Propiedades Psicométricas del Trait Meta-Mood Scale (TMMS ...
A-29 scale plan
5
N P R S T UVXWYZ AB AC AD B C D E F G J H K L M A B CD E F G H J K L M N P R S T U V X W Y Z AB AC AD A Drawings by Felipe Canuto Miranda
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Plano em escala do Tucano A-29
Transcript of A-29 scale plan
DESTRAVAR
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PRESSURE REFUELLINGCONTROL PANEL
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B C D E F G H J K L M N P R S T U V X W Y ZAB
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A
Drawings by Felipe Canuto Miranda
4,66 m15ft 3in
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DRAINFUSELAGE TANK
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ATENÇÃO:
NO SOLO, CERTIFIQUE-SE QUE O PINO DESEGURANÇA DA TRAVA DO TREM DE POUSOESTEJA INSTALADO
PRESSÃO DEENCHIMENTO DO PNEU121 +/- 3 PSI
WARNING:
ON GROUND BESURE THAT THE SAFETY PINOF LANDINGGEAR LOCK IS INSTALLED
TIRE INFLATION PRESSURE121 +/- 3 PSI
INFLATE TIRES WITH NITROGENONLY (SEE A.M.M. 12-13-05)
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NO SOLO, CERTIFIQUE-SE QUE O PINO DESEGURANÇA DA TRAVA DO TREM DE POUSOESTEJA INSTALADO
PRESSÃO DEENCHIMENTO DO PNEU121 +/- 3 PSI
WARNING:
ON GROUND BESURE THAT THE SAFETY PINOF LANDINGGEAR LOCK IS INSTALLED
TIRE INFLATION PRESSURE121 +/- 3 PSI
INFLATE TIRES WITH NITROGENONLY (SEE A.M.M. 12-13-05)
ATENÇÃO:
A PORTA FECHA HIDRAULICAMENTE QUANDOO TREM DE POUSO É RECOLHIDO
NO SOLO, CERTIFIQUE-SE QUE O PINO DESEGURANÇA DA TRAVA DO TREM DE POUSOESTEJA INSTALADO
PRESSÃO DE ENCHIMENTO DO PNEU121 +/- 3 PSI
WARNING:
DOOR HIDRAULICALLY CLOSES WHENLANDING GEAR IS RETRACTED
ON GROUND BE SURE THAT THE SAFETY PINOF LANDING GEAR LOCK IS INSTALLED
TIRE INFLATION PRESSURE121 +/- 3 PSI
INFLATE TIRES WITH NITROGENONLY (SEE A.M.M. 12-13-05)
ANTES DO REBOQUE DESCONECTAR A TESOURA DO TREM
BEFORE TOWNING DESCONECT THE TORQUE LATCH
36 ft 55 in11,14 m
7ft 81 in2,38 m
Rear view
11,30 m37 ft 7 in
3,97 M13 ft 02 in
3,76 m12 ft 34 in
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DIMENSIONS
PERFORMANCE
STRUTURE
PROPULSION
Wingspan : 11.14 mLength : 11.30 mHeight: 3.97 m
Empty Weight : 3200 kgMaximum takeoff : 5400 kgMaximum combat load : 1550 kg ( external cargo / ammunition )Crew: 1 pilot in single-seater or 2 ( 1 pilot + 1 systems operator / cadet) in two seaters
Maximum level speed : 590 km / h (clean )Cruising speed : 520 km / hStall speed : 148 km / hShuttle Range : 1445 km ( internal fuel ) and 2855 km (with external tanks )Service ceiling : 10,665 mAutonomy: 3.4 h ( internal fuel ) and 8.4 h (with external tanks )Combat radius : 550 km ( Hi- Lo - Hi)Distance from takeoff / landing : 900 m / 860 m
Load factors : +7 G / G -3.5Pressurization : 5 psiFatigue life : 12,000 h (typical combat) and 18,000 h (typical training )Windshield : Impact-resistant birds of 1.8 kg at 555 km / h
Motor : 1 turboprop Pratt & Whitney Canada PT6A - 68C with 1,600 shp power ,that incorporates FADEC (digital motor control with full authority ) and EICAS( engine indication system and alert the crew) 19Propeller: 1 Hartzell Propeller five blades with 2.38 m in diameter
