Category Archives: Avionics

What are the ATA Chapters and sub-chapters, and Avionics related ATA’s

An Exhaustive list can be found here:

http://www.s-techent.com/ATA100.htm#[80]

Here is the

ATA Chapters

Chapter 05

  • 05-00-00 Periodic Inspections
  • 05-10-00 Time Limit
  • 05-20-00 Scheduled Maintenance Checks
  • 05-30-00 [As Required]
  • 05-40-00 [As Required]
  • 05-50-00 Unscheduled Maintenance Checks

Chapter 06

  • Dimensions & Areas
  • Those charts, diagrams, and text which show the area, dimensions, stations, access doors / zoning and physical locations, of the major structural members of the aircraft. Includes an explanation of the system of zoning and measurement used.

Chapter 07

  • 07-00-00 Lifting & Shoring
  • 07-10-00 Jacking
  • 07-20-00 Shoring

Chapter 08

  • 08-00-00 Leveling & Weighing
  • 08-10-00 Weighting & Balancing
  • 08-20-00 Leveling

Chapter 09

  • 09-00-00 Towing & Taxiing
  • 09-10-00 Towing
  • 09-20-00 Taxiing

Chapter 10

  • 10-00-00 Parking, Mooring, Storage & Return To Service
  • 10-10-00 Parking / Storage
  • 10-20-00 Mooring
  • 10-30-00 Return To Service

Chapter 11

  • 11-00-00 Placards & Marking
  • 11-10-00 Exterior Color Schemes & Markings
  • 11-20-00 Exterior Placards & Markings
  • 11-30-00 Interior Placards

Chapter 12

  • 12-00-00 Servicing Routine Maintenance
  • 12-10-00 Replenishing
  • 12-20-00 Scheduled Servicing
  • 12-30-00 Unscheduled Servicing

Airframe Systems

Chapter 20

  • 20-00-00 Standard Practices

Chapter 21

  • 21-00-00 Air Conditioning
  • 21-10-00 Compression
  • 21-20-00 Distribution
  • 21-30-00 Pressurization Control
  • 21-40-00 Heating
  • 21-50-00 Cooling
  • 21-60-00 Temperature Control
  • 21-70-00 Moisturize / Air Contamination Control

Chapter 22

  • 22-00-00 Auto flight
  • 22-10-00 Autopilot
  • 22-20-00 Speed-Attitude Correction
  • 22-30-00 Auto Throttle
  • 22-40-00 System Monitor
  • 22-50-00 Aerodynamic Load Alleviating

Chapter 23

  • 23-00-00 Communications
  • 23-10-00 Speech Communication
  • 23-20-00 Data Transmission & Automatic Calling
  • 23-30-00 Passenger Address, Entertainment & Comfort
  • 23-40-00 Interphone
  • 23-50-00 Audio Integrating
  • 23-60-00 Static Discharging
  • 23-70-00 Audio & Video Monitoring
  • 23-80-00 Integrated Automatic Tuning

Chapter 24

  • 24-00-00 Electrical Power
  • 24-10-00 Generator Drive
  • 24-20-00 AC Generation
  • 24-30-00 DC Generation
  • 24-40-00 External Power
  • 24-50-00 AC Electrical Load Distribution
  • 24-60-00 DC Electrical Load Distribution
  • 24-70-00 Primary & Secondary Power

Chapter 25

  • 25-00-00 Equipment & Furnishings
  • 25-10-00 Flight Compartment
  • 25-20-00 Passenger Compartment
  • 25-30-00 Buffet / Galley
  • 25-40-00 Lavatories
  • 25-50-00 Cargo Compartments
  • 25-60-00 Emergency
  • 25-70-00 Accessory Compartments
  • 25-80-00 Insulation

Chapter 26

  • 26-00-00 Fire Protection
  • 26-10-00 Detection
  • 26-20-00 Extinguishing
  • 26-30-00 Explosion Suppression

Chapter 27

  • 27-00-00 Flight Controls
  • 27-10-00 Aileron & Tab
  • 27-20-00 Rudder & Tab
  • 27-30-00 Elevator & Tab
  • 27-40-00 Horizontal Stabilizer
  • 27-50-00 Flaps
  • 27-60-00 Spoiler, Drag Devices, Fairings
  • 27-70-00 Gust Lock & Damper
  • 27-80-00 Lift Augmenting

