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SAAB 340 Tech Course > Tech exam > Flashcards

Tech exam Flashcards

1
Q

MTOW and MLW for A and B model

A

12700/12340 & 13605/12930

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2
Q

How do you test the Auto Ignition in the A model?

A

PL above FI with both engines shut down

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3
Q

How do you test Auto Ignition in the B model?

A

Before engine shut down when CL at Fuel shutoff, as the Ng decreases, the FSP IGN lights must illuminate until Ng decelerates below 62%

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4
Q

What is the ITT Limitation for the B model with No APR 2mins and 5 mins?

A

927 and 917- FCOM Chpt 2

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5
Q

What is the ITT Limitation for the B model with APR - 2mins and 5 mins?

A

950 and 940 - FCOM chpt 2

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6
Q

What causes the HP HIGH light to illuminate on the OVRHD panel?

A

HP valve fails to close after close command is received- FD Panels and lights

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7
Q

What causes the BAT HOT light to illuminate ?

A

Battery temp over 71 degrees

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8
Q

When does EMERG POWER illuminate on the overhead panel?

A

Emerg bus not powered,
Emerg battery less than 24v, or
Emerg battery not being charged

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9
Q

When does the INVERTER light illuminate on the Overhead panel ?

A

If inverter fails or the switch is in the OFF position - FD Lights and panels

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10
Q

“Pitch trim” on the CWP indicates what?

A

Pitch trim sync is deactivated- Bonus what causes this? 1 unit of disagreement

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11
Q

What is touchdown protection?

A

It prevents from landing with brakes on
In order to function we need-
Anti skid ON,
Gear level DOWN and
WoW for over 3 seconds, or
PL below FI for over 3 seconds or
Average wheel speed 50KIAS

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12
Q

How do you energise the MAIN START BUS?

A

Gen bus or GPU online
Bus tie must be closed

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13
Q

What are the functions of the Hydraulic AUTO pump?

A

Pressurise system in normal operations and shuts off when there is no demand

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14
Q

What does GPU relay do to other relays?

A

Opens Start/Gen/Battery relays

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15
Q

When is the EMERG Battery charged?

A

When the L Batt bus is powered by at least one battery switch on

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16
Q

Where does the ignition system get its power from?

A

1 of the 3 windings in the Alternator

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17
Q

What does DE ICE OVERTMP light indicate?

A

Either temperature sensor is reading over 150 degrees

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18
Q

When does the Hydraulic system operate in AUTO?

A

Turns on at 2100psi and off at 2900psi
Also during gear extension and retraction
Extension until left main is down and locked
Retraction until both main are up and locked

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19
Q

If we start the BATT in override, what are we doing?

A

Overriding the 71 degree battery protection

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20
Q

If the px controller is functioning normally in AUTO, what px will it limit the system to?

A

7.1psi

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21
Q

When does CABIN PRESS altitude warning illuminate?

A

10000ft Cabin alt

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22
Q

What does the emergency accumulator do?

A

Release emergency up-locks and pressurise the main reservoir

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23
Q

What is the accumulator nitrogen precharge pressure?

A

1650psi

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24
Q

How do we pressurise the brakes if the main accumulator pressure is lost?

A

Hand pump

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25
Q

What is the first memory item for the HYDR light?

A

Hydraulic pump off

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26
Q

If the cabin is over pressurising and electro pneumatic valve (primary) is stuck, how can you de-pressurise?

A

Can do so manually by moving switch to manual and using secondary outflow valve

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27
Q

What is the ancillary system for the Hydraulics system?

A

The hand pump - FO side

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28
Q

How is the fuel heater operated?

A

Operated thermostatically- thermostat switch

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29
Q

How is the fuel heated?

A

Heat exchanger uses PGB oil to heat the fuel before it is transferred to the HMU

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30
Q

To operate the hydraulic pump in override do we need battery on?

A

L Batt bus and AUTO is preferred

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31
Q

Initial pressure for the main reservoir is supplied by ?

A

Internal spring pressure and emergency accumulator

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32
Q

What controls propeller blade on ground and in sky?

A

Power lever below FI (Beta) and Condition levers above FI

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33
Q

What is the SHP on the B model (APR on)

A

1870

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34
Q

Max prop RPM for take off?

A

1396 rpm

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35
Q

Engine starter duty limitations

A

Max start 2 with 3 minutes then 25 between start cycles

Max motoring 3 x 30 second ventilations then 1 hour for subsequent start/motoring cycles

Max start time is 20 seconds

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36
Q

If the Ng is going through 40% and stays there, what do you do?

