systest Flashcards
1
Q
cowl anti?ice
A
overpressure in duct between engine cowl anti?ice valve and cowl lip
2
Q
hyd OVERHEAT
A
electric pump has overheated
3
Q
overwing exit
A
not closed and locked. related flight lock failed to engage (inhibited from t/off to 30 sec after landing)
4
Q
engine control
A
not dispatchable
condition: eng operating, on ground, won’t indicate after 80 kts till 30 sec after ldg
5
Q
PSEU
A
a ground only light
fault in pseu or overwing exit flight lock failed to disengage
inhibited: throttle advance for takeoff till 30 sec after landing
6
Q
lav SMOKE
A
smoke OR
test being conducted
7
Q
ZONE TEMP ? control cabin
A
duct overheat or failure of flt deck primary & secondary temp control
8
Q
ZONE TEMP ? control cabin during recall
A
failure of flight deck primary and stby temp controller
9
Q
ZONE TEMP ? fwd or aft cabin
A
duct overheat
10
Q
ZONE TEMP ?fwd or aft cabin during recall
A
failure of zone temp control
11
Q
PACK
A
pack trip off or failure of both primary and stby pack controllers
12
Q
PACK during recall
A
failure of either primary or secondary controller
13
Q
WING BODY OVERHEAT ?left
A
bleed air leak in one of:
- lt eng strut
- lt inbd wing leading edge
- lt a/c bay
- keel beem
- APU bleed air duct
14
Q
WING BODY OVERHEAT ? rt
A
leak in:
- rt eng strut
- rt. inbd wing leading edge
- rt a/c bay
15
Q
BLEED TRIP OFF
A
high temp or press
bleed air valve closes
16
Q
AUTO FAIL
A
auto press sys fail
1. w/ ALTN light: single controller fault
- on alone: dual controller failure
17
Q
STAB OUT OF TRIM
A
autopilot not trimming stab properly
18
Q
DC FAIL
A
dc pwr for irs not normal. if no other lights on, irs ops normal
19
Q
GPS
A
failure of both gps’s
failure of one when recall pushed
20
Q
idg DRIVE
A
low oil pressure due to:
- idg failure
- eng shutdown
- idg autodisconnect due to high oil temp
- idg disconnected
21
Q
STANDBY PWR OFF
A
one of following not powered:
- a/c stby bus
- d/c stby bus
- battery bus
22
Q
SOURCE OFF
A
transfer bus is not powered by source selected by related generator swithch
- selected source has failed and auto bus transfer has closed BTB to power transfer bus from another source
- no source selected to power transfer bus
23
Q
TR UNIT
- on ground
- airborne
A
on ground: any TR has failed
airborne: TR1 or TR2 & TR3 have failed
24
Q
ELEC
A
ground ONLY
fault exists in DC or standby power system
25
apu LOW OIL PRESSURE
auto shutdown due to low press
26
apu FAULT
causes auto shutdown
27
apu OVERSPEED
causes auto shutdown
28
apu MAINT
can use if req, maint req
29
TWIP
terminal weather information for pilots
30
ACARS
airborne comm and reporting sys
31
ACP
audio control panel
32
ADIRS
air data inertial rreference sys
33
AFDS
auto flt director sys
34
CDS
common display sys
35
CDU
control display unit
36
CVR
cockpit voice recorder
37
DCP
display control panel
38
DEU
display electronic unit
39
ECU
electronic control unit
40
FDD
flight director display
41
FMA
flight mode annunciators
42
FMC
flight management computer
43
FMS
flight management system
44
GPWS
ground prox warning sys
45
IDG
integrated drive generator
46
MCP
mode control panel
47
MFD
multi?function display
48
N1
low prressure compressor and turbine on N1 shaft
49
N2
high pressure comprressor and turbine of engine on N2 shaft
50
PACK
air conditioning package
51
PFD
primary flight display
52
PSU
passenger service unit
53
PTU
power transfer unit
54
SMYD
stall mgmt and yaw damper computer
55
TCAS
traffic alert and collision aviodance system
56
VOR
very high frequency omni directional radio
57
WATRS
west atlantic route system
58
PANS OPS
ICAO ? procedures for air navigational services ? aircraft operations
59
TERPS
U.S. ? standard for terminal instrument approach procedures
60
<4000 RVR / 3/4m considerations
1. capt ldg
2. max x wind 15 kts
3. ldg wt = wet r/w
4. autobrakes (if operable)
5. autopilot recommended
61
flaps 40 recommended
1. wet/contaminated
2. tailwind
3. braking action < good
4. R/W < 6000'
62
autobrakes armed
1. r/w < 7000'
| 2. < good
63
configuration STRONGLY recommended for r/w 6000' or less
flaps 40, brakes 3 or max
64
what r/w length do you enter in HUD
landing beyond threshold
65
when need gear down / flap 15 on non precision app
prior to FAF
66
what does PM select to monitor on non?precision app?
lateral limits
vertical limits
1. Progress pg 4
2. in lnav, max xtk error = RNP value from IAF inbd
3. in VNAV, max vert dev = 75' from FAF inbd
67
deviation callout on localizer app ? when?
diamond touches rectangle on expanded scale OR > 1/3 dot, airplane symbol on 10 mile scale not touching LNAV track
68
procedure if have coded GP to MAXX, EPXX or coded missed app point
expect VNAV disconnect & A/T ARM at these points. Throttles must be manually controlled for remainder of app 7 ldg flare. selecting V/S will keep A/T engaged
69
what do at FAF?
1. CA: final approach fix
70
when select MAA on non?precision app/
1. inside FAF
2. at least 300' below MAA
3. NLT 1000' AFL
71
when disengage autopilot on non?precision app?
