Category Archives: AircraftTroubleshooting
F50 ops tests for 4A check
Ruler
Tape
Soap
Targets
Protractor
SQUAWKS
Pressure bump on takeoff. Verified on ground.
Flap assym left side has 1.7 inches displacement. Vrrified.
Crew temp needle stuck cold. Verified.
Elt fails selftest. Short chirp after 16 seconds.
Large screws at pilot overhead stripped. Heads are too large. Overlay is becomi b get damaged
Pedistal. Brush.clean
Yokes. Black touch up.
Lower eied screen
Cb panel cover. Clean
On ann panel…. fire test label is missing
Center qty reads slightly low. R fuel reads slightly high
How do I find fuel leaks in a mooney?
Put plexiglass on panels
Apply vacuum to inside.
Mirrors inside.
Soap the outside of the wing
See the bubbles inside the wing
Beech jet 400 cockpit notes
Controller screen
Where can I buy reasonable priced deec download cable
turbsocal@gmail.com
Hi todd, yes i do, my cell is 760-219-7878 give me a buzz. mike
Tutorial
https://www.youtube.com/watch?v=6EZMvNxmIUs5
Iogear. USB serial adapter
What would cause the slats to bang in and out on Stall 2 on a F900EX?
Missing ground in the latch circuit of the R3cm slat control relay. This was a misswire from the Duncan installation of Aviation Partners winglets.
Original WDM
Sh0p notes
Aviation Partners wire mods
F90-0095S01REV-DVR–Slat Control Wiring Modification (1)
Aviation Partners Final disposition for F900ex 028
slat diagram large
How do the carbon brakes age on a F900?
(these numbers were from Spring 2014 on bmb)
Warn Pack = 3.621
Shim = approx .45
Pin = .354 below
Total pack is 4.92
Total wear before Shim is 1 inch.
Shim adds .45
Total life is 1.45
2000 landings
.000725 inch per landing.
29 dollars per landings per brake.
try this for the whole document
https://docs.google.com/spreadsheets/d/1uTJgjMsK7voB2dsyOmcUYxOQYy3BF0OQkD1glkY3DD4/pubhtml
This was from June 13, 2014, prior to the installation of shim in 1 and 4, and a new brake on 2
How do I call VQ-BZZ aircell?
All calls to Iridium phones are international calls.
If your phone allows international calls:
dial the Country code of the country you are calling from
from the USA: 011 88162345lastfour for the Cockpit.
from the USA: 011 88162345lastfour for the Cabin.
–OR– two stage dialing if that does not work
From inside USA/Canada 1.480.768.2500 &WaitPromt 88162345lastfour
From outside USA/Canada 1.011.480.768.2500 &WaitPromt 88162345lastfour
AircellAxxesIIQuickCallingGuide042010
remember to use AIRINC 429 label Label 204 for Baro Corrected altitude
CHECK SLIDE 417 for Dial Prefixes.
How do I comply the Honeywell ADC AD on a Falcon 900
Here is now I would do it:
AD not applicable by reason of part number of installed equipment.
here’s why: EASA AD US-2012-26-15-1 effectivity cites Honeywell Service Bulletin ADM/ADC/ADAHRS–34–A01.
Honeywell Service Bulletin ADM/ADC/ADAHRS–34–A01, page 5,1.A. Effectivity…. details the applicable part number of the affected equipment.
The currently installed Air Data Computers: 7000700-647 do not appear on that table.