A

Abort start- CL off and Ign Off

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37
Q

Max start ITT for a B Model?

A

965 degrees

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38
Q

What does the ANTI ICE light on the FSP indicate?

A

Anti Ice switch position is ON

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39
Q

Max starter engaged time?

A

70 seconds including 30 seconds of motoring

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40
Q

Fuel Conundrum- Left to Right

A

Battery ON
Power Fuel Panel
Fuel Mid/High
Open de fuel valve
XFEED ON
LH STBY pump OVRD

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41
Q

Pneumatic jet pump connected to WoW switch does what?

A

Assists the airflow around the precooler on the ground

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42
Q

When is the bottoming governor enabled in the A model?

A

581 RPM
Normal ground ops = 1040 rpm
Reverse thrust ops = 1200rpm

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43
Q

What is the voltage required for a battery start?

A

24 Volts

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44
Q

What powers the engine electrical intake mats?

A

AC Wild generator

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45
Q

If you lose an AC generator airborne, what do we lose?

A

Ice protection for that side. Cannot fly in icing conditions anymore as it cannot be crossfed

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46
Q

Gas generator overspeed is prevented by what?

A

Overspeed shut off valve in the HMU, when the Ng reaches 110% the overspeed shut off valve induces flame out by shutting off fuel. There is no auto relight function– overspeed governer in the HMU (exam)

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47
Q

What is the CTOT T/O function in the B model? How do you switch it on?

A

CTOT T/O provides constant power at take off to counteract torque bloom caused by RAM air at take off.
Require CTOT and Autocoarsen ON

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48
Q

If the Left aileron system is jammed what trim do we use?

A

Use the standby trim on the right aileron.

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49
Q

How do we reset torque motor?

A

By shutting engine down, CL to Fuel SHUT OFF

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50
Q

What is the purpose of the CTOT?

A

Is to increase engine speed beyond the power lever position

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51
Q

What happens when you pull the fire handle?

A

Engine fuel shut off
Bleed air OFF
Start/Gen relay open
Silence fire bells
Reset master warning
Squibs armed

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52
Q

How is the power turbine (Np) protected from overspeed?

A

When Np speed is 25000rpm (1573 prop rpm) is reached, the DECU shuts fuel, after a 5 second delay it initiates ignition for 7 seconds. If the rpm has dropped below overspeed value, the fuel is reintroduced

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53
Q

What is the purpose of the autocoarsen system?

A

Fast reduction of the windmilling drag experienced at engine failure

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54
Q

How do you feather the propeller?

A

Move condition lever to the Start detent

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55
Q

What does Duct OVER TEMP light indicate?

A

ACP compressor discharge temp is above 225 degrees, or
Distribution duct temp is above 82 degrees

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56
Q

Engine fire detection system incorporates what? How is fire detected?

A

Using a single continuous loop detection circuit

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57
Q

Where does the fire detection system get its power from?

A

Emergency battery bus

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58
Q

How does the extinguishing system work?

A

1301 Halon extinguisher in each engine nacelle able to cross-feed

Dual wall 1301 Halon in the cargo with 35 minutes run time, external immediately dispersed and internal slowly to prevent re-ignition

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59
Q

How does the extinguishing system work?

A

1301 Halon extinguisher in each engine nacelle able to cross-feed, discharged using switch in cockpit overhead

Dual wall 1301 Halon in the cargo with 35 minutes run time, external immediately dispersed and internal slowly to prevent re-ignition, no auto discharge, use switch in cockpit overhead

1211 Halon extinguisher in the lavatory bin, extinguishes automatically when 75 degrees or above is sensed.

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60
Q

Where does the extinguishing system get its power from?

A

HOT Battery bus

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61
Q

How do you stop the stick pusher from pushing?

A

Push 1 of 2 “Pusher Disarm” buttons in the cockpit

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62
Q

At what temp will the “Tail Pipe Hot” light illuminate?

A

235 degrees

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63
Q

What do you do when there is an elevator trim runaway in the nose down position?

A

Use the standby trim to disconnect or pull circuit breaker (Right is standby)

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64
Q

If you have used the fire extinguisher in the right engine and the fire is still on, what do you do?

A

AAHHHHH Fuaarkkk!!

Cross feed the left extinguisher into the right nacelle

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65
Q

What is the indication the fire is out?

A

Fire handle and CWP are not illuminated anymore.

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66
Q

What is the extinguishing agent for the cargo compartment?

