Wires, pressure bung, wire protection

 

Falcon wire standards

 

 

 

 

 

 

Pilot squawk:

 

Pilot verbal:  runs extend .45 seconds, then lockup. Then bypass will not work.

 

Initial run:

slat conditioned .21 split midrun

Slat Retract left raw -11.33, conditioned = 10.01

Slat Retract right raw -11.27, conditioned = 9.91

Slat extend left raw

 

flap  conditioned. 179 v split mid travel.

 

 

 

 

 

 

 

El Cayo.

 

 

 

 

Weller

spare tips

Lunch box

2 solder

2 wick   gootwick has good review

Solder sucker

Rosin

solder wicking technique

 

 

 

 

for connector

D38999/20FH55PN

could be txb4-s-13n

https://www.alvatek.com/txb4-s-13n/#

 

 

selector

https://www.milnec.com/mil-d38999-connectors/d38999-connector-catalog.pdf

requested milnic quote

 

https://www.milnec.com/quote-request/?sub=1

 

 

Largest hole to remove outer

 

 

Bare Shield

 

 

Bunch the shield

 

Cut the side off the bunch

 

Clean up a small portion of the shield that remains

 

Smooth the small portion

 

Prepare shield ground

 

Untwist it until its flared out.

 

 

carefully wind 1 TURN ONLY.

Clip the rest with flush cut

 

Heat the whole thing until solder FLOWS fully into both braids

 

Smallest applicable heat shrink.

 

 

This is the Great Bob Knuckolls take

http://www.aeroelectric.com/articles/pigtail/pigtail.html

 

 

 

 

 

903 fuel

Falcon 2000 sn 018.

code 903 eqt 050qt

right collect tank probe

 

768343-1 .GAUGE,FUEL
OPT TO 768-343-1
L50QJ
R50QJ
768-343-1 .GAUGE,FUEL
OPT TO 768343-1
L50QJ
R50QJ

 

f2000 better pictorial

F2000 fuel qty

F2000 Fuel test

f2000 ipc

F2000 quick transfer

F2000 wing pictorial

Bleed speed brakes

SpeedBrakes

Notes;

 

 

 

 

 

 

Missing prints from DFJ:

FD-018-WIRING-003 (F2M-191 TO275)

 

FD-018-WIRING-003 (F2M-004 TO 066)

 

 

 

 

 

 

 

Probe S/N 2129 was installed to 5 months