Rivets (and the power of the Internet)
So I order up the rivets, job done, we e ell not quite. Ben is now concerned about riveting in general and asks me to let him know in what other positions I have to replace them. Books and drawings spread all over the table I set to finding out wherever else they may lurk Luckily out of the ones that I turn up only one other place that worries Ben. This is the mounting plates for the interplane struts, he tells me that the stress on these is very complex. After a think I see what he means, not only the flying and landing loads transmitted though the rigging wires there are the torsional loads from the changing lift distribution in manoeuvring and at differing speeds and also the loads caused by control deflections. Complicated stuff and way beyond my aging brain cells so it is good for my moral that Ben has to consult Billy Brooks who is just about the most experienced microlight engineer in the country. Between them they come up with an answer. That is that neither are happy to use monal rivets in that position and the recommendation is that I use Avdel Monobolts, a sort of super pop rivet. I trace a source and order some up, how did we manage before the Internet?
Ordering up both rivet types I find that they have more that Bens approval in common, minimum orders for both of a 100 rivets. Oh well I’ll not run out for a while, it also makes me appreciate the brilliant service that I have become used to from LAS.

I write these recommendations into my repair scheme as modifications and send off the latest version. Result! At last the draft MAAN comes back, which will allow me to go ahead. As far as approvals go I feel that I am on the downhill run with just some answers to find about the last missing service bulletins. I put out an appeal on the BMAA forums and the Tiger Cub Yahoo group for these but without much hope. I get two replies but neither is able to help. So I’m back on my own resources again and I start to wade though all the associated paperwork that I have accumulated. This is fascinating stuff, it’s like taking a trip back to the early exciting days of microlighting. I find that I have a very nicely produced sale brochure complete with picture of a Cub flying, undergoing load tests and loads of enthusiastic blurb.
All these pictures are of the first Cub that is now proudly displayed in Newark Air Museum, where the curator was so helpful to me when I started this project so many years ago.

Quote from Test Pilots Report
“Take off, however was a different story. No gentle transition from ground to air with this ship. Full throttle gives a very rapid acceleration with a swing to the left needing firm pressure on the rudder to keep straight. The tail comes up almost before the aircraft has moved and in approximate 20 to 25yds we were airborne and I had to quickly raise the nose to hold the speed back to 40 knots IAS. A glance at the ASI confirmed an initial climb rate of 1000 feet per minute which settles down to 800 feet per minute once clear of ground effect.” Sounds good to me
There are price lists from your local friendly microlight dealer including ballistic parachute systems, I didn’t know that they went back that far. Local flying club newsletters that talk of long past meetings and flyins, many of these seeming just to be held in a farmers field. Also in the collection are newsletters from MBA and Tiger Cub Developments giving warnings that you need to be a taildragger pilot to handle a Cub and introducing a coaching scheme to train pilots. These newsletters also track the introduction of airworthiness requirements for microlights and MBAs struggle to gain approval as the flow of new customers dried up awaiting the outcome. Then as Type Acceptance was gained the company was broke and the banner passed to Tiger Cub Developments.
For me though, the important thing was that I believe from the contents of the newsletters I can prove the content of the missing service bulletins.
Once again out with the spanners! I have a front floor to fit with my nice shiny stainless steel rivets and despite my concerns about using a hand puller on 4.8mm stainless fixings they went in well with a generous dollop of Zinc Chromate. Then an afternoon spent with my collection of bracing wires got to the top of my list. These were just tied into bundles according to the aircraft that they came from and had to be sorted into their various functions. I had wires from GMJSP, GMJSU, GMNKM and Kit 208 but none of them singly forming a complete set. I laid them all out on the lawns at the back of the house and started checking them by length and the fittings still attached to them. After hours of patient detective work I was confidant that I knew where they all belonged and labelled them all with their function and origin. Phew I was glad that was over with. Although I have no intention of using the old wires I need them for patterns when the new ones are made up.
Then out of the blue I get an e-mail from South Africa, a chap called Christian has just purchased a Tiger Cub but is short of information, can I help? His Cub is an interesting little beast with sprung undercarriage and a centre section fuel tank. It has suffered a landing accident but looks in fairly good shape. By UK standards he has had an epic trip to collect it and he has a history of kit building so it seems that little aircraft is in good hands.

Thanks to my assiduous gathering of Tiger Cub paperwork I can supply the handbooks, kit build instructions and most of the Service Bulletins. Loaded on a disc. It is a pleasant feeling to know that all those miles away another little Cub is on its way back where it belongs, in the air.
Just after that disc is launched I hear from Paul who has just obtained one Tiger Cub G-MMIH and almost enough of another one to restore it so we exchange information.

Paul can supply me with some of my missing service bulletins and I have some stuff that is useful to him, result!
After having read some of the (until now) mysterious missing bulletins I find that one that had caused me some concern MS SB 020. Mandatory. In the Type Acceptance Data Sheets in simply states “Rear Fuselage Bulkhead” with no further detail. A bit worrying that as that bulkhead is the anchor point for the rear ends of the longerons the rear tube of the fin from which the rudder is hinged and the tailwheel. Although I have a bulkhead that has done much flying attached to GMNKM it looked exactly to same to me as the ones from GMJSU and GMMKT. Had they all been modified? A bit difficult to be certain, was I missing something? I checked and measured everything, plate thickness, hole sizes the lot, identical! Not really reassured but unable to think of anything else I re-read all the circulars to see if there was a clue, nothing. Then Paul e-mailed me a copy and all was revealed, due to heavy tailfirst touchdowns some lower longeron brackets had been found cracked. The requirement was to check condition before flight, literally lift the tail and look, I’d never have guessed that. So no modification needed just a check, thanks Paul. Copies added to the information disc and sent on to Christian and a new disc to be made for Ben and one niggling worry out of the way.
Back to the workshop first to dismantle the main undercarriage from SU and to check the same bits from Kit 208, as usual taking photos and labelling all the bits.

Then with this done and ready for cleaning I can treat myself to some thing that I have been looking forward to, re-uniting the front and rear sections of fuselage. After much tweaking, fiddling and a bit of cursing the fuselage stood as a single unit for the first time since. 1986.