B757 - ALL Flashcards
This deck was created by combining two or more decks (157 cards)
0
Q
Pack “High Flow” inhibited
A
One engine supplying bleed air AND wing A/I ON
Engine Inop
Flaps > 1
Aft cargo fire Sys armed
1
Q
Trim Air (off or Inop.)
Air temps (selectable)
A
A average
N constant moderate
W warm
2
Q
EICAS inhibits
A
Inhibits aural & Master Caution
Caution @ 80 kts.
Warning @ Rotation
3
Q
Flight instrument transfer buses
A
Capt. instruments normally on L. AC bus
F/O. instruments normally on R. AC bus
w/ Bus Ties in AUTO - flight instruments will auto transfer to opposite main AC bus w/ main AC bus failure.
4
Q
Cancel APP (approach mode)
A
Push G/A switch
OR
Disengage A/P & turn OFF both F/D’s
(to abandon approach, can put G/A switch & immediately press ALT HOLD)
5
Q
Hydraulics System powers…(L. C. R.)
A
LEFT - CENTER - RIGHT -
A/P A/P A/P
Flight controls Flight controls Flight controls
Left T/R Right T/R
FSSG (flaps, slats,
nose steering, gear)
Alternate brakes Normal brakes
Main cargo door
Rudder ratio
——————————————————————————––——————-
PTU RAT Reserve Brakes
6
Q
Flight Ops N. of 73° & S. of 60°
A
Night and/or IFR ops. prohibited if navaids are referenced to Magnetic North. (Must be referenced to TRUE).
7
Q
Lower cargo fire detection/protection
A
2 detectors each compartment FWD & AFT
Discharge #1 bottle first
Discharge #2 bottle after 50 minutes or during approach (whichever occurs first).
8
Q
APU start & shutdown
A
Battery ON
Stby power ON
APU switch on (fault light on then off)
APU switch START then ON
Shutdown OFF
APU bleed closes, 1 minute cool down then APU shuts down
(if putting airplane to bed, Stby OFF, then Bat OFF)
APU Starter duty - 3 starts in 60 min.
9
Q
Slats & Flaps
A
LEFT HYD Sys
2 Inboard
8 Outboard
Flaps 1-20 = slats at midrange position
Flaps 25-30 = slats at landing position
10
Q
Pressurization
A
Auto rate 500 fpm climb, 300 fpm descent
Max diff 8.6 @ FL350
Manual Outflow valve - Stby DC bus
Cabin warning stops below cabin alt. of 8500’
Outflow valve FULLY closed at cabin alt. of 11000’ (operational again at 9500’)
11
Q
Dimensions
A
Length - 155’ 6” (48 M)
Wing Span - 124’ 10” (38 M)
Height - 44’ 6” (14 M)
12
Q
R/L ENG HI STAGE (EICAS message) and “HI STAGE” annunciator
A
Over pressure condition exists. Bleed should auto close.
13
Q
GPWS limitations
A
Do not use if:
QFE ops.
IRS Nav only
Non WGS-84 reference
No FMS position update
14
Q
Cargo isolation switch - PRESSED
A
Turns off left recirc fan
Opens overboard exhaust valve
Closes main deck air distribution shut off valves
Closes trim air valve
Depressurizes main cargo deck compartment
NO FIRE PROTECTION
15
Q
IRU’s & alignment
A
3 IRU’s L., C., R.
10 minute alignment
17 min. alignment @ high latitudes
ALIGN lights extinguish when NAV is ready.
16
Q
Fuel control switches (Rich & Run)
A
Always motor engine during start until EGT < 100°C
If EGT = 0°C raise fuel control switch to RICH. When engine stabilized at idle, then raise sw. to RUN
If EGT > 0°C then raise to RUN
25% N3 - raise start lever during normal start
17
Q
Spoilers
A
6 panels on each wing
Uses all HYD Sys. (diff Sys to diff panels)
Speedbrake moves 5 panels on each wing
18
Q
Brake accumulator (# of applications)
A
Pressurized from RIGHT HYD system.
At least ONE (possibly more) brake application.
