N506RV
Enclosed is the POH that I developed during the flight testing of my RV-6A. It is roughly based on a typical Cessna POH, with modifications specific to an RV. There are also specific references to my tail number and equipment installed in my RV-6A. For this POH to be useful, you must tailor it to your specific aircraft. The tail number can easily be changed with a search and replace. Other modifications will take longer, such as references to the trike, tip-up canopy, C/S prop, RMI engine monitor, internal ski rack, etc.
Most performance figures (fuel flow, endurance, speed, ROC, glide performance, etc) were obtained from actual flight test data.
I found it beneficial to print the checklists separately and use them during the preflight (pages 7-13, 23-26). This document is best used when printed on a color printer. The 8 ½” X 11” paper should be cut to the proper size after printing.
The Annual Condition Inspection was taken from the RV-List. I think it was originally written by George Orndorff. The Van’s Airforce logo was downloaded from the Internet and I have no idea of the original artist. If George, or the designer of the logo, objects to these being included in the POH, I will remove them from all further distributions.
This POH can be considered “freeware”. It is distributed free of charge. You may pass it on to anyone else as long as this title page remains intact.
This manual was first posted online in the fall of 1997. Since then, it appears that it has been used as a template for many additional manuals that have also been published. If anyone copies information from this manual and then republishes it, I ask that you include a cover page indicating what data has been copied. This manual covers the performance of a 160 HP RV-6A. When these new manuals are then used by a third party, that person will not be able to know what information has been copied, and what was obtained from actual flight test. My goal is to ensure the sharing of ACCURATE data.
I am not a technical writer and make no warrantee as to the accuracy of the information contained in the enclosed document. You MUST review, modify and be comfortable with the enclosed information PRIOR to using it as a preflight/ inflight reference. Due to the nature of homebuilt aircraft, I feel it is impossible to develop one standard POH to cover all RV’s. Use the enclosed information at your own risk. If you don’t agree with this disclaimer, just delete this entire document and get on with your life.
This document is under constant revision. If anyone has any ideas on how it can be improved, please let me know. I hope this is of help to others.
Scott Gesele N506RV – Flying (1000 hrs)
sgesele@
Van’s Aircraft RV-6A
Pilot’s Operating Handbook
N506RV
PERFORMANCE – SPECIFICATIONS
SPAN: ……………………………………………………………….. 23’ 0”
LENGTH: ……………………………………………………………. 19’ 9”
HEIGHT:………………………………………………………………. 6’ 8”
SPEED:
Maximum at Sea Level …………………………………….. 180 Knots
Cruise, 75% Power at 8,000 Ft …………………………….. 167 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 …………………………….…. 2,050 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: ……………………...……………………. 1800 Lbs
EMPTY WEIGHT …………………………………………………. 1142 Lbs
MAXIMUM USEFUL LOAD: …………………………………….. 658 Lbs
BAGGAGE ALLOWANCE ………………………………………… 100 Lbs
