B757 B767 Misc

Front 1

B757 Flap Speed Limits

Back 1

1...........................240
5...........................220
15..........................210
20..........................195
25..........................190
30..........................162

Front 2

B767 Flap Speed Limits

Back 2

1...........................250
5...........................230
15..........................210
20..........................210
25..........................180
30..........................170

Front 3

UPS is approved to use the B757/767 FMC for enroute and terminal RNAV operations, but not
_______________.

Back 3

RNAV approaches

Front 4

RNP stands for:

Back 4

Required Navigation Performance (RNP)

Front 5

RNAV1

Back 5

Crosstrack error/deviation should be limited to 0.5 NM

Front 6

RNAV2

Back 6

Crosstrack error/deviation should be limited to 1 NM

Front 7

Required Equipment for RNP

Back 7

1FMCandCDU
1 VOR and 2 DME receivers
1 IRU in the NAV mode
1autopilotorflight director and the AFDS LNAV mode
2 map displays (can be from the same FMC)
GPS or DME/DME/IRU with updating
Current nav database

Front 8

The B757 and B767 are not authorized to fly Q routes in ____________ and RNAV routes in ____________ ?

Back 8

Gulf of Mexico

Alaska

Front 9

Engine Anti-ice is required when

Back 9

Engine Anti-Ice –10°TAT
Engine anti-ice must be on during all
ground and flight operations when icing
conditions exist or are anticipated

except during climb and cruise when
the temperature is below –40°C SAT

Front 10

NON PRECISION APPROACH
configure when?

Back 10

NON PRECISION APPROACH

4. 4 miles GEAR DOWN flaps 20

2. 2 miles flaps 30 ldg chk list

1. 1 mile walk the panel

Front 11

The ASA monitors what?

Back 11

ASA

F -FCCs
I -ILS Receivers
I -IRS’s
R -Radar Altimeter
E -Electrical System
S -Auto-pilot
OR FIIREP like pirep

Front 12

ASA when tells you what on the top and bottom?

Back 12

What you can do.


What you can't do.

Front 13

CAT II, III AUTO-BRAKE CHART

Back 13

CAT II, III AUTO-BRAKE CHART

Easy to misread.
G/S intercept runway length needs to
Be longer than the number in the briefing guide

ie: 35R in SDF needs MAX auto-brakes

Front 14

03.04.09.03
WEATHER REQUIREMENTS FOR Departure ALTERNATE

Back 14

03.04.09.03
WEATHER REQUIREMENTS FOR Departure ALTERNATE

WX is below CAT I mins

The alternate needs to be:

Within 1 hour or
Within 300 nm

Front 15

Destination Alternate forecast WX mins vs
destination

Back 15

Destination Alternate
Unlike, at a destination, both ceiling and visibility must be forecast at the alternate ETA to be at least as good as that derived from the following:

Front 16

03.04.05.01
FLIGHT DIRECTOR AND AUTO COUPLER POLICY

Back 16

03.04.05.01 FLIGHT DIRECTOR AND AUTO COUPLER POLICY
Do not
dispatch an aircraft to a destination
forecast to be below 3/4 statute mile visibility or RVR 4000 unless the aircraft has either
(a) operable dual flight director systems or
(b) one operable flight director and an operable auto coupler.

A single flight director with dual display does not satisfy this requirement.

Front 17

PW start procedure

Back 17

PW 18% N2 min
position fuel control switch to RUN at maximum motoring:
Oil pressure rise:
(757) Prior to selecting RUN
EGT rise:
Within 20 seconds after selecting RUN/RICH
N1 Indication:
(PW) At EGT rise.
(PW) engine reaches stabilized
idle within 90 seconds after
selecting RUN

Front 18

RR start procedure

Back 18

RR 25% N3
Position fuel control switch to RUN at max motoring:
Oil pressure rise:
(757) Prior to selecting RUN
EGT rise:
Within 20 seconds after selecting RUN/RICH
N1 Indication:
(RR) Prior to selecting RUN

Front 19

GE start procedure

Back 19

767 15% N2
Position fuel control switch to RUN at max motoring:
Oil pressure rise:
(767) Prior to stabilized IDLE
EGT rise:
Within 20 seconds after selecting RUN/RICH
N1 Indication:
(767) Within 30 seconds after N2
stabilized at IDLE

Front 20

IRS
What information does it give us?

