GENERAL (NON SPYDER)

During an air start, the cutoff for deciding starter assist vs not is: (CBT)

15% N2. To use the starter, go to STOP, then START, then run

Automatic FSS nitrogen discharge is armed any time: (CBT)

ANY TIME an engine start switch is in the RUN position

(Stallimiter) The flaps down/slats retracted config may (CBT)

not give adequate stall warning. (As opposed to the slats extend, flaps up will provide adequate warning)

If doing a 40% approach, flaps may be lowered to 100% once: (CBT)

Landing is assured (this is for emergency, confirm OK for normal as well)

What comes first, stick shaker or aural "STALL, STALL"? (CBT)

Stick shaker first, if AOA continues to increase, aural goes off, along with red in "special alert window"

Failure of a single or two engines may not affect continued flight, but either case will definitely affect (CBT)

Landing considerations, specifically, rudder trim and reverse thrust

If an engine fails at or above (VMCO flaps still 40%) bank angles up to: (CBT)

30 deg may be used, however rate of climb reduced by 200 fpm

One long sustained blast signals what? (CBT)

Brace for impact

Ground evac

Ditching immediately after takeoff

Crash immediately after takeoff

Six short blasts signals what? (CBT)

Prepare for ditching

Prepare for crash landing

Which start malfunctions do I have to perform manual action? (CBT)

SAV failure CWA (white): Engine start switch - STOP, more actions...

Causes for STARTER SHAFT SHEAR CWA (yellow)? (CBT)

Actual shear

Insufficient bleed air

Partially open SAV (starter air valve)

Multiple approaches: A flight plan discontinuity (-1 2.33.3)

must be inserted in the ACTIVE route to allow the FMS to correctly construct the flight plan legs

Initiate a DIRECT-TO modification to any waypoint. There is no need to EXECUTE this modification.

Select the desired approach on the DEP/ARR page. A discontinuity will be created on the legs page between the

DIRECT-TO waypoint and the approach.

EXECUTE this modification and manipulate the flight plan as desired.

WARNING When past the final approach fix at night or in IMC and an EGPWS aural or visual

warning is received (-1 2.33)

immediately add power, execute a positive pullup until the

warning stops, and verify terrain clearance, sink rate, and proper gear and flap

configuration. If the approach cannot be safely continued, execute a missed approach.

ALL Instrument approaches: bank angles shall be limited to (-1 2.33)

30 degrees for ease in controlling the airplane

With the flaps in the up position, the minimum airspeed shall be (-1 2.30)

100 percent flaps approach speed plus 60 KCAS

Typical Takeoff and Initial Climb (-1 figure 2-13)

Rotate 8-10 deg

Gear up (3 seconds, 25 seconds)

Follow TOGA pitch or VMCO + 10

HMFR/VMFR Flaps up

Climb Power Set

After takeoff climb checklist

After Takeoff, Climb, Cruise, and Descent checklists may be omitted (-1 2.18)

In case of an immediate return after takeoff

or a flight of 60 minutes or less to a base of intended landing

Climbout flight path performance planning assumes landing gear retraction is initiated (-1 2.17.7)

3 seconds after liftoff and the landing gear is fully retracted 28 seconds after liftoff

For Split Marker Takeoffs, the PM will state (-1 2.17.2)

''ROTATE'' over interphone upon reaching VROT

A rolling takeoff shall be made when (-1 2.17)

tailwind component exceeds 10 knots

crosswinds exceed 25 knots below 6,000 feet

(10 knots above 6,000 feet) or if the

airplane begins to creep while at higher takeoff power settings

When performing a castered turn, do not reverse turn direction until (-1 2.14)

the MLG FREE lights extinguish and the aft MLG are centered.

CAUTION The airplane must be moving prior to and during actuation of the (-1 2.14.1)

aft MLG Bogie Emergency Positioning switches.

Do not actuate the Main Landing Gear Bogie Emergency Positioning switch if any

MLG (-1 2.14)

is kneeled or partially kneeled

If any main landing gear is more than 4 degrees from another (-1 2.14)

do not taxi the airplane

Limit taxi speed to knots in congested areas. (-1 2.14)

10

Extreme caution should be used while taxiing at loadings aft of percent CG (-1 2.14)

32

Can an engine be started without associated hydraulic suction system? (-1 2.10)

NOTE the engine may be started without suction pressure; however, this procedure should be used only when absolutely necessary since repeated engine starts without suction

pressure will reduce hydraulic pump life.