DA/DDA
72
when descending using App Lights, what do you need to see to go below 100'
r/w environment
73
what do when APPROACHING FAF?
1. set mins
2. verify VNAV path on FMA
3. gear down, fl 15
74
for non?ils approaches, do 4 things
1. VOR updating off
2. Enter RNP value as req
3. PM monitors Prog pg 4
4. passing FAF, x altimeters +/? 100'
75
not authorized approaches
LPV, WAAS
lpv = Localizer Performance with Vertical guidance
waas = wide area augmentation system
76
is vnav req for RNAV RNP app?
yes
77
is vnav req for RNAV GPS/GNSS approaches
yes, if available
78
can we shoot RNAV GPS approaches?
yes
79
can we shoot GNSS approaches
yes
80
what do if want to shoot app that's not in database?
use raw data instrument approach procedures in QRH
81
what can u check if coded GP on legs page is missing?
check VNAV cruise alt
82
does VNAV GP protect intermediate step down altitudes?
yes
83
what does it mean when stepdown fix on Jepps is not shown on legs page?
the VNAV flt path will satisfy the crossing altitude
84
if shooting an ILS w/ GS inop & there is a coded GP angle on legs page, can you modify the FAF crossing altitude?
no
85
on vor or ndb approaches, when can you add named waypoints?
1. outside FAF or
| 2. after MAP
86
if no GP angle on legs page, how control descent?
vertical speed
87
minimum RNP value
0.11
88
requirements if RNP is less or equal to .3, what need
ANP included w/ flight plan
89
when is autopilot required for RNP approach?
less than .3 RNP
90
max airspeed for final app segment for RNP app?
180
91
accept vectors to RNP RF leg?
no
92
for RNP app & are outside temp limits, can you shoot app?
no
93
when autobrakes?
1. < 4000/ 3/4m
3. contaminated r/w
4. braking action < good
94
what see w/ 3000' r/w remaining?
red/white centerline lights
95
what see w/ 2000' r/w remaining?
amber edge lights
96
what see w/ 1000' r/w remaining?
red centerline lights
97
what ILS cat 3 is 737, a,b or c?
none of them, comply with lowest mins
600 rvr
50' DH radio
98
cat 3 winds max
1. headwind
2. tailwind
3. x?wind
1. 25
2. 10
3. 15
99
1. min alt for selecting A111?
2. alt that flare guidance appears
3. alt throttles retard
1. 500
2. 90
3. 27
100
dev calls on app:
1. localizer
2. glideslope
3. go around
4. centerline
1. diamond touches rectangle or 1/3 dot
2. 1/2 dot
3. anthing amber or red caution or warning annunciated on hud annunciator panel below 1000'
4. after ldg, if grd path diverges from loc
101
what do is tailstrike" annunciates?"
go around RECOMMENDED
102
when can descend below 100' using ALS as reference?
red terminating bars or red side row bars are visible OR BETTER
103
CA's callouts
loc capture
gs capture
OM crossing alt
Flare armed (at 500)"
104
when have to go around on cat 2/3 prior to DH?
any of the req a/c or grd equip fails OR eng fails and are unable to maintain a stable app
105
when go around at DH?
requirements to continue below DH have not been met
106
when go around inside DH?
1. reduction in visibility makes it unsafe to land
| 2. captain determined that ldg cannot be safely made in touchdown zone
107
flap 15 landing speed additives ? where found?
on paper checklist
108
PM callouts
```
trans lvl, altimeters
11000 ft
2500'
1000
500
plus hundred
minimums
50,40,30,20,10
```
109
deviation callouts
1. airspeed
2. rate of descent
3. glideslope
4. loc
1. ? 5 .. +10
2. 2000' ? 2000 fpm
1000' ? 1000 fpm
inside FAF ? 1000 fpm
3. 1/2 dot
4. diamond touches rectangle or 1/3 dot
110
go around requirements
1. a/s
2. rate of descent
3. distance down r/w
1. ?5 +10 without correction
2. >1000 fpm below 1000' w/out correction
3. >3000' down r/w
111
are ceiling limits required on approach?
only when specified on the inst procedure
112
if airport temp is lower or higher than the vnav temp limits on RNAV GPS app, can you shoot the approach?
yes, use the boro?vnav to the published lnav mda + 50', not the lnav/vnav da
113
if airport temp is lower or higher than the van temp limits for a RNAV RNP app, can you shoot the approach?
no
114
what course do you set in the mode control panel for a back course app?
front course
115
when do you have to do timing for an approach?
when UNABLE REQU NAV PERF?RNP is displayed
116
shooting VNAV app to a MAXX or coded MAP, what can you do to prevent loss of vertical guidance & allow the autothrottles to stay connected?
select V/S just prior to MAXX or MAP
117
special authorization CAT 1 (SACAT 1) approaches
1. who flies it?
2. what airplanes
3. what procedures
4. HUD fails?
5. xwind max
6. what RVR is controlling?
7. wx mins
1. captain
2. cat 2 capable w/ HUD
3. cat 2/3
4. go around unless vfr
5. 15
6. TDZ
7. 1400 RVR w/ 150' DH
118
when disengage autopilot on CAT 1 ILS
nlt 50' agl
119
loc dev for cat 2 go around
2 1/2 dots (loc diamond goes hollow)
120
are cat 2 or cat 3 procedures the same?
yes
121
what is purpose of LMP (lower minimums program)?
govern ops below cat 1 mins
122
what rvr mins is the 737 capable of
TDZ 600
MID 400
R/O RPT
123
general rule regarding CAT 3 mins:
the min RVR value shown on the far left column of the app plate mins box is the controlling RVR for the app and must be applied to all the controlling transmissometers
124
what if cat 3 app plate say 3 on left side of plate, what mins do i need?
