Boeing 737-200 Type Rating

Front 1

Approximate range of the 737-200?

Back 1

Approx 1500 NM

Front 2

What side of the aircraft is the service side??

Back 2

The right side

Front 3

What service items are on the right side of the airplane?

Back 3

Forward Lav
Aft Lav
Forward Galley
Aft galley
Potable water
Fueling

Front 4

Cargo is accessed on what side of the airplane?

Back 4

Right side

Front 5

What is the total volume of the forward and aft cargo bins?

Back 5

FWD - 370 cu. ft.
AFT - 505 cu. ft.

Front 6

Size of forward and aft cargo doors?

Back 6

FWD - 51 x 48''
AFT - 48 x 48''

Front 7

Where is external power receptical located?

Back 7

Forward, right side below first officers window

Front 8

What are the dimensions of the Boeing 737-200?

Back 8

Wheel Base - 17'
Height - 37'
Main Wingspan - 93'
Horiz wingspan - 36'
Length - 100'

Front 9

Max. nose wheel steering angle?

Back 9

78 deg. minus 3 deg tire slip resulting in 75 deg

Front 10

Minimum taxiway width required for maximum effort turn is?

Back 10

60'

Front 11

Max take off weight?

Back 11

117,000 lbs

Front 12

Max landing weight?

Back 12

105,000 lbs

Front 13

Max zero fuel weight?

Back 13

95,000 lbs

Front 14

Operating empty weight?

Back 14

82,000 lbs

Front 15

What is the fuel capacity of the boeing 737-200?

Back 15

25,250 lbs

Front 16

How many pitot/static probes are on the front of the plane and which side?

Back 16

2 on the pilots side and 2 on co-pilots side

Front 17

What type of temperature probe is on the airplane and which side?

Back 17

Rosemont Total Air Temp probe on pilots side

Front 18

Is there an Angle of Attack vane?

Back 18

Yes on pilots side

Front 19

How many alternate static ports are there?

Back 19

there are 2. One on each side of the front of plane

Front 20

Other than the 4 pitot static tubes at the front of the airplane, are there any other pitot tubes? if so, where and why?

Back 20

Yes, 2 others, one on each side of vertical fin.
For, airspeed sensing information which delivers information to the elevator feel system

Front 21

How many nose wheel steering cylinders are there?

Back 21

2

Front 22

Are the cargo compartments ventilated??

Back 22

No, they are FAA Category Class D, not ventilated and will not support a fire

Front 23

Are the cargo compartments pressurized? If so, how?

Back 23

Yes. pressure maintained by pressure equalization valves

Front 24

What in the cargo compartments are installed to protect the aircraft in the event of a rapid decompression?

Back 24

There are blow out panels installed

Front 25

What lights illuminate in the cockpit if either cargo door is not closed?

Back 25

Master Caution lights and annunciator DOOR light

Front 26

Where is the access door for the electrical/electronics compartment?

Back 26

On the underside of the aircraft behind the nose wheel

Front 27

Behind the electrical access door on the underside of aircraft there is a port...what is it for?

Back 27

The exhaust port for the electrical equipment cooling air

Front 28

Where are the air conditioning heat exchangers located?

Back 28

One each side near wing root.

Front 29

What regulates the temperature for the air conditioning heat exchangers?

Back 29

Intake on front fairing near wing root and exhaust at rear of fairing. Automatic doors open/close to regulate temperature.

Front 30

On the leading edge of each wing there are two lights...what are they for?

Back 30

Inboard lights are Runway Turn off Lights.
Outboard lights are Landing Lights

Front 31

What engines are on the 737-200?

Back 31

Pratt and Whitney JT8D -15A Turbo fans

Front 32

How much thrust does each engine produce?

Back 32

14,500 lbs at sea level

Front 33

What type of thrust reverser system is mounted on the engines?

Back 33

Hydraulically operated "bucket-type" system on each engine

Front 34

What hydraulic system operates the thrust reverser system?

Back 34

Usually the "A" Hydraulic system, with back-up operation from the Standby Hydraulic system.

Front 35

What type of leading edge flaps are on the 737-300 and what positions do they operate in?

Back 35

Krueger Type LE Flaps mounted under-wing.
2 positions - Retract and Full Extend

Front 36

How many leading edge slats are there?

Back 36

6 total - 4 inboard and 2 outboard

Front 37

Which handle operates the LE slats?

Back 37

All operation is with the flap handle

Front 38

What positions do the LE Slats operate in?

Back 38

ALL SLATS - Retract, Extend and Full Extend

Front 39

The trailing edge flaps are operated through what system?

Back 39

Operated hydraulicaly with electric motor available for alternate flap operation

Front 40

The normal flap take off range is?

Back 40

Between 1 and 25

Front 41

Normal Flap landing selection is?

Back 41

Flaps 30 or 40

Front 42

What system powers the ailerons?

Back 42

Hydraulic system

Front 43

How many aircraft air stairs are on the airplane?

Back 43

2 - Fwd and Aft

Aft only used in Emergency

Front 44

What is the purpose for the fire extinguishers in the lavatories?

Back 44

To put out a fire in the trash containers

Front 45

How many evacuation exits are there?

Back 45

total of 6.

4 doors with evacuation slides
2 over wing exits

Front 46

Where are the manual gear extension handles?

Back 46

On the floor behind and inboard from the FO's seat.

Front 47

How many handles can you expect to see behind the door for the Manual Gear Extension?

Back 47

3 total - 1 for each gear

Front 48

When you pull a respective Manual Gear Extension handle, what does the handle do?

Back 48

Just releases the gear up locks for the individual gear you pull the handle to.

Front 49

Where is the Manual Passenger Oxygen Control handle located?

Back 49

On the floor, behind and inboard of Pilots seat (next to man. gr. ext. handles)

Front 50

When you pull the Manual Passenger Oxygen Control handle, what happens?

Back 50

Pax oxygen system will operate

Front 51

How long after pulling the Manual Passenger Oxygen Control handle do you have to push it in for to deactivate?

Back 51

Push in for 5 secs when cabin pressure below 14,000 feet will deactivate

Front 52

How many cockpit windows are there on the airplane?

Back 52

ten total

Front 53

How many cockpit jump seats are installed?

Back 53

2

Front 54

Which two blowout panels in cockpit door can be removed for emergency evac.?

Back 54

Top two panels

Front 55

When the autopilot is in use, what is the maximum;

Roll command?
Pitch command

Back 55

32 deg roll
25 deg up
10 deg down

Front 56

Can the autopilot function without any hydraulic system operational?

Back 56

NO - requires Hyd system to function

Front 57

With the Yaw Damper inop, what is the altitude restriction for the autopilot roll function?

Back 57

30,000 ft Max

Front 58

For the air conditioning system. Where does the left pack receive bleed air from?

Back 58

Left pack left engine
Right pack right engine

Front 59

Can the APU provide the A/C packs with bleed air?

Back 59

Yes, APU can provide bleed air to both at same time

Front 60

In flight can the APU still power the electrical system and a/c system if necessary?

Back 60

Yes, in flight the APU can provide power to one electrical system and one a/c pack up to 10,000 ft

Front 61

Can the APU power the a/c in flight over 10,000ft?

Back 61

Yes, it can provide power to one pack between 10,000 to 17,000 with no other electrical load

Front 62

Can the a/c packs receive bleed air from a ground source?