Back 20

HATSWAP
Heading
Accleration
Track
Speed
Wind
Attitude
Position

Front 21

IRS
What instruments does it give information to?

Back 21

IAFWY
4 I: VSI HSI RDMI ADI
3 A: brake Accel, AntiSkid,
ASA
2 F: FCC FMC
W WX Radar
Y Yaw

Front 22

IRS
What can cause it to flash?

Back 22

no bad moves, faults
no input position.
bad position input,
the aircraft is move or
faults

Front 23

IRS's, on battery power for the 757 what lives and dies?

Back 23

757
L and C die after 5 minutes
R remains

Front 24

IRS's, on battery power for the 767 what lives and dies?

Back 24

767
L and C live and
R dies after 5 minutes

Front 25

Fire Protection
SYS-Fail Switch/Light

Back 25

Is a press to test and
also
a reset like the Master Caution to be ready to warn of another failure

Front 26

What happens when you move the gear handle down.

Back 26

Press is provided to the actuators
Releases door uplocks
light comes on
Releases gear uplocks
light comes on
extends gear

Front 27

What do you see when gear extension is successful.

Back 27

3 green and doors and gear lights are off

Front 28

What happens when you move the gear handle up.

Back 28

Pressure is provided to the up acutuators
Door and gear lights come on
then off after uplocks are engaged

Front 29

How many gear position indicators are there?

Back 29

2 which are redundant

Front 30

TRACTALL

Back 30

Thrust
Region
Airspeed Bugs
Climb Restriction
Trim
Apu
Level Off
Log Book

Front 31

B757 Which hydraulics power what brake systems?

Back 31

L---Alternate
C---Nothing
R---Normal-Reserve-Accum

Front 32

B767 Which hydraulics power what brake systems?

Back 32

L---nothing
C---Alternate-Reserve
R---Normal-Accumulator

Front 33

The Reserve Brake switch does what?

Back 33

Turns on the electric hyd pump.

Front 34

B757 and B767 Which hydraulics power what brake systems? (stated in another way.

Back 34

Right-Normal
Right-Accumulator
Standpipe-Reserve
Heavy-Alt

Front 35

How do you establish crew communication?

Back 35

Put on oxygen mask
Switch from boom to mask
Switch on speaker
talk to the other and thumbs up

Front 36

ATM bucks

Back 36

Altimeter
Tailwind
MELS
Bleeds

Front 37

Before top of descent

Back 37

A-
I-install approach
R-Radios
B-Brief
A-Approach Check List
G-Go around Brief

Front 38

Reserve fuel input on preflight

Back 38

Domestic Rules
• Enter alternate + reserves
International Rules
• (B757) alternate + 6000 lbs
• (B767) alternate + 8000 lbs

Front 39

Pilots must not fly an RNAV procedure unless

Back 39

Pilots must not fly an RNAV procedure unless it is retrievable by procedure name from the
FMC database and conforms to the charted procedure.

Front 40

Some approaches restrict the use of DA with the statement in the Jeppesen Briefing Strip: “For
uncompensated Baro-VNAV systems, LNAV/VNAV not authorized below -15C or above 48C.” All
B767 aircraft have ____?

Back 40

uncompensated Baro-VNAV systems

Front 41

To avoid unnecessary RAs:

Back 41

vertical speed should be reduced to 1000 FPM when within 2000
feet of a level off altitude.

Front 42

The PF must respond immediately to satisfy corrective RAs by:

Back 42

disconnecting autopilot and
autothrottles and using positive control inputs in the direction and magnitude TCAS advises.
Attempt to visually acquire the conflicting traffic while complying with the RA.

Front 43

The TCAS mode selector should be selected to TA ONLY during the following situations:

Back 43

• If one engine is inoperative
• If takingoff or landing at an
airport elevation above
5300 feet MSL
• During operations beyond
ISA +/-27.8°C (50°F)
• When required by the MEL
or Non-Normal procedure

Front 44

GO-AROUND PROCEDURE

Back 44

Push G-A switch and call
“Go-around thrust Flaps 20.”
pos rate
gear up

Front 45

Single Eng Go around

Back 45

Push G-A switch and call

“Go-around thrust Flaps 5.”

Front 46

How many ground carts are required for engine start

Back 46

2
3 on the RR during severe cold

Front 47

APU pneumatic output is controlled barometrically.
How and when?

Back 47

In climb it shuts off air at 23000.
In descent it restores air at 20000.