Chapter 28

  • 28-00-00 Fuel
  • 28-10-00 Storage
  • 28-20-00 Distribution
  • 28-30-00 Dump
  • 28-40-00 Indicating

Chapter 29

  • 29-00-00 Hydraulic Power
  • 29-10-00 Main
  • 29-20-00 Auxiliary
  • 29-30-00 Indicating

Chapter 30

  • 30-00-00 Ice & Rain Protection
  • 30-10-00 Airfoil
  • 30-20-00 Air Intakes
  • 30-30-00 Pitot & Static
  • 30-40-00 Windows, Windshields & Doors
  • 30-50-00 Antennas & Radomes
  • 30-60-00 Propellers & Rotors
  • 30-70-00 Water Lines
  • 30-80-00 Detection

Chapter 31

  • 31-00-00 Indicating & Recording Systems
  • 31-10-00 Instrument & Control Panels
  • 31-20-00 Independent Instruments
  • 31-30-00 Recorders
  • 31-40-00 Central Computers
  • 31-50-00 Central Warning Systems
  • 31-60-00 Central Display Systems
  • 31-70-00 Automatic Data Reporting Systems

Chapter 32

  • 32-00-00 Landing Gear
  • 32-10-00 Main Gear & Doors
  • 32-20-00 Nose Gear & Doors
  • 32-30-00 Extension & Retraction
  • 32-40-00 Wheels & Brakes
  • 32-50-00 Steering
  • 32-60-00 Position & Warning
  • 32-70-00 Supplementary Gear

Chapter 33

  • 33-00-00 Lights
  • 33-10-00 General Compartment
  • 33-20-00 Passenger Compartments
  • 33-30-00 Cargo and Service Compartments
  • 33-40-00 Exterior
  • 33-50-00 Emergency Lighting

Chapter 34

  • 34-00-00 Navigation
  • 34-10-00 Flight Environment Data
  • 34-20-00 Attitude & Direction
  • 34-30-00 Landing & Taxiing Aids
  • 34-40-00 Independent Position Determining
  • 34-50-00 Dependent Position Determining
  • 34-60-00 Flight Management Computing

Chapter 35

  • 35-00-00 Oxygen
  • 35-10-00 Crew
  • 35-20-00 Passenger
  • 35-30-00 Portable

Chapter 36

  • 36-00-00 Pneumatic
  • 36-10-10 Distribution
  • 36-20-00 Indicating

Chapter 37

  • 37-00-00 Vacuum
  • 37-10-00 Distribution
  • 37-20-00 Indicating

Chapter 38

  • 38-00-00 Water & Waste
  • 38-10-00 Potable
  • 38-20-00 Wash
  • 38-30-00 Waste Disposal
  • 38-40-00 Air Supply

Chapter 39

  • 39-00-00 Electrical – Electronic Panels & Multipurpose Components
  • 39-10-00 Instrument & Control Panels
  • 39-20-00 Electrical & Electronic Equipment Racks
  • 39-30-00 Electrical & Electronic Junction Boxes
  • 39-40-00 Multipurpose Electronic Components
  • 39-50-00 Integrated Circuits
  • 39-60-00 Printed Circuit Card Assemblies

Chapter 41

  • 41-00-00 Water Ballast
  • 41-10-00 Storage
  • 41-20-00 Dump
  • 41-30-00 Indication

Chapter 42

  • 42-00-00 Integrated Modular Avionics
  • 42-10-00 Core System
  • 42-20-00 3D Network Components

Chapter 44

  • 44-00-00 Cabin System
  • 44-10-00 Cabin Core System
  • 44-20-00 In-flight Entertainment System
  • 44-30-00 External Communication System
  • 44-40-00 Cabin Mass Memory System
  • 44-50-00 Cabin Monitoring System
  • 44-60-00 Miscellaneous Cabin System

Chapter 45

  • 45-00-00 Central Maintenance Systems (CMS)
  • 45-10-00 CMS / Aircraft General
  • 45-20-00 CMS / Airframe Systems
  • 45-30-00 Central Maintenance System
  • 45-40-00 CMS / Airframe Systems
  • 45-50-00 CMS / Structures
  • 45-60-00 CMS / Propellers
  • 45-70-00 CMS / Power Plant

