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The AIR-BRITAIN Militarv Aviation Historical Quanerlv

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15Dec67 Remains sold to Ministry of Technology (used for<br />

ground trials).<br />

22Jan69 Struck off Charge after making 141 flights.<br />

May 1974 Allotted to the RAF Museum, but in May 1978<br />

loaned to the Royal Navy Engineering College at<br />

Manadon as an instructional airframe (numbered<br />

A2619) . It was then loaned to the School of Aircraft<br />

Handling at RNAS Culdrose from 11 Apr78 (marked<br />

as 'SAH-6') before moving to storage at Carding ton<br />

in Feb94 and then to display at the Cosford<br />

Aerospace Museum.<br />

XS696<br />

05Mar65<br />

24Mar65<br />

01 Apr65<br />

First flight.<br />

Allotted to TES West Raynham.<br />

Caught fire on take-off at West Raynham and<br />

destroyed. sac same day as Cat.5(c). <strong>The</strong><br />

accident happened on its tenth flight.<br />

Below: Seven of the TES Kestrels on their flight line at<br />

RAF West Raynham during September 1965, wearing the final<br />

digit of their individual serial numbers as codes.<br />

(Central Press Photos via Phil Butler)<br />

Bot1om: XV·6A 64-18262 in the external display line-up at the<br />

US Air Force Museum at Wright-Patterson Air Force Base on<br />

30July1974. (Phil Butler1C71319)<br />

Aeromilitaria - Winter 2010<br />

Chris Farara kindly made some comments on my earlier<br />

article on the P .1127 prototypes, a digest of which<br />

appears below:<br />

On page 51 of the Summer issue, the photo of XP980 shows<br />

that a Harrier wing has been fit1ed for the trials that it was<br />

being used for. On page 52, it should be stated that MWDP<br />

funding was only provided for the Bristol engine, not the<br />

P.1127 airframe; it should also be stated that all Hawker<br />

development flying was carried out at Dunsfold, and the work<br />

at Bedford was research being carried out by the RAE. <strong>The</strong><br />

photo showing the ram-air turbine should have stated that this<br />

was always exposed when the engine was shut down, as it<br />

relied on positive pressure in the flying control circuit, provided<br />

by the running engine. <strong>The</strong> lower photo on page 52 shows<br />

XP831 having 'inflated'-shape intake lips, while XP836 has the<br />

'deflated' shape, with XP831 being dedicated to low-speed<br />

and XP836 to high-speed testing, these shapes being most<br />

appropriate for their intended flight envelopes. <strong>The</strong> photographs<br />

on pages 51 and 53 show the inflatable lips installed,<br />

while those on page 54 show alternative metal types, with<br />

those on XP984 being the finalised type, as used on the<br />

Kestrels. <strong>The</strong> inflatable type was abandoned, being liable to<br />

tearing in certain flight conditions. Finally, the crash of XP831<br />

at Paris was due to rotation of the air nozzles because of a<br />

malfunction, leading to a modification to the control valve to<br />

prevent any recurrence. Although the malfunction might have<br />

been caused by 'FaD', this was never proved.<br />

151

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