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S-92A > FSI Quick Refresh > Flashcards

FSI Quick Refresh Flashcards

0
Q

Aerobatic Maneuvers Are

A

Prohibited

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1
Q

Minimum Flight Crew

A

Two pilots

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2
Q

Practice Touchdown Autorotations Are

A

Prohibited

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3
Q

360 Hovering Turn In Less Than xx Seconds Are Prohibited

A

12

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4
Q

This Aircraft Is Certified IAW…

FAA Part xx, Cat “X” and Cat “X”

A

FAA Part 29, Cat “A” and Cat “B”

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5
Q

Maximum Seating Of xx Passengers

A

19

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6
Q

What is Required Equipment For Flight? 1-3 of 7
1. One XXX
2. Two XXX
3. Four XXX’s configured as follows:
a. XXX mode both outboard displays
b. XXXXX mode on one inboard

A
  1. One APU
  2. Two DCU
  3. Four MFDs configured as follows:
    a. PFD mode both outboard displays
    b. EICAS mode on one inboard
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7
Q

What is Required Equipment For Flight? 4 of 7

  1. AFCS
    a. Day/Night VFR
    i. PXXXX/XXX or PXXXX/XXX
    ii. xxxxxx trim release
    b. IFR
    i. PXXXX and PXXXX
    ii. XXX and XXX
    iii. xxxxxx trim and xxxxxx trim
A
  1. AFCS
    a. Day/Night VFR
    i. PSAS1/AP1 or PSAS2/AP2
    ii. cyclic trim release
    b. IFR
    i. PSAS1 and PSAS2
    ii. AP1 and AP2
    iii. cyclic trim and rudder trim
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8
Q

What is Required Equipment For Flight? 5-7 of 7
5. Two xxxxxxx XX Xxx (IFR)
6. All Xxxxxxx Xxxxxxxxxxx (IFR)
7. A xxxxxxxxxx and xxxxxxxxxxxxx system that has demonstrated compliance with pertinent FAA requirements.

A
  1. Two primary AC Gen (IFR)
  2. All Standby Instruments (IFR)
  3. A navigation and communication system that has demonstrated compliance with pertinent FAA requirements.
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9
Q

Max T/O Gross Weight (Internal Load)

A

26,500

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10
Q

Max T/O Gross Weight (External Load)

A

28,300

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11
Q

Minimum Operating Weight

A

16,200

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12
Q

Category “A” Takeoffs and Landings Are Limited to xx knots of crosswind component or less.

A

35

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13
Q

Limits with Low Fuel Light(s) Illuminated

Avoid…

A

…steady state pitch attitudes in excess of
10 degrees nose up and lower than
5 degrees nose down.

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14
Q

Slope Limitations

A

10 degrees nose up/down

13 left/right side slope

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15
Q

Max Groundspeed For Landing/Takeoff

A

50 Kts Temporary Restiction

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16
Q

Max Groundspeed For Taxi Operations

A

35

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17
Q

Max Groundspeed Brake Application

A

35

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18
Q

What is your Temperature Range for Flights

A

-40C to ISA+35C

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19
Q

Pre-Heat Must Be Used For All Starts When

A

OAT is –25C or below

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20
Q

Maximum Allowable Cabin Floor Loading

A

75-lbs/sq ft or 200-lds/sq ft (heavy duty floor)

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21
Q

Maximum Tie-Down Ring Limit Is

A

5,700 lbs/ring

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22
Q

Maximum Baggage Load to Rear Ramp

A

1000 lbs

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23
Q

Maximum Shelf Capacity

A

300 lbs

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24
Q

Vne Power ON

A

165 Kts

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25
Q

Vne Power OFF

A

120 knots (If Vne is less than 120, the lower Vne shall apply for power as well)

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26
Q

Max Airspeed OEI

A

120 Kts

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27
Q

Max Airspeed One or Both SAS Inoperative

A

120 Kts

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28
Q

Max Airspeed w/one Pri Flight Servo Inoperative

A

120 Kts

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29
Q

Max Airspeed w/Hyd Boost Inoperative

A

120 Kts

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30
Q

Max Airspeed w/Landing Gear Down/Transient

A

165 Kts

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31
Q

Max Airspeed Activation L/G Blowdown

A

90 Kts

32
Q

Max Airspeed w/APU Operating

A

150 Kts

33
Q

Max Airspeed w/Emerg Flotation System Armed

A

80 Kts

34
Q

Max Airspeed for Sideward/Crosswind Flight

A

35 Kts

35
Q

Max Airspeed for Rearward/Tailwind Hover

A

35 Kts

36
Q

Main gear width

A

10’ 5”

