Falcon 50 Nose Landing Gear Box Beam Fasteners
A quick torque check of these fasteners can be done in 10 minutes from the outside of the aircraft and is a good indicator of the integrity of this high stressed area.
Read More...
A quick torque check of these fasteners can be done in 10 minutes from the outside of the aircraft and is a good indicator of the integrity of this high stressed area.
Read More...
On the Falcon 50, 900 and 2000 model aircraft, task code 30-20-00-710-801 has you do any operational test of the engine inlet anti-icing system. Extreme caution is warranted to prevent an overheat condition and possible structural damage.
Read More...
Dassault has new “A” check requirement: task 28-00-00-280-801, on the detection of microbiological contamination that provides a new and faster method for fuel sampling.
Read More...
The upper top skins of the pylons are prone to ramp standing water and is a "hot spot" for corrosion.
Read More...
Seeing spots on the forward radome EVS glass? There's no cause for concern. It's normal.
Read More...
Don’t get left with your NLG door open. Inspect brackets for corrosion and cracks.
Read More...
Is it normal for outboard slats not to retract fully after winglet installation on a Falcon 900? Keep reading for the answer.
Read More...
Don’t overlook inspecting the phenolic bushing in the top mount of the APU exhaust. It is commonly broken or missing.
Read More...
Although Service Bulletin SBF2-12-001 is not mandatory, API strongly recommends compliance during the next maintenance event in which the ailerons are removed from the aircraft.
Read More...
If the static port on your Falcon 50B/EX has an added shim, extra caution is needed during removal as not to cause damage.
Read More...
Dassault has a Special Commercial Program for FSA900EX-54-10-02-R5 that extends the warranty and provides a discount for parts.
Read More...
Dassault requires that after discharge of a fire bottle, whether by accident or intention, the rubber silicone nipple must be replaced.
Read More...
Because of the high probability of future corrosion around the fasteners of the front center panel ahead of frame 10, Duncan Aviation strongly recommends to comply with SB 392.
Read More...
The wiring harnesses for nose wheel anti-skid transducers are known to break down internally which can cause intermittent anti-skid issues.
Read More...
Engine cracks have been found as small as a couple of millimeters to as long as six inches.
Read More...