LN-LLT

 


Flyet er eigd av Oddvar Strand.

Aircraft Registration: LN-LLT
Kit Manufacturer and Model: Van’s Aircraft RV-6
Serial Number: 60005
Maiden Flight: 16. September 2006

 

FIREWALL FORWARD EQUIPMENT

Engine: America’s Aircraft Engines Eagle IV Titan Experimental Lycoming IO-360-A1A S/N 206045
Injection system: Airflow Performance Injection FM-200
Fuel Pump: Aero Accessories LW 15473 S/N AA20332
Magnetos:

Left:                      Unison Slick 4371 S/N 06040746
Right                     Unison Slick 4371 S/N 06040749

Maximum Power @ 2700 rpm

180 hp

Maximum Torque @ 2200 rpm

360 lb-ft

Max Power Loading

10.56 lb/hp)

 

 

Engine Mount (4):

Dynafocal

Thrust Line Incidence

Thrust Line Offset

1.25° right

 

 

Propeller

Hartzell HC-C2YK-1BF  S/N CH39885B

Propeller Pitch Range @ 75%R

12° to 38°

Prop Governor

MT Propeller P-420-3 S/N 031042

Starter

Sky-Tec 149-12LSX S/N F2LX-070623

Alternator

B&C L40 S/N 0611060

Voltage Regulator

B&C LR3C-14

S/N 0306802

Vacuum Pump

RAPCO RA211CC S/N 121563

Exhaust System

Vetterman  S/S Crossover

Oil Cooler

Stewart Warner 10599R

S/N 5417

 

EQUIPMENT

Fuel Boost Pump: Holley 12-815-1
Fuel Gauge (2): Van´s Aircraft Inc
Fuel pickup L: Stewart Warner 385 (no aerobatic)
Fuel pickup R: Stewart Warner 385 (no aerobatic)
Suction Regulator: Airborne 2H3-23 S/N 9AK
Suction Gauge: Varga Enterprises 5001
Trim Servo : MAC
Trim Servo Relay Deck: Ray Allen REL-1
Trim Indicator: Ray Allen RP3
Flap Motor: Motion Ind 85615-021
Engine Monitor: Rocky Mountain Instrument µMonitor
Fuel flow sensor: FloScan 201B
Fuel pressure sensor: VDO 360-043
Manifold Pressure Sensor: Wells SU129 #52-0003
Strobe/Position Light System: Wheelen S/N 01960, 04426, 04439
Attitude Gyro: R.C. Allen Instruments RCA 22-7
Directional Gyro: R.C. Allen Instruments RCA 11A-8
Altimeter: United Instruments 5934P-3 S/N 450745
Vertical Speed Indicator (VSI): Weston A720
Airspeed Indicator with speed limits: UMA
Pitot Tube, heated: Falcon Gauge 12-AN5812 S/N 07074
Compass  S.I.R.S Navigator Compass NV2C-12V
Autopilot / Needle & Ball: TruTrak Flight Systems    TruTrak I
Altitude Hold TruTrak Flight Systems: Altrak
Elevator Servo: TruTrak DSB-B S/N 207647
Aileron Servo TruTrak DSB-B-RV6   S/N 207353
Ignition Switch: ACS A-510-2
Brake Master Cylinder (2L/2R): Cleveland 10-30
Brake Caliper (2): Cleveland 30-9
Fuel Selector Valve: Andiair

INSTRUMENT READINGS
Manifold Pressure Range: 10 to 30 inHg
Engine Idle: 700 to 850 rpm
Mixture Lean Increase: 20 rpm
L/R Mag Drop @ 1800 rpm: <200 rpm
Exhaust Gas Temperature [Max]: 1200°F to 1400°F [1650°F]
Cylinder Head Temperature [Max]: 200°F to 435°F [500°F]
Fuel Pressure [Range]: 0 to 99 PSI [25 – 30 PSI]
Oil Pressure [Idle]: 65 to 95 PSI [>25 PSI]
Oil Temperature [Range]: 170 to 220°F [140 to 245°F]
Bus Voltage: 14 ± 0.2 VDC
Alternator Current: 5 to 40A
Gyro Suction: 5 ± 0.5 inHg
Cruise Fuel Flow: 7 to 11 gph
WOT Cruise Power Settings (Note: All figures are approximate)
REF = inHg + (rpm/100)

Power

%

GPH

Range (nm)

TAS (mph)

Alt (MSL)

55

7.5

660

150

16500

58

8.0

660

160

15000

62

8.5

660

170

13500

65

9.0

643

175

12000

69

9.5

625

180

10500

72

10.0

608

185

9000

75

10.5

590

190

7500

Airspeed Indicator Markings:

White Arc:      Bottom VS0 50 mph          Top VFE 103 mph
Green Arc:      Bottom VS1 54 mph          Top VNO: 180 mph
Blue Line:      VA 135 mph
Red Line:       VNE 210 mph

Takeoff Distance, Hard Surface (Gross weight)
10° Flaps, no Wind: 430 ft
To Clear 50 ft Obstacle:  630 ft

Landing Distance, Hard Surface
Flaps @ 45°, No Wind: 660 ft
To Clear 50 ft Obstacle: 1250 ft

Other limitations
Empty Weight: 1122 lb/ 509 kg
Utility Gross Weight (@+4.4/-3 g): 1800 lb
Utility Useful Load: 678 lb
Baggage Capacity: 100 lb max
Service Ceiling: 20,000 ft

Design Ultimate Load Factors @ Aerobatic Gross Weight:   +9/-6 g
Aerobatic Gross Weight (@+6/-4 g): 1410 lb
Aerobatic Useful Load: 289 lb

Never Exceed Speed (VNE): 210 mph
Maximum Direct Crosswind Component: 15 Knots
Prop Restriction: Avoid continuous operation from 2000 - 2250 rpm
Engine Redline: 2700 rpm
Fuel Capacity: 36 US gal Usable

THIS AIRCRAFT IS APPROVED FOR POSITIVE G AEROBATIC OPERATIONS.

INTENTIONAL SPINS ARE NOT RECOMMENDED, AS AIRSPEED TENDS TO BUILD RAPIDLY IN THIS AIRCRAFT.


LN-LLT cockpit

Aerobatics.

Entry speeds for various aerobatic maneuvers are as follows:

Loops, horizontal eights:                        140 to 190 mph
Immelmann turns                                   150 to 190 mph
Aileron and Barrel Rolls                         120 to 190 mph
Snap rolls (not recommended)              80 to 110 mph
Vertical Rolls                                            180 to 190 mph
Split-S                                                        100 to 110 mph

 

LN-LLT




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