1994 crash flight 427 737-300, mid air deployment of one rev thruster at 6000 feet
also found this...
The logic of thrust-reverser deployment, taken from the Boeing 737 Operations
Manual, revision 001.1, April 1988, p 21.20.08, is that the Boeing 737 can
deploy the thrust reverser on either engine if ...
EITHER: spin-up is detected on any two main gear wheels,
OR: at least one of Captain's and First Officer's Low Range Radio Altimeters reads below 10ft,
OR: right main gear strut is compressed,
Last edited by FlightPathOBN; 22nd Feb 2013 at 14:43.