Table of Contents
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N97HD
TABLE OF CONTENTS
1.
AIRCRAFT GENERAL INFORMATION ..................................2
2.
OPERATING LIMITATIONS .....................................................2
3.
DIMENSIONS AND SPECIFICATIONS: ..................................3
...............................................................................................3
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DIMENSIONS:
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CHECKLISTS ..............................................................................4
4.
5.
FLIGHT TEST PROGRAM.........................................................5
6.
MINIMUM EQUIPMENT LIST ..................................................5
7.
AIRCRAFT and SYSTEMS DESCRIPTION..............................6
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..................................................................................11
8.
FORMS.......................................................................................13
9.
CENTIGRADE TO FAHRENHEIT CONVERSION................14
10.
WEIGHT AND BALANCE ...................................................15
..............................................................3
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Summary of Contents for Avid Technology SPEEDWING MKIV
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Page 1: Table Of Contents
TABLE OF CONTENTS AIRCRAFT GENERAL INFORMATION ........2 OPERATING LIMITATIONS .............2 DIMENSIONS AND SPECIFICATIONS: ........3 FLIGHT MANUAL ....................3 POWER: ..................3 DIMENSIONS: ....................3 WEIGHT: AVID SPEEDWING ...................3 WING LOADING: ...................3 LOAD FACTORS: ..............3 CENTER OF GRAVITY LIMITS: N97HD .....................3 RIGGING: ..................3 FUEL CAPACITY: ................3 OPERATING SPEEDS ..............3... -
Page 2: Aircraft General Information
AIRCRAFT GENERAL INFORMATION OPERATING LIMITATIONS AVID MK4 Speedwing Aircraft flight characteristics are similar to the flight characteristics of THESE OPERATING LIMITATIONS SHALL BE ACCESSIBLE TO THE PILOT other Standard Category aircraft. EXPERIMENTAL OPERATING LIMITATIONS Aeronautical skill and knowledge required to obtain FAA issued Private Pilot class license is sufficient, and required, for the operation of the Avid Mk4 aircraft. -
Page 3: Dimensions And Specifications
DIMENSIONS AND SPECIFICATIONS: RIGGING: POWER: Flaperon Travel 15 deg. Max DOWN Engine Jabiru 2200 Elevator Travel 30 deg. UP, 17 deg. DOWN Power 80 hp Aileron Travel deg. UP, deg. DOWN Power Loading (with 80 HP) (1050 lbs.) 13.13 lb/HP Trim Tab Travel deg. -
Page 4: Checklists
CHECKLISTS PREFLIGHT EXTERIOR CHECK AFTER LANDING Check controls Flaps “UP” Switches off Strobe “OFF Check engine oil Exhaust pipe covers removed Check tire inflation and tread Check wing pins installed and safetied ENGINE SHUTDOWN Fuel tank vent clear Radio “OFF” Lift strut attach bolt tights and safetied. -
Page 5: Flight Test Program
MINIMUM EQUIPMENT LIST FLIGHT TEST PROGRAM GENERAL A Flight Test program has been developed for AVID IV N97HD. This program is fully documented in a document entitled “Flight Test Protocol”. The program consists of the following This Minimum Equipment List is to be used prior to flight to determine if this aircraft is steps: legal to fly with one or more components inoperative. -
Page 6: Aircraft And Systems Description
Pistons are General Motors aftermarket re-machined to include a piston pin circlip groove. They are fitted with 3 rings, the top rings being cast iron to complement the chrome molybdenum AIRCRAFT and SYSTEMS DESCRIPTION cylinder bores. Valves are 7mm (stem dia) which are purpose manufactured for the Jabiru engine. - Page 7 Displacement 2210cc Bore 97.5mm Stroke 74mm Compression Ratio Rotation of Prop Shaft Clockwise - Pilot's View – Tractor 60kg (132lb) inc. Exhaust, Carburetor, Starter Motor, Alternator Ramp Weight & Ignition System & Accessory pack. Ignition Timing fixed @ 25° BTDC Firing Order 1-3-2-4 DC Output...
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Page 8: Propeller
CARBURETOR The Bing pressure compensating carburetor is mounted at the rear of the engine. There is no The magneto switches are located to the left of the master switch. The engine starter solenoid mixture control and the carburetor automatically adjusts for altitude. is located at the front of the firewall on the passenger side and is activated by a momentary push button switch. - Page 9 pushbuttons are push-push switches that alternately lock in when pushed and then release Pressing [RST] stops the timer if it was running and resets it to 0.0. when pushed again. Pressing [PRE] stops the timer and sets it to the preload value of 60 mins Pressing [ 10] will add ten minutes to the value shown.
- Page 10 Pressing [PRE] sets the fuel quantity to the preload value which is set at 18 Gallons. reduce the possibility of an intermittent alarm, the unit will not activate the alarm for most Pressing [10], [1] or [.1] will add that respective value of gallons to the value shown. functions unless the function has been continuously out of limits for 5 seconds.
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Page 11: Transponder
TRANSPONDER is first turned on there is no backlighting. Pressing the ON key multiple times cycles through the low level backlighting to high level backlighting to no backlighting The aircraft is equipped with a Microair Avionics T2000SFL transponder. Operation of the TURNING OFF The T2000 is turned off by holding down the ON Key. - Page 12 pressing the ENTER key, the display will typically give the message SAVED for a short period. Buffer Altitude The user can input a buffer altitude, above and below the assigned altitude, to define a height band in which to fly. When the aircraft exceeds the upper or lower limit, an indicator alert message will be TOGGLE KEY This key acts as a TOGGLE switch, exchanging the active and standby codes.
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Page 13: Forms
FORMS SQUAWK and OPEN ITEMS LIST - N97HD OIL CONSUMPTION LOG - N97HD DATE HOBBS ITEM CLEARED DATE HOBBS QTS. ADDED... -
Page 14: Centigrade To Fahrenheit Conversion
CENTIGRADE TO FAHRENHEIT CONVERSION °C to °F °F to °C (°C x 9/5)+32 = °F (°F-32)/(9/5) = °C °C °F 0=32 100=212 200=392 300=572 400=752 600=1112 800=1472 10=50 110=230 210=410 310=590 420=788 620=1148 820=1508 20=68 120=248 220=428 320=608 440=824 640=1184 840=1544 30=86 130=266... -
Page 15: Weight And Balance
WEIGHT AND BALANCE Avid Aircraft MK IV Weight and Balance Calculations Gross Weight 1050 Lbs. CG Limits Forward- 11.19 Aft- 16.5 EMPTY WEIGHT Weight Moment Left Wheel 20.50 4161.50 Right Wheel 20.50 4305.00 Nose Wheel -19.00 -3059.00 Ballast 226.00 5633.50 9.78 Most Forward CG Weight...
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