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TECHNICAL SPECIFICATION

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nakamura@skynet-1.com‚Ü‚ÅB

‹@‘̔Ԇ DESIGNATION

§Ž®–¼Ì TYPE NUMBER
’ÊÌ NICKNAME
ÝŒv DESIGN AND MANUFACTURER
‹@Ží—p“r DUTY
Œ^Ž® TYPE
‰†Š®¬ PROTOTYPE
¶ŽY PRODUCTION QUANTITY
æˆõ CREW
”­“®‹@ ENGINE
–¼Ì MODEL
Œ^Ž® TYPE AND CYLINDERS
Šî” NUMBER
’¼Œa DIAMETER
‘S’· LENGTH
d—Ê WEIGHT
—£¸o—Í TAKE OFF POWER
ŒöÌo—Í NORMAL POWER
퓬o—Í MILITARY POWER

ƒvƒƒyƒ‰ PROPELLER
–¼ÌŒ^Ž® MODEL AND TYPE
ãÀ” NUMBERS OF BLADE
’¼Œa DIAMETER
ƒsƒbƒ` PITCH SETTING
d—Ê WEIGHT

‘S‘Ì GENERAL
‘S• SPAN
‘S’· OVER ALL LENGTH
‘S‚ OVER ALL HEIGHT
…•½ HORIZONTAL ATTITUDE
‚R“_ TAIL DOWN

Žå—ƒ WING
‘S• SPAN
–ÊÏ AREA
•tªŒ·’· CHORD AT ROOT
—ƒ’[Œ·’· CHORD AT TIP
Œã‘ÞŠp SWEPT ANGLE
㔽Šp DIHEDRAL
Žæ•tŠp INCIDENCE
€‚艺‚° TWIST DOWN
c‰¡”ä ASPECT-RATIO
‹ó—Í“I•½‹Ï—ƒŒ· M. A. C.iMEAN AERODYNAMIC CHORDj
—ƒ’f–Ê AIRFOIL SECTION

•â•—ƒ AILERON
• SPAN
•tªŒ·’· CHORD AT ROOT
—ƒ’[Œ·’· CHORD AT TIP
–ÊÏ AREA
ì“®Šp RANGE OF MOVEMENT

ƒtƒ‰ƒbƒv FLAP

ő匷’· MAX. CHORD
–ÊÏ AREA
Å‘åŠJŠp“x MAX. MOVEMENT

…•½”ö—ƒ HORIZONTAL STABILIZER
• SPAN
ő匷’· MAX. CHORD
ˆÀ’è”–ÊÏ STABILIZER AREA
¸~‘Ç–ÊÏ ELEVATOR AREA
Œv TOTAL AREA
Žæ•tˆÊ’u SETTING POSITION
Žæ•tŠp INCIDENCE
ì“®Šp RANGE OF MOVEMENT@@@ã@UP@‰º@DOWN

‚’¼”ö—ƒ FINCVERTICAL STABILIZER
‚‚³ HEIGHT
ő匷’· MAX. CHORD
ˆÀ’è”–ÊÏ VERTICAL STABILIZER AREA
•ûŒü‘Ç–ÊÏ RUDDER AREA
Œv TOTAL AREA
Žæ•tŠp SETTING ANGLE
ì“®Šp MOVEMENT@@@¶@LEFT@‰E@RIGHT

“·‘Ì FUSELAGE
‘S’· OVER ALL LENGTH
Å‘å‚ MAX. HEIGHT
Å‘å• MAX. WIDTH

~’…‘•’u LANDING GEAR
ŽÔ—ÖŠÔŠu WHEEL TRACKiTREADj
ŽÔ޲ŠÔŠu WHEEL BASE
ŽåŽÔ —Ö MAIN WHEEL
”ö—Ö TAIL WHEEL
‚R“_ÃŽ~Šp THREE POINT ANGLE STATIC LOADED

•‘• ARMAMENT
‹@e GUNS
”š’e BOMBS

–³ü RADIO
”R—¿ FUEL
ƒ^ƒ“ƒN FUEL TANK CAPACITIES
ŠŠ–û OIL
ƒ^ƒ“ƒN OIL TANK CAPACITIES
d—Ê WEIGHT
ީd BASIC WEIGHT
‘S”õd—Ê GROSS WEIGHT
‰ß‰×d—Ê OVER LOAD WEIGHT
ő嗣—¤ MAX. TAKE-OFF WEIGHT

ӊ RATIO
—ƒ–ʉ×d WING LOADING
”n—͉×d POWER LOADING

«”\ PERFORMANCE
ő呬“x MAX. SPEED
„q‘¬“x CRUISING SPEED
’…—¤‘¬“x LANDING SPEED
㸎žŠÔ CLIMB TIME
ŽÀ—p㸌À“x SERVICE CEILING
q‘±‹——£ RANGE