737600.txt for the cdu [Archive]

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Tom Stian Bjerk

02-12-2007, 10:42 PM

Hi..

Anyone have a 737600.txt file for the cdu that is working good with the
737600pmdg airfileconfig?

Best Regards
Tom Stian Bjerk

Ray Proudfoot

02-13-2007, 07:15 PM

Hi..

Anyone have a 737600.txt file for the cdu that is working good with the
737600pmdg airfileconfig?

Best Regards
Tom Stian Bjerk

Hi Tom,

I've tried and failed to upload a TXT file. So, paste the text below into Notepad and save the file with the name B736-7B22.txt in the Types folder.

;Configuration file for Project Magenta Software
;Created by Steve Reyling - sreyl19368@aol.com
;Updated 25 April, 2006
;
;737-600 IGW with CFM56-7B22 Engines
TOGAPitch=13
N1ref = 90.3
NetWeight= 80200 ;update from aircraft.cfg file
Payload = 21200 ;get values from aircraft.cfg file
Fuelmax = 46063
FFFactor= 1
FuelFactor=1
FFMax= 11
AircraftType = B737-600
Engines=CFM56-7B22
EnginesRate=22.7k
N1Init=4.3
N1Stable=20
N2Stable=59
N1StartupDelay=23
N2StartupDelay=55
radioalt=8
TrimScaleMax=17
TrimScaleMin=-8
;highest speed for gear extraction
vle=270
mle=.84
flppos=0
flpset=0
vmin=vref40+50
vret=0
vext=vref40+70
vmax=340
flppos=1
flpset=1
vmin=vref40+70
vret=vref40+50
vext=vref40+50
vmax=250
flppos=2
flpset=2
vmin=vref40+30
vret=vref40+50
vext=vref40+50
vmax=250
flppos=5
flpset=5
vmin=vref40+20
vret=vref40+30
vext=vref40+30
vmax=250
flppos=10
flpset=10
vmin=vref40+20
vret=vref40+30
vext=vref40+30
vmax=210
flppos=15
flpset=15
vmin=vref40+10
vret=vref40+20
vext=vref40+20
vmax=195
flppos=25
flpset=25
vmin=vref40
vret=vref40+10
vext=vref40+10
vmax=170
flppos=30
flpset=30
vmin=120
vret=0
vext=0
vmax=165
flppos=40
flpset=40
vmin=120
vret=0
vext=0
vmax=156
vss=0
80000 129
85000 133
90000 137
95000 141
100000 144
105000 149
110000 152
115000 154
120000 157
125000 161
130000 165
135000 168
140000 172
145000 174
150000 177
155000 179
160000 182
165000 184
170000 187
vssend
vss=30
80000 89
85000 92
90000 95
95000 97
100000 100
105000 103
110000 105
115000 107
120000 110
125000 112
130000 114
135000 116
140000 118
145000 120
150000 122
155000 124
160000 126
165000 128
170000 130
vssend
vss=1
vss30 1.39
vssend
vss=2
vss30 1.32
vssend
vss=5
vss30 1.26
vssend
vss=10
vss30 1.19
vssend
vss=15
vss30 1.11
vssend
vss=25
vss30 1.07
vssend
vss=40
vss30 0.985
vssend
;v1,vr,v2 for flaps 1
vr=1
88200 89 99 112
97000 95 105 117
106000 102 111 122
114600 108 117 127
123500 114 123 132
132300 120 128 136
141000 125 134 141
150000 130 138 145
158700 136 143 149
vrend
;v1,vr,v2 for flaps 5
vr=5
88200 85 95 109
97000 92 102 115
106000 98 108 120
114600 104 114 125
123500 110 119 128
132300 116 125 134
141000 121 130 138
150000 126 143 142
158700 132 139 146
vrend
;v1,vr,v2 for flaps 15
vr=15
88200 82 91 104
97000 88 96 108
106000 94 102 113
114600 100 107 117
123500 105 112 121
132300 111 117 125
141000 117 122 129
150000 123 126 132
158700 129 129 135
vrend
;vref for flaps 15
vref=15
80000 109
90000 115
100000 121
110000 127
120000 133
130000 139
140000 145
150000 150
160000 155
170000 159
vrefend
;vref for flaps 30
vref=30
80000 105
90000 111
100000 117
110000 123
120000 129
130000 134
140000 140
150000 144
160000 149
170000 153
vrefend
;vref for flaps 40
vref=40
80000 102
90000 108
100000 114
110000 120
120000 126
130000 132
140000 137
150000 142
