Van’s Aircraft RV-4

Pilot’s Operating Handbook

 

 

PERFORMANCE – SPECIFICATIONS

SPAN: ……………………………………………………………….. 23’ 0"

LENGTH: ……………………………………………………………. 19’ 9"

HEIGHT: ……………………………………………………………. 6’ 8"

SPEED:

Maximum at Sea Level …………………………………….. 173 Knots

Cruise, 75% Power at 8,000 Ft …………………………….. 165 Knots

RANGE (includes 3 gal. for taxi, takeoff & climb):

75% @ 8000’ , no reserve .…………………………………. 695 nm

55% @ 8000’ no reserve ….………………………………. 840 nm

75% @ 8000’, one hour (8 gal) reserve …………………….. 540 nm

55% @ 8000’, one hour (8 gal) reserve …………………….. 650 nm

RATE OF CLIMB AT SEA LEVEL ……………………@1650lbs 1600 FPM

SERVICE CEILING …………………………………………..……. 19,500 FT

TAKEOFF PERFORMANCE: ……………. ……………….……… 535 Ft

LANDING PERFORMANCE: ………………..…………….……… 500 Ft

STALL SPEED (CAS):

Flaps Up, Power Off ……………………………………… 47 Knots

Flaps Down, Power Off …………………………………… 43 Knots

MAXIMUM WEIGHT (Normal Category): …………………………. 1800 Lbs

EMPTY WEIGHT …………………………………………………. 1131 Lbs

MAXIMUM USEFUL LOAD: …………………………………….. 669 Lbs

BAGGAGE ALLOWANCE ………( see Weight and Balance )……… 50 Lbs

WING LOADING (Pounds/ Sq. Ft) ………………………………… 15

POWER LOADING (Pounds/ HP) …………………………………. 10.3

FUEL:

Capacity …………………………………………………… 36 Gal Total

Type ………………………………………………………. 100 LL

OIL CAPACITY ……………………………………………………. 8 Qts

ENGINE: Lycoming ……………………………………………….. O-320-B2C

PROPELLER: Sensenich ……… 70CM 7S16-0-79

NOTE - Prop limitation 2600 rpm

AIRSPEED LIMITATIONS

 

SPEED

KIAS

REMARKS

VNE

Never Exceed Speed

182 Kts

Do not exceed this speed in any operations.

VNO

Maximum Structural Cruising Speed

156 Kts

Exceed this speed only in smooth air.

Maneuvering Speed

115 Kts

Do not make full control movements above this speed. Full elevator deflection will result in a 6g load at this speed.

VFE

Maximum Flap Extended Speed

96 –20 deg
87 -
Full

Do not exceed this speed with flaps down

Vy

Best Rate of Climb

75 Kts

Vx

Best Angle of Climb

65 Kts

Vs

Stall Speed Clean

47 Kts

Vso

Stall Speed Landing Configuration

43 Kts

AIRSPEED INDICATOR MARKINGS

MARKING

KIAS VALUE OR RANGE

SIGNIFICANCE

White Arc

43 – 87 Kts

Full Flap Operating Range. Lower limit is Vso. Upper limit is maximum speed with flaps extended

Green Arc

47 – 156 Kts

Normal Operating Range. Lower limit is Vs. Upper limit is maximum structural cruising speed

Yellow Arc

156 – 182 Kts

Operations must be conducted with caution and only in smooth air.

Red Line

182 Kts

Maximum speed for all operations

 

N 4 1 R V

 

 

 

 

 

 

 

AEROBATIC INFORMATION

 

Weight Limitation – 1375 Pounds

Recommended Entry Speeds:

Loops, Horizontal Eights …. 120 – 165 Kts

Immelman Turns ………….. 130 – 165 Kts

Aileron Rolls, Barrel Rolls .. 105 – 165 Kts

Snap Rolls………………….. 70 – 95 Kts

Vertical Rolls ……………… 155 –165 Kts

Split-S …………………….. 85 - 95 Kts

 

 

 

N 4 1 R V

PREFLIGHT INSPECTION

1. CABIN

  1. Documentation -- Available In Airplane
  2. Aeronautical Charts – CURRENT AND APPROPRIATE TO FLIGHT
  3. Seat Belt Securing Control Stick -- RELEASE
  4. Ignition Switch -- OFF
  5. Avionics -- OFF
  6. Master Switch -- ON
  7. Fuel Quantity -- CHECK QUANTITY
  8. Flaps – DOWN
  9. Master Switch -- OFF
  10. Carb Heat – COLD

