SLUSH WATER ON THE MOVEMENT AREAS
__________________

-ALWAYS PUT START SWITCHES TO CONTINUOUS BEFOR PUTTING ON ANTI ICE

-ENGINE AND WING ANTI ICE COMES ON, ON THE GROUND IN ICEING CONDITIONS

-WING ANTI ICE OFF IF GETTING A DEICE FOR TYPE ll or lV
STAYS ON FOR A FROST SPRAY

-IN THE AIR
ENGINE ANTI ICE ON WHEN IN ICEING CONDITIONS
WING ANTI ICE ON ONLY WHEN THE NUT ON WIPER HAS ICE ON IT
off at 35000ft
delay use and let build up, then on continually especially for severe

-NO ENGINE ANTI ICE NEEDED WHEN IN CLIMB OR CRUISE WHEN SAT PROG PG 3? IS LOWER THEN -40°
USE DURING DECENT IN ALL ICEING CONDITIONS

taxi out flaps up with reduced speed.

With engine anti-ice on and temperature is below 4° Do an engine run up 50% N 1 for 5 seconds Every 60 minutes

STABILIZED APPROACH

BY 1000 FT IF THE STABILIZED APPROACHED CRITERIA ARE NOT MET THEN GO AROUND MUST BE INITIATED UNLESS
THE AIRCRAFT SPEED DOES NOT MEET THE CRITERIA BUT CAN BE ACHIEVED BY 500 FT OR AIRCRAFT HAS MET ALL CRITERIA BUT NOT COMPLETED THE LANDING CHECKLIST

CRITERIA
AIRCRAFT IS ON CORRECT FLIGHT PATH AND ONLY SMALL CHANGES IN HEADING PITCH ARE REQUIRED

AIRCRAFT IS AT APPROACH SPEED +10 TO -5 ARE ACCEPTABLE

AIRCRAFT IS IN CORRECT LANDING CONFIG

SYNC RATE IS NO GREATER THAN 1,000 FT PER MINUTE

THRUST SETTING IS APPROPRIATE FOR CONFIGURATION

ILS FLOWING WITHIN HALF DOT OF GLIDE SLOPE AND LOCALIZER

DURING A CIRCLING APPROACH WING MUST BE LEVEL ON FINAL BEFORE 300 FT

BRIEFINGS AND CHECKLISTS HAVE BEEN COMPLETED

in gusty conditions air speed and decent rate can exceed criteria if captain deems it safe

MAX WEIGHTS MAX

MAX

MAX TAXI            82 871 KG

MAX TAKEOFF    82 644 KG

MAX LANDING    69 308 KG

MAX ZERO FUEL  65 952 KG

MAX WEIGHTS NG

- 800

MAX TAXI            79 242KG

MAX TAKEOFF    79 015KG

MAX LANDING    65 317KG

MAX ZERO FUEL  61 688KG

minimum flight weight is 36,651kg

MAXIMUM TAKE OFF AND LANDING TAILWIND

15 KTS

RUNWAY SLOPE

+/- 2%

MAXIMUM OPERATING ALTITUDE

41,000 FT

MAXIMUM TAKE OFF AND LANDING ALTITUDE

8400 FT  

10000 FT  FOR SOME MAXs
you would have to look it up in FCOM 1.
then go into performance section of QRH or first 4 pages of FCOM 1 for list of aircraft

MAXIMUM FLIGHT LATITUDES

you're okay to fly too
82 North and 82 South latitude

except between 80° West and 170° west longitude and maximum latitude is 73 north

and
between 120° East and 160° east longitude the maximum latitude is 60° South

WHAT MUST BE VERIFIED WITH PASSENGERS ON BOARD INSIDE THE CABIN

HANDLE COVERS ON THE OVERWING EXITS

FLIGHT DECK DOOR ACCESS SYSTEM CHECK MUST BE

CHECKED ONCE EACH FLIGHT DAY, SO A PRIOR CREW COULD HAVE DONE THE CHECK BUT HOW WOULD YOU KNOW REALLY?

GROUND WIND OPERATING ENVELOPE

CROSSWINDS GREATER THAN 43 KNOTS THRUST MUST BE LIMITED TO A SETTING NORMALLY USED FOR TAXI

WINDS GREATER THAN 58 KNOTS LIMIT ENGINE THRUST TO IDLE

NARROW RUNWAY OPERATIONS

WIDTHS LESS THAN 148 FT
(45M)
AND NOT LESS THAN 98 FT (30M)
centerline must be visible

DISPATCH TO NARROW RUNWAYS IS NOT ALLOWED. YOU TECHNICALLY COULD LAND ON 148 FT TO 98 FT BUT YOU WOULDN'T BE ABLE TO TURN AROUND IF YOU HAD LOST HYDRAULIC SYSTEMS NOSE WHEEL STEERING THRUST REVERSER ETC

HEIGHT AND WINGSPAN

HEIGHT
40 FT 4 IN
12.3(M)

WINGSPAN
117 FT 10 IN
35.92(M)

