Engine start procedure in a Cessna 172 with G1000 avionics
Aviatech Zone
Friday, 20 February 2015
Engine Priming and Starting Procedures: Models 182T, T182T, 172R, and 172S
This video will serve as a guide to priming and starting the engine on Models 182T, T182T, 172R, and 172S. Applicable to Lycoming-engined single engine aircraft.
Sunday, 25 January 2015
LANDING GEAR - HYDRAULIC LOADING VALVE WIRE BUNDLE INSPECTION - Citation Model 560XL
EFFECTIVITY
MODEL SERIAL NUMBERS
560XL (XLS) - 5501 thru -5830
560XL (XLS+) - 6001 thru -6150, -6152 thru -6160
The equivalent of this service letter has been incorporated on production airplanes -6161 and On.
NOTE: SL560XL-29-04 -Hydraulic Power - Hydraulic Manifold Control Valve Wire Bundle Inspection should be done in conjunction with this service letter.
REASON
To inspect the cannon plug and wire bundle for the hydraulic loading valve on the hydraulic manifold for chafing and install protective sleeving.
DESCRIPTION
This service letter provides instructions to inspect the cannon plug and wire bundle for the hydraulic
loading valve and install protective sleeving.
COMPLIANCE
MANDATORY. This service letter must be accomplished within 300 flight hours or 90 days from the date of receipt, whichever occurs first.
MODEL SERIAL NUMBERS
560XL (XLS) - 5501 thru -5830
560XL (XLS+) - 6001 thru -6150, -6152 thru -6160
The equivalent of this service letter has been incorporated on production airplanes -6161 and On.
NOTE: SL560XL-29-04 -Hydraulic Power - Hydraulic Manifold Control Valve Wire Bundle Inspection should be done in conjunction with this service letter.
REASON
To inspect the cannon plug and wire bundle for the hydraulic loading valve on the hydraulic manifold for chafing and install protective sleeving.
DESCRIPTION
This service letter provides instructions to inspect the cannon plug and wire bundle for the hydraulic
loading valve and install protective sleeving.
COMPLIANCE
MANDATORY. This service letter must be accomplished within 300 flight hours or 90 days from the date of receipt, whichever occurs first.
Using Grinding Compound or Aircraft Friction Drops to Remove Screws
Video: Using Grinding Compound or Aircraft Friction Drops to Remove Screws | ||
ATA: 51-20 | Models: All Models | Published: 11-11-2014 |
Dennis Kelderman, Customer Service Engineer, Team Structures demonstrates how to use a grinding compound or E-Z Grip to remove screws.
|
Location and Types of Standby Power Supplies for the Excel Fleet
Inform customers of the location and types of the standby power supplies based on unit numbers.
Models: 560XL, XLS, XLS+
Monday, 22 December 2014
What are the differences between Airworthiness Directives and Service Bulletins
Airworthiness Directives(AD) are issued when the FAA finds that an unsafe
condition exists in a product (aircraft, aircraft engine, propeller, or
appliance.)
These AD's notify aircraft owners and operators of potential unsafe conditions
and require special inspections, repairs, or alterations to correct the unsafe
condition.
Service Bulletins (SB) are notices to aircraft operators from
a manufacturer notifying them of a product improvement.
Alert service bulletins are issued by the manufacturer when a condition exists
that the manufacturer feels is a safety related item as opposed to just a
product improvement. These SB's usually result in the FAA issuing an AD. The AD
will reference the alert service bulletin as a method of compliance with the
airworthiness directive.
If a service bulletin is not an alert service bulletin or a bulletin referenced
in an AD, it becomes optional and may or may not be incorporated by the
operator.
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