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767/757 RAT
Hey tech nerds,
it came up on the air India accident thread about possible RAT deployment. Someone said something along the lines of “every heavy Boeing twin has a RAT”, there was another post about a 757 that had a fuel control switch shut off SNAFU and they “flew all the way to wherever with the RAT deployed”. And I’m like, whoa, I flew thousands of hours on the 767, around 30+ airframes and none of them had a RAT. So I asked chatGPT (ok I know could be incorrect), and it said the 767 200/300 didn’t have a RAT, but the 400 did. So I posted that (i didn’t say I asked chatGPT) and a couple of people were like “this dumbass flew the 767 and didn’t know it had a RAT”, “what an idiot”, “EVERY 767 Boeing built has a RAT” etc etc. So, normally I don’t name companies but you’ll be able to guess - I flew 767-238ER PW and 767-338ER GE and 767-336ER (leased from BA). All of those had backup HMGs, hydraulic generators, but no RAT! The 238ERs and 338ERs were 180 min ETOPS and, from memory, the -236ERs were maybe only 120 min ETOPS, I am a little fuzzy here but that may have been because they had one less HMG than our 338s. I think 338s had 3 HMGs and the 336s had only 2. Our 238 and 338ERs flew across the pacific constantly. On non-revenue disposal (and I assume deliveries) they flew direct east coast Aus to west coast USA. Have I gone senile? I feel like i am taking crazy pills! Am I a “total dumbass” as “every 767 Boeing ever delivered had a RAT!”?? Any 767 drivers, what are/were the RAT configs on your aircraft? You don’t have to name your operator/company if you don’t want to, but identify if it’s a 200/300 or 400. |
Both 757-200 (RB211-E4) and 767-300ER (CF6-80C2) experience, both had a RAT to power flight controls only from memory (although the 767 might have done a little more, I only flew it briefly so can't remember the detail). All the 767's had HMGs (again don't remember how many) but only some of the 757's had a single HMG, the rest were non-ETOPs and had none. 757's were all passenger config, the 767's were a mixture of factory built and converted freighters.
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https://cimg9.ibsrv.net/gimg/pprune....6a0dd326f.jpeg
757-200 RAT location https://cimg4.ibsrv.net/gimg/pprune....e065b7520.jpeg 767-300 RAT Location |
A cursory search for images of Qantas 767s on a popular airliner photos site reveals a panel with a red outline in the same place as in the image Downwind posted, and a RAM AIR TURB switch on the cockpit overhead panel.
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Originally Posted by skkm
(Post 11900555)
A cursory search for images of Qantas 767s on a popular airliner photos site reveals a panel with a red outline in the same place as in the image Downwind posted, and a RAM AIR TURB switch on the cockpit overhead panel.
Theres no writing/red box near the right wing root below. Please show/link me the image of a red rat 767 with the red box if you can. https://cimg4.ibsrv.net/gimg/pprune....bda3245bd.jpeg |
Originally Posted by skkm
(Post 11900555)
a panel with a red outline in the same place as in the image Downwind posted.
https://cimg6.ibsrv.net/gimg/pprune....74f130c33.jpeg Interestingly enough, the aircraft above, VH-OGV is now flying with the Israeli AF (jet went to maybe freighter stateside in the interim). The photo of that below clearly shows a red outline on that panel. I remember OGV because it was the only one of the entire fleet of 238/338s that had FADEC (did the RR 336s have FADEC?). OGV went to cairns for a few years before coming back in mainline colours. I’m thinking the following. 1. I’m completely wrong. Every 238/338 767 had a RAT; or 2. The red rat, in their infinite Wisdom, got Boeing to disable the RAT. They have a history of annoying customer options. Israeli AF (or other operator in between) re-enabled it? https://cimg1.ibsrv.net/gimg/pprune....fb3aac62d.jpeg ideally we need a fellow ex 767-238/338 driver to come out of the woodwork and say option 1 or 2? :} |
I would submit that as Boeing sells parts for the RAT on various 767 models, we can fairly infer that at least some 767s are fitted with them.