TDZE 600
MID 400
R/O advisory
125
what if cat 3 app plate says 6 on left side of plate, what wx do i need?
TDZE 600
MID 600
R/O ADVISORY
126
if cat 3 app plate says 7 on lt side of plate, what wx do i need?
TDZE 700
MID 700
R/O advisory
127
at what altitude can HUD begin TAILSTRIKE warnings?
300'
128
can we land with >50 kts wind?
only in emergency
129
max xwind B.A. fair
20 kts
130
max xwind B.A. poor
10 kts
131
max xwind cat 2 or 3 OR < 4000/ 3/4
15
132
which is stronger braking, max autobrakes or full manual
full manual
133
what flaps do you set for F15 go around?
flaps 1
134
max thrust required when?
```
1. wet r/w (not pfc or grooved)
reduce V1 5 pfc/grooved
reduce 8 or 9 non pfc/grv
2. MEL/CDL not in tps
3. anti?ice not in tps
4. t.o. wt > ATOW
```
135
when use low vis t/off procedures
<500 rvr down to 300 rvr
136
when use 26K Max thrust?
1. improved performance
2. contaminated r/w
3. windshear
4. gust>10 / 15 kt x/wind
137
distance behind heavy?
2 minutes or 5 miles
138
min turn altitude
400' (100' if ops advisory page says so)
139
distance between ctr line lights
50'
140
distance between r/w edge lights
200'
141
wet r/w considerations
1. max thrust (unless PFC/grooved
2. improved perf not auth
3. anti?skid req
4. reduce V1
5. r/w limited t/off wt reduced (if not pfc or grooved
142
damp r/w defined
no shiny appearance, is considered dry
143
V1 reductions for wet r/w
1. pfc or grooved
2. F1 non?pfc/grooved
3. F5 non?pfc/grooved
4. F15 non?pfc/grooved
1. 5
2. 8
3. 9
4. 8
144
contaminated r/w definition
1. standing water, slush, wet snow >1/8
145
contaminated r/w limitations
1. no tailwind t/off
| 2. NGT 1/2 wet snow, slush or standing water or >4"dry snow
146
1. normal t/off pitch
2. normal t/off tail clearance
3. tailstrike at what pitch
1. 8?9 degrees
| 2. 20 (at fl 1 & 5)
147
max tailwind for t/off
15 kts
148
when atl does lnav become active
50'
149
t/off with greater than 20 Kts, what is recommended
rolling takeoff
150
t/off w/ gusts > 10 kts or x/wind > 15 kts, what is recommended?
26K max
151
when does ldg gear transfer unit work?
1. airborne
2. #1 engine fails
3. gear lever up
4. either main not up & locked
152
what does PTU power?
1. autoslats
| 2. LED
153
when does PTU work?
1. B hyd sys press low
2. airborne
3. flaps 1?10
154
of sys that power brakes
1. normal
2. alternate
3. accumulator
155
PSEU checks?
1. t/off config
2. ldg config
3. ldg gear
4. air/ground sensing
156
how do autoslats work?
extend slats from extend to full extend
157
what can power autoslats?
1. B hyd
| 2. PTU
158
A hyd sys powers?
```
a real giant p
aileron
rudder
elevator
autopilot A
ldg gear
grd spoilers
inbd flt spoilers
alt brakes
nose wheel steering
thrust reversers
ptu
```
159
b hyd sys powers
```
a real toy baatl
aileron
rudder
elevator
autopilot b
ldg gear transfer unit
t.e. flaps
outboard spoilers
yaw damper
brakes normal
autoslats
alt nws
thrust reversers
l.e. devices
```
160
stby hyd powers?
```
l s t s
l e flaps & slats
stby rud ptu
thrust reversers
stby yaw damper
```
161
flight controls #s
1. l.e.d.
2. spoilers
3. flaps
L.E.D. ? 12 .. look at overhead ? 8 slats, 4 flaps
spoilers ? 12 ? 8 airborne, 4 on ground
flaps ? 2 per wing
162
reversers ? # of detent
there are 2 beyold idle reverse
163
when use trans lvl?
when use trans alt
1. on descent
| 2. on climbout
164
how do autoslats work?
extend slats from extend to full extend
165
what can power autoslats?
1. B hyd
| 2. PTU
166
A hyd sys powers?
```
a real giant p
aileron
rudder
elevator
autopilot A
ldg gear
grd spoilers
inbd flt spoilers
alt brakes
nose wheel steering
thrust reversers
ptu
```
167
b hyd sys powers
```
a real toy baatl
aileron
rudder
elevator
autopilot b
ldg gear transfer unit
t.e. flaps
outboard spoilers
yaw damper
brakes normal
autoslats
alt nws
thrust reversers
l.e. devices
```
168
stby hyd powers?
```
l s t s
l e flaps & slats
stby rud ptu
thrust reversers
stby yaw damper
```
169
flight controls #s
1. l.e.d.
2. spoilers
3. flaps
L.E.D. ? 12 .. look at overhead ? 8 slats, 4 flaps
spoilers ? 12 ? 8 airborne, 4 on ground
flaps ? 2 per wing
170
reversers ? # of detent
there are 2 beyold idle reverse
171
when use trans lvl?
when use trans alt
1. on descent
| 2. on climbout
172
what sys use bleed air?
```
a/c and press
aspirated TAT probe
wing and engine anti?ice
engine start
hyd reservoir press
water tank press
```
173
why get bleed air trip
overtemp
| overpressure
174
what is req when using external air for bleed pressure?
batt switch on ?so that protective circuits are enabled
175
how many packs can apu power
2 on ground
| 1 airborne
176
pack high flow .