Back 62

Yes, they both can receive from a ground air source

Front 63

Both a/c packs supply air conditioned air to where??

Back 63

first to the Main Supply Duct

Front 64

The left a/c pack delivers air through the main supply duct to the....?

Back 64

Cockpit

Front 65

The right a/c pack delivers air through the main supply duct to the.......?

Back 65

Cabin through the right sidewall risers

Front 66

Additional or excess air not delivered to the cockpit is delivered to.....?

Back 66

Through the main duct to the cockpit and the same happens in reverse also

Front 67

What does the Gasper fan do??

Back 67

If the left pack is inop, it will draw air from the supply duct through the gasper air system

Front 68

When the gasper fan system is operating, what is it doing?

Back 68

Drawing air from right pack to the gasper overhead eyeball outlets in cabin.

Front 69

Where does most of the cabin air exhaust?

Back 69

Through the main outflow valve rear of aircraft

Front 70

There is a Forward outflow valve on the aircraft in addition to the main outflow valve, what does it do??

Back 70

Closes automatically to assist the main valve to regulate cabin pressure

Front 71

When will the Forward Outflow Valve Close

Back 71

Closes automatically when the main valve is almost closed.

2.5psid

Front 72

The turbofans in the a/c system will not operate when the aircraft is in flight and the ______?

Back 72

Wing flaps are retracted

Front 73

During normal operation in flight with the engines supplying bleed air to their respective packs, the isolation valves is?

Back 73

Closed

Front 74

Where is the APU located?

Back 74

Tail section of the aircraft

Front 75

APU inlet air is supplied for what?

Back 75

combustion and cooling

Front 76

Where is the APU inlet air door?

Back 76

right side of fuselage

Front 77

When on the ground, the APU typically supplies power to what?

Back 77

#1 and #2 Generator buses and bleed air to one a/c pack

Front 78

Between 10,000 and 17,000ft the APU can be used to power how many items?

Back 78

One electrical system OR one a/c pack

Front 79

What is the maximum altitude for APU start?

Back 79

30,000ft

Front 80

What is the maximum altitude for APU use?

Back 80

35,000ft

Front 81

Bleed air from the APU can not be used when the aircraft is above what altitude?

Back 81

17,000ft

Front 82

Fuel for the APU is supplied from which fuel tank?

Back 82

#1 (left) tank

Front 83

The APU comprises of what components?

Back 83

2 stage compressor
Turbine Drive
Accessory Gear Box

Front 84

Bleed air from the APU should not be used until the APU has run for how long?

Back 84

1 minute

Front 85

How long prior to APU shut down should bleed air finish being used

Back 85

1 minute prior to shut down

Front 86

If an overspeed occurs in the APU what happens?

Back 86

Auto shut down

Front 87

The APU will shut down when what conditions exist?

Back 87

Overspeed
Low oil pressure
High Oil Temp
APU on fire

Front 88

How are APU fuel temps maitained above freezing?

Back 88

done automatically

Front 89

The APU starting motor will not engage until the inlet door is......?

Back 89

Fully open

Front 90

What is the minimum battery voltage prior to APU start?

Back 90

22volt

Front 91

Does the battery charger continue charging the battery during APU start?

Back 91

No - the charger disconnects, and then with power will reconnect and charge the battery during APU operation

Front 92

Which fuel tank serves the APU during operation?

Back 92

Usually the left tank, but for extended operations use the center tank

Front 93

Should a boost pump be running for APU start?

Back 93

If A.C. power is available, then yes turn on one boost pump for the left tank or the center tank depending on length of intended APU use.

Front 94

Will the APU Low Oil Pressure light be on when APU starts?

Back 94

When the APU initially starts, yes it will illuminate then once it is running it should go out.

Front 95

On the Bus Transfer panel, the center GEN OFF BUS will illuminate when during APU operations?

Back 95

It will illuminate when the APU reaches 95% and then will go out once the APU generator is applied to one or both Electrical Buses.

Front 96

With the APU running, if the Battery switch is turned off what happens to the APU?

Back 96

The APU will shut down if the aircraft is on the ground.
If the aircraft is in flight, the APU will continue to operate.

Front 97

How many audio selector panels are there in the cockpit?

Back 97

3 total.

2 in between pilots on pedestal and 1 in the over head panel

Front 98

How may audio receivers can be monitored simultaneously?

Back 98

As many as desired.

Front 99

What is the flight interphone used for?

Back 99

Used to allow the ground crew to communicate to the pilots, through use of the flight jack on the external power receptacle.

Front 100

When can the cockpit voice recorder be erased?

Back 100

When the aircraft is on the ground and with the parking brake set.

Front 101

How many CSD Generators are in each engine?

Back 101

there is one Generator in each engine

Front 102

How much electrical power does each generator supply?

Back 102

3 phase
115 Volt
400 Cycle AC (alternating current)

Max load 111 amp draw

Front 103

Which electrical system is powered by which generator?

Back 103

Left system - Left Gen
Right system - Right Gen
Bus Transfer feature permits operation of all if one Gen fails.

Front 104

Will the operating Generator power all loads if the other fails?

Back 104

Yes, will power all but the heavy non-essential loads

Front 105

Does the APU generator operate like the engine generators?

Back 105

Yes they are identical

Front 106

When the aircraft is on the ground the APU can power which electrical systems?

Back 106

Can power both the #1 and #2 electrical systems.

Front 107

Can the APU power both electrical systems in flight?

Back 107

No only one

Front 108

Is there a time where both engine generators can power the same electrical system?

Back 108

No

Front 109

The installed generators are referred to as CSD Generators.... what does this mean and why?

Back 109

Constant Speed Drive

No matter the engine RPM the generators operate the same speed/power

Front 110

The gear drive system of the CSD is connected to which part of the engine?

Back 110

N2 shaft

Front 111

Do the CSD's use oil from the engine?

Back 111

No they have their own oil reservoir and oil cooler

Front 112

If the CSD's experience high oil temps, what lights on what panels are observed?

Back 112

High Oil Temp - on CSD panel
Master Caution Light
Amber ELEC light on annun. panel

Front 113

On the CSD panel, the temp gauges show "Rise" and "In" temps, what do they mean?

Back 113

Rise - Differential between temp of CSD outlet and Inlet

In - Oil entering CSD

Front 114

The Max permitted Oil Temp in the CSD is?

Back 114

157 deg C

Front 115

How is CSD oil cooled?

Back 115

Engine Fan airflow

Front 116

High CSD "Rise" temps usually indicate what?

Back 116

The need for oil servicing in that CSD.

Front 117

If the High Oil Temp light illuminates on either CSD, what is the correct action?

Back 117

Disconnect the affected CSD

Front 118

When can you re-connect a CSD that a pilot has disconnected?

Back 118

Can only be re-connected by maintenance.

Front 119

The normal position for the CSD drive temp switch is...?

Back 119

The "In" position.

Front 120

The 111amp generator limit applies when the aircraft is on the ground or in flight?

Back 120

The limit applies to both

Front 121

What happens to the GEN OFF BUS lights when the respective generators are placed online?

Back 121

The GEN OFF BUS lights should go out

Front 122

The generators in each engine power their respective generator buses, which in turn power what?

Back 122

Power their respective main buses.

In addition the Gen Bus 1 powers the ground service bus

Front 123

If during normal operations, the generator 2 is disconnected for some reason, what happens to that bus and it's equipment?