See https://shop.boeing.com/cpd/bpp_258t7100-7 and other items in the shop. |
Originally Posted by Gin Jockey
(Post 11900599)
I don’t think the switch was enabled, I looked at a few photos, but they are angled and I couldn’t quite see… I don’t remember it being there. it wasn’t in our dual engine fail memory items that I recall (I assume it’s like the pax O2 switch in a depress where it’s pushed to backup the automatic activation if needed).
Theres no writing/red box near the right wing root below. Please show/link me the image of a red rat 767 with the red box if you can. Can’t be much help other than that I’m afraid! |
752 for 25 years, some pax some pax to freighter conversions. Alongside that for 16 years 763, some brand new freighters some conversions. They all had a RAT. 75s we’re all RR, 76 all GE. Their only function was flying control hydraulics. Hth, rgds
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Originally Posted by OldLurker
(Post 11900687)
I would submit that as Boeing sells parts for the RAT on various 767 models, we can fairly infer that at least some 767s are fitted with them.
See https://shop.boeing.com/cpd/bpp_258t7100-7 and other items in the shop. yep, no doubt many have them, it appears most have a RAT. I don’t doubt that. There was a post of an FCOM page on the AI thread with a reference, I just wish I had old manuals to see what ours said. |
Were the RATs possibly removed/deactivated and then reinstalled/reactivated at some point? It appears from these photos the panel is marked- on both OGx and ZXx series.
https://www.jetphotos.com/photo/6541888 https://www.jetphotos.com/photo/6751952 https://www.jetphotos.com/photo/6809138 https://www.jetphotos.com/photo/7105098 https://www.jetphotos.com/photo/7160608 https://www.jetphotos.com/photo/7751036 https://www.jetphotos.com/photo/7962488 https://www.jetphotos.com/photo/9113366 |
Gin, I was a Propulsion engineer at Boeing for 40 years - a good share of that working the 767. The RAT was basic on the 767 (and I believe the same for the 757, although no firsthand knowledge of that). It was required for cert to meet controllability requirements if both engines shutdown. Unlike the 737 (and 707/727), the 767 requires hydraulics for flight control, and windmilling engines simply don't provide sufficient hydraulic power to meet the minimum requirements. It's not optional, or removeable - it's required for cert. The HMGs were optional (added when ETOPS become the norm - ETOPS hadn't been invented at the time the 767 was originally certified), but the RAT was basic.
The 747 requires hydraulics for flight control, but (except for the 747-8), four windmilling engines would provide sufficient hydraulic power for controllability, so it didn't need a RAT. It simply boggles my mind that you could have flown them and not known that. |
Originally Posted by tdracer
(Post 11901052)
Gin, It was required for cert to meet controllability requirements if both engines shutdown.
as for boggling the mind, I remember many tiny details about the 767 10ish years later, but zero about the RAT. That part of my brain must be mush. |
Both those photos in post #5 and #6 (Qantas & Australian 767's) shows the red outline at the right aft wing root!
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Originally Posted by Capt Fathom
(Post 11901088)
Both those photos in post #5 and #6 (Qantas & Australian 767's) shows the red outline at the right aft wing root!
But… see my previous post, I have conceded on other grounds (tdracer post). I will repeat for all your collective glee, “I am an idiot.” https://cimg8.ibsrv.net/gimg/pprune....f77a48c4e.jpeg |
We deployed, modded and tested many a RAT on the 767 fleet.
QF 200ERs had one HMG, whereas the rest (including VH-EAQ) had three fitted, from memory. |
Originally Posted by Lifer01
(Post 11901121)
We deployed, modded and tested many a RAT on the 767 fleet.
Noted. I have no memory of the system. I assume manual deploy was clear plastic flip guard over push switch like a gen drive disconnect or cargo fire bottle discharge? And with equally irreversible results? MEA CULPA. |
Yes, one time action from the Flt deck on P5.
Stow switch (and back drive handle for testing) is on the keel beam in the right wheel well. |
Originally Posted by Gin Jockey
(Post 11901126)
Noted. I have no memory of the system. I assume manual deploy was clear plastic flip guard over push switch like a gen drive disconnect or cargo fire bottle discharge? And with equally irreversible results?
MEA CULPA. |
Genuine question: never trained a dual engine failure in the sim ?
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