Wednesday, October 1, 2014

September XP-82 Twin Mustang Restoration Project Update


It has been quite a month!


Tail Sections
For the majority of the past month, most of the crew has been on the final alignment and attachment of the aft fuselage extensions, verticals and horizontal stabilizer. The initial lineup when perfectly, but the microscopic adjustments down to .010 (ten-thousandths - 3 times the thickness of a cellophane  plastic sheet) seemed to have taken forever, but everything is now permanently aligned and attached, and the team has started the final fitting and riveting of the side skins.


Right-hand Aft Fuselage Extension


Left-hand Aft Fuselage Extension

The pulley brackets for all of the primary controls (elevator and rudder), and secondary (trims) are now completed and awaiting final installation along with the four side skins. All four of the elevator and rudder mounting castings and associated matching bellcranks have been final fitted. 


Elevator Push Rods


Right-hand Inboard


Right-hand Outboard


Elevator and Rudder Bellcranks

Both dorsal fins are well on their way to completion. We had to make a few ribs and attachment parts, but the job of alignment and installation of the dorsals went smoothly.

Two other team members have been restoring the multitude of tail wheel gear parts. One cannot believe how many moving parts are in our XP-82’s tail wheels: retraction, extension, steering, oleo, tail door opening and closing, etc. Virtually all the parts needed attention and overhaul to bring them back up to airworthy condition. 


Just some of the tail gear parts


Notice the milling marks on the XP prototype tail gear fitting.


Tail Wheel Oleos

Canopies, Trucks, Opening/Closing Cranks, Windshield Side Glasses
Both hand cranks are now completed and are being installed, and both canopies are ready for installation. All four windshield side glasses are nearing completion. We should have them within a week for routing, trimming and final installation. Even though they look similar to the P-51 series, these canopies and windshield glasses are nowhere close in shape or dimension.    


Canopy Hand Cranks

Outboard Wings
The work on both outboard wings has slowed as we are waiting for the final aileron and flap hinge points for final completion and close-out of the four bottom rear skins.  The remainder of these parts are due here within the next two weeks to coincide with the team completing the riveting of the tail sections. 


Outboard Aileron Hinges

Main Gear Door Opening/Closing Hook Mechanisms
We have received the final forgings for the main inboard gear doors. These parts hold the multitude of push/pull rods that control the positive lock/unlock hooks, which keep the doors securely closed during flight.  They all will be installed this coming month.  Thanks, John, Advanced Manufacturing Concepts.


Inboard Flap Hinges
Both center section flap hinges are now aligned and permanently installed.


Right-hand Inboard Flap Hinge

Coolant Exit Doors,  Header Tanks
Casey Hill, English wheel forming wizard, is due here this week to complete the forming of the two complicated interior coolant exit door skins. Also, both coolant header tanks are now installed, one in each rear fuselage.


Coolant Header Tank

Gun Mounts
The six aluminum gun mounts that will be bolted into the center section are now completed and awaiting installation.  Thanks, Vic, Peres Pattern.



Left: Outboard aileron hinge bearing mounts
Right: Outboard flap push rods


The Katz

"What do you mean you again forgot to get my treats!"
- Allison






Please support the Wounded Warrior Project.


Thanks.
Tom

Sunday, August 31, 2014

August XP-82 Twin Mustang Restoration Update

August was an incredible month for accomplishments.

Wings Removed and Fuselages/Center Section Pivoted
This past 15 August the time came to turn the fuselages/center section 90 degrees to the south in our hangar. We used the factory-mounted 45 degree lift points on the inboard side of the center section, right against the fuselage lower longerons. These lift points (¾-16 threaded ports) are designed to bear the entire weight of the aircraft including the engines.  We were able to lift the entire balanced center section with both fuselages and engine mounts with one man lifting and guiding each rear fuselage. The lift and pivot took only about two hours to reposition the aircraft where it would fit out the large south door.


After the lift and pivot, we leveled the aircraft in pitch and roll to within 1/30th of one degree, about the thickness of a piece of cellophane.  We manufactured two vertical steel support pipes to fit into the rear jack points (right forward of the tail wheel attach), and designed them to be vertically adjustable.  At that time we leveled both fuselages on the center section by using the factory shims, and are final-attaching the fuselages to the center section longerons with the remaining six of the twenty internal wrenching NASA bolts. (Longerons are the main beams that are the lower structural rails mounted in the bottom of both fuselages.)




We moved the outboard wing fixture into the hangar and attached the wings to check the washout and made the final microscopic adjustments.


Verticals, Horizontal and Rear Fuselage Extensions
The next day we installed all of trim actuators  in each vertical and the horizontal, (three) and installed all the trim cable pulleys in each vertical. 



