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RC12X Study Guide > 5s & 9s > Flashcards

5s & 9s Flashcards

1
Q

VMO Max Allowable Below 11,500 feet

Max Autopilot Operation

A

248 KIAS

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2
Q

Brake Deice

A
  • Max Temp +15°C
  • 10 Minute Max Cycle
  • Minimum 85% N1 for simultaneous use of wing and antenna boots
  • Prohibited During Single Engine Operations
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3
Q

Loss of Pressurization

Above 10,000 FT AGL

A

Crew oxygen masks –100% and don.

MIC switch – OXYGEN MASK

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4
Q

Autofeather

A

Armed above 89% N1
20 to 14% Torque, Opposite Side Disarms
13 to 7% Torque, Failed Prop Feathers

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5
Q

Electrical Fire

A

Oxygen masks EMERGENCY and don

MIC switch - OXYGEN MASK

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6
Q

Bank Limits

A

60°

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7
Q

Ground Power Unit Amps Limits

A

1000 Amps for 5 Seconds
500 Amps 2 minutes
300 Amps continuously

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8
Q

Max if Windshield Icing

A

226 KIAS

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9
Q

Max Altitude for Inoperative Yaw Damper

A

17,000 ft

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10
Q

Wing Fire

A
  1. Perform engine shutdown on affected side.

2. Land as soon as possible.

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11
Q

AC/DC Power

A 
22 VDC         Min Battery Start
28 VDC         Max GPU Start
AC Freq         394-406
AC Voltage     104-124
DC Voltage     28-28.5
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12
Q

Weight Limitations (lbs)

A 
Toilet Seat for Takeoff and Landing =	238
Airstair Door Limit = 300
Max Zero Fuel = 13,100
Max Landing Weight = 15,675
Max Takeoff = 16,500
Ramp Weight = 16,620
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13
Q

Oil Temperature

A

-40° (Min) Starting
-40° to 110° Low Idle / Transient (10 min)
+10° to 105 Max Climb/Cont/Cruise/Norm/Reverse
+10° to 110° Takeoff (5 Minutes)
74° to 80°C Recommended

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14
Q

TGT Limits

A 
400-830°C Normal
750°C	Max for Low Idle
760°C	Max Reverse
800°C	 Normal Cruise and Climb
810°C	Max Cruise and Climb
830°C	Max Continuous
840°C for 5 Minutes Max for Takeoff
870°C for 20 Seconds Max Transient
1000°C for 5 Seconds Max for Starting
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15
Q

Max for Approach Flap Extension

A

197 KIAS

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16
Q

Landing Gear Retraction

A

160 KIAS

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17
Q

Starter Limitations

A

40 Seconds On, 15 Minutes OFF

40 Seconds ON, 30 Minutes OFF

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18
Q

Pitot Tube Limit

A

15 Minutes Maximum on the Ground

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19
Q

Engine Failure After V1

A
  1. POWER — Maximum allowable.
  2. LDG GEAR CONTROL handle – UP
    (two positive climb indications).
  3. Propeller — Verify feathered.
  4. FLAPS — UP after Vyse/Venr, (130 KIAS).
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20
Q

VB (Turbulence Penetration)

A

150 KIAS

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21
Q

Max Operating Temperature to 25,000 ft

A

ISA +37°C

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22
Q

Max Design Sink Rate

A

500 feet per minute

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23
Q

Min Altitude for Autopilot Use

A

200’ AGL

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24
Q

SPINS

A

Control Wheel - Full Forward, Ailerons Neutral
Full Rudder - Opposite the direction of spin
Power Levers - IDLE
Rudder - Neutralize when rotation stops
Execute a smooth recovery

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25
Q

Engine Fire In Flight

Fire Pull Handle Illuminated

A
  1. POWER Lever (affected engine) – IDLE.
  2. PROP Lever (affected engine) – FEATHER
  3. MISSION CONTROL switch - OFF
  4. CONDITION lever (affected engine) – FUEL CUTOFF.
  5. FIRE PULL handle – PULL.
  6. PUSH TO EXTINGUISH switch – Push (if required)
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26
Q

G Loading with Flaps Beyond Approach

A

0 to 2.0

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27
Q

N1 Limits

A 
62-104% Normal 
62%	Low Idle (Min)
72%	High Idle (Approximately)
88% Max Reverse
104%	Normal Cruise
104%	Max Cruise
104%	Max Continuous
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28
Q

Engine Ice Vanes

A

Extended +5°C or below and in visible moisture.

