Dry Guy wrote: ↑Wed Aug 13, 2025 7:25 pm
Yes, we call the knobs "fuel control switches". I believe the metal side guards were in place since the prototype 767. The guards they added later I believe are the plastic covers over the EEC switches that used to be below the fuel control switches like in the photo above.
I believe you are correct about the metal side guards. Below are exerpts from the two ADs issued to deal with this issue. It appears that the fuel control switch guards installed on in the first AD were then removed once the EEC switches were relocated away from beside the cutoff switches.
FAA AD T87-13-51
This AD requires the installation of a guard device between the two engine fuel control switches to preclude inadvertent simultaneous shutdown of both engines. This action is prompted by a recent incident that occurred when the flight crew inadvertently shut off the fuel control switches to each engine while intending to operate the electronic engine control (EEC) switches.
SUPPLEMENTARY INFORMATION: On July 1, 1987, the FAA issued telegraphic AD T87-13-51, applicable to Boeing Model 767 series airplanes and Model 757 series airplanes equipped with Rolls Royce RB211 series engines, which requires the installation of a guard device between the two engine fuel control switches to inhibit simultaneous activation of the fuel control switches. This action was prompted by an incident that occurred on June 30, 1987, where a Boeing Model 767, on climb out, had a cockpit message indicating a failure of the electronic engine control (EEC) on one engine. The flight manual procedure for such a failure message is to retard both thrust levers to a mid-position and place both EEC switches to the "OFF" position. In following this procedure, the crew inadvertently shut off the fuel control switches to both engines instead of the EEC switches, which are located in the same vicinity on the control panel. The airplane was at approximately 1,600 feet at the time of the shutdown and engine restart was initiated immediately. Both engines were recovered at approximately 500 feet altitude.
FAA AD 88-07-02
To minimize the potential for inadvertent engine shutdown when using the electronic engine control (EEC) or engine limiter control (ELC) switches, accomplish the following:
A . Relocate the electronic engine control switches or engine limiter control switches, as applicable, from the control stand to the overhead panel in a manner approved by the Manager, Seattle Aircraft Certification Office, FAA, Northwest Mountain Region.
B. The fuel control switch guard installation made in compliance with AD T87-13-51, Amendment 39-5718, may be removed following accomplishment of paragraph A., above.
AD T87-13-51 can be read here: Page 11 of this pdf
https://tile.loc.gov/storage-services/s ... 052174.pdf
AD 88-07-02 is available through the normal search engine:
https://drs.faa.gov/browse/ADFRAWD/doctypeDetails