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Caproni Vizzola C22J, Руководство по эксплуатации самолета

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CAPRONI VIZZOLA 
C 22 J 

5-5 

 

5.5.

 

TAKE-OFF DISTANCE OVER 50 FT OBSTACLE 

Air Temperature 

20°C 

Altitude 

2000 ft 

Takeoff Weight 

1175 Kg 

Wind 

5 Kt Head 

Takeoff Distance 

920 m 

 

5.6.

 

CLIMB PERFORMANCE 

5.6.1.

 

Best Rate of Climb Speed 

–

 Flaps Down 

Thrust 

Continuous (100%) 
2 engines 

Flaps 

Down 

Airbrakes 

Closed 

Landing Gear 

Retracted 

Weight 

Maximum Takeoff 

Atmosphere 

ISA Standard Day 

 

 

 

0

2500

5000

7500

10000

12500

110

120

130

140

PRE

SSU

RE

 ALT

IT

U

DE

 -

FE

ET

BEST RATE OF CLIMB SPEED

IAS - KNOTS

Содержание C22J

Страница 1: ...______ Type Certificate NO _____________ THIS HANDBOOK INCLUDES THE MATERIAL REQUIRED TO BE FURNISHED TO THE PILOT BY REGRISTRO AERONAUTICO ITALIANO REGULATIONS AND ADDITIONAL INFORMATION PROVIDED BY...

Страница 2: ...ABLE OF CONTENTS SECTION 1 General 1 1 SECTION 2 Limitations 2 1 SECTION 3 Emergency Procedures 3 1 SECTION 4 Normal Procedures 4 1 SECTION 5 Performance 5 1 SECTION 6 Weight and Balance 6 1 SECTION 7...

Страница 3: ...1 1 SECTION 1 GENERAL 1 1 Notes to Users 1 2 1 2 Dimensions And Areas 1 2 1 3 Engines 1 3 1 4 Fuel 1 4 1 5 Oil 1 5 1 6 Weights 1 5 1 7 Specific Loading 1 5 1 8 Baggage compartment 1 5 1 9 Definitions...

Страница 4: ...irworthiness is required to be carried this flight manual must also be aboard the aeroplane as it is an essential part of the above mentioned certificate Applicability Application of this flight manua...

Страница 5: ...bo c Engine Model Number TRS 18 1 202 d Take Off Thrust 145 daN e Engine RPM at Take Off 48750 f Maximum Continuous Thrust 130 daN g Engine RPM 47000 h Engine type Compressor stages and Type 1 centrif...

Страница 6: ...ification FUEL TYPE NATO CODE SPECIFICATIONS COMMERICAL DENOMINATION FRANCE U K Kerosene 50 C S 7 48 F 34 AIR 3405 C F 34 D Eng RD 2453 Fuel TRO Kerosene JP 5 AVTUR FS II with antifreeze additive MIL...

Страница 7: ...e US Gal lit 0 211 0 8 b Usable Oil US Gal lit 0 132 0 5 c Oil Specification MIL L 23699 or MIL L 7808 1 6 WEIGHTS Lb Kg a Maximum Take Off Weight 2764 1255 b Maximum Landing Weight 2582 1172 c Maximu...

Страница 8: ...hich application of full available aerodynamic control will not overstress the airplane VFE Maximum Flap Extended Speed is the highest speed permissible with wing flaps in a prescribed extended positi...

Страница 9: ...ea level is 29 92 In Hg 1013 2 mb The temperature gradient from sea level to the altiutude at which temperature is 56 5 C 69 7 F is 0 00198 C 0 003564 F per foot and zero above that altitude OAT Outsi...

Страница 10: ...onstrated during certification tests Is not considered a limitation f Weight and Balance REFERENCE DATUM An imaginary vertical plane from which all horizontal distances are measured for balance purpos...