1. when?
2. when inhibited?
3. when high flow w/ APU supplying air?
1. either pack not operating
2. a/c on ground OR airborne w/ flaps extended
3. always (eng bleed air switches must be off)
177
when do ram air doors go full open?
on the ground OR
| airborne w/ flaps extended
178
if all temp selectors are turned off, what temp do packs produce?
zone temp controllers temp range
lt pack = 75, rt pack = 65
65?85
179
if both zone and primary pack controllers fail, what happens?
standby pack controller will command packs to produce air which will satisfy the avg temp demand of the 2 cabin zones
180
trim air switch . what do?
opens/ closes trim air regulating & shutoff valve which allows hot bleed air to enter the zone supply ducts thru the trim air modulating valves
181
2. on following mstr caut recall"
1. overheat
| 2. failure of temp controller
182
2. of following master caution recall"
1. duct overheat or failure of primary & secondary temp controllers
2. either primary or secondary controller failed
183
what happens if turn off one of the 3 temp selector controls?
trim air mod valve closes and temp is governed by the output of the a/c packs
184
recirc fans: when turn off automatically?
1. on ground
2. airborne
1. lt fan off if both pack switch to high
rt fan stays on even if both pack switches to high
2. lt fan: off if either pack switch in high
rt fan: off if both pack switches in high
185
pack light
1. why
2. why if comes on at recall?
1. overheat or both primary and secondary pack controllers have failed
2. failure of one of the pack controllers
186
APU bleed switch closes when?
fl200
187
LEFT wing body overheat light
```
lt engine pylon
left inboard wing leading edge
left side of a/c bay
keel beem
APU duct
```
188
RIGHT wing body overheat light
right engine pylon
right inboard wing leading edge
right side of a/c bay
189
when does overboard exhaust valve open?
both packs high flow AND
| recirc fans off
190
what powers manual press controller?
how long to go from full open to full closed/
battery
20 seconds
191
what brings on AUTOFAIL light?
1. loss of DC power
2. cabin climb > 2000FPM
3. controller failure
4. high cabin altitude (>15,800')
192
can you use both APU air & external air to power packs?
yes ... there's a checklist in vol 2
193
what happened when get ALTN & AUTO FAIL lights on?
single controller failure and auto switch to the other controller
194
minimum pressure when using external high?pressure for air conditioning
20 psi
195
when do l.e. slats go from extend to full extend?
flaps moved to 10
196
what l.e. devices does wing anti?ice heat?
3 inboard l.e. slats only
197
what lose if lose one of two irs's?
lose autobrakes @ thus cat 2/3 capability
198
what are 3 ground only" annunciator lights on ov'hd panel?"
engine control
elec
pseu
199
how many gps's?
2
200
irs fault light .. what mean?
nav or attitude fault
201
what also happens if get an irs on dc" light when on the ground?"
ground crew call horn sounds
202
irs alignment times
fast alignment times
fast alignment requirement
what do if inadvertent sw to OFF or ATT?
5?17 min (7?10 at our latitudes)
30 sec
a/c must be stationary (procedure in vol 1 systems section)
must do full alignment
203
what do?"
eec fault
| no?go
204
what happens when move alternate flaps switch to arm?
1. stby elect pump on
2. close t.e. flap bypass valve
3. arms alt flap pos sw
4. allows stby sys to pwr l.e. flaps, slats, thrust reversers
205
speedbrakes extended light
speedbrake lvr is past arm position &
flaps >10 OR
below 800'
206
what controls eng valve closed" & "spar valve closed" lights, meaning what can open/close those valves"
eecs
| fire handle
207
can wing tank pumps suction feed?
can ctr tank pumps suction feed?
total fuel
yes
no
8.6+8.6+28.8 = 46.0
208
elec fault" light"
dc or stby bus fault
209
depart w/ batt discharge, tr unit or elec light on?
no
210
stby pwr off ... wht mean?
loss of stby a/c, stby d/c or batt bus
211
when will idg disconnect work?
elect pwr available AND
| start lvr ? idle
212
apu maint light ..
3 apu fault lights . what do
maint req, can still use apu
shut down apu
213
eec's powered at what n1?
15%
214
fuel filter bypass" light"
impending fuel filter bypass
215
a/c sys 'OVHT TEST button"
tests wing/body overheat detectors
216
a/c sys trip reset button resets
pack trip
bleed trip
zone temp trip
217
wing body ovht light
```
eng strut
engine strut
inbd wing leading edge
a/c bay
+
lt .. keel beam
... apu bleed duct
```
218
pack light
pack trip OR
| primary & secondary pack controller failed
219
flashing align light
nothing entered or position entered is > 4 nm off
220
stab out of trim" light .. when work?"
autopilot on & autopilot not trimming stabilizer correctly
221
will a/t work with eec's in alt?
yes
222
6. when get climb power?"
1. pitch to 15 degrees nose up
2. throttle hold
3. pitch to 15 degress till sufficient climb rate, then pitch to meet mcp speed, normally v2 + 20
4. LNAV
5. a/t in throttle hold till 800', can now reduce to climb power
6. when vnav, alt acq or alt hold are selected .. if engaging lvl chg or v/s, auto thrust reduction is inhibited for 2 1/2 min after t/off
223
what happens when TO/GA?
what happens when TO/GA 2nd time?
1. a.t. give 1000?2000 fpm climb
| 2. pitch to 15 degrees till get certain climb rate, then maneuvering speed for each flap setting is directed
224
how terminate TO/GA?
