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SECTION 3

CUB CRAFTERS

EMERGENCY PROCEDURES

CC11-100

REPORT SC10000AFM

Issued: 08/01/06

Page Number: 3-20

Date of Revision: 11/23/18

3.4.7 LOSS OF OIL PRESSURE

More often than not, a loss of oil pressure will be gradual.
If it is accompanied by an increase in oil temperature, it is
a sign that there is a problem with the engine’s oil system
and the aircraft should be landed as soon as practical, as
the engine may stop suddenly. At reduced power
maintain altitude and proceed to the nearest suitable
landing site. Be prepared for a power-off, forced landing.

Low oil pressure can be the result of a faulty gauge or
sending unit or a malfunction in the oil pressure
regulating system. In any case, land as soon as practical
and have the problem investigated.

3.4.8 HIGH OIL TEMPERATURE

Abnormally high oil temperature indications may be
caused by a variety of reasons, among them:



Low oil level



Obstruction in the air flow reaching the oil cooler



Defective gauge

A rapid rise in oil temperature must be treated seriously.
Monitor the oil pressure gauge. Reduce power, enrich the
mixture and, if practical, maintain a high airspeed to ram
cooling air through the oil cooler.

Land as soon as practical and investigate the cause, but
be prepared for a power-off forced landing.

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Содержание CC11-100

Страница 1: ...irplane Serial Number Airplane Registration Number This airplane is approved as a special light sport category aircraft S LSA as defined by 14CFR 1 1 and meets the requirements of ASTM consensus stand...

Страница 2: ...CUB CRAFTERS CC11 100 REPORT SC10000AFM Issued 08 01 06 Page Number 0 ii Date of Revision 11 23 18 INTENTIONALLY LEFT BLANK...

Страница 3: ...23 18 Page Number 0 iii WARNING THIS OPERATING MANUAL IS ONLY VALID FOR USE WITH THE AIRCRAFT IDENTIFIED ON THE FACE PAGE ANY REVISIONS TO THIS MANUAL MUST BE INSERTED AS APPROPRIATE NOTE This documen...

Страница 4: ...CUB CRAFTERS CC11 100 REPORT SC10000AFM Issued 08 01 06 Page Number 0 iv Date of Revision 11 23 18 INTENTIONALLY LEFT BLANK...

Страница 5: ...has been prepared to provide you with information about your airplane s equipment operating procedures performance and suggested performance and care This POH which was put in your aircraft at the ti...

Страница 6: ...ccordance with consensus standard ASTM F 2295 Standard Practice for Continued Operational Safety Monitoring of a Light Sport Aircraft Please note that this standard describes the responsibilities of t...

Страница 7: ...and Oil Temperature Gauge Markings B Section 0 Section 2 Section 3 Revision to Handbook Revised Table 2 2 for Oil Pressure and Oil Temperature Gauge Markings Revised all Airspeeds to IAS Revised Maxim...

Страница 8: ...rature Added Max Weight Options Added if equipped to 2 10 and 2 13 Added Total Fuel Capacity Added Operating Maneuvering Speed for Floats Removed fully from 3 3 2 Added radio frequency to 3 3 4 and 3...

Страница 9: ...7 5 12 to Left Wing Revised 7 7 Added 7 11 Music Jack G Section 0 Section 4 Section 7 Section 8 Revision to Handbook Added Preflight check for Front and Rear Seats Added Rear Seat Strap Routing Inform...

Страница 10: ...0 Section 2 Section 4 Section 7 Section 9 1 Revision to Handbook Added Placard to 2 19 Added Step to 4 3 1 2 Revised Procedure in 4 4 1 2 Added Figures to 7 5 9 Added Seat Caution to 7 6 Added Step to...

Страница 11: ...from 101 to 93 IAS 01 28 08 SJT SJH C 0 2 2 4 4 26 5 11 5 14 7 5 7 9 Log of Revisions Revised Engine Operating Limits Oil Temperature to 240 Revised wording to state Retract flaps Revised Figure 5 5 f...

Страница 12: ...l Capacity Corrected placard location Revised 3 2 Removed fully from 3 3 2 Added radio frequency for 3 3 4 and 3 3 5 Revised 3 4 10 Loss of Primary Instruments Added Loss of Flight Controls Added Shor...

Страница 13: ...emoved Optional Revised fiberglass to composite materials Added LED Light Information Revised vane location to left wing Revised 7 7 Added Music Jack Information 04 09 10 SJT SJH G 0 4 0 8 4 3 4 16 7...

Страница 14: ...Added Window Operation Placard Revised for converted units Revised Ciruit Breaker Check Revised Cowling to Cowl Added Circuit Breakers Windows and Landing Lights sections to 4 3 3 1 Added Doors and Wi...

Страница 15: ...2 13 3 8 4 4 4 16 7 4 Log of Revisions List of Effective Pages Added Serial Number Effectivity Added Rec Oil Qty Revised Figure 1 1 Added Rec Oil Qty Separated Environmental Limitations by S LSA and E...

Страница 16: ...CUB CRAFTERS CC11 100 REPORT SC10000AFM Issued 08 01 06 Page Number 0 12 Date of Revision 11 23 18 INTENTIONALLY LEFT BLANK...

Страница 17: ...ECTION 2 LIMITATIONS SECTION 3 EMERGENCY PROCEDURES SECTION 4 NORMAL PROCEDURES SECTION 5 PERFORMANCE SECTION 6 WEIGHT AND BALANCE SECTION 7 AIRCRAFT AND SYSTEMS SECTION 8 HANDLING AND SERVICING SECTI...

Страница 18: ...CUB CRAFTERS CC11 100 REPORT SC10000AFM Issued 08 01 06 Page Number 0 14 Date of Revision 11 23 18 INTENTIONALLY LEFT BLANK...

Страница 19: ...d 08 01 06 REPORT SC10000AFM Date of Revision 11 23 18 Page Number 1 i TABLE OF CONTENTS SECTION 1 GENERAL INFORMATION Paragraph Page 1 GENERAL INFORMATION 1 1 INTRODUCTION 1 1 1 2 WARNING CAUTIONS AN...

Страница 20: ...SECTION 1 CUB CRAFTERS GENERAL INFORMATION CC11 100 REPORT SC10000AFM Issued 08 01 06 Page Number 1 ii Date of Revision 11 23 18 INTENTIONALLY LEFT BLANK...

Страница 21: ...airplane or applicable aviation regulations The pilot in command is responsible for determining whether the airplane is safe for flight She he is also responsible for ensuring that all operations are...

Страница 22: ...ner 1 2 WARNINGS CAUTIONS AND NOTES WARNINGS CAUTIONS and NOTES are used to emphasize critical and important information and are used as defined below WARNING AN OPERATING PROCEDURE PRACTICE OR A COND...

Страница 23: ...Range 6000 75 w reserves 407sm Endurance 6000 75 w reserves 4 1 hours Rate of Climb 800 fpm Stall Speed full flaps 32 mph 27 knots Stall Speed no flaps 40 mph 35 knots Fuel Capacity Total both tanks...