Страница 11: ...e Equipment List BASIC EMPTY WEIGHT Standard Empty Weight plus optional equipment actually installed PAYLOAD Weight of occupants Cargo and baggage USEFUL LOAD Difference between takeoff weight and bas...

Страница 12: ...t Limitations 2 4 2 5 POwerplant Instrument Markings 2 6 2 6 Weight Limits 2 6 2 7 Center of gravity limits 2 7 2 8 Maneuvers Limits 2 8 2 9 Flight Maneuvering Load Factor Limits 2 8 2 10 Flight Crew...

Страница 13: ...vering Speed VA Knots 228 231 Do not make full or abrupt control movements above this speed Maximum Flap Extended Speed VFE Knots 150 152 Do not exceed this speed with a given flap setting Maximum Lan...

Страница 14: ...CAPRONI VIZZOLA C 22 J 2 3 Figure 2 2 Airspeed Limitation with Altitude VMO 260 10700 ft 0 5 10 15 20 25 30 0 50 100 150 200 250 300 Altitude x1000 ft IAS Knots...

Страница 15: ...Red Lines 260 0 48 Maximum Speed for all operations VMO MMO Figure 2 3 Airspeed Indicator Markings NOTE The Flight Simulator model depicts the Airspeed indicator as mounted in the prototype airframes...

Страница 16: ...CAPRONI VIZZOLA C 22 J 2 5 Figure 2 5 Operating Envelope...

Страница 17: ...3699B or MIL L 7808 h Ambient Temperature Limitations Maximum atmospheric Temperature at which compliance with cooling requirements is shown 37 8 C 100 F 2 5 POWERPLANT INSTRUMENT MARKINGS Meaning of...

Страница 18: ...imum takeoff weight 97 02 in 2464 mm aft of Datum at 2588 pounds 1172 Kg or less The chord is 35 433 in 900 mm long NOTES Straight line variation between points indicated The Datum is located 82 677 i...

Страница 19: ...oad Factor Flaps Down and or Airbrakes Open 3 5 g 2 10 FLIGHT CREW Minimum Crew One Pilot 2 11 KINDS OF OPERATION The standard airplane is approved for day and night operations under VFR conditions pr...

Страница 20: ...00 ft is approved if the aircraft is equipped with oxygen in accordance with the applicable operational rules 2 14 SEATING LIMITATION The maximum number of occupants is two including the pilot Pilot m...

Страница 21: ...CAPRONI VIZZOLA C 22 J 2 10...

Страница 22: ...CAPRONI VIZZOLA C 22 J 2 11...

Страница 23: ...CAPRONI VIZZOLA C 22 J 2 12 On Baggage Compartment On canopy Ceiling Calibration placard for magnetic compass...

Страница 24: ...APRONI VIZZOLA C 22 J 3 1 SECTION 3 EMERGENCY PROCEDURES 3 1 Introduction 3 2 3 2 Ground Operation Emergencies 3 2 3 3 Takeoff emergencies 3 3 3 4 In Flight Emergencies 3 5 3 5 Landing Emergencies 3 9...

Страница 25: ...landing should be accomplished at the nearest suitable airfield considering the severity of the emergency weather conditions field facility lighting A C gross weight Land As Soon As Practical Emergenc...

Страница 26: ...raft is on the ground 3 3 1 Engine Fire Before rotation 1 Throttles IDLE 2 Engine MAST both OFF 3 Brakes APPLY 4 BATT switch OFF 3 3 2 Engine Failure before rotation speed below 78 Knots 1 Throttles I...

Страница 27: ...FE ALTITUDE IS REACHED 6 Inoperative engine MASTER OFF 7 Operative engine throttle 100 8 Flaps UP 9 Accelerate to 115 KIAS Land as soon as practical 3 3 5 Tire blowout at takeoff IF IT IS POSSIBLE TO...

Страница 28: ...condition should be indicated by the FUEL PRESS indicator The engine failure does not cause sudden directional variation of this airplane The pilot must decide on the action to be undertaken To resta...

