Automatic fault reporting system

Communications: electrical – Aircraft alarm or indicating systems

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Details

340963, 73178R, G06F 1520

Patent

active

047885319

ABSTRACT:
An aircraft automatic fault reporting system having a plurality of ARINC 429 low-speed data buses between the aircraft maintenance control panel and the aircraft communications addressing and reporting system provides two-way communication therebetween. Detected faults through an eight-digit fault code are by means of a transient logic circuit under certain conditions of the aircraft communications and addressing systems provided to maintenance personnel thereby eliminating flight crew use of FRM's.

REFERENCES:
patent: 4470116 (1984-09-01), Ratchford
patent: 4510803 (1985-04-01), Perara
patent: 4592055 (1986-05-01), Fischer et al.
patent: 4675675 (1987-07-01), Corwin et al.
Crawforth, "Realtime Flight Test Control", IEEE Transaction on Aerospace and Elect. Sys., vol. AES-2, No. 4 (1966).
Batten, "The Use of Computer Testing", Aircraft Engineering, vol. 47, No. 6 (1975).

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