We then attached each vertical to its respective side of the horizontal stabilizer. We had to align and hold the verticals in a perfect 90 degree position in relation to the horizontal stabilizer. We used diagonal wires and turnbuckles to make the final tiny adjustments as the verticals are permanently held in place when the aft fuselages are high-shear riveted and bolted to the forward fuselages.



The following Saturday the team built a temporary cushioned wood scaffold and lifted the horizontal/verticals/aft fuselage sections up and forward to within ½ inch of their final attach positions. 


Then came all of the final adjustments to make sure everything was properly aligned prior to drilling and reaming any of the attach holes for the fittings. There were eight exact measurements that had to be aligned:

*  The angle of incidence (the pitch up and down on the horizontal stabilizer in relation to the center section.

*  The alignment of the two vertical stabilizers (toe in, toe out).

*  The exact vertical measurements on the verticals in relation to the horizontal measured between the two top and two bottom rudder hinge points horizontally and diagonally.

*  The exact forward and aft dimension of the center section trailing edge to the leading edge of the horizontal stabilizer.

*  The left and right measurements on the aft fuselage extensions to the forward fuselages. This exact measurement is obtained by shaving the attach fittings of the horizontal stabilizer to the vertical stabilizer.  We intentionally machined all four of them 1/32" thicker to give us extra material if we needed to make small adjustments.

*  The twist of both aft fuselage extensions to align the upper and lower attach points.

*  The vertical attachment of the aft fuselage extensions to the forward fuselage attach points.

*  The alignment of the dorsal fins with the leading edge of the vertical stabilizers.

Everything lined up perfectly.  So then the team started final drilling and reaming all the attachment hardware for the high shear rivets. 

Outboard Wings and Center Section
We completed the riveting of all the top skins while on the fixture, and one more bottom skin on each wing which locked the wings into their final shape.

Both wings are now off the fixture, and the team is completing the final riveting and finishing the fuel cell stand-off angles.

Two of our team members are now fitting and installing the new aileron attach hinge point fittings. One of our machine shops is making the final two outboard flap hinges.



The new inner and center aileron attach hinge point fittings
 are now being installed on both wings.


Two inboard and two outboard ailerons

The final Adel clamping of the wiring harnesses in the center section is now being completed along with the final attachment of the three wiring terminal strips in each wheel well. One of our volunteers is sewing the canvas covers that shield and protect these wiring bundles and terminal strips from dirt and moisture thrown up by the rotating tires on retraction.  Thank you.

The center section nut-plate channels, that attach the fuel tank close-out panels between the outboard wing and center section, are now completed.


Fuel cell stand-off angle installed.


Newly machined forward and aft door lock bell crank
mounts for each main gear door


The new wheels and tires are now installed on the main gear legs

The Katz

"You will not get into this rivet case until I get my treats!"     --- Allison



Thankx
Tom

Friday, August 1, 2014

July Restoration Update




It was a very interesting month

Wings
A lot of to-complete projects on both wings are being done, i.e., flap and aileron hinges, drop tank pressure and feed lines, de-ice hot air discharge vents (14), countersinking the remaining lower skins, aileron trim jack screws, etc., etc.


Drop tank  pressure and fuel feel lines



Riveting the de-ice hot air discharge vents in the lower skins of both wings.  
There are fourteen of them.


Vertical Stabilizers
Both vertical stabilizers are now completed, less the side skins that must be left off to gain access for alignment and fitting. Each vertical needed its lower skin riveting completed. Both verticals are awaiting mounting to the horizontal stabilizer and then to the aft fuselages.  All of the trim tab (rudder and elevator) pulley brackets have been installed along with all of the closeout panel, fairing and tip nut plates. The alignment, final installation and riveting of the four rudder trailing edge hinge points are now completed on each vertical. 

The two aft jack points are now installed along with the gap seal extrusions in the vertical stabilizer-to-rudder bays. 


One of the two wood-forming blocks for the vertical tip cap has also been completed, awaiting the forming of two new vertical tip caps out of 5052-0 aluminum.


Vertical Stabilizers to Aft Fuselage Attachments
The special angles (four) have now been final fitted and drilled and reamed for the attaching 5/16” and 3/8” nut plates and close-tolerance bolts. The excess skin overlap on both aft fuselages has now been flush trimmed to accept the zero-tolerance butt-fit of the four vertical stabilizer side skins (two per vertical). 


Wheels and Tires
The new Michelin Air 32 x 8.8” tires have now been mounted on our new wheels. We had to lathe out of a piece of billet two new inner-bearing and seal spacers. None of the original ones that we had from the Soplata or the Alaska wreck site were salvageable due to deep rust pits. 