Use ONE steady application, do NOT pump brakes.
Normal antiskid.
19
Q
Forward E/E racks cooled from…
A
Exhaust from upper cargo deck
20
Q
Center Hydraulic #2 electric pump
A
Load shed feature
21
Q
R.A.T. (Ram Air Turbine)
A
Deploys automatically if both engines fail.
Airspeed 130 kts. or greater provides flight controls on center hydraulic system.
22
Q
Standby power distribution
A
- Standby instruments
- Instrument panel flood lights
- Left VHF radio
- Left VOR
23
Q
Antiskid annunciator comes on…
A
with partial power loss to antiskid system AND system malfunction.
24
Oil Pressure
2 sensors
- numerical value on EICAS
- < 18 psi gives low pressure annunciator
Main oil filter - NO BYPASS
Scavenge oil filter - YES bypass
25
Bleed air supplies...
...
Packs & pressurization
Wing Anti-ice
Engine start
Hyd reservoirs
supplied by APU, engines, & external air cart
26
EMER EQUIP flight deck
Crash axe, fire gloves, chemical gloves, portable ELT, PBE, life vests, 1st aid kit, portable O2 bottle and mask, halon fire ext., haz mat exemption kit, full face O2 masks, escape ropes, flashlight, spare bulbs kit, landing gears pins, normal checklists and QRH.
27
Brake temp monitors
Values 1-9
Init. 0-2, cyan box & #
Norm. 3-4, white box & cyan #
High. 5-9, white box & #
10-15 min. to reach high temp after brake application
28
Autobrakes - Landing activation and disarm
After landing, autobrake application begins when:
Both thrust levers are retarded to idle, gear untilts, and the wheels have spun up.
AutoBrake - Disarm
Pedal braking applied.
Either thrust lever advanced after landing.
Speedbrake lever is moved from the full up position after the speed-brakes have deployed on the ground.
DISARM or OFF position selected on the AUTOBRAKES selector.
Autobrake fault.
Normal antiskid system fault.
29
TCAS alerts
TA - 35-40 sec. warning
RA - 20-30 sec. warning
Proximate traffic 6 nm and +/-1200'
30
Useable fuel
14.5 (L) + 46.0 (C) + 14.5 (R)
31
FRM - fault reporting manual
Used by flight crew to report system faults/malfunctions to Mx.
32
Nose wheel steering range
Rudder pedals - 7°
Tiller - 65°
180° turn in 120' (37M)
33
Brake system
4 total systems from both L & R Hyd Sys
- -Normal - R Sys
- -Alternate - L Sys
- -Reserve - R Sys
- -Accumulator
R Hyd Sys should ALWAYS be pressurized FIRST & depressurized LAST to prevent fluid transfer through brake Sys.
34
EICAS Takeoff configuration warnings
```
Flaps
Spoilers
Stab Trim
Parking Brake
Main Cargo Door
```
35
Utility bus load shedding
B.O.S.S.
Both throttles advanced on ground with APU running
Overload
Start engines
Single source of electrical power
36
APU fire handle PULLED
```
Fuel shutoff valve closes
Shuts down
Fire extinguisher armed
Generator breaker & field trips
Bleed valve closes
Exterior horn silenced
```
37
APU fault light
APU switch OFF, then ON.
If fault light extinguishes, the one attempted restart.
38
AUTO extend ground spoilers
Spoilers ARMED
Throttles IDLE
HYD pressure to tilt sensor detects A/C on ground
39
Flap load relief
Retracts the flaps from 30 to 25 is airspeed > 162 kts. (or prevents extension to 30)
40
Crew oxygen
1 bottle (separate from courier O2)
41
Fly course from PPOS
in scratchpad - "FIX150" ("FIX" is waypoint & 150 is intended course)
42
Creating Waypoints
PB/D
PB/PB
PD/+ or - mileage
LAT/LONG (no slash)
43
Auto & Manual ignition
T.I.L.T.