160000 147
170000 151
vrefend
n1totable
C 0 1000 2000 3000 4000 5000 6000 7000 8000 9000
60 88.7 88.8 88.9 89.1 89.2 89.1 89.1 88.6 88.3 88.7
54 89.6 89.8 89.9 90.0 90.1 90.1 90.1 89.6 89.1 89.0
49 90.5 90.7 90.8 90.9 91.0 91.0 91.0 90.6 90.1 90.0
43 91.5 91.6 91.7 91.8 91.9 91.9 91.9 91.5 91.1 91.0
38 92.5 92.6 92.7 92.7 92.8 92.8 92.7 92.4 92.1 92.0
32 93.5 93.6 93.7 93.7 93.8 93.7 93.7 93.4 93.0 92.9
27 93.3 94.0 94.4 94.5 94.6 94.6 94.4 94.1 93.8 93.8
21 92.5 93.1 93.8 94.5 95.2 95.4 95.4 95.1 94.7 94.5
16 91.6 92.3 92.9 93.6 94.3 94.9 95.4 96.0 95.9 95.7
10 90.8 91.4 92.1 92.8 93.5 94.0 94.5 95.1 95.7 96.4
4 89.9 90.6 91.2 91.9 92.6 93.1 93.7 94.2 94.8 95.5
-1 89.1 89.7 90.3 91.0 91.7 92.2 92.8 93.4 93.9 94.6
-7 88.2 88.8 89.4 90.1 90.8 91.3 91.9 92.5 93.0 93.7
-12 87.3 87.9 88.5 89.2 89.9 90.4 90.9 91.5 92.1 92.8
-18 86.4 87.0 87.6 88.3 89.0 89.5 90.0 90.6 91.2 91.9
-23 85.5 86.1 86.7 87.4 88.0 88.6 89.1 89.7 90.3 91.0
-29 84.6 85.2 85.8 86.4 87.1 87.6 88.2 88.8 89.3 90.1
-34 83.6 84.2 84.8 85.5 86.2 86.7 87.2 87.8 88.4 89.1
-40 82.7 83.3 83.9 84.5 85.2 85.7 86.2 86.8 87.4 88.2
-46 81.7 82.3 82.9 83.6 84.2 84.7 85.2 85.9 86.5 87.2
end
n1clbtable
C 0 5000 10000 15000 20000 25000 30000 35000 37000 41000
60 88.4 88.6 88.5 88.2 88.9 91.3 92.9 94.3 94.4 92.7
55 89.4 89.3 89.1 89.3 90.6 92.3 93.6 93.7 92.0 89.2
50 90.0 90.1 90.1 89.9 90.2 90.7 91.6 92.9 93.0 91.3
45 90.7 90.8 90.9 90.7 91.1 91.6 91.6 92.2 92.3 90.6
40 91.5 91.6 91.6 91.4 92.0 92.4 92.4 91.5 91.6 89.9
35 92.3 92.3 92.2 92.8 93.2 93.2 92.3 91.6 90.0 92.0
30 91.3 93.0 93.0 92.9 93.5 94.0 93.9 93.1 92.5 91.0
25 90.5 93.0 93.8 93.5 94.3 94.8 94.6 93.9 93.3 92.0
20 89.8 92.3 94.5 94.3 95.1 95.5 95.3 94.6 94.1 92.9
15 89.1 91.5 93.9 95.1 95.8 96.2 96.0 95.4 94.9 93.9
10 88.3 90.8 93.1 95.3 96.7 96.9 96.6 96.1 95.7 94.8
5 87.5 90.0 92.4 94.5 97.7 97.8 97.3 96.9 96.5 95.7
0 86.8 89.2 91.6 93.7 97.1 98.9 98.3 97.8 97.4 96.6
-5 86.0 88.4 90.8 92.9 96.3 98.8 99.3 98.5 98.2 97.7
-10 85.2 87.6 89.9 92.1 95.5 98.0 99.6 99.4 99.1 98.6
-15 84.4 85.8 89.1 91.2 94.7 97.3 98.8 100.4 100.1 99.6
-20 83.5 86.0 88.3 90.4 93.9 96.5 98.0 100.1 100.6 100.2
-25 82.8 85.2 87.5 89.6 93.1 95.7 97.2 99.2 99.8 99.4
-30 82.0 84.3 86.6 88.7 92.3 94.9 95.4 98.4 98.9 98.6
-35 81.2 83.5 85.8 87.9 91.4 94.0 95.5 97.6 98.1 97.7
-40 80.4 82.6 84.9 87.0 90.6 93.2 94.7 96.7 97.2 96.9
end
; Climb 1 is 3% reduction in %N1 to 10,000 feet, increasing to full climb at 15,000 feet.
CLB1-reduction
3, 10000, 15000
; Climb 2 is 6% reduction in N1 to 5,000 feet, increasing to full climb at 15,000 feet.
CLB2-reduction
6, 5000, 15000
; cost index is truly based on weight, altitude, and wind.
; Values below are based on 737-700 - 140,000 lbs, 37,000 feet, and no wind.
costindex
0 284/.758 284/.758 250/.737 3.0
30 298/.782 298/.782 273/.777 3.1
100 315/.798 315/.797 315/.785 3.1
200 315/.801 315/.798 315/.785 3.2
500 315/.803 315/.803 315/.785 3.2
end
costindexinterpolated = on
ASPD1=ARM
CSPD1=1
ASPD2=N1
ASPD3=MCP SPD
ASPD4=RETARD
ASPD5=THR HLD
ASPD6=GA
ASPD7=FMC SPD
ASPD9=FMC SPD
AHDG1=HDG SEL
AHDG2=VOR/LOC
CHDG2=1
AHDG3=VOR/LOC
AHDG4=VOR/LOC
AHDG5=VOR/LOC
CHDG5=1
AHDG8=LNAV
AALT1=G/S
AALT2=ALT HOLD
AALT3=MCP SPD
AALT4=V/S
AALT5=ALT ACQ
AALT6=G/S
CALT6=1
AALT7=TO/GA
AALT8=TO/GA
AALT9=VNAV SPD
AALT10=VNAV PTH
AALT11=ALT HOLD
ACMD1=CMD
ACMD2=FD
ACMD3=CMD
ACMD4=CMD
ACMD5=NO AUTOLAND

