Brainscape's Knowledge GenomeTM

Browse over 1 million classes created by top students, professors, publishers, and experts.


See full index

SAAB 340 Tech course > Memory Items > Flashcards

Memory Items Flashcards

1
Q

DC Generators’ max voltage

A

29 VDC

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
2
Q

Nominal load per generator

A

400 A

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
3
Q

Maximum load for 5 minutes on Generator

A

600 A

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
4
Q

Main Battery Voltage

A

24 VDC

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
5
Q

GPU max voltage

A

29.5 VDC

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
6
Q

Battery cart max voltage

A

29.5 VDC (Higher than aircraft
batteries for engine start)

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
7
Q

Normal operation Amps

A

600 A

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
8
Q

Engine start max Amps

A

Min 1400 A - Max 1600 A

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
9
Q

Min fuel for take-off on each side

A

135 KG

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
10
Q

Maximum fuel imbalance between tanks

A

90 Kg

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
11
Q

Fuel low-level light

A

135 KG +- 30 kg

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
12
Q

Max useable fuel quantity in both tanks

A

2565 KG (Confirm if this is correct for exam)

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
13
Q

XFEED and CONN VALVE switches position during takeoff and landing?

A

XFEED and CONN VALVE switches shall be in the OFF and CLOSED position during take-off and landing in normal
operation.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
14
Q

Windshield heating Time in NORM before switching to HIGH

A

7 mins

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
15
Q

Pitot Tubes Time from switching STBY PITOT ON until full ice protection is obtained

A

5 mins

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
16
Q

Windshield Wipers (in low)

A

130 Kts

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
17
Q

Windshield Wipers (in high)

A

160 kts

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
18
Q

Altimeters, Operational Tolerances

A

When the actual QHN set the altimeter myst read with +-60 ft. If it reads +-75 ft it is considered US.

Saab 340 needs 3 altimeters for IFR.
If 2 are reading +-60 ft and 3rd is reading between +-60 - +-75 ft. You can fly to the first destination and recheck there. If still reads the same then the Altimeter must be considered as US.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
19
Q

Airspeed Indicator Operational Tolerances.

A

The max difference between 2 altimeters can be +- 8 kts

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
20
Q

Landing Gear max extension (VLE)

A

200 Kts

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
21
Q

Landing gear max retraction (VLR)

A

150 kts

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
22
Q

Number of brake applications on fully charged accumulators

A

11 each

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
23
Q

Max speed for the use of brakes when anti-skid system is OFF

A

40 kts

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
24
Q

Saab 340 B Model Engine & Propeller Limitations:

Take off power + App. and go around power

A
  • (Max 5 mins) TRQ (107 %) ITT (940 deg) Prop (1396 RPM)
  • (Max 2 mins) TRQ (107 %) ITT (950 deg) Prop (NIL)
    *
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
25
Q

Saab 340 B Model Engine & Propeller Limitations:

Take off power

A
  • (Max 5 mins) TRQ (100 %) ITT (917 deg) Prop (1396 RPM)
  • (Max 2 mins) TRQ (107 %) ITT (927 deg) Prop (1396)
    *
26
Q

Saab 340 B Model Engine & Propeller Limitations:

Max Continous (OEI)

A
  • TRQ (100 %) ITT (944 deg) Prop (1396 RPM)*
27
Q

Saab 340 B Model Engine & Propeller Limitations:
Transient except take-off (max 12
sec)

A
  • TRQ (112 %) ITT (965 deg) Prop (1572 RPM)*
28
Q

Saab 340 B Model Engine & Propeller Limitations:
Engine Start

A
  • ITT (965 deg)
  • Engine RPM (Note) - For the Hamilton Sunstrand propeller avoid steady state PRPM in the range from 650 to 950 PRPM, except for required checks.
29
Q

NG Limitaions for motoring start

A
  • Max NG for motoring - 26%
  • Min stablized NG prior to Condition lever to START - 17%
  • Min NG prior to tailwind start - 20%
30
Q

ITT Exceedance Program (B Model Only)

A
  • If during take off and incursion to ITT range between 927deg/917dec and 944dec, the take off shall continue.
  • If during take off 944dec is exceeded prior to V1, the take off must be aborted
  • If exceedence between 944 dec to 965 dec for less that 12 sec and engine runs operates normaly, the flight shall continue.
  • If ITT exceeds 265 deg after V1. Record ITT and time return to the departure port and contact engineering
31
Q

Starter/Generator (S/G) Duty Cycle Limits.

