Ad: This forum contains affiliate links to products on Amazon and eBay. More information in Terms and rules
Oh they're out there!!!! You'll have to look in the old AAF regs and TOs. Many of the outdated regs pertaining to aircraft maintenance are hard to find (at least in my experience).It would not be army if there were not rules and lots of forms i think. And i think it is strange we cant find the "rules"
You're correct to a point. As far as "assembly line aircraft" not being easy to work on, it depends on the aircraft. Part of the design team on some aircraft involve maintainability engineers.I presume aircraft are like most things in engineering. A structure can be repaired if it is damaged following procedures but those procedures apply to a structure not previously repaired and a separation is required between repaired areas,a point is reached where it is easier and safer to replace the whole thing. Aircraft made on an assembly line are not so easy to work on, I would imagine getting a burned out/shot up fuselage back to A1 condition would be a nightmare for the electrics and hydraulics.
In this case, the USAF has worked long and hard with Boeing to extend the B-52 life. As I have mentioned many times, this is done at Tinker AFBthinking about this...they must have abandoned this idea or at a certain number of hours do major overhauls because the B52s have been flying for a LONG time. maybe flyboyj has the answer for that one
I read somewhere that some B-52s had the wing to fuselage joints replaced 4 times and that was over 15 years agothinking about this...they must have abandoned this idea or at a certain number of hours do major overhauls because the B52s have been flying for a LONG time. maybe flyboyj has the answer for that one
In peacetime the logistic supply chain means that any major repair can be carried out in accordance with the manuals, really, but during the war, that wasn't always the case.
I don't think corrosion was seen as a huge issue back then (that's my biggest moneymaker- then cracks.)
Modern aircraft are designed with maintenance criteria set by the manufacturer .
You know I could have sworn that my father served in WW2 during 1939 (France), 1940 (France, Egypt). 1941(Egypt, Iraq, Iran, Syria), 1942 (Egypt, Libya, Morocco, Algeria) 1943 (Tunisia, Italy), 1944 (Italy), 1945 (Italy) which I make 7 years.The war only lasted five years during which there were over 20 marques of the spitfire, how many planes do you work on under 5 years old?
I wasnt meaning to cause offense just discussing the European air war which kicked off for real in 1940 and ended in early 1945 when the LW were just about out of planes pilots and fuel.You know I could have sworn that my father served in WW2 during 1939 (France), 1940 (France, Egypt). 1941(Egypt, Iraq, Iran, Syria), 1942 (Egypt, Libya, Morocco, Algeria) 1943 (Tunisia, Italy), 1944 (Italy), 1945 (Italy) which I make 7 years.
The war only lasted five years during which there were over 20 marques of the spitfire, how many planes do you work on under 5 years old?
Someone posted a stat on the US air force, I cant remember the percentage but I think that today most US pilots are flying planes older than themselves.
War Weary as labeled by AAF was a threshold based on airframe hours - different from 'unsafe to fly' based on other factors like major bending of an airframe with damage type such as severely deformed longerons in the fuselage. Many WW Mustangs for example, were pressed into operations when a maximum effort was required. WW was a judgment, not an objective flight safety criteria.
There were no sophisticated Zyglo or X-Ray Penetrant methods to detect stress cracks ordinarily hidden from sight unless major inspections are performed at scheduled hours. Basically most WW bombers had a far higher threshold than fighters because of the Design Limit differences and many WW B-17s and B-24s were older models replaced by better equipment and no longer required for operations.
That said WW wasn't applied to observable abnormalities such as skin buckling, popped rivets, etc - which were a sign of the airframe exceeding design limits pointing to near failure and destruction. These a/c were inspected by Engineering officer and most frequently Salvaged Class 26. Don Gentile's Mustang "Shangri La" was an example of the Salvaged Category.
thinking about this...they must have abandoned this idea or at a certain number of hours do major overhauls because the B52s have been flying for a LONG time. maybe flyboyj has the answer for that one