Brainscape's Knowledge GenomeTM

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


See full index

Systems > Operating Limitations > Flashcards

Operating Limitations Flashcards

1
Q

Torque limits: Normal range

A

0-104%

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

Torque limits: Max

A

107.8%

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

RPM: Min

A

64%

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

RPM: Normal

A

65-101.5%

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

RPM: Normal In-flight range

A

82-100.5%

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

RPM: Max

A

105.5% for 30sec

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

EGT: Min

A

300C

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

EGT: Normal In-flight range

A

350-650C

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

EGT: Max

A

675C

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

Oil temp: Normal In-flight range

A

56-110C

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

Oil temp: Max In-flight temp

A

115C

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

Oil px: Normal px operating range

A

50-120psi

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

Oil px: Max px

A

126psi

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

Fuel: Min feed px

A

16psi

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

Fuel: Normal px range

A

18-55psi

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

Fuel: Max feed px

A

60psi

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

Fuel: Normal temp range

A

-21 - 50C

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

Electrical: A/c system voltage

A

28VDC

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

Electrical: Max system voltage

A

32 V

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

Electrical: Min bus volt fuel heater auto shutoff

A

26 V

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

Aircraft performance: AOA range

A

-6 to +10

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

Aircraft performance: Vne

A

230 IAS / 249 TAS

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

Aircraft performance: Max gear in tx speed

A

135 KIAS

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

Aircraft performance: Max gear ext speed

A

160 KIAS

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
25
Q

Aircraft performance: Max speed on 90F+ Climb out, 45 min

A

135 KIAS

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
26
Q

Aircraft performance: Va at max weight

A

158 KIAS

-4.5 kts/ 500lbs less than max gross weight

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
27
Q

Weights: Max ramp weight

A

10500 lbs

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
28
Q

Weights: Max landing weight

A

8500 lbs

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
29
Q

Weights: Max fuel weight

A

3764 lbs

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
30
Q

AN/DAS-1: Operating temp

A

-40C to +55C

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
31
Q

AN/DAS-1: Laser lockout zone

A
  • 110 - +110 Az / +5 Dep

- 180 - +180 Az/ -10 Dep

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
32
Q

the deec will not allow RPM to dwell between xx.x and xx.x%

A

89.5 to 92.5

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
33
Q

Normal EGT start range

A

695-700 C

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
34
Q

What is the EGT max for start only?

A

770-776 C for 1 sec

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
35
Q

Continuous engine ground ops with oil temperature between xxx and xxx are authorized with torque below xx%

A

116 & 127 below 86%

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
36
Q

flight ops with oil temp between xxx and xxx are authorized for up to x min with torque below xx%

A

110 and 127 for 5min below 86%

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
37
Q

oil temp low red and yellow indications activate at xx and xx. If oil temp is below xx , refer to Low Oil Temp procedure.

A

40 C and 45 C

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
38
Q

Min oil temp for start

A

-20C

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
39
Q

high oil px yellow caution limit

A

120 psi

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
40
Q

if fuel feed px is below xx psi, the RCM auto turns on pump not in use and displays a pump failure warning.

A

15 psi

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
41
Q

fuel feed pressure min

A

16 psi

42
Q

fuel feed px normal range

A

18-55 psi

43
Q

max fuel feed px

A

60 psi

44
Q

fuel tank min temp

A

-31C

45
Q

fuel tank normal temp range

A

-21-50C

46
Q

max fuel tank temp

A

56C

47
Q

are there operating temp limits for the manifold fuel temperature?

A

no

48
Q

in automatic dump mode, how many fuel tanks will be selected (if theres fuel in them) and in what order?

A

2 tanks. wing tanks first, then fuselage

49
Q

In manual dump mode, how many tanks are selected?

A

only 1

50
Q

fuel dump rate via primary valve 1 tank selected

A

3000pph for all tanks

51
Q

dump rate via backup valve 2 tanks selected

A

950 pph

52
Q

dump rate via backup valve 1 tank selected

A

1950 pph

53
Q

dump rate via primary dump valve 2 wing tanks selected

A

2000 pph

54
Q

dump rate via primary valve 2 tanks selected (forward tank)

A

2100 pph

55
Q

dump rate via primary valve 2 tanks selected (aft tank)

A

1900 pph

56
Q

A landing gear fault is generated if gear extension/retraction is completed in less than xx sec or more than xx sec

A

11 or 29

57
Q

what AOA equates to best rate of climb speed?