Страница 24: ...SECTION 1 CUB CRAFTERS GENERAL INFORMATION CC11 100 REPORT SC10000AFM Issued 08 01 06 Page Number 1 4 Date of Revision 11 23 18 Figure 1 1 Three View Drawing...

Страница 25: ...CUB CRAFTERS SECTION 1 CC11 100 GENERAL INFORMATION Issued 08 01 06 REPORT SC10000AFM Date of Revision 11 23 18 Page Number 1 5 Figure 1 2 Turning Radius...

Страница 26: ...SECTION 1 CUB CRAFTERS GENERAL INFORMATION CC11 100 REPORT SC10000AFM Issued 08 01 06 Page Number 1 6 Date of Revision 11 23 18 INTENTIONALLY LEFT BLANK...

Страница 27: ...S 2 3 2 4 POWERPLANT LIMITATIONS 2 4 2 5 POWERPLANT INSTRUMENT MARKINGS 2 5 2 6 WEIGHT LIMITS 2 6 2 7 CENTER OF GRAVITY 2 6 2 8 MANEUVERS 2 6 2 9 MANEUVER LOAD FACTORS 2 6 2 10 MINIMUM FLIGHT CREW 2 7...

Страница 28: ...SECTION 2 CUB CRAFTERS LIMITATIONS CC11 100 REPORT SC10000AFM Issued 08 01 06 Page Number 2 ii Date of Revision 11 23 18 INTENTIONALLY LEFT BLANK...

Страница 29: ...ements can be found in Section 9 Supplements 2 2 AIRSPEED LIMITATIONS SPEED IAS mph kts Never Exceed Speed VNE 141 122 Do not exceed this speed in any operation Maximum Operating Maneuvering Speed VA...

Страница 30: ...Second notch 35 81 70 Full flaps 50 81 70 Do not exceed the flap speed corresponding to a given setting Maximum Demonstrated Crosswind Component 13 11 Stall Speed Stall Speed with Full Flaps 32 27 Sta...

Страница 31: ...d their significance are shown in Table 2 1 MARKING SPEED RANGE OR VALUE IAS mph kts SIGNIFICANCE Red radial line 141 122 Never exceed speed VNE Yellow arc 101 141 87 122 Operations must be conducted...

Страница 32: ...0 bhp Maximum Engine Speed 2750 rpm Oil Pressure Minimum 30 psi Oil Pressure Maximum 60 psi Oil Temperature Maximum 240 F Fuel Limitations grade 100 or 100LL Oil Capacity 3 5 to 6 Quarts 4 Quarts Reco...

Страница 33: ...ine 2750 rpm Green arc normal operating range 900 2750 rpm OIL PRESSURE Yellow arc caution low 10 30 psi Green arc normal 30 60 psi Yellow arc caution high 60 100 psi Red radial line maximum 100 psi O...

Страница 34: ...3 0 inches aft of datum At 1100 lbs 500 kg or less 70 5 inches aft of datum Straight line variation between points given Aft CG Limit at all weights 78 5 inches aft of datum The datum is 60 inches for...

Страница 35: ...Flight into I M C Instrument Meteorological Conditions is prohibited Flight into known icing is prohibited E LSA This aircraft may operate day and night VFR when equipped in accordance with the appro...

Страница 36: ...167 Liters total capacity 40 0 US gallons 150 Liters total usable 2 15 BAGGAGE AND CARGO LOADING Standard Configuration Forward cargo compartment behind passenger 100 lbs 45 kg Extended cargo compart...

Страница 37: ...he aircraft may be operated from paved and unpaved runways 2 18 VORTEX GENERATORS The aircraft is allowed to fly with the following number of vortex generators missing Not more than three vortex gener...

Страница 38: ...In view of the pilot OR If equipped with extended range fuel tanks or On top inboard of all lift struts Behind the front seat S LSA Aircraft OPERATOR MUST READ AND BE FAMILIAR WITH PILOT OPERATING HA...

Страница 39: ...CC11 100 LIMITATIONS Issued 08 01 06 REPORT SC10000AFM Date of Revision 11 23 18 Page Number 2 11 In forward cargo compartment or Next to fuel selector for standard tanks or Next to fuel selector for...

Страница 40: ...ATIONS CC11 100 REPORT SC10000AFM Issued 08 01 06 Page Number 2 12 Date of Revision 11 23 18 In cargo shelf compartment or On extended baggage compartment door or On flap lever On wing next to tank fi...

Страница 41: ...ONS Issued 08 01 06 REPORT SC10000AFM Date of Revision 11 23 18 Page Number 2 13 On wing next to tank filler with extended range tanks or Near stall warning vane On right hand side of empennage On ope...

Страница 42: ...of Revision 11 23 18 Next to windows Right side of seat base Only required for aircraft with both the Artex ELT and battery compartment insert installed Located above the right fuel drain left fuel d...

Страница 43: ...GENCY LANDING WITHOUT ENGINE POWER 3 6 3 3 5 PRECAUTIONARY LANDING WITH ENGINE POWER 3 7 3 3 6 FIRE IN FLIGHT 3 8 3 3 7 LOSS OF OIL PRESSURE 3 9 3 3 8 HIGH OIL TEMPERATURE 3 9 3 3 9 EMERGENCY DESCENT...

Страница 44: ...FLIGHT 3 19 3 4 7 LOSS OF OIL PRESSURE 3 20 3 4 8 HIGH OIL TEMPERATURE 3 20 3 4 9 EMERGENCY DESCENT 3 21 3 4 10 ALTERNATOR FAILURE 3 23 3 4 11 OVERVOLTAGE 3 24 3 4 12 INADVERTENT SPIN 3 24 3 4 13 INAD...

Страница 45: ...ected to refer to in an emergency situation This information should be reviewed regularly Pilots must familiarize themselves with the procedures in this section and must be prepared to take appropriat...

Страница 46: ...ERGENCY OPERATIONS IAS MPH KNOTS STALL SPEEDS Flaps up VS1 40 35 Flaps down 50 VS0 32 28 OPERATING MANEUVERING SPEED VA At 1320 lb On Wheels or Skis 93 81 At 1430 lb On Floats 97 84 BEST GLIDE VG Flap...

Страница 47: ...gine If engine starts Power 1700 RPM for a few minutes Engine Shut down by pulling mixture to idle cut off Have a qualified technician thoroughly inspect the engine and the airframe If engine fails to...

Страница 48: ...mal landing land straight ahead If insufficient runway remains Maintain a safe airspeed Use shallow turns to avoid obstructions Use of flaps depends on circumstances Normally flaps should be extended...

Страница 49: ...e Airspeed best glide MAINTAIN 68 59 If altitude permits Airspeed best glide MAINTAIN 68 59 Fuel Selector Both Mixture Full rich Carburetor Heat On Hot Magnetos Ensure both on Engine Instruments Check...