Takeoff
Icing
Landing
(Auto with slats/anti-ice)
Turbulence (Manually selected)
44
OFFSET
Lives in RTE
45
Center tank pumps (electrical load)
Pumps inhibited (when switched on) until respective engine start.
46
EICAS
Engine Indication and Crew Alert System
400 sensors
Left EICAS computer normally controls
TCAS
GPWS
System Alerts
47
Fuel pumps
2 in each tank
Center tank pumps output pressure is TWICE that of wing pumps
1 DC pump in left wing for APU. Left forward pump for APU on AC power.
48
```
Terrain Mapping (for NAV)
& Airport not in EGPWS database
```
```
Terrain Mapping (for NAV) - Prohibited
& Airport not in EGPWS database - Do not use within 15 NM for T/O, Approach, & Lndg.
```
49
Deploying reversers (effect on A/T & speedbrakes)
Disengages A/T
Deploys speedbrakes
Need to come out of Reverse starting @ 60 kts, and be fully out by taxi speed
50
Crew Alert Messaging
- Time critical warnings (red)
- Warnings (red)
- Cautions (amber)
- Advisories (amber & indented)
Top message is newest
11 messages displayed, then press CANCEL for next page
CANCEL removes Cautions & Advisories (NOT WARNINGS)
RECALL shows any canceled message
51
Brake accumulator isolation valve opens...
with total HYD system loss
52
Alternate brakes (hyd source & antiskid)
Transfer to LEFT HYD system automatically (shuttle valve) if right side hyd pressure is too low.
Antiskid is provided to laterally paired wheels so NO autobrakes.
53
FWD EQPT SMOKE
2 smoke sensors
Exhaust side downstream of left recirc fan
Supply side downstream of supply fans
AUTO ACTIONS (Smoke FWD exhaust duct)
left recirc fan shuts OFF (if slats are up)
left pack goes to HIGH flow
overboard exhaust valve latched open
54
P.T.U. (Power Transfer Unit)
If left engine fails or left hyd pressure is low
PTU (hyd motor - hyd pump) uses right hyd power to power left system
For (FSSG) flaps, slats, nose wheel steering, landing gear
55
FMC pre-flight
```
Ident
Pos init
Rte 1 (page 1&2)
DEP & ARR
PERF
T/O REF
```
56
Stall Warning - Auto slats
Upon receiving a signal from the stall warning system, the slats automatically extend from the midrange position to the fully extended landing position. The slats retract a few seconds after the signal is removed.
57
A/P power sources (electrical)
Normal
L & C Autopilot - left main bus
R Autopilot - right main bus
On approach (Autoland)
L Autopilot - left main bus
R Autopilot - right main bus
C Autopilot - Batt/Stby
58
Rolls Royce engines (RB211)
Dual channel EEC
N1 - Fan + 3 stage turbine (75% of thrust)
N2 - 6 compressors + 1 turbine
N3 - 6 compressors + 1 turbine (drives accessory section)
Reverses are HYD actuated.
59
Yaw damper Inop
Fault
IRU align
IRU off
60
Max. lateral fuel imbalance
1950 # - structural limit
61
Autobrakes (settings)
Landing 1, 2, 3, 4, MAX
ALL are decel rates. Max MANUAL is > Max AUTO
Takeoff - RTO
at > 85 kts. & both throttles to idle, then MAXIMUM braking applied (= to MAX MANUAL)
62
Engine bleed air supplied by...
Low thrust uses high pressure compressor section
High thrust uses low pressure compressor section
63
Equipment cooling
| - left recir fan fails
Overboard discharge valve auto opens
64
APU altitudes
Electrical - 42,000 '
Pneumatics (Bleed Air) - 17,000 '
65
Nose strut (compress/extension) - FLT vs. GND logic
Master Warning & Caution
Stall warning Sys
66
Hydraulic Sys RSVR light
Reservoir Qty or Head Pressure is LOW
67
Normal FMC descent path
```
Cruise alt. until T/D point (down to lowest alt. constraint)
Econ idle
Decel to 240 kts. @ 10,000'
240 to decel
Arrive at FAF @ 170 kts.