Chapter 46

  • 46-00-00 Information Systems
  • 46-10-00 Airplane General Information Systems
  • 46-20-00 Flight Deck Information Systems
  • 46-30-00 Maintenance Information Systems
  • 46-40-00 Passenger Cabin Information Systems
  • 46-50-00 Miscellaneous Information Systems

Chapter 47

  • 47-00-00 Inert Gas System
  • 47-10-00 Generation / Storage
  • 47-20-00 Distribution
  • 47-30-00 Control
  • 47-40-00 Indicating

Chapter 49

  • 49-00-00 Airborne Auxiliary Power
  • 49-10-00 Power Plant
  • 49-20-00 Engine
  • 49-30-00 Engine Fuel & Control
  • 49-40-00 Ignition / Starting
  • 49-50-00 Air
  • 49-60-00 Engine Controls
  • 49-70-00 Indicating
  • 49-80-00 Exhaust
  • 49-90-00 Oil

Structures

Chapter 50

  • 50-00-00 Cargo & Accessory Compartments
  • 50-10-00 Cargo Compartments
  • 50-20-00 Cargo Loading Systems
  • 50-30-00 Cargo Related Systems
  • 50-40-00 Unassigned
  • 50-50-00 Accessory Compartments
  • 50-60-00 Insulation

Chapter 51

  • 51-00-00 Standard Practices & Structures General
  • 51-10-00 Investigation, Cleanup & Aerodynamic Smoothness
  • 51-20-00 Processes
  • 51-30-00 Materials
  • 51-40-00 Fasteners
  • 51-50-00 Support of Airplane for Repair & Alignment Check Procedures
  • 51-60-00 Control-Surface Balancing
  • 51-70-00 Repairs
  • 51-80-00 Electrical Bonding

Chapter 52

  • 52-00-00 Doors
  • 52-10-00 Passenger / Crew
  • 52-20-00 Emergency Exit
  • 52-30-00 Cargo
  • 52-40-00 Service
  • 52-50-00 Fixed Interior
  • 52-60-00 Entrance Stairs
  • 52-70-00 Door Warning
  • 52-80-00 Landing Gear

Chapter 53

  • 53-00-00 Fuselage
  • 53-10-00 Main Frame
  • 53-20-00 Auxiliary Structure
  • 53-30-00 Plates-Skin
  • 53-40-00 Attach Fittings
  • 53-50-00 Aerodynamic Fairings
  • 53-60-00 [As Required]
  • 53-70-00 [As Required]
  • 53-80-00 [As Required]
  • 53-90-00 [As Required]

Chapter 54

  • 54-00-00 Nacelles / Pylons
  • 54-10-00 Nacelle [As Required]
  • 54-20-00 Nacelle [As Required]
  • 54-30-00 Nacelle [As Required]
  • 54-40-00 Nacelle [As Required]
  • 54-50-00 Pylon [As Required]
  • 54-60-00 Pylon [As Required]
  • 54-70-00 Pylon [As Required]
  • 45-80-00 Pylon [As Required]

Chapter 55

  • 55-00-00 Stabilizers
  • 55-10-00 Horizontal Stabilizer / Canard
  • 55-20-00 Elevator
  • 55-30-00 Vertical Stabilizer
  • 55-40-00 Rudder

Chapter 56

  • 56-00-00 Windows
  • 56-10-00 Flight Compartment
  • 56-20-00 Passenger Compartment
  • 56-30-00 Door
  • 56-40-00 Inspection & Observation

Chapter 57

  • 57-00-00 Wings
  • 57-10-00 Center Wing
  • 57-20-00 Outer Wing
  • 57-30-00 Wing Tip
  • 57-40-00 Leading Edge & Leading Edge
  • 57-50-00 Trailing Edge &Trailing Edge
  • 57-60-00 Ailerons & Elevons
  • 57-70-00 Spoilers
  • 57-80-00 [As Required]
  • 57-90-00 Wing Folding System