Back 123

The Gen 1 bus will power the number 2 bus through the transfer system if the switch is in AUTO, all systems should operate normally

Front 124

What reasons will cause a generator to trip offline?

Back 124

High current draw
Electrical grounding
incorrect voltage/frequency

Front 125

What are the APU Generator load limits on the ground and in flight?

Back 125

Ground - 125 amps
Flight - 111 amps

Front 126

Do the engine generators come online aurtomatically when the engines have been started??

Back 126

No - they have to manually be turned on

Front 127

The APU GEN OFF BUS light is illuminated when??

Back 127

When the APU is running but not supplying generator power to anything.

Front 128

If during normal operations, you lose a generator, the transfer bus automatically picks up the load on the operating generator, what will happen to the Galley Power in the aircraft? Why?

Back 128

The Galley Power is automatically shed as it is non-essential
It reduces the load on the operating generator.

Front 129

What other auto load shedding functions happen when you lose a generator, other than the galley power?

Back 129

One of the B Hydraulic System pumps will automatically shut down. If there is only one running it will continue to run on the power of the remaining generator.

Front 130

The aircraft battery charger is powered by what bus? What happens if this bus fails?

Back 130

Normally powered by the Ground Service Bus (Gen Bus #1)
If this fails and the #1 transfer bus is running, then the battery charger is powered by the #2 main bus

Front 131

What light illuminates in the cockpit when the external power is plugged in?

Back 131

GRD POWER AVAILABLE

Front 132

Which electrical systems can be powered by the GRND POWER?

Back 132

Both Electrical systems can be powered.

Front 133

When you arrive at the gate, with both generators operating normal, ground power is plugged in, you verify good power. What will happen if you switch the ground power on before disconnecting generators?

Back 133

This is normal procedure, both engine generators will automatically go offline once ground power is turned on. At this time you can switch off GEN's prior to engine shut down

Front 134

The Ground Service Switch that is located in the Forward Galley supplies power to what?

Back 134

Cabin Lights
Utility outlets

Front 135

When there is no ground power source entered in to the aircraft or Gen Bus 1 is offline, when you select the Ground Service Switch to the ON position, what will happen?

Back 135

With no power, the switch will be magnetically held in the ON position until power is provided then it will snap to the OFF position when electrical power is given. This allows use of ground service items.

Front 136

If during start up, either engine generators are brought online, what will happen to the External Power?

Back 136

It will kick offline, in the reverse of what happens when you plug in external power during the shut down sequence.

Front 137

The aircraft generators and APU Gen provide A.C power to the aircraft, how do we get D.C. power?

Back 137

The battery can provide DC power.

There are 3 Transformer Rectifiers (TR's)

Front 138

Transformer Rectifiers T.R. #1, #2 and #3 are powered by what bus' on the a.c. elec system?

Back 138

TR 1 - Transfer Bus 1

TR 2 - Transfer Bus 2

TR 3 - Main Bus # 2

Front 139

Is there any back up in the DC electrical system?

Back 139

TR #3 will provide back up 28 volt power to TR 1 and 2 along with powering the Battery Bus

Front 140

In the event of a generator failure, with the BUS TIE switch to AUTO, allowing the crossfeed of power through the AC elec system, what else happens to aid the continuation of power to all DC systems?

Back 140

There is a disconnect relay, which will also automatically close to allow TR #3 to power TR #1 if it is not producing power (failed)

Front 141

What type of battery is in the aircraft?

Back 141

28 Volt
Nickel Cadmium

Front 142

How long can the aircraft battery supply standby DC power?

Back 142

for roughly 30 mins on a fully charged battery

Front 143

What buses does the Battery supply DC power to?

Back 143

The;
Hot Battery Bus
Battery Bus
APU Start Circuit

Front 144

During normal operations, the Standby Power Switch is in the AUTO position, if the aircraft loses power what extra bus will the battery supply power to?

Back 144

The DC Standby Power bus will be supplied power also, if the aircraft is in the air.

Front 145

When in flight, if the aircraft loses power, with the battery supplying power to the DC Standby Power bus, what else does this bus supply power to?

Back 145

Will supply power to the static inverter which in turn supplies power to the AC Standby Power bus.

Front 146

The DC External Bus is powered through the Hot Battery Bus, what elements does this external bus power?

Back 146

Powers the fueling valves

Front 147

What is the purpose of connecting External DC Power?

Back 147

To power the fueling valves and/or to start the APU when the battery is discharged.

Front 148

How does the Battery Charger work?

Back 148

Gets power from the Ground Service Bus which is A.C. powered, it converts 115 a.c. power to 28 volt DC power and then delivers it to the battery to charge.

Front 149

How do you operate the Battery Charger?

Back 149

It is all automatic

Front 150

The Battery Bus is normally powered by TR #3 from the Main Bus #2. If the TR #3 is not powered then the Battery Bus is then powered by the....?

Back 150

Hot Battery Bus.

Front 151

When operating using only standby power, what is powered?

Back 151

Captains - Primary Flight Inst's

Captains - Comms Radio

Captains - Navigation Radio

Front 152

If the aircraft is on the ground, can the standby buses be powered automatically?

Back 152

No they can't even with the Standby Power switch in AUTO

Front 153

With the aircraft in flight and the Standby Power switch in the AUTO position, no power on the # 1 Transfer Bus. The AC Standby bus is powered by what?

Back 153

The Inverter which is powered by the battery bus.

Front 154

With the aircraft in flight and the Standby Power switch in the AUTO position, no power on the # 1 DC BUS. The DC Standby Bus is powered by what?

Back 154

The Battery Bus

Front 155

The Standby Power Off light monitors the status of the....?

Back 155

AC and DC Standby buses

Front 156

On the amperage display in the cockpit, a typical TR amps should indicate what??

Back 156

Slight positive up to the max 65 amps

Front 157

A zero reading on the amps display in the cockpit when a TR is selected indicates what?

Back 157

That there is some sort of malfunction in that TR

Front 158

Name all instruments that are powered by the standby battery power when the aircraft is in flight?

Back 158

Captains;
ADI
HSI
ALT
VSI

Standby Horizon

FO's;
IAS
ALT
VSI

Front 159

For fire protection, an upper and lower detection loop is installed in each engine nacelle for what conditions?

Back 159

Overheat and Fire

Front 160

Power for the overheating and fire detection elements in the engine nacelles is provided by the...?

Back 160

Battery bus

Front 161

Can the aircraft be dispatched if the engine nacelle fire detection loops do not test properly??

Back 161

Yes - the pilot can select the Over heat detector loop for fire protection

Front 162

If in the event of a Fire Detection Loop failure, what can be used as a back up?

Back 162

The Overheat Detection Loops

Front 163

The engine nacelle Overheat Detection loops activate at approx what temp?

Back 163

410 Deg F

Front 164

The engine nacelle Fire Detection loops activate at approx. what temp?

Back 164

600 Deg F

Front 165

Is there any fire detection in the APU?

Back 165

Yes

Front 166

The Fire Detection loop in the APU will alarm when the temp reaches?

Back 166

385 Deg F

Front 167

Other than the engine nacelles and the APU, where else is there fire detection?

Back 167

In the Main wheel wells

Front 168

What powers the APU Fire detection?

Back 168

Battery Bus

Front 169

What powers the wheel well fire detection?