 

2. EMPENNAGE

  1. Tail Tie-Down -- DISCONNECT
  2. Control Surfaces -- CHECK freedom of movement and security
  3. Static Sources (both sides of fuselage) –CHECK for blockage

 

3. RIGHT WING

  1. Aileron -- CHECK freedom of movement and security
  2. Flap -- CHECK security
  3. Nav igation Lights and Strobes - CHECK condition
  4. Wing Tie-Down -- DISCONNECT
  5. Main Wheel Tire -- CHECK for proper inflation
  6. Chock -- REMOVE
  7. Right Wing Tank – SUMP
  8. Fuel Quantity -- CHECK VISUALLY
  9. Fuel Filler Cap – SECURE

 

 

N 4 1 R V

 

 

5. NOSE

  1. Engine Oil Level -- CHECK, do not operate with less than 4 quarts
  2. Propeller and Spinner -- CHECK for nicks and security
  3. Cowl Hinge Pins – CHECK for security
  4. Air Inlet -- CHECK for restrictions
  5. Nose Wheel Tire -- CHECK for proper inflation
  6. Chock -- REMOVE
  7. Fuel Tank Vents -- CHECK for blockage
  8. Fuel Boost Pump – ON
  9. Gascolator – SUMP
  10. Fuel Boost Pump – OFF

 

6. LEFT WING

  1. Wing Tie-Down -- DISCONNECT
  2. Main Wheel Tire -- CHECK for proper inflation
  3. Chock -- REMOVE
  4. Left Wing Tank -- SUMP
  5. Fuel Quantity -- CHECK VISUALLY
  6. Fuel Filler Cap -- SECURE
  7. Pitot Tube Cover -- REMOVE and check for blockage
  8. Landing Light -- CHECK condition
  9. Nav igation Lights and Strobes - CHECK condition
  10. Aileron -- CHECK freedom of movement and security
  11. Flap -- CHECK security

 

N 4 1 R V

 

BEFORE STARTING ENGINE

  1. Preflight Inspection -- COMPLETE
  2. Seat Belts and Shoulder Harnesses -- ADJUST and LOCK
  3. Canopy -- DOWN
  4. Fuel Selector Valve -- DESIRED TANK
  5. Avionics and Electrical -- OFF
  6. Brakes -- SET
  7. Circuit Breakers -- CHECK IN
  8. Flaps -- UP

STARTING ENGINE

  1. Mixture -- RICH
  2. Carb Heat -- COLD
  3. Master Switch – ON
  4. Fuel Boost Pump -- ON
  5. Radio Master – ON Check Boost Pressure
  6. Radio Master OFF
  7. Prime -- AS REQUIRED (5 seconds = 3 Primes)
  8. Throttle -- OPEN approx 1/4"
  9. Propeller Area -- CLEAR
  10. Ignition Switch -- START
  11. Radio Master -- ON
  12. Engine Monitor -- Check
  13. Oil Pressure -- CHECK 25 psi at idle
  14. Fuel Boost Pump -- OFF

 

 

N 4 1 R V

BEFORE TAKEOFF

  1. Brakes -- SET
  2. Canopy -------- Main Latch -- SECURE
    -------- Secondary Latch -- SECURE
  3. Flight Controls -- FREE and CORRECT
  4. Flaps - UP
  5. Flight Instruments – SET
    Altimeter – CORRECT PRESSURE
    D/G – CORRECT HEADING
  6. Fuel Selector Valve -- DESIRED TANK
  7. Mixture -- RICH (below 3000’)
  8. Elevator and Aileron Trim – NEUTRAL( Elevator center of Green)
  9. Throttle -- 1700 RPM
    1. Magnetos -- CHECK (125 max drop, 50 differential)
    2. Suction – CHECK (5" Hg)
    3. Carb Heat -- CHECK for drop
    4. Engine Instruments -- CHECK
    5. Throttle -- IDLE
    6. Carb Heat -- COLD
  1. Radios – SET
  2. Transponder -- ALTITUDE
  3. Fuel Boost Pump -- ON

 

N 4 1 R V

 

TAKEOFF

NORMAL TAKEOFF

  1. Wing Flaps – UP
  2. Carb Heat – COLD
  3. Throttle -- FULL OPEN
  4. Elevator Control – LIFT NOSE WHEEL (at 55KIAS)
  5. Climb Speed -- 110 KIAS

SHORT FIELD TAKEOFF

  1. Wing Flaps – 10 Deg
  2. Carb Heat – COLD
  3. Brakes – APPLY
  4. Throttle – FULL OPEN
  5. Mixture – RICH (above 3000’ lean to obtain max RPM)
  6. Brakes – RELEASE
  7. Climb Speed – 80 KIAS (Vy)

ENROUTE CLIMB

  1. Airspeed – 110 - 130 KIAS
  2. Throttle – 25 in Hg, or full throttle
  3. Boost Pump – OFF at 1000 feet AGL
  4. Fuel Pressure – CHECK
  5. Mixture – LEAN above 5000’

CRUISE

  1. Throttle – 23 in Hg
  2. Prop – 2300 RPM
  3. Trim – ADJUST
  4. Mixture – LEAN to 50 deg F rich of peak

 

 

 

 

 

 

 

N 4 1 R V

 

POSTFLIGHT

AFTER LANDING

    1. Wing Flaps – UP
    2. Boost Pump – OFF
    3. Transponder – STANDBY

ENGINE SHUTDOWN

    1. Engine Monitor - CHECK flight time
    2. Avionics -- OFF
    3. Electrical – OFF
    4. Throttle – IDLE
    5. Mixture – IDLE CUT-OFF
      (After Engine Stops)
    6. Ignition – OFF
    7. Flaps – DOWN
    8. Master – OFF

SECURING AIRCRAFT

    1. Wheel Chocks – INSTALL
    2. Wing & Tail Tie-Down – INSTALL AS REQUIRED
    3. Pitot Tube Cover – INSTALL AS REQUIRED
    4. Cockpit – CLEAN AND SECURE
    5. Ignition Key – REMOVED
    6. Master and Electrical Switches – OFF

 

 

 

 

 

N 4 1 R V

 

 

ANNUAL CONDITION INSPECTION REPORT

HOURS: __________

MAKE: RV-4 SERIAL #: 1992

REGISTRATION #: N 4 1 R V DATE: ___________

DESCRIPTION : COMMENTS:

A. PROPELLER GROUP

1. Inspect spinner and back plate....

2. Inspect blades for nicks and cracks....

  1. Check for grease and oil leaks...

4. Check spinner mounting brackets....

5. Check propeller mounting bolts and safety....

6. Inspect hub parts for cracks and corrosion....

B. ENGINE GROUP

CAUTION: ground mags before working on engine

1. Remove engine cowl....

2. Clean and check cowling for cracks, distortion

and loose or missing fasteners....

3. Drain oil sump....

4. Clean suction oil strainer at oil change....

5. Clean pressure oil strainer or change full

flow oil filter element......

6. Check oil temp. sender for leaks

and security....

7. Check oil lines and fittings for leaks, chafing

security, dents and cracks....

8. Clean and check oil radiator cooling fins....

9. Fill engine with oil per lubrication chart...

10. Clean engine....

11. Check condition of spark plugs adjust gap....

12. Check ignition harness and insulators....

13. Check magneto points for proper clearance

maintain at .018 +- .006....

14. Check magneto for oil seal leaks....

15. Check breaker felt for proper lubrication....

16. Check distributor block for cracks, burned

areas or corrosion....

17. Check magnetos to engine timing....

18. Remove air filter and clean....

19. Drain carburetor and clean inlet line fuel

strainer....

20. Check condition of carburetor heat air door

and box....

21. Check intake seal for leaks and clamps for

tightness....

22. Clean screens in fuel pump....

23. Clean and check gascolator....

24. Inspect condition of fuel lines....

25. Check fuel system for leaks.....

26. Check electric fuel pump for operation.....

27. Check engine controls throttle, carb heat,

mixture, and prop....

28. Inspect exhaust stacks, connections, gaskets....

29. Inspect heat exchange and baffles....

30. Check breather tube for obstructions and

security....

31. Check crankcase for cracks, leaks, security

of bolts....