Propeller / Rotor

Chapter 60

  • 60-00-00 Standard Practices-Propeller / Rotor

Chapter 61

  • 61-00-00 Propellers / Propulsion
  • 61-10-00 Propeller Assembly
  • 61-20-00 Controlling
  • 61-30-00 Braking
  • 61-40-00 Indicating
  • 61-50-00 Propulsor Duct

Chapter 62

  • 62-00-00 Rotors
  • 62-10-00 Rotor Blades
  • 62-30-00 Rotor Head
  • 62-40-00 Rotor Shaft / Swashplate Assembly
  • 62-50-00 Indicating

Chapter 63

  • 63-00-00 Rotor Drives
  • 63-10-00 General
  • 63-20-00 Engine / Gearbox Couplings
  • 63-30-00 Gearbox
  • 63-40-00 Mounts / Attachments
  • 63-50-00 Indicating

Chapter 64

  • 64-00-00 Tail Rotor
  • 64-10-00 Rotor Blades
  • 64-20-00 Rotor Head
  • 64-30-00 [Unassigned]
  • 64-40-00 Indicating

Chapter 65

  • 65-00-00 Tail Rotor Drive
  • 65-10-00 Shafts
  • 65-20-00 Gearboxes
  • 65-30-00 [Unassigned]
  • 65-40-00 Indicating

Chapter 66

  • 66-00-00 Folding Blades & Tail Pylon
  • 66-10-00 Rotor Blades
  • 66-20-00 Tail Pylon
  • 66-30-00 Controls & Indicating

Chapter 67

  • 67-00-00 Rotors Flight Control
  • 67-10-00 Rotor Control
  • 67-20-00 Anti-Torque Rotor Control (Yaw Control)
  • 67-30-00 Servo-Control System

Power Plant

Chapter 70

  • 70-00-00 Standard Practices Engine

Chapter 71

  • 71-00-00 Power Plant
  • 71-10-00 Cowling
  • 71-20-00 Mounts
  • 71-30-00 Fire Seals & Shrouds
  • 71-40-00 Attach Fittings
  • 71-50-00 Electrical Harness
  • 71-60-00 Air Intakes
  • 71-70-00 Engine Drains

Chapter 72

  • 72-00-00 Engine Turbine / Turboprop
  • 72-10-00 Reduction Gear & Shaft
  • 72-20-00 Air Inlet Section
  • 72-30-00 Compressor Section
  • 72-40-00 Combustion Section
  • 72-50-00 Turbine Section
  • 72-60-00 Accessory Drives
  • 72-70-00 By-Pass Section
  • 72-80-00 Propulsor Section (Rear Mounted)

Chapter 73

  • 73-00-00 Engine Fuel & Control
  • 73-10-00 Distribution
  • 73-15-00 Divider Flow
  • 73-20-00 Controlling
  • 73-25-00 Unit Fuel Control
  • 73-30-00 Indicating

Chapter 74

  • 74-00-00 Ignition
  • 74-10-00 Electrical Power Supply
  • 74-20-00 Distribution
  • 74-30-00 Switching

Chapter 75

  • 75-00-00 Air
  • 75-10-00 Engine Anti-Icing
  • 75-20-00 Engine Cooling
  • 75-30-00 Compressor Control
  • 75-40-00 Indicating

Chapter 76

  • 76-00-00 Engine Controls
  • 76-10-00 Power Control
  • 76-20-00 Emergency Shutdown

Chapter 77

  • 77-00-00 Engine Indicating
  • 77-10-00 Power Control
  • 77-20-00 Temperature
  • 77-30-00 Analyzers
  • 77-40-00 Integrated Engine Instrument Systems

Chapter 78

  • 78-00-00 Exhaust
  • 78-10-00 Collector / Nozzle
  • 78-20-00 Noise Suppressor
  • 78-30-00 Thrust Reverser
  • 78-40-00 Supplementary Air

Chapter 79

  • 79-00-00 Oil
  • 79-10-00 Storage
  • 79-20-00 Distribution
  • 79-30-00 Indicating

Chapter 80

  • 80-00-00 Starting
  • 80-10-00 Cranking

Chapter 81

  • 81-00-00 Turbines
  • 81-10-00 Power Recovery
  • 81-20-00 Turbo-Supercharger

Chapter 82

  • 82-00-00 Water Injection
  • 82-10-00 Storage
  • 82-20-00 Distribution
  • 82-30-00 Dumping & Purging
  • 82-40-00 Indicating