EYE TO WHEEL HEIGHT
13-16ft
BOEING WEBSITE

TURNING RADIUS 80 FT
SIM C CBT

LENGTH 116FT 8IN

TAKE OFF CROSSWIND COMPONENT

DRY 34

WET/ GOOD 25

GOOD TO MEDIUM 22

COMPACT SNOW /DRY SNOW/ WET SNOW/ MEDIUM
20

STANDING WATER/SLUSH /MEDIUM TO POOR 15

POOR 13

THE GUST DOESN'T COUNT

LANDING CROSSWIND COMPONENT

DRY (6) 37

GOOD (5) 37

GOOD TO MEDIUM (4) 35

MEDIUM (3) 25

MEDIUM TO POOR (2)17

POOR (1) 15

NIL 0

CRFI LESS THAN.25

check limitation section when you're Landing runway less than 148 ft width

also landings are not recommended with winds greater than
15 knots at flap 15
18 knots at flap 30
21 knots at flap 40

THE GUST DOESN'T COUNT EXAMPLE 26 GUSTING 59 YOU CAN STILL LAND

COM APPENDIXr

flairAIR OPERATOR CERTIFICATE APPENDIX A

TRANSPORTATION OF DANGEROUS GOODS APPENDIX B

IATA DANGEROUS GOODS TABLES APPENDIX C

FLIGHT CREW MEMBER FATIGUE MANAGEMENT APPENDIX D

EXEMPTION AND INCAPACITATED FLIGHT ATTENDANT APPENDIX E

RUNWAY CONTAMINATION LIMIT

DRY SNOW 102 MM OR 4 INCH

STANDING WATER WET SNOW/ SLUSH 13 MM OR 1/2 INCH

THE GIRT BAR OR ESCAPE SLIDE RETENTION MUST

BE INSTALLED FOR TAXI TAKE OFF AND LANDING ON REVENUE FLIGHTS

WHAT SHOULD YOU NOT DO DURING REFUELING

OPERATE HIGH FREQUENCY RADIOS
OR
SWITCH POWER SOURCES

ALTIMETER LIMITS FOR RVSM

INFLIGHT BETWEEN CAPTAIN AND FIRST OFFICER
200 FT

ON THE GROUND
SEA LEVEL TO 5,000 FT
50 FT

ON THE GROUND
5,000 FT TO 10,000 FT
60 FT

MAX DIFFERENCE BETWEEN CAPTAIN OR FIRST OFFICER AND THE FIELD ELEVATION
75 FT

HYDRAULIC QUANTITY

76% MINIMUM
100% MAXIMUM
OR
IF  RF  MESSAGE

CONTACT MAINTENANCE

OVERFILL COULD LEAD TO CONTAMINATION OF THE PACKS

OIL QUANTITY

MAX
69%  14.5 L

NG
65% 13 L

62% AND 60%
AS PER MAINTENANCE MANUAL

acess to all fluid reservoirs require maintenance as per
CBT aeroplane servicing and ground handling training for pilots

MAX CABIN DIFFERENTIAL PRESSURE

9.1

SAFEY OUT FLOW

WITH EITHER OR BOTH ENGINE BLEED AIR SWITCHES ON DO NOT

OPERATE THE PACK SWITCHES IN HIGH FOR TAKEOFF APPROACH OR LANDING

except when doing the cargo fire and smoke fume removal checklist

IT IS PROHIBITED TO USE AILERON TRIM WHEN

THE AUTOPILOT IS ENGAGED

DO NOT ENGAGE THE AUTOPILOT BELOW

400 ft

SINGLE CHANNEL AUTOPILOT ON APPROACH WILL BE DISCONNECTED BY

50 ft

MAXIMUM WIND SPEEDS FOR AUTOLAND

HEAD WIND 25 KTS
CROSSWIND 20 KTS
TAILWIND  15 KTS
10 KTS FLA

MAXIMUM MINIMUM GLIDE SLOPE ANGLES FOR AUTO LAND

3.25° AND 2.5°

AUTOLAND RESTRICTIONS

MUST BE USED WITH FLAP 30 OR FLAP 40

BOTH ENGINES MUST BE OPERATIVE

no overweight auto land

FLAP 40 FOR BETTER VIZ
FLAP 30 IF GUSTY

AND WIND RESTRICTIONS
25
20
15

IL075 - IL078 AUTOLAND RESTRICTIONS

NO AUTO LAND FOR RUNWAYS ABOVE 8,400 FT ELEVATION OR ON NARROW RUNWAYS

DO NOT USE LEVEL CHANGE

WHEN ON FINAL APPROACH BELOW 1000FT

USE THE VHF ANTENNA ON THE TOP OF THE FUSELAGE WHEN

COMMUNICATING WITH ATC WHILE ON THE GROUND

ENGINE IGNITION MUST BE ON FOR

TAKE OFF
LANDING
HEAVY RAIN
AND
ANTI-ICE OPERATION

ignition
SHOULD BE SELECTED TO THR RIGHT SIDE FIRST FLIGHT OF THE DAY
Starting on right switch is connected to battery, left is connected to one of the busses,
RIGHT CAN NOT BE  MEL'D