A

1301 Halon

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67
Q

What type of extinguisher in the cargo compartment?

A

Dual wall with 35 minutes run time
(2 bottles in WT - 60 minute run time)

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68
Q

What is the usable fuel capacity?

A

2542 kg @ 0.79kg/l

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69
Q

When do the standby fuel pumps operate?

A

At start up when CL out of fuel shutdown the standby pumps operate until main pumps are fully operative, 10psi differential.
Also on when main pump pressure decreases

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70
Q

At what differential pressure will the “FUEL FILTER” light illuminate?

A

9 psi

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71
Q

What causes the bleed valve to close?

A

Fire handle pulled,
bleed air temp at 288 degrees,
regulated pressure 43.5psi,
ACP discharge temp 225 degrees,
Distribution duct at 82 degrees
Bleed closed by pilot

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72
Q

When does the inverter light illuminate in the A model?

A

Inverter is offline
or
switch is off

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73
Q

When does the oxygen light on the CWP illuminate?

A

When the pressure is below 800 +/- 35 psi

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74
Q

What does the BLUE FUELLING light onthe overhead panel indicate?

A

Fuel panel switched ON, or
De-fuel valve OPEN

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75
Q

Fuel indicators calibrated to?

A

Usable fuel

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76
Q

Apart from the main cabin door warning light, what other door warnings are displayed?

A

Main door, Cargo door and crew emergency escape hatch

77
Q

What is the max fuel imbalance?

A

90 kgs

78
Q

How is cabin temperature controlled?

A

AUTO or MANUAL
AUTO- using a knob in cockpit can maintain 18-29 degrees

Manual- by holding the switch in hot or cold position, care must be taken as it can be detrimental to systems, 3-75 degrees

79
Q

What is the source for low pressure air?

A

5th stage compressor

80
Q

How do we get airflow across dual heat exchangers? Battery compartment ventilated?

A

Internal fan connected to WOW switch and RAM air in flight

81
Q

What ACP provides air to the flight deck

A

Right ACP provides 1/3 to the cockpit and 2/3 to the cabin. Left provides entirely to the cabin

82
Q

What is the max gear extension speed?

A

200 KIAS

83
Q

What systems are operated by the hand pump?

A

Flaps, Landing gear and brakes

84
Q

How are the main and nose gears held up and down?

A

Using mechanical uplocks

85
Q

How much castoring does the NWS GND Handling lockout switch permit?

A

120 degrees with the lockout (C Clamp)

60 degrees when on tiller

86
Q

What is the source for EMERG braking?

A

Hand pump or brake accumulator

87
Q

Boot de-icing system will not function unless?

A

Unless there is adequate supply at the boot distribution valve

88
Q

When do we get a stab or boot indication?

A

When stabs or boots are inflated. Sequence-
STAB, OUTBOARD, INBOARD, STAB

89
Q

How does pulling fire handle affect pneumatic system?

A

Closes bleed valves

90
Q

How are propellers de-iced?

A

115 V AC Wild generator

91
Q

If controls are jammed, how do we permanently disconnect?

A

Electrically, using PITCH or ROLL handle as required

92
Q

If one of the stall warning systems fail, will the pusher work?

A

No requires both systems working

93
Q

How is asymmetric flap position prevented?

A

By the use of a mechanical interconnect

94
Q

What does switching rudder limit switch to override permit?

A

Full scale rudder deflection at any airspeed

95
Q

If the L DPU Fails with EFIS in NORM position what will you see ?

A

Blank screens. Can use the R DPU using drive XFR, but can only adjust the brightness on the screens

96
Q

How do you know the AHRS has failed? How we we fix ?

A

RED ATT or HDG Flag. On failure you can use XSIDE Data for data from other Attitude heading computer, should display yellow XATT on screen

97
Q

What is the source of power for the STBY Pitot ?

A

28 VDC

98
Q

Max continuous power in the A Model?

A

100TRQ, 1396 RPM and 917 ITT

99
Q

What causes the impending bypass light on the overhead panel?

A

Fuel filter or Engine Oil

100
Q

In the event of a tailwind what start what process would you consider?

A

Introduce fuel at 20% Ng or Battery start instead

101
Q

What does hydraulic pump do in override?

A

Continuously pumps at 3000psi

102
Q

If we use CTOT for TO and what would DECU try to maintain?

A

Maintain the Torque set while the ITT increases.

103
Q

CTOT is used to set the TRQ for climb at 1500ft. Passing 10,000ft you notice that the ITT has risen
on both engines by 50°C. All other engine indications are normal. What is the reason for this?