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29
Q

Pneumatic Limits

A

12-20 Normal

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30
Q

Max Operating Altitude

A

35,000 ft

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31
Q

Minimum Airspeed for using Reverse

A

40 KIAS

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32
Q

Fuel System Limitations

A

265 lbs Min for takeoff (Mains Only)
300 lbs Max Fuel Imbalance
540 gal Usable Capacity
549 gal Max Capacity (9 gal within fuel lines)
10 hrs With Fuel Press Annunciator On
150 hrs Operating with AVGAS
15,000 ft Standby Boost Pumps When Using AVGAS
30,000 ft Standby Boost Pumps When Using JP4

33
Q

Propeller Failure (OVER 1802 RPM)

A
  1. POWER lever (affected engine) – IDLE.

2. PROP lever (affected engine) – FEATHER.

34
Q

VA Design Maneuvering Speed

A

167 KIAS

35
Q

Pitch Limits

A

30°

36
Q

Generator Load Limits

A

0 -95% load 65% N1

95-100% load 70% N1

37
Q

Oil Pressure

A

+/- 10 Fluctuations Authorized
40 (Min) Starting
60 (Min) Low Idle
60-90 Torque Limited to 54%
90 Undesirable
90 to 135 All Flight Conditions
90 to 135 Takeoff (5 Minutes)
40 - 200 Transient (20 sec)
200 (Max) Starting

38
Q

VLE Landing Gear Extension

A

179 KIAS

39
Q

Windshield Heat Must be On

A

Freezing level or 10,000’ AGL

40
Q

Min Speed During Icing

A

140 KIAS

41
Q

Max 90° crosswind (Less than 13000 lbs)

A

20 KIAS

42
Q

Engine/Nacelle Fire During Start or Ground Operations

A
  1. PROP levers – FEATHER.
  2. CONDITION levers – FUEL CUTOFF.
  3. FIRE PULL handle (illuminated) – PULL.
  4. PUSH TO EXTINGUISH switch – Push (if required).
  5. MASTER SWITCH – OFF.
43
Q

Engine Malfunction During Final Approach

A
  1. POWER – As required.

2. GEAR – Recheck DN.

44
Q

Propeller De-Ice Ammeter

A

26-32 Amps

45
Q

Max Demonstrated Crosswind

A

20 or 25Kts @ 90 if below / above 13,000 lbs

46
Q

VMCA (Red Line)

A

103 KIAS

(VMCA = the minimum flight speed at which the aircraft is directionally controllable. Certification conditions include one engine becoming inoperative and propeller feathered, up to a 5° bank toward the operative engine, takeoff power on the operative engine, landing gear up, flaps up, most rear-ward CG)

47
Q

Gyro Suction

A

2.8 - 5.9 Normal

48
Q

Overspeed Governor

A

1802 RPM

Test: 1540 to 1580 RPM

49
Q

De-Ice Boots

A

½ (.5) inch Ice Build Up Prior to Activating Surface Deice

¼ (.25)°inch Ice Build Up Prior to Activating Antenna Deice

16 psi min With One Bleed Air Source Inoperative

Below -40°C Operation Can Cause Permanent Damage

50
Q

Engine Malfunction Prior to or at V1 (Abort)

A
  1. POWER levers — GROUND FINE.
  2. Braking – AS REQUIRED

^^^^^^^^^^^^^^^^^^^^

  1. REVERSE THRUST - AS REQUIRED

if insufficient runway remains for stopping perform the following:

  1. CONDITION LEVERS - FUEL CUTOFF
  2. FIRE PULL HANDLES - PULL
  3. MASTER SWITCH - OFF
51
Q

Fuselage Fire

A
  1. Fight the fire.

2. Land as soon as possible if fire continues.

52
Q

VSSE (Safe One-engine Operating Speed)

A

115 KIAS

(The safe one engine inoperative speed selected to provide a reasonable margin against the occurrence of an unintentional stall when making intentional engine cuts)

53
Q

Landing Gear Cycling

A

5 Complete Cycles (Extension and Retraction) in a 20 minute period.

10 to 15 minute cooling period Between 20 Minute Time Groupings.

Cycle rate should Not Exceed 10 cycles Equally Spaced in 1 Hour.