1. below 400'
2. above 400'
1. both flight directors off
| 2. different pitch or roll mode selected
225
what happens when select ALT on audio control panel
1. can only control respective vhf radio
2. speaker and volume control functions inop .. also inop interphone, hand mike and p.a. sys ... can't hear alt alerts, gpws and windshear
226
eec protection
1. airborne
2. on ground
1. n1 and n2 overspeed
| 2. overspeeds + wet and hot start
227
thrust reverser pwr sourse
1. #1
2. #2
1. sys A hyd w/ stby as backup
| 2. sys B hyd w/ stby as backup
228
fire detection .. what pwr source?
| fire protection .. what pwr source?
1. battery bus
| 2. hot battery bus
229
will APU auto?shutdown w/ fire?
where is apu fire handle?
yes
right wheel well
230
how many cargo fire bottles?
power source
how many apu fire bottles
one halon bottle
hot battery bus
one
231
lav fire detection:
1. discharge nozzle appearance
2. flight deck indication of discharge
3. temperature indicator appearance
1. flat black, turns gray if sys discharges
2. none
3. white dots turn black when exposed to heat
232
horns that can be silenced
1. fire warning (press fire warn light)
2. landing gear horn
3. cabin alt horn
4.
233
when do spoilers deploy during landing
1. armed
2. throttles idle
3. radio alt < 10 ft
4. mains touch & > 60 kts = flt spoilers
5. rt main strut compresses = grd spoilers deploy
234
during RTO, when do auto speedbrakes deploy?
both throttles to idle & reverser levers to reverse
235
what does FSEU (flap/slat electronic unit) do?
protect TE flaps from excessive airload .. flaps 40 to 30 or 30 to 25
236
autoslats .....
1. what happens?
2. pwr source?
1. w/ flaps 1?5 & approach stall, LE slats go to full extend
| 2. sys B w/ PTU as backup
237
CDS FAULT or CDS MAINT ?
non?dispatchable fault, ground only
238
AOA green band
for any flap setting, the 3 o'clock position, green band provides safe speed
239
VNAV speed ... ensure altitude restriction will be met?
no
240
which fuel tank pumps have higher pressure
center tank pumps are higher
241
which tank has a scavenge pump
center tank, which ops automatically when fuel in #1 tank reaches around 4500# and the #1 main tank fwd pump is operating. pump ports fuel into the #1 tnk at approx 177 lb/hr
242
cowl anti?ice light .. what mean?
excessive pressure has built up in the duct between the engine cowl anti?ice valve and the cowl lip
243
when do wing anti?ice valves auto?close?
what happens when turn switch on/
1. overtemp
2. t/off pwr selected
bleed air to l.e. devices
sets stick shaker logic for icing conditions
244
which windows are heated?
all but rear most side windows
245
do autobrakes work w/ alt brakes?
anti?skid with alt brakes?
no
yes, but for wheel pairs only, not individual wheel
246
what happens if raise ldg gear & have damaged main gear tire is detected?
the individual main gear will free fall down
247
how do you deactivate autobrakes
switch off
grd spoilers/speed brake to down detent
thrust lvrs past 11 degrees
manual brakes
248
how detect parking brake fault?
ANTI SKID INOP light on when brake is being set
249
tcas:
1. red RA
2. amber TA
3. fully white rectangle
4. reverse video rectangle
1. threat within 25 seconds
2. 40 seconds
3. . 6 miles & +/? 1200' vertical
4. +/? 8700' vertical
250
predictive windshear
1. warning
2. caution
3. when active on ground
4. ceiling limit for warnings
1. 1.5 nm ahead of a/c
2. 3 nm ahead of a/c
3. thrust lever to takeoff pwr
4. 1200'
251
sys a standpipe protects what?
elect pump
252
sys b standpipe protects what?
ptu
253
what does ptu power
l.e. flaps and slats and autoslats
254
when does ptu come on
1. sys b eng pump low press
2. airborne
3. flaps 1?10
255
stby hyd uses what fluid
fluid from b res
256
stby hyd .. when come on automatically?
1. sys a or b lost
2. airborne or wheel spinup >60 kts
3. flaps extended
257
stby hyd .. why does it come on automatically
1. pwr rudder if airborne
| 2. pwr thrust reversers if abort
258
what systems does stby hyd pwr?
LSTS
1. l.e. flaps and slats (extend only)
2. stby rudder
3. thrust reversers
4. stby yaw damper
259
landing gear transfer unit ..
1.when powered?
2. what fluid does it use?
1. airborne
2. raise gear and one of mains is not up and locked
3. #1 engine drops below limits
2. sys B
260
a hyd sys powers:
size of reservoir
cooled by:
a real giant p
1. ailerons
2. rudder
3. elevators
4. autopilot A
5. landing gear
6. ground spoilers
7. inboard flight spoilers
8. alt brakes
9. nose wheel steering
10. thrust reversers
11. ptu
5.7 gallons
fuel tank 1
261
lose a hyd sys and lose what sys:
a giant p
1. alt braks
2. ground spoilers
3. inbd flt spoilers
4. autopilot a
5. normal nose wheel steering
6. thrust reverser
7. ptu
262
b hyd sys powers:
size of reservoir
cooled by:
a real toy baatl
1. ailerons
2. rudder
3. elevators
4. autopilot b
5. landing gear transfer unit
6. trailing edge flaps
7. outboard spoilers
8. yaw damper
9. brakes (normal)
10. autoslats
11. alt nose wheel steering
12. thrust reversers
13. leading edge devices
8.2 gallons
fuel tank 2
263
b hyd sys loss and lose what sys:
a toy baat
1. autoslats
2. trailing edge flaps
3. outboard spoilers
4. yaw damper
5. brakes (normal)
6. autopilot B
7. thrust reverser
264
force flight monitor: what does it do?
detects opposing pressure from a & b sys to rudder which could happen if a or b input is jammed or disconnected from rudder. will auto turn on stby hyd and pwr rudder.
