| grlowe@avfab.com,
|
We are looking for a Cable P/N MC6424-00. It is the lateral track release cable from a Model 5000 seat installed in a Falcon 900 EX.
| grlowe@avfab.com,
|
We are looking for a Cable P/N MC6424-00. It is the lateral track release cable from a Model 5000 seat installed in a Falcon 900 EX.
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9. June 6 2004. 0 to 5.00 memorial day motor cycles. 5.30 Mom with water hose. 9.00 lucia scooter 10.00 Joe lands in j4. June 12 13.26 Lucia rides bike. 21.00 luci shoot footage. 23.30 Florida. 2004. 27.00 grandma. 36.00 lucia skate. with Sam and Kinsey. 49.00 twister 107.00 end.
Here is the raw picture of the overhead;
Here is the outside dimensions
Here is the .PDF on a 20×20 sheet. Print it on heavy paper.
possibly could be laminated to make it more durable.
f900exoverheadpapertemplate f900exoverheadrev3 .pdf
Then razor blade all the cutouts
1. Hyd. pressure gage 2 inop. – Number 2 hyd gage dead below the zero peg until it warms up. PN 5502-360-80-10 SN 764, then it started working half way through our troubleshooting. rang wires.
Number 1 gage will not go to 2100 lbs with the AUX pump, hangs at 1600 lbs until you tap it. video. PN5502-360-80-10 SN 765
2. Number 1 engine ignition – L3KK left ignition switch. 820UN01S1BAOA. IPC 31-11-30-21 . SO number 403787. 1 gage only. ref.
3. Printer cockpit jammed – fixed paper jam
4. Look in radome – visual inspection good
5. Landing LED taxi – provide quote
6. ANTISKID Menelco. – Suspect moisture in nose axle.
7 . Overhead panels loose – resecured
8. Face on entry away light – Reinstalled face.
9. Light check , logo lights – LOGO lights not installed on this AC.
10. reevaluate possibility of repair for overhead panel. – paper overlay, month long repair removal.
11. change router password
.375 is pin
Old go/ no go was :
.370
.378
SB 101 from ALCON
Now company is called redling .
recommended not to use the old .378 tester. it opens the springs too far.
Instead, use a shoulder from a 3/8 inch bolt. Any tighter than slip fit is good.
Complaint: Cabin cold in flight in auto mode:
EDIT squawk turned out to be : cabin cold in AUTO and in MANUAL.
I failed to realise early on that the cabin valve backing away from hot was normal operation. Also, when crew is max hot, the cabin backs down even lower. This also seems to be normal operation.
Observation: Pass Valve position needle will drive full hot, then immediately back down to half scale or lower. In the air and on the ground with APU.
EDIT 20/20 hindsight, this is normal operation. Also, it is exaggerated when the crew valve is toward hot. Who knew?
At about :40 seconds the valve runs cold on its own.
Reference:
F50 Pass temp electrical: f50passtempcontrol
Associated:
With the flood duct open, the problem is reduced.
EDIT: with the flood duct open, the cabin will quickly overheat.
With CABIN and CREW valves selected OFF, the problem goes away.
With a SEPARATE temp sensor plugged into 163H, hanging in free air, THE PROBLEM GOES AWAY. THIS is the ONLY way we have affected the squawk.
Troubleshooting so far:
We have shorted 162H AMP pin A and B together. This takes the temp select system out of the system and commands full hot. Squawk remains the same.
Crew Bleed or Pass bleed or both yield the same result. Squawk remains the same.
AMP to 163H wires rung out carefully. M, H, J.
AMPs swapped cabin and crew. Squawk remains the same.
162H Temp select controllers swapped for a loaner unit, Squawk remains the same.
Back-pinned v to assure it had a solid ground during operation.
With amp unplugged, Ohm meter on M, H, and J Both halves of the sensor read ~89 ohms at max cold, ~124 ohms at max hot.
Unrelated?
pulled 5 temp switches for a unrelated bleed oheat light when wing heat switched off, turned out to be a sticking PRV
Unrelated?
Removed failed seals at upper and lower turbo cooler Best-O-Bell inlet pipes. Installed 4 each new seals.
PARTS OFF: P/N 460-150 S/N NA.
PARTS ON: P/N 460-150 REV P LOT# 0110336483.
Performed leak check.
Quoted text from John Taylor:
- Leading Particulars.
Type of Control …………………………………………………………………………………………………….. Pulse modulated
Temperature Selector Range ……………………………………………………………. 60°F to 90°F (15.4°C to 31.9°C)
Input Voltage ……………………………………………………………………………………………………………… 18 to 32 VDC
Maximum Output …………………………………………………………………………………………………. 2 amps at 28 VDC
Ambient Temperature Range ………………………………………………………………-65°F to 165°F (-54°C to 72°C)
Deadband ………………………………………………………………………………………………………………….. 3.0°F (1.7°C)
Transient Voltage Protection …………………………………………………………………………………. + 80 volt, -600 volt
Reverse Voltage Protection ………………………………………………………………………………………………………. Yes
Output Protection …………………………………………………………………………………………………………………….. Yes
Hi-Limit Protection ………………………………………………………………………………………………………. 160°F (70°C)
Cabin Sensor …………………………………. Negative Temperature Coefficient Disc Thermistor ( See Figure 1 )
Temperature Readout Sensor ……………………………….. Wire wound positive temperature coefficient 0.2°/F
Construction …………………………………………………………………………………………………………. Repairable Assy.
Connector Type …………………………………………………………………………………… Mates with MS3120A-14-195
Size
Length (max) ……………………………………………………………………………………… 8.400 inches (213.36 mm)
Width (max) ………………………………………………………………………………………….. 3.900 inches (99.06 mm)
Height (max) …………………………………………………………………………………………. 3.225 inches (81.91 mm)
Weight (approx.) ……………………………………………………………………………………….. 18 ounces (510.3 gm)
Temp Amplifier simplified block diagram:
Pixma
225pgbk black
226 color
7TS0
Here is a zip with the originating documents for FARA.
They were part of the now deprecated www.7ts0.com
FARADocs FromFairviewAirportdotcom
I found this minutes on the old interwebs, not assured to be approved
Here is a 2011, Source unknown
Here are the scans of the the minutes as filed in the Secretaries Box, “Meetings” folder. Enjoy.