54
Q

G Loading with Flaps Up or Approach

A

–1.21 to 3.02

55
Q

Engine Malfunction (Second Engine)

A
  1. Airspeed – As required.
  2. POWER lever – IDLE.
  3. PROP lever – As required.
56
Q

Torque Limitations

A 
54%	With <1000 RPM (N2)
75%	Max Reverse
83% Max at 1700 RPM (N2)
94%	Max at 1500 RPM (N2)
100%	Max for Takeoff
100%	Continuous
138% for 20 Sec	Max Transient
57
Q

Max Cabin Differential

A

6.5 psi

58
Q

Engine Malfunction During Flight

A
  1. Autopilot/Yaw Damper – Disengage.
  2. POWER – As required.
  3. Dead engine – Identify.
  4. Propeller – Verify feather.
59
Q

VREF

A

111 KIAS

60
Q

Max Operating Temperature above 25,000 ft

A

ISA +31°C

61
Q

Emergency Descent

A
  1. POWER levers – IDLE.
  2. PROP levers – HIGH RPM.
  3. FLAPS – APPROACH.
  4. Gear– DN.
  5. Airspeed – 179 KIAS maximum.
62
Q

Max for FULL Flap Extension

A

151 KIAS

63
Q

Max 90° crosswind (Greater than 13000 lbs)

A

25 KIAS

64
Q

PROP RPM N2

A 
1000	Minimum unless in Feather
1450-1700 Normal
1650	Max Reverse
1700 	Max Continuous
1870 	Max Transient (for 20 Sec)
65
Q

Cruise Climb Airspeeds

A 
SL to 10,000 ft at Pilot’s Discretion = 160
SL to 10,000 ft = 135
10,000 to 20,000 ft = 130
20,000 to 25,000 ft = 125
25,000 to 35,000 ft = 120
66
Q

SINGLE ENGINE GO-AROUND

A
  1. POWER – Maximum allowable.
  2. LDG GEAR CONTROL HANDLE – UP.
  3. FLAPS – UP.
  4. Airspeed – VYSE
67
Q

Smoke and Fume Elimination

A

Crew oxygen masks –EMG and Don.

MIC Switch - Oxygen Mask

^^^^^^^^^^^^^^^^^^^^^^^^^^^

  1. “ENVIRO & PNEU BLEED AIR valve switches — PNEU ONLY.
  2. FWD VENT BLOWER switch — AUTO.
  3. AFT VENT BLOWER switch — Off.
  4. CABIN AIR MODE SELECT switch — OFF.”

If smoke and fumes are not eliminated:

  1. CABIN PRESS switch — DUMP.

NOTE Opening storm window (after depressurizing) will facilitate smoke and fume removal.

  1. Engine instruments — Monitor.
68
Q

VYSE
VENR
Recommended for Autopilot-Coupled Approaches

A

130 KIAS

69
Q

In-Flight Starting Limitations

A

In-flight engine restarts shall be conducted within 2 minutes or after 10 minutes, except if the engine is required for safety.

(This is due to thermal expansion issues)

70
Q

Wing Tip Pod Limitations

A

254 lbs Minimum Weight for Pods w/out Limits
14,000 lbs Maximum Gross Takeoff Weight
11,000 lbs Maximum Zero Fuel Weight

71
Q

Common Missile Warning System Safety Pin Limitations

A

The Safe/Arm Control Panel SAFETY PIN shall be installed during all ground operations.

72
Q

Use of A/P During Severe Icing is ____________

A

Use of A/P During Severe Icing is Prohibited

73
Q

Sustained Flight in Icing w/ Flaps Extended is ____________

A

Sustained Flight in Icing w/ Flaps Extended is Prohibited

74
Q

Cracked Or Shattered Windshield (One-Time Evac Mission)

A

25,000 ft Max Altitude
25 Hours Max

Continued Flight with Cracked WS Cracks must NOT impair visibility

Cracks must NOT interfere with windshield wipers

Windshield anti-ice REQUIRED for flights into icing

2.0-4.6 PSID Required Cabin Diff until Landing

75
Q

Crack in Any SIDE Window (One-Time Evac Mission)

A

25 Hours Maximum

Pressurized flight is PROHIBITED due to cracked side window.

Conduct flight w/ the cabin pressure switch in DUMP position

76
Q

Vmo between 11,500-35,000ft

A

0.472 Mach

77
Q

Spins, Aerobatics, Abrupt Maneuvers above 167KIAS

A

Prohibited

78
Q

Do not attempt an airstart if N1 indicates ____, if there was a ____ ____ or there was a ____. Starting an engine under these conditions may have catastrophic results. Loss of aircraft control, damage to equipment, injury, and/or loss of life may occur.

A

0

Fuel Leak

Fire

RC12X Study Guide (16 decks)

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