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707 Vs DC8

  • Thread starter Thread starter AvroGuy
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Diesel Eight!

Tough old bird. From my understandings the 707's also have some corrosion issues and from what I have heard a life-limited airframe, the -8 does not.

A 61/71 & 63/73 -8 is a pretty big aircraft. All of those models are categorized as "heavies" (> 300,000 # MGTOW) With the CFM-56's mounted they are very efficient. I don't think that UPS is planning to retire theirs any time soon. If I remember correctly UPS is currently operating the largest fleet of -8's. From my understanding they have all been updated with glass cockpits - EADI, EHSI, FMS
 
OK..I guess I'll get to be the first to disagree with your post. The Air Force did buy a large number of 707's to use for parts on the -135 fleet. Specifically the JT3D turbo fan engines. And as to the second part of your post, as a previously qualified -135 F.E., I take umbrage. The Air Force used FE's on WC-135, VC-135, and some EC-135's.


Yeah, I agree with what you said above. I was trying to make the distinction that the 707 and Kc-135 are not the same plane. I was not aware that the USAF bought 707s to use as spare parts for the -135 fleet. But you cannot buy a used 707 and turn it into a KC-135.
 
While I understand your position, B767Inst, no umbrage should be taken regarding the comment that C-135s never had FEs. You've been there, so you know what L'il J said is semi-correct in that the aircraft never had a dedicated FE panel. It's not exactly common knowledge that various AF commands did and still do use a PFE on the 135s. Don't get me wrong - I always appreciated the reduced workload as a pilot with W&B, performance and with the overhead panel for pressurization and electrics in those cases:cool:, and the only complaint, if you want to call it that, is that it could get a bit awkward at times with the FE reaching over the throttles to handle to fuel panel. And you can't say that the fold-away jumpseat was exactly first rate. It wasn't even really rated for crash loads. The plane was designed to be operated in wartime with two pilots, a nav, and a boom operator.

Back to the topic, Waldom and HeavyJet's comments hit the nail on the head regarding the landing gear. And while I still miss flying the 707 and the C-135, I've sure come to appreciate the bulletproof but Rube Goldberg design philosophy of the DC-8. It's a great freighter.
 
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While I understand your position, B767Inst, no umbrage should be taken regarding the comment that C-135s never had FEs. You've been there, so you know what L'il J said is semi-correct in that the aircraft never had a dedicated FE panel. It's not exactly common knowledge that various AF commands did and still do use a PFE on the 135s. Don't get me wrong - I always appreciated the reduced workload as a pilot with W&B, performance and with the overhead panel for pressurization and electrics in those cases:cool:, and the only complaint, if you want to call it that, is that it could get a bit awkward at times with the FE reaching over the throttles to handle to fuel panel. And you can't say that the fold-away jumpseat was exactly first rate. It wasn't even really rated for crash loads. The plane was designed to be operated in wartime with two pilots, a nav, and a boom operator.

Back to the topic, Waldom and HeavyJet's comments hit the nail on the head regarding the landing gear. And while I still miss flying the 707 and the C-135, I've sure come to appreciate the bulletproof but Rube Goldberg design philosophy of the DC-8. It's a great freighter.


God that is a beautifule -8 in the background....
 
Mr. Patroni, she ain't going to take much more....

Well any way she is going to get it!

"That's the great thing about the 707 -- She can do everything but read."

All mechanics should smoke cigars.
 
lil jerry

reread my post....it says kc-135 e "mods"....never implied they were they sme airplane or that you can make one into the other
 
Heard from some engineers that Boeing (like Lockheed) had enough high-powered engineering talent to design a lighter, efficient wing that flexed enough in turbulence to give a nice soft ride, but the stresses were consequently above the "fatigue limit", and the wing would eventually get enough cracks here and there to doom the airplane.

Douglas engineering just built a "bridge" of a wing, with wing stresses below the fatigue limit, (and a "harder" ride in turbulence) and consequently the wing will not fatigue (ever), the airplane will be undone by old wiring harnesses or fuselage pressurization cycle fatigue, or politics, or something.

Both awesome flying machines!!!
 
No FMS on ours. We still use the good ole' INS.

Do you mean that your still using the Mighty 9 lat/long waypoint Delco/Litton Carousel IVA?

I would think that Big Brown would spend some money on that!

I was in the Tech Museum in Munich - They had a Carousel control head, main chassis and MSU panel on display. I was looking to see if it had a Serviceable Tag, I could have then purloined it for use in our aircraft!
 
Whoever designed the Litton 72/92 series shoulda been shot! Those things are the most user unfriendly #@$%&*()_ @#%$*&@$$*&@$$@^@$%^$&@)(.!!!!!!!!!!

Well, you get the idea.
 
I once heard a DC-8 captain refer to them as the Douglas Cable Company. One pretty tough bird.

Three American companies built heavy jets in the sixties.

The Boeing electric company

The Lockheed hydraulic company

The Douglas cable and accumulator company.

The outfit I worked for in the eighties sent a mechanic out to measure all the cables in the DC-8. That was 1987, and he ain't back yet.
 
Joe Patroni would disagree.

In the book he found a part that was defective by design and threatened the whole airline fleet.

He jumpseated to New York, burst into the airline CEO's office, pulled the oily part out of a sack and dropped it on the CEO's desk, saying something like "You're going to lose your company over this."
 
Maintenance--- look at any Boeing product versus Douglas start with DC3
Payload
Range

Are there any other issues than these that obsolete aircraft.
 

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