RULES: Damage Tolerance and Fatigue Evaluation of Structure,
Published: 2008-04-11
This action corrects a paragraph reference that appeared in
the final rule, Airworthiness Standards; Airframe Rules Based on
European Joint Aviation Requirements, which the FAA published in the
Federal Register on February 9, 1996. In that final rule, the FAA
inadvertently changed a paragraph reference. The intent of this action
is to correct the
PROPOSED RULES: Embraer S.A., Model EMB-500, Airspeed Indicating System 23.1323(e),
Published: 2008-01-28
This action proposes special conditions for the Embraer Model
EMB500 airplane. This airplane will have a novel or unusual design
feature(s) associated with airspeed system. The applicable
airworthiness regulations do not contain adequate or appropriate safety
standards for this design feature. These proposed special conditions
contain the
PROPOSED RULES: Embraer S.A.; Model EMB-500; Brakes-Designation of Applicable Regulations,
Published: 2008-01-23
This notice proposes special conditions for the Embraer S.A.;
Model EMB500 airplane. This airplane has a novel or unusual design
feature associated with the braking system. The applicable
airworthiness regulations do not contain adequate or appropriate safety
standards for this design feature. These proposed special conditions
contain the
PROPOSED RULES: Embraer S.A.; Model EMB-500; Static Pressure System,
Published: 2008-01-23
This notice proposes special conditions for the Embraer S.A.;
Model EMB500 airplane. This airplane has a novel or unusual design
feature associated with the static pressure system. The applicable
airworthiness regulations do not contain adequate or appropriate safety
standards for this design feature. These proposed special conditions
contain the
PROPOSED RULES: Embraer S.A., Model EMB-500; High Fuel Temperature,
Published: 2008-01-23
This notice proposes special conditions for the Embraer S.A.,
Model EMB500 airplane. This airplane will have a novel or unusual
design feature(s) associated with high fuel temperature. The applicable
airworthiness regulations do not contain adequate or appropriate safety
standards for this design feature. These proposed special conditions
contain
RULES: Embraer S.A., Model EMB–500; Fire Extinguishing for Aft Fuselage Mounted Engines,
Published: 2008-01-18
These special conditions are issued for the Embraer Model EMB-
500 airplane. This airplane will have a novel or unusual design
feature(s) associated with aft mounted engine fire protection. The
applicable airworthiness regulations do not contain adequate or
appropriate safety standards for this design feature. These special
conditions contain the
RULES: Special Conditions—; Adam Aircraft Industries Model A700; External Fuel Tank Protection During Gear-Up or Emergency Landing,
Published: 2008-01-03
These special conditions are issued for the Adam Aircraft
Industries Model A700 airplane. This airplane will have a novel or
unusual design feature(s) associated with an External Centerline Fuel
Tank (ECFT) that increases the total capacity of fuel by 184 gallons.
The tank is located below the fuselage pressure shell immediately below
the wing.
RULES: Special Conditions—; AmSafe Aviation; Inflatable Restraints Installation; Approved Model List of Normal and Utility Category Airplanes, etc.,
Published: 2008-01-02
These special conditions are issued for AmSafe Aviation for a
list of approved models. These airplanes, as modified by AmSafe
Aviation, will have novel and unusual design features associated with
the lap belt or shoulder harness portion of the safety belt, which
contains an integrated airbag device. The applicable airworthiness
regulations do not
RULES: Embraer S.A. EMB-500; Protection of Systems for High Intensity Radiated Fields (HIRF),
Published: 2008-04-25
These special conditions are issued to Embraer S.A., for a
type certificate for the EMB500 airplane. This airplane will have
novel and unusual design features when compared to the state of
technology envisaged in the applicable airworthiness standards. These
novel and unusual design features include the installation of
electronic flight instrument