StormAircraft Rally Manual del propietario
Rally Pilot Operating Handbook
Copyright 2008, Rally Aircraft Revision 4.1 1
STORMAIRCRAFT
RALLY LSA
PILOT OPERATING HANDBOOK
Revision .1
Manufacturer: Stor Aircraft
Model: Rally
Aircraft Registration Nu ber:
N
Airfra e Serial Nu ber:
Date Purchased:
Rally Pilot Operating Handbook
Copyright 2008, Rally Aircraft Revision 4.1 2
Rally Pilot Operating Handbook
Copyright 2008, Rally Aircraft Revision 4.1 3
TABLE OF CONTENTS
SECTION TITLE PAGE
1.0 GENERAL 5
2.0 SYSTEM DESCRIPTIONS 11
3.0 LIMITATIONS 13
4.0 WEIGHT AND BALANCE 17
5.0 PERFORMANCE 23
6.0 EMERGENCY PROCEDURES 31
7.0 NORMAL PROCEDURES 41
8.0 HANDLING SERVICE AND MAINTENANCE 55
9.0 REQUIRED PLACARDS AND MARKINGS 59
10.0 SUPPLEMENTS 63
11.0 QUICK REFERENCE 65
NOTICE: This Pilot Operating Handbook has be designed to co ply with AC 23-
8B, Appendix 5, Effective 14 August 2003.
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SECTION 1.0
GENERAL
1.1 INTRODUCTION ............................................................................... 6
1.2 DESCRIPTIVE DATA .......................................................................... 6
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5.5 TAKE-OFF DISTANCE CHART
Take off Speed 32°F 32°F 50°F 50°F 70°F 70°F 85°F 85°F 100°F 100°F
Weight
Lift off
at 50 ft
Press.
Alt—ft.
A
B
A
B
A
B
A
B
A
B
GW:
1320 lbs .
5 Kts.
S.L. 300 558 348 626 404 797 488 1,011 601 1,346
1,000 342 622 400 792 480 1,004 586 1 328 709 1,701
2,000 393 779 468 997 581 1,308 703 1,671 876 2.058
3,000 464 986 571 1.302 686 1,656 851 2,025 1,401 2.,62
,000 557 1,295 680 1,642 837 2,008 1,098 2,431 1,129 2,899
5,000 668 1,627 824 1,988 1,075 2,405 1,361 2,862 1,619 3,343
6,000 815 1,973 1,046 2,380 1,333 2,827 1,586 3,315 1,943 3,921
7,000 1,027 2,358 1,303 2,807 1,565 3,281 1,911 3,859 — —
8,000 1,284 2,787 1,544 3,257 1,888 3,813 — — — —
55 KtS.
B = 50 ft Obstacle
Figure 5— 3, Take-off distance chart
Rally Pilot Operating Handbook
Copyright 2008, Rally Aircraft Revision 4.1 7
5.6 TIME, FUEL, AND DISTANCE TO CLIMB CHART (Maximum Rate of Climb)
Conditions: flaps up; full throttle (5500 RPM); standard te perature; zero wind.
Notes:
1) add 1 gal of fuel for engine start, taxi and takeoff
2) increase ti e, fuel and distance by 10% for each 46°F above standard
te p.
From sea level
Weight
(lbs.)
Pressure
Altitude
(feet)
Temp.
(°F)
Climb-
Speed
(knots)
Rate of
Climb
(fp )
Time
( in.)
Fuel
Used
(gal.)
Distance
(s )
SL 60 72 720 0 0 0
1,000 55 72 700 2 0.2 2.5
2,000 52 71 660 3 0.5 4.2
3,000 48 71 620 5 0.7 6.7
,000 44 70 580 7 1.0 9.0
GW: 5,000 41 70 530 9 1.3 11.5
1,320 6,000 37 69 480 11 1.6 15.0
7,000 34 69 425 14 1.9 18.0
8,000 30 68 375 17 2.3 21.0
9,000 26 68 315 20 2.7 26.0
10,000 23 67 275 23 3. 0 30.0
11,000 20 67 220 27 3.7 36.0
12,000 16 66 180 33 4.2 42.5
Time, Fuel and Distance to Climb Chart
Figure 5—4 Ti e, Fuel and Distance to Cli b Chart
Rally Pilot Operating Handbook
Copyright 2008, Rally Aircraft Revision 4.1 8
1.1 INTRODUCTION
Section 1 provides basic data and infor ation of general interest.
1.2 DESCRIPTIVE DATA
Engine:
• Nu ber of engines .................... 1
• Engine anufacturer ................. ROTAX
• Engine odel .........................… 912 UL S2
• Engine type .................………... nor ally aspirated, 4-cyl, 4-stroke, liquid/air
cooled engine with opposed cylinders, dry su p forced lubrication with separate
0,8 gal oil tank,
• 2 carburetors, echanical and electric fuel pu ps, Ducati electronic dual igni-
tion, electric starter, integrated reduction gear 1:2.43.
• Horsepower rating and engine speed ........... 100 BHP at 5800 RPM ( ax. 5 in.)
• 95 BHP at 5500 (continuous).
Detailed information on the ROTAX 912 ULS engine shall be found on the engine
Manufacturer’s operating manual.
Propeller:
• Nu ber of blades ........... 3
• Propeller type ................ Ground adjustable
• Propeller dia eter ......... 70 in.
Fuel:
• Nu ber of tanks ......................……………… 2 Wing leading-edge tanks
Oil:
• Oil tank capacity ............................................ 0.8 U. S. gallons
Maximum Aircraft Weights:
• Standard E pty Weight, Basic.......... 760 lbs
• Maxi u useful load …………………… 560 lbs (Ed: Does this change with s aller
tanks?)
Cabin and Entry Dimensions:
• Cabin Height: Top of seats to roof = 40 inches
• Doors: 34 inches wide X 39 inches high
• Length: Instru ent panel to rear bulkhead (baggage area) = 70 inches
Fuel Capacity U.S. Gallons
Total—Standard Tanks 24
Usable—Standard Tanks 23
Total—Long Range Tanks 35
Usable—Long Range Tanks 34
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Baggage Space Dimensions:
• Cabin width: (Door to Door) = 43.7 inches @ door handles
• Baggage Area:
Length = 26 inches.
Width = 28—42 inches at front edge.
Height = 27—32 inches.
Volu e = approx. 16 cu. ft.
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Copyright 2008, Rally Aircraft Revision 4.1 10
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