DERATED TAKEOFF THRUST IS NOT ALLOWED FOR

ALTERNATE EEC MODE OPERATION

ASSUMED TEMPERATURE REDUCED THRUST IS NOT ALLOWED WHEN

RUNWAY IS CONTAMINATED WITH STANDING WATER, ICE, SLUSH, OR SNOW

OR
ALTERNATE EEC MODE OPERATION

OR
ANTI-SKID IS INOPERATIVE

it is allowed with wet runway as long as opt says it's okay

THRUST REVERSER LIMITATIONs

THRUST REVERSER IN FLIGHT PROHIBITED

BACKING THE AIRPLANE USING REVERSE THRUST PROHIBITED

DO NOT ATTEMPT TO GO AROUND AFTER THE THRUST LEVERS ARE DEPLOYED

APU ALTITUDE LIMITATIONS

IN FLIGHT BLEED AND ELECTRICAL MAX ALTITUDE 10,000 FT

BLEED ONLY IN FLIGHT 17,000 FT

ELECTRICAL ONLYIN FLIGHT 41,000 FT

ON THE GROUND BLEED AND ELECTRICAL MAX ELEVATION 15,000FT

APU 110 KG/HOUR

IF 2 GENS FAIL DONT START TILL BELOW 25000 FT QRH

2 minutes before turning APU bleed air on.
turn a APU BLEED AIR off for 1 minute before turning off APU

APU BLEED AIR VALVE MUST BE CLOSED WHEN

BURN IS 110 KG / HOUR

GROUND AIR IS CONNECTED AND ISOLATION VALVE IS OPEN

ENGINE NUMBER ONE BLEED AIR VALVE IS OPEN

ISOLATION VALVE AND ENGINE NUMBER 2 BLEED VALVE OPEN

AFTER THREE CONSECUTIVE APU START ATTEMPS

A 15 MINUTE COOLING PERIOD IS REQUIRED

RUN THE APU FOR TWO FULL MINUTES BEFORE

TURNING THE APU BLEED AIR ON

APU BLEED AIR VALVE CAN BE OPEN DURING ENGINE START BUT

AVOID ENGINE POWER ABOVE IDLE

MAXIMUM FLAP EXTENDED ALTITUDE IS

20000 FT

HOLDING IN ICING CONDITIONS WITH______ IS PROHIBITED

FLAPS

INFLIGHT DO NOT EXTEND THE SPEED BRAKE LEVER BEYOND THE________ POSITION

FLIGHT

IN FLIGHT DID NOT EXTEND THE SPEED BRAKE LEVER BEYOND THE ARMED POSITION WITH

FLAP 40 SELECTED

DO NOT DEPLOY SPEED BRAKE AT AN ALTITUDE LESS THAN

1000ft

ALTERNATE FLAP LIMITATION

WHEN USING THE ALTERNATE FLAP SWITCH WAIT 15 SECONDS BEFORE USING THE ALTERNATE FLAP SWITCH AGAIN TO AVOID DAMAGING THE FLAP MOTOR CLUTCH

AFTER A COMPLETE EXTEND AND RETRACTION CYCLE ALLOW 5 MINUTES COOLING BEFORE ATTEMPTING ANOTHER EXTENSION. EG 0-30 AND BACK TO 0

AVOID WEATHER RADAR OPERATION OPERATION WHEN

IN A HANGER
OR
PERSONAL ARE WITHIN THE AREA ENCLOSED BY THE NOSE RADOME

VSD MUST BE SELECTED WHEN

TEMPERATURE CORRECTED ALTITUDES HAVE BEEN MANUALLY ENTERED INTO FMC

GRAYS FAQ SAYS EVERY APPROACH

ADIRU ALIGNMENT MUST NOT BE ATTEMPTED

AT LATITUDES GREATER THAN 78°, 15 MINUTES

DO NOT USE TERRAIN DISPLAY FOR

NAVIGATION
OR
WITHIN 15  MILES OF TAKEOFF or APPROACH TO LANDING TO AN AIRPORT THAT IS NOT IN THE GPWS TERRAIN DATABASE

locate those airports in the Honeywell document 060-4267
or on egpws.com

WHEN OVERRUN ALERT WARNING

WHEN YOU HEAR THE WARNING

COMMENCEMENT IMMEDIATE GO AROUND

YOU CAN CONTINUE APPROACH OR TAKE OFF AND INHIBIT SWITCH INHIBIT

IF THE  ALTITUDE IS ABOVE 10,000 FT

OUTSIDE AIR TEMPERATURES LESS THAN -40 DEGREES

GROSS WEIGHT IS GREATER THAN MAXIMUM LANDING WEIGHT

NOTAMS SHORTENS RUNWAY

*RUNWAY INHIBIT SWITCH
INHIBIT SWITCH BACK TO NORM
AFTER TAKEOFF OR  BEFORE LANDING

*YOU GOT A "SHORT RUNWAY" CALL OUT ON TAKE OFF WITH PATTY IT'S ADVISORY ONLY

DO NOT USE RAAS FOR

NAVIGATION
OR
A SUBSTITUTE FOR NOTAMS OR ATIS

MINIMUM FUEL REQUIRED FOR A HYDRAULIC PUMP COOLING

760 KGS IN THE RELATED MAIN TANK

cockpit companion says only if fuel in tank  1 is below 760kg do not operate any pump

MAX FUEL TANK TEMPERATURE

49°

MINIMUM FUEL TANK TEMPERATURE

-43 OR 3° ABOVE THE FUEL FREEZING POINT TEMPERATURE WHICHEVER IS HIGHER

-47 is jet A1 freezing point
so -43

-40 is jet A freezing point
so -37

INTENTIONAL DRY RUNNING OF A CENTER TANK PUMP IS

PROHIBITED

after 10 seconds the of low pressure light illuminated steady the master caution light will illuminate. 5 seconds later the pumps will automatically shut off. total 15 seconds of dry running pumps
cockpit companion