Страница 50: ...red Door Open Touchdown At the lowest possible airspeed ELT Activate If time permits check GPS or charts for airports in the immediate vicinity If possible notify your difficulty and intentions by rad...

Страница 51: ...Maximum speed full flaps 15 81 70 Trim As required Speed As required 1 3 times full flaps stall speed at gross weight is 42 mph or 36 knots IAS If time permits check GPS or charts for airports in the...

Страница 52: ...table airport or landing area All Electrical Switches Off Avionics Master Switch and Avionics Off Circuit Breakers Check for faulty circuit If any breakers are out note the circuits and do not reset o...

Страница 53: ...OF OIL PRESSURE Land as soon as practical and investigate cause Prepare for emergency landing without power Section 3 3 4 3 3 8 HIGH OIL TEMPERATURE Airspeed Increase Power Reduce as much as practical...

Страница 54: ...f Circuit Breakers Check In If the alternator drive belt failure is NOT obvious and NO circuit breakers are out Master Switch On If the drive belt failure is obvious the circuit breaker is out or elec...

Страница 55: ...without electrical system 3 3 12 INADVERTENT SPIN Aileron Control Neutral Throttle Closed Rudder Full opposite Opposite to direction of spin Elevator Control Forward To break stall Elevator and Thrott...

Страница 56: ...ness and or loss of power Ice formations on the propeller may cause severe propeller engine vibrations Ice accumulation over the pitot tube may cause erroneous airspeed indications Ice build up on the...

Страница 57: ...FTERS SECTION 3 CC11 100 EMERGENCY PROCEDURES Issued 08 01 06 REPORT SC10000AFM Date of Revision 11 23 18 Page number 3 13 3 3 14 UNCOMMANDED TRIM ACTUATION Standard Trim Switch TRIM circuit breaker O...

Страница 58: ...off and the throttle opened fully before cranking the engine If the engine starts and fire goes out within a few seconds run it at 1700 rpm for a few minutes If the fire continues for more than a few...

Страница 59: ...most cases the landing should be straight ahead with only small changes in direction to avoid obstacles There is seldom enough altitude and airspeed to execute a 180 gliding turn to the runway In a t...

Страница 60: ...he immediate vicinity If there is enough altitude try to determine the cause of failure In most cases the reason is fuel exhaustion due to the selector being on an empty tank Switching to the BOTH pos...

Страница 61: ...your pattern using flaps slipping or by using a combination of these techniques If possible transmit a MAYDAY message on 121 5 MHz stating location and intentions and squawk 7700 Activate the ELT Onc...

Страница 62: ...out the window on the left side Next protect your head with one arm and release the seat harness with the other Exit the aircraft through the door or the windows Once the risk of fire has passed ensur...

Страница 63: ...e action to be taken The maximum rate of descent may be obtained by diving the aircraft to 141 mph or 122 knots IAS and adjusting the throttle so as not to exceed 2750 rpm Use extreme caution when fly...

Страница 64: ...power off forced landing Low oil pressure can be the result of a faulty gauge or sending unit or a malfunction in the oil pressure regulating system In any case land as soon as practical and have the...

Страница 65: ...lled fire or when smoke toxic fumes or other situation threatens control of the airplane through incapacitation or restricted visibility for the pilot See paragraph FIRE IN FLIGHT 3 4 6 Retard throttl...

Страница 66: ...EXTENDED SPEED CAN CAUSE DAMAGE TO THE WING STRUCTURE AND POSSIBLE FAILURE OF THE FLAP ATTACHMENTS IF THE DESCENT IS TO BE MADE WITH THE FLAPS RETRACTED DO NOT EXCEED 141 mph or 122 knots IAS IN SMOO...

Страница 67: ...s to reduce the electrical load to a minimum NOTE Duration of the battery is dependent on the condition of the battery at the time of the failure and the electrical load being demanded Turn the master...

Страница 68: ...n the master switch off and plan to continue flight without using the electrical system 3 4 12 INADVERTENT SPIN If an inadvertent spin is entered close the throttle neutralize the ailerons and apply f...

Страница 69: ...lent if flying in clouds or visible moisture This aircraft is approved for VFR flight only If ice build up becomes evident on the windshield and or the lift struts or if the engine operates rough appl...

Страница 70: ...ation over engine induction air inlet can cause engine roughness and or loss of power Ice formations on the propeller may cause severe propeller engine vibrations Ice accumulation over the pitot tube...

Страница 71: ...levator Failure cable driven In the event of a failure of the elevator control system the airplane may be controlled and landed using the stabilizer trim power and flaps Land as soon as possible and i...

Страница 72: ...SECTION 3 CUB CRAFTERS EMERGENCY PROCEDURES CC11 100 REPORT SC10000AFM Issued 08 01 06 Page Number 3 28 Date of Revision 11 23 18 INTENTIONALLY LEFT BLANK...

Страница 73: ...1 2 Nose Section 4 4 4 3 1 3 Left Fuselage Wing and Landing Gear 4 5 4 3 1 4 Empennage 4 6 4 3 1 5 Right Fuselage Wing and Landing Gear 4 7 4 3 1 6 General 4 7 4 3 2 STARTUP AND TAXI 4 8 4 3 2 1 Befo...

Страница 74: ...and Landing Gear 4 18 4 4 1 6 General 4 18 4 4 2 STARTUP AND TAXI 4 19 4 4 2 1 Before Starting the Engine 4 19 4 4 2 2 Starting the Engine 4 19 4 4 2 3 Starting Engine when Flooded 4 19 4 4 2 4 Warm U...

Страница 75: ...he checklists It provides the pilot with detailed descriptions that will help him understand the procedures and techniques This manual assumes that the pilot is appropriately rated in an aircraft with...

Страница 76: ...SECTION 4 CUB CRAFTERS NORMAL PROCEDURES CC11 100 REPORT SC10000AFM Issued 08 01 06 Page Number 4 2 Date of Revision 11 23 18 Figure 4 1 Walk around...

Страница 77: ...uges Sufficient fuel for intended flight Mixture Idle cut off Carburetor Heat Cold Ignition Switch Off Electrical Switches Off Navigation Strobe Lights if installed Check operation Landing Light if in...

Страница 78: ...with the flight controls or the pilot during flight 4 3 1 2 Nose Section Cowl Secure Cowl Flaps if installed Secure Oil Door Open Oil Quantity 4 Quarts recommended Check and cap secure Engine Conditi...

Страница 79: ...ntity Fuel Cap Vent Check vent is clear and cap secure Pitot Tube Check condition Jury Struts and Brackets Check condition Stall Warning Vane Check operation Landing Light if installed Check condition...

Страница 80: ...sued 08 01 06 Page Number 4 6 Date of Revision 11 23 18 4 3 1 4 Empennage Bracing Wires and Attach Brackets Check for tension Hinges Check Rudder Cables Check Beacon and Position Light if installed Ch...

Страница 81: ...s Check Aileron Surface Check Condition Aileron Hinges Check Wing Tip and Lights if installed Check Vortex Generators Check Tie Down Remove Wing Strut Check Condition Jury Struts and Brackets Check Co...