265
autoslats:
| when work?
move slats from extend to full extend prior to stick shaker ... when t.e. flaps are at 1?5 degrees
266
what powers autoslats?
sys B unless sys B pressure is low, then PTU
note: slat/flap skew detection is inop during autoslat deployment
267
what is powered when you move flt control switches to STBY?
rudder & thrust reversers
268
if both flt control switches are moved to STBY, what happens to aileron and elevator control?
manual reversion
269
what happens when alt flap master switch is moved to down pos?
1. T.E. flaps electrically move down (can be moved back up)
| 2. Leading edge devices moved to full down pos hydraulically (cannot be moved back up)
270
when is hyd q RF indication valid?
1. a/c on ground w/ both engines shutdown OR
| 2. after ldg w/ flaps up during taxi?in
271
sys a & b pressures
normal
max
min
3000
3500
2800
272
electric hyd pump overheat" light: what means?"
pump overheated and has shut down
273
3 ways to turn stby hyd pump on
3 switches on flight controls overhead
274
3 ways stby hid pump get turned on automatically
force fight monitor
thrust reversers
autoslats
275
when abort engine start
1. n1
2. lightoff
3. no/slow n1 or n2
4. oil pressure
1. need before raise start lvr to idle
2. within 10 sec (30 sec airborne)
3. after EGT rising
4. need it by stable idle
276
what do braking advisorys mean?
continue the approach: poor or nil have been reported or conditions are deteriorating rapidly
277
can you t/off and land with:
1. windshear alert
2. microburst advisory
3. microburst alert
1. yes
2. yes
3. no
278
wet r/w takeoff:
1. power
2. speeds
3. req equip
4. additional notes
1. not grooved or pfc: max pwr
2. reduce v1
3. anti?skid
4. improved perf not auth .. r/w limited t/off reduced for non grooved or pfc r/w's
279
when is max pwr req?
1. wind
2. r/w conditon
3. weight
4. engine anti?ice
1. tailwind
2. wet r/w
3. closeout > ATOW
4. eng anti?ice used and tps doesn't show it
280
max pwr 26k req
1. r/w condition
2. wind
3. performance
4. other
1. contaminated
2. windshear
3. improved performance
4. fm?2 airport advisory requires it
281
r n p notes
1. temp ngt rnav/rnp temp
2. x min equip
3. rnp< 0.3 .. autopilot req
4. vor update off
if rnp specified on app plate, manually enter in prog 4/4
5. pm = in lnav, monitor xtk error on app ngt app rnp from iaf inbd
6. in vnav path , pm monitor vert dev on prog 4/4 ngt 75' from iaf inbd
anp prediction req for rnp values < 0.3
282
flaps 40 recommended
1. r/w slippery
2. b.a. < good
3. tailwind
283
autobrakes req
1. r/w < 7000'
2. wx < 4000 3/4
3. b.a. < good
4. contaminated r/w
5. recommended: gusty winds
284
flaps 15 req when?
high density airports when climb limited max ldg wt is exceeded for f30 & f40
285
how determine 3 degree glideslope?
1/2 airspeed x 10 = ft / minute descent required
286
holding speeds
1. 6000' or less
2. 6000?14000
3. >140000
4. timing
1. 200
2. 230 (210 dca & ny)
3. 265
4. 1 min inbd 14K
287
max landing distance down r/w
3000'
288
737 category
C
289
when get ground crew call horn?
1. battery discharging
2. equip cooling fan fail & get overheat
3. button pushed
4. irs on battery pwr
290
takeoff and don't to/ga?
wwill get tailstrike annunciation
291
when can inhibit glideslope?
1. ils on 1 r/w and landing on another
| 2. following g/s prrecludes landing on 1st 1000'
292
best cabin cooling?
both engine bleeds off, apu bleed on
293
r/w contamination factors
1. snow
2. ice
3. wet
4. hydroplane
1. 2 x dry
2. 4?16 x
3. + 60%
4. 2?3 x
294
allowable overweight landing weight
lesser of r/w limited and clib limited land weight
295
zero cost index .. what does it give u?
max range cruise
296
select deny" on flt deck door control"
disables auto unlock function, cancels alerts and prevents keypad entry for 5 minutes
297
dual generator failure prior to v1 .. what do?
captain takes a/c and continues t/off
298
do g/a and come back for another app. what have to do?
1. vnav cruise pg; select altitude that you climbed to on m.a.
2. reselect cat 3 if you are doing a cat 3 approach
3. note: x usable r/w length on pg 9B if doing a cat 3 and put in cat 3 page
299
when don't you have to use wind corrections for ldg
1. hud
| 2. autothrottles
300
last minute bags?
shutdown #2
301
engine fails on final, what mins can you use?
cat 1
302
speed brake load alleviation sys
1. when
2. what happens
1. flaps up, >155k #, >320 kts
2. if spd brake > 50%, will retract to 50%
3. if < 50%, will limit use to 50%
4. note: can be overridden
303
when do autospeed brakes work
1. armed
2. 60kts (flt spoilers
4. rt strut compresses (grd spoilers)
304
force fight monitor: what does it do?
senses imbalance in pressure from sys A & B and will add stby pump to that side of rudder
305
what is the NGS?
nitrogen generating sys, converts bleed air to nitrogen enriched air & delivers to the center fuel tank to reduce flammability of the tank. dispatch w/ sys inop is OK
306
abort .. why?
engine failure, fire, predictive windshear or anything that makes a/c unsafe or unable to fly
307
abort .. considerations after stop a/c
1. advise F/A's & psgrs: stay seated or evac?
2. alert fire equip?