Страница 29: ...ition 5 Land as soon as possible If light remains ON on the corresponding engine 4 Engine MAST OFF 5 BOOST pump OFF 6 Fuel shut off light check SHUT If fuel shut off light OPEN is ON 7 Shut off switch...

Страница 30: ...or fumes persist 5 Oxygen Mask Wear 6 Diluter 100 not simulated If no reduction of smoke is observed 7 Land as soon as possible 3 4 3 Electrical System Failure 3 4 3 1 Single Generator Failure The Fa...

Страница 31: ...e 3 4 4 Fuel System Failure 3 4 4 1 Hight Fuel Pressure warning light lighted 1 Throttle Reduce If light is still on 2 Descend as low as practical If light is still on 3 Land as soon as practical 3 4...

Страница 32: ...he tendency of the airplane to pitch up The airplane is easily controllable by applying a pitch down control force The force depends on the speed the higher the speed the higher the force being very l...

Страница 33: ...gear DOWN 3 Airspeed 105 KIAS 4 Airbrakes as required After touchdown 5 Throttles IDLE 6 Airbrakes OPEN 7 Brakes Apply as required 3 5 5 Emergency Landing Gear Extension 1 Airspeed below 120 KIAS 2 F...

Страница 34: ...witch OFF 8 Contact runway at speed as slow as possible 9 After a complete stop Abandon A C In case of unsafe nose gear 1 Land in nose up attitude 2 Control stick aft to hold nose up as long as possib...

Страница 35: ...CTION 4 NORMAL PROCEDURES 4 1 General 4 2 4 2 Preparation for flight 4 2 4 3 Pre Flight Check 4 2 4 4 Take Off Checks 4 10 4 5 In Flight Checks 4 11 4 6 Post Flight Checks 4 12 4 7 Oxygen System 4 12...

Страница 36: ...e The figures are for standard airplanes flown at maximum gross weight under normal conditions at sea level KIAS Best Rate of Climb Speed Flaps Up 157 Best Rate of Climb Speed with one engine inoperat...

Страница 37: ...ydraulic fluid oil and fuel leaks as well as for the following Figure 4 1 Walk Around A NOSE 1 Canopy CLOSED 2 External Canopy Handle LOCKED 3 Left Static Port Clean and free from obstructions 4 Winds...

Страница 38: ...ire Condition inflation and alignment of slippage marks 3 Landing Gear Leg Condition 4 Fuse Bolts Condition 5 Brake and line Condition 6 Landing Gear Bottom Door Condition and Locked 7 Landing Gear La...

Страница 39: ...ding Gear Lateral Door Condition H LEFT WING 1 Wing Flap Condition and free play 2 Airbrake Condition 3 Aileron Condition 4 Antenna Lower side Condition and security 5 Tip Tank Cocks Closed Check for...

Страница 40: ...control CLOSED 21 Defogger CLOSED 22 Throttle Friction Adjust 23 Throttle IDLE 24 Emergency Throttle Fully counter clockwise CAUTION If the throttle is not in the idle position after the startup the e...

Страница 41: ...sed to be present in the combustion chamber such as after an aborted starting 1 Engine MAST switches Check OFF 2 VENT button keep depressed as long as necessary max 10 Sec 4 3 5 Starting the Left Engi...

Страница 42: ...Check within limits 4 3 7 Emergency engine control box check This check must be performed at the first flight of the day 1 Left Throttle IDLE 2 L TEST switch ON 3 PUMP NORM L light Check ON 4 Left Eme...

Страница 43: ...ght throttle Advance for 100 RPM 23 Fuel Pressure Check within limits 0 95 bar min 24 Right Throttle IDLE 25 R BOOST PUMP ON Figure 4 2 Speed Limitation in function of Air Intake temperature 4 3 9 Bef...