A

2 AOA

58
Q

max altitude

A

fl 520

59
Q

max alt for air start

A

fl300

60
Q

3 prohibited maneuvers

A

intentional stalls, spins, inverted flight

61
Q

AOA op range

A

-6 through +10

62
Q

“stall conditions - exceeding limits” is triggered in the GCS when the commanded bank angle would exceed Cl of x.xx

A

1.25

63
Q

max fuel weight

A

3764lbs

64
Q

empty weight

A

4900 lbs

65
Q

useful load (GTOW - empty weight)

A

5600 lbs

66
Q

inboard wing stations

A

1500 lbs

67
Q

middle wing stations (2/6)

A

750 lbs

68
Q

outboard wing stations

A

150 lbs

69
Q

wingspan

A

66’

70
Q

wing area

A

256 sq ft

71
Q

wing aspect ratio

A

16:1

72
Q

wing root chord

A

65.2”

73
Q

wing tip chord

A

28.8”

74
Q

overall fuselage length

A

36.2’

75
Q

fuselage height

A

11.8’

76
Q

propeller diameter

A

110”

77
Q

define empty weight

A

airframe structure, unusable fuel, full operational support fluids

78
Q

define useful load

A

payload + fuel + operational avionics + ballast

79
Q

define gross weight

A

empty weight + useful load

80
Q

The MQ9 is equipped with a Honeywell “xxx” turboprop engine

A

TPE331-10YGD

81
Q

how much of the mechanical shaft power produced by the engine is used to rotate (drive) the compressor?

A

approximately 2/3

82
Q

when operating in normal mode, the DEEC controls what 2 functions of the engine?

A

throttle and speed

83
Q

How many servos does the DEEC have and what are they?

A

2, throttle and stop/feather

84
Q

the DEEC controlled RPM in-flight ops range

A

82.5% to 100.5%

85
Q

what are the DEECs secondary functions? (6x)

A
  1. engine torque and temp limiting
  2. engine speed switches (10% fuel + ignitors on, 60% starter/ignitor switch off, 80% SRL activations switch)
  3. auto fuel enrichment
  4. SRL EGT conditioning
  5. closed loop power control
  6. engine/deec fault monitoring
86
Q

engine dry weight?

A

375lbs

87
Q

installed weight with propeller

A

525lbs

88
Q

reduction gearbox ratio

A

26:1

89
Q

shaft horsepower

A

900

90
Q

jet thrust

A

157lbs max continuous

91
Q

total takeoff thrust

A

2000lbs (standard day, sea level)

92
Q

reverse thrust

A

700lbs (standard day, sea level)

93
Q

propeller shaft RPM

A

1591 max continuous

94
Q

oil type

A

exxon/bp turbine oil 2380 (type II)

95
Q

propeller pitch range

A

-15 to +90

96
Q

what mechanical actions cause the BETA light to illuminate?

A

the governor oil pump sends full discharge px approx. 450psi to pitch controller and beta switch which closes and illuminates the BETA indication on the HUD

97
Q

the BETA light may not illuminate if engine RPM is less than

A

85% due to lower oil px

98
Q

when the throttle is moved past the flight idle position, RPM will transition from xx% to xx%. At xx% RPM, the BETA light should extinguish regardless of speed lever position.

A

65 to 82. 82%

99
Q

If the BETA light illuminates in flight 1 of 5 conditions may be present

A
  1. rigging problem
  2. low fuel flow
  3. failed beta switch
  4. insufficient airspeed
  5. improperly calibrated throttle
100
Q

what does the feathering valve do?

A

sends oil px to the PCU in response to NTS (negative torque sensing), the deec or condition lever activation

101
Q

what does the unfeather pump do?

A

electronic oil pump supplies oil px to force the prop blades from feathered position onto start locks = flat position

102
Q

the engine lubrication system is a wet/dry sump that provides a constant supply of clean filtered oil to …(4x) The system also…(2x)

A

dry

  1. bearings
  2. reduction gears
  3. accessory drives
  4. prop control system
  5. cools engine components
  6. carries away impurities to oil filter

Systems (6 decks)

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