A
  • Starter Duty Cycle:
    – Two start attempts with 3 minutes cooling between, then 25 minutes cooling before
    subsequent starts. (M)
  • Motoring:
    – Three 30-second ventilations with 3 minutes cooling between each, then a
    one-hour cooling period before subsequent starts or motoring. (M)
  • Time to light-off (from initial Ng rotation to ITT rise), 20 seconds maximum (direct start
    only). (M)
  • Maximum time with starter engaged is 70 seconds of which max 30 seconds plain
    motoring. (M)
32
Q

Icing conditions

A

Icing conditions exist when visible moisture in any form is present (such as clouds, fog with visibility
of one mile (1,850 m) or less, rain, snow, sleet, ice crystals) or standing water, slush, or snow (hard
packed snow excluded) is present on the ramps, taxiways or runways and the OAT or SAT is +5°C
and below during ground and flight operation. In these conditions, or whenever the blue ICE SPD
status light or EAI is on, the minimum speed for flight in icing conditions must be observed. IAS
mode must be selected on the FD if climbing when these conditions exist.

Caution

The defined or minimum speed for flight in icing conditions must be observed whenever the blue ICE SPD status light or EAI is ON regardless of the actual conditions the aircraft is operating in.

33
Q

Maximum Flaps Extended Speeds, VFE

A

Flaps may only be extended on ground, as required for take-off, low altitude holding, approach and
landing, up to a maximum altitude of 14,000 ft. (M)

7 or 15 175 KIAS (M)
20 165 KIAS (M)
35 140 KIAS (M)

34
Q

Maximum Landing Gear Speeds

A

Retraction Speed VLOR = 150 KIAS (M)
Extension Speed VLOE = 200 KIAS (M)
Emergency Extension Speed VLOEE = 200 KIAS (M)
Extended Speed VLE = 200 KIAS (M)

35
Q

Minimum Control Speeds

A

VMCG = Incorporated into calculations for RTOW charts
VMCL = 103 KIAS (Flaps 20 and 35) (SF340A) (M)
VMCL = 106 KIAS (Flaps 20 and 35) (SF340B) (M)
VMCL = 103 KIAS (Flaps 20 and 35) (SF340B (WT)) (M)
VMCA = Incorporated into calculations for RTOW charts

36
Q

Maximum Operating Speed, VMO

A

VMO = 250 KIAS up to approx. 16,000 ft. Above this altitude
VMO decreases as indicated by the VMO pointer to approx. 210 KIAS at 25,000 ft. (M)