Страница 82: ...Avionics Master Switch Off Propeller Area Clear CAUTION The parking brake on each main wheel is set by depressing the top of each rudder pedal and rotating the valve on each master cylinder so the lev...

Страница 83: ...on Switch Both Lights As required Avionics Master Switch On Normal procedure three times If engine is hot omit this step WARNING ENSURE THAT THE PRIMER IS CLOSED AND LOCKED AFTER THE ENGINE HAS STARTE...

Страница 84: ...1700 rpm Magnetos Check Drop not to exceed 150 rpm or 75 rpm differential between magnetos and no engine roughness Carburetor Heat Hot note rpm drop then cold Engine Instruments Check Ammeter if inst...

Страница 85: ...des and or temperatures it may be necessary to lean the mixture for peak rpm 4 3 3 2 Takeoff Accelerate to 52 mph or 45 knots IAS depending on aircraft weight allowing tail to rise maintain directiona...

Страница 86: ...SECTION 4 CUB CRAFTERS NORMAL PROCEDURES CC11 100 REPORT SC10000AFM Issued 08 01 06 Page Number 4 12 Date of Revision 11 23 18 Mixture Adjust Carburetor Heat As required...

Страница 87: ...1 3 times full flaps stall speed at gross weight is 42 mph or 36 knots IAS Doors and windows Closed 4 3 3 6 2 Crosswind Landing Fuel Selector Both Seat Belts Fastened Mixture Set Flaps Set below white...

Страница 88: ...aintain directional control 4 3 3 7 Go Around Throttle Full power Carburetor Heat if applicable Off Airspeed Above 52 mph or 45 knots Flaps Retract slowly Trim As required 4 3 3 8 Stopping Engine Park...

Страница 89: ...itch trim to the takeoff position using the rocker switch on the control stick Ensure that the stabilizer moves smoothly The trim is in the takeoff position when the leading is within the marks on the...

Страница 90: ...ficate aircraft flight manual weight and balance data etc Adjust the position of both the front seat Turn the master switch off before leaving the cockpit Verify rear seat straps are correctly routed...

Страница 91: ...el system In heavy or prolonged precipitation Whenever there is any question that water may have accumulated in the fuel system 1 Gently rock the wings of the aircraft 2 Drain at least 1 8 gallon of f...

Страница 92: ...eneral condition of the wings lift struts jury struts and wing tip Check the flaps and ailerons for general condition Pay particular attention to the hinges to make sure they are secure and the cotter...

Страница 93: ...ng the Engine Turn the master switch on Push the mixture control in to full rich If the engine is cold it may be desirable to prime the engine To do this rotate the primer control until it unlocks pul...

Страница 94: ...idle for too long as it will tend to foul the spark plugs If you need to add power over loose stones or gravel do so carefully to avoid damaging the propeller 4 4 2 5 Taxiing Before starting to taxi m...

Страница 95: ...ld be inspected prior to flight Apply the carburetor heat to be sure that it is operating You will note a drop of about 50 to 75 rpm when it is applied This will also clear any ice that may have forme...

Страница 96: ...power Slowly lean the mixture until you observe the peak RPM Retard the throttle slowly and proceed with the rest of the run up Prior to takeoff verify that the flight instruments operate correctly E...

Страница 97: ...2 knots IAS and best angle VX is at 50 mph or 43 knots IAS with flaps up Normal en route climbs should be carried out at 80 to 90 mph or 70 to 78 knots While climbing lean the mixture to achieve maxim...

Страница 98: ...aps may be lowered to the first notch 15 when the airspeed is below 85 mph or 74 knots IAS The maximum speed for more flaps 15 is 81 mph or 70 knots IAS CAUTION Plan the pattern so steep turns are not...

Страница 99: ...as airspeed is reduced Maintain directional control Apply brakes as necessary 4 4 3 6 2 Crosswind Landing When established on a short final approach use the ailerons and rudder to maintain the approa...

Страница 100: ...t 40 mph or 35 knots accelerate to VX 50 mph or 43 knots and climb out until obstacle clearance is achieved then raise flaps and decrease climb rate as desired 4 4 3 7 2 Landing Make a normal approach...

Страница 101: ...ys be stopped by pulling the mixture control to the idle cut off position Turn the ignition switch off Finally turn the master switch off NOTE Any device s plugged into an accessory port may drain the...

Страница 102: ...SECTION 4 CUB CRAFTERS NORMAL PROCEDURES CC11 100 REPORT SC10000AFM Issued 08 01 06 Page Number 4 28 Date of Revision 11 23 18 INTENTIONALLY LEFT BLANK...

Страница 103: ...mber 5 i TABLE OF CONTENTS SECTION 5 PERFORMANCE Paragraph Page 5 PERFORMANCE 5 1 INTRODUCTION 5 1 5 2 PERFORMANCE CHARTS 5 3 5 2 1 AIRSPEED CALIBRATION 5 4 5 2 2 STALL SPEED 5 5 5 2 3 TAKEOFF 5 7 5 2...

Страница 104: ...SECTION 5 CUB CRAFTERS PERFORMANCE CC11 100 REPORT SC10000AFM Issued 08 01 06 Page Number 5 ii Date of Revision 10 31 11 INTENTIONALLY LEFT BLANK...

Страница 105: ...t tests taking into account the proficiency of an average pilot The pilot must use sound judgment when assessing the effect of conditions not found in the charts such as soft runways and winds aloft T...

Страница 106: ...The aircraft may be equipped with different tires and propellers All of the data presented in this chapter are based on an aircraft equipped with the McCauley Propeller Systems model 1B90 CM7141 prop...

Страница 107: ...S Figure 5 1 Airspeed System Calibration 5 4 Figure 5 2 Stall Speed versus Angle of Bank 5 5 Figure 5 3 Takeoff Ground Distance 5 7 Figure 5 4 Maximum Rate and Gradient of Climb 5 9 Figure 5 5 Cruise...

Страница 108: ...Airspeed mph Calibrated Airspeed mph Clean Ldg Flaps Figure 5 1 Airspeed System Calibration NOTE Indicated airspeed assumes zero instrument error NOTE Airspeed indication can vary by several miles pe...

Страница 109: ...E Issued 08 01 06 REPORT SC10000AFM Date of Revision 10 31 11 Page Number 5 5 5 2 2 STALL SPEED 30 35 40 45 50 55 60 65 0 10 20 30 40 50 60 Angle of Bank deg Stall Speed IAS mph Clean Landing Flaps Fi...

Страница 110: ...SECTION 5 CUB CRAFTERS PERFORMANCE CC11 100 REPORT SC10000AFM Issued 08 01 06 Page Number 5 6 Date of Revision 10 31 11 INTENTIONALLY LEFT BLANK...