WING LOADING (Pounds/ Sq. Ft) ………………………………… 15
POWER LOADING (Pounds/ HP) …………………………………. 10.3
FUEL:
Capacity …………………………………………………… 38 Gal Total
Type ………………………………………………………. 100 LL
OIL CAPACITY ……………………………………………………. 8 Qts
ENGINE: Lycoming ……………………………………………….. O-320-D1A
PROPELLER: Hartzell ……………………………………………. HC-C2YL-1BF
AIRSPEED LIMITATIONS
| |SPEED |KIAS |REMARKS |
|VNE |Never Exceed Speed |182 Kts |Do not exceed this speed in any |
| | | |operations. |
|VNO |Maximum Structural Cruising|156 Kts |Exceed this speed only in smooth air. |
| |Speed | | |
|VA |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 |Do not exceed this speed with flaps |
| | |87 - Full |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 |43 Kts | |
| |Configuration | | |
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 |
N506RV
N506RV
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
N506RV
PREFLIGHT INSPECTION
1. CABIN
a) Documentation -- Available In Airplane
b) Aeronautical Charts – CURRENT AND APPROPRIATE TO FLIGHT
c) Seat Belt Securing Control Stick -- RELEASE
d) Ignition Switch -- OFF
e) Avionics -- OFF
f) Master Switch -- ON
g) Engine Monitor – ON
h) Engine Monitor – RESET FLIGHT TIME
i) Fuel Quantity -- CHECK QUANTITY
-- VERIFY ENGINE MONITOR PRESET
j) Flaps – DOWN
k) Master Switch -- OFF
l) Carb Heat – COLD
2. EMPENNAGE
a) Tail Tie-Down – DISCONNECT
b) Rudder Gust Lock -- REMOVE
c) Control Surfaces -- CHECK freedom of movement and security
d) Static Sources (both sides of fuselage) –CHECK for blockage
3. RIGHT WING
a) Aileron -- CHECK freedom of movement and security
b) Flap -- CHECK security
c) Wing Tie-Down -- DISCONNECT
d) Main Wheel Tire -- CHECK for proper inflation
e) Chock -- REMOVE
f) Right Wing Tank – SUMP
g) Main Buss Alternate Feed – ON
h) Fuel Boost Pump – ON
i) Gascolator – SUMP
j) Fuel Boost Pump – OFF
k) Main Buss Alternate Feed -- OFF
l) Fuel Quantity -- CHECK VISUALLY
m) Fuel Filler Cap – SECURE
N506RV
5. NOSE
a) Engine Oil Level -- CHECK, do not operate with less than 4 quarts
b) Propeller and Spinner -- CHECK for nicks and security
c) Cowl Hinge Pins – CHECK for security
d) Air Inlet -- CHECK for restrictions
e) Nose Wheel Tire -- CHECK for proper inflation
f) Chock -- REMOVE
g) Fuel Tank Vents -- CHECK for blockage
6. LEFT WING
a) Wing Tie-Down -- DISCONNECT
b) Main Wheel Tire -- CHECK for proper inflation
c) Chock -- REMOVE
d) Left Wing Tank -- SUMP
e) Fuel Quantity -- CHECK VISUALLY
f) Fuel Filler Cap -- SECURE
g) Pitot Tube Cover -- REMOVE and check for blockage
h) Landing Light -- CHECK condition
i) Aileron -- CHECK freedom of movement and security
j) Flap -- CHECK security
N506RV
BEFORE STARTING ENGINE
a) Preflight Inspection – COMPLETE
b) Rudder Gust Lock Removed -- VERIFY
c) Seat Belts and Shoulder Harnesses -- ADJUST and LOCK
d) Canopy -- DOWN
e) Fuel Selector Valve -- DESIRED TANK
f) Avionics and Electrical -- OFF
g) Brakes -- SET
h) Circuit Breakers -- CHECK IN
STARTING ENGINE
a) Mixture -- RICH
b) Carb Heat -- COLD
c) Prop -- HIGH RPM
d) Master Switch – ON
e) Fuel Boost Pump -- ON
f) Strobe – ON
g) Flaps -- UP
h) Prime -- AS REQUIRED (3-4 seconds when cold)
i) Throttle -- OPEN approx 1/4”
j) Propeller Area -- CLEAR
k) Ignition Switch -- START
l) Engine Monitor -- ON
m) Oil Pressure -- CHECK 25 psi at idle
