Vans Aircraft RV-4
Pilots 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 |
|
|
V NE |
Never Exceed Speed |
182 Kts |
Do not exceed this speed in any operations. |
|
V NO |
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. |
|
V FE |
Maximum Flap Extended Speed |
96 20 deg87 - 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
2.
EMPENNAGE
3.
RIGHT WING
N 4 1 R V
5
. NOSE
6.
LEFT WING

N 4 1 R V
BEFORE STARTING ENGINE
STARTING ENGINE
N 4 1 R V
BEFORE TAKEOFF
N 4 1 R V
TAKEOFF
NORMAL TAKEOFF
SHORT FIELD TAKEOFF
ENROUTE CLIMB
CRUISE
N 4 1 R V
POSTFLIGHT
AFTER LANDING
ENGINE SHUTDOWN
SECURING AIRCRAFT
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....
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. 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...
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
ENGINE FAILURE IMMEDIATELY AFTER TAKEOFF
ENGINE FAILURE DURING FLIGHT
EMERGENCY PROCEDURES
FIRES
DURING START ON GROUND
If engine starts:
If engine fails to start:
ENGINE FIRE IN FLIGHT
ELECTRICAL FIRE IN FLIGHT
CABIN FIRE
WING FIRE
EMERGENCY PROCEDURES
ELECTRICAL / ALTERNATOR FAILURE
IF ALTERNATOR IS STILL OFF-LINE: