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Special conditions · electric or hybrid design · aircraft

Special Conditions: Learjet Inc., Model LJ-200-1A10 Airplane; Crashworthiness, Emergency Landing Conditions

Special conditions are rules the FAA writes for one design when the standard certification rules do not cover something new about it. These were published February 6, 2014 for Learjet. System: electric propulsion.

What it applies to

Applicant
Learjet
Makes
Learjet
Models
—
Published
February 6, 2014
Effective
March 9, 2014
The FAA's document
On the FAA's site

The FAA's summary their words, unchanged

These special conditions are issued for the Learjet Inc. Model LJ-200-1A10 airplane. This airplane will have a novel or unusual design feature when compared to the state of technology envisioned in the airworthiness standards for transport category airplanes. This feature is a hybrid construction that uses both composite and metallic materials in the structure for which the crashworthiness responses for occupant safety may not be equivalent to current all-metallic airplanes. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for this design feature. These special conditions contain the additional safety standards that the Administrator considers necessary to establish a level of safety equivalent to that established by the existing airworthiness standards.

Source: FAA special conditions (final) from the Dynamic Regulatory System; the Federal Register carries the same notices.