Flash Deck Flashcards

1
Q

Propulsion System Failure

A
  1. Altiture - Level
  2. Airspeed - 70 KTS
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2
Q

Autopilot Failure

A
  1. KNOBS - Select
  2. Payload - Cage (If AV is uncontrollable or unable to verify control of AV within 10 seconds.)
  3. FTS - Deploy
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3
Q

Engine Failure Above 2,000 FT AGL

A
  1. Airspeed - 70 KTS
  2. Safe Heading - Establish
  3. FTS Site - Select
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4
Q

AV Fire on Launcher

A
  1. “Abort, Abort, Abort Fire on Launcher’ - Announce (cc)
  2. LHCU Launch Switch Cover - Closed (cc)
  3. Total sticks - Select
  4. Throttle - Idle
  5. Engine - Cut
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5
Q

Oil Starvation (HUMS Caution & Alert)

A
  1. Altitude - Level
  2. Airspeed - 70 KTS
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6
Q

TALS Abort Below Decision Point

A
  1. ‘TALS Abort’ - Announce
  2. ‘AV Touchdown’ - Announce (cc)
  3. Engine - Cut (if required)
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7
Q

Low Oil Pressure

A
  1. Altitude Level
  2. Airspeed 70 KTS
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8
Q

Fuel System Failure (Fule Flow Alert (HUMS Alert)

A
  1. Altitude Level
  2. Airspeed 70 KTS
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9
Q

Magnetometer Failure

A
  1. Knobs ROLL - Select
  2. Land - As Soon As Possible
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10
Q

Engine Failure Below 2,000 FT AGL

A
  1. Safe Heading - Establish
  2. FTS - Deploy
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11
Q

In-Flight Servo Failure

A
  1. Servo Status - Query
  2. AV Control - Assess
    (if AV uncontrollable)
  3. FTS - Deploy
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12
Q

Uncontrolled Flight

A
  1. Knobs - Select
  2. Payload - Cage
    (If AV Uncontrollable)
  3. FTS - Deploy
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13
Q

Stuck throttle (Low RPM)

A
  1. KNOBS - Select
  2. Safe Heading - Establish
  3. Altitude - Cycle
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14
Q

Auto launch Abort

A
  1. ‘Abort, Abort, Abort’ - Announce
  2. LHCU Launch Switch Cover - Closed (cc)
  3. Total Sticks - Select
  4. Throttle - Idle
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15
Q

GCS Electrical Power Failure

A
  1. Heading - RTB
  2. Non-Essential Components - Off
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16
Q

AV Fire On Ground

A
  1. ‘Fire, Fire, Fire on AV’ - Announce (cc)
  2. Throttle - Idle
  3. Engine - Cut
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17
Q

High Engine Temperature

A
  1. Altitude - Level
  2. Airspeed - 70 KTS
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18
Q

No Oil Pressure

A
  1. Altitude - Level
  2. Airspeed - 70 KTS
  3. Heading - RTB
  4. FTS Site - Select
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19
Q

Uncommanded Firing of LDRF/LP (Physical)

A
  1. Payload - Standby
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20
Q

Max Operational RPM

A

8000 RPM for 2 min

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21
Q

Max Continuous Climb RPM

A

7800 RPM

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22
Q

Max Continuous Cruise RPM

A

7500 RPM

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23
Q

Min Inflight RPM

A

3800 RPM

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24
Q

Max Static Full Throttle RPM

A

7200 RPM

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25
Q

Min Static Full Throttle RPM

A

6300 RPM

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26
Q

Min Auto Launch Climb Out RPM

A

6600 RPM up to 800ft AGL

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27
Q

Max Transient CHT

A

> 259°c During Climb to 1,000 ft AGL

28
Q

Min Cylinder Head Temperature

A

80°c

29
Q

Max Continuous Cylinder Head Temperature

A

249°c

30
Q

Rotor Temperature Operating Range on ground/flight

A

50 - 175°c

31
Q

Static Idle RPM (payload and IFF On)

A

3600 - 3840 RPM

32
Q

LIB Battery Fail

A

<10 min remaining

33
Q

Bus Voltage (with engine operating)

A

28 ±2 VDC

34
Q

Allowable Fluctuation (With no change to electrical load)

A

<3 different values within 30 seconds

35
Q

Maneuvering Limits Roll: TALS

A

± 25° AOB

36
Q

Maneuvering Limits Roll: Knobs

A

± 20° AOB

37
Q

Maneuvering Limits Roll: Pitch

A

+20° / -15°

38
Q

Launcher pitch Angle (as reported in the GCS)

A

8° - 12°

39
Q

Maneuvering Limits Roll: Commanded Toll Tolerance

A

± 6° AOB

40
Q

Airspeed - Turbulence (rough air)

A

70 KIAS

41
Q

Airspeed - Normal Range

A

65 - 110 KIAS

42
Q

Airspeed - Maximum Commanded Airspeed (Descent)

A

80 KTS

43
Q

Low Airspeed

A

55 KIAS

44
Q

TALS Auto Abort

A

< 52 or > 78 KIAS for 2 seconds

45
Q

Descent Law

A

70 - 90 KIAS

46
Q

Climb Law

A

62 KIAS

47
Q

Max Flight Time (reg)

A

9 hours

48
Q

Minimum Fule on ground (reported in GCS)

A

10L

49
Q

Max Capacity (reg)

A

58L

50
Q

Min Safe FTS Deploy

A

500ft AGL
800ft stanman

51
Q

Max Service Ceiling

A

15,000 ft AGL

52
Q

Min Altitude

A

ELOS

53
Q

Maximum Launch ALT & Weight up to 10,000 ft

A

467 lbs

54
Q

Maximum Launch ALT & Weight > 10,000 ft

A

450 lbs

55
Q

Maximum Tailwind During TALS Auto Recover

A

5 kts

56
Q

Maximum Tailwind Upon Selecting “Land AV”

A

0 Kts

57
Q

Maximum Headwind / Crosswind

A

20 G25 KTS

58
Q

Relative Humidity limitations

A

100% Non-Condensing

59
Q

Prohibited Manoeuvres 1

A

Reported airspeed of greater than 90 KIAS during descent. commanded airspeed in excess of maximum airspeed chart.

60
Q

Prohibited Manoeuvres 2

A

Flight into forecast moderate or severe icing or any known level of icing conditions.

61
Q

AV TALS Profiles During Recovery
Weight < 410 lbs TDP-AG Distance < 210

A

Profile 5

62
Q

AV TALS Profiles During Recovery
Weight > 410 lbs TDP-AG Distance < 210

A

Profile 6

63
Q

AV TALS Profiles During Recovery
Weight < 410 lbs TDP-AG Distance > 210

A

Profile 7

64
Q

AV TALS Profiles During Recovery
Weight > 410 lbs TDP-AG Distance > 210

A

Profile 8

65
Q

Fire, Smoke or Fumes In Control Station

A
  1. Fire, Fire, Fire in control station - Announce
  2. If AV link established: place AV in ‘safe’ state - Conduct
  3. Access door - Open
  4. GCS: Emergency STOP - Select
  5. Control Station - Evacuate
  6. PGCS: Power Source - Emergency STOP