37
Q

Nose gear to Main gear distance

A

20’ 4”

38
Q 
AEO
Max Continuous 
TRQ - xxx% Up to xxx KIAS (XXXXX controlled limit value) 
TRQ - xx% above xxx KIAS
T4.5 - xxx
Ng - xx.x%
A

TRQ - 100% Up to 100 KIAS (FADEC controlled limit value)
TRQ - 86% above 100 KIAS
T4.5 - 935
Ng - 99.9%

39
Q 
AEO
30 Min 
TRQ - xxx% (XXXXX controlled limit value)
T4.5 - xxx
Ng - xxx.x%
A

TRQ - 100% (FADEC controlled limit value)
T4.5 - 988
Ng - 101.5%

40
Q

AEO
5 Min Takeoff
TRQ - xxx% (XXXXX controlled limit value)
T4.5 - xxx (XXXXX controlled limit value)
Ng - xxx.x% (XXXXX controlled limit value)

A

TRQ - 100% (FADEC controlled limit value)
T4.5 - 995 (FADEC controlled limit value)
Ng - 102.9% (FADEC controlled limit value)

41
Q

AEO
12 Sec Transient
T4.5 - x,xxx
Ng - xxx.x%

A

T4.5 - 1,003

Ng - 103.7%

42
Q

AEO

10 Second Transient TRQ - xxx%

A

10 Second Transient TRQ - 120%

43
Q 
OEI
Max Continuous 
TRQ - xxx (XXXXX controlled limit value)
T4.5 - xxx
Ng - xxx.x
A

TRQ - 120 (FADEC controlled limit value)
T4.5 - 988
Ng - 102.4

44
Q

OEI
2-Minute
TRQ - xxx% (XXXXX controlled limit value)
T4.5 - x,xxx (XXXXX controlled limit value)
Ng - xxx.x%

A

TRQ - 120% (FADEC controlled limit value)
T4.5 - 1,006 (FADEC controlled limit value)
Ng - 102.9%

45
Q

OEI
30 Second
TRQ - xxx% (XXXXX controlled limit value)
T4.5 - xxxx (XXXXX controlled limit value)
Ng - xxx.x% (XXXXX controlled limit value)

A

TRQ - 141% (FADEC controlled limit value)
T4.5 - 1049 (FADEC controlled limit value)
Ng - 103.7% (FADEC controlled limit value)

46
Q

Maximum Starting TGT

A

1,000 deg c

47
Q

Avoid prolonged operations in Np/Nr range
xx% to xx%
and
xx% to xx%

A

36% to 49%
and
56% to 67%

48
Q

ENGINE OIL PRESSURE

Min Idle - xx to xx psi
Continuous - xx to xxx psi
Maximum (x mins) - xxx to xxx psi
Max Fluctuation - x psi

A

Min Idle - 20 to 30 psi
Continuous - 30 to 100 psi
Maximum (5 mins) - 100 to 120 psi
Max Fluctuation - 5 psi

49
Q

Do not apply engine power above ground idle until Oil pressure is below xxx psi

A

100 psi

50
Q

Engine Oil Temperatures
Max Continuous - xxx C
15 Minute - xxx C to xxx C
Maximum Allowable - xxx C

A

Max Continuous - 132 C
15 Minute - 132 C to 149 C

Maximum Allowable - 149 C

51
Q

Fuel Anti-Icing Additives Are Required At Temperatures Below -xx C

A

-20 C

52
Q

When can you operate in CROSS FEED?
CAT A – Xxxxxxxxxxx
CAT B – Xxxxxx Xxxxxx

A

CAT A – Emergencies only

CAT B – Cruise Flight only

53
Q

Starter Limits
Motor (At All Ambient Temperatures)
x minutes motoring
x minutes OFF
x minutes motoring
xx minutes OFF (cooling) repeat cycle