```
68
EGPWS aural alerts
"CAUTION TERRAIN" (solid amber) - 40-60 sec. warning
"TERRAIN TERRAIN PULL UP" (solid red) - 20-30 sec. warning
69
EICAS landing warnings
Below 800' & gear NOT down and locked AND throttles @ idle
OR
Landing Flaps selected
70
Bus Tie Ops (both in AUTO)
P, P, I
Prevents
Powers
Isolates
71
WINDSHEAR warning lights
1' to 1500' on climb out
1500' to 1' on descent
72
Forward Cargo warning light switch - PRESSED
```
Forward cargo heat fan shuts off
Recirc fan shuts off
Opens overboard exhaust valve
Both packs switch to high flow
Silences the fire bell
Disables the forward squib test function
```
73
Landing Gear (Hyd Sys & lever lock)
Left hyd Sys normal
Lever lock controlled by tilt.
74
SMOKE - FWD exhaust OR Supply ducts
EXHAUST
Left recirc fan off (if slats are up)
Left pack high flow
Overboard exhaust valve latched open
```
SUPPLY
Both supply fans shut off
OVHT light inhibited for 5 min.
Left recirc fan shuts off
BOTH packs high flow
Overboard exhaust valve latched open
(pushing ALT starts ALT supply fan)
```
75
ALT FLAPS
0°-20° in about 2 min.
Slats are fully extended at flaps 20 (with alt Sys)
76
Speedbrakes EXT (annunciator)
Speedbrakes extended below 800' AGL
or
Speedbrakes extended AND landing flaps extended
77
ADC inputs
2 ADC's
4 pitot probes
- -Capt. & left aux
- -F/O & right aux
- -Capt. static (x2)
- -F/O static (x2)
- -Capt. AOA
- -F/O AOA
- -TAT
78
Main cargo fire detection & annunciation
16 smoke detectors
```
Cargo fire alarm sounds
Master warning illuminates
Discreet fire warning illuminates
EICAS - MAIN CARGO FIRE
FWD, MID, AFT illuminates on smoke control panel
LED's illuminate on cargo electric unit
```
79
Center fuel tank - Weight restrictions
If actual fuel + ZFW is > MAX ZFW & CG limits are observed then,
Center Fuel Tank
80
Aft Cargo warning light switch - PRESSED
Turns off aft cargo heater and fan
Right pack switches to high flow
Silences fire bell
Disables aft squib test function
81
Rudder ratio fault
Rudder ratio changer on LEFT HYD Sys.
X-wind limit is 15 kts.
Avoid abrupt rudder input above 160 kts.
82
Reserve Brakes
RIGHT HYD system from electic pump and reserve fluid. Switched on when manually selected.
Used when LEFT & RIGHT HYD systems are both lost.
Normal antiskid on all 8 wheels.
83
Creating waypoints - multiple LAT/LONGS
W144-4
will show:
```
W144
W148
W152
W156
etc.
```
84
HYD "RF" (magenta)
Less than .75 gallons
85
Tie bus priority
"RAO"
Respective IDG
APU generator
Opposite Engine IDG
External power must be switched on manually
86
All GEN fail
30 min. of battery power to Stby. systems
```
Stby instruments
L. VHF
C. ILS
L. VOR
Stby. Engine indicators
Interphone
```
87
E.E.C. & E.L.C.
EEC - Electronic engine control
Provides EPR overboost protection.
ELC - Engine limiter control
Provides N1 overspeed protection.
88
Standby Power items
.357 (overhead, forward, pedestal)
3 overhead - right IRU, fuel indicators, manifold pressure
5 forward - Master warning, SEI, ESIS, landing gear green lights, Capt. marker beacon (audio)
7 pedestal - alt. stab trim, speed brakes, flap handle, fuel control switches, ENG/APU fire handles, left VHF, center ILS
89
Anti skid protection
Touchdown, hydroplaning, and locked wheel protection is provided.
90
EGPWS (red, yellow, green)
RED +2000'
YELLOW -500' to +2000'
GREEN -1000' to -500'
LT. GREEN -2000' to -1000'
91
Alt. Equipment cooling
Must be selected w/ annunciator "EQPT OVHT"
Means there was low flow on either supply side OR exhaust side.