32. Check engine mounts for cracks and loose

mountings.......

33. Check all engine baffles....

34. Check firewall seals....

36. Check condition and tension of alternator

and drive belt....

36. Check condition of starter....

37. Check fluid in brake reservoir....

38. Lubricate all controls....

39. Reinstall engine cowl....

 

C. CABIN GROUP

1. Inspect canopy and windows....

2. Check upholstery for tears....

3. Check seats, seat belts, shoulder straps....

4. Check trim operation...

5. Check rudder pedals....

6. Check control column, systems and connection.....

7. Check landing, nav, cabin, and instrument

lights...

8. Check instrument, lines and attachments....

9. Check gyro operation, and electric turn

and bank....

10. Check or replace gyro air filter....

11. Clean or replace vacuum regulator filter....

12. Check altimeter....

13. Check operation of fuel selector valve....

14. Check operation of engine primer....

15. Check condition of heater controls....

16. Check condition and operation air vents....

  1. FUSELAGE AND EMPENNAGE GROUP

1. Remove inspection plates and panels...

2. Check battery box, battery and cables...

3. Check electronic installations....

4. Check bulkheads and stringers for damage...

5. Check antenna mounts and wiring....

6. Check fuel lines and valves....

7. Check vertical fin and rudder surfaces....

8. Check rudder horn and attachment....

9. Check vertical fin attachments....

10. Check rudder bolts for wear...

11. Check horizontal stabilizer and elevators...

12. Check horizontal stabilizer attachment...

13. Check elevator horn...

14. Check elevator bolts for wear...

  1. Check elevator bell cranks, controls and control tubes...

16. Lubricate all bearings as needed.....

17. Reinstall inspection plates and panels....

E. WING GROUP

1. Remove inspection plates...

2. Check surfaces and tip for damage and loose

rivets and condition of walkways....

3. Check aileron mounts and attachments....

4. Check aileron bellcrank and control tubes....

5. Check flaps and attachment for damages....

6. Check all wing attachment bolts....

7. Check fuel tanks and lines for leaks and....

8. Check fuel tank vents....

9. Reinstall inspection plates....

 

 

 

F. LANDING GEAR GROUP

1. Check nose gear....

2. Check main gear attachments...

3. Check tires for cuts and wear....

4. Remove wheel, clean, and repack bearings...

5. Check wheels for cracks, corrosion and broken

bolts....

6. Check tire pressure....

7. Check brake lining and disc....

8. Check brake lines....

G. OPERATIONAL INSPECTION

1. Check fuel pump and fuel tank selector....

2. Check fuel pressure....

3. Check oil pressure and temperature....

4. Check alternator output....

5. Check manifold pressure....

6. Check alternate air....

7. Check vacuum gauge....

8. Check gyros for noise and roughness....

9. Check Cabin heat operation....

10. Check magneto switch operation....

11. Check magneto RPM variation....

12. Check throttle and mixture operation....

13. Check propeller smoothness....

14. Check electronic equipment operation....

 

H. Known problem areas:

a) Smoking rivets on forward bottom skin

b) Chafing brake lines on gear leg fairing and beneath wheel pant

c) Chaffing of wheel on wheel pant

d) Fretting corrosion at gear leg fairing intersection

e) Corrosion of exposed rod end bearings

f) Rudder contacting elevator roots in flight (dynamic clearance less than

static clearance!)

NOTES

 

 

N 4 1 R V

 

 

Performance

Cruise Performance at 8,000’:

KTAS

RPM

MAP

Fuel Flow

% Power

170

2580

22"

8.4 GPH

75%

160

2300

21"

7.4 GPH

65%

No Wind Range at 8,000’:

One hour (8 gal.) reserve:

75% Power ……………………………………………….. 540 nm

65% Power ……………………………………………….. 575 nm

55% Power ……………………………………………….. 650 nm

No Reserve:

75% Power ……………………………………………….. 695 nm

65% Power ……………………………………………….. 745 nm

55% Power ……………………………………………….. 840 nm

 

 

N 4 1 R V

WEIGHT AND BALANCE DATA

Make: Philip Condon Model: RV-4

Serial: 1992 Registration: N 4 1 R V

Maximum Weights:

Aerobatic Category ………………………… 1375 Lbs

Utility Category ……………………………. 1650 Lbs

Normal Category …………………………… 1800 Lbs

Datum= 60 inches forward of wing leading edge (L.E.)