What is alternate starting procedure, and is it defined? (-1 2.10)

It's not defined, but it is 4-1

CAUTION If all engines are required to be shut down prior to takeoff, accomplish the (-1 2.10)

After Landing check before accomplishing the Engine Shutdown check. This will prevent power interruptions and possible damage to avionics equipment.

How many APUs do you need? (-1 2.10)

Flight without at least one operable APU is prohibited. This is to ensure that bleed air will be available in the event of a four engine flameout. The generator must be operable on the operating APU and must be capable of carrying the airplane electrical loads to supply power for the Four Engine Flameout procedure.

A complete preflight is required when the airplane has not been flown or preflighted in the last (-1 2.3.2.3)

48 hours

Do I have to read steps containing an irrelevant aircraft mod?

NO. (-1 2.1.1)

Advisory callouts are provided by what?

EGPWS mode 6 using the radar altimeter. The 500-foot callout is intended to be provided only during nonprecision approaches and is determined by pilot CDI source selection. If the B-LOC switch is active on the AFCS panel, the 500-foot call will be provided. If either CDI is set to an ILS frequency and the aircraft is within 2 dots of the localizer, the 500-foot call will be inhibited.

How long does the SAI (Standby Attitude Indicator) take to initialize?

3 minutes

Minimum Maneuvering Speed is indicated by?

yellow diagonal stripes placed over the black background of the airspeed scale and extending up from the bottom of the scale or, when in view, the top of the stall warning onset indication. Minimum maneuvering airspeed (the top of the indication) will vary depending on airplane gross weight, configuration, bank angle, maneuvering load factor and pressure altitude, and is based on 1.2 VSTALL.

STALL WARNING ONSET Speed is indicated by?

The stall warning onset airspeed is indicated by red diagonal stripes placed over the black background of the airspeed scale extending up from the bottom of the scale. Stall warning onset airspeed (the top of the indication) will vary depending on airplane gross weight, configuration, bank angle, maneuvering load factor, and pressure altitude, and indicates the speed at which the stick shaker is activated, 1.05 VSTALL. ( -1)

Normally corresponds to the stickshaker onset point (CBT)

How can the ACCELERATION CUE and the AIRSPEED DEVIATION INDICATOR be used together?

Can be used to first get on speed, and then stay on speed. There is a caution about the acceleration cue not being as reliable in turns.

Can the APU fire warning horn be silenced?

No. Fire must be put out, OR CB must be pulled. Section 1 APU

How many APU fire bottles are there?

2 Total. They may be discharged into a single APU, or both, via the bottle select switch. Section 1 APU

Will an ATM fire be announced?

Not directly, it will be presented as an APU Fire CWA. Section 1 APU

Will APU fire detection and suppression be available without a VIA online?

Yes, hardwired indications and suppression capability still exist with no VIA operating. Section 1 APU

What all happens when you pull fire handle

Hifive acronym?

Hydro 2 places

Fuel 2 places?

Exposes discharge button

Bleed air

IDG

Sends signal to VIA, creates red box

2 Igniters off

Fire suppression 3 buttons

Crew has to fight fire manually

How many seconds do FSS buttons discharge for

45 seconds

How much nitrogen does airplane hold

750 per dewar, usable amount?

Reject mandatory items

Throttles idle

Spoilers optional

TR optional

Brakes optional

When does takeoff inhibit period start/end

80 knots/160 knots or 400AGL?

What are brake temperature ranges

100 normal taxi (anything over 10000 ft is extended taxi)

200 IP only/do not retract gear

300 hydro leak, may encounter brake fire

400 nobody approach brakes

740 end of normal zone, start of first caution, probably wouldn't even taxi in with this, because with increase from taxi, would end up in second caution

800 start of second caution, fuse plugs probably blow, evacuate asapractical

1000 danger zone evacuate immediately

Bleed air stages

Primary 8

Augment 14

Nacelle Anti ice 11

Left or right pylon ovht or overpx how many valves close

7

2 PrSov

2 Hipov

2 PSOV

Respective wing iso valve

Abrupt changes in throttles

Can cause pressure spike and tube bust. Anytime scanner is in eveironmental compartment, especially important

Can you silence oxy warning horn?