MAXIMUM FUEL IMBALANCE

453 KG

MAIN TANKS 1AND 2 MUST BE FULL IF

CENTER TANK CONTAINS MORE THAN 453 KG

VMO

340 IAS

.82 M

FLAP PLACARD SPEEDS

1, 2, 5 - 250 kias

10 - 210 kias

15 - 200 kias

25 - 190 kias

30 - 175 kias

40 -162 kias

Alternate Flap System - 230 kias

LANDING GEAR PLACARD SPEEDS
( VLO ) (VLE)

Retract...235 kias

Extend...270 kias/.82M

Extended...320 kias/.82M

Note: Verify Ldg Gear Limit (IAS) on the placard under Ldg Gear Lever during normal operations

MAX ALLOWABLE CABIN DIFF FOR TAKEOFF LANDING

.125 psi (236 feet below airport pressure altitude)

EGT LIMITS FOR STARTING
MAX CONTINIOUS
TAKE OFF

Takeoff...................1038C      5 min limit

Max Continuous......1013C

Starting...................753C

STARTER DUTY CYCLE

MAX
3 MINUTES ON 10 SECONDS OFF

EXTENDED ENGINE MOTORING LIMITED TO 5 MINUTES ON 5 MINUTES OFF 5 MINUTES ON 5 MINUTES OFF 5 MINUTES ON EACH ONE AFTER 10 MINUTES OFF

NG
2 MINUTES ON 10 SECONDS OFF

EXTENDED ENGINE MOTORING
15 MINUTES ON 2 MINUTES OFF
15 MINUTES ON 2 MINUTES OFF
5 MINUTES ON 10 MINUTES OFF

THREE SITUATIONS WHERE CENTER TANK FUEL PUMP SHOULD BE TURNED OFF ON THE GROUND

When no personnel are available on the flight deck to
monitor the low pressure lights

Center tank quantity not greater than 453kg (unless defueling or transferring)

when the low pressure lights illuminate (both off if quantity zero)

HYDRAULIC SYSTEM A

A REAL GIANT P

AUTOPILOT A

RUDDER ELEVATOR AILERON

LANDING GEAR

GROUND SPOILERS

CERTAIN FLIGHT SPOILERS

ALTERNATE BRAKES

NOSE WHEEL STEERING NORMAL

THRUST REVERSERS NORMAL

POWER TRANSFER UNIT

HYDRAULIC SYSTEM B

B REAL TOY BAAT L

AUTOPILOT B

RUDDER ELEVATOR AILERON

LEADING EDGE DEVICES NORMAL

TRAILING EDGE FLAPS NORMAL

CERTAIN FLIGHT SPOILERS

YAW DAMPER

BRAKES NORMAL

AUTO SLATS

ALTERNATE NOSE WHEEL STEERING

THRUST REVERSER

LANDING GEAR TRANSFER UNIT

WAKE TURBULENCE LIMITATIONS

737 IS  A MEDIUM

FOR DEPARTURE

2 MINUTES BEHIND A HEAVY
 
3 MINUTES BEHIND A SUPER HEAVY

FOR LANDING

3 MILES BEHIND MEDIUM

5 MI BEHIND A HEAVY

7 MI BEHIND A SUPER HEAVY

remember 23 357 Jordan holding a magnum
wake turbulence descends 300 to 500 ft per minute

land after the touchdown point
and
take off before it's rotate point

AERODROME LIGHTING

if runway has ILS the last 2,000 ft of runway Edge lighting turn Amber or last half the runway whichever is less

centerline lighting white until the last 3,000 ft. they will alternate red and white. then the last 1000 ft will be red

if the runway is displaced red and white runway Edge lights will be installed in that area this area is suitable for takeoff not for landing

high speed taxi alternating green and yellow
airdrome code 1 and 2
30knots or 65 kph
airdrome code 3 and 4
50 knots or 93kph
code 3 are runways less than 5,500 ft code 4 runways 5,500 feet or more

eye to wheel height for Boeing 737 is 13-16 ft
on the taxi: take off minimums page

high speed taxiway turn off
you can call down and clear with low visibility when you were 200 ft off the taxiway. you will know this when your nose is 4 solid green lights off the high speed tax anyway not the yellow and green

TO/GA

one click is reduced go around thrust is 10% below Max thrust the green cursors gives a climb rate of 1,000 to 2,000 ft per minute

two button presses gives you Max  thrust and is mainly used when terrain separation is doubtful

AIR SYSTEM SWITCHES

IF GROUND AIR IS CONNECTED PACKS MUST BE IN THE OFF POSITION

IF DURING A PUSHBACK AND AN ENGINE STARTS CAPTAIN WANTS THE AIR ON MAKE SURE TO CLOSE THE ISOLATION VALVE SO THE ENGINE ISN'T ROBBING ENERGY FROM THE ENGINE THAT NEEDS TO START

WHEN SHUTTING DOWN ONE ENGINE TAXING BACK CONSIDERATION SHOULD BE MADE TO SHUTTING DOWN THE NUMBER ONE ENGINE SO PASSENGERS IN THE BACK HAVE  CONDITIONED AIR

ONE ENGINE CAN ONLY SUPPLY ONE PACK IF SHUTTING DOWN ONE ENGINE TAXING BACK TURN THE PACK OFF??