A

The DECU is trying to maintain the TRQ while the altitude is increasing, leading to increase in ITT

104
Q

What happens when hydraulic fluid is lost?

A

Loose all hydraulics except emergency

105
Q

When does fuel low level caution illuminate?

A

Fuel level at 135 kgs +/- 30 kgs

106
Q

If there is no pressure in the emergency accumulator, can the emergency handle release the landing gear?

A

No it cannot.

107
Q

If the Hydraulic fluid in the main reservoir is lost, will the HYDR light illuminate on the CWP?

A

No, only when high temp or loss of pressure

108
Q

Can the brake accumulators be pressurised by the hand pump?

A

Yes

109
Q

What is the SHP for the A model?

A

1735 and 1800

110
Q

What is the SHP for the B Model? APR Off and On

A

1750 and 1870

111
Q

What is the external power Norm and Engine start amperage?

A

600 and 1600

112
Q

How do you un-feather a propeller?

A

Move Condition Lever to UNF (Unfeather) detent

113
Q

What power source has priority? External, Battery, Generator

A

External

114
Q

How is prop gear box overspeed prevented?

A

Independent overspeed governor should the governor in the PCU fail

115
Q

Wing span without wingtips

A

21.44

116
Q

Wingspan with extended wingtips

A

22.75

117
Q

Define icing conditions

A

Temp below +5 degrees and visible moisture

118
Q

When must Icing speeds be observed? FD IAS

A

When flying in icing conditions or the Blue Ice speed light is ON

119
Q

When must Icing speeds be observed? FD IAS

A

When flying in icing conditions or the Blue Ice speed light is ON

120
Q

Maximum flap extended speed–
7 or 15

20

35

A

175

165

140

121
Q

Maximum altitude for flap operation?

A

FL140

122
Q

Maximum gear operation speeds

Retraction

Extension

Extended

A

150 kts

200 kts

200 kts

123
Q

Minimum control speeds– Vmcl
340A

340B

340WT

A

103

106

103

124
Q

Maximum operation speed- Vmo

A

250kts to 16,000 ft then reduces until 210kts at 25,000 ft

125
Q

Maneouvering speed- Va

A

180 kts

126
Q

Maximum rough airspeed- Vra

A

190 kts to 21,000 ft then Vmo minus 30kts until 25,000 ft

127
Q

Max tailwind- Take off & Landing

A

10kts

128
Q

Max tailwind landing - AFMS 54/55

A

15kts

129
Q

Max crosswind

A

35kts

130
Q

Max operating altitude

A

25000 ft

131
Q

When can you deviate from ATC assigned altitude?

A

Only for a TCAS RA

132
Q

Can you use flight directors during a go-around?

A

No you cannot

133
Q

When is use of the autopilot not authorised?

A

Below 200ft on take off
Below 500ft in cruise
Below 50ft during an approach
Below 100ft during a non-coupled approach

134
Q

What AP mode can be used for climb in icing conditions

A

IAS mode only

135
Q

What do we do to the autopilot when you experience an engine failure?

A

Disconnect, trim aeroplane and then reconnect

136
Q

When is Yaw Damper not authorised for use?

A

During take-off, landing & go-around

137
Q

When must landing flap be set by?

A

Should be set by 300ft and asked for by 500ft

138
Q

What flap to be used for holding?

A

Zero flaps for holding

139
Q

What is the Cargo fire extinguisher protection duration for the
B model

WT model

A

35 minutes with 1 extinguisher

60 minutes with 2 extinguishers

140
Q

Can you move the aircraft on the ground during AHRS initialisation?

A

No you cannot

141
Q

How long after AHRS initialisation is take-off permitted? Any requirements?

A

Take-off is permitted 2 minutes after initialisation, attitude difference less than 3 degrees and heading is not slewing

142
Q

MTOW 340B and WT

A

13605 and 13155

143
Q

MLW 340B and WT

A

12930

144
Q

MZFW 340B and WT

A

12020

145
Q

Cabin differential pressure?
Normal
Max
Landing
Negative

A

7.1psi
7.5psi
0.3psi
-0.5psi

146
Q

Cabin pressure warning at what psi?

A

7.5psi

147
Q

When does the Cabin altitude Cabin press warning activate?

A

Cabin altitude at 10,000 ft

148
Q

Voltage of the DC generator? Min
Norm &
Max

A

27.5
28
29

149
Q

DC generator Nominal load

A

400A

150
Q

DC generator Maximum load for 5 minutes

A

600A

151
Q

Main battery voltage

A

24volts

152
Q

GPU min and max voltage?