Yes, Copilot overhead panel

Center duct ovht how many valves close

8, look up which ones

How many IDG to power whole airplane?

1

This is why there's no bus priority?

How many RTRUS to power all DC

1

How many RTRUS

4

2 main

1 IRCM

1 emergency

Conditions for emergency generator to come on

All gens off or depowered

Something else?

7 bus ops considerations

7 bus ops (emergency), can fly IFR, no autopilot, no tacan, need emergency extend, flaps will work, but slats will decouple, which means they will be stuck out the rest of the time, because the targets are depowered, anti-skid still works.

When does RAT come out

2 onboard engines, and at least 1 outboard

If hydro boost pump in sys 2-3 fails

Must be treated as loss of system quantity

Which fuel tanks cool hydro through fuel

2-3 main

If you get an overpressure hydro

Don't depress pumps, could cause explosion from trapped pressure, leading to fire

Purpose of PTU

Balance work from a heavily taxed system, to a lighter taxed system

Purpose of ATMs

Provide hydro to sys 1-4, work at less px 2500?

Why does PTU 1-2 shutoff when RAT ext

Make sure sys 2 has max avail px for air start ops?

Can you land with RAT ext?

Yes

What does main tank low mean

Fuel less than 75% in outboard main tank 1 and (or?) 4, because there is an associated spd lim. 280/.825. with normal sequencing, it's around 75-80k left, which is about 3 hours.

What does main sump low mean

280/.825. fuel in sump is below 1600 lbs for sys 1 and (or?) 4

Vent fill light on FE

Vent box is more than one-third full.

Follow on, how does the vent fill happen, valves broken somewhere.

Is it possible for LN2 To get into vent box with crack in LN2 lines because of the fuel heat exchanger

Yes

Where do apu tanks get fuel

Main tanks 2-3

How much fuel do we have to have for hydro cooling

1800 lbs? Has to do with which tanks it comes from

Which hydro power flaps and slats

1 and 4

Can use single system, but will take twice as long

Can we do slats by themselves

No, they go automatically after 37% of flaps are out

4 thing's to do whenever flap slat problem

Hand fly so you can feel

If rolling moment, immediately return to previous position. Warning about aircraft loss of control

If no rolling moment, match handle to actual position

Send scanner

Do I need any electrics to do flaps slats?

No, all mechanical connections

How many ways to get nose gear down?

3

Hydro 1

Hydro 4

Crew entry emergency accumulator

How many ways to get MLG?

3

For each forward and aft know it

Normal hydro

Alternate hydro

MLG emergency accumulator

How many ways to get caster?

2?

How many ways to get steering?

?

How many ways to get brakes?

?

Brake supp emergency what do I lose?

Anti-skid

Nlg steer emergency what do I lose?

Rudder pedal steering

What speed do I need anti-skid above?

20 kts

When does gear warning horn sound?

Less than 1000k

Less than some speed

Flaps greater than 80% and gear not down

Which gear has uplock?

Only nose, MLG don't have, they have over center and positioning collars instead

How does crew entry door work with no hydraulics

Lanyard with yellow plate on top, allows locks to release

Pull yellow handle on right side to release locks

Kick door out

Jump last 5 feet

What causes emergency generator to come on?

Move emergency power switch

Emergency bus power relay deenergizes

What does slat flap sync mean?

2 things

What has to be in run for auto discharge FSS to work?

Engine Shutdown switch

3 functions of BCEM

Battery Fill in power

Normal charging of battery

Over voltage protection?

Rat minimum speeds

190 above 15k

175 below 15k

155 to power instruments

Which doors are pressure doors?

Crew entry

Aft ramp

Aft pressure door

Forward ramp

Visor door

What is the priority of the zone alarm pushbuttons

1-4 first, and then down and to the right for 5-12

Fire protection provided by what type of sensors in N2 areas?

Thermal

Dewars provide N2 for which purposes

3 things

Pressurizing

Fuel scrubbing

Fire suppression

Manned areas smoke detectors are which type of sensor?

Optical

Smoke detectors

8

Center wing above flap pack

Avion compartment

A-41 rack

AC load center

Electric power control rack

Troop compartment

Center cargo compartment

Aft cargo compartment

ICAO step size

4000ft

For RTA to function

Must have VNAV in ECON VNAV