SERIAL NUMBER OR TABULATION NUMBER IF LISTED IN A QRH ACTION
AND EQUIPMENT REQUIRED FOR AN APPROACH

SERIAL AND TABULATION NUMBERS ARE FOUND ABOUT 5 PAGES PAST THE FIRST PAGE OF THE PERFORMANCE IN FLIGHT SECTION OF THE QRH OR 1ST PG OF CHECKLIST INSTRUCTIONS SECTION QRH or
beginning of FCOM 1

AIRCRAFT EQUIPMENT REQUIRED IS FOUND FIRST PAGE OF OPERATIONAL INFORMATION IN QRH

NEGATIVE PRESSURE RELIEF VALVE OPENS AT

SAFETY RELIEF VALVE'S
LIMITS THE MAX PRESSURE DIFF TO

WHEN OUTSIDE PRESSURE IS 1 PSI MORE THAN INSIDE

SAFEY RELIEF VALVE
9.1 PSI

CROSS WIND TAKE OFF CONTROL WHEEL INPUTS

WHEN ABOVE 20KTS CROSS
OR
10KT TAILWIND

START ROLL WITH NO INPUT INCREASING CONTROL INPUT WITH SPEED INCREASE.

DONT GO OVER 7 °  BANK OR SPOILER WILL DEPLOY

HOLD RUDDER AND CONTROL INPUT UNTILL RIGHT AFTER ROTATION SLOWLY RELEASING

I KINDA REMEMBER
PUT FULL INPUTS WHEN LANDING

MASTER CAUTION

IN AIR  IF RECALL HAS LIGHT QRH DOESNT NEED TO ACTIONED
the system has a back up

ON GROUND IF MASTER CAUTION OR RECALL THEN PULL QRH and MEL THEY HAVE TO BE ACTIONED

PRIOR TO START  APPERENTLY NO QRH OR MEL.

THE HIGHEST LIGHT ILLUMITAED IS THE PRIORITY ON THAT SYS PANEL

CAN YOU CHANGE POWER SOURCE WHILE RE FUELING

FROM APU TO GPU TO BATTERIES

NO

EMERGENCY EQUIPMENT IN FLIGHT DECK

4 CREW LIFE VESTS
1FIRE AXE
1HELLOTRON FIRE EXTINGUISHER 1PAIR OF PROTECTIVE GLOVES
2 FLASHLIGHTS
1 PBE
4 CREW MEMBER OXYGEN MASKS
4 SMOKE GOGGLES

STATIC DISCHARGE WICK S

22 total installed
- three can be missing with no penalty

-there are four on the winglets none can be missing

-when there is only two on the horizontal or vertical stab the outer most tip must be there

STEADY STREAM OUT OF DRAINS ON and AFTER STARTUP

CONTINUE THE START

RUN ENGINE AT IDLE THRUST FOR UP TO 5 MINUTES
OR

SHUT DOWN ENGINE CONTACT MAINTENANCE
OR

SHUT DOWN ENGINE RESTART AND RUN IDLE THRUST FOR UP TO 5 MINUTES

ON THE WALK AROUND IF ANY FLUID IS A STEADY STREAM GET MAINTENANCE

TAXI SPEEDS

20 knots normal

30 knots on straightaways

10 knots on turns

CONSIDER PUTTING IGNITIONS TO BOTH ON STARTUP WHEN

GROUND ELEVATION IS ABOVE 2,000 FT

TEMPERATURES BELOW + 5

AND FIRST START OF THE DAY

FMC TRICKS

CROSS TRACK
OFF SET ON ROUTE PG
and init ref ident
you cannot set a cross track when on a vector after takeoff

RTA
ON CRUISE PG
WILL GET YOU TO A POSITION AT A CERTIN TIME

BEST RATE = TIME
BEST ANGLE = DISTANCE
cockpit companion FMC guide says best angle is really best rate
CRUISE PG

fixradial/distance
birla180/20 or -20

RVR TAKEOFF 600

CARVIT

ONLY CAPTAIN CAN DO
1200 RVR AND OR 600 RVR

- ONE ENGINE CLIMB GRADIENT IS SUFFICIENT FOR OBSTACAL
CLEARENCE ON DEPARTURE END OF RUNWAY
35ft above departure end/400ft before turning/200fpnm

-ALTERNATE. TAKEOFF ALTERNATE WITH IN 1 HOUR SINGLE ENGINE CRUISE 430NM SPECIFIED ON FLIGHT PLAN

-RUNWAY HAS SERVICABLE HIGH INTENSITY LIGHTS/EDGE
*AND*
CENTER LINE LIGHTS
*AND*
CENTERLINE MARKINGS VISABLE THROUGHOUT THE TAKE OFF ROLL.

