Members Login
Username 
 
Password 
    Remember Me  
Post Info TOPIC: Hastings TG502


Administrator

Status: Offline
Posts: 799
Date:
Hastings TG502


TG502 only ever used in experimental and research work, 502 was a Mark C1 when built, it had the tail plane lowered to the C2 configuration and was converted to a C1A with underwing fuel tanks, Boscombe Down was its home for much of its life, sent to St Mawgan for fire training in 1972 

http://i.ebayimg.com/t/RAF-A-AEE-Handley-Page-Hastings-C-1A-TG502-B-W-Photo-/00/s/MTA2NlgxNjAw/z/aV0AAMXQ74JTT-Nu/$_12.JPG



__________________


Administrator

Status: Offline
Posts: 799
Date:

Have read your page with interest, I recount my experience as a passenger on Hastings TG502 whilst on the ground at Ottawa, Canada in the winter of 1966/7.
At the time, I was a Senior Technician in the RAF, based at Boscombe Down. We were support crew to a Vulcan (XH 606) doing cold weather trials at CEPE Cold Lake, in Northern Alberta. The general procedure was for the Vulcan to fly ahead and the ground crew to follow in a Hastings, which was either TG500 or TG502, which were both used as support aircraft at Boscombe Down at the time.
This aircraft had made the trip to Cold lake, many times without incident, and an overnight stay at Ottawa was part of their usual itinerary, were the aircraft was left outside for the night. After boarding the aircraft for take off from Ottawa, the usual crew checks were being carried, out before start up, when the captain emerged and asked for the rear door to be opened and the boarding ladder lowered. After a few minutes, he called for everyone to disembark, which we all did. It was quite cold, about minus 20, but not unusually so for the time of year. Since all passengers were either engineers or technicians we gathered around to be shown the problem. The captain explained that he had been unable to move the elevators when checking the controls from the ****pit, which was a mandatory pre-flight check, hence is sudden disembarkation to find the reason. We all observed that the normal gap between the elevator and its surrounding tailplane was none-existent, and therefore the elevator and tailplane were seized together. A Special Incident Report (SIR) was raised and the aircraft towed in to the heated hanger.
Within 10 minutes, the previously, none-existent gap had opened to over 8mm, and the elevators were free. Since several airframe men on board had experience of rectification modifications to the Elevator Horns which had caused at least one previous crash of a Hastings, they were none too happy to leave things as they were! The last rib of the tailplane was therefore moved about 10mm away from the elevator, and the now spare metal trimmed flush, leaving a gap that could easily accommodate a hand thickness. Thoughts were voiced about this happening at 7000 feet, which was our normal cruising altitude and the resulting inability to control our altitude by normal means! We carried on to Cold Lake, via Winnipeg, without incident and the same aircraft made the same trip many times later. Why it happened this one time, no one seems to know. It was concluded that freak weather conditions had caused it, but I always thought that the air at 7000 feet was always colder than at sea level, were Ottawa, on the St Lawrence Seaway is located!.
Hope you found this interesting. Has anyone heard of a similar occurence?

 

Peter Kay



__________________


Administrator

Status: Offline
Posts: 799
Date:

TG502 C1A at Boscombe Down 1970 note the nose cone

JY Handley Page Hastings C1A A&AEE Boscombe Down TG502.JPG

 

 



Attachments
__________________


Member

Status: Offline
Posts: 12
Date:

History of TG502. Constructed as a standard C1 in 1947 then used by Handley Page for stability development flight trials in an attempt to improve the handling, during these trials several different horizontal tailplane configurations were tested, some with dihedral and some anhedral, until eventually in January 1949 a completely new tailplane of wider span was fitted, now positioned on the fuselage centre line some 16 inches lower than before. This proved to be the answer to the problem and it became the production standard for all the Hastings C2s that were about to be built. All other C1/C1as retained the early shorter span tailplane but TG502 retained its modified tail for the rest of its operational life. After the HP trials it was allocated to the A&AEE Boscombe Down where it was used as a support aircraft for trials in the UK and abroad and later received the C1a upgrade modifications including the under wing fuel tanks, in addition it gained a weather radar radome when a Ekco Weather Radar system was installed.  It was retired and SOC 15/12/72 and dispatched to RAF St Mawgan where it was used for fire practice, being partially burnt by 1974 and completely consumed by late 1977.

Richard

 



-- Edited by Sandown on Wednesday 28th of September 2016 10:00:42 PM



-- Edited by Sandown on Wednesday 28th of September 2016 10:01:50 PM

__________________
Page 1 of 1  sorted by
 
Quick Reply

Please log in to post quick replies.

Tweet this page Post to Digg Post to Del.icio.us


Create your own FREE Forum
Report Abuse
Powered by ActiveBoard