Страница 44: ...Free 2 Trim Set for takeoff position 3 Airbrakes Check closed 4 Flaps Set DOWN 5 Engine instruments Check within green sectors 6 Flight Instruments Check 7 Fuel quantity Check 8 Safety Harness LOCKED...

Страница 45: ...Before Landing NOTE Airbrake must be deployed after flaps lowering to avoid lift drop in case of airbrake retraction Airbrakes down and flaps up is not a normal approach configuration 1 Speed Reduce t...

Страница 46: ...F 4 Attitude Indicator OFF 5 Turn Slip Indicator OFF 6 Internal External Lights OFF 7 L R BOOST pumps OFF 8 Stabilize EGT Check 9 Engine MAST OFF 2 10 Engine turn to stop 52 20 CHECK 11 Battery OFF 4...

Страница 47: ...ks are not part of the aircraft they are part of the crew equipment 4 8 SPIN CHARACTERISTICS 4 8 1 Spin The aircraft has been approved for intentional spin with gear and flaps up only Spins in any oth...

Страница 48: ...e nose moves down Release the stick forward to neutral position and centralize the rudder control The aircraft will recover from the spin within turn after neutral stick is applied CAUTION The stick s...

Страница 49: ...ZZOLA C 22 J 5 1 SECTION 5 PERFORMANCE 5 1 General 5 2 5 2 Summary of Required Performance 5 2 5 3 Wind Component 5 2 5 4 Stall Speeds 5 4 5 5 Take Off Distance over 50 ft Obstacle 5 5 5 6 Climb Perfo...

Страница 50: ...RFORMANCE The following Performance figures are based on measured Flight Test Data corrected to I S A Standard Day conditions and to the Maximum Takeoff Weight for takeoff data and to the maximum land...

Страница 51: ...CAPRONI VIZZOLA C 22 J 5 3 Figure 5 1...

Страница 52: ...m Altitude loss during stall recovery is approximately 400 ft 2 Maximum nose down pitch attitude and altitude loss recover from single engine stalls are approximately 20 and 400 feet respectively 3 Ef...

Страница 53: ...5 Kt Head Takeoff Distance 920 m 5 6 CLIMB PERFORMANCE 5 6 1 Best Rate of Climb Speed Flaps Down Thrust Continuous 100 2 engines Flaps Down Airbrakes Closed Landing Gear Retracted Weight Maximum Take...

Страница 54: ...eed Flaps Down Thrust Continuous 100 2 engines Flaps Down Airbrakes Closed Landing Gear Retracted Weight Maximum Takeoff Atmosphere ISA Standard Day 0 2500 5000 7500 10000 12500 100 110 120 130 PRESSU...

Страница 55: ...Climb Speed Flaps Up Thrust Continuous 100 2 engines Flaps Up Airbrakes Closed Landing Gear Retracted Weight Maximum Takeoff Atmosphere ISA Standard Day 0 5000 10000 15000 130 140 150 160 PRESSURE ALT...

Страница 56: ...limb Speed Flaps Up Thrust Continuous 100 2 engines Flaps Up Airbrakes Closed Landing Gear Retracted Weight Maximum Takeoff Atmosphere ISA Standard Day 0 5000 10000 15000 130 140 150 160 PRESSURE ALTI...

Страница 57: ...Fig 5 3 Associated Conditions Thrust Continuous 100 Flaps Up Best Rate of Climb Speed 124 KIAS at Sea Level 114 KIAS at 14000 ft Linear variation between S L and 14000 ft Example Outside Air Temperat...

Страница 58: ...CAPRONI VIZZOLA C 22 J 5 10 Figure 5 3...

Страница 59: ...Angle of Climb Speed Flaps and Landing Gear Down Thrust Continuous 100 2 engines Flaps Down Airbrakes Closed Landing Gear Extended Weight Maximum Takeoff Atmosphere ISA Standard Day 5000 ft Altitude S...