Design C.G. Range = 15% to 29% of wing chord

8.7" to 16.8" from L.E.

68.7" to 76.8" aft of Datum

Wing L.E. = 60 inches aft of datum

Main wheel right = 84.25" aft of datum

Main wheel left = 84.25" aft of datum

Nose wheel = 28.50" aft of datum

Fuel …………………… 70" aft of datum

Pilot and Passenger …… 87.4" aft of datum

Baggage ………………. 117" aft of datum

Aircraft weighed in level flight attitude.

(Includes 8 qts. of oil)

Weight Arm Moment

Right Wheel 450 84.25 37913

Left Wheel 490 84.25 41283

Nose Wheel 247 21.75* 5372

Fuel 56 70 (3920)

Total 1131 80647

Empty CG = 71.3 aft of datum

*Datum to Pivot , Fuel weighed separately

N 4 1 R V

 

WEIGHT AND BALANCE DATA

 

Sample:

Weight Arm Moment

Aircraft 1131 71.3 80647

Fuel (6lbs/gal) 70

Pilot 87.4

Passenger 87.4

Baggage 117

Total

 

CG = Total Moment / Total Weight

CG = in aft of datum

CG Range = 68.7 to 76.8 in aft of datum

N 4 1 R V

WEIGHT AND BALANCE DATA

*With a CG Range of 68.7 to 76.8 in., The following loading configurations are within limitations.

 

 

 

Pax, Full fuel, 70lbs bags

200# Pax, Full fuel, 40lbs bags

Item

Weight

Arm

Moment

Item

Weight

Arm

Moment

Empty Wt

1131

71.3

80640

Empty Wt

1131

71.3

80640.3

Pilot

200

84.25

16850

Pilot

200

84.25

16850

Passenger

170

84.25

14323

Passenger

200

84.25

16850

Fuel

228

70

15960

Fuel

228

70

15960

Baggage

70

117

8190

Baggage

40

117

4680

TOTAL

1799

135963

TOTAL

1799

134980

CG

75.58

CG

75.03

Zero Fuel CG

76.39

Zero Fuel CG

75.76

No Pax, Full fuel, 100lbs bags

250# Pax, Full fuel, No bags

Item

Weight

Arm

Moment

Item

Weight

Arm

Moment

Empty Wt

1131

71.3

80640

Empty Wt

1131

71.3

80640.3

Pilot

200

84.25

16850

Pilot

200

84.25

16850

Passenger

0

84.25

0

Passenger

250

84.25

21062.5

Fuel

228

70

15960

Fuel *

219

70

15330

Baggage

100

117

11700

Baggage

0

117

0

TOTAL

1659

125150

TOTAL

1800

133883

CG

75.44

CG

74.38

Zero Fuel CG

76.3

Zero Fuel CG

74.99

* Reduced Fuel

 

 

N 4 1 R V

 

Engine Information

Model: …….. Lycoming O-320 B2C

HP: ………… 160

Fuel: ……….. 91/96 or 100/130 octane minimum

……….. 100LL

Oil Filter: ….. Champion CH48110

Alt Belt…….. NAPA XL 25 09403

Vac Pump Rapco 211CC

Vac Filter

OIL: Avg MIL-L-6082 Ashless Dispersant

Ambient Air Grades Grades

Above 80F SAE 60 SAE 60

Above 60F SAE 50 SAE 40 or SAE 50

30 – 90F SAE 40 SAE 40

0-70F SAE 20 SAE 30 or SAE 40

Below 10F SAE 20 SAE 30

Oil Sump Capacity …….. 8 U.S. Quarts

Minimum Safe Quantity ...2 U.S. Quarts

Operating Conditions:

Oil Inlet Temp: 180 deg F desired, 245 deg F Maximum

Oil Pressure: 90 psi max; 60 psi min; 25 psi idle

Fuel Pressure: 8 psi max; 0.5 psi min; 3.0 psi desired

Cyl. Head Temp 150 deg F – 435 deg F desired range, 500 deg F max

N 4 1 R V

 

ENGINE INFORMATION

 

 

 

N 4 1 R V

 

 

 

