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FS139INIT > 001-139 AGO > Flashcards

001-139 AGO Flashcards

1
Q

Aircraft General Cover Slide

A

Nothing

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2
Q

Aircraft General

A

Nothing

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3
Q

Lesson Objectives

A

Discuss slide

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4
Q

Lesson Organization

A

Discuss slide

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5
Q

AW139 Overview

A
  • Multi-purpose
  • 2-Pratt & Whitney PT6C-67C turboshaft engines.
  • 5-Fully articulated main rotor blades
  • 4-Fully articulated tail rotor blades
  • Max gross weight 14,991 lbs (6800 kg)
  • Vne - 167 kts
  • Flight Range 420 nm
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6
Q

AW139 Cockpit

A
  • 4-LCD displays
  • Honeywell Primus Epic avionics system
  • Honeywell MCDU (Multifunction Control Display Unit)
  • 4-axis digital AFCS
  • Show CAS (Crew Alert System) window for future reference
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7
Q

Aircraft Terminology

A

Discuss slide content

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8
Q

Lesson Organization - Aircraft Dimensions and Configurations

A

Nothing

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9
Q

Aircraft Dimensions

A

Discuss primary aircraft dimensions

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10
Q

Cabin & Baggage Door Dimensions

A

Discuss aircraft dimensions

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11
Q

Aircraft Major Zones

A

Discuss aircraft zones

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12
Q

Aircraft Danger Areas

A

Discuss aircraft danger areas

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13
Q

Cockpit Configuration

A

Discuss cockpit configuration

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14
Q

Cabin Configuration

A

Discuss cabin configuration

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15
Q

Lesson Organization - Performance Limitations & Certification

A

Nothing

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16
Q

Performance Limits & Certification

A
  • RFM - Section 1 - Limitations

* Day / night - VFR / IFR

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17
Q

Airworthiness Certificate

A

Airworthiness Certificate must be on-board at all times

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18
Q

Aircraft Data Plate

A

Nothing

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19
Q

Lesson Organization - Panels, Doors & Exits

A

Nothing

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20
Q

Access panels / Doors

A

Discuss panels and doors

21
Q

Maintenance Steps

A

Discuss maintenance steps

22
Q

Nose Door

A

Discuss nose door

23
Q

Cockpit Doors

A

Discuss Cockpit doors

24
Q

Cabin Doors & Windows

A

Discuss cabin doors and windows

  • Windows are held into the door with rubber seals
25
Q

Cabin Door Operation

A

Discuss cabin door operation

  • Safety Precaution:
  • Door handle held until door is at full travel and locked
26
Q

Baggage Compartment Door

A

Discuss operation of the baggage compartment door

27
Q

Baggage Compartment Door Ops

A

Discuss the operation of the baggage compartment door

28
Q

Emergency Exits

A

Discuss emergency exits

  1. Remove the red strap
  2. Pull the inner filler wedge and seal
  3. Window pushed/pulled inboard to remove the window.
29
Q

HEELS

A

Helicopter Emergency Exit Lighting System

  • Illuminate the emergency exits
  • 4 green on the corners, 1 white to identify pullout strap
  • 5 independent batteries - One for each door and one for the windows
  • Ten water activated sensors - 2 for each door, 1 for each window
30
Q

Door CAS Messages

A

Discuss Slide

31
Q

Lesson Organization - Ground Handling

32
Q

Ground Handling

A
  • AW139 RFM Section 8

* Employer requirements

33
Q

Aircraft on Jacks & Leveling

A

Discuss Slide

34
Q

Aircraft Towing

A
  • Towed at a walking speed
  • Max towing speed - 23 mph (37 km/hr)
  • RFM Section 8-1
35
Q

Parking & Securing

A
  • RFM Section 8-3
  • Tiedowns required:
  • Thunderstorms forecasted
  • Winds 20 kts +
  • Wind gusts 15 kts +
  • Parking within 150 feet of hovering or taxiing aircraft above 11,900
  • Parked overnight
  • No slack in the tiedowns but not so much to flex the rotor blades
36
Q

Protective Covers

A

Discuss protective covers

37
Q

Mooring

A
  • Wind forcasted at 45 knots or greater

* Aircraft evacuated when winds forecasted at 75 knots or greater.

38
Q

Lesson Organization - Marking & Placards

39
Q

Marking & Placards - Exterior

A
  • information
  • Operating instructions
  • Limitations
  • Safety precautions
  • Escape/Rescue instructions
  • Servicing instructions
40
Q

Marking & Placards - Interior

A
  • information
  • Operating instructions
  • Limitations
  • Safety precautions
  • Escape/Rescue instructions
  • Servicing instructions
41
Q

Lesson Organization - Summary

42
Q

Summary

A
  • Multi-purpose
  • 2-Pratt & Whitney PT6C-67C turboshaft engines.
  • 5-Fully articulated main rotor blades
  • 4-Fully articulated tail rotor blades
  • Max gross weight 14,991 lbs (6800 kg)
  • Vne - 167 kts
  • Flight Range 420 nm
43
Q

Question #1

A

Question #1

44
Q

Question #1

A

C. Door handle held until door is at full travel and locked

45
Q

Question #2

A

Question #2

46
Q

Question #2

A

A. Remove red strap from the clinch stud and pull

47
Q

Aircraft General

A

Aircraft General

48
Q

FlightSafety Slide

FS139INIT (2 decks)

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