Chapter 83

  • 83-00-00 Accessory Gear Boxes
  • 83-10-00 Drive Shaft Section
  • 83-20-00 Gear Box

Chapter 84

  • 84-00-00 Propulsion Augmentation
  • 81-10-00 Jet Assist Takeoff

Chapter 91

  • 91-00-00 Charts

____________________________________________________________________________

Avionics related ATA’s

 

Modern Avionics related ATA’s

ATA Chapters

  • 12-00-00 Servicing Routine Maintenance

  • 12-10-00 Replenishing

  • 12-20-00 Scheduled Servicing

  • 12-30-00 Unscheduled Servicing

Airframe Systems

Chapter 20

  • 20-00-00 Standard Practices

Chapter 21

  • 21-00-00 Air Conditioning

  • 21-10-00 Compression

  • 21-20-00 Distribution

  • 21-30-00 Pressurization Control

  • 21-40-00 Heating

  • 21-50-00 Cooling

  • 21-60-00 Temperature Control

  • 21-70-00 Moisturize / Air Contamination Control

Chapter 22

  • 22-00-00 Auto flight

  • 22-10-00 Autopilot

  • 22-20-00 Speed-Attitude Correction

  • 22-30-00 Auto Throttle

  • 22-40-00 System Monitor

  • 22-50-00 Aerodynamic Load Alleviating

Chapter 23

  • 23-00-00 Communications

  • 23-10-00 Speech Communication

  • 23-20-00 Data Transmission & Automatic Calling

  • 23-30-00 Passenger Address, Entertainment & Comfort

  • 23-40-00 Interphone

  • 23-50-00 Audio Integrating

  • 23-60-00 Static Discharging

  • 23-70-00 Audio & Video Monitoring

  • 23-80-00 Integrated Automatic Tuning

Chapter 24

  • 24-00-00 Electrical Power

  • 24-10-00 Generator Drive

  • 24-20-00 AC Generation

  • 24-30-00 DC Generation

  • 24-40-00 External Power

  • 24-50-00 AC Electrical Load Distribution

  • 24-60-00 DC Electrical Load Distribution

  • 24-70-00 Primary & Secondary Power

Chapter 25

  • 25-00-00 Equipment & Furnishings

  • 25-10-00 Flight Compartment

  • 25-20-00 Passenger Compartment

  • 25-30-00 Buffet / Galley

  • 25-40-00 Lavatories

  • 25-50-00 Cargo Compartments

  • 25-60-00 Emergency

  • 25-70-00 Accessory Compartments

  • 25-80-00 Insulation

Chapter 27

  • 27-00-00 Flight Controls r 30

  • 30-00-00 Ice & Rain Protection

Chapter 31

  • 31-00-00 Indicating & Recording Systems

  • 31-10-00 Instrument & Control Panels

  • 31-20-00 Independent Instruments

  • 31-30-00 Recorders

  • 31-40-00 Central Computers

  • 31-50-00 Central Warning Systems

  • 31-60-00 Central Display Systems

  • 31-70-00 Automatic Data Reporting Systems

Chapter 33

  • 33-00-00 Lights

  • 33-10-00 General Compartment

  • 33-20-00 Passenger Compartments

  • 33-30-00 Cargo and Service Compartments

  • 33-40-00 Exterior

  • 33-50-00 Emergency Lighting

Chapter 34

  • 34-00-00 Navigation

  • 34-10-00 Flight Environment Data

  • 34-20-00 Attitude & Direction

  • 34-30-00 Landing & Taxiing Aids

  • 34-40-00 Independent Position Determining

  • 34-50-00 Dependent Position Determining

  • 34-60-00 Flight Management Computing

Chapter 36

  • 36-00-00 Pneumatic

  • 36-10-10 Distribution

  • 36-20-00 Indicating

Chapter 39

  • 39-00-00 Electrical – Electronic Panels & Multipurpose Components

  • 39-10-00 Instrument & Control Panels

  • 39-20-00 Electrical & Electronic Equipment Racks

  • 39-30-00 Electrical & Electronic Junction Boxes

  • 39-40-00 Multipurpose Electronic Components

  • 39-50-00 Integrated Circuits

  • 39-60-00 Printed Circuit Card Assemblies

Chapter 44

  • 44-00-00 Cabin System

  • 44-10-00 Cabin Core System

  • 44-20-00 In-flight Entertainment System

  • 44-30-00 External Communication System

  • 44-40-00 Cabin Mass Memory System

  • 44-50-00 Cabin Monitoring System

  • 44-60-00 Miscellaneous Cabin System

Chapter 45

  • 45-00-00 Central Maintenance Systems (CMS)