ENGINE INFORMATION

 

 

 

 

N 4 1 R V

 

 

 

ENGINE INFORMATION

 

 

N 4 1 R V

 

 

N 4 1 R V

 

Engine Information System

Parameter HI LO Aux Off Aux SF

Oil Pressure 45psi 0(Oil Zero)

Oil Temp 210F ----

Voltage ---- 11.8

Fuel Press ---- 2psi 93 33

RPM 2600

Manifold Press. ---- ---- 88 143

EGT 1500 ----

CHT 460 ----

EMP setting 1

Options setting +-Fec

Avionics

Component Make Model S/N

GPS/Com Terra

Transponder Terra

Encoder Ameriking AK350

ELT Ameriking AK450

Strobes Whelen

 

 

 

 

 

 

 

 

 

EMERGENCY PROCEDURES

AIRSPEEDS FOR EMERGENCY OPERATIONS

Engine Failure After Takeoff:

Wing Flaps Up ………………………… 80 Kts

Wing Flaps Down …………………….. 70 Kts

Maneuvering Speed (Va) ………………………. 115 Kts

 

Maximum Glide ………………………………… 80 Kts

 

EMERGENCY PROCEDURES

ENGINE FAILURES

ENGINE FAILURE DURING TAKEOFF RUN

  1. Throttle –IDLE
  2. Brakes – APPLY
  3. Wing Flaps – RETRACT
  4. Mixture – IDLE CUT-OFF
  5. Ignition Switch – OFF
  6. Master Switch – OFF

ENGINE FAILURE IMMEDIATELY AFTER TAKEOFF

  1. Airspeed – 70 KIAS
  2. Mixture – IDLE CUT-OFF
  3. Fuel Selector Valve – OFF
  4. Ignition Switch – OFF
  5. Wing Flaps – AS REQUIRED
  6. Master Switch – OFF

ENGINE FAILURE DURING FLIGHT

  1. Airspeed –80 Knots
  2. Boost Pump – ON
  3. Fuel Selector – SWITCH TANKS
  4. Carb Heat – ON
  5. Mixture – RICH
  6. Ignition Switch – BOTH, LEFT, RIGHT
  7. Transponder – 7700

 

 

 

 

 

 

 

 

 

 

 

 

 

EMERGENCY PROCEDURES

FIRES

DURING START ON GROUND

  1. Cranking – CONTINUE, to get a start which would suck the flames and accumulated fuel through the carb and into the engine.

If engine starts:

  1. Power – 1700 RPM for a few minutes
  2. Engine – SHUTDOWN and inspect for damage

If engine fails to start:

  1. Throttle – FULL OPEN
  2. Mixture – IDLE CUT-OFF
  3. Cranking – CONTINUE
  4. Fire Extinguisher – OBTAIN
  5. Engine – SECURE

ENGINE FIRE IN FLIGHT

  1. Mixture – IDLE CUT-OFF
  2. Fuel Selector Valve – OFF
  3. Master Switch – OFF
  4. Cabin Heat and Air – OFF

ELECTRICAL FIRE IN FLIGHT

  1. Master Switch – OFF
  2. Avionics – OFF
  3. All Other Switches (except ignition) – OFF
  4. Vents/ Cabin Air/ Heat – CLOSED
  5. Fire Extinguisher – ACTIVATE (if available)

CABIN FIRE

  1. Master Switch – OFF
  2. Vents/ Cabin Heat – CLOSED
  3. Fire Extinguisher – ACTIVATE (if available)

WING FIRE

  1. Nav Lights – OFF
  2. Landing Light – OFF

 

EMERGENCY PROCEDURES

ELECTRICAL / ALTERNATOR FAILURE

  1. Avionics –OFF
  2. Master Switch – OFF, both sides
  3. Master Switch – ON

IF ALTERNATOR IS STILL OFF-LINE:

  1. Master Switch – OFF
  2. Electrical Switches – OFF
  3. Alternator Breaker – PULL
  4. Avionics – OFF
  5. Main Feed Breaker – PULL
  6. Alternate Feed Switch Guard – UP
  7. Alternate Feed Switch – ON
  8. Avionics – ON as required
  9. Electrical Equipment – ON, as required
  10. Flight – TERMINATE as soon as practical, aircraft is on battery reserves only.