Страница 111: ...B CRAFTERS SECTION 5 CC11 100 PERFORMANCE Issued 08 01 06 REPORT SC10000AFM Date of revision 10 31 11 Page number 5 7 5 2 3 TAKE OFF 5 2 3 1 Normal takeoff Figure 5 3 Takeoff Ground Distance at 1320 l...

Страница 112: ...n two lines place point A between the appropriate lines at approximately the correct spacing Extend a line horizontally from point A to the reference line on the second graph the one in the center Fro...

Страница 113: ...72 62 11 3 8000 72 62 4 3 0 71 61 59 4 2000 71 61 52 4 4000 72 62 45 3 6000 72 62 38 3 8000 73 63 31 2 0 71 61 75 4 2000 71 61 68 3 4000 72 62 61 2 6000 73 63 54 2 8000 74 64 47 2 0 71 61 100 4 2000 7...

Страница 114: ...4 1950 60 92 80 5 0 2150 68 97 84 5 3 2350 76 102 88 5 6 2550 80 103 89 5 6 2750 88 107 93 6 0 1950 56 82 71 4 7 2150 64 91 79 5 0 2350 66 90 78 4 9 2550 75 99 86 5 2 2750 82 102 88 5 6 1950 52 4 3 2...

Страница 115: ...AFTERS SECTION 5 CC11 100 PERFORMANCE Issued 08 01 06 REPORT SC10000AFM Date of Revision 10 31 11 Page Number 5 11 5 2 6 LANDING 5 2 6 1 Landing over 50 obstacle Figure 5 6 Landing Distance over 50 Ob...

Страница 116: ...s place point A between the appropriate lines at approximately the correct spacing Extend a line horizontally from point A to the reference line on the second graph the one in the center From there fo...

Страница 117: ...06 REPORT SC10000AFM Date of Revision 10 31 11 Page Number 5 13 5 2 7 BALKED LANDING Pressure Altitude ft Airspeed IAS Climb Gradient MPH KNOTS 4 000 70 60 2 3 Figure 5 7 Balked Landing Climb Gradien...

Страница 118: ...Statute Miles Nautical Miles Altitude Loss ft 1 4 1 2 1000 2 8 2 5 2000 4 3 3 7 3000 5 7 4 9 4000 7 1 6 2 5000 8 5 7 4 6000 9 9 8 6 7000 11 3 9 9 8000 12 8 11 1 9000 14 2 12 3 10000 15 6 13 6 11000 1...

Страница 119: ...ANCE Paragraph Page 6 WEIGHT AND BALANCE 6 1 INTRODUCTION 6 1 6 2 PERTINENT INFORMATION FOR WEIGHT AND BALANCE 6 2 6 2 1 TERMINOLOGY 6 3 6 3 WEIGHING PROCEDURES 6 5 6 3 1 PREPARATION 6 5 6 3 2 LEVELIN...

Страница 120: ...SECTION 6 CUB CRAFTERS WEIGHT AND BALANCE CC11 100 REPORT SC10000AFM Issued 08 01 06 Page Number 6 ii Date of Revision 10 31 11 INTENTIONALLY LEFT BLANK...

Страница 121: ...eight Weight and the position of the center of gravity affect both the performance and the stability and control characteristics particularly in stall and spin recovery The aircraft will only attain t...

Страница 122: ...INFORMATION FOR WEIGHT AND BALANCE Position of datum 60 inches ahead of wing leading edge Maximum gross weight 1320 lbs Forward CG Limits At 1320 lbs 73 0 inches aft of datum At 1100 lbs or less 70 5...

Страница 123: ...gravity CG The point at which an aircraft or an item of equipment would balance if suspended Its distance from the reference datum is found by dividing the total moment by the total weight CG Arm The...

Страница 124: ...Maximum Takeoff Weight Maximum weight approved for the start of the takeoff run Standard Empty Weight Weight of a standard airplane including unusable fuel full operating fluids and oil 5 qts Unusabl...

Страница 125: ...d and is in the proper location 1 Remove any items not listed on the Aircraft Equipment List such as rags charts tools etc 2 Clean the aircraft to remove excess dirt and grease 3 Remove the fuel from...

Страница 126: ...aircraft approximately in a flight level attitude by supporting the tail wheel on a bench 2 Place the aircraft on the calibrated weighing scales 3 Level the aircraft as follows Place a spirit level o...

Страница 127: ...CUB CRAFTERS SECTION 6 CC11 100 WEIGHT AND BALANCE Issued 08 01 06 REPORT SC10000AFM Date of Revision 10 31 11 Page Number 6 7 Figure 6 1 Leveling the Aircraft Figure 6 2 Leveling the Aircraft...

Страница 128: ...0AFM Issued 08 01 06 Page Number 6 8 Date of Revision 10 31 11 6 3 3 WEIGHING 1 Once the aircraft has been leveled record the weight on the main wheels and the tailwheel Figure 6 3 Standard Aircraft G...

Страница 129: ...er 6 9 Standard Aircraft CG Calculation W W W Arm CG t m 90 261 50 62 3X3 Landing Gear Equipped Aircraft CG Calculation W W W Arm CG t m 90 261 50 59 Where CG Arm Distance from the datum to the center...

Страница 130: ...SECTION 6 CUB CRAFTERS WEIGHT AND BALANCE CC11 100 REPORT SC10000AFM Issued 08 01 06 Page Number 6 10 Date of Revision 10 31 11 INTENTIONALLY LEFT BLANK...

Страница 131: ...ic empty Weight Center of Gravity Useful Load MODEL CC11 100 Aircraft Serial Number Registration Number Date Basic empty weight lbs Arm inches Moment in lbs Table 6 1 Basic Empty Weight Useful load Ma...

Страница 132: ...SECTION 6 CUB CRAFTERS WEIGHT AND BALANCE CC11 100 REPORT SC10000AFM Issued 08 01 06 Page Number 6 12 Date of Revision 10 31 11 INTENTIONALLY LEFT BLANK...

Страница 133: ...er 6 13 MODEL CC11 100 SERIAL NUMBER _______________ REGISTRATION NUMBER ____________ PAGE NUMBER ___ Date Item No Description of Article or Modification Added Removed Weight Change Running Basic Empt...

Страница 134: ...SECTION 6 CUB CRAFTERS WEIGHT AND BALANCE CC11 100 Table 6 2 Weight and Balance Record REPORT SC10000AFM Issued 08 01 06 Page Number 6 14 Date of Revision 10 31 11 INTENTIONALLY LEFT BLANK...

Страница 135: ...craft 1 Insert the respective loads in Table 6 3 or 6 4 2 Multiply each load by its respective arm and note the moment 3 Add the loads to calculate the takeoff weight 4 Add the moments to compute the...

Страница 136: ...08 Forward Cargo Compartment 100 lb max 110 40 Extended Cargo Compartment 20 lb max 134 40 TOTAL CG Station Table 6 3 Weight and Balance Loading Form Item Weight lbs Moment Arm in Moment in lbs Aircr...