Back 169

115 Volt AC Transfer Bus #1

Front 170

How many Fire Agent Bottles are provided for the engine fire protection?

Back 170

Two Freon Bottles are installed, agent can be routed to each or both engines through shuttle valves.

Front 171

The engine fire protection bottle squibs are powered by??

Back 171

Hot Battery Bus - can gain power in an elec failure

Front 172

How many agent bottles are provided for APU fire protection?

Back 172

There is 1 Freon bottle for the APU.

Pressure gauge on right side of aircraft

Front 173

At the right side tail of aircraft, there is a red disk and a yellow disk, these are part of the APU fire protection system, what do they mean?

Back 173

Red disk - will blow out if the freon bottle is discharged for over pressure or over heat

Yellow Disk - will blow out if freon bottle is manually discharged

Front 174

There is an APU ground control panel on the 737, where is it?

Back 174

Right wheel well

Front 175

If the aircraft is on the ground and the APU detects fire, what will be noticed on the Ground control panel?

Back 175

Red light will flash and horn will sound

Front 176

Can the APU be shut down in the event of a fire from the ground control panel?

Back 176

Yes, you can activate the bottle discharge and discharge the bottle from the GCP, these actions will shut down the fuel flow thus shut down the APU

Front 177

What actual actions occur when the APU Fire Control Handle is pulled down on the Ground Control Panel?

Back 177

Fuel Shut off
Bleed Air Shut off
Inlet Door Close
Gen. Control Relay Tripped
Gen Breaker Tripped
Arms Bottle Discharge Switch

Front 178

In the cockpit, where are the fire detection/protection control handles located?

Back 178

Aft electronics panel rear of the throttle quadrant

Front 179

In the cockpit, on the fire protection control panel, the two switches for the OVERHEAT DETECTION have two positions - what are they for?

Back 179

NORM - The overheat detection loops will trigger the ENG OVHT lights on the panel

FIRE - The overheat detection loops will activate a fire warning

Front 180

The fire warning switched on the protection panel will unlock automatically when what conditions occur?

Back 180

If the detection loops sense an overheat or a fire condition in the ENGINES.

Only unlock for a fire in the APU

Front 181

What happens when a pilot pulls on an Engine Fire Warning Switch Handle??

Back 181

F - fuel shutoff valve close
E - engine driven hydraulic pump shutoff valve close
L - low pressure light for hyd pump deactivated
T - thrust reverser isolation valve close
B -bleed valve close
A - arms fire extinguishing circuit
G - generator breaker and field relay trip

Front 182

When you pull up on a Fire Warning Switch and the rotate it to the left or right what is the difference?

Back 182

Rotating to left fires left discharge bottle and right is the right bottle. You can fire both bottle to same engine if required.

For the APU, either direction fires the one and only bottle

Front 183

What indications are displayed if there is a fire in the main wheel well.

Back 183

Wheel Well Light, on the Fire control panel
Master Warning Light.
Warning Bell sounds

Front 184

During normal cruise flight, the Master Caution light Illuminates and the Eng 2 Overheat light also illuminates. You cancel the Caution light, so it goes out, what will happen to the OVHT light?

Back 184

It will remain illuminated until the Temperature in the nacelle drops below the

Front 185

When testing the overheat and fire detection system, what lights will illuminate for the;
Overheat test??
Fire test??

Back 185

Overheat test - All amber lights

Fire test - Only 6 red lights illuminate

Front 186

The electrical power supply for the engine overheat and fire detection system and the APU Fire detection is supplied from?

Back 186

The 28 Volt DC Battery Bus

Front 187

The discharge squibs for the fire suppressant agent bottles for engines and APU are powered by?

Back 187

28 Volt DC Hot Battery Bus

Front 188

Where are the fire extinguishers placed in the lavatory?

Back 188

Small ones under the wash basins

Front 189

The fire extinguishers in the lavatories are positioned in such a fashion to put out small fires in??

Back 189

the trash can or underneath the sink area.

Front 190

How do you know when inspecting the fire extinguisher in the lavatory if it has been discharged or not?

Back 190

If it has been discharged the nozzle end will be aluminum colored.

Front 191

What Hydraulic system powers the:

Inboard flight spoilers

Back 191

A system

Front 192

What Hydraulic system powers the:

Ground Spoiler

Back 192

A system

Front 193

What Hydraulic system powers the:

Trailing Edge Flaps

Back 193

A system

Front 194

What Hydraulic system powers the:

Landing Gear

Back 194

A System

Front 195

What Hydraulic system powers the:

Thrust Reversers

Back 195

A System

Front 196

What Hydraulic system powers the:

Nose Wheel Steering

Back 196

A System

Front 197

What Hydraulic system powers the:

Inboard Manual Brakes

Back 197

A System

Front 198

What Hydraulic system powers the:

Outboard Flight Spoilers

Back 198

B System

Front 199

What Hydraulic system powers the:

Outboard Manual Brakes

Back 199

B System

Front 200

What Hydraulic system powers the:

Leading Edge Devices

Back 200

A system with back up from the standby system

Front 201

What is installed on the aircraft to assist the movement of the ailerons?

Back 201

Balance Tabs

Front 202

What Hydraulic system powers the:

Ailerons

Back 202

Both the A and B System, if one fails then the normal ops can performed with only one

Front 203

What Hydraulic system powers the:

Elevators

Back 203

Both the A and B System, if one fails then normal ops can be performed with only one

Front 204

What Hydraulic system powers the:

Rudder

Back 204

Both the A and B system, and also an extra back up from the standby system

Front 205

If both hydraulic systems fail, is there any manual reversion available?

Back 205

Yes

Front 206

When a roll command is performed by either pilot, when more than 10 deg of the control wheel is moved, what happens?

Back 206

Flight Spoilers will rise to enhance roll input (downward wing)

Front 207

Can the elevators operate without any hydraulic pressure??

Back 207

Yes manually

Front 208

What operates the elevators in the upward position?

Back 208

The Mach Trim Computer to prevent Mach Tuck tendencies

Front 209

What is used to adjust the horizontal stabilizer on the aircraft?

Back 209

Either the main electric trim or the autopilot trim or the manual trim wheel

Front 210

When discussing the trim systems for the Horiz. Stab. can the electric trims and manual trim travel the same range?

Back 210

No the manual trim has more range than the electric trim

Front 211

If the A hydraulic system fails, can the T.E. Flaps be placed down?

Back 211

Yes they can with the aid of an electric motor

Front 212

T.E Flaps must not be extended when above what altitude?

Back 212

FL 200

Front 213

If the A hydraulic system fails, can the LE Flaps be used??

Back 213

Yes the standby hyd. system will provide pressure

Front 214

How many positions do the leading edge slats have (adv ac)

Back 214

Three positions;
Retract
Extend
Full Extend

Front 215

If the A hydraulic system fails can the LE SLATS be used?

Back 215

Yes, the standby system can provide pressure

Front 216

The LE SLATS are operated through what handle?

Back 216

The Flap Handle

Front 217

The LE Slats will not move past the extend position until the TE Flaps move beyond what position?

Back 217

Flaps 5

Front 218

The Leading Edge Flaps will extend fully when the TE flaps do what?

Back 218

Leave the UP position

Front 219

Is hydraulic pressure required for Aileron trim operation?