  • 45-10-00 CMS / Aircraft General

  • 45-20-00 CMS / Airframe Systems

  • 45-30-00 Central Maintenance System

  • 45-40-00 CMS / Airframe Systems

  • 45-50-00 CMS / Structures

  • 45-60-00 CMS / Propellers

  • 45-70-00 CMS / Power Plant

Structures

Power Plant

Chapter 70

  • 70-00-00 Standard Practices Engine

How do I make peace with the broadband in VP-BMB

Aircell

VP-BMB Broad band QuickGuide:

The Airstream AOC Router is found at 192.168.0.1 user admin pw flightstream

I modified the Proxy and so-on with Jo Krimsrieter on the phone. Screen captures below.

The 5040 box is found at 192.168. 1 . 10  user: admin: PW 1234

as I left it June 20, 2014, the DHCP SERVER is OFF in the 5040 box. That is contrary to the wishes of Chis Habina.

Back on, now that we understand that the 5040 connection is on the WAN side of the AOC Wireless router

_______________________________________________________________________________________

Access the 5040 through the face…. Under the 3rd floorboard.

Or through the  VIP right drink ledge.

192.168.0.1 brings you to the splash screen.

Notes
image

Here is the 5040. Dashboard

While in the 5040 box I set ADMINISTRATION> LAN>     DHCP  > DISABLED……that is contrary to Chris Habinas wishes.

Here are craigs notes after getting started on the Cobham 5040

https://www.dropbox.com/s/g06alafma499qix/VP-BMB_FDR_DownloadJune2014.DLU
Here is the screen shots while configurng

 

Here is some notes while Jo had me button clicking inside the FlightStream

DNS to 192.168.0.1

Static IP to 192.168.0.200  /24

Gateway to 192.168.0.1

 

Not sure if I entirely follow that logic.

 

What do we use fo9r Speed Test?

 

Speed Tests

How to I troubleshoot a Honeywell 880 radar

Here are some example faults

 

880 has RS 232 troubleshooting port out of the RT base.

Roll Cal proceedure

To exit force standby , STAB button 4 times in 3 seconds. Remember a 870 is different, some combination of push and hold 3 buttons.

_____________________________________-

 

 

Pilot Event Marker

(1) A pilot event marker is created by operating the switch on the GAIN control for two

cycles (pull out, push in, pull out, push in). A full set of parameters at that instant is

stored in the fault log. This can be useful if the pilot senses that there may be

something abnormal with the radar operation, but no fault code is being shown. This

data must be read using the RS–232 port.

 

Altitude rings

How do I make peace with Baker Audio switching….MHE

The software is called MHcom

 

In BMB the 9 pin test port is in the right mid-cabin cabinet.

 

Buss terminators are there also on the Tstrip.

!!!!!!!!!!!!!!!!!!!!FIRST!!!!!!!!!!!!!!!!!!!

 

The buss at any/every pin 3 to 4 must read 60 ohms, that is 1 120 OHM resistor on each end of the buss.

 

THEN go to MH com

 

here is the initial hookup

 

http://youtu.be/qnlo6bzNQRQ

 

for BMB the direct ping is 4.27.0.XX where XX is the id of the unit you are trying to hit

 

here are the print for BZZ

 

59454300 Baker MH Entertainment Sys

 

Switch Panel Options

baker_SwPanel_definitions

 

Notes from a previous mechanic lost in the mist of time

baker_SwPanel_Shopnotes

t

P p

 

 

How do I come to terms with a Honeywell MK V EGPWS?

How Often should I install a EGPWS database?

Our ICA’s for the installatins on BMB and BZZ do not require ANY update, EVER.

