R console dimmer on N305LM
Dimmer at MED floorboard 1.
Inverter at copilot rh rudder pedal
R console dimmer on N305LM
Dimmer at MED floorboard 1.
Inverter at copilot rh rudder pedal
New to me (2022)
Problem that reduces resistance on fuel probes and wires, resulting in increased ability to make house payments.
I think i have observed this two times.
1 falcon 900ex 2 months following a possible over application of BioBor.
Result was 7 condemned probes in the wings. I could not save any of the 7 probes by slosh/clean/dry/repeat method. Very unusual.
LaserRef II and III, Inertial Navigation Unit, End-Of-Life
DFJ announcement of obsolescence
Honeywell announcement
Operator Information Bulletin
Proline IV Display tubes aging support
After market support
Regional Avionics
Duncan Blurb
Airshow 400, Moving Map Display
Discontinuance
Audio Internation Cabin Management
Obsolete Duncan Blurb
Baker Audio Management obsolete
Falcon 10 YD/Arthor box no longer supported by vendor
There was a little controversy on weighing, here is how it played out:
here is the math
Known:
transponders are installed at the same rack as the existing transponders.
UNKNOWN:
What bulkhead connector was used to route GPS wires to the nose?
Does the owner posses a STC permission document, proving the STC was paid for on this SN aircraft?
Verfy WAAS GPS source is in use as per page 45/371
Where is WAAS GPS module mounted? PN, SN?
Duncan or Memon to do a ADSB ops check.
ADSB FAIL annunciator located beside TCAS head.
Checkout proceedures start around 121/371
Major alteration as per page 128/371
Outine drawing of WAAS gps. 279/371
tRANSPONDER wb IS PAGE 77
control head is Gables G7534 Control Panel
checkout starts at 121
Check on suitability of CB installed on the perifery of Copilot cb panel.
ELA 356/371
Look at configuration page 94 of 371
EQUIPMENT LIST, WEIGHT AND BALANCE UPDATE
MDL:
1. AFMS
2. ELA
3. STC
4. STC PERMISSION LETTER
5. AML
6. ACASS INST. DIAGRAM
7. ADSB INST. DIAGRAM
8. ANTENNA STRUCT. APPROVAL/ INSPECTION RESULTS
9. LOG ENTRY
10. . PREVIOUS ADSB INSTALLATION LOG ENTRY.
27 lbs to close, only when upper trim is installed.
After 30 hours or so the top 5 inches of the seal blows out at ~ 9.3 psi.
Items suggested prior to flight.
Blend nicks in Propeller.
Verify allowable length of Propeller blades.
Lower strut attaches show less than 1 thread exposed outside of the fibrelock.
Clean engine / engine compartment to allow detection of leak.
Inspect nose wheel casting, copilots side inside fairing.
Final inspection of flight controls.
Battery is possibly 6 years old
Items that can be attended later
Corrosion at skin laps under fuselage tailcone.
https://youtube.com/shorts/XQgOaoJfDVo?feature=share
Light corrosion/red rust on engine accessories.