A

2 minutes motoring

5 minutes OFF
2 minutes motoring
30 minutes OFF (cooling) repeat cycle

54
Q

Back-To-Back Starter Limits
Ambient Temp Greater Than +15C
x consecutive starts
x minutes Off (cooling)
x consecutive start
xx minutes Off (cooling)
xxxxxx cycle

A

2 consecutive starts
5 minutes Off (cooling)
2 consecutive start
30 minutes Off (cooling)
repeat cycle

55
Q 
Back-To-Back Starter Limits
Ambient Temp At +15C or Less
x consecutive starts 
xx minutes Off (cooling) 
x consecutive start
xx minutes Off (cooling) 
repeat cycle
A

4 consecutive starts
15 minutes Off (cooling)
4 consecutive start
30 minutes Off (cooling)
repeat cycle

56
Q

What is the caution associated with the weather radar system operations?
(In part) …If an active radar mode is selected, ensure all people are at least xxx feet away from the forward xxx deg arc of the aircraft prior to takeoff.

A

CAUTION
The weather radar has a weight on wheels override that forces the system into standby when the aircraft is on the ground. Unless STBY or OFF are selected, the weather radar will radiate as soon as the helicopter lifts to a hover. If an active radar mode is selected, ensure all people are at least 100 feet away from the forward 270 deg arc of the aircraft prior to takeoff.

57
Q

Total capacity of the aircraft fuel system

Pressure Refuel - xxx Gals
Gravity refuel - xxx Gals
Total Un-useable fuel - x.x gals

A

Pressure Refuel - 764 Gals
Gravity refuel - 712 Gals
Total Un-useable fuel - 4.8 gals

58
Q

MGB OIL TEMPERATURE LIMITS
Continuous - x to xxx C
Precautionary - xxx C to xxx C
Maximum - xxx C

A

Continuous - 0 to 120 C
Precautionary - 120 C to 130 C
Maximum - 130 C

59
Q

MGB OIL PRESSURE LIMITS (In Flight)
Minimum - xx to xx psi
Continuous - xx to xx psi
Precautionary - xx to xxx psi
Maximum - xxx psi

A

Minimum - 35 to 45 psi
Continuous - 45 to 70 psi
Precautionary - 70 to 130 psi
Maximum - 130 psi

60
Q

ROTOR SPEED LIMITS - POWER ON
Maximum - xxx%
Precautionary Range - xxx% to xxx%
Norm Rotor Speed Dual Engine - xxx% to xxx%
Norm Rotor Speed OEI - xxx% to xxx%
Precautionary Range Dual Engine - xx% to xxx%
Precautionary Range OEI - xx% to xxx%
Minimum - xx%
Transient Minimum OEI - xx%
Transient At Touchdown During OEI Landing - xx%

A

Maximum - 110%
Precautionary Range - 106% to 110%
Norm Rotor Speed Dual Engine - 104% to 106%
Norm Rotor Speed OEI - 100% to 106%
Precautionary Range Dual Engine - 95% to 104%
Precautionary Range OEI - 95% to 100%
Minimum - 95%
Transient Minimum OEI - 90%
Transient At Touchdown During OEI Landing - 80%

61
Q

ROTOR SPEED LIMITS POWER OFF
Maximum - xxx%
Minimum (“LOW ROTOR” aural alert) - xx%
Transient - xx%

A

110%
95%
80%

62
Q

ROTOR BRAKE LIMITS
Engine Operating limited to xxx or xxxx engs at idle.
Both Engines Must Be Shut Xxxx Before Applying Xxxxx Xxxxx
Recommended Rotor Speed For Normal Rotor Brake Application is xx% Nr.

A

one or both
Down
Rotor Break
40%

63
Q 
When does the hydraulic backup isolation valve automatically open and close?
Start Up 
>xx% Nx WOW - Closed
>xx% Nx - Open
Shutdown 
@xx% Nx - Normal
<xx%Nx Last Engine - Open
A 
Start Up 
>15% Ng WOW - Closed
>50% Nr - Open
Shutdown 
@80% Nr - Normal
<15%Ng Last Engine - Open
64
Q

Max Airspeed after inadvertent Float Deployment
xx KIAS in a Climb
xx KIAS Level Flight
xx KIAS Descent/Auto

