About 1 psi at 200 KTS
knots
airspeed
http://www.cactus2000.de/uk/unit/masswsp.shtml
About 1 psi at 200 KTS
knots
airspeed
http://www.cactus2000.de/uk/unit/masswsp.shtml
http://www.s-techent.com/ATA100.htm#[80]
Here is the
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Avionics related ATA’s
12-00-00 Servicing Routine Maintenance
12-10-00 Replenishing
12-20-00 Scheduled Servicing
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
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
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
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
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
27-00-00 Flight Controls r 30
30-00-00 Ice & Rain Protection
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
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
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
36-00-00 Pneumatic
36-10-10 Distribution
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
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
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
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
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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.
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
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?
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.
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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.
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
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
Notes from a previous mechanic lost in the mist of time
P p
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:
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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;
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.
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here is a typical interface
WRT54GL Log In