n) Fuel Boost Pump – OFF
o) Autopilot / Encoder -- ON
p) Avionics -- ON
N506RV
BEFORE TAKEOFF
a) Brakes -- SET
b) Canopy -------- Main Latch -- SECURE
-------- Secondary Latch -- SECURE
c) Flight Controls -- FREE and CORRECT
d) Flight Instruments – SET
Altimeters – CORRECT PRESSURE
A/H – ALLIGNED
Autopilot – TURN COORDINATOR MODE
e) Navigational Instruments -- SET
f) Fuel Selector Valve -- DESIRED TANK
g) Mixture -- RICH (below 3000’)
h) Elevator and Aileron Trim -- NEUTRAL
i) Throttle -- 1700 RPM
1) Magnetos -- CHECK (125 max drop, 50 differential)
2) Suction – CHECK (5” Hg)
3) Carb Heat -- CHECK for drop
4) Prop -- CHECK operation
5) Engine Instruments -- CHECK
6) Throttle -- IDLE
7) Carb Heat -- COLD
i) Radios – SET
j) Flaps -- AS REQUIRED
k) Fuel Boost Pump -- ON
l) Transponder -- ALTITUDE
N506RV
TAKEOFF
NORMAL TAKEOFF
a) Wing Flaps – UP
a) Carb Heat – COLD
b) Prop – HIGH RPM
c) Throttle -- FULL OPEN
d) Elevator Control – LIFT NOSE WHEEL (at 55KIAS)
e) Climb Speed -- 110 KIAS
SHORT FIELD TAKEOFF
a) Wing Flaps – 10 Deg
b) Carb Heat – COLD
c) Prop – HIGH RPM
d) Brakes – APPLY
e) Throttle – FULL OPEN
f) Mixture – RICH (above 3000’ lean to obtain max RPM)
g) Brakes – RELEASE
h) Climb Speed – 80 KIAS (Vy)
ENROUTE CLIMB
a) Airspeed – 110 - 130 KIAS
b) Throttle – 25 in Hg, or full throttle
c) Prop – 2500 RPM
d) Boost Pump – OFF at 1000 feet AGL
e) Fuel Pressure – CHECK
f) Mixture – LEAN above 5000’
CRUISE
a) Throttle – 23 in Hg
b) Prop – 2300 RPM
c) Trim – ADJUST
d) Mixture – LEAN
N506RV
Enroute
Fuel Schedule:
|Fuel Selector |Switch At: |Starting |Starting |
|Position |(Aircraft Total) |Total (Left) |Total (Right) |
|Left |37 |18.5 |18.5 |
|Left to Right |27 |8.5 |18.5 |
|Right to Left |11.5 |8.5 |3 |
Oxygen Duration (hours):
(AL-645 Tank 22.8 cu ft max, with A3 Flowmeters, 1800 psig at 70 F)
|Crew |10,000 ft |15,000 ft |18,000 ft |
|One |29 |16 |12 |
|Two |14.5 |8 |6 |
N506RV
POSTFLIGHT
AFTER LANDING
a) Wing Flaps – UP
b) Boost Pump – OFF
c) Transponder – STANDBY
ENGINE SHUTDOWN
a) Avionics – OFF
b) Autopilot / Encoder -- OFF
c) Electrical – OFF
d) Throttle – IDLE
e) Prop – FULL FORWARD
f) Mixture – IDLE CUT-OFF
(After Engine Stops)
g) Ignition – OFF
h) Strobe -- OFF
i) Flaps – DOWN
j) Master – OFF
SECURING AIRCRAFT
a) Wheel Chocks – INSTALL
b) Wing & Tail Tie-Down – INSTALL AS REQUIRED
c) Pitot Tube Cover – INSTALL AS REQUIRED
d) Cockpit – CLEAN AND SECURE
e) Ignition Key – REMOVED
f) Master and Electrical Switches – OFF
g) Engine Monitor Fuel Quantity – RESET AFTER REFUELING
N506RV
Performance
Cruise Performance at 8,000’:
|KTAS |RPM |MAP |Fuel Flow |% Power |
|167 |2400 |23” |8.4 GPH |75% |
|157 |2200 |23” |7.4 GPH |65% |
|151 |2200 |21” |6.3 GPH |55% |
No Wind Range at 8,000’:
← All range calculations include 3 gal. for engine start, taxi, takeoff and climb.
← Engine is leaned for best economy.
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
N506RV
WEIGHT AND BALANCE DATA
Make: Scott Gesele Model: RV-6A
Serial: 22717 Registration: N506RV
Maximum Weights:
“Aerobatic”………………………………… 1375 Lbs
“Utility” ……….……………………………. 1650 Lbs*
“Normal” …………………………………… 1800 Lbs*
* Recommended maximum landing weight is 1650 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
Internal Ski Rack ……... 144” aft of datum
Aircraft weighed empty in level flight attitude.