3. clear r/w
4. set brakes?
5. complete x/list for conditions causing RTO
6. remote parking?
7. wheel plugs melt?
8. brake cooling sked
9. inspect: >80 kts, hvy, max brakes
10. when speed brakes deploy? select reverse thrust
308
upset recovery .. nose high
1. autopilot/autothrottle ? off
2. nose down elevator / trim
3. roll to get nose down pitch
4. reduce thrust
5. approaching horizon .. wings lvl
6. x airspeed & adjust throttle
309
upset recovery .. nose low
1. autopilot/autothrottle . off
2. recover from stall if req
3. roll to wings lvl
4. recover to lvl flight / nose up elevator / trim (as req), adjust thrust & drag as req
310
windshear/microburst on takeoff
1. rotate to 15 degrees
2. airborne: escape maneuver
3. if a/s decreases < rotate:
a. if can't stop, rotate by 2000' remaining even if slow
b. note: 3000' = red/white ctr?line lites, 2000? = amber r/w edge lights, 1000' = red ctr line lights
311
windshear .. airborne
1. escape"
312
engine failure on t/off
1. positive rate, gear up
2. set speed ? at engine out alt
3. lvl change, mct ... checklist
notes: 4 xlists, 14.5 ctr?line, v2?v2+20, a/p from good eng side, rudder trim = 1 unit/sec = amt of fuel flow, = 5 units @ s&lvl, fly the hud, marry up the throttles, hud no see eng out lvl?off, reduce 3% n1 at glide slope, select a/p at lvl?off
SL, normal weight pattern = 72% N1 4.5 units trim
313
engine failure at cruise
1. disconnect a.t.
2. adjust rudder
3. select CON thrust in FMC
4. manually select CON thrust
5. select engine out cruise in vnav ..
6. select engine out alt and speed on panel
6. slow to eng out a/s
7. select lvl chg & descend to alt
314
pull up, terrain, terrain""
1. a/p, a.t. .. off
2. throttles ? max
3. pitch ? 20 degrees nose up or >
4. speed brakes ? retract
315
tcas"
1. autopilot ? off
2. autothrottles ? off
3. maneuver as req
316
climb, climb now" when in ldg config"
1. autopilot ? off
2. autothrottle ? off
3. throttles ? max
4. flaps 15, positive rate, gear up
317
go?around
1. go around"
318
1 engine go ? around
1. to/go . (max pwr, max foot)
2. flaps 1, pos rate, gear up
3. approx 15 degrees nose up
4. set m.a.a.
5. lnav or hdg select
6. 1000' ? set speed
7. flaps up
8. level change . set mct
319
when set altitudes during vnav app
1. faf
2. mda
3. maa
1. when cleared for app
2. when faf is active waypoint
3. when 300' below maa, inside faf & > 1000' afl
320
engine failure on final 3 choices
1. go around
2. stay at fl 30 .. adjust rudder, add 1 knob width pwr (60% to 80%)
3. select fl 15: adjust rudder, add 20 kts, grd prox flap o'ride ? inhibit
321
circling approach #s
1. airspeed
2. weather mins
3. mda
1. 140 kts max
2. 1000?3
3. 1000' or published mins if are higher
322
vertical speed approach
1. when use
2. how descent prior and after faf
3. dda = ?
1. vnav won't work or no coded gp angle on legs page
| 2. prior = lvl change , after ? vert spd
323
engine failure during go?around
1. perform normal go?around
2. max thrust
3. maintain f15, vref 30?40 and limit bank angle to 15 degrees till maneuvering complete and safe alt
324
problems during engine start
engine start lever ? cutoff
325
airspeed unreliable
1. adjust attitude & thrust . maintain aircraft control
2. probe heat switches ? check on
3. crosscheck mach airspeed indications
326
apu fire
1. apu fire switch . confirm . pull and rotate . hold 1 second
2. apu switch ? off
327
cabin altitude warning .. cabin altitude exceedence and/or intermittent horn & cabin altitude lights
1. o2 mask on @ 100 % o2
2. crew comm establish
3. pressurization mode selector ? manual
4. outflow valve sw ? hold in close pos until valve indicates closed
5. if cabin alt is not controllable
a. fasten belt sw ? on
b. if cab > or expected to be > 14k'
psgr o2 sw on
c. go to emergency descent xlist
328
emergency descent
1. announce emergency descent
a. captain advises cabin crew
b. f.o. tells atc and gets atlimenter
2. fasten belt sw on
3. engine start switches ? cont
4. flt lvl change, vmo descent w/
speedbrakes, autopilot on ...stop
descent at 10K or lowest safe,
whichever is higher
329
ENGINE FIRE or ENGINE SEVERE DAMAGE or SEPERATION
1. autothrottles ? off
2. thrust lever ? confirm ? close
3. engine start lever ? confirm ? close
4. engine fire sw ? confirm ? pull
(to manually unlock, press
override & pull)
5. if engine fire switch or eng overheat light stays on
a. engine fire sw ? rotate to stop & hold for 1 sec
b. if after 30 sec & eng fire sw or overheat light still on, engine firre sw ? rotate to other stop & hold for 1 sec
330
ENGINE LIMIT or SURGE or STALL
1. autothrottle ? off
| 2. thrust lever ? confirm ? retard till indications stay within limits or thrust lvr is closed
331
engine overheat
1. auththrottle ? disengage
2. thrust lvr ? confirm ? close
3. if engine overheat stays illuminated ? go to engine fire or engine severe damage or separation xlist
332
engine tailpipe fire
1. engine start lvr ? cutoff
| 2. advise cabin
333
