Special Conditions: Lockheed Martin Aerospace Corp. Model L382J Airplane
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 April 8, 1997 for Lockheed Martin. System: instruments and avionics.
What it applies to
- Applicant
- Lockheed Martin
- Makes
- Lockheed Martin
- Models
- —
- Published
- April 8, 1997
- Effective
- May 8, 1997
- The FAA's document
- On the FAA's site
The FAA's summary their words, unchanged
These special conditions are for the Lockheed Martin Aerospace Corp. Model L382J airplane. This airplane will have a novel or unusual design feature(s) associated with the installation of a dual head up display (HUD) to be used as a primary flight display (PFD) for all regimes of normal operation. The HUD will satisfy the basic requirements of Sec. 25.1321 and serve as the primary source of flight director command information. These special conditions contain the additional safety standards which the Administrator considers necessary to establish a level of safety equivalent to that established by the airworthiness standards of Part 25 of the Federal Aviation Regulations (FAR)
Source: FAA special conditions (final) from the Dynamic Regulatory System; the Federal Register carries the same notices.