(Includes 8 qts. of oil, no fuel)
Weight Arm Moment
Right Wheel 428 84.25 36059
Left Wheel 420 84.25 35385
Nose Wheel 294 28.5 8379
Total 1142 79832
Empty CG = 69.91 aft of datum
N506RV
WEIGHT AND BALANCE DATA
Sample:
Weight Arm Moment
Aircraft 1142 79832
Fuel (6lbs/gal) 70
Pilot 87.4
Passenger 87.4
Baggage 117
Skis 144
(Skis weigh 9 lbs/adult pair)
Total
CG = Total Moment / Total Weight
CG = in aft of datum
CG Range = 68.7 to 76.8 in aft of datum
N506RV
WEIGHT AND BALANCE DATA
*With a CG Range of 68.7 to 76.8 in., all foreseeable loading configurations are within limitations.
N506RV
Engine Information
Model: …….. Lycoming O-320 D1A
HP: ………… 160
Fuel: ……….. 91/96 or 100/130 octane minimum
……….. 100LL
Oil Filter: ….. Champion CH48110
OIL: Avg MIL-L-6082 Ashless Dispersant
Ambiant 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: 82 deg C desired, 118 deg C 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 66 deg C – 223 deg C desired range, 260 deg C max
N506RV
ENGINE INFORMATION
N506RV
ENGINE INFORMATION
N506RV
ENGINE INFORMATION
N506RV
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:
2. Power – 1700 RPM for a few minutes
3. Engine – SHUTDOWN and inspect for damage
If engine fails to start:
4. Throttle – FULL OPEN
5. Mixture – IDLE CUT-OFF
6. Cranking – CONTINUE
7. Fire Extinguisher – OBTAIN
8. 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. Alternator Breaker – RESET
4. Main Feed Breaker - RESET
5. Circuit Breakers – VERIFY POSITIONS
6. Master Switch – ON
IF ALTERNATOR IS STILL OFF-LINE:
7. Master Switch – OFF
8. Electrical Switches – OFF
9. Alternator Breaker – PULL
10. Avionics – OFF
11. Main Feed Breaker – PULL
12. Alternate Feed Switch Guard – UP
13. Alternate Feed Switch – ON
14. Avionics – ON as required
15. Electrical Equipment – ON, as required
16. Flight – TERMINATE as soon as practical, aircraft is on battery reserves only.
In accordance with Item 15 of the Transport Canada and Bahamas Civil Aviation Department Standardized Validation of A Special Airworthiness Certificate- Experimental, I, , as the registered owner of authorize the following persons for continued operation of this aircraft in both Canadian and Bahamian airspace.
Registered Owner’s Signature Date
N506RV
ANNUAL CONDITION INSPECTION REPORT
HOURS:
MAKE: RV-6A SERIAL #: 22717
REGISTRATION #: N506RV DATE:
DESCRIPTION : COMMENTS:
A. PROPELLER GROUP
1. Inspect spinner and back plate....
2. Inspect blades for nicks and cracks....
3. Check for grease and oil leaks....
4. Lubricate propeller per lubrication chart....
5. Check spinner mounting brackets....
6. Check propeller mounting bolts and safety....
7. 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 belts....
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....
D. 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...
15. Check elevator bell cranks and controls....
16. Check EHSI / EFIS Electronic Compass …
17. Check autopilot pitch servo and pushrod
17. Lubricate all bearings as needed.....
18. 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 autopilot roll servo and pushrod
6. Check flaps and attachment for damages....
7. Check all wing attachment bolts....
8. Check fuel tanks and lines for leaks and....
9. Check fuel tank vents....
10. Reinstall inspection plates....
E. LANDING GEAR GROUP
1. Check nose gear travel and damper tightness....
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....
F. 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....
15. Perform 2 hr Capacity Check of EHSI/EFIS Backup Battery ….
G 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!)
g) Nose gear leg bolt security
NOTES
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