Страница 137: ...CUB CRAFTERS SECTION 6 CC11 100 WEIGHT AND BALANCE Issued 08 01 06 REPORT SC10000AFM Date of Revision 10 31 11 Page Number 6 17 Figure 6 4 Weight and Balance Envelope...

Страница 138: ...le weight and balance calculation using the methods given in paragraph 6 5 Item Weight lbs Moment Arm in Moment in lbs Aircraft Empty 883 72 28 63825 5 Fuel 120 83 90 10068 0 Pilot 170 71 40 12138 0 P...

Страница 139: ...CUB CRAFTERS SECTION 6 CC11 100 WEIGHT AND BALANCE Issued 08 01 06 REPORT SC10000AFM Date of Revision 10 31 11 Page Number 6 19 Figure 6 5 Sample CG Location...

Страница 140: ...SECTION 6 CUB CRAFTERS WEIGHT AND BALANCE CC11 100 REPORT SC10000AFM Issued 08 01 06 Page Number 6 20 Date of Revision 10 31 11 INTENTIONALLY LEFT BLANK...

Страница 141: ...OLS 7 3 7 5 POWERPLANT 7 4 7 5 1 ENGINE 7 4 7 5 2 ENGINE MOUNT 7 4 7 5 3 PROPELLER 7 4 7 5 4 ENGINE COWLING 7 4 7 5 5 EXHAUST SYSTEM 7 5 7 5 6 IGNITION SYSTEM 7 5 7 5 7 AIR INDUCTION SYSTEM 7 5 7 5 8...

Страница 142: ...SECTION 7 CUB CRAFTERS AIRCRAFT AND SYSTEMS CC11 100 REPORT SC10000AFM Issued 08 01 06 Page Number 7 ii Date of Revision 11 23 18 INTENTIONALLY LEFT BLANK...

Страница 143: ...uded wing spars Tubular drag and compression struts and high strength stainless steel drag wires make up the rest of the structure The leading edges are covered with aluminum sheet The wing tip is mad...

Страница 144: ...can be installed in place of the bungee cord suspension See Burl s Aircraft LLC for manufacturer s information Each main wheel is provided with a set of disc brakes The left and right systems are inde...

Страница 145: ...ng a lever in the upper left hand side of the cockpit ahead of the pilot The flaps have four positions retracted 15 35 and 50 The flap lever has a spring latch system that will hold the flap in the se...

Страница 146: ...the way back operates a cut off valve on the carburetor that stops the supply of fuel to the engine The mixture control should always be used to stop the engine 7 5 2 ENGINE MOUNT The structure of the...

Страница 147: ...t both magnetos are operating correctly prior to takeoff In an emergency the engine will continue to run if one of the magnetos fails The engine should be started with the ignition switch in the BOTH...

Страница 148: ...START TO LOSE POWER OR STOP COMPLETELY AT THIS POINT THERE MAY NOT BE SUFFIECIENT HOT AIR IN THE ENGINE COMPARTMENT TO MELT THE ACCUMULATION OF CARBURETOR ICE EVEN WHEN THE CARBURETOR HEAT CONTROL IS...

Страница 149: ...at is mounted on the lower left hand side of the firewall The oil filler is on the right side of the engine An optional spin on oil filter may be installed and is located on an adapter on the lower le...

Страница 150: ...dard Fuel Tank Configuration with Additional Fuel Drain S N 00264 and on In the extended range configuration there are two interconnected tanks on the inboard end of each wing Between the two tanks th...

Страница 151: ...ed before each flight to test for water and sediment in the fuel system The fuel system is gravity fed with no separate boost pump The fuel flows from the tanks into a selector valve located on the lo...

Страница 152: ...etween the aircraft and the fueling equipment and will minimize the risk of electrical sparks when the aircraft is being refueled 7 5 10 ELECTICAL SYSTEM The main sources of electrical energy are a 12...

Страница 153: ...ons for airspeed altitude and rate of climb will be affected by opening the windows door or cabin air vents 7 6 COCKPIT Entry to the cockpit is through a door and window arrangement on the right side...

Страница 154: ...e flown from this position The aft occupant is provided with a control stick rudder pedals throttle and brakes for flight instruction The forward seat is adjustable fore and aft To move the seat remov...

Страница 155: ...nylon straps holding the seat cross bar to the floor by unscrewing and pushing in on the screw This will allow the tab to rotate and slide the pin out of the seat base connector Lift the rear seat cr...

Страница 156: ...f the rear seat cross bar sleeves and the nylon straps Remove the seat cushion from the rear seat Fold the rear seat for stowage See Figure 8 Figure 8 Folding of Rear Seat Tuck the rear seat seat cush...

Страница 157: ...d re attached to the floorboard in order to securely hold the cross bar in place 7 7 INSTRUMENT PANEL The instrument panel contains all flight navigation and engine instruments that are required for V...

Страница 158: ...partment located behind the pilot that has a capacity of 100 lbs and an extended cargo compartment that has a capacity of 60 lbs 7 10 ELT OPERATION AND LOCATION The aircraft is supplied with an ELT tr...

Страница 159: ...SECTION 8 HANDLING AND SERVICING Paragraph Page 8 HANDLING AND SERVICING 8 1 INTRODUCTION 8 1 8 2 GROUND HANDLING 8 1 8 2 1 TOWING INSTRUCTIONS 8 1 8 2 2 TIE DOWN INSTRUCTIONS 8 1 8 3 SERVICING FUEL...

Страница 160: ...SECTION 8 CUB CRAFTERS HANDLING AND SERVICING CC11 100 REPORT SC10000AFM Issued 11 26 08 Page number 8 ii Date of revision 10 31 11 INTENTIONALLY LEFT BLANK...

Страница 161: ...bar The forward lift struts and the leading edge of the horizontal or vertical stabilizer may also be used for moving the aircraft Pushing or pulling on the propeller is not recommended 8 2 2 TIE DOW...

Страница 162: ...he cowl Determine oil level by reading the markings on the dipstick Recommended quantity is 5 quarts With the spin on oil filter option the maximum oil change interval is every 50 hours Otherwise the...

Страница 163: ...approximately 2 3 full to leave space for the reservoir cap when it is installed 8 3 4 AIR FILTER Approved Air Filter Cub Crafters Part Number SC54108 001 Visually inspect air filter Depending on the...

Страница 164: ...C11 100 REPORT SC10000AFM Issued 11 26 08 Page number 8 4 Date of revision 10 31 11 8 4 2 INTERIOR A damp rag is typically adequate for cleaning the interior of the aircraft The windows and windshield...

Страница 165: ...SC10000AFM Date of Revision 03 13 12 Page Number 9 0 i TABLE OF CONTENTS SECTION 9 SUPPLEMENTS 9 0 GENERAL 9 1 STRAIGHT AND AMPHIBIOUS FLOATS 9 1 1 9 2 SINGLE PLACE CONVERSION 9 2 1 9 3 CONVERSION TA...

Страница 166: ...SECTION 9 0 CUB CRAFTERS SUPPLEMENTS CC11 100 REPORT SC10000AFM Issued 10 31 11 Page Number 9 0 ii Date of Revision 03 13 12 INTENTIONALLY LEFT BLANK...