Heat Exchangers / Cooling System
One of our machine shops has completed the remainder of the brass water neck and purge fittings that get soldered on to the shell(s) of each heat exchanger. (For a size reference, the diameter of the large flanges is about 6”.)



Another one of our shops completed the sewing of the chafe straps (10) for the oil and glycol header tanks.  Thank you, all.

Windshields
As mentioned in the previous news release, the two center windshield glasses are now completed and fit. The four side glasses have been sent out to an aviation Plexiglass-forming company in Ohio. We hope to have these back soon.


The Katz - It’s Hot!
“Would you be so kind to let everyone know as they pass the water cooler, to push the cold water button.  Thanks.”
-- Rivet

Thankx
Tom

Monday, June 30, 2014

June XP-82 Restoration Update




Wings/Center Section
The crew completed the left-hand leading edge and final riveted it to the forward spar of the left-hand wing.


Left-hand Wing

The remainder of the top inboard skins are now completed through their structural high-shear riveting (special collared steel rivets through the wing-attach angles and stringers).  On both wings, the crew has three of the four top skins completed along with the two lower inboard skins at the attach angles. 

We chose to use the center section as the parent fixture for the attachment of the wing-attach angles and the riveting of these upper and lower inboard skins to lock everything in place on sweep and dihedral. The two wings will come off during the second week of July and go into the fixtures for final adjustment and to confirm washout (the downward twist of the outboard section of the wings). 


Lower and Upper Views of the Right-hand Wing


Hydraulic, Instrumentation and Brake Lines
The majority of the lines running along both cockpit floors and up behind and through each firewall are now completed. It has been difficult attempting to duplicate the exact routing of each line as most of them had been removed during the disassembly of the fuselage from the center section in the early l950s.  We were able to get the routing accurate by observing the through-fittings in the center section floor and the line mounts on each longeron. The drawings we have depicted the “B” and later model fuselages, a number of them having the same routing as our XP. 

The overhauled hydraulic firewall-mounted tank has now been completed, including the fuselage suction feed/return and pressure lines. 


Left-hand cockpit prior to final Adel clamping


Completed right-hand cockpit less master cylinders


Hydraulic tank with new hydraulic quick disconnect now mounted to firewall

Seats
We have been restoring the seats and the question came up as to whether we are going to use the original steel armor plate or replace with .437 (7/16”) aluminum plate for weight savings. We have two original steel armor plate panels that can be easily welded, surface ground and repainted.  Where the airplane comes in on weight and balance will make the decision for us.




One of our machine shops completed the two
 XP non-boosted aileron hinge points. 
The left-hand pair show the two separated subcomponents.


The left-hand aileron acme screw trim tab control box and bronze chain sprocket 
are now completed.


Parts Find
The first week of June I received a call from a man in Mint Hill, NC, just south of Charlotte, who had purchased a P-40 project from Ms. Janie Odgers, the family from whom we had bought from the remains of the crashed F-82H out of Fairbanks, AK. Richard Odgers, the now deceased husband, was too ill back in 2008 to travel to Anchorage to complete the sorting of the F-82 parts from the P-40 parts that he had in his warehouse.  Brent VanDervort, whose business is a large hot rod fabrication facility, purchased the P-40 project along with a small cache of F-82 parts.

I made a trip to Charlotte last week to examine what he had and, he had a number of important parts that we were still missing, i.e., four throttle quadrant cable quick disconnects and throttle handle, pilot’s glare shield gun site mount, one leading edge .50 caliber gun barrel fairing and blast tube, and a number of other small pieces of gold.  He declined my offer to pay him and said these parts were supposed to come to us six years ago. 


If anyone is contemplating building a street rod, his company is Fat Man Fabrication, Mint Hill, NC. One cannot believe the quality and the massive amount of different parts that his factory manufactures for the street rod business. Thank you, Brent.


One of the six center section leading edge machine gun ports 
and .50 cal cooling blast tubes.


Pilot's knurled throttle quadrant handle


The last four NAA throttle quadrant cable quick disconnects
that we still needed to complete our cabling.

A Special Visitor
Mr. Jim Sampson, a retired USAF Alaska F-82H pilot from 1946 - 1949, gave us a very nice visit last week. He is the youngest and most agile 93-year-old I have ever met in my life. He could remember flight details, i.e., air speeds, manifold pressures, climb rates, as if it were yesterday. He was very impressed with our restoration and promises to come back on a regular basis.  Thank you, Mr. Sampson, for your USAF service.


Mr. Jim Sampson and Tom

The Katz

Allison selecting a bolt


Allison's Selection of Bolts


"I don't think that the Rockwell hardness on this bolt
 is good enough as I can bite into it." -- Allison



Thankx
Tom