1200RVR BECOMES *OR*

2 RVR SENSORS OR 3 CENTER CAN BE U/S

-VISABILITY 3 RUNWAY LIGHTS
OR 6

-INSTRUMENT WARNING SYSTEM TO DETECT INSTRUMATION FAILURE
AN ATTITUDE INDICATOR
INCORPORATES PITCH ATTITUDE INDEX LINES REFERENCE TO AT LEAST 15°

-TRAINING/WE GET TRAINING CERTIFICATION IN TRAINING FILE
100 HRS PIC ON TYPE

-RUNWAY HAS TO BE APPROVED FOR LVOP IN CAP GEN OR JEPP PLATE

YOU KNOW YOU ARE TRULY CLEAR OF THE RUNWAY WHEN YOUR NOSE  HAS GONE FOUR SOLID GREEN TAXI LIGHTS IN OFF THE HIGH SPEED TAXI WAY

WHAT CATAGORY IS NG AND THE MAX

CATEGORY A <90
CATEGORY B 91-120
CATEGORIE C 121-140
CATEGORY D 141-165
CATEGORY E +165

ON APPROACH

NG IS CAT C for flap 40
D for flap 30

MAX IS CAT D

NO FLIGHT IN WHAT KIND OF ICEING CONDITIONS

FREEZING FOG, FREEZING DRIZZLE, SLD FREEZING RAIN

DONT KNOW WHY BUT CANT FIND THIS ANYMORE

THESE ABBREVIATIONS ARE IN THE COM BUT NOT SAYING YOU CAN'T FLY IN IT

RVSM REQUIREMENTS

-2 INDEPENDENT ALT MEASURING SYSTEMS

-1 SECONDARY SURVEILLANCE RADAR TRANSPONDER

-1 ALT ALERTING SYSTEM

-1 AUTOMATIC CONTROL SYSTEM
(autopilot)

Min crew oxygen

2 crew 500 psi

3 crew 700 psi

found in MEL

WHEN DOING WINDSHEER OPT CALCULATIONS YOU WILL GET 2  SPEED VALUES

PUT THE WHITE VALUE IN FMC

WRITE DOWN YELLOW AND BRIEF

ROTATE WILL BE THIS YELLOW NUMBER ONLY USE MENTALLY
DO NOT BUG

APU TURN OFF ONLY AFTER

GPU SWITCH HAS BEEN TURNED ON

leave aircraft with APU running if
maintenance or other crew is there

IF gpu is on
and after secure checklist is complete
you can turn off APU bleed air
PACKS OFF 1 MIN
APU OFF
FUEL PUMP OFF
then
leave batteries on , if gpu is unplugged there will be a loud alarm outside and ground staff should reattache

OR IF NO MAINTENANCE OR CREW THEN
secure checklist
APU BLEED OFF
PACKS OFF 1 MIN
APU OFF
FUEL PUMP
after 5 minutes APU cool down period
hold switch at fa PANNEL
GPU off

RECALCULATE  OPT WEIGHT AND BALANCE WHEN

NEW FLIGHT PLAN WHEN

ANY WEIGHT ABOVE ZERO FUEL WEIGHT OR MORE THAN 500 KG BELOW

FO WILL ALWAYS RECALCULATE AND GIVE ZERO FUEL WEIGHT AND NEW
C OF G

NEW FLIGHT PLAN IF OVER 2000KG GROSS WEIGHT FROM FLIGHT PLAN
it will result in grater fuel burn
OR
1 HOUR OVER LAST FLIGHT PLAN
OR
ANY CHANGES TO ROUTE

IRS

FULL ALIGNMENT
IS RECOMENDED
OFF THEN NAV
YAW DAMPER WILL TURN OFF AND ERROR MESSAGES ON DISPLAY UNITS

FAST REALIGNMENT
IRS MODE SELECTORS
ALIGN
CDU ENTER PRESENT POSITION
THEN IRS SELECTOR NAV

AIR SPEED INDICATOR

-HIGH SPEED BARBER POLE-
VMO
MAX LANDING GEAR SPEED
FLAP PLACARD SPEED

-MAGENTA SPEED BAND-
V NAV SPEED BAND
bottom range auto throttle wake up
top range v NAV path changes to v NAV speed
alt constraints are both respected in VNAV path and speed

-LOW AMBER BAND-
MANOUVER SPEED
1.3 G'S 40° bank below 20000 ft
to shaker

ABOVE 20000
low speed Buffett
you will hear call out "air speed low"
then stick shaker

if ATC says slow down go at least ten kts above this speed

-LOW SPEED BARBER POLE-
TOP END STICK SHAKER

-TOP AMBER BAND-
NEXT FLAP SPEED RANGE
NORMAL SEQUENCE
1,5,15,30,40
YOU CAN FLY IN THIS RANGE JUST DONT SELECT NEXT FLAP WHILE IN IT

WHAT SIDE SHOULD IGNITION BE STARTED ON FIRST FLIGHT OF DAY

SELECT RIGHT SIDE IF IT FAILS IT CAN BE MEL'D LEFT SIDE CAN'T

EXTERNAL AIR CART
USED FOR STARTING

BATTERY SWITCH ON

RECIRC AUTO
PACKS AUTO
ISO OPEN

ONLY THING REALLY DIFFERENT IS *APU BLEED IS OFF*

cabin temp selectors set

if external air can't hold 20 psi and APU is on then
-ISO auto
-APU BLEED on

APU will supply left cart will supply right

CONTAMINATED RUNWAY
depth and type

TAKEOFFS ARE NOT *RECOMMENDED*
WHEN SLUSH, WET SNOW, STANDING WATER DEPTH IS MORE THAN 1/2 IN (13MM), OR DRY SNOW IS MORE THAN 4 IN (102MM)

FCOM 1 supplementary procedures adverse westher

FLAP AREA SHOULD BE CHECKED WHEN

FLYING IN ICING CONDITIONS AND VISABLE ICE IS ON AIRCRAFT DONT RETRACT FLAPS PAST 15 UNTILL INSPECTED.