Страница 167: ...rplanes equipped with one or more of the optional systems These systems are not part of the standard package In addition this section contains forms for the owner operator to report service difficulti...

Страница 168: ...SECTION 9 0 CUB CRAFTERS SUPPLEMENTS CC11 100 REPORT SC10000AFM Issued 10 31 11 Page Number 9 0 iv Date of Revision 03 13 12 INTENTIONALLY LEFT BLANK...

Страница 169: ...OF REVISIONS Current revisions to the Pilot s Operating Handbook and Flight Training Supplement Section 9 1 Rev Pages Description of Revision NC ALL Initial Release A ALL Added 1500A Amphibious infor...

Страница 170: ...SECTION 9 1 CUB CRAFTERS SUPPLEMENT FLOATS CC11 100 REPORT SC10000AFM Issued 04 15 09 Page Number 9 1 2 Date of Revision 04 09 13 INTENTIONALLY LEFT BLANK...

Страница 171: ...t Section 2 of this Pilot s Operating Handbook 9 1 2 FUEL QUANTITY INDICATORS To determine the fuel quantity when equipped with floats use the fuel quantity indication for level flight Fuel indication...

Страница 172: ...operating limitations instrument markings color coding and basic placards for operation that are specific to the Cub Crafters CC11 100 when equipped with floats Please refer to Section 2 of this manu...

Страница 173: ...speed VA at 1430 lb 97 84 Maximum Flap Speed VFE flaps 50 81 70 Best Rate of Climb Speed VY at 1430 lb 71 62 Best Angle of Climb Speed VX at 1430 lb 50 43 Maximum Demonstrated Crosswind Velocity 11 kt...

Страница 174: ...mber 9 1 6 Date of Revision 04 09 13 9 1 4 4 PLACARDS Locate near water rudder retraction handle stowage hook Next to the water rudder retraction handle On the landing gear handle Amphibious Only LAND...

Страница 175: ...that is not readily adaptable to a checklist format or which the pilot could not be expected to refer to in an emergency situation This information should be reviewed regularly Pilots must familiarize...

Страница 176: ...5 3 1 Emergency Landing on Water without Engine Power INDICATED AIRSPEED IAS MPH KNOTS Approach flaps up VG 68 59 Seat Belts Tight and secure When landing area assured Flaps As required Gear Amphibiou...

Страница 177: ...op Magnetos Ignition Off Master Switch Off Fuel Selector Off If time permits check GPS or charts for suitable landing areas in the immediate vicinity If possible notify your difficulty and intentions...

Страница 178: ...escent will be approximately 890 feet per minute Most GPS devices have a Direct to function that shows the closest airports Use charts to assess the topography of airports in the immediate vicinity 9...

Страница 179: ...econd part amplifies the information given in the checklists It provides the pilot with detailed descriptions that will help him her understand the procedures and techniques This section contains comp...

Страница 180: ...cations for float operation Mixture Idle cut off Carburetor Heat Cold Magnetos Ignition Off Ignition Backup Battery Normal Electrical Switches Off Landing Gear Amphibious Only Up for Water Down for La...

Страница 181: ...Nose Gear Amphibious Only Check Float Check for damage and water accumulation use bilge pump as necessary Bilge Rubber Plugs Secure Oar Check stowed and secure Float Hatches Cargo secure and hatches l...

Страница 182: ...plugs which serve as stoppers on the standpipe in each float compartment and pump out any accumulation of water Reinstall rubber plugs with enough pressure for a snug fit Bilge Rubber Plugs Secure Fue...

Страница 183: ...4 7 Startup and Taxi Preflight Inspection Complete Pilot Seat Adjusted Seat Belts Fastened Passenger Briefing Complete Door Closed Fuel Selector Both Avionics Master Switch Off Water Rudders Down for...

Страница 184: ...ires Mixture Rich Throttle Retard to 1200 RPM Oil Pressure Check Lights As required Avionics Master Switch On 9 1 6 4 10 Warm up Throttle 1000 to 1200 RPM 9 1 6 4 11 Taxiing Taxi Area Clear Throttle A...

Страница 185: ...gh altitudes for peak RPM 9 1 6 4 13 Takeoff Water Rudders Check Up Landing Gear Amphibious Only Up for Water Down for Land Control Stick Full Aft Throttle Full Control Stick Move forward On water whe...

Страница 186: ...Carburetor Heat As required 9 1 6 4 17 Approach Fuel Selector Both Seat Belts Fastened Mixture Set Flaps Set INDICATED AIRSPEED IAS MPH KNOTS Maximum speed first notch flaps 15 85 74 Maximum speed 15...

Страница 187: ...imum speed first notch flaps 15 85 74 Maximum speed 15 81 70 Trim As required Speed As required A higher speed than normal is recommended Water Rudders Check up Landing Gear Amphibious Only Up for Wat...

Страница 188: ...f gravity relative to the datum It also describes how to calculate the empty weight of the aircraft based on data for the landplane Should it be necessary to weigh the aircraft on floats please consul...

Страница 189: ...or concern in values listed performing an actual weight and balance is recommended Item Weight lb Arm in Straight floats with attachment gear oar and bilge pumps 195 approx 81 5 Rudder Bar and Springs...

Страница 190: ...late the takeoff weight 4 Add the moments to compute the total moment 5 Divide the moment by the takeoff weight This is the final position of the center of gravity 6 Plot the point on Figure 9 1 2 If...

Страница 191: ...cargo compartment 100 lb max 110 40 Extended cargo compartment 60 lb max 138 40 Takeoff weight Table 9 1 4 Weight and Balance Loading Form with Floats Extended Cargo Compartment Figure 9 1 2 Weight a...

Страница 192: ...CLIMB Pressure Altitude ft IAS Rate of Climb MPH Knots 1 000 70 61 1426 2 000 70 61 1359 3 000 70 61 1292 4 000 71 62 1225 5 000 71 62 1158 6 000 71 62 1091 7 000 71 62 1024 8 000 72 63 957 9 000 72 6...

Страница 193: ...e of Revision 10 31 11 Page Number 9 2 1 9 2 SINGLE PLACE CONVERSION LOG OF REVISIONS Current revisions to the Pilot s Operating Manual and Flight Manual Section 9 2 Rev Pages Description of Revision...

Страница 194: ...SECTION 9 2 CUB CRAFTERS SUPPLEMENT SINGLE PLACE CONVERSION CC11 100 REPORT SC10000AFM Issued 04 15 09 Page Number 9 2 2 Date of Revision 10 31 11 INTENTIONALLY LEFT BLANK...

Страница 195: ...ace to a two place configuration as described in this supplement as long as it meets the empty weight requirements for that configuration per Section 9 2 2 2 This may be useful for owners operators to...

Страница 196: ...table below The aircraft must always comply with the weights shown below Max Empty Weight CC340 Engine Configuration Wheels Skis 900 lbs Two Place Wheels Skis 1090 lbs Single Place Floats 1010 lbs Two...

