1964 Folland Gnat
Asking $189,000 / Offer / Trade?
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| 1964 Folland Gnat Ex-British Royal Air Force 3979 TTSN (Actual appears to be 3572 after correcting an appearant logbook error) U S Airworthiness issued by the FAA in 1995. A/C flew regularly until 1998. Hanger by it's then new owner until 2004. Sold to present owner who did a 15 month $200K restoration that was completed in 2006. |
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| Rolls Royce (Bristol Sydley) Orpheus 101 645 TTSN 50 SMOH |
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| King NavComm King KT 76A Transponder IFR Certified |
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| "Hot" Ejection Seats Speed Brakes Fire Suppression System Anti-skid Brakes Drag Chute G-meter Mach Meter Built-in Oxygen Pressurized Air Conditioned |
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| Red with Blue Graffics |
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| Refurbished |
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Converted from air start to electric start (self-contained) |
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| Currently out of annual. Can be sold with a fresh annual. |
| Aircraft subject to prior sale. All times and specifications subject to verification by Buyer. © 2010 |
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General Information
Gross Weight......................................9,350 lbs
Max Landing Weight...........................7,850 lbs
Engine thrust....................................4,250 lbs
Fuel Capacity.....................445 gal / 3,000 lbs
Ceiling.........................................48,000 feet
Takeoff speed.............................. 135 knots
Gear operating speed.................... 250 knots
Flap operating speed...................... 200-300 kts
Never exceed speed........................... 1.3 mach
Maximum cruise speed....................... 500 knots
Maximum drag-chute deployment spd....160 knots
Maximum air brake speed.............. no restriction
G-limits..........................................+7 & -2.5
360 degree roll...........................under 1 second
Fuel burn....................................150-300 gal/hr
Maximum range...........................1,150 st. miles
Sea level TO to 10K ft, with full fuel.... 2.5 minutes
Normal climb speed............................350 knots
Maximum climb rate................10,000 ft / minute
Gross Weight......................................9,350 lbs
Max Landing Weight...........................7,850 lbs
Engine thrust....................................4,250 lbs
Fuel Capacity.....................445 gal / 3,000 lbs
Ceiling.........................................48,000 feet
Takeoff speed.............................. 135 knots
Gear operating speed.................... 250 knots
Flap operating speed...................... 200-300 kts
Never exceed speed........................... 1.3 mach
Maximum cruise speed....................... 500 knots
Maximum drag-chute deployment spd....160 knots
Maximum air brake speed.............. no restriction
G-limits..........................................+7 & -2.5
360 degree roll...........................under 1 second
Fuel burn....................................150-300 gal/hr
Maximum range...........................1,150 st. miles
Sea level TO to 10K ft, with full fuel.... 2.5 minutes
Normal climb speed............................350 knots
Maximum climb rate................10,000 ft / minute