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FLIGHT MANUAL 

AVID SPEEDWING 

N97HD 

 

 

 

 

 

 

 

 

 

 

 TABLE OF CONTENTS

 

1. 

AIRCRAFT GENERAL INFORMATION ..................................2 

2. 

OPERATING LIMITATIONS .....................................................2 

3. 

DIMENSIONS AND SPECIFICATIONS: ..................................3 

POWER:

...............................................................................................3 

DIMENSIONS:

.......................................................................................3 

WEIGHT:

..............................................................................................3 

WING LOADING:

...................................................................................3 

LOAD FACTORS:

...................................................................................3 

CENTER OF GRAVITY LIMITS:

................................................................3 

RIGGING:

.............................................................................................3 

FUEL CAPACITY:

..................................................................................3 

OPERATING SPEEDS

..............................................................................3 

PERFORMANCE INFORMATION:

..............................................................3 

4.

 

CHECKLISTS ..............................................................................4 

5. 

FLIGHT TEST PROGRAM .........................................................5 

6. 

MINIMUM EQUIPMENT LIST ..................................................5 

7. 

AIRCRAFT and SYSTEMS DESCRIPTION ..............................6 

GENERAL

..............................................................................................6 

ENGINE

................................................................................................6 

PROPELLER

.........................................................................................8 

FUEL SYSTEM

......................................................................................8 

ELECTRICAL SYSTEM

...........................................................................8 

PITOT and STATIC SYSTEM

.....................................................................8 

AVIONICS

............................................................................................8 

ENGINE MONITOR

................................................................................8 

TRANSPONDER

..................................................................................11 

8. 

FORMS.......................................................................................13 

OIL CONSUMPTION LOG - N97HD

..........................................................13 

SQUAWK and OPEN ITEMS LIST -  N97HD

................................................13 

9. 

CENTIGRADE TO FAHRENHEIT CONVERSION................14 

10. 

WEIGHT AND BALANCE ...................................................15 

 

Summary of Contents for SPEEDWING MKIV

Page 1: ...3 FUEL CAPACITY 3 OPERATING SPEEDS 3 PERFORMANCE INFORMATION 3 4 CHECKLISTS 4 5 FLIGHT TEST PROGRAM 5 6 MINIMUM EQUIPMENT LIST 5 7 AIRCRAFT and SYSTEMS DESCRIPTION 6 GENERAL 6 ENGINE 6 PROPELLER 8 FU...

Page 2: ...aphical area 25 NAUTICAL MILE RADIUS OF TRACY AIRPORT TRACY CA 3 No operations including takeoffs and landings shall be conducted over densely populated areas or in congested airways except at those a...

Page 3: ...dder Travel deg RIGHT deg LEFT Wing Angle of Incidence deg Stabilizer Angle of Incidence deg Wing Washout Geometric Twist 1 5 inches at tip Wing Dihedral deg FUEL CAPACITY Wing Tank 17 gallons Right w...

Page 4: ...idle Choke on PULL if OAT below 5 degree C Both magneto switches on BEFORE TAKEOFF Check brakes Engine run up RPM to 1600 Mag check RPM to 1000 idle check Altimeter set Trim set for takeoff Oil temp...

Page 5: ...0 Degree Bank at MGW mid CG 26 Service Ceiling 6 MINIMUM EQUIPMENT LIST GENERAL This Minimum Equipment List is to be used prior to flight to determine if this aircraft is legal to fly with one or more...

Page 6: ...etween each big end it therefore does not have flying webs 48mm main bearings are also of the automotive slipper type Thrust bearings are located for and aft of the front double bearing allowing eithe...

Page 7: ...Phase Power Rating 60kw 80hp 3300rpm Fuel Consumption Cruse power 0 46 lbs per horsepower hour 274 grams Kw hour at cruse power Fuel AVGAS 100 130LL Oil AeroShell W100 or 15W50 or equivalent aircraft...

Page 8: ...To reset the circuit breaker simply push in the reset button It may be necessary to allow approximately two minutes for cooling before resetting a circuit breaker Corrective action should be taken in...

Page 9: ...smallest time division is one tenth of a minute or six seconds Pressing RST stops the timer if it was running and resets it to 0 0 Pressing PRE stops the timer and sets it to the preload value of 60 m...

Page 10: ...he SIL VOLT pushbutton is held in the clock portion of the display indicates the time to fuel exhaustion in hours and 1 10 s The endurance is calculated using the amount of fuel remaining and the fuel...

Page 11: ...e T2000 is turned off by holding down the ON Key The word SHUT DOWN is displayed and the T2000 counts down from 3 then turns off If the ON Key is lifted before the count is finished the T2000 returns...

Page 12: ...ert Tone option Rotate CODE SELECT knob scroll lower line to select ON or OFF The default is ON ENTER KEY The ENTER key is a confirmation key used to confirm information the user has input After press...

Page 13: ...13 8 FORMS OIL CONSUMPTION LOG N97HD DATE HOBBS QTS ADDED SQUAWK and OPEN ITEMS LIST N97HD DATE HOBBS ITEM CLEARED...

Page 14: ...8 320 608 440 824 640 1184 840 1544 30 86 130 266 230 446 330 626 460 860 660 1220 860 1580 40 104 140 284 240 464 340 644 480 896 680 1256 880 1616 50 122 150 302 250 482 350 662 500 932 700 1292 900...

Page 15: ...t Forward CG Weight Arm Moment CG Aircraft 576 9 78 5633 50 Pilot 170 16 00 2720 00 Fuel 0 5 3 15 00 45 00 749 8398 50 11 21 Most Aft CG Weight Arm Moment CG Aircraft 576 9 78 5633 50 Pilot 170 16 00...

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