Weird problem…… After the aircraft arrived at gate, the crew was having a difficult time of doing their post-flight shutdown. Among some of the problems noted was that the captain could not turn off the center tank pumps and the Hydraulic Panel was displaying “Select Manual” for controller operation. There were other anomalies visually noted, although with the crew describing the problems, I didn’t get a chance to account for them all.
One thing that “was” absorbed, was a crew comment about the ADI airspeed tape not switching to a ground mode display (I’m assuming all the V-Speeds go dashes). For simplicity sake, the crew just wrote up their most noted fault which was that the Auto-Ground Spoilers did not deploy (they moved the handle manually).
What do we have going on here???? We’ve got an aircraft still stuck in the air mode…… or at least partially.
There were no crew bitches about Thrust Reversers, Anti-Skid, or Auto-Brakes. I noted the outflow valve was open (which “should” go open upon landing).
The first thing any Douglas mechanic is going to try to do is disconnecting the scissors to simulate air mode by pushing down on the upper arm (simulating weight off the nose gear with full strut extension). After several cycles, the problem remained. The issue only cleared after a complete aircraft power dump.
For people not familiar with how McDonnell Douglas built aircraft…… air-ground switching is accomplished by using a cable attached to the upper scissor rod. Depending on strut extension, (short with weight on – long with weight off), this cable actuates two fairly large switches in the forward electronics compartment. These switches control a shit-load of air-ground relays that feed all the separate systems needing air-ground information. This system has been used on all MD products from the DC-8 on through to the MD-11.
(In this view we're looking towards the top of the strut. The upper link rod is located on the left. The cable is visible on the right wrapped around the bell crank.)
After some digging for information, the CFDS was accessed to look at flight fault history. Both FCC’s showed this.
Of all the air-ground relays, R2-5209 (Left Ground Sensing) and R2-5112 (Right Ground Sensing) feed the FCC’s. Each FCC gets input from “both” relays. Obviously, one of those relays was wrong.
What was puzzling was the fact that all the air-ground relays are controlled mechanically via the strut, cable, and switches mechanism. If we had something stuck, wouldn’t cycling the upper scissors arm correct the problem? Why did only the power dump correct the problem? I don’t have an answer, but I “will” be watching the aircraft for a while.
MD-11 ASM 32-24-00