Regarding this Crashed SOPWITH CAMEL Aircraft .
The machine was 1st Identified as a Sopwith & not a Nieuport by Powerfix .
Just as soon as larger photos were supplied , he was then able to identify it as a Camel .
Most of the talk following from others is the blind leading the blind and going nowhere !
-----------------------------------------------
Regarding the 5 posted photos in post #1 on This Aerodrome Thread .. I will confirm the ID of these parts ....
Photo #1.....
Visible is the UPPER PORTION of a CAMEL TAILPOST , complete with the remains of a bent TAILPLANE REAR SPAR , which , for some reason , is "FACING the WRONG WAY" ..ie ...The central , internal wiring lugs at its centre , appear to be "Facing towards the Elevator" ! ,... instead of facing towards the wooden front spar .
To the far Left of the photo , one can Just see the Top of the CURVED TUBE ,coming from above the tailskid position , curving up & round towards the "just" visible point , where it is welded to the Main vertical Tailpost Tube member .....................................[ A...This confirms Camel Only]
The Elongated D ring for Tailskid bungee is attached by a Clip under the square longeron sockets ..............[ B...This confirms Pup or Camel].
There are NO Gusset plates between the Square sockets & the vertical tailpost tube member ....................[ C... confirms NOT a Pup].
There are NO side gussets to fix the D ring between...( thanks to bigger photo)..............................[ D... confirms with B, NOT Snipe].
------------------------------------
Photo#4.....
MOTOR MOUNTING PLATE .
16 holes ....Could be 110 LeRhone , Clerget ,or Bently ...No dimensions given so
Could be Camel or Snipe......[ A...Conformed NOT 80 LeRh Pup ..(12 holes) ].
6 long Slots up each Vertical Side Member ...
.......................................[ B...Conforms Camel or Snipe...ONLY ]
( Snipe has the Slots according to Sopwith Pts Illustration .)
Possible that the 2 Upward & Splayed out Channels behind the motor plate , pointing towards the MG's , for Sopwith Kauper Gear ...Might be there under the brush...Can't be sure .
.......................................[ C...IF there , they then confirms a Camel Only]
-----------------------------
Photo#3... ( This part laying , Right side uppermost , Fwd to the Right ).
RH, UPPER LONGERON Fitting located at Junction between TOP of the DIAGONAL WOODEN MEMBER & the TOP of the 2nd VERTICAL WOOD MEMBER ,... AFT of the Motor Plate Station .
This is the Station corresponding to the REAR MG BRIDGE , CROSS TUBE , which is welded either end , to the RH & LH Brackets , forming one complete assembly .....( Jim K gives this as Pt
D.2034.).
There is NO INDICATION of "Welding of the tube" to the Upper side strip part of the fitting .
The tube would overlap on the Inside plate by the Full depth of the strip & the welded joint continue over & cover the rear of the TOP of the fitting .....( There is a Sq Ltng hole in the Fwd portion)
Therefore , we can probably be 90% certain that we are seeing the RH Fitting .
The Cable that holds in the rear of the All'y side panel attaches to a 1/4 BSF ,Eye-Bolt placed some 2+" up the bridge tube on either side...
The Tube part is either missing ( torn away) or buried in the dirt .
The Pattern and Shape of the Lightning holes (see JK's posted Camel drg) precisely matches the crash pieces .
....................................[ A...Confirms its a Camel ..ONLY ]
Reference to Snipe & Pup Photos & Sketches .
.....................................[ Confirms NOT a Pup or Snipe]
The shape of the part shows that it is obviously Not a Spar fitting as BobT thought .
Looking at the fitting , the rear part of the Inside looks torn away & this may be due to the separation of it from the main part of the fitting ,..it may be with the remains of the MG bridge tube .
---------------------------------
Photo #2....[This has been miss- ID'd here on this thread as the " Stabalizer Front Attachment Fitting , B. 2035 " .]
This part actually is the LEFT HAND , LOWER REAR , WING SPAR , BOX FITTING (spar socket) at the INTERPLANE STRUT position .
At the centre of the top of the "Box" , one can see the Single Hole Lug for the Anti-Lift Raf-wire , Part of the Fork end is still attached , pointing off towards the Left & slightly Downwards . ( see photo)
Behind this is the Streamlined Socket ( for interplane strut ,..Pointig Fwd , which is to the Left in the photo.) .
This is integral with its lug on the right , which is for the Incidence bracing wire...
This lug passes a little way down the "vertical" Front face of the "Square "(sic) socket & is welded on .
On this forward facing ( to the right) , "vertical Front face , are formed the Internal Drag & antidrag wiring lugs ...A very BENT ( pos'. French type) Turnbucke is still attached here along with ferrule & bit of wire.
The Square Section shape of this Rear spar box is , as here , more of a regular Dm'd Sq/diamond shape ,... whereas the Front Spar sockets are much Higher relative to their Width .
.................................................. ............[ Confirms a Camel ] .
-----------------------------
Photo #5...This is the TUBULAR SOCKET located at the Mid-point of the ELEVATOR SPAR ...For the Attachment of the TRAILING EDGE TUBES @ the CENTRE ..
It has 6 lightening holes , useful for Sil Solder joint flow .
Welded at an outward angle , at its ends , are 2 Short Streamlined Sockets , that accept the pinned & Sil.Soldering in AP121 Trailing edge Tube .(Either side of the Fin/rudder) .....Just see the taper pins perhaps .
Both the main spar & T/E tubes are broken off at the ends of the sockets .
Without dimensions ...............[ This Only confirms Sopwith part ]
-----------------------------------
Photo#6..See photo , Post # 15 ..OF THIS THREAD.
FUSELAGE ATTACHMENT , SL/LUG , Fittings FOR the TAILPLANE / FIN/ FUSELAGE ,.."BRACING" by Raf Wires & TIE ROD ...( My Description )
This is the two fittings joined by a BENT TIE ROD & held up by a hand .
Each fitting consists of an SL1 (modified), with a wiring plate riveted underneath it ....
These clips fit on the Lower Longeron , first bay Forward of the Tailpost .
The SL clips have the usual bracing wires & ferrules exiting from their lug holes , some parts of which remain in place .
The thick riveted-on wiring plate , can be seen on the TOP of the Inverted LH clip as seen in the photo ...This & the corresponding other side clip/plate are Joined by the BENT Tie rod .
The Bent Rod ( when Strait) , was the " Tension load, Carry-Through Tie Rod" , that passes UNDER the the LOWER FUSELAGE REARMOST WOODEN CROSS MEMBER........Next Station Forward of the Tailpost .
At the outer ends of each RH & LH , SL/lug fitting , a Raf-Bracing Wire goes up to the fitting on the T/Plane Front spar , located appx. Mid-span on each side .
Above the spar , other Raf-Wires go upwards to converge on the Top of the fwd Fin -post .
.............[ This confirms a Camel part , Not a Snipe ,..Not sure exactly how the Pup is , but it's different .]
Jim Kigers drawing above gives the riveted on wiring plate Assy's as D 2094 .
--------------------------------------------------------------
That concludes the ID of the fittings ...All quite simple really ! .
I hope I have placed the Photo #'s in the right order .
--------------------------
If anyone cared to carefully read the threads posted by "powerfix" in an intelligent manner , one will see that , Once some decent size Photos were available , then all these things that say it's a Camel ,..( except the Rear Wing fitting & other stuff that the Moderator obliterated .).... were posted there quite early on ,and long before all the subsequent confused sniping drivel , that needlessly went on .
Regards & QED Camel ...All we need to know now from document guys , is the Military ID .