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Hawker Siddeley Trident  
User currently offlineStarship From South Africa, joined Nov 1999, 1098 posts, RR: 14
Posted (15 years 4 days 5 hours ago) and read 1418 times:

Can anyone please explain the logic behind the Trident's nosegear being offset to the left and retracting sideways to the right? I have never seen this on any other aircraft and it certainly looks very odd when viewed from the front.

On another note, did you know that the Trident 3 had a fourth engine? It was located between the centre engine and the rudder above and was a Rolls Royce RB.162-86 booster with a thrust of 5 250 lbs. It was only used during take-off.

Nick


Behind every "no" is a "yes"
7 replies: All unread, jump to last
 
User currently offlineBuddster From , joined Dec 1969, posts, RR:
Reply 1, posted (15 years 4 days 5 hours ago) and read 1327 times:

It is an interesting a/c isn't it? In some circles it was referred to as the world's only "three and a half" engined jetliner. I understand that the booster turbo jet was added to increase takeoff performance (obviously) but the RR speys where pretty much at their economical limit of upgradability. It was cheaper to add the booster which could also be used during other phases of flight. The Trident was also the first airliner to be certificated for automatic landing in zero visibility. As far as the unusual landing gear, particularly the side retracting nose gear, I can't help you there. Perhaps this arrangement would make for an easier manual deployment since it wouldn't be competing with the wind as much as a forward extending gear. Regards, Doug.

User currently offlineViscount From Gibraltar, joined Dec 1999, 112 posts, RR: 0
Reply 2, posted (15 years 3 days 13 hours ago) and read 1309 times:

We used to see loads of Tridents (mainly two's and three's) here in GIB in the 70's.

These were truly majestic aircraft. Pity that they were not stretched slightly and re-engined otherwise the 727 would have had a real competitor.

They were certainly underpowered. The three's had to stop in TNG en-route GIB-LHR because they could not lift enough fuel from here for the trip.

I think that the front bogie thing was just a space problem but I'll try and find out.


User currently offlineTg 747-300 From Norway, joined Nov 1999, 1318 posts, RR: 0
Reply 3, posted (15 years 3 days 13 hours ago) and read 1306 times:

where is TNG?

Tg 747-300



intentionally left blank
User currently offlinePilot21 From Ireland, joined Oct 1999, 1386 posts, RR: 2
Reply 4, posted (15 years 3 days 7 hours ago) and read 1298 times:

Just a quick question in regard to the main landing gear of the Trident. I thought I saw/read somewhere that they turned 90 Degrees and retracted into the wing. Was this the case??


Aircraft I've flown: A300/A310/A320/A321/A330/A340/B727/B732/B733/B734/B735/B738/B741/B742/B744/DC10/MD80/IL62/Bae146/AR
User currently offlineDC-10 From , joined Dec 1969, posts, RR:
Reply 5, posted (15 years 3 days 5 hours ago) and read 1291 times:

Yes it's true the gear turned 90 degrees then inward. Each bogie had 4 tires...not like you'd see on a 747 but all on a single axle, 2 on each side of the strut..thats the primary reason for the 90 degree rotation

User currently offlineChris Keeping From , joined Dec 1969, posts, RR:
Reply 6, posted (15 years 2 days 22 hours ago) and read 1291 times:

The nosewheel was offset to one side on the Tridents to accomodate the automatic landing system which was located on the centre line of the fuselage towards the nose

User currently offlineAKelley728 From United States of America, joined Dec 1999, 2194 posts, RR: 5
Reply 7, posted (15 years 2 days 9 hours ago) and read 1281 times:

TNG - Tangier, Morocco

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