92
R/L ENG BLEED VALVE (EICAS message) and "BLEED" annunciator
Overheat condition exists. Bleed air valve should auto close.
93
Reverse Thrust - Flight vs. Ground use
Ground use only
| Inflight use prohibited
94
G/A armed
Flaps extended
OR
G/S is captured
95
ALT gear extension
250 KIAS (.75M)
DC pump releases uplocks (power pack on HOT BAT BUS)
Fluid from supply lines to the DC pump
Gear free falls and locks
Gear doors stay open
96
Exterior Safety Check
W.F.N.G.
Wheels chocked
Flaps up
Nose gear tethered
Gear doors closed
97
I.S.S.P. - Instrument Source Select Panel
```
Flight Director
Nav. Selector
EFI
IRS
Air Data
DCP
```
EFI -----> S.I.R.
Symbol generator
ILS
Radio altimeter
98
Cancel APP (approach mode)
Push G/A switch
OR
Disengage A/P & turn OFF both F/D's
(to abandon approach, can put G/A switch & immediately press ALT HOLD)
99
V1 cut - Single engine climb out
```
Engine failure
Rotate -----> 12.5°
Positive rate
Gear up
@ 400' select roll mode (HDG or LNAV)
@ 1000' AFE
---V/S +200
---Set speed 180
---A/P on
---What's the problem?
---Phase ones
---FLCH 180
---Select and set Max continuous
```
QRH
After T/O checklist
100
Interior safety check
1. ARD check
2. Battery switch - ON
3. Standby power switch - AUTO
4. Hydraulic panel - Pumps OFF
5. Landing gear lever - DOWN
6. Alt. flaps - NORMAL
7. Flap handle - CHECK
8. Radar - TEST
101
Single engine approach and landing
Gear down
Flaps 20
Before landing checklist
Speed following
102
Single Engine Go Around
```
Go Around
Flaps 5
Positive rate
Gear up
Check missed approach altitude
@ 400' select roll mode (HDG or LNAV)
@ 1000' AFE
---Set speed 180
---Approaching 180, FLCH 180
---A/P on
---Select and set Max continuous
```
After T/O checklist
103
Max. Flap speeds
```
1 = 240 kts.
5 = 220 kts.
15 = 210 kts.
20 = 195 kts.
25 = 190 kts.
30 = 162 kts.
```
104
Starter duty cycle PW
2 min. ON - 0% N2
2 min. ON - 0% N2
2 min. ON - 0% N2 & 15 minutes cooling
or
4 min. ON & 15 minutes cooling
Normal re-engagement 0-20% N2
105
Max. Crosswind - Takeoff & Landing (braking FAIR/MEDIUM)
15 kts.
106
Max. Operating Altitude
42,000 ft. Pressure altitude
107
Dimensions -
Length -
Wingspan -
Height -
Gear width -
Dimensions -
Length - 155' 3" / 47.3M
Wingspan - 124' 10" / 38M
Height - 44' 6" / 13.6M
Gear width - 24' / 7.3M
108
Max. Crosswind - Single Engine
30 kts.
109
Starter duty cycle RR
2 min. ON - 0% N3
2 min. ON - 0% N3
2 min. ON - 0% N3 & 15 minutes cooling
or
4 min. ON & 15 minutes cooling
Normal re-engagement 0-20% N3
110
Max. Zero Fuel Weight
184,000 lbs.
111
Max. wind - All other doors
60 kts.
112
Single FMC during non-precision approach. One pilot...
Must have raw data displayed on PFD/ND no later than FAF.
113
Autopilot minimum altitudes -
ILS Coupled (no Autoland)
Non precision w/ VNAV
Non precision w/ V/S
ILS Coupled (no Autoland) - 50' AGL
Non precision w/ VNAV - 50' below DA / 100' below DDA
Non precision w/ V/S. - 50' below MDA / 100' below DDA
114
Max. Landing Weight
198,000 lbs.