A

50 KIAS in a Climb
55 KIAS Level Flight

60 KIAS Descent/Auto

65
Q

Rotor Diameter - xx’ x”
Overall Length - xx’ x”
Overall Height - xx’ xx”

A

Rotor Diameter - 56’ 4”
Overall Length - 68’6”
Overall Height - 17’11”

66
Q 
What sub-modes are available from the PFD display?
Xxxx
Xxx
Xxxxx
Xxxx
Xxx X
A 
FULL 
ARC 
HOVER 
COMP 
CAT A
67
Q

What items are Auto Shed when the APU is the sole source of AC Power in flight?
X - Xxxxxxxxxx Xxxx-Xxx (Xxxxx xxxx xxxxxxxxxxx)
X - XXX
X - XXXX
X - Xxxx - #x Xxxxxx Xxxxx Xxxx-Xxx Xxxx
Xxx - Xxx Xxxxxxxxxxxx

A

W - Windshield Anti-Ice (Pilot side recoverable)
A - AVC
R - RIPS
M - Mats - #1 Engine Inlet Anti-Ice Mats
Air - Air Conditioning

68
Q 
What Systems are driven by the #2 hydraulic pump?
Xxxxx
#2 XXX Xxxxxxxx
#2 Xxxx Xxxxx Xxxxxx
#2 Xxxx Xxxxx Xxxxx
A 
Boost
#2 SAS Actuator
#2 Main Rotor Servos
#2 Tail Rotor Servo
69
Q

Ng Overspeed?

xxx.x%

A

108.5%

70
Q

Ng Limits
Dual Engine
Max Continuos - xx.x%
xx Minutes - xxx.x%
x Minute Takeoff - xxx.x% (Limiter)
xx Seconds Transient - xxx.x%

A

Max Continuos - 99.9%
30 Minutes - 101.5%
5 Minute Takeoff - 102.9% (Limiter)
12 Seconds Transient - 103.7%

71
Q

TGT
Single Engine
Max Continuous - xxx (XXX Limiter)
x minute - x,xxx (x Min Limiter)
xx second - x,xxx (xx Sec Limiter)

A

Max Continuous - 988 (MCP Limiter)

2 minute - 1,006 (2 Min Limiter)
30 second - 1,049 (30 Sec Limiter)

72
Q

VNE
VFR Day/Night (With certain PSAS/AP components inoperative):
xxx - PSAS1 and PSAS2, AP1 or AP2, ATT Mode,
cyclic and rudder trim.
xxx - PSAS1 and PSAS2, AP1 and/or AP2, SAS
Mode, cyclic and rudder trim.
xxx - PSAS1 or PSAS2, AP1 and AP2, ATT Mode,
cyclic and rudder trim.
xxx - PSAS1/AP1 or PSAS2/AP2, SAS Mode,
functional cyclic trim release.

A

165 Kts
165 Kts
120 Kts
120 Kts

73
Q

ALTITUDE LIMITS

Enroute - xx,xxx’ DA

A

15,000’

74
Q

COUPLED LIMITS
If airspeed > xxx KIAS, Then AGL must be > xxx’
If airspeed xx’
When coupled below xxx’ AGL, the pilot will monitor the flight controls and take action in the event of an excessive rate of descent.
Coupled flight below xxx’ AGL will be in visual meteorological conditions.

A

> 120 KIAS / 200’

75
Q

What if any AFCS mode can be coupled below 50 KIAS?

A

RA ALT

76
Q 
How many DC Busses are there and
what are they labeled?
#x XX Pxxxxxx
#x XX Pxxxxxx
XX Exxxxxxxx
Xxxxxxx
Xxxxxxx Xxxxxx
Xxxxxxx Xxxxxxx
A 
#1 DC Primary 
#2 DC Primary 
DC Essential 
Battery
Battery Holdup 
Battery Utility
77
Q 
What are the busses powered by the #1 DC Converter?
#x XX Pxxxxxx
Xxxxxxx Xxxxxx
Xxxxxxx Xxxxxxx
A 
#1 DC Primary
Battery Holdup
Battery Utility
78
Q

Where are the only two circuit breakers not available to the pilots from the cockpit?
x.x Amp
x Amp

A

7.5 Amp in nose compartment
4 Amp inside the external power
door

S-92A (1 decks)

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