Back 219

Yes

Front 220

If the captains control wheel becomes jammed, can the FO's control wheel be moved? Is there roll control available?

Back 220

Yes it can be operated

Roll control is available through the spoiler mixing system

Front 221

Is spoiler mixing for aileron control available with the loss of both hydraulic systems?

Back 221

No - not available

Front 222

With failure of both hydraulic systems, can the elevators still function?

Back 222

Yes, through manual reversion.
Balance tabs unlock when the hyd. systems fail to assist elevator control

Front 223

What is the purpose of the elevator feel system?

Back 223

It is to provide different pressure for the pilots on the control wheel depending on aircraft speed to avoid over pitching and mach tuck.

Front 224

Where does the elevator feel system receive its inputs from?

Back 224

The two pitot probes on the vertical Stab
Both Hydraulic systems
Horizontal stabilizer position sensors

Front 225

What does the FEEL DIFF PRESS light mean when illuminated on the hydraulic control panel?

Back 225

Means the system is sensing different or inaccurate feel on the elevator system.

Front 226

When the FEEL DIFF PRESS light illuminates indicating a problem, what other lights will illuminate in the cockpit?

Back 226

Both Master Caution Lights

Flight Cont light on Annunciator

Front 227

Describe Mach Tuck? What does it mean?

Back 227

It's the pitch down tendency of swept wing aircraft flown at high speeds

Front 228

The mach trim system will begin to move the elevators above when the aircraft flies above what speed?

Back 228

Mach 0.715

Front 229

What is the maximum airspeed when the mach trim system fails?

Back 229

Mach 0.740

Front 230

What is the purpose of the trim brake system?

Back 230

It allows the pilot to arrest a trim runaway situation

Front 231

How does the pilot reset the trim brake once it has been placed on by the pilot?

Back 231

Two methods to reset...

Electric trim in the opposite direction to the initial runaway

Pull the STAB BRAKE RELEASE PULL knob

Front 232

Can all trim systems operate in the same range for the elevator trim system?

Back 232

No -

Main trim - entire range
Autopilot trim - 2.3 - 13.0
Electric Trim - 2.8 - 12.5

Front 233

Is the standby hydraulic system automatic or does it need to be manually operated by the pilot?

Back 233

Manual operated to turn pump on.

Front 234

What is the Yam Damper system primarily for?

Back 234

To avoid the tendency to dutch roll while in flight

Front 235

Which hydraulic system does the Yaw Damper system use?

Back 235

B system

Front 236

During taxi check of the yaw damp system, what is the pilot looking for?

Back 236

When the pilot pushes down on one rudder pedal the yaw damp gauge should show an opposite correcting indication

Front 237

The flight spoiler handle placed in the FLIGHT DETENT position allows for deployment of ? degrees?

Back 237

25 degrees?

Front 238

The flight spoiler handle placed in the UP DETENT position allows for deployment of ? degrees?

Back 238

40 Degrees

Front 239

Is the Speedbrake handle permitted to the UP position in flight?

Back 239

No

Front 240

When looking at the aircraft from above, which panels of the flight spoiler system are the flight spoilers and which panels are the ground spoilers only

Back 240

The 2 furthest outboard and inboard are the GROUND ONLY

The 2 panels on each wing that are in the middle are the FLIGHT

Front 241

The Ground Spoiler Shutoff Valve will only open when..?

Back 241

There is weight on the Right Main landing gear.

Front 242

With the speedbrake lever in the ARMED position, what happens?

Back 242

Speed Brake lever will automatically move to the UP position from ARMED when?

-Throttles are closed and main wheels have spun up
- No wheel spin up sensed and squat switched sense on grnd
-

Front 243

What is the maximum speed allowed for Landing Gear Extension?

Back 243

270kts / 0.82m

Front 244

What is the maximum speed allowed for Landing Gear Retraction?

Back 244

235 kts

Front 245

What is the maximum speed allowed for flight with the Landing Gear Extended?

Back 245

320 kts / 0.82m

Front 246

What is the maximum speed allowed for Alternate Flap Extension?

Back 246

210 kts

Front 247

What are the flap speed limits for flap setings...
1-
2-
5-
10-

Back 247

1- 230k
2- 230k
5- 225k
10- 210k

Front 248

What are the flap speed limits for flap setings...
15-
25-
30-
40-

Back 248

15- 195k
25- 190k
30- 185k
40- 170k

Front 249

The normal two engine go-around flap position is

Back 249

Flaps 15

Front 250

Single Engine Flap setting for Landing is?

Back 250

Flaps 15

Front 251

The flap setting for a single engine go-around is?

Back 251

Flaps 1

Front 252

What does the Flap Bypass Valve do on the flap system?

Back 252

A comparator switch will close the bypass valve if the flaps become split.

Front 253

After one complete cycle of the alternate (electric) flap system, how long to wait prior to next usage?

Back 253

25 mins

Front 254

If in flight with the flaps selected to flaps 40 and the airspeed exceeds 158 kts, what will happen?

Back 254

The flaps will automatically raise to Flaps 30

Front 255

Will the flap load relief system function with the loss of hydraulic pressure or if the flaps have been selected to position with the electric motor?

Back 255

No the Flap relief system will not function in either of these cases

Front 256

The flap load relief system has raised the flaps to 30 since the airspeed exceeded 158 kts, what speed will the aircraft need to be reduced to in order to automatically lower the flaps again

Back 256

Below 152 kts.

Front 257

The LE Flaps will extend fully at what point?

Back 257

When ever the Trailing Edge Flaps leave the up position - Flaps 1 or higher setting

Front 258

When and what positions do the LE SLATS move??

Back 258

All LE Slats move to intermediate Extend when flaps are selected between 1 and 5

LE Slats move to Full Extend when the flaps are selected to more than flaps 5

Front 259

What is the max speed permitted with the outboard landing lights extended

Back 259

They have no speed restriction

Front 260

How many exterior escape route lights are on the aircraft?

Back 260

8

Front 261

How long will the emergency exit light battery packs last?

Back 261

20 mins

Front 262

Can the aircraft dispatch without the stall warning heat testing properly?

Back 262

No, can not be dispatched.

Front 263

Where is the Flight Crew emergency oxygen bottle located and how much does it hold?

Back 263

Fwd cargo compartment, right side

39 cu ft of oxygen

Front 264

Where is the Passengers emergency oxygen bottle located and how much does it hold?

Back 264

Fwd cargo compartment, right side

114 cu ft of oxygen

Front 265

At what altitude does the cabin pressure need to be at for the oxygen system to force 100% pure oxygen to pilots masks no matter what the selection of the switches?

Back 265

Above 28,000 ft

Front 266

Will the crew oxygen bottle pressure display on the overhead oxygen panel, if the crew oxygen shut off valve is closed?

Back 266

Yes

Front 267

When will the PASS OXY ON Light go out if the system is supplying pressure?

Back 267

When the cabin pressure drops below 14,000ft

Front 268

What makes the oxygen masks drop from the overhead in the PSU's?

Back 268

Once cabin pressure reaches above 14,000ft, a pressure surge forces the masks out automatically

Front 269

Can the pilot manually operate the passenger oxygen?

Back 269

Yes, electric switch on the over head panel will pressurize the system or there is a manual handle on the floor rear of captain seat, pull to activate.

Front 270

If the pilot wishes to shut off the oxygen supply with the manual handle, what will he need to do?