IF YOU WANT THE E AND E BAYS HEATED AFTER SHUT DOWN

THERE IS A SUPPLEMTAL PROCEDURE FOR THIS IN F COM 1

HOT WEATHER OPS YOU CAN COOL DOWN THE CABIN THE MOST BY

USING APU BLEED AIR
not air cart
turning down all electrics and screens
FOLLOW PROCEDURE IN F COM IF NECESSARY

SANDY OR DUSTY OPS

THERE'S MANY PROCEDURES
FOUND IN FCOM 1 SUPPLEMTAL

OPTIMUM ALT AND MAX ALT

(T) is thrust limited, purpose is turbulence at that Altitude, you won't have enough to re climb up so says Brendon from ykf
I think you won't climb higher due to thrust is maxed out. no room to get more power =stuck at that alt

(B) is Buffet limited any higher and you'd get too close to high speed Buffet. not sure if low speed Buffett is thought of when (B) is displayed

skybrarry says
 the altitude at which a 1.3g loading from turning, manoeuvring or turbulence may be experienced without encountering buffet associated with either low speed stall or Mach stall 

FMC LANDING G's

FMC /ACARS/--------
USE THE THIRD ONE
AMCS

DISPLAY DATA

SELECT MNNONIC PG

SCRATCH PAD VACMAXL

SELECT ANY OF THE LEFT BUTTONS

ANY THING MORE THAN 1.9 CALL MAINT MORE THAN 2.1 WRITE IN BOOK

TRANSMITT BUTTONS YOLK

UP IS TRANSMIT TO ATC

DOWN IS INT TALK DURING RAPID DECENT

IF TEMP IS LOWER THAN THE UN COMP BARO V NAV

THEN DONT USE  THE RNP Y  ,

or the
L NAV /V NAV

USE JUST L NAV add 50 to MDA

X PONDER WHEN PUSH BACK REQUIRED ON DIFFERENT KIND OF TRANSPONDER IS

ALT ON

In the FCOM 1

V REF WIND ADDITIVE

half the headwind off opt you can cut this number down depending on degrees crosswind

all the gusts no matter the degrees

don't apply any tailwind keep it 5 knots

maximum of 15 kts tailwind

IF PLANE DOESNT TURN WHEN GIVEN A VECTOR IN HDG SELECT
NO IDEA WHY

SELECT CWS
OR
DISENGAGE HDG RE ENGAGE
OR
DIESSENGAGE AUTOPILOT

TOUCHDOWN ZONE MARKINGS

runways that are 4000 to 7900 ft will have a big touchdown zone marking at 1000 feet.
touchdown zone is 2000ft

runways longer than 7,900 ft will have big touchdowns on markings at 1315 ft , next will be at 2000 ,2500 and 3000 ft.
touchdown zone is 3000ft

if performing an ILS fly the glide slope to touch down. do not utilize the VASI, it does not recommended it due to eye wheel height issues

this is in the line check guide for first edition email sent by Gray

APU START RECEOMENDED ALT

25000ft
(QRH loss of both generators)

MVA

MINIMUM VECTOR ALTITUDE

over the Rockies 14000ft

DURING COLD WEATHER OPERATIONS AFTER THE PRELIMINARY CHECKLIST
FO

TURN PROB HEATS ON

THIS IS DURING COLD WEATHER OPERATIONS DEFINED IN THE SUPPLEMENTARY PROCEDURE FIRST PAGE ADVERSE WEATHER
LOW TEMPERATURES, ICE, SNOW, SLUSH, STANDING WATER ON THE AIR PLANE RAMP TAXIWAY
OR
DURING ICEING CONDITIONS

FMA MODES THAT DIDNT WORK ON SIM AT HOME FROM CBT

CWS pitch didn't alt aquire and alt hold when selected a different alt and still in CMD

with flight directors off on the takeoff roll I could not engage toga through 80 knots
CBT said you could

TOBT
TTOT

Target OFF BLOCK TIME
Target TAKE OFF TIME

ILS CAT II WIND CORRECTION TO VREF

NO CORRECTION

KEEP IT ONLY 5KTS EVEN WITH GUSTS, TAILWIND, OR HEADWINDS

APU AND GPU AND CONDITIONED AIR RULES

START A TIMER AFTER BOTH ENGINES ARE SHUT DOWN APU SHOULD BE SHUT DOWN 5 MINUTES AFTER ENGINE SHUT DOWN

WHEN TEMP IS BELOW 5 AND ABOVE 20 REQUEST CONDITIONED AIR

AFTER SHUTDOWN CHECKLIST CONTACT RAMP STAFF REQUESTING GPU AND PRECONDITIONED AIR

FCOM 1 APU GROUND USAGE

THERE IS A TANKERING FLOW CHART IN COMPANY MEMOS BULLETIN 23-001

FIRST MEMO IN 2023

DANGEROUS GOOD UNUSUAL ITEMS KNOWLEDGE

DO NOT ACCEPT OXYGEN CYLINDERS
ONLY PORTABLE OXYGEN CONCENTRATORS

COM 3.47.1

BATTERY OPERATED WHEELCHAIR NOT PERMITTED IN THE CABIN AS CARRY ON. THE LOADING OF POWERED WHEELCHAIRS IS PERMITTED AS CHECK BAGGAGE BUT SUBJECT TO RESTRICTIONS