ekezz

02-14-2007, 07:25 PM

Saved the file as instructed.
Added TXT extension to allowed upload file types
Uploaded the file to the Project Magenta section in the Download Library

Ray Proudfoot

02-15-2007, 11:48 AM

Saved the file as instructed.
Added TXT extension to allowed upload file types
Uploaded the file to the Project Magenta section in the Download Library

I'm sorry but I don't understand. Are those instructions?

I press the Browse button and locate the file I want to upload. I then press Upload and I would expect the upload to be successful. But, I just get the message "Upload of the file failed" without any explanation of what is wrong. The filesize is well within the limit.

I've tried it using both IE and Firefox but I can't get any type of file - jpg, zip, txt to upload.

ekezz

02-15-2007, 01:52 PM

Ray Proudfoot

02-15-2007, 03:20 PM

Hi Ray,
These are not instructions, this is a short log of what I did, in telex style, maybe too much shorthand writing.

The TXT file extension was not in the allowed upload list so I had to add it (this addition requires one being an administrator)

If an upload fails, please check the entire page for RED text, there should be a reason mentioned in red somewhere.

Thanks Kester. I'll try uploading a txt file now and check for any red warning text.

Later... The upload of a txt file is still failing. No red text is visible. The message at the top of the 'Manage Attachments' window states 'B736-7B22.txt:
Upload of file failed.'

I'm probably doing something extremely silly but for the life of me I can't work out what it is. I'm trying to upload a file from my own computer.
Help! :sad:

PaRa

02-23-2007, 02:52 AM

Hi Ray its possible that your windows settings are playing a part in this (and masking the true file extension of your files).

Check is in your windows folder options (see attached images).

1) Open "My Computer"
2) Click on "Tools" from the top menu
3) Click on "Folder Options ..." (the Folder Options window will appear)
4) Click on the "View" tab
5) Scoll down to the option that says "hide extensions of known filetypes" and make sure this is not ticked.

The result of this will is that "sometextfile" will now appear as "sometextfile.txt" within Windows explorer.

Having this option off will also let you change the file-extension.

Eg : "somefile.abc" can be renamed to "somefile.txt" and therefore able to be uploaded to the forum.

Not sure if this is your problem however :(

EDIT : Also triple check that their are no spaces in the filename, an after thought

Ray Proudfoot

02-23-2007, 01:24 PM

Hi PaRa,

Thanks for suggesting those solutions. I already have file extensions showing and the filename had no spaces in it.

Very frustrating :-)

ekezz

02-23-2007, 05:11 PM

Hmmm, frustrating indeed.

the problem is that I cannot see what you are going through.
I have tried it with a non-admin userid and it worked fine.

without any error message it's looking for the needle in the haystack.

maybe you can email me the file you are trying to upload
send a mail to kester at mycockpit.org
(replace at with @)

Ray Proudfoot

02-23-2007, 08:29 PM

Hi Kester,

Thanks for your help. I'm mailing you the file now. I'm also attempting to attach it to this message. Let's see... Well, well, well. It's working now. I swear I did nothing different to all my previous attempts. This one is zipped but I'd tried that too without success.

No need for the private message now. I wonder what changed? :?