37
Q

VMO

A

Max operating speed at SL

38
Q

```

VA (Caution)

A

Full application of rudder and aileron controls, as well as manoeuvres that involve angles of attack near stall, must be confined to speeds below VA.

39
Q

Maximum Manoeuvring Speed, VA

A

VA = 180 KIAS

40
Q

Maximum Rough Air Penetration Speed, VRA

A

VRA = 190 KIAS up to 21,000 ft ISA. Above this altitude, reduce the speed as indicated by the VMO
pointer minus 30 kts.

41
Q

Operational Limits

A

Maximum Take-off Tailwind Component 10 kts (M)
Maximum Landing Tailwind Component 10 kts (M)
Maximum Landing Tailwind Component 15 kts (M) AFMS-54/55
Maximum Operating Altitude 25,000 ft pressure altitude (M)
Maximum Crosswind Component 35 kts (M)

42
Q

Maximum Take-off Tailwind Component
Maximum Landing Tailwind Component

A

10 kts (M)

43
Q

Maximum Landing Tailwind Component (AFMS-54/55)

A

15 kts (M) AFMS-54/55

44
Q

Maximum Operating Altitude

A

25,000 ft pressure altitude (M)

45
Q

Maximum Crosswind Component

A

35 kts (M)

46
Q

Airborne Collision Avoidance System (ACAS)

A

Deviations from the ATC assigned altitude is authorised only to the extent necessary to comply
with an ACAS Resolution Advisory (RA). (M)
Manoeuvres must not be based solely on information presented on the Traffic Advisory (TA)
display. (M)

47
Q

Flight Director

A

Use of flight director information in go-around mode during take-off is not authorised. (M)

48
Q

Autopilot

A

Autopilot operations not authorised:
 Below 200 ft AGL - during take-off or go-around. (M)
 Below 500 ft AGL - during cruise. (M)
 Below 50 ft AGL - during approach. (M)
 Below 100 ft AGL - for a non-coupled approach. (M)

In icing conditions (as defined) FD/AP IAS MODE IS THE ONLY VERTICAL MODE TO BE USED
DURING CLIMB WHEN ICE ACCUMULATION IS OBSERVED OR IF IT IS NOT CERTAIN THERE
IS NO ICE ACCUMULATION ON THE AIRCRAFT. (M)

It is a requirement to disconnect the autopilot following an engine failure and re-trim the aircraft
before re-engagement of the autopilot. (M)

49
Q

Yaw Damper

A

Yaw Damper Operation is not authorised for:
 Take-off (M),
 Go-around (M), or
 Landing (M).

50
Q

Flap

A

 Landing Flap is to be set by 300 ft radio height during normal landing. (M)
Company requires that the final flap setting is called for at no less than 500 ft AGL.
 When holding in icing conditions (as defined) Flap 0 must be used. (M)

51
Q

Placards and Instrument Markings

A

Operating limits RED (M)
Caution, temporary or idle range YELLOW (M)
Normal operating range GREEN (M)

52
Q

Cargo Fire

A

 60 min for 340B (WT) (Mod No. 1149 incorporated (2 bottles)). (M)
 35 min for all other REX aircraft. (M)

53
Q

Attitude/Heading Reference System

A

During initialisation on ground the aircraft must not be moved. (M)
Take-off is not permitted until two minutes after initialisation is completed and the attitude difference
between the attitude displayed on both EADIs and the standby attitude indicator is 3 degrees or
less (bank and pitch) and the heading on the compass card is not slewing away from the aircraft
heading. (M)

54
Q

Structural Weight Limitations SF340 B

A

Maximum Taxi Weight (MTW) 13,740 kg (M)
Maximum Take-Off Weight (MTOW) 13,605 kg (M)
Maximum Landing Weight (MLW) 12,930 kg (M)
Maximum Zero Fuel Weight (MZFW) 12,020 kg (M)

55
Q

Structural Weight Limitations SF340B(WT)

A

Maximum Taxi Weight (MTW) 13,290 kg (M)
Maximum Take-Off Weight (MTOW) 13,155 kg (M)
Maximum Landing Weight (MLW) 12,930 kg (M)
Maximum Zero Fuel Weight (MZFW) 12,020 kg (M)

56
Q

Structural Weight Limitations WEIGHTS (SF340A)

A

Maximum Taxi Weight (MTW) 12,840 kg (M)
Maximum Take-Off Weight (MTOW) 12,700 kg (M)
Maximum Landing Weight (MLW) 12,340 kg (M)
Maximum Zero Fuel Weights (MZFW) 11,660 kg (M)

57
Q

AIRCONDITIONING AND PRESSURISATION
Cabin differential pressure

A

In flight (Normal) 7.1 (MaX) 7.5 Psi (M)
Landing (Max) 0.3 Psi (M)
CABIN PRESS warning (Normal) 7.5 Psi (M)
Cabin altitude CABIN PRESS warning (Max)10,000 ft (M)

58
Q

Windshield heating

A

Time in NORM before switching to HIGH min 7 (M)

59
Q

Pitot Tubes heat

A

Time from switching STBY PITOT ON until full
ice-protection is obtained min 5 (M)

60
Q

Windshield Wipers use limitations

A

– In LOW position kts – – 130 (M)
– In HIGH position kts – – 160 (M)

61
Q
A

SAAB 340 Tech course (4 decks)

Brainscape helps you reach your goals faster, through stronger study habits.
© 2024 Bold Learning Solutions. Terms and Conditions