landing configuration (steady horn)
assure proper landing configuration
334
loss of thrust on both engines
1. engine start switches ? flight
2. engine start lvr's ?cutoff
3. when egt decreases ? engine start lvrs (both) ? idle
4. if egt reaches 950 or no increase in 30 seconds ? eng start lvr ? confirm cutoff, then idle detent
5. if egt again reaches 950 or no egt increase in 30 sec, repeat
335
overspeed
reduce thrust & if needed, adjust attitude to reduce a/s to below vmo / mmo
336
rapid depressurization
same as cabin altitude warning
337
runaway stabilizer
1. control column ? hold firmly
2. autopilot ? disengage ? control pitch attitude manually w/ control column & main electric trim
3. if runaway stops: end
4. if runaway continues ? stab trim cutout switches (both) ? cutout
5. if runaway continues: stab trim wheel ? grasp & hold
338
takeoff config horn (intermittent) OR tafeoff config light
fix it ... TE flaps, LED, stab trim, spoiler handle, parking brake
339
inflight: intermittent horn or cabin altitude light above 10000'
1. don o2 mask & set 100%
2. establish crew comm
3. CABIN ALTITUDE WARNING or RAPID DERESSSURISATION XLIST
340
max altitude
410
341
o2 required when other pilot leaves cockpit
fl250
342
max t/off alt
8400
343
max alt for a/p on t/off
500'
344
max flaps alt
fl200
345
min speedbrake alt
1000
346
max fuel temp
| why/
49 degrees .. fuel cools oil
347
std r/w width min
148'
348
a/c turning radius
79'
349
dry r/w xwind
33
350
rolling t/off recommended w/ winds
20 kts
351
braking action fair max x/winds
20
352
braking action poor max x/winds
10
353
< 4000 rvr landing max x/wind
15 ... captain's landing
354
<1800 rvr landing max x/wind
10
355
cat 2 or 3 max x/wind
10
356
max gust
50
357
r/w less than std max x/wind
20
358
contaminated r/w t/off not authorized
3 dry snow
359
```
apu max:
alt
start
bleed air
electric
bleed/elect
```
max 410
start 410 (250 recommended)
bleed 170 (bleeds auto close @ 200)
bleed/elect 100 (max demo 200)
360
fuel quantity
8.6 +8.6 +26.6 = 46K = around 7K gal
361
min fuel for ground ops of elect hyd pumps
1676
362
low fuel lights
2000
363
main tanks req full if center tank has ___?
1000
364
quantities for ctr tank fuel pumps on:
a. ctr tank q at push
b. ctr tank at 10000'
c. cruise .. when turn 1 pump off
d. t.o.d. ? when turn 1 pump off
a. 5000
| b. <3000
365
fuel config light comes on when?
>1600 in ctr tanks w/ ctr tank pumps off
366
fuel Q used during g/around to vfr pattern & land
900 #
367
min crew 02 for dispatch
1000 psi (not a hard #)
368
psgr o2
1. how long does it last?
2. when does it auto?drop?
3. when do you get cabin horn (intermittent)?
4. when do you get auto?fail" light?"
1. 12 minutes
2. 14000'
3. 10000'
4. 15,800'
369
weights
1. max taxi
2. max t/off
3. max ldg
4. max zfw
1. 174.7
2. 174.2
3. 144
4. 136
370
min r/w width w/ snow or r/w
100'
371
engine start times
1. length of start
2. time between starts
1. 2 min
| 2. 10 seconds
372
taxi n1 recommendations
1. congested ramp
2. elsewhere on ramp
3. taxiway
1. 35
2. 40
3. 45
373
boom mike req below what alt?
180
374
engine runups during bad cold wx?
1. ground?
2. airborne?
1. 70% n1 every 10 minutes
| 2. 80% n1 every 15 min
375
takeoff speeds
1. 60 knots
2. hot egt after 80 kts
3. 84 kts
4. 90 kts
5. no throttle hold?
6. want full thrust w/ thr hold" displayed?"
1. final thrust adjustments
2. don't retard throttles yet, wait till 400'
3. throttle hold .. a.t. can't change throttle pos, but I can
4. autobrakes now available
5. no crew action req
6. manually advance them
376
min pavement for 180 degree turn
78'
377
a/c
1. length
2. width
3. height
1. 129'6
378
PBE
1. time
2. flashing green?
3. flashing green/red?
4. preflight down?
1. 15 minutes
2. good
3. bad
4. green tamper seal disturbed or humidity indicator pink
379
captain t/off mins?
f/o takeoff mins?
300' (sea, slc, mem, den
500'
380
max speed rnp app final app segment
180
381
a/p off
1. non?ils
2. cat 1
3. cat 2/3
4. takeoff
1. da/dda
2. 50'
3. 1000'
4. 500'
382
max altitude that you can select go?around?
2000'
383
windshear
1. scans below what altitude?
2. alerts below what altitude
1. 2300'
| 2. 1200'
384
distance from U.S. coast that you can go >250 kts below 10000'
12 nm
385
weather <4000/ 3/4
1. who can land?
2. max x/wind?
3. equipment req on?
1. ca ldg only
2. 15 kts
3. autopilot & autobrakes
386
how long does it take engines to spool up?
7?8 seconds
387
no go takeoff contaminated r/w
1. dry snow
2. wet snow
3. other
1. 3
388
cat 1, 2, 3 weather
1800, 1200, 600
389
what do if wx goes below mins after final app segment?
define final app segment
continue
g/s intercept
non?precision: FAF or if no FAF, where procedure turn intercepts final app cus
390
touchdown points
1. preferred
2. must land by distance
3. must land by percentage
1. 800?1500'
2. 3000'
3. first third
391
time to allow APU to cool down before turning battery off
2 minutes ? allow APU to shutdown and doors to close