Many N registered aircraft are never updated, until upgrade time.

That seems a little slack.

The Honeywell website informally recommends this:

http://www51.honeywell.com/aero/Products-Services/Avionics-Electronics/Egpws-Home3/GeneralInformation.html

EGPWS Recommendations
Update to the latest Terrain Database at least twice a year. Updates can be downloaded from the Database Page of the EGPWS web site.

 

So, how about twice a year?

here is the schedule of database release dates.

http://www51.honeywell.com/aero/common/documents/egpws-documents/Maintenance-documents/SIL-documents/MKV-VII-documents/SIL_MKV_MKVII.pdf

here are the kown issues;

 

http://www51.honeywell.com/aero/Products-Services/Avionics-Electronics/Egpws-Home3/raas4/raas_certifications.html?c=21

bottom of the page “RAAS Known Issues”

 

Click Here to download database:

htthttps://www.honeywellaes.com/redirection?Operation=1&heading=Business&subheading=egpws

 

same password as NZ2000 data base. call 800-247-0230 to get to account access

Must be OMNI Drive LF for linear format.

Only good for MK5 and MK7

If you have a 6 or 8or 22, you must also have smart cable.

SIL468

AES website

 

For realtime troubleshooting, Here is the Winviews text:

11 APPENDIX A: WINVIEWS

WinVIEWS (Windows Virtual Interface to the Enhanced Warning System) is a software tool developed by Honeywell
to monitor or view values within the EGPWC, and perform certain test interface functions.
Overview: The WinVIEWS software provides a monitor function that does not alter the operation of the EGPWS.
The monitoring of the values assists in the testing of the EGPWS by allowing the operator to quickly determine if the
correct signal and scaling is being used by the EGPWS. Additionally, WinVIEWS provides a detailed status of the
software configuration and input signals, which enables quick identification of system anomalies. WinVIEWS is also
utilized for programming the Configuration Module in MK VI, MK VIII, and MKXXII applications.
To obtain a copy of the WinVIEWS software, please visit www.egpws.com, select the Installation Information page,
then select the Diagrams, Drawings & Software sub-page. WinVIEWS is available as a self extracting .zip file. A
User’s Guide is available there as well.
In addition to the WinVIEWS software, a command file may be utilized. The command file is a simple text file that
includes each Current Value Table (CVT) Item used in a test procedure. The file must be ‘text only’ such as those
created in the Microsoft Windows NotePad program. It should have a filename extension of .wvc or .cmd. The
webpage mentioned above also contains generic command files for use in ground and flight testing the various
EGPWS models.
To use WinVIEWS a RS-232 cable (PN 704-2670-001 is required) to connect the PC 9-pin comm port to the
EGPWC 15-pin test port.
Typical WinVIEWS operation with the EGPWC:
1. Connect the PC to the EGPWC via the RS-232 cable defined above.
2. On the PC, start the WinVIEWS program (requires Windows 95 or later).
3. WinVIEWS opens in the Terminal Mode. Various commands are available in this mode. Type “HELP” or “?” for
command help. In particular, CVT Items may be added or deleted to/from the display to assist with system
analysis.
4. Under the File Menu select the “Load Command File” option and load the appropriate Command File.
5. Use F6 to select the Display Mode: each CVT item listed in the Command File will be continuously updated at a
rate of at least once per second. The value shown for each CVT Item listed is the current value used by the
EGPWS. F6 toggles between the Display and Terminal Modes.

 

___________________________________________________

here is a typical interface

275-087-M1134 Ground Promity Warning System

How do I make peace with the internet service in F900EX s/n 028, VQ-BYT

switch off the laptop wireless connection.. switch near handle.
 
If the Satcom is turned off, there is no DHCP server,,,, so:
 
set the troubleshooting computer to:  Static IP 192.168.1.100surf to 192.168.1.1
 
Hard-wire Ethernet connection to the RJ45 in the Pedestal.
 

WRT54GL Log In

User: Admin
Password: *aircell1*
And yes those are asterisks or stars included in the password
 
Tread Carefully.
 
The Satcom is a Thrane&Thrane SwiftBroadband
 
Aircell Aviator 300 , tt5040A SBU
Aircell CTR