Страница 197: ...CE Install rear seat Remove the rear stick stub cover and install rear stick if desired Remove the placard governing single place operation only The aircraft maximum empty weight configuration is show...

Страница 198: ...s stowed and not removed remove this from your calculations If any changes are made for main gear or tailwheel the main gear arm is 62 5 inches and the tailwheel arm is 261 9 inches Item Weight lbs Mo...

Страница 199: ...R STICK COVER 1 Loosen and remove the AN3 bolt washers and AN365 lock nut holding the rear stick into the rear stick stub 2 For first time installation remove floor fasteners and install the rear stic...

Страница 200: ...the stick cover install the fasteners back into the floorboard Install the rear stick and torque the fastener to 43 48 in lbs Ensure full range of motion including trim is met without the rear stick c...

Страница 201: ...oss bar out of the rear seat cross bar sleeves and the nylon straps Remove the seat cushion from the rear seat Fold the rear seat for stowage above the Sling Seat Holder also stores the Pilot s Operat...

Страница 202: ...ing seat holder 6 If the seat is completely removed from the aircraft loosen the two straps at the top of the seat and remove the seat and rear seat cross tube If removed note that the 6 15 lbs includ...

Страница 203: ...TABLES Issued 10 31 11 REPORT SC10000AFM Date of Revision N A Page Number 9 3 1 9 3 CONVERSION TABLES LOG OF REVISIONS Current revisions to the Pilot s Operating Manual and Flight Manual Section 9 3 R...

Страница 204: ...SECTION 9 3 CUB CRAFTERS SUPPLEMENT CONVERSION TABLES CC11 100 REPORT SC10000AFM Issued 10 31 11 Page Number 9 3 2 Date of Revision N A INTENTIONALLY LEFT BLANK...

Страница 205: ...916 40 370 90 40 823 41 277 41 731 42 184 42 638 43 091 43 545 43 999 44 452 44 906 100 45 359 45 813 46 266 46 720 47 174 47 627 48 081 48 534 48 988 49 442 9 3 2 LENGTH FEET INTO METERS PIEDS EN ME...

Страница 206: ...8 246 4 248 9 251 5 100 254 0 256 5 259 1 261 6 264 2 266 7 269 2 271 8 274 3 276 9 9 3 3 VOLUME GALLONS INTO LITERS GALLONS EN LITRES Gal 0 1 2 3 4 5 6 7 8 9 Liters Liters Liters Liters Liters Liters...

Страница 207: ...00 25 60 26 10 80 26 70 27 20 27 80 28 30 28 90 29 40 30 00 30 60 31 10 31 70 90 32 20 32 80 33 30 33 90 34 40 35 00 35 60 36 10 36 70 37 20 100 37 80 38 30 38 90 39 40 40 00 40 60 41 10 41 70 42 20 4...

Страница 208: ...3 9 74 7 75 6 76 5 77 3 90 78 2 79 1 79 9 80 8 81 7 82 6 83 4 84 3 85 2 86 0 100 86 9 87 8 88 6 89 5 90 4 91 2 92 1 93 0 93 8 94 7 110 95 6 96 5 97 3 98 2 99 1 100 0 100 8 101 7 102 5 103 4 120 104 3...

Страница 209: ...Issued N A REPORT SC10000AFM Date of Revision 10 31 11 Page Number 9 4 1 9 4 FORMS LOG OF REVISIONS Current revisions to the Pilot s Operating Handbook and Flight Training Supplement Section 9 4 Rev P...

Страница 210: ...SECTION 9 4 CUB CRAFTERS SUPPLEMENT FORMS CC11 100 REPORT SC10000AFM Issued 04 15 09 Page Number 9 4 2 Date of Revision 10 31 11 INTENTIONALLY LEFT BLANK...

Страница 211: ...CUB CRAFTERS SECTION 9 4 CC11 100 SUPPLEMENT FORMS Issued N A REPORT SC10000AFM Date of Revision 10 31 11 Page Number 9 4 3 9 4 1 CHANGE OF ADDRESS OWNERSHIP...

Страница 212: ...SECTION 9 4 CUB CRAFTERS SUPPLEMENT FORMS CC11 100 REPORT SC10000AFM Issued 04 15 09 Page Number 9 4 4 Date of Revision 10 31 11 INTENTIONALLY LEFT BLANK...

Страница 213: ...CUB CRAFTERS SECTION 9 4 CC11 100 SUPPLEMENT FORMS Issued N A REPORT SC10000AFM Date of Revision 10 31 11 Page Number 9 4 5 9 4 2 CONTINUED OPERATIONAL SAFETY REPORTING...

Страница 214: ...SECTION 9 4 CUB CRAFTERS SUPPLEMENT FORMS CC11 100 REPORT SC10000AFM Issued 04 15 09 Page Number 9 4 6 Date of Revision 10 31 11 INTENTIONALLY LEFT BLANK...

Страница 215: ...SUPPLEMENTS TWO SWITCH ELEVATOR TRIM SYSTEM Issued 03 13 12 REPORT SSC100000AFM Date of revision N A Page number 9 5 1 9 5 1 TWO SWITCH ELEVATOR TRIM SYSTEM LOG OF REVISIONS Rev Pages Description of...

Страница 216: ...SECTION 9 CUB CRAFTERS SUPPLEMENTS TWO SWITCH CC11 100 ELEVATOR TRIM SYSTEM REPORT SSC100000AFM Issued 03 13 12 Page number 9 5 2 Date of revision N A INTENTIONALLY LEFT BLANK...

Страница 217: ...t contained in this supplement consult section 2 of this Pilot s Operating Handbook and FAA Approved Airplane Flight Manual This supplement must remain in the handbook at all times when the Two Switch...

Страница 218: ...9 CUB CRAFTERS SUPPLEMENTS TWO SWITCH CC11 100 ELEVATOR TRIM SYSTEM REPORT SSC100000AFM Issued 03 13 12 Page number 9 5 4 Date of revision N A Figure 1 Switches on control sticks Figure 2 Trim Selecto...

Страница 219: ...uld the elevator trim system begin to move without being operated intentionally switch the selector switch on the left wing root panel to the OFF position middle position Figure 2 9 5 5 NORMAL PROCEDU...

Страница 220: ...balance information in section 6 of the Pilot s Operating Handbook If it was retrofitted to the aircraft the installation instructions provided by Cub Crafters will have the appropriate weight informa...

Страница 221: ...FRONT position to avoid inadvertent operation by an occupant in the aft seat Similarly if the switch is in the REAR position operation by the aft occupant will take priority over operation by the for...

Страница 222: ...SECTION 9 CUB CRAFTERS SUPPLEMENTS TWO SWITCH CC11 100 ELEVATOR TRIM SYSTEM REPORT SSC100000AFM Issued 03 13 12 Page number 9 5 8 Date of revision N A INTENTIONALLY LEFT BLANK...

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