A

Min 28 and Max 29.5

153
Q

Battery cart max voltage

A

29.5

154
Q

External power Normal ops amperage requirement

A

600A

155
Q

External power engine start amperage requirement

A

Min 1400
Max 1600

156
Q

Min fuel for take off each tank

A

135kgs

157
Q

Max fuel imbalance

A

90kgs

158
Q

When does the fuel Low Level light turn on?

A

135kgs +/- 30kgs

159
Q

Total usable fuel

A

2542 @ .079 specific gravity

160
Q

Windshield heating- Time in NORM before HIGH

A

7 minutes

161
Q

Pitot tube- time until full ice protection is obtained once STBY PITOT ON

A

5 minutes

162
Q

Windshield wipers operation speeds
LOW
&
HIGH

A

130 kts
&
160kts

163
Q

Altimeter accuracy and requirements

A

Require 3 within+/-60 feet of nominated elevation. One may read 60ft-75ft at departure aerodrome as long as it can be rechecked at next aerodrome

164
Q

Maximum difference between 2 airspeed indicators?

A

+/- 8 KIAS

165
Q

Number of applications on a fully charged brake accumulator

A

11 applications

166
Q

Max speed for use of brakes with the anti-skid system inop

A

40 knots

167
Q

B model take off power or go-around with APR

A

TRQ 107 Engine 1396 RPM
ITT 940 degree for 5 minutes and
950 degrees for 2 minutes

168
Q

B model take off power or go-around - No APR

A

TRQ 100 Engine 1396 RPM
ITT 917 degree for 5 minutes and
927 degrees for 2 minutes

169
Q

B Model max continuous power

A

TRQ 100 Engine 1396 RPM
ITT 944 degrees

170
Q

B model transient power

A

TRQ 112 Engine 1572 RPM
ITT 965 degrees

171
Q

B model transient power

A

TRQ 112 Engine 1572 RPM
ITT 965 degrees

172
Q

B model engine start max ITT

A

965 degrees

173
Q

Ng limitations for motoring start-
Max Ng for motoring
Min Ng prior to CL to Start
Min Ng in tailwind start

A

26%
17%
20%

174
Q

Max ITT for climb and Cruise power

Below FL150

Above FL150

A

840

875

175
Q

Memory items-
Hot or hung start

A

Condition level - Fuel shut off
Ignition - off
Motor to ITT below 175 or 10 seconds

176
Q

Memory Items-Engine failure at V1

A

Power level = 20-30%
Condition lever = Fuel shut off

177
Q

Memory Items- Engine Fire at V1

A

Power Lever = 20-30 %
Condition lever = Fuel shut off
Fire handle = Pull
Fire Extinguisher = On
after 30 seconds if fire persists, discharge opposite extinguisher

178
Q

Memory Items- Uncommanded engine operation in flight

A

Power lever = 20-30&
Condition lever = T/M then SET
Autocoarsen = OFF

179
Q

Memory Items- Uncommanded engine operation on ground

A

Shut engine down

180
Q

Memory Items- Compressor stall

A

CTOT = OFF
Power lever = 20-30%

181
Q

Memory Items- Aircon smoke or avionics smoke or fire

A

Oxygen masks = on and 100%
Goggles = on
comms = establish

182
Q

Memory Items- Rapid depressurisation

A

Oxygen = on and 100%
Comms = Establish
transponder = 7700
Seatbelt sign = on
Emergency descent = initiate

183
Q

Memory Items- Tail pipe hot

A

Power lever affected side 20-30%

184
Q

Memory Items- Cargo compartment smoke

A

Fire extinguisher switch = ON

185
Q

Memory Items- Hydraulic light

A

Hydraulic pump = off
Check hydraulic indicators
Speed - under 200kts
Landing gear handle - down
Emergency ldg handle - pull

186
Q

Memory Items- Hydraulic fluid loss

A

Hydraulic pump = off

187
Q

Memory Items- Elevator or Aileron system jammed

A

AP = Off
Interconnect unit = Overpower
Pitch disconnect handle = Pull

188
Q

Memory Items- Emergency evacuation

A

FO Duties
Emerg panel switches = on
Fire handles both = Pull
Fire Extg switches = On

189
Q

Memory Items- unreliable airspeed

A

AP= disconnect
Flight path = Stablise
Power setting= maintain attitude and power

SAAB 340 Tech Course (1 decks)

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