Barry, 12.07.2016 13:32 Flew for the first time on 29th December 1986 and was built under contract from DARPA. It is currently de-registered and in storage at Edwards Air Force base. Span 53'2" Foreplane span 37'8" Length 44'10" Height 14'1" Wing area 179.4 sq ft Foreplane wing area 118 sq ft Maximum take off weight 11,500 lb Max speed 196 mph

Phil Regulinski, e-mail, 04.08.2015 01:30 Do you know where I might be able to buy a photo of this plane? Something along the lines of 10" x 12" to hang above my desk.

Karl Reese, 30.03.2010 03:24 Where could I find a three-view? Thanks

Ray Cox, e-mail, 02.10.2007 01:00 As this aircraft clearly has a horizontal rear stabilizer, I suspect the stub wing at the front provides lift, making the ATTT a Tandem-Wing aircraft.

Simon Gunson, e-mail, 25.02.2007 21:36 I notice the canard has anhedral and the main wing dihedral. I take it therefore that this is because there is a real risk of the front wing interfering with or blocking airflow to the main wing ? Also when Mt Cook Airlines in the 1980s used BN Islanders as skiplanes in New Zealand they found the attachment of undercarriage to a very rigid wing structure caused wing spar cracks. Is this aircraft going to be tested/evaluated for this type of stress ? -Simon Gunson

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