Back 270

push and hold manual handle in for 5 seconds to stop flow.

Front 271

How many masks can be connected to the portable oxygen bottle?

Back 271

2

Front 272

What is the typical fuel full quantities for each tank.
Left -
Right -
Center -

Back 272

Left - 10,120
Right - 10,120
Center - 5010

Front 273

Is suction feed from the center fuel tank possible?

Back 273

No

Front 274

Is suction feed from the left and right tank possible?

Back 274

Yes, left tank to left engine and right tank to right engine

Front 275

Can the APU receive fuel from the right fuel tank?

Back 275

Yes, but only if the crossfeed valve is open.

Front 276

How many AC boost pumps are there in each fuel tank?

Back 276

2 in each so 6 total.

Front 277

How many fuel pressure sensors are there total in the fuel system?

Back 277

6 total, 1 after each fuel pump

Front 278

Engine fuel shut off valves are powered from what electrical bus?

Back 278

Hot battery bus

Front 279

Can the APU suction feed fuel?

Back 279

Yes from the left tank only

Front 280

Can one boost pump, supply enough fuel pressure to both engines?

Back 280

Yes

Front 281

If all the boost pumps were running (6) and the crossfeed valve is closed, will the engines draw fuel from the wings first or the center tank? - Why?

Back 281

Fuel will burn from the center tank first because the check valves open at a lower pressure than the wing tank valves.

Front 282

Are both AC boost pumps in each engine supplied from the same electric bus?

Back 282

No they are powered by separate buses in case one fails.

Front 283

If a FILTER ICING light illuminates on the fuel panel, what is the appropriate action?

Back 283

Turn on the fuel heat

Front 284

What is used to heat the fuel?

Back 284

13th stage bleed air

Front 285

Does the fuel heat remain on for entire operations?

Back 285

No only comes on when required. Solenoid holds switch on for 1 minute and auto shuts off

Front 286

Describe basic operation of fuel balancing process. what switches to switch etc

Back 286

Open crossfeed valve. turn off boost pumps on lighter side of fuel and heavier side will supply both engines

Front 287

What is the maximum acceptable fuel imbalance permitted during....

Taxi/TO and flight?
With center tank fuel?
landing

Back 287

1500 lbs for taxi, t/o and flight

1300 lbs for landing

If center tank has more than 100lbs on ground wings must be full

Front 288

On the fuel panel, when do the FUEL VALVE CLOSED lights illuminate?

Back 288

When the pilot moves the engine start levers to cutoff.

Front 289

Single point refueling is accomplished on which side of plane? all tanks??

Back 289

right side

yes all tanks

Front 290

Can any fuel be gravity fed to the plane?

Back 290

Ye the wings can receive gravity fuel.

Center tank can not, has to be transferred in to this tank

Front 291

Which boost pumps provide pressure to the de-fueling valves when trying to transfer fuel between tanks?

Back 291

Either of the # 2 pumps or the right pump in center tank

Front 292

explain the basic process to transfer fuel from #1 tank to the center tank?

Back 292

Turn on either boost pump in #1 tank
Open fuel cross-feed valve
Open engine #2 shut off valve
Open De-fueling valve
Open center tank fill valve

Front 293

Can fuel transfer between tanks be done in the air?

Back 293

No can only be done on the ground as it required operation from outside the aircraft under right wing leading edge

Front 294

Can the APU receive fuel from tank #2?

Back 294

Yes but only if the cross-feed valve is open and a #2 boost pump is running

Front 295

How many fuel drip sticks are installed on the aircraft?

Back 295

10 total

5 on each wing tank

Front 296

What are the fuel drip sticks for??

Back 296

Used to compare remaining fuel on the displays for accuracy.

Front 297

What pressurizes the hydraulic system?

Back 297

Engine bleed air pressurizes A system
2 Electric pumps Pressurize B system
1 Electric pump Standby system

Front 298

What does the balance line do on the hydraulic system?

Back 298

Interconnected between all hyd. reservoirs. to allow even pressure throughout all systems and maintain correct quantity

Front 299

How many hydraulic quantity gauges are there in cockpit?

Back 299

1 gauge for A system
1 low light only for B and Stby system

Front 300

The hydraulic pressure gauges in the cockpit display pressure for which systems?

Back 300

A and B

Front 301

When can the hydraulic ground interconnect be used?

Back 301

Only on ground when brakes set

Front 302

How much pressure do the hydraulic pumps usually put out?

Back 302

approx 3000 psi each

Front 303

The purpose of the ground interconnect switch is what??

Back 303

To inter-connect the A and B hydraulic systems when on the ground. (electric pumps running and not engine bleed air)

Front 304

How much hydraulic fluid is in the A reservoir

Back 304

3.5 gals

Front 305

Where are the hydraulic system reservoirs located?

Back 305

Wheel well

Front 306

If the B hydraulic system leaks and empties, will this issue also drain the A system as it feeds fluid through the balance line?

Back 306

It will only drain to the stand pipe but no furher

Front 307

What lubricates the pumps on the hydraulic system?

Back 307

Fluid from the respective system will lubricate and cool their respective pumps

Front 308

The OVERHEAT lights on the hydraulic control panel are only associated to what part of the system?

Back 308

Only associated to the temp of fluid in the pumps

Front 309

What is the main purpose of the Ground Interconnect switch other than knowing it connects the two systems?? Why do pilots need it??

Back 309

It allows pilots to test all of the hydraulically operated components prior to flight. Using the electric pumps in B system to power everything to test

Front 310

What switches power the standby hyd. pump?

Back 310

Either of the FLT CONT switches to the STBY RUD position or the ALT FLAP to the ARM position will power the pump

Front 311

The standby hydraulic system can pressurize what components?

Back 311

The Rudder, LE Devices and thrust reversers

Front 312

When using standby power, how long will the standby horizon be powered for?

Back 312

30 mins

Front 313

How long does it take the standby horizon to initialize?

Back 313

60 secs

Front 314

How many of the cockpit windows are heated?

Back 314

4 of the 5 each side. The rear most window is not

Front 315

When the window heat is on, does it stay on for the whole time or does it cycle?

Back 315

cycles on and off based upon temp. at 100ºF they shut off

Front 316

At what temp does the window OVERHEAT light come on?

Back 316

145ºF

Front 317

Are there any speed limitation placed on whether the window heat does not operate?

Back 317

Yes, 250 below 10,000.

Front 318

Is overheat protection available when testing the window heat?

Back 318

Yes still available

Front 319

After testing window overheat, does the system need to be reset?

Back 319

yes all four individual switches need to be reset by pilot

Front 320

Are the alternate static ports heated?

Back 320

no don't need

Front 321

The AOA is heated, is there a switch or is it automated?

Back 321

Auto

Heated when engine #1 N2 power at or above 40%

Front 322

What parts of each engine are heated? How?

Back 322

The engine cowling - 13th stage bleed air

The Fan shroud, Inlet guide Vanes and bullet - 8th Stage bleed air

Front 323

Are the leading edge flaps heated?

Back 323

No only other LE devices

Front 324

Are the LE slats heated when extended?

Back 324

Yes, telescopic ducts continue to provide heat when extended

Front 325

Does the tail of the aircraft have ice protection?

Back 325

No doesn't have anything

Front 326

Can the wings and engines receive thermal anti icing while on the ground and in flight?

