Downloaded from https://www.everyspec.com MIL-STD-1808B SYSTEM SUB-SYSTEM TITLE DEFINITION 08 50 STATIC STABILITY The system information required to determine the minimum nose wheel reaction necessary to ensure that the aircraft remains stable while being moved, while static during servicing operations, and during jacking operations. Includes tabular and graphical data for the calculation of nose wheel reaction in relation to aircraft mass and residual moment (and wing sweep angles, if appropriate) for both a fully equipped aircraft and for situations where items of equipment or stores have been removed or the fuel state is outside the normal sequence.
Includes safety precautions and limitations for defueling sequences, maximum movement speeds, and movement on gradients or over rough ground. 10