115
Max Crosswind - Takeoff & Landing (dry/damp)
30 kts.
116
Do NOT operate NIGHT or IFR at latitudes greater than...
73°N or 60°S if navaids are referenced to MAGNETIC north.
117
Tailwind limit Autoland
10 kts.
118
Max. Take Off Weight
230,000 lbs.
119
Max. wind - Main cargo door OPEN
60 kts.
120
Nav & display system does not support ops. at latitudes
Greater than 87° North or South
121
CAT II/III Crosswind limit Autoland
15 kts.
122
Max. Taxi Weight
231,000 lbs.
123
Max. wind - Main cargo door OPERATION
40 kts.
124
VOR accuracy
4° between both (AML entry if greater)
125
Do NOT use EGPWS if...
QFE ops.
IRS Nav only
No WGS-84 reference
No FMS position update
126
Crosswind limit Autoland
25 kts.
127
FLAPS - Max. Operating Altitude
20,000 ft.
128
Turbulent penetration airspeed
290 kts. / .78 Mach - whichever is lower
129
RVSM Altimeter Crosscheck
In-flight difference - 200 feet
On ground -
Sea level - 35' between / 75' vs. field elev.
130
Non standard fuel load - Center tank
May contain up to 2000 lbs. with less than full wing tanks if...
Center tank fuel + ZFW is less than MAX ZFW (and CG limits are observed).
131
Headwind limit Autoland
25 kts.
132
Max. Depth - dry snow
4 inches / 102mm
133
RVSM - Stby Altimeters
Do NOT meet RVSM requirements.
134
Taxi speeds
Normal - 20 kts.
| Long straight - 30 kts. acceptable
135
Autopilot engagement & limitations
Do not engage below 1000' AGL (FDX)
Use of aileron trim w/ autopilot engaged is PROHIBITED.
136
Max. Depth - slush, wet snow, standing water
1/2 inch (13mm)
137
Fuel temp. - MIN
-45°C or 3°C above freeze point (of fuel type), whichever is higher.
138
Max. Lateral fuel imbalance
1950 lbs. - structural limit
139
Max. Tailwind - Takeoff & Landing
10 kts.
140
Ignition - Severe turbulence
CONT (Continuous) must be selected
141
Engine Anti-Ice
Ground - OAT is 10°C or less (visible moisture)
In Flight - TAT is 10°C or less (visible moisture)
Visible moisture = clouds/fog & visibility less than 1 mile
DO NOT USE - Climb/Cruise when SAT is -40°C or less.
142
Fuel temp. - MAX
49°C
143
Minimum runway width - 180 degree turn
120 ft. / 37M
144
Max. Runway slope
+/- 2%
145
Max. Gear speeds
Normal 270 kts. - .82M
Alt. 250 kts. - .75M
146
Ground Cooling (OAT & packs)
34°C - 49°C - one A/C pack or ground cooling
| 49°C or hotter - BOTH A/C packs or ground cooling
147
Max. Crosswind - Takeoff & Landing (braking POOR)
10 kts.
148
Takeoff - Minimum OIL temp. (PW)
50°C
149
Max. Takeoff & Landing Altitude
8,400 ft. Pressure Altitude
| 14,000 ft. w/ High Altitude Switch
150
DUAL ENGINE FAILURE
Engine Start Selectors....FLT
Thrust Levers .................IDLE
Fuel Control Switches.....CUT OFF, THEN RUN
151
ABORTED ENGINE START
Fuel Control Switch.......CUT OFF
152
CABIN ALTITUDE
Oxygen Masks......ON, 100%
153
SMOKE OR FIRE OR FUMES
Oxygen Masks ......ON, 100%
154
ENGINE FIRE, SEVERE DAMAGE, OR SEPARATION
Autothrottle Arm Switch.....OFF
| Thrust Lever.......................IDLE
155
MAIN CARGO FIRE
Oxygen Masks .....ON, 100%
156
ENGINE LIMIT OR SURGE OR STALL
Autothrottle Arm Switch......OFF
| Thrust Lever.......................RETARD