Back 326

Engines - yes both

Wings - only in air, squat switch right main closes valve when on grd

Front 327

The wing over heat sensors will shut off the anti ice valve at what temp?

Back 327

93ºC

Front 328

If the L VALVE OPEN light on the wing anti ice system remains bright and does not dim, what does this mean?

Back 328

That the valve position does not agree with the switch position.

Same for all valve type lights on the plane

Front 329

Rain repellant liquid should only be used in what conditions?

Back 329

Moderate to heavy rain

Front 330

How many positions on the landing gear lever?

Back 330

3
up down off

Front 331

The normal position of the landing gear lever in flight is?

Back 331

Off position

Front 332

How much steering of the nosewheel can be done through the rudder pedals?

Back 332

approx 7 deg

Front 333

Normal nose wheel steering is done by?

Back 333

Tiller on captains side

Front 334

What do the wheel well seals do? supplied air from?

Back 334

They form a seal around wheel for flight.
Engine bleed air supplies air

Front 335

How is the gear held up?? Pressure?

Back 335

Not pressure UPLOCK HOOKS for Main and Over Center link for Nose wheel

Front 336

Can the gear handle be moved up when plane on ground?

Back 336

No squat switch on right main activates a handle lock to prevent accidental movement

Front 337

After the gear is raised, how long should pilot wait to move handle to off position?

Back 337

min 10 secs

Front 338

Moving gear handle to off position does what?

Back 338

removes hydraulic pressure from gear system

Front 339

How are the gear held down?

Back 339

Mechanically and also hyd pressure

Front 340

When using the manual gear extension, what position should the gear handle be in?

Back 340

The OFF position

Front 341

When the aircraft is being towed should the A hydraulic system be on or off?

Back 341

Should be OFF

Front 342

Is brake pressure available in the event of a total hydraulic pressure failure?

Back 342

Yes, accumulators help provide pressure.

Front 343

Basically - how does the anti-skid system operate?

Back 343

Transducers provide signals to the anti-skid system which control pressure applied to avoid skidding

Front 344

Is touchdown anti-skid available?

Back 344

Yes

Front 345

The Pneumatic System supplies bleed air to what systems?

Back 345

Air Conditioning
Wing Anti Ice
Engine Starting

Front 346

The pneumatic system is supplied compressed air from?

Back 346

either the:
engines
APU or a ground source

Front 347

Once the engine is running 8th stage bleed air is available - what other bleed air is used to assist?

Back 347

13th stage is also available when valve is opened

Front 348

The bleed air isolation valve normally operates in the _____ position?

Back 348

Auto

Front 349

Bleed air cooling is provided by? regulated how?

Back 349

Engine fan air - temp regulated automatically

Front 350

If on continued operation the Bleed Air is just too hot, what happens?

Back 350

A TEMP sensor will close the bleed valve and activate the Bleed Trip Off light

Front 351

There are 2 pneumatic packs, left and right. What supplies air to each pack not discussing the isolation valve?

Back 351

Left engine and APU supply to left pack

Right engine and ground supply to right pack

Front 352

With the pneumatic isolation valve in the AUTO position, the valve will remain open until when??

Back 352

Until both engine bleed air switches are on and both pack switches are also on

Front 353

The DUAL BLEED light comes on for what reason?

Back 353

If the #1 bleed air valve is open and APU valve is open. Problem could cause back pressure to APU system

Will also occur with APU and #2 on if isolation valve open

Front 354

Is it normal at any time to see the DUAL BLEED light come on?

Back 354

Yes after start up while turning on one system and turning off another

Front 355

With the DUAL BLEED light on the engine thrust should be at?

Back 355

Idle

Front 356

The WING BODY OVERHEAT lights come on if there is what problem?

Back 356

Bleed air leak

Front 357

Are the left and right packs on or off for engine start?

Back 357

both off so APU air is used for engine start

Front 358

Are the engine bleed air switches on or off for engine start?

Back 358

both on

Front 359

What is the minimum air pressure required for engine start?

Back 359

30 psi

can decrease 1/2 psi per 1000ft elevation

Front 360

Can the pilots set up the bleed air system to provide more engine power for take off if required??

Back 360

Yes turning off engine bleed air and using APU bleed air for the ac packs will do this

Front 361

What items are in the engine accessory compartment?

Back 361

Fuel Pump
Engine Starter
Oil Pump
CSD and Generator
Tachometer
Engine Driven Hyd pumps

Front 362

When the pilot activates the starter what happens?

Back 362

It initially rotates the N2 spool

Front 363

Which engine spool is referred to as the free spool?

Back 363

the N1

Front 364

What cools the oil in the oil cooler?

Back 364

Cold fuel that passes thru the fuel/oil cooler

Front 365

What draws the oil back to the tank through the return line?

Back 365

Scavenge pump

Front 366

The main engine fuel shut off valve is open/closed by what items?

Back 366

If engine fire switch pulled (closes)

Engine start level (open/close)

Front 367

If the fuel filter is clogged with ice, does it starve the engine of fuel?

Back 367

No the fuel can automatically bypass until the filter is heated by 13th stage bleed air

Front 368

From the tank electric boost pumps the fuel then goes to _____. If open the fuel then goes to _____. This pump is driven by____? Fuel then goes to _____, then finally to ____?

Back 368

Main shut off valve
First stage engine driven fuel pump
N2 shaft
2nd stage engine pump
Engine nozzles

Front 369

What does EPR mean?

Back 369

Exhaust
Gas
Pressure

Front 370

What source powers these gauges?
EPR
N1/N2
EGT
Fuel flow

Back 370

EPR - Electric power
N1/N2 - self powered (tachometer)
EGT - self powered (thermocoupler)
FF - Elec power

Front 371

Normal oil quantity is?

Which oil tank holds .5 gals more oil

Back 371

3.5 - 4 gals

#1 hold slightly more (dihedral)

Front 372

The max take off, climb and cruise thrust settings are derived from the?

Back 372

Performance Management System

Front 373

We know that the aircraft thrust reverser's aren't usable in flight, but what makes them unusable on the ground?

Back 373

If the engine oil is low or if the fire handle is pulled on a particular engine, then that reverser will not operate

Front 374

If we lose the A hydraulic system, is there any way to use the thrust reverser system?

Back 374

There is a hydraulic accumulator that can provide limited usage yes

Front 375

The thrust reverser isolation valve fails to the ____ position with the loss of electrical power?

Back 375

Close position

Front 376

What is the minimum N2 for pilot to raise the start lever?

Back 376

15% min
Normal 20%

Front 377

To start the engine what happens???
APU is running and bleed air supplied at min___? Pilot Selects GRD to open starter valve, Bleed air spins____, at a minimum of ___%...pilot moves starter switch to____. Pilot releases start switch at ___% N2

Back 377

30psi
N2
15
idle to light off
35-40

Front 378

On the starter switch the FLT position is for?

Back 378

Used if necessary to re-start an engine in flight

Front 379

The electronic pressurization controller controls pressure by doing what?

Back 379

opening and closing outflow valves.

Front 380

Sea level pressure can be maintained in the cabin up to what altitude?

Back 380

18,000ft

Front 381

When in cruise flight, what pressure is the cabin altitude at?

Back 381

8000 ft

Front 382

The outflow valves are powered by?

Back 382

normal electric power

Front 383

What is the negative pressure relief valve for?