NON-SPILLABLE AND APPROPRIATE WET CELL BATTERIES MUST BE CARRIED IN THE CARGO COMPARTMENT ALONG WITH THE WHEELCHAIR

WHEELCHAIRS WITH LITHIUM ION BATTERIES MUST BE REMOVED FROM WHEELCHAIR AND CARRIED IN THE PASSENGER CABIN WITH THE PASSENGER
MEMO FLE23-010 REV1
MEMO FLE23-006

CBs TRIPED

TRIPPED CB SHALL NOT BE RESET UNLESS CAPTAIN DEEMS NECESSARY FOR SAFETY

NO FUEL PUMP/ FUEL QUANTITY RESETTING EVER

YOU CAN RE- SET ON GROUND AFTER MAINTENANCE WAS CONSULTED 

AFTER A CB HAS TRIPED A 2 MINUTE COOL DOWN PERIOD IS REQUIRED

NOSE WHEEL DEFLECTION

7° rudder only
78° tiller

DESCENT RATES IN DIFFERENT CONFIGURATIONS

IDLE THRUST 250 KNOTS VERTICAL SPEED 1300 FT PER MINUTE

IDLE THRUST 250 KNOTS/
SPEED BREAK
VERTICAL SPEED 1800 FT PER MINUTE

IDLE THRUST  220 KNOTS FLAP 5 SPEED BRAKE
VERTICAL SPEED 2300 FT PER MINUTE

IDLE THRUST 180 KNOTS FLAP 10 SPEED BRAKE
VERTICAL SPEED 1500 FT PER MINUTE

JET FUEL FREEZING TEMPERATURE

JET A -40

JET A1 -47

JET B -60

THREE WAYS TO INCREASE YOUR TAT
descend or climb
deviate to a warmer air mass
increase Mach number

you can lose approximately 3° an hour
you should descend between 3000 - 5,000 ft
mach increase 0.1 results in .5° to .7°

AUTO THROTTLE KICKS OFF WHEN

THE OVERSPEED BY FOUR KNOTS

THERE IS NO OVERSPEED WARNING HORN FOR FLAPS
JUST FLAP OVER SPEED PROTECTION

LAV AND WATER

LAV TOTALY EMPTY

POTTABLE WATER 3/4 FULL MIN

TOUCH DOWN ZONE
AND
MARKINGS

OVER 7900FT RUNWAY
FIRST 3000FT OR 1/3RD
touchdown point big white pair is 1312ft

UNDER 7900
FIRST 2000FT OR 1/3RD
touchdown point big white pair is
1000ft

FOR RUNWAYS SHORTER THAN 6998 FT YOU MUST

CHECK FCOM 1 SHORT RUNWAY LANDING PROCEDURES

GOMEX

EQUIPMENT REQUIREMENTS
2 FMC
2 IRU
1 GPS
1 HF radio

IF EQUIPMENT FAILURE HAPPENS INFORM ATC NEGATIVE RNP 10

input rnp level 10 in page 4Prog

PRIOR TO WATERS PLUS ENTRY
give to ATC
entry point ETA
flight level
requested Mach number
(MACH NUMBER MUST BE MAINTAINED PRECISELY. PRIOR ATC APPROVAL MUST BE OBTAINED TO CHANGE IT)

when no VHF frequency has been assigned set number one VHF to 123.45 and number two VHF to 121.5

DECELERATING STRIGT AND LEVEL

FROM 280KTS-250KTS
30 SECONDS
2.5 MILES

FROM 250-200
55 SECONDS
4 MILES

YOU WILL DECEND 1000FT IN 3 NM

SPEED BRAKE CUTS THOES TIMES/DISTANCES IN HALF

FAA SPEED LIMIT ORDER

BELOW 200 KNOTS
WHEN BELOW 2500 FEET
WITHIN 4NM

WING ANTI ICE MAX ALT

350000ft
FCOM 1

FUEL BURN ON THE GROUND PER HOUR

300 KILO PER HOUR per engine

600 PER HOUR 2 ENGINES

so for Marcello 600 KG extra would be 1 HOUR for EXTRA  fuel
sitting on apron
or
2 hours single engine
or
3 hours WITH  APU

PROBABLY 700 PER HOUR FOR NG

WEATHER RADAR HATCHED LINES AND ⚡

SOLID WEATHER IS +-4000FT
HATCHED WEATHER IS BELOW 4000FT

HAIL AND LIGHTINING PREDICTION  BY THE WEATHER RADAR IS JUST A PREDICTION WITH THE INFO IT HAS NOT A LIGHTNING DETECTOR

FA LIFE VEST BRIEF MUST BE MADE WHEN

50NM FROM SHORE

MEXICO SPEED GREATER THAN 250

CANADIAN AIM
PG 197 RUEL OF THE AIR
CANNOT REQUEQEST HIGH SPEED CLIMB

YOU NEED A SPECIAL CERTIFICATE
OR FOR OPERATIONAL REASONS MIN SAFETY SPEED