Страница 60: ...CAPRONI VIZZOLA C 22 J 6 1 SECTION 6 WEIGHT AND BALANCE 6 1 Introduction 6 2 6 2 Weight and Balance Determination for Flight 6 2...

Страница 61: ...puting the total weight and moment and then determining whether they are within the approved envelope 6 2 WEIGHT AND BALANCE DETERMINATION FOR FLIGHT NOTE It is the responsibility of the pilot and air...

Страница 62: ...s loaded properly Note 1 The influence on C G is negligible Figure 6 2 Figure 6 3 Center of Gravity Envelope NOTE This Flight Simulator Model provides an automated version of the Load Form in the docu...

Страница 63: ...IZZOLA C 22 J 7 1 SECTION 7 PANEL SYSTEMS MANUAL 7 1 Main Instrument Panel 7 2 7 2 Lower Panel between seats 7 14 7 3 GPS Panel Error Bookmark not defined 7 4 Checklist Panel 7 14 7 5 General System N...

Страница 64: ...tor model some controls may require additional explanation Toggle Switches Left Click Multi Position switches Knobs Left Click Mouse Wheel Knobs Levers Left Drag Mouse Wheel Rotary knobs Left Click Mo...

Страница 65: ...rce 10 Attitude Indicator 30 Landing Light Switch 49 Pedal Adjust Handle RH 11 Course Indicator HSI 31 Landing Gear Lever 50 GEN Arm Button 12 Altimeter 32 LH RH Gen Switches 51 Instrument Lights Pote...

Страница 66: ...ive g units and from 0 to 4 negative g units A PUSH TO SET knob on the lower left side of the instrument allows zero setting of the maximum positive and negative g units displayed 7 1 8 Airspeed Indic...

Страница 67: ...elected Course Arrow It indicates the selected VOR radial or ILS localizer course Aircraft position in relation to a VOR radial or the localizer beam is represented by the relative position of the min...

Страница 68: ...offline GEN R No 1 or Right Hand Generator offline OIL L Left engine oil pressure Refer to 7 1 42 OIL R Right engine oil pressure Refer to 7 1 42 LOW P Pressure in the collector tank is below 0 1 bar...

Страница 69: ...R knob is located on the lower left side of the control panel and is labelled STORE SELECT RECALL It is used to control the single channel memory When in SELECT position a desired frequency may be may...

Страница 70: ...windows located each above the corresponding knob 7 1 25 ADF equipment The RCR 650 A ADF receiver is fitted with the following controls and indications VOL ID CONTROL KNOB when rotated fully contracl...

Страница 71: ...green GEN label illuminates Pressing the button attempts to bring the respective generator online or disconnects it if online The GEN ARM pushbutton needs to be pressed if a generator has been manuall...

Страница 72: ...g these switches toggles ON OFF the respective engine electric fuel boost pump 7 1 37 Eng Master Switches ON L MAST ON R MAST Engine Master Switches When electrical power is available to the main bus...

Страница 73: ...al display labelled V A A selector knob labelled V A controls the V A display The selector has 4 positions from left to right 1 LH system Volts 2 RH System Volts 3 LH System Amperes 4 RH system Ampere...

Страница 74: ...position toggle switch labelled NM KTS and MIN In the NM position distance from the station in nautical miles is displayed to a maximum of 199 9 nautical miles The KTS position displays ground speed...

Страница 75: ...mediate flap position may be selected In this simulation the switch is operated by clicking UP or DOWN The mouse wheel may also be used Standard Flight simulator Flap commands are also usable 7 1 53 L...

Страница 76: ...s running and aircraft flying In this simulation windshield ice may form under rainy conditions if external temperature is low enough Operating this control will reverse the icing process 7 2 3 Emerge...

Страница 77: ...tion 7 4 2 Heating system Windshield frosting is simulated Operate the Windshield Defrost lever as required 7 4 3 Flight Controls In this aircraft airbrakes provide positive lift They shall be deploye...

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