Back 383

prevents excess pressure on the outside of aircraft. If rapid descent happens and pressurization isn't set correctly this valve will equalize pressure

Front 384

Max cabin pressure differential is?

Back 384

8,65 psid

Front 385

What is the pressure differential limit for take off and landing?

Back 385

.125 psid

Front 386

When the OFF SCHED DESCENT light illuminates on the pressurization panel what does this mean.

Back 386

The plane never came within 1000ft of selected cruise altitude and started descending, so the system begins the descent computation

Front 387

For the pressurization system, in the auto mode it climbs at ___ft/min and descends at___ ft/min

Back 387

Climb 500

Des 300

Front 388

The pressurization system has 3 possible modes - they are?

Back 388

Auto
Standby
Manual

Front 389

Where are the flight director controls located?

Back 389

On light shield next to autopilot controls

Front 390

Do the flight director modes and autopilot modes mix? will one affect the other?

Back 390

No they are independent

Front 391

Which flight director mode will remove the pitch and roll command bars from view?

Back 391

Standby

Front 392

When a go-around is commanded for the flight director, what will the roll and pitch angle be?

Back 392

roll - wings level

pitch - 14º up

Front 393

The FLT CONT light illuminates when??

Back 393

Any of the lights on the flight control panel come on

Front 394

The FUEL annunciatior light comes on when?

Back 394

When in one tank both fuel low pressure lights come on or a filter ice light comes on

Front 395

The ELEC annunciatior light comes on when?

Back 395

When any light on the electrical system control panel come on

Front 396

The APU annunciatior light comes on when..?

Back 396

Any of the 3 APU lights come on, on the control panel

Front 397

The OVHT/DET light comes on on the annunciator panel when?

Back 397

When either of the engines overheat detection loop lights come on or the APU overheat detection loop light

Front 398

The ANTI-ICE annunciator light comes on when?

Back 398

Any of the anti-ice (pitot static) lights illuminate or the window overheat light

Front 399

The HYD annunciatior light comes on when?

Back 399

Any of the hydraulic low pressure, overheat lights come on on the hydraulic control panel

Front 400

The DOORS annunciatior light comes on when?

Back 400

Any of the lights illuminate indicating that the doors are open or if one of the tire screens in the wheel well is damaged

Front 401

The OVERHEAD annunciatior light comes on when?

Back 401

Any of the amber lights on the overhead panel illuminate

Front 402

The AIR COND annunciatior light comes on when?

Back 402

When on the air con control panel either the;
Dual Bleed / Duct Overheat lights come on.
Or any of the lights on the Pneumatic system or Pressurization control panel come on

Front 403

How may a pilot recall a system annunciatior light?

Back 403

Press either system annunciatior light panel

Front 404

When do the two FIRE WARNING big red lights illuminate?

Back 404

When either;
-Any of the 3 Fire Switches illuminate
-Wheel well fire illuminates

Front 405

Pressing either of the big red FIRE WARNING lights will do what?

Back 405

Extinguish the bell/horn and extinguish the light

The fire switch will remain illuminated

Front 406

What is the Vmo?

Back 406

350 kts @ sea level

367 kts @ 23,500 ft

Front 407

What is the Mmo?

Back 407

0.840 mach

Front 408

At roughly what altitude does Mmo become more limiting than Vmo?

Back 408

approx FL 230

Front 409

When will the TAKE OFF WARNING sound??

Back 409

When any of these items are not in the Take Off config.

- LE Device not in TO pos.
- TO Flaps not set (1-25)
- Speedbrake lever not dwn
- Stab. Trim not set within green band

Front 410

**MEMORY ITEMS**

Aborted Engine Start (ground)

Back 410

Start Lever - Cutoff

Motor Engine 20 sec then start switch off

Front 411

**MEMORY ITEMS**

Air Con Smoke/Fumes

Back 411

Oxygen Masks - On / 100%

Smoke Goggles - On if reqd

Crew Comms. - Establish

Gasper Fan - Off

if smoke stops, continue flight with gasper fan off

Front 412

**MEMORY ITEMS**

Airspeed Unreliable

Back 412

Airplane Attitude/Thrust - Adjust

Pitot Static Heat - Chk ON

Airspeed Indicators - X Check

Front 413

**MEMORY ITEMS**

AUTO Fail / Unscheduled Pressurization Change

Back 413

Increase Thrust may help supply adequate air to control cabin Alt.

Eng Bleed Switches - ON 1@time

Pack Switches - ON 1 @ time

Front 414

**MEMORY ITEMS**

Cabin Alt Warning
Rapid Depressurization

Back 414

Oxygen - DON & 100%

Crew Comms - Establish

Pressurization Mode - Manual

Outflow Valve Switch - Close

Pax Signs - On

Pax Oxygen - On

Emer. Descent - Initiate

Front 415

**MEMORY ITEMS**

Electrical Smoke / Fumes or Fire

Back 415

Oxygen and goggles - On

Crew Comms - Establish

Gasper Fan - Off

KNOWN SOURCE
Electric Power affected equipment - REMOVE

UNKNOWN SOURCE:
Bus transfer - OFF
Galley Power - OFF
Cabin/Galley Lights - ON
Cabin Equipment - OFF

LAND @ NEAREST SUITABLE AIRPORT

Front 416

**MEMORY ITEMS**

Emergency Descent

Back 416

Emer. Desct. - Announce

Engine Start Switches - Low IGN

Thrust Levers - Close

Spd Brake - Flight Detent

Descent - Initiate

Speed - Vmo/Mmo

Altitude - Lowest or 14K (highest)

Spd Brake - Down when level

Front 417

**MEMORY ITEMS**

APU Fire

Back 417

APU Fire Switch - PULL

APU Power - OFF

Front 418

**MEMORY ITEMS**

APU High Oil Temp/Low press
APU Overspeed

Back 418

APU Power - OFF

Front 419

**MEMORY ITEMS**

Engine Fire

Back 419

Thrust Level - Close

Engine Start Switch - Cutoff

Engine Fire Warning Switch - PULL

REMAINS ILLUMINATED;

Engine Fire Switch - L or R

30 seconds, still same

Engine Fire Switch - Remaining Bottle

Front 420

**MEMORY ITEMS**

Aborted Take off (prior to V1)

Back 420

Power Levers - Idle

Brakes - Max Apply

Speed Brake - Raise Lever and deploy

Reverse Thrust - Apply Max

Brakes - Continue Max Braking

Front 421

What settings are the go around flaps detents at?

Back 421

Flaps 15 normal go around (2 eng)

Flaps 1 abnormal (1 eng)

Front 422

What is the maneuvering speed (flaps up)

Back 422

210 kts

Front 423

Max tailwind component for take off and landing?

Back 423

15 kts

Front 424

Max turbulent airspeed?

Back 424

280kts .70m

Front 425

Max operating Alt.

Back 425

37,000ft

Front 426

Max take off and landing alt.

Back 426

8,300ft

Front 427

Autopilot pitch channel should not be used above what speed with A or B hyd system depressurized?

Back 427

not above .81m

Front 428

Max APU -

Start temp?
Cont Temp?

Back 428

760

710

Front 429

What are the engine ignition duty cycle limits?

LOW IGN

FLT

Back 429

LOW IGN- Continuous

FLT - 2 min on